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Surveillance
Category of spacecraft.
Subtopics
| CBNT Surrey Satellite Technology experimental imaging satellite. SSTL did not disclose the meaning of the CBNT abbreviation. 22:10 local time longitude of descending node sun synchronous orbit. Technology satellite for SSTL, UK. Launched 2015. |
| Daichi-2 Advanced Land Observing Satellite 2, placed in a noon/midnight sun-synchronous orbit. Carried the PALSAR-2 radar imager with 1 to 3 meter resolution in spotlight mode and 3 to 10 m in high resolution mode. |
| JB-3 Chinese sun synchronous orbit military reconnaisance satellite. Built by CAST, it used a BISME (Beijing Institute of Space Mechanics and Electronics) optical sensor. |
| Jilin One of two 'smart video imaging' satellites in the Jilin cluster. |
| Aist Small satellite developed by TsSKB-Progress and the Samara Aerospace University; carried a magnetometer, acclerometers and a micrometeor experiment. Technology satellite built by Samara Aerospace University, TsSKB-Progress for Samara Aerospace University, Russia. Launched 2013. |
| Bars Believed to be a new-generation electro-optical reconnaisance satellite based on a heavily modified Yantar bus. Placed in sun synchronous orbits. Reconnaissance, opticalsatellite built by TsSKB-Progress (bus), LOMO (payload) for VKO. Used Yantar bus. |
| BCP-2000 American Ball satellite bus in the 1000-kg class to accommodate high-precision optical surveillance payloads. |
| CAST1000 The CAST1000 bus was a microsatellite class (30-200 kg) platform designed to satisfy missions including earth observation, atmospheric exploration, electromagnetic exploration, technological demonstration, on-orbit service, and LEO communication, while supporting use in satellite constellations
and formation flying. |
| CAST2000 The CAST2000 bus was in the minisatellite class (200-400 kg bus mass; 300-600 kg payload capacity). It was designed for diverse missions, including earth observation, technological demonstration, scientific exploration, earth environmental exploration, formation flight and networking, meteorological research and application, communications, and navigation. |
| CAST3000 The CAST3000 satellite bus was designed for high resolution optical imaging and radar imaging missions in sun synchronous orbit. It could be adapted to other missions. The bus had a mass of 400 kg and could support payloads of up to 400 kg requiring 1100 W of power. |
| ChubuSat A project of Nagoya and Daido universities. (The name Kinschachi refers to the golden sea-monster statues on Nagoya castle). It carries d 10m resolution, 14 km swath imager, a 130 m resolution, 7-13 micron infrared camera reported to be for atmosphere temperature profiles and space debris monitoring, and an amateur radio relay payload. Sun synchronous orbit; 1055 GMT local time of the descending node. Technology satellite for Nagoya University, Daido University, Japan. Launched 2016. |
| EIS Secret payload for the National Reconnaissance Office; thought to be an imaging spy satellite of the EIS/Enhanced CRYSTAL type. Reconnaissance, electro-opticalsatellite built by Lockheed Martin for NRO. Used Bus-1. |
| Fajr Fourth Iranian satellite, and Iran's first successful orbital launch since February 2012. Fajr (Aurora) had a technology payload with a cold-gas thruster developed by Iran Electronics Industries. There is suggestive evidence (mostly based on satellite imagery of launch pad
damage revealed by the magazine Jane's Intelligence Review) that Iran had two launch failures in 2012, as well as more speculative evidence of further launch failures since then. The satellite did not seem to make any orbital maneuvers. The orbit decayed from an initial 223 km x 470 km to 196 km x 293 km by February 22, and then after falling to 134 km x 155 km early on February 26 it reentered. The Safir rocket stage orbit decayed a bit more slowly, and was at 203 km x 325 km on Feb 26. Technology satellite built by IEI (Iran Electronics Industry), Iran. Launched 2012 - 2015. |
| Hodoyoshi Satellite of the University of Tokyo and AXELSPACE, carried an imager with 6.8m resolution and 28 km swath. Sun synchronous orbit; 1100 GMT local time of the descending node. Technology, Earth observation satellite for University of Tokyo, NESTRA, Japan. Launched 2014. |
| Intruder Intruder was a naval electronic intelligence satellite for the National Reconnaissance Office (NRO). |
| Kanopus Remote sensing satellite. Imager provided a resolution of 2.5 m in a 20 km swath and 12.5 m in four spectral channels along the same swath. A separate imager provided optical resolution of 25 m in a 250 km swath. Earth Observation satellite built by NPP VNIIEM for Roskosmos, Russia. Launched 2012. Used Kanopus bus. |
| LEOStar-2 ?Civil or defense satellite bus for use in ?LEO orbit and launch by ?Pegasus or Minotaur I, IV or C. Lifetime ??1-5 years and delivery possible ?16-36 months after receipt of order. Electrical system solar cells, average power 750W |
| NEXTAR NX-300L High resolution imaging satellite developed by NEC and managed by Japan Space Systems (formerly USEF, part of the Ministry of Trade and Industry) rather than by the main Japanese space agency JAXA. The ASNARO had 0.5m resolution on a 10 km nadir swath width. |
| Oceansat Remote sensing satellite with an 8-band ocean color monitor, a radar scatterometer and a radio occultation atmospheric sounder. Earth Observing satellite for ISRO, India. Launched 2009. Used IRS-1 Bus. |
| Persona Russian sun-synchronous orbit electro-optical reconnaissance satellite first flown in 2008. Reports also gave the code name Kvarts; and it was said to utilize a LOMO-built 17V321 optical system originally developed for the Arkon satellite. There were reports that a a Yantar-derived service module was used, but an illustration published in a Russian military document showed a satellite with a new service module and cruciform solar arrays. The first Persona satellite was launched in July 2008; it reportedly malfunctioned in February 2009 due to an electronics failure. The second was not launched until June 2013. It was said to be delayed because compenents had to be cannibalized from a Resurs-P 1 satellite.This spacecraft also failed after a short time in orbit, necessitating to bring the old film-return Kobalt-M satellites into service to bridge the gap. Reconnaissance, optical satellite built by TsSKB-Progress (bus), LOMO (payload) for VKS > VKO, Russia. Launched 2008 - 2015. |
| Phoenix Eye The Phoenix Eye bus was designed for sun synchronous orbits and used in the ZY-2 and CBERS earth observation satellites. |
| Prima Satellites in the European Commission's Sentinel/Copernicus Earth observing program. |
| Proteus The Proteus (Plateforme Reconfigurable pour l'Observation, les Telecommunications Et les Usages Scientifiques) bus was developed by Thales Alenia Space in partnership with the French Space Agency CNES from 1996 to 2000. The result was design and qualification of a small and versatile satellite bus as well as a generic ground segment that could accomodate a variety of payloads. These included all types of Earth environmental and science missions; surveillance, and communications applications. |
| Quasar Classified communications and data relay satellite for the National Reconnaissance Office. |
| Satrec The South Korean Satrec Initiative built on earlier Kitsat technology to develop 100-kg and 200-kg satellite buses for national and international customers. |
| Sentinel European visible/infrared band earth observing satellite. The visible camera had a 10 metre resolution and a 290 km swath. Sun synchronous orbit; 1030 GMT local time of the descending node. |
| SI-300 Satreci South Korea imaging satellite bus. |
| SJ-11 Chinese military surveillance satellite constellation. Launched from Jiuquan by the CZ-2C launch vehicle into 690 km, 98.7 deg inclination sun synchronous orbits from 2009. Reported to carry an infrared tracking system, part of a missile-launch early warning / tracking system. Built by Dongfanghong Satellite Co., China. |
| SKRL Calibration sphere. Calibration satellite, Russia. Launched 2013. |
| SkySat Commercial imaging satellite by the US company Skybox. The satellite produced sub-meter resolution imagery and high-definition video. It could capture up to 90-second video clips at 30 frames per second. The resolution was high enough to view objects like shipping containers while maintaining not tracking human activity. Earth Observation satellite built by Skybox Imaging for Skybox Imaging, USA. Launched 2013 - 2014. |
| SSTL-300 Surrey minisatellite bus, 300 kg class. |
| Sterkh Dedicated COSPAS-SARSAT search-and-rescue satellite. Total mass 170 kg, including 55 kg payload. |
| Tianhui Mapping-1 Satellite 02; carried visible-band mapping cameras with 5 m resolution. |
| Tiantuo Technology satellite for the National University of Defense Technology; carried an payloads such as an imager, an atomic oxygen sensor, and an AIS (maritime tracking)
receiver. |
| Topaz Classified US radar satellite. |
| Trumpet Follow-on Probably a signals intelligence satellite with an attached SBIRS-HEO early warning sensor as a secondary payload. ELINT satellite for USAF, USA. Launched 2014. |
| Tsukushi 'Horsetail'; also called QSAT-EOS, Kyushu Satellite for Earth Observation System Demonstration. The satellite carried a CMOS camera with 4 m resolution and 7 km swath, a magnetometer and an in-situ space debris detector, as well as a deployable 3-meter kapton sail used as a drag augmentation device. Sun synchronous orbit; 1055 GMT local time of the descending node. |
| UGATUSAT Remote sensing satellite built by the Ufa State Aviation Technical University. Technology, Earth observation satellite for Ufimskiy Gosudarstvenniy Aviatsionniy Tekhnicheskiy Universitet, Russia. Launched 2009. |
| Pleiades French military optical reconnaisance satellite. The Pleiades constellation consists of two one metric ton satellites offering a spatial resolution at nadir of 0.7 m and a field of view of 20 km. While designed for off-nadir imaging to support rapid retasking of targets, the satellites will also offer stereoscopic capability to meet detailed cartography requirements for urban regions. Earth Observing satellite built by Astrium (prime), Alcatel for CNES, France. Launched 2011 - 2012. |
| KH-1 American military surveillance satellite. First US film reconnaissance satellite, and first polar orbiting satellite. Reconnaissance, photo (film return type) satellite built by Lockheed for USAF, USA. Launched 1959 - 1960. |
| Midas American military early warning satellite. Part of a then-secret USAF program known as WS-117L, the MIDAS (Missile Defense Alarm System) program began in November 1958. Early Warning satellite built by Lockheed (prime), Aerojet-General (payload) for USAF, USA. Launched 1962 - 1963. |
| GRAB First American military signals intelligence satellite, launched 1960-1962; not declassified until 1998. ELINT Research satellite built by Naval Research Laboratory (NRL) for Naval Research Laboratory (NRL) / US Navy, USA. Launched 1960 - 1962. |
| Samos American military surveillance satellite. First generation photo surveillance; return of camera and film by capsule; program still partially classified, evidently due to embarrassment. |
| KH-2 American military surveillance satellite. Early US reconnaissance satellite. Carried one 'C-Prime' panoramic camera, with a focal length of 61 cm and a ground resolution of 9 m. Reconnaissance, photo (film return type) satellite built by Lockheed for USAF, USA. Launched 1960 - 1961. |
| KH-5 American military surveillance satellite. US mapping satellite. Carried one frame camera, with a focal length of 76 mm, and a ground resolution of 140 m. Reconnaissance, photo (Area survey) satellite built by Lockheed for USAF, USA. Launched 1963 - 1964. |
| KH-3 American military surveillance satellite. Early US reconnaissance satellite. Carried one 'C-Double Prime' panoramic camera, with a focal length of 61 cm and a ground resolution of 7.6 m. Reconnaissance, photo (film return type) satellite built by Lockheed for USAF, USA. Launched 1961 - 1962. |
| Zenit-2 satellite Russian military surveillance satellite. The Zenit-2 was a derivative of the manned Vostok, and the Soviet Union's first spy satellite. Reconnaissance, photo (low resolution, film return type), ELINT satellite built by OKB-1 for GRU, Russia. Launched 1961 - 1970. Used Zenit bus. |
| SURCAL American military target satellite. Calibration satellite for NRL, USA. Launched 1962-1965. |
| Ferret American military signals intelligence satellite. |
| KH-4 American military surveillance satellite. Early US reconnaissance satellite. Carried two 'Mural' panoramic cameras, with a focal length of 61 cm, and a ground resolution of 7.6 m. Reconnaissance, photo (film return type) satellite built by Lockheed for USAF, USA. Launched 1962 - 1963. |
| KH-6 American military surveillance satellite. US reconnaissance satellite, lashed together to meet an emergency requirement for close-up imaging of a suspected Soviet ICBM site near Tallinn. Reconnaissance, photo satellite built by Lockheed (prime); Kodak (camera) for USAF, USA. Launched 1963. |
| SSF American military signals intelligence satellite. ELINT satellite built by Lockheed for USAF, USA. Launched 1963 - 1964. Used P-11 bus. |
| KH-7 American military surveillance satellite. US reconnaissance satellite. Still classified. Camera believed to have ground resolution of 0.46 m. Film returned in two capsules. Reconnaissance, photo (film return type) satellite built by General Electric for USAF, USA. Launched 1963 - 1967. |
| KH-4A American military surveillance satellite. Early US reconnaissance satellite. Carried two 'J-1' panoramic cameras, with a focal length of 61 cm, and a ground resolution of 2.7 m. Reconnaissance, photo (film return type) satellite built by Lockheed for USAF, USA. Launched 1963 - 1969. |
| LAMPO American military target satellite. Radar calibration satellite, USA. Launched 1963. |
| Vela American nuclear detection surveillance satellite. The Vela (meaning "watchman" in Spanish) series of spacecraft were designed to monitor world-wide compliance with the 1963 nuclear test ban treaty. Nuclear Detection satellite built by TRW for USAF, USA. Launched 1963 - 1965. |
| Zenit-4 Russian military surveillance satellite. Zenit-4 was the second Soviet photo-reconnaissance satellite, providing high-resolution imagery to complement the area coverage of the Zenit-2. Reconnaissance, photo (high resolution, film return type) satellite built by TsSKB for GRU, Russia. Launched 1963 - 1970. Used Zenit bus. |
| TGR Russian military surveillance satellite. Study 1963. Two new directions were pursued in the Soviet Union for space optical reconnaissance systems in the mid-1960's: automated systems with television transmission of pictures, and manned systems. |
| Calsphere American military target satellite. Radar calibration objects (but also cover for other classified subsatellites). Radar calibration satellite for Naval Research Laboratory (NRL), USA. Launched 1962-1967. |
| LCS American military target satellite. Aluminum sphere used for radar calibration. Radar Calibration satellite built by Rohr Corp. for Lincoln Laboratory, USA. Launched 1965 - 1971. |
| Tempsat American military target satellite. Surveillance Calibration; black 14 inch diameter. sphere. |
| US-A Russian military naval surveillance radar satellite. The US-A (later known as RLS) was a nuclear powered RORSAT (Radar Ocean Reconnaissance Satellite). Ocean surveillance, active radar satellite, Russia. Launched 1970 - 1988. Used US-Bus. |
| Bluebell American military target satellite. Calibration satellite operated by US Air Force, USA. Launched 1966. |
| KH-8 American military surveillance satellite. Longest-lived and last US film-return reconnaissance satellite. Ground resolution 0.5 m. Film returned in two capsules. Typical life 50 days. Reconnaissance, photo (film return type) satellite operated by USAF, USA. Launched 1966 - 1969. |
| Tselina-O Ukrainian ELINT satellite. From 1965 to 1967 two dedicated ELINT systems were tested by the Soviet Union: Tselina and US. Both were routinely operated. ELINT satellite built by Yuzhnoye (prime), TsNII-108 GKRE (payload), Russia. Launched 1967 - 1982. |
| KH-4B American military surveillance satellite. Early US reconnaissance satellite. Carried two 'J-3' panoramic cameras, with a focal length of 61 cm, and a ground resolution of 1.8 m. Reconnaissance, photo (film return type) satellite built by Lockheed for USAF, USA. Launched 1967 - 1972. |
| Zenit-2M satellite Russian military surveillance satellite. 1 Planning began in mid-1967 for military systems to enter service through 1975. Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1968 - 1979. Used Zenit bus. |
| Canyon American military signals intelligence satellite. The first large US signals intelligence satellite. ELINT satellite built by Lockheed for NRO, USA. Launched 1968 - 1977. |
| Zenit-4M Russian military surveillance satellite. Planning began in mid-1967 for military systems to enter service through 1975. Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1968 - 1974. Used Zenit bus. |
| Yantar-1 Russian military surveillance satellite. Study 1968. Survey reconnaissance satellite project of KB Yuzhnoye worked on 1964-1967. |
| Yantar-2 Russian military surveillance satellite. Study 1968. High resolution reconnaissance satellite project worked on by KB Yuzhnoye 1964-1967. Was to have been derived from Soyuz-R manned spacecraft. |
| SOICAL American military target satellite. |
| Zenit-4MK Russian military surveillance satellite. Modernized high resolution version of the Zenit-4M satellite that went into service in 1972. Maneuverable; (two-tone telemetry). Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1969 - 1977. Used Zenit bus. |
| Yantar-3KF Russian military surveillance satellite. Study 1969. Survey reconnaissance satellite system studied in 1969. Not put into production. |
| Rhyolite American military signals intelligence satellite. ELINT satellite built by TRW, E-Systems for USAF, USA. Launched 1970 - 1978. |
| DSP American military early warning satellite. An evolving series of satellites built by the United States to detect intercontinental ballistic missiles on launch. Early Warning satellite built by TRW for USAF, USA. Launched 1970 - 1973. |
| Tselina-D Ukrainian military signals intelligence satellite. The Tselina D was the detailed observation portion of the two-satellite Tselina ELINT satellite system. ELINT satellite built by Yuzhnoye (prime), TsNII-108 GKRE (payload), Russia. Launched 1970 - 1994. |
| Yantar-1KF Russian military surveillance satellite. Cancelled 1970. Survey reconnaissance satellite project worked on by Kozlov from 1967, succeeding Yantar-1. To be launched on Soyuz 11A511M launch vehicle. |
| Jumpseat American military signals intelligence satellite. Jumpseat signals intelligence satellites were launched by Titan 3B or 34B into highly elliptic Molniya-type orbits.Built by Hughes for USAF, USA. Launched 1971 - 1983. Used HS-318 bus. |
| KH-9 American military surveillance satellite. Popularly known as 'Big Bird'. Titan 3C-class film-return reconnaissance satellite. Reconnaissance, photo satellite built by Lockheed (prime); Perkin-Elmer (cameras) for USAF, USA. Launched 1971 - 1986. |
| Rigidsphere American military target satellite operated by USAF STP (Space Test Program), USA. Launched 1968 - 1971. |
| NOSS US Navy Ocean Surveillance Satellite to track and surveil ships at sea worldwide. Built by Naval Research Laboratory (#1, 2); Martin Marietta (#3 - 9). Launched 1976 - 1987. |
| Zenit-4MT Russian military surveillance satellite. Special version of Zenit developed for topographical photography. This was developed by OKB-1 Filial 1 based on the Zenit-4M. Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1971 - 1982. Used Zenit bus. |
| Oko Russian military early warning satellite. Work on the Soviet Union's first infrared ICBM launch detection satellite began in 1967 as the USK - space system to observe rocket launches. |
| JSSW Chinese military surveillance satellite. Mysterious early Chinese satellite, orbited by the cancelled FB-1 launch vehicle. Technology, Reconnaissance? satellite, China. Launched 1973 - 1976. |
| Yantar-2K Russian military surveillance satellite. Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1974 - 1983. Used Yantar Bus, main reentry module, 2 small reentry capsules. |
| Taifun-1 Ukrainian military target satellite. From 1969 KB Yuzhnoye built the Lira targets for exercise and test of PVO air defense and space tracking systems. Radar calibration satellite built by Yuzhnoye, Russia. Launched 1974 - 1994. |
| FSW Chinese military surveillance satellite. Reconnaissance, Earth observation satellite built by CAST, China. Launched 1974 - 1987. |
| US-P Russian military naval radarsat. The US-P (later known as RTR) was a solar powered EORSAT (Electronic Ocean Reconnaissance Satellite). Ocean surveillance, passive satellite, Russia. Launched 1974 - 1991. Used US-Bus. |
| Zenit-4MKT Russian military surveillance satellite. The Zenit-4MKT / Fram was an adaptation of the recoverable Vostok spacecraft for reconnaissance/remote sensing missions. Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1975 - 1985. Used Zenit bus. |
| Prognoz SPRN Russian military early warning satellite. Development began of the Soviet Union's Prognoz geosynchronous ballistic missile early warning satellite in 1980. |
| Taifun-2 Ukrainian military target satellite. In 1969 KB Yuzhnoye introduced targets for exercise and test of PVO air defense and space tracking systems. Radar calibration satellite built by Yuzhnoye, Russia. Launched 1976 - 1995. Used AUOS-3 bus. |
| NOSS-Subsat American military naval signals reconnaissance satellite. Detected the location of naval vessels using radio interferometry. Ocean Surveillance Launch Dispenser satellite built by Naval Research Laboratory (NRL) (#1, 2); (#3 - 9) for, USA. Launched 1976 - 1987. |
| Zenit-6U Russian military surveillance satellite. A universal variant of the Zenit spacecraft, used in two altitude ranges, for both observation and high resolution missions. Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1976 - 1984. Used Zenit bus. |
| KH-11 American military surveillance satellite. Also known as Kennan, Program 1010. Used systems developed for KH-10 Manned Orbiting Laboratory. Reconnaissance, electro-optical satellite built by Lockheed => Lockheed Martin for NRO, USA. Launched 1976 - 2013. Used Bus-1. |
| Yantar-4K2 Russian military surveillance satellite. Cancelled 1991. Improved military photo-reconnaissance satellite, using the basic Yantar-4K1 bus. Boost by the Zenit-2 launch vehicle would have allowed 22 film return capsules to be used over a 180 day mission. Reconnaissance, photo (film return type) satellite built by TsSKB > TsSKB-Progress for GRU, Russia. Launched 1981 - 2002. Used Yantar Bus, main reentry module, 2 small reentry capsules. |
| Yantar-6K Russian military surveillance satellite. Study 1977. Extremely high resolution version of Yantar studied in 1969. A draft project was completed in May 1977, but the decision was made to keep the basic Yantar-2K satellite bus instead. |
| Yantar-6KS Russian military surveillance satellite. Study 1977. Electro-optical imaging operational high resolution version of Yantar studied in 1969. |
| Zenit-4MKM Russian military surveillance satellite. A further modification of the Zenit-4MK, accepted for military service in 1976, entered service in 1978. Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1977 - 1980. Used Zenit bus. |
| Chalet American military signals intelligence satellite. Geosynchronous orbit signals intelligence satellite series that replaced Canyon. Also called Program 366 and Vortex. ELINT satellite built by E-Systems for NRO, USA. Launched 1978 - 1989. |
| Yantar-4K1 Russian film-return military surveillance satellite. Flight trials of the Yantar-2K indicated the satellite was not capable of providing strategic warning of attack. The high resolution Yantar-4K provided that capability, while still capable of being launched by the existing Soyuz-U launch vehicle. Lifetime was 45 days. Two small capsules could return film an interim basis before the main spacecraft with film returned to earth. |
| Taifun-1Yu Ukrainian military target satellite. The Taifun-1Yu, a modification of the basic design with smooth calibration surfaces, was to be in service by 1980. Launched 1979 - 1996. |
| Yantar-2K-M Russian military surveillance satellite. Study 1980. Planned upgrade of Yantar-2K. Not put into production. |
| Yantar-1KFT Russian military surveillance satellite. Version of the Yantar photo satellite for topographic mapping on behalf of the Red Army. Area Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1981 - 2005. Used Yantar Bus, Zenit reentry module. |
| SSTL-70 British microsatellite bus. 1 Basic Surrey Microsat bus. |
| Yantar-4KS1 Russian military electro-optical surveillance satellite. Reconnaissance, photo (data transmitting) satellite built by TsSKB for GRU, Russia. Launched 1982 - 1990. Used Yantar Bus. |
| Yantar-4KS2 Russian military surveillance satellite. Cancelled 1983. The Yantar-4KS2 was a heavy military optical reconnaissance satellite, required to have the same capabilities as the KH-11/Crystal reconnaissance satellite of the United States. |
| Zenit-8 Russian military surveillance satellite. 1 Reconnaissance, photo (film return type) satellite built by TsSKB for GRU, Russia. Launched 1984 - 1994. Used Zenit bus. |
| Tselina-2 Ukrainian military signals intelligence satellite. ELINT satellite built by KB Yuzhnoye (bus), TsNIRTI Minradioprom (ELINT payload), Russia. Launched 1984 - 2007. |
| Energia Control Sat Russian military surveillance satellite. Study 1984. This satellite would consist of a 33 metric ton equipment bus and a 17 metric ton rocket stage. It would be placed in a 600 km / 97 degree orbit for arms control and environment monitoring. |
| Magnum American military signals intelligence satellite. Shuttle-launched geostationary ELINT satellite model that replaced Rhyolite/Aquacade. ELINT satellite built by TRW for USAF, USA. Launched 1985 - 1989. |
| NUSAT American military target satellite. Air traffic control radar calibration. Technology satellite, USA. Launched 1985. |
| Koltso Russian military target satellite. Cosmos 1786. Calibration mission. Tentatively identified as third generation replacement for Taifun-2, perhaps to have been launched by the Tsyklon 3 launch vehicle. Radar calibration satellite built by Yuzhnoye, Russia. Launched 1988 - 1990. |
| Orlets-2 Russian military surveillance satellite. Reconnaissance, photo (film return) satellite operated by GRU, Russia. Launched 1994 - 2000. |
| Almaz-T Russian civilian surveillance radar satellite. The results of the manned Almaz flights showed that manned reconnaissance from space was not worth the expense. Radar satellite (modified manned spacecraft) satellite for NPO Machinostroenye, USSR. Launched 1986-1991. |
| Pirs-1 Russian military naval surveillance radar satellite. 2 launches, 1987.02.02 and 1987.07.10 . |
| Plazma-A Russian ion engine technology satellite. In 1987 two experimental Plazma-A satellites (Cosmos 1818 and 1867) were launched with new-generation Topaz reactors. |
| IRS Indian Remote Sensing Satellite. Remote sensing of the Earth for natural resources management applications. Earth Observing satellite for ISRO, India. Launched 1988-1991. Used IRS-1 Bus. |
| Singleton American signals intelligence satellite; possibly some kind of imaging also done. On-board propulsion boosts spacecraft to 800 km operating orbit. |
| Taifun-3 Russian military target satellite. Specifications for a third generation Taifun-3 system were developed in 1980 with flight trials to have started in 1984. |
| Orlets-1 Russian military surveillance satellite. Multi-purpose satellite, designed for both close-look and survey missions, equipped with a panoramic camera, equipped with 8 film return capsules. Reconnaissance, photo (film return) satellite operated by GRU, Russia. Launched 1989 - 2006. |
| Misty American nuclear detection surveillance satellite. Reconnaissance, electro-optical, stealth satellite built by Lockheed Martin for NRO, USA. Launched 1990 - 1999. |
| Badr Pakistani communications technology satellite. Pakistani experimental series with a variety of payloads. Technology satellite for SUPARCO, Pakistan. Launched 1990. |
| Improved Crystal American military surveillance satellite. Operational, first launch 1992.11.28. Improved CRYSTAL was an optical reconnaissance satellite built for the US National Reconnaissance Office. Prime contractor was thought to be Lockheed. |
| US-PU Ukrainian military naval radarsat. Ocean surveillance, passive satellite, Russia. Launched 1993 - 2006. Used US-Bus. |
| Radcal American military target satellite. Radar calibration. Radar calibration satellite built by DSI for USAF STP (Space Test Program), USA. Launched 1993. |
| Almaz-1B Russian civilian surveillance radar satellite. Study 1993. |
| ODERACS American military target satellite. Orbital Debris Radar Calibration Spheres were small, low-earth orbiting calibration targets for ground based radar and optical systems. The primary objective was to calibrate the Haystack Long Range Imaging Radar and validate the Johnson Space Center's Orbital Debris Analysis System. Radar calibration satellite operated by NASA Goddard, USA. Launched 1992 - 1995. |
| Mercury ELINT American electronic intelligence satellite. Class of heavy signals intelligence satellites introduced at the end of the 1990's. |
| Resurs-Spektr Russian civilian surveillance satellite. Study 1994. Earth Observation (all), cosmic rays (#2) satellite built by TsSKB-Progress for Roskosmos, Russia. Launched 2013 - 2016. Used Yantar bus. |
| Ofeq 3 Israeli military surveillance satellite. Ofeq 3 was Israel's second-generation imaging surveillance satellite. Reconnaissance, optical satellite built by IAI for Tsahal, Israel. Launched 1995 - 1998. Used OPSAT-1000 Bus. |
| Advanced Orion American military signals intelligence satellite. Highly classified. |
| STEP Space Test Experiment Program; series of USAF technology test satellites. |
| Helios 1A-1B French military surveillance satellite. Helios 1A an 1B were advanced French military surveillance satellites which were widely believed to have 1 meter resolution capability. Reconnaissance, electro-optical satellite built by ATrospatiale, Matra Marconi for DGA, France. Launched 1995 - 1999. Used the SPOT Mk.2 bus. |
| MicroSat-100 British microsatellite bus. Enlarged version of the basic Surrey Microsat-70 bus. |
| Radarsat Canadian earth resources radar satellite. T Canada's Radarsat was a radar satellite featuring variable resolution, and different view angles at a number of preset positions. Earth Observing (Radar) satellite built by Spar Aerospace (Prime), Ball Aerospace (Bus) for CSA, Canada. Launched 1995. Used the BCP-4000 bus. |
| Almaz-2 Russian civilian surveillance radar satellite. Study 1995. Plans for an even more sophisticated and capable civilian Almaz 2 spacecraft were made in the early 1990's. Almaz 2's payload mass of 6. |
| AS 2100 American communications satellite. Cost per satellite $100 million for the spacecraft including ground support equipment, but not including launch costs. 3-axis stabilized. |
| Arkon-1 Russian military surveillance satellite. |
| Orbview-2 American civilian surveillance satellite. The SeaStar satellite carries the SeaWiFS instrument which was designed to monitor the color of the world's oceans. Earth observing satellite built by Orbital Sciences Corporation (OSC) for OrbImage (for NASA) => GeoEye, USA. Launched 1997. Used the PegaStar bus. |
| Early Bird American civilian surveillance satellite. Civilian earth resources / intelligence photo-imaging program. Earth observing satellite built by CTA => Orbital Sciences Corporation (OSC) for Earthwatch Inc., USA. Launched 1997. |
| Kondor Russian communications satellite. Study 1997. The Khrunichev State Space Research and Production Center (including the Salyut Design Bureau), proposed the Kondor communications system for mobile users. |
| Predvestnik Russian civilian surveillance satellite. Study 1998. The Predvestnik satellites were planned to form a space-based earthquake prediction system. |
| ROCSAT Taiwanese earth sea satellite. Taiwan's ROCSAT (Republic of China Satellites) were built for Taiwan's National Space Program Office. Earth Observing satellite built by TRW for NSPO, Taiwan. Launched 1999. Used the T200A bus. |
| Ikonos American civilian surveillance satellite. The first high resolution commercial imaging satellite. Earth observing satellite built by Lockheed Martin Commercial Space Systems for Space Imaging => GeoEye, USA. Launched 1999. Used the LM-900 bus. |
| Yamal Russian communications satellite. The Yamal communications satellite bus was developed by RKK Energia for Gazprom. Communication satellite built by RKK Energiya for Gazkom > Gazprom Space Systems, Russia. Launched 1999. Used the USP Bus bus. |
| KOMPSAT South Korean technology satellite. KOMPSAT was the first joint spacecraft development project for the South Korean aerospace agency KARI (Korea Aerospace Research Institute). Earth Observing satellite built by KARI, TRW (Bus) for KARI, Korea South. Launched 1999. Used the T200B bus. |
| MTI American military surveillance satellite. The Multispectral Thermal Imager (MTI) was a space-based research and development project sponsored by the U. Experimental satellite built by Ball Aerospace for DoE, USAF STP (Space Test Program), USA. Launched 2000. Used the BCP-600 bus. |
| SA-200 The Spectrum Astro SA-200 satellite bus provided a flexible platform for satellites launched by the Pegasus booster.he Spectrum Astro SA-200 satellite bus provided a flexible platform for satellites launched by the Pegasus booster. |
| Saudisat Saudi amateur radio communications satellite. Technology satellite built by KACST Space Research Institute, Space Quest for KACST Space Research Institute, Saudi Arabia. Launched 2000 - 2002. |
| Orbview American civilian surveillance satellite. Earth observing satellite built by Orbital Sciences Corporation (OSC) for OrbImage => GeoEye, USA. Launched 2003. Used the LEOStar bus. |
| QuickBird American civilian surveillance satellite. One launch, 2001.10.18. The QuickBird commercial imaging satellite was owned by DigitalGlobe (formerly EarthWatch) and used a Ball BCP2000 bus with a launch mass of 1028 kg and a dry mass of about 995 kg. Earth observing satellite built by Ball Aerospace for Earthwatch Inc. => DigitalGlobe, USA. Launched 2000 - 2001. Used the BCP-2000 bus. |
| PROBA Project for On-Board Autonomy, spearheaded by ESA and CNES, was a small satellite bus to accommodate instruments previously flown on larger spacecraft. Qinetiq Space Belgium built the satellite, designed to be compatible with the Vega, Soyuz and Falcon-1e launch vehicles. Technology satellite built by Qinetiq Space Belgium (prime); OIP Space Systems (payload) for ESA, Europe. Launched 2013. |
| TES Indian military surveillance satellite. TES was an imaging satellite equipped with cameras and instruments to test military reconnaissance satellite technology. Earth Observing, Technology satellite for ISRO, India. Launched 2001. Used IRS-1 Bus. |
| SPOT-5A-5B French earth land resources satellite. Trench earth land resources satellite. SPOT was the French government sponsored civil Earth observation program. A single SPOT satellite provided complete coverage of the Earth every 26 days. Earth Observing satellite built by Astrium for Spot Image, France. Launched 2002. Used the SPOT Mk.3 bus. |
| Ofeq 5 Israeli military surveillance satellite. Ofeq-5 was said to be about 33% heavier than its predecessors. Reconnaissance, optical satellite built by IAI for Tsahal, Israel. Launched 2002-2010. Used OPSAT-2000 Bus. |
| IGS Japanese military surveillance satellite. Launched in optical and radar versions. |
| Cubesat American low-cost nanosatellite bus. Used in dozens of launches. |
| Shenzhou OM Chinese manned spacecraft module. The orbital module provided quarters for the crew during the space mission, and could be fitted out with different internal and external equipment according to mission requirements. |
| Shiyan Chinese civilian surveillance satellite. The first 'Experiment Satellite', with a mass of 204 kg, was China's first transmission-type small satellite capable of stereo mapping. |
| SJ-6 Chinese military surveillance satellite constellation. Each launch was said to consist of a primary satellite using the CAST968 bus and a subsatellite built by SAST Shanghai. Five pairs were launched from ?Taiyuan by the CZ-4B launch vehicle into 590 km, 97.7 deg inclination sun synchronous orbits from 2009. Reported to carry systems for optically tracking satellites in orbit. In 2013 SJ-15 was launched from Jiuquan, and SJ-16 from Taiyuan, in very similar but slightly different orbits. These may have been the successor system. |
| Helios 2 French military surveillance satellite. French military surveillance satellite series which began service in 2004. Reconnaissance, electro-optical satellite built by Astrium for DGA, France. Launched 2004 - 2009. Used the SPOT Mk.3 bus. |
| Myriade Micro-satellite product line developed jointly by EADS Astrium and the French Space Agency CNES beginning in 1998. |
| MS-1 Ukrainian earth land resources satellite. Ukrainian microsatellite bus that could be equipped with imaging or other scientific or technical equipment. |
| SSETI Express European civilian surveillance satellite. Student-built technology satellite sponsored by the ESA. It ejected three 1-kg Cubesats after separating from the booster, but then itself lost power less than 14 hours later. Technology satellite for SSETI, Europe. Launched 2005. |
| Daichi Japanese civilian surveillance optical and radar satellite used for cartography, regional observation, disaster monitoring, and resource surveying. It lost all power on 22 April 2011. Earth Observation, Radar satellite operated by NASDA, Japan. Launched 2006. |
| KOMPSAT-2 South Korean civilian surveillance satellite. Kompsat 2. Earth Observing satellite built by KARI, Astrium for KARI, Korea South. Launched 2006. |
| Tacsat ORS American military surveillance satellite. The Tactical Satellite / Operationally Responsive Satellite program's objective was to demonstrate techniques to dramatically shorten the development time for small satellites. Technology, imaging satellite built by Air Force Research Laboratory (AFRL); MicroSat Systems (bus) for Air Force Research Laboratory (AFRL), USA. Launched 2006. Used the Road Runner Bus (NGMB, Next Generation Multifunctional Bus). Launched 2006. |
| SAR-Lupe German military surveillance radar satellite. Germany's first satellite-based radar reconnaissance system. It consisted of five identical small satellites and a ground segment. Reconnaissance, Radar satellite built by OHB-System GmbH for Bundeswehr, Germany. Launched 2006 - 2008. |
| Cosmo-SkyMed Italian military surveillance radar satellite. Constellation of four satellites launched 2007.06.08 - 2010.11.06. Earth Observing (Radar) satellite built by Alenia Spazio for ASI, Italy. Launched 2007 - 2010. Used the Prima Bus bus. |
| TerraSAR-X German civilian surveillance radar satellite. Scientific / commercial surveillance satellite, equipped with an X-band synthetic aperture radar with 1 meter resolution SAR satellite built by EADS Astrium for DLR, InfoTerra, Germany. Launched 2007 - 2010. Used AstroBus. |
| WorldView American civilian surveillance satellite. DigitalGlobe's WorldView satellite provided highly detailed imagery for precise map creation, change detection and in-depth image analysis. Earth observing satellite built by Ball Aerospace for DigitalGlobe, USA. Launched 2007. Used the BCP-5000 bus. |
| Dawn American asteroid probe. Asteroid belt unmanned probe designed to first orbit and survey the asteroid Vesta, and then fly on to the largest asteroid, Ceres. Orbit asteroids Ceres and Vesta. Multiple asteroid lander built by Orbital Sciences Corporation (OSC) for NASA, USA. Launched 2007. |
| Tecsar Israeli military surveillance radar satellite. Israeli military radar/optical surveillance satellite using synthetic aperture x-band radar, with estimated 10 cm radar and 1 m optical ground resolution. |
| IMS Indian military surveillance radar satellite. Indian Mini Satellite, a small imaging satellite. |
| SSTL-150 German civilian surveillance satellite. Surrey satellite bus, notably used for the RapidEye constellation of five environmental monitoring satellites. Mass of 152 kg including 12 kg of propellant. |
| HJ-1 Chinese civilian surveillance satellite. 2 launches, 2008.09.06 (Huan Jing-1A) to 2008.09.06 (Huan Jing-1B). |
| KKS Japanese picosatellite built by Kouku-kosen, the Tokyo Metropolitan College of Aeronautical Engineering, carrying an Earth imager. |
| PRISM Japanese remote sensing picosatellite built by the University of Tokyo, with a 10-cm aperture Earth imager on a 1-meter deployable boom. Technology satellite for ISSL (Intelligent Space Systems Laboratory) at the University of Tokyo (UT), Japan. Launched 2009. |
| SOHLA Japanese satellite built by the Space Oriented Higashi-osaka Leading Association, Osaka, carrying a cloud cover imager. |
| JB-5 Chinese military surveillance satellite constellation. Launched from ?Jiuquan by the CZ-4C launch vehicle into 630, 98 deg inclination sun synchronous orbits beginning in 2006. Built by SAST. Reported to carry an IE (Institute of Electronics, CAS) side-looking radar system. |
| JB-9 Chinese military surveillance satellite constellation.Launched from Taiyuan by the CZ-4C launch vehicle into 1200 km, 100.4 deg inclination sun synchronous orbits. The first was launched in 2009, followed by annual launches beginning in 2012. Built by SAST. Reported to carry a CIOMP (Changchun Institute of Optics, Fine Mechanics and Physics) optical imaging system, believed to be a low resolution mapping and area surveillance mission. |
| JB-7 Chinese military surveillance satellite constellation. Launched from Taiyuan by the CZ-2C launch vehicle into 510 km, 97.5 deg inclination sun synchronous orbits beginning in 2009. Built by SAST. Reported to carry an IE (Institute of Electronics, CAS) side-looking radar system. |
| JB-6 Chinese military surveillance satellite constellation. Launched from ?Jiuquan by the CZ-2D launch vehicle into 650 km, 98 deg inclination sun synchronous orbits beginning in 2007. Built by CAST; reported to carry a BISME (Beijing Institute of Space Mechanics and Electronics) optical imaging system. |
| JB-8 Chinese military surveillance satellite. Each launch consisted of a primary satellite and two sub-satellites. Three sets of these triplets were launched from ?Jiuquan by the CZ-4C launch vehicle into 1090 km, 63.4 deg inclination orbits beginning in 2010. Reported to have a naval surveillance / sigint mission similar to those of the US PARCAE/NOSS system. This utilized a group of satellites flying in loose formation to locate radio emitters using the difference in time of arrival of the radio signals at the different satellites. Built by DFH. |
| JB-10 Chinese military surveillance satellite constellation. Launched from Taiyuan by the CZ-4B launch vehicle into 490 km, 97 deg inclination sun synchronous orbits beginning in 2008. Built by CAST. Reported to carry the XIOPM (Xian Institute of Optics and Precision Mechanics) optical imaging system. |
| JB-11 Chinese military surveillance satellite constellation using a BISME (Beijing Institute of Space Mechanics and Electronics) imaging sensor with an 0.8 m resolution. Built by CAST. Launched from Taiyuan by the CZ-4B launch vehicle into 470 km, 97 deg inclination sun synchronous orbits beginning in 2012. |
| Arirang South Korean civilian surveillance satellite. Study 2015. South Korean indigenously-designed, multipurpose 1500 kg sun-synchronous orbit satellite, to be lofted by KSLV-III by 2015. |
1959 February 28 - .
21:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 1 - .
Payload: KH-1 prototype / Agena A 1022. Mass: 618 kg (1,362 lb). Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1959-03-03 . USAF Sat Cat: 13 . COSPAR: 1959-Beta-1. Apogee: 968 km (601 mi). Perigee: 163 km (101 mi). Inclination: 89.70 deg. Period: 96.00 min.
In the first use of a Thor as a space booster, the world's first polar orbiting satellite, Discoverer I, was launched by a Thor/Agena (Thor 163) booster combination from Vandenberg AFB. The mission was also the first successful flight test of Lockheed's Agena A upper stage vehicle designed for orbiting U.S. satellite systems. First polar orbiting satellite; KH-1 prototype; did not carry camera or film capsule.
1959 April 13 - .
21:18 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 2 - .
Payload: KH-1 prototype / Agena A 1022. Mass: 743 kg (1,638 lb). Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1959-04-26 . USAF Sat Cat: 14 . COSPAR: 1959-Gamma-1. Apogee: 346 km (214 mi). Perigee: 239 km (148 mi). Inclination: 89.90 deg. Period: 90.40 min.
An Air Force Thor/Agena A booster vehicle lifted Discoverer II into orbit from Vandenberg AFB. Discoverer II became the world's first satellite to be stabilized in orbit in all three axes, to be maneuvered on command from earth, to separate a reentry vehicle on command, and to send its reentry vehicle back to earth. The capsule ejector system malfunctioned, causing the capsule to impact near Spitsbergen on 14 April rather than near Hawaii as planned. KH-1 prototype; tested capsule recovery techniques; did not carry camera; capsule recovery failed. Because of a timing error, the US believed that the capsule landed somewhere on the island of Spitsbergen, north of Norway, instead of landing in the recovery zone near Hawaii. The capsule was never found; and CIA officials suspect it may have been snatched by the Soviets. The search for this capsule formed the basis of the book and film 'Ice Station Zebra'.
In the winter of 1960/1961, a US Discovery spy satellite capsule was found by loggers near Kalinin, 200 km north of Moscow. The loggers cracked it open with an axe. Sergei Khrushchev believed this to be the Discoverer 2 capsule. What was left was examined by Soviet engineers but didn't reveal much information - it was a polished aluminium sphere, 30 cm in diameter, gilded on the exterior. Some said it was found as early as the winter of 1959.
1959 June 3 - .
20:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
FAILURE: No telemetry after Agena ignition..
Failed Stage: U.
- Discoverer 3 - .
Payload: KH-1 prototype / Agena A 1018. Mass: 753 kg (1,660 lb). Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1959-06-03 . KH-1 prototype; did not carry camera; film capsule recovery failed..
1959 June 25 - .
22:47 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
FAILURE: Insufficient stage 2 velocity..
Failed Stage: U.
- Discoverer 4 - .
Payload: KH-1 9001. Mass: 743 kg (1,638 lb). Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1959-06-25 . COSPAR: F590625A. KH-1; 1st generation low resolution photo surveillance. Failed to achieve orbit..
1959 August 13 - .
19:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 5 - .
Payload: KH-1 9002 / Agena A 1029. Mass: 781 kg (1,721 lb). Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1959-09-28 . USAF Sat Cat: 18 . COSPAR: 1959-Epsilon-1. Apogee: 731 km (454 mi). Perigee: 214 km (132 mi). Inclination: 79.90 deg. Period: 94.10 min. KH-1; 1st generation low resolution photo surveillance; film capsule boosted into higher orbit, decayed 2/11/61. Mission failed. Power supply failure. No recovery..
- Discoverer 5 Capsule - .
Payload: KH-1 9002 Capsule. Mass: 779 kg (1,717 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1961-02-11 . USAF Sat Cat: 26 . COSPAR: 1959-Epsilon-2. Apogee: 1,700 km (1,000 mi). Perigee: 218 km (135 mi). Inclination: 78.90 deg. Period: 104.30 min. KH-1; 1st generation low resolution photo surveillance; film capsule boosted into higher orbit, decayed 2/11/61. Mission failed. Power supply failure. No recovery..
1959 August 19 - .
19:24 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 6 - .
Payload: KH-1 9003 / Agena A 1028. Mass: 783 kg (1,726 lb). Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1959-10-20 . USAF Sat Cat: 19 . COSPAR: 1959-Zeta-1. Apogee: 846 km (525 mi). Perigee: 207 km (128 mi). Inclination: 83.90 deg. Period: 95.10 min. KH-1; 1st generation low resolution photo surveillance; film capsule recovery failed. Mission failed. Retro rockets malfunctioned negating recovery..
1959 November 7 - .
20:28 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 7 - .
Payload: KH-1 9004 / Agena A 1051. Mass: 794 kg (1,750 lb). Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1959-11-26 . USAF Sat Cat: 24 . COSPAR: 1959-Kappa-1. Apogee: 820 km (500 mi). Perigee: 158 km (98 mi). Inclination: 81.60 deg. Period: 94.40 min. KH-1; 1st generation low resolution photo surveillance; satellite tumbled; film capsule not recovered. Mission failed. Failed to achieve orbit..
1959 November 20 - .
19:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 8 - .
Payload: KH-1 9005 / Agena A 1050. Mass: 795 kg (1,752 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-03-08 . USAF Sat Cat: 25 . COSPAR: 1959-Lambda-1. Apogee: 1,661 km (1,032 mi). Perigee: 186 km (115 mi). Inclination: 80.50 deg. Period: 103.50 min. KH-1; 1st generation low resolution photo surveillance; film capsule recovery failed. Mission failed. Eccentric orbit negating recovery..
1960 February 4 - .
18:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 9 - .
Payload: KH-1 9006. Mass: 765 kg (1,686 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-02-04 . KH-1; 1st generation low resolution photo surveillance. Mission failed..
1960 February 19 - .
20:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 10 - .
Payload: KH-1 9007. Mass: 765 kg (1,686 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-02-19 . KH-1; Mission failed..
1960 February 26 - .
17:25 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC14.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena A.
FAILURE: Second stage failed to separate..
Failed Stage: U.
- Midas 1 - .
Payload: Midas / Agena TV 1008. Mass: 2,025 kg (4,464 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
Decay Date: 1960-02-26 .
The Air Force MIDAS I satellite was launched from Cape Canaveral in the first successful launch of the Atlas D/Agena A booster-upper stage combination. MIDAS I, however, failed to achieve orbit because an accident at the Atlas-Agena staging damaged the Agena. The entire vehicle reentered and burned up about 2,500 miles downrange. Missile Defense Alarm System.
1960 April 13 - .
12:02 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Thor Ablestar.
- Dummy subsatellite - .
Payload: GRAB dummy. Mass: 18 kg (39 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: GRAB.
Decay Date: 1960-07-17 . USAF Sat Cat: 33 . COSPAR: 1960-Gamma-3. Apogee: 615 km (382 mi). Perigee: 285 km (177 mi). Inclination: 51.30 deg. Period: 93.60 min. Mass model of GRAB ELINT satellite..
1960 April 15 - .
20:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 11 - .
Payload: KH-1 9008 / Agena A 1055. Mass: 790 kg (1,740 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-04-26 . USAF Sat Cat: 32 . COSPAR: 1960-Delta-1. Apogee: 603 km (374 mi). Perigee: 166 km (103 mi). Inclination: 80.40 deg. Period: 92.20 min. KH-1; film capsule recovery failed. Mission failed. Attitude control system malfunctioned..
1960 May 24 - .
17:36 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC14.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena A.
- Midas 2 - .
Payload: Midas / Agena TV 1007. Mass: 2,300 kg (5,000 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
Decay Date: 1974-02-07 . USAF Sat Cat: 43 . COSPAR: 1960-Zeta-1. Apogee: 494 km (306 mi). Perigee: 473 km (293 mi). Inclination: 33.00 deg. Period: 94.30 min.
Missile Defense Alarm System. Test launch with W-17 sensor. The last Atlas D/Agena A booster to be used by the Air Force placed into orbit the MIDAS II infrared scanning satellite designed to detect and give early warning of missile launchings. Although intended to function for 40 months, the satellite's telemetry system failed on 26 May. MIDAS II was the first early warning satellite system placed in orbit.
1960 June 22 - .
05:54 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Thor Ablestar.
1960 June 29 - .
22:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 12 - .
Payload: KH-1 prototype. Mass: 790 kg (1,740 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-06-29 . KH-1 prototype; designed to test capsule recovery system; did not carry camera..
1960 August 10 - .
20:37 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 13 - .
Payload: KH-1 prototype / Agena A 1057. Mass: 850 kg (1,870 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-11-14 . USAF Sat Cat: 48 . COSPAR: 1960-Theta-1. Apogee: 683 km (424 mi). Perigee: 258 km (160 mi). Inclination: 82.80 deg. Period: 94.00 min.
A Thor/Agena A launched from Vandenberg AFB placed Discoverer XIII in orbit. On 11 August, the data capsule was ejected during the 17th pass and recovered Pacific Ocean near Hawaii by a Navy helicopter that was part of the 6593d Test Squadron's task force. Although the planned mid-air recovery was not made, the return of Discoverer XIII1s data capsule marked the first successful recovery of a man-made object ejected from an orbiting satellite. KH-1 prototype; designed to test capsule recovery system; did not carry camera; capsule successfully recovered from ocean.
1960 August 18 - .
19:57 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 14 - .
Payload: KH-1 9009 / Agena A 1056. Mass: 850 kg (1,870 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-09-16 . USAF Sat Cat: 54 . COSPAR: 1960-Kappa-1. Apogee: 803 km (498 mi). Perigee: 177 km (109 mi). Inclination: 79.60 deg. Period: 94.40 min. Discoverer XIV was launched from Vandenberg AFB aboard a Thor/Agena A booster.' KH-1; film capsule recovered 1.2 days later; 1st successful photosurveillance mission. First successful mission. Cameras operated satisfactorily..
1960 September 13 - .
22:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena A.
- Discoverer 15 - .
Payload: KH-1 9010 / Agena A 1058. Mass: 863 kg (1,902 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-1.
Decay Date: 1960-10-18 . USAF Sat Cat: 57 . COSPAR: 1960-Mu-1. Apogee: 755 km (469 mi). Perigee: 200 km (120 mi). Inclination: 80.90 deg. Period: 94.10 min. KH-1; film capsule lost at sea. Mission failed. Attained orbit successfully. Capsule sank prior to retrieval..
1960 October 11 - .
20:33 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena A.
FAILURE: Second stage failure..
Failed Stage: U.
- Samos 1 - .
Payload: Samos E-1 no. 1. Mass: 1,845 kg (4,067 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1960-10-11 . First generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite..
1960 October 26 - .
20:26 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 16 - .
Payload: KH-2 9011. Mass: 1,091 kg (2,405 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-2.
Decay Date: 1960-10-26 . KH-1; mission failed..
1960 November 12 - .
20:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 17 - .
Payload: KH-2 9012 / Agena B 1062. Mass: 1,091 kg (2,405 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-2.
Decay Date: 1960-12-29 . USAF Sat Cat: 61 . COSPAR: 1960-Omicron-1. Apogee: 984 km (611 mi). Perigee: 190 km (110 mi). Inclination: 81.70 deg. Period: 96.40 min.
The second Thor/Agena B to be launched from Vandenberg AFB was the first successful flight of the more advanced Lockheed Agena B upper stage. KH-1; film capsule recovered 2.1 days later. Mission failed. Obtained orbit successfully. Film separated before any camera operation leaving only 1.7 ft of film in capsule. On December 2, the Air Force revealed that exceedingly valuable information had been obtained from human tissues carried by Discoverer 17 (the cover story for the mission). The tissues had been exposed to an unexpectedly heavy dose of radiation for more than 50 hours in flight.
1960 November 30 - .
19:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Thor Ablestar.
FAILURE: Failure.
- Solrad 2 - .
Payload: Grab B. Mass: 18 kg (39 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: GRAB.
ELINT satellite..
1960 December 7 - .
20:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 18 - .
Payload: KH-2 9013 / Agena B 1103. Mass: 1,240 kg (2,730 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-2.
Decay Date: 1961-04-02 . USAF Sat Cat: 67 . COSPAR: 1960-Sigma-1. Apogee: 510 km (310 mi). Perigee: 233 km (144 mi). Inclination: 81.50 deg. Period: 92.00 min. KH-2; film capsule recovered 3.1 days later. First successful mission employing KH-2 camera system..
1960 December 20 - .
20:32 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 19 - .
Payload: Midas test payload. Mass: 1,060 kg (2,330 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
Decay Date: 1961-01-23 . USAF Sat Cat: 68 . COSPAR: 1960-Tau-1. Apogee: 359 km (223 mi). Perigee: 186 km (115 mi). Inclination: 83.40 deg. Period: 90.00 min. A Thor/Agena B vehicle successfully launched Discoverer XIX into a polar orbit from Vandenberg AFB. The spacecraft carried a Project MIDAS test payload. Tested IR sensors for Midas program; did not carry camera or film capsule. .
1961 January 31 - .
20:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena A.
1961 February 17 - .
20:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 20 - .
Payload: KH-5 s/n 9014A / Agena B 1104. Mass: 1,110 kg (2,440 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1962-07-28 . USAF Sat Cat: 83 . COSPAR: 1961-Epsilon-1. Apogee: 491 km (305 mi). Perigee: 277 km (172 mi). Inclination: 80.80 deg. Period: 92.30 min. KH-5; film capsule not ejected. Mission failed. Program malfunctioned and capsule did not reenter. First attempted ARGON mission. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1961 February 18 - .
22:58 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 21 - .
Payload: Midas test payload. Mass: 1,110 kg (2,440 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
Decay Date: 1962-04-20 . USAF Sat Cat: 84 . COSPAR: 1961-Zeta-1. Apogee: 458 km (284 mi). Perigee: 212 km (131 mi). Inclination: 80.60 deg. Period: 91.30 min. Tested IR sensors for Midas program; did not carry camera or film capsule..
1961 March 30 - .
20:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 22 - .
Payload: KH-2 9015. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-2.
Decay Date: 1961-03-30 . KH-2; Mission failed..
1961 April 8 - .
19:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 23 - .
Payload: KH-5 s/n 9016A / Agena B 1106 / Capsule SRV 521. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1962-04-16 . USAF Sat Cat: 100 . COSPAR: 1961-Lambda-1. Apogee: 651 km (404 mi). Perigee: 295 km (183 mi). Inclination: 82.30 deg. Period: 94.10 min. KH-5; film capsule boosted into higher orbit, decayed 5/23/62. Mission failed. Loss of satellite control gas caused unstable condition. No recovery. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1961 June 8 - .
21:16 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 24 - .
Payload: KH-5 s/n 9018A. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1961-06-08 . KH-5. Mission failed..
1961 June 16 - .
23:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 25 - .
Payload: KH-2 9017 / Agena B 1107. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-2.
Decay Date: 1961-07-12 . USAF Sat Cat: 108 . COSPAR: 1961-Xi-1. Apogee: 404 km (251 mi). Perigee: 222 km (137 mi). Inclination: 82.10 deg. Period: 90.80 min. KH-2; film capsule recovered 2.1 days later. Capsule recovered from water on orbit 32. Streaks throughout film..
1961 June 29 - .
04:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Thor Ablestar.
- Solrad 3 - .
Payload: Grab 2. Mass: 18 kg (39 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: GRAB.
COSPAR: 1961-Omicron-xx. ELINT satellite, retransmitting to US ground stations signals from Soviet radar stations. Classified at time; official purpose and secondary payload collected solar radiation data..
1961 July 7 - .
23:29 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 26 - .
Payload: KH-2 9019 / Agena B 1109. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-2.
Decay Date: 1961-12-05 . USAF Sat Cat: 160 . COSPAR: 1961-Pi-1. Apogee: 803 km (498 mi). Perigee: 228 km (141 mi). Inclination: 82.90 deg. Period: 94.90 min. KH-2; film capsule recovered 2.1 days later. Main camera malfunctioned on pass 22..
1961 July 12 - .
15:11 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
1961 July 21 - .
22:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 27 - .
Payload: KH-5 s/n 9020A. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1961-07-21 . KH-5; destroyed by range safety. Mission failed..
1961 August 4 - .
00:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 28 - .
Payload: KH-2 9021. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-2.
Decay Date: 1961-08-03 . KH-2; Mission failed..
1961 August 30 - .
20:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 29 - .
Payload: KH-3 s/n 9023 / Agena B 1112. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1961-09-09 . USAF Sat Cat: 181 . COSPAR: 1961-Psi-1. Apogee: 542 km (336 mi). Perigee: 152 km (94 mi). Inclination: 82.10 deg. Period: 91.50 min. KH-3; film capsule recovered 2.1 days later. First use of KH-3 camera system. All frames out of focus..
1961 September 9 - .
19:28 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
FAILURE: Exploded on launch pad..
Failed Stage: 1.
- Samos 3 - .
Payload: Samos E-2 no. 1. Mass: 1,890 kg (4,160 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1961-09-09 . First generation photo surveillance; radio relay of images..
1961 September 12 - .
19:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 30 - .
Payload: KH-3 s/n 9022 / Agena B 1113. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1961-12-11 . USAF Sat Cat: 182 . COSPAR: 1961-Omega-1. Apogee: 557 km (346 mi). Perigee: 219 km (136 mi). Inclination: 82.50 deg. Period: 92.30 min. KH-3; film capsule recovered 2.1 days later. Best mission to date. Same out-of-focus condition as in 9023..
1961 September 17 - .
21:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 31 - .
Payload: KH-3 s/n 9024 / Agena B 1114. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1961-10-26 . USAF Sat Cat: 186 . COSPAR: 1961-A-Beta-1. Apogee: 403 km (250 mi). Perigee: 231 km (143 mi). Inclination: 82.60 deg. Period: 90.80 min. KH-3; film capsule recovery failed. Mission failed. Power failure and loss of control gas on orbit 33..
1961 October 13 - .
19:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 32 - .
Payload: KH-3 s/n 9025 / Agena B 1115. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1961-11-13 . USAF Sat Cat: 189 . COSPAR: 1961-A-Gamma-1. Apogee: 391 km (242 mi). Perigee: 233 km (144 mi). Inclination: 81.60 deg. Period: 90.70 min. The 100th successful firing of a Thor placed Discoverer XXXII in orbit. KH-3; film capsule recovered 1.1 days later. Capsule recovered on orbit 18. 96% of film out of focus..
1961 October 21 - .
13:53 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Midas 4 - .
Payload: Midas / Agena TV 1202. Mass: 1,800 kg (3,900 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
USAF Sat Cat: 192 . COSPAR: 1961-A-Delta-1. Apogee: 3,763 km (2,338 mi). Perigee: 3,482 km (2,163 mi). Inclination: 95.90 deg. Period: 165.90 min. Missile Defense Alarm System. Deployed subsatellites..
1961 October 23 - .
19:23 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 33 - .
Payload: KH-3 s/n 9026. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1961-10-23 . KH-3; Mission failed..
1961 November 5 - .
20:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 34 - .
Payload: KH-3 s/n 9027 / Agena B 1117. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1962-12-07 . USAF Sat Cat: 197 . COSPAR: 1961-A-Epsilon-1. Apogee: 859 km (533 mi). Perigee: 231 km (143 mi). Inclination: 82.40 deg. Period: 95.60 min. KH-3; film capsule recovery not attempted. Mission failed. Improper launch angle resulted in extreme orbit..
1961 November 15 - .
21:23 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 35 - .
Payload: KH-3 s/n 9028 / Agena B 1118. Mass: 2,100 kg (4,600 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1961-12-03 . USAF Sat Cat: 201 . COSPAR: 1961-A-Zeta-1. Apogee: 278 km (172 mi). Perigee: 238 km (147 mi). Inclination: 81.60 deg. Period: 89.70 min. KH-3; film capsule recovered 1.1 days later. All cameras operated satisfactorily. Grainy emulsion noted..
1961 November 22 - .
20:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
FAILURE: Failure..
Failed Stage: U.
- Samos 4 - .
Payload: Samos E-5 no. 1. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1961-11-22 . Apogee: 200 km (120 mi). First generation photo surveillance; return of camera and film by capsule; SAMOS type satellite..
1961 December 11 - .
09:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8K72K.
FAILURE: RO-7 engine of block E upper stage cutoff prematurely. Spacecraft liquidated by self destruct system APO in 407th second of flight. Debris landed 100 km north of Vilyuisk..
Failed Stage: 2.
- Zenit-2 11F61 s/n 1 - .
Payload: Zenit-2 11F61 s/n 1. Mass: 4,610 kg (10,160 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1961-12-11 .
First attempted launch of Zenit photo-reconnaisance satellite. According to Kamanin, there was a problem with the third stage, and the capsule landed between Novosibirsk and Yakutsk, but could not be located. There was no information on the nature of the problem. Korolev stayed at Tyuratam, preparing for the next launch attempt.
1961 December 12 - .
20:40 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 36 - .
Payload: KH-3 s/n 9029 / Agena B 1119. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1962-03-08 . USAF Sat Cat: 213 . COSPAR: 1961-A-Kappa-1. Apogee: 173 km (107 mi). Perigee: 131 km (81 mi). Inclination: 89.50 deg. Period: 87.50 min. KH-3; film capsule recovered 4.1 days later. Best mission to date..
1961 December 22 - .
19:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Samos 5 - .
Payload: Samos E-5 no. 2. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1962-01-09 . USAF Sat Cat: 218 . COSPAR: 1961-A-Lambda-2. Apogee: 310 km (190 mi). Perigee: 187 km (116 mi). Inclination: 89.60 deg. Period: 89.40 min.
First generation photo surveillance; return of camera and film by capsule; SAMOS type satellite. Reached orbit but failed to deorbit and be recovered. In his memoirs Sergei Khrushchev recounts recovery of what he believed to be a recoverable Samos, except the date given is the winter before tests of this configuration actually started. He relates that a second American capsule was recovered in the spring of 1961. It was equipped with a 30 cm lens and 100's of metres of 10 cm wide film. Also recovered were a pear-shaped module made of fibreglass, and an inertial orientation system powered by electric motors. It may have been a SAMOS prototype. The capsule was found by tractor drivers, who disassembled it and used the film to wrap around the frame of their outhouse to provide some privacy in the treeless area. Unfortunately this ruined the film, preventing the Russians from developing it and discovering the technical capabilities of the system.
1962 January 13 - .
21:41 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Failure.
Failed Stage: U.
- Discoverer 37 - .
Payload: KH-3 s/n 9030. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-3.
Decay Date: 1962-01-13 . KH-3. Mission failed. Last attempted flight of KH-3 series..
1962 January 24 - .
09:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Thor Ablestar.
FAILURE: Failure.
- Solrad 4 - .
Payload: Grab D. Mass: 18 kg (39 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: GRAB.
ELINT satellite..
1962 February 21 - .
18:44 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
FAILURE: Partial failure. Agena failed to restart to circularize orbit..
Failed Stage: U.
- Ferret 1 - .
Payload: Ferret 1 / Agena B 2301. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1962-03-04 . USAF Sat Cat: 242 . COSPAR: 1962-Delta-1. Apogee: 219 km (136 mi). Perigee: 169 km (105 mi). Inclination: 81.90 deg. Period: 88.30 min.
1962 February 27 - .
19:39 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 38 - .
Payload: KH-4 s/n 9031 / Agena B 1123. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-03-21 . USAF Sat Cat: 247 . COSPAR: 1962-Epsilon-1. Apogee: 277 km (172 mi). Perigee: 207 km (128 mi). Inclination: 82.20 deg. Period: 89.40 min. First mission of the KH-4 series. Much of film slightly out of focus.. Capsule recovered 4.1 days later..
1962 March 7 - .
22:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Samos 6 - .
Payload: Samos E-5 no. 3. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1963-06-07 . USAF Sat Cat: 259 . COSPAR: 1962-Eta-3. Apogee: 686 km (426 mi). Perigee: 236 km (146 mi). Inclination: 90.90 deg. Period: 93.90 min. First generation photo surveillance; return of camera and film by capsule; SAMOS type satellite. Failed to return camera and film. Samos film return project cancelled; remaining 4 cameras placed in warehouse and later used on KH-6 Lanyard..
1962 April 9 - .
15:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Midas 5 - .
Payload: Midas / Agena TV 1203. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
USAF Sat Cat: 271 . COSPAR: 1962-Kappa-1. Apogee: 3,405 km (2,115 mi). Perigee: 2,784 km (1,729 mi). Inclination: 86.70 deg. Period: 152.90 min. Missile Defense Alarm System..
1962 April 18 - .
00:54 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Discoverer 39 - .
Payload: KH-4 s/n 9032 / Agena B 1124. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-05-28 . USAF Sat Cat: 276 . COSPAR: 1962-Lambda-1. Apogee: 540 km (330 mi). Perigee: 158 km (98 mi). Inclination: 73.50 deg. Period: 91.60 min. KH-4. Best mission to date..
1962 April 26 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC5.
LV Family:
Scout.
Launch Vehicle:
Scout X-2.
FAILURE: Failure..
Failed Stage: U.
1962 April 26 - .
10:02 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8K72K.
- Cosmos 4 - .
Payload: Zenit-2 11F61 s/n 2. Mass: 4,610 kg (10,160 lb). Nation: Russia.
Related Persons: Nikolayev,
Popovich.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Flight: Vostok 3,
Vostok 4.
Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 3.00 days. Decay Date: 1962-04-29 . USAF Sat Cat: 287 . COSPAR: 1962-Xi-1. Apogee: 317 km (196 mi). Perigee: 285 km (177 mi). Inclination: 65.00 deg. Period: 90.50 min.
Area survey photo reconnaissance satellite. Program partially completed. Failure of primary spacecraft orientation system. It was to spend four days in space, to be followed by another mission during 5-10 May. This meant that Vostok 3/4 could not be launched before 20-30 May. The cosmonaut prime crew returned from their in-suit parachute training at Fedosiya.
1962 April 26 - .
18:56 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Samos 7 - .
Payload: Samos E-6 no. 1 / Agena B 2401. Mass: 1,588 kg (3,500 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1962-04-28 . USAF Sat Cat: 286 . COSPAR: 1962-Pi-1. Second generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results..
1962 April 29 - .
00:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9033 - .
Payload: KH-4 s/n 9033 / Agena B 1125. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-05-26 . USAF Sat Cat: 290 . COSPAR: 1962-Rho-1. Apogee: 475 km (295 mi). Perigee: 180 km (110 mi). Inclination: 73.10 deg. Period: 91.10 min. KH-4. Mission failed. Parachute ejector squibs holding parachute container cover failed to fire. No recovery..
1962 May 15 - .
19:36 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-5 9034A - .
Payload: KH-5 s/n 9034A/Agena B 1126. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1963-11-26 . USAF Sat Cat: 292 . COSPAR: 1962-Sigma-1. Apogee: 550 km (340 mi). Perigee: 283 km (175 mi). Inclination: 82.30 deg. Period: 93.00 min. KH-5; film capsule recovered 4.1 days later. First successful KH-5 mission. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1962 May 30 - .
01:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9035 - .
Payload: KH-4 s/n 9035 / Agena B 1128. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-06-11 . USAF Sat Cat: 302 . COSPAR: 1962-Phi-1. Apogee: 350 km (210 mi). Perigee: 192 km (119 mi). Inclination: 74.10 deg. Period: 89.90 min. KH-4; film capsule recovered 3.1 days later. Slight corona static on film..
1962 June 1 - .
09:38 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
FAILURE: Shutdown of Block B strap-on engine stage 1.8 seconds after liftoff. The booster crashed 300 m from the pad. Pad damaged..
Failed Stage: 0.
- Zenit-2 11F61 s/n 3 - .
Payload: Zenit-2 11F61 s/n 3. Mass: 4,610 kg (10,160 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1962-06-01 .
Area survey photo reconnaissance satellite. Third attempted launch of Zenit photo-reconnaissance satellite. It blew up 300 m from the pad, and did enough damage to put the launch complex out of operation for a month. Therefore the Vostok 3/4 launches could not take place until the end of July at the earliest.
1962 June 2 - .
00:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9036 - .
Payload: KH-4 s/n 9036 / Agena B 1127. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-06-28 . USAF Sat Cat: 304 . COSPAR: 1962-Chi-1. Apogee: 401 km (249 mi). Perigee: 211 km (131 mi). Inclination: 74.50 deg. Period: 90.60 min. KH-4. Mission failed. During air catch, chute tore loose. Capsule sank..
1962 June 17 - .
18:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Samos 8 - .
Payload: Samos E-2 no. 2 / Agena B 2402. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1962-06-18 . USAF Sat Cat: 307 . COSPAR: 1962-Psi-1. Apogee: 198 km (123 mi). Perigee: 198 km (123 mi). Inclination: 96.20 deg. Period: 88.40 min. First generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results..
1962 June 18 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- Ferret 2 - .
Payload: Ferret 2 / Agena B 2312. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1963-10-30 . USAF Sat Cat: 308 . COSPAR: 1962-Omega-2. Apogee: 377 km (234 mi). Perigee: 347 km (215 mi). Inclination: 82.10 deg. Period: 91.80 min.
- FTV 2312 - .
Payload: Ferret 2. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1963-10-30 . USAF Sat Cat: 308 . COSPAR: 1962-Omega-1. Apogee: 170 km (100 mi). Perigee: 161 km (100 mi). Inclination: 82.20 deg. Period: 87.80 min.
1962 June 23 - .
00:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9037 - .
Payload: KH-4 s/n 9037 / Agena B 1129. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-07-07 . USAF Sat Cat: 315 . COSPAR: 1962-A-Beta-1. Apogee: 314 km (195 mi). Perigee: 199 km (123 mi). Inclination: 75.10 deg. Period: 89.60 min. KH-4. Corona static occurs on some film..
1962 June 28 - .
01:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9038 - .
Payload: KH-4 s/n 9038 / Agena D 1151. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-09-14 . USAF Sat Cat: 316 . COSPAR: 1962-A-Gamma-1. Apogee: 698 km (433 mi). Perigee: 205 km (127 mi). Inclination: 76.00 deg. Period: 93.60 min.
The first Agena D (#1151) upper stage vehicle was successfully flown on a Thor booster (#340) launched from Vandenberg AFB. The Lockheed Agena D was a redesign of the basic Agena B and was intended to be the standard stage vehicle for most Defense Department and NASA programs. The program was begun in August 1961, revised and accelerated in November, and had its first flight in June 1962. KH-4; film capsule recovered 4.1 days later. Severe corona static.
1962 July 18 - .
20:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Samos 9 - .
Payload: Samos E-2 no. 3 / Agena B 2403. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1962-07-25 . USAF Sat Cat: 342 . COSPAR: 1962-A-Zeta-1. Apogee: 234 km (145 mi). Perigee: 184 km (114 mi). Inclination: 96.00 deg. Period: 88.60 min. First generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results..
1962 July 21 - .
00:56 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9039 - .
Payload: KH-4 s/n 9039 / Agena B 1130. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-08-14 . USAF Sat Cat: 344 . COSPAR: 1962-A-Eta-1. Apogee: 376 km (233 mi). Perigee: 206 km (128 mi). Inclination: 70.00 deg. Period: 90.30 min. KH-4. Aborted after 6 photo passes. Heavy corona and radiation fog..
1962 July 28 - .
00:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9040 - .
Payload: KH-4 s/n 9040 / Agena B 1131. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-08-24 . USAF Sat Cat: 345 . COSPAR: 1962-A-Theta-1. Apogee: 403 km (250 mi). Perigee: 204 km (126 mi). Inclination: 71.00 deg. Period: 90.60 min. KH-4; film capsule recovered 4.1 days later. No filters on slave horizon cameras. Heavy corona and radiation fog..
1962 July 28 - .
09:18 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 7 - .
Payload: Zenit-2 11F61 s/n 4. Mass: 4,610 kg (10,160 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 4.00 days. Decay Date: 1962-08-01 . USAF Sat Cat: 346 . COSPAR: 1962-A-Iota-1. Apogee: 356 km (221 mi). Perigee: 197 km (122 mi). Inclination: 64.90 deg. Period: 90.00 min. Area survey photo reconnaissance satellite. Also performed radiation measurements..
1962 August 2 - .
00:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9041 - .
Payload: KH-4 s/n 9041 / Agena D 1152. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-08-22 . USAF Sat Cat: 360 . COSPAR: 1962-A-Kappa-1. Apogee: 423 km (262 mi). Perigee: 212 km (131 mi). Inclination: 83.00 deg. Period: 90.80 min. KH-4; film capsule recovered 4.1 days later. Severe corona and radiation fog..
1962 August 5 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Samos 10 - .
Payload: Samos E-6 no. 2 / Agena B 2404. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1962-08-06 . USAF Sat Cat: 361 . COSPAR: 1962-A-Lambda-2. Apogee: 203 km (126 mi). Perigee: 201 km (124 mi). Inclination: 96.20 deg. Period: 88.50 min. Second generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results..
1962 August 29 - .
01:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9044 - .
Payload: KH-4 s/n 9044 / Agena D 1153. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-09-10 . USAF Sat Cat: 377 . COSPAR: 1962-A-Sigma-1. Apogee: 400 km (240 mi). Perigee: 187 km (116 mi). Inclination: 65.20 deg. Period: 90.40 min. KH-4; film capsule recovered 4.1 days later. Erratic vehicle attitude. Radiation fog minimal..
1962 September 1 - .
20:39 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-5 9042A - .
Payload: KH-5 s/n 9042A/Agena B 1132. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1964-10-26 . USAF Sat Cat: 385 . COSPAR: 1962-A-Upsilon-1. Apogee: 639 km (397 mi). Perigee: 293 km (182 mi). Inclination: 82.80 deg. Period: 94.00 min. KH-5. Mission failed. Parachute shrouds parted during air catch, capsule sank. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1962 September 17 - .
23:46 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9043 / TRS 1 (ERS 2) - .
Payload: KH-4 s/n 9043 / TRS 1 (ERS 2) / Agena B 1133. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-11-16 . USAF Sat Cat: 396 . COSPAR: 1962-A-Chi-1. Apogee: 668 km (415 mi). Perigee: 204 km (126 mi). Inclination: 81.80 deg. Period: 93.30 min. KH-4; film capsule recovered 1.1 days later; ERS-2 subsatellite failed to deploy. Capping shutter malfunction, slight corona and radiation fog..
1962 September 27 - .
09:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 9 - .
Payload: Zenit-2 11F61 s/n 7. Mass: 4,700 kg (10,300 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 4.00 days. Decay Date: 1962-10-01 . USAF Sat Cat: 422 . COSPAR: 1962-A-Omega-1. Apogee: 981 km (609 mi). Perigee: 829 km (515 mi). Inclination: 67.60 deg. Period: 103.10 min. Area survey photo reconnaissance satellite. Also performed radiation measurements..
1962 September 29 - .
23:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9045 - .
Payload: KH-4 s/n 9045 / Agena D 1154. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-10-08 . USAF Sat Cat: 427 . COSPAR: 1962-B-Beta-1. Apogee: 388 km (241 mi). Perigee: 190 km (110 mi). Inclination: 65.40 deg. Period: 90.30 min. KH-4. First use of stellar camera, erratic vehicle attitude, numerous light leaks..
1962 October 9 - .
18:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-5 9046A - .
Payload: KH-5 s/n 9046A/Agena B 1134. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1962-10-16 . USAF Sat Cat: 436 . COSPAR: 1962-B-Epsilon-1. Apogee: 427 km (265 mi). Perigee: 213 km (132 mi). Inclination: 82.00 deg. Period: 91.00 min. KH-5; film capsule recovered 4.1 days later. 50% of stellar terrain film was blank due to shutter malfunction. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1962 October 17 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 10 - .
Payload: Zenit-2 11F61 s/n 5. Mass: 4,700 kg (10,300 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 4.00 days. Decay Date: 1962-10-21 . USAF Sat Cat: 437 . COSPAR: 1962-B-Zeta-1. Apogee: 376 km (233 mi). Perigee: 178 km (110 mi). Inclination: 64.90 deg. Period: 90.00 min. Area survey photo reconnaissance satellite. Also performed radiation measurements..
1962 November 5 - .
22:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9047 - .
Payload: KH-4 s/n 9047 / Agena B 1136. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-12-03 . USAF Sat Cat: 453 . COSPAR: 1962-B-Omicron-1. Apogee: 403 km (250 mi). Perigee: 208 km (129 mi). Inclination: 75.00 deg. Period: 90.60 min. KH-4; film capsule; film capsule recovered 4.1 days later. Camera door malfunctioned, flare degraded 15% of film..
1962 November 11 - .
20:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Samos 11 - .
Payload: Samos E-6 no. 3 / TRS 1 / Agena B 2405. Mass: 1,860 kg (4,100 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: Samos.
Decay Date: 1962-11-12 . USAF Sat Cat: 455 . COSPAR: 1962-B-Pi-1. Apogee: 292 km (181 mi). Perigee: 128 km (79 mi). Inclination: 96.00 deg. Period: 88.70 min. Second generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results. SAMOS project cancelled..
1962 November 24 - .
22:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- KH-4 9048 - .
Payload: KH-4 s/n 9048 / Agena B 1135. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-12-13 . USAF Sat Cat: 481 . COSPAR: 1962-B-Rho-1. Apogee: 339 km (210 mi). Perigee: 206 km (128 mi). Inclination: 65.00 deg. Period: 89.90 min. KH-4. Some film exposed through base..
1962 December 4 - .
21:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9049 - .
Payload: KH-4 s/n 9049 / Agena D 1155. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1962-12-08 . USAF Sat Cat: 490 . COSPAR: 1962-B-Sigma-1. Apogee: 273 km (169 mi). Perigee: 194 km (120 mi). Inclination: 65.10 deg. Period: 89.20 min. KH-4. Mission failed. During air catch chute tore, capsule sank..
1962 December 13 - .
04:07 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- Black Sphere - .
Payload: NRL PL120 / Poppy 1A (Poppy 20-inch). Mass: 23 kg (50 lb). Nation: USA.
Agency: USAF,
USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
Decay Date: 1967-02-09 . USAF Sat Cat: 502 . COSPAR: 1962-B-Tau-1. Apogee: 2,385 km (1,481 mi). Perigee: 230 km (140 mi). Inclination: 70.30 deg. Period: 111.80 min. First launch of a pair of Poppy naval signals intelligence satellites, which would lead to the NOSS production series..
- SURCAL 1A - .
Mass: 37 kg (81 lb). Nation: USA.
Agency: USAF,
USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SURCAL.
Decay Date: 1966-01-18 . USAF Sat Cat: 508 . COSPAR: 1962-B-Tau-4. Apogee: 2,160 km (1,340 mi). Perigee: 227 km (141 mi). Inclination: 70.30 deg. Period: 109.30 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Calsphere 1A - .
Mass: 23 kg (50 lb). Nation: USA.
Agency: USAF,
USN.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: Calsphere.
Decay Date: 1967-02-05 . USAF Sat Cat: 513 . COSPAR: 1962-B-Tau-5. Apogee: 2,069 km (1,285 mi). Perigee: 228 km (141 mi). Inclination: 70.30 deg. Period: 108.40 min. Surveillance calibration..
- SURCAL 2A - .
Payload: NRL PL121 / Poppy 1B (Poppy 20-inch). Mass: 3.00 kg (6.60 lb). Nation: USA.
Agency: USAF,
USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
Decay Date: 1963-07-01 . USAF Sat Cat: 507 . COSPAR: 1962-B-Tau-3. Apogee: 2,762 km (1,716 mi). Perigee: 222 km (137 mi). Inclination: 70.20 deg. Period: 115.80 min. Poppy naval signals intelligence satellite. Officially: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1962 December 14 - .
21:26 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9050 - .
Payload: KH-4 s/n 9050 / Agena D 1156. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-01-08 . USAF Sat Cat: 505 . COSPAR: 1962-B-Phi-1. Apogee: 386 km (239 mi). Perigee: 200 km (120 mi). Inclination: 70.00 deg. Period: 90.30 min. KH-4; film capsule recovered 4.1 days later. Best mission to date..
1962 December 17 - .
20:36 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
FAILURE: Failure.
Failed Stage: U.
- Midas 6 - .
Payload: Midas / Agena TV 1205. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
Decay Date: 1962-12-17 . Missile Defense Alarm System. Carried ERS-3, ERS-4 subsatellites..
1962 December 22 - .
09:23 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 12 - .
Payload: Zenit-2 11F61 s/n 6. Mass: 4,700 kg (10,300 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1962-12-30 . USAF Sat Cat: 517 . COSPAR: 1962-B-Omega-1. Apogee: 385 km (239 mi). Perigee: 202 km (125 mi). Inclination: 64.80 deg. Period: 90.40 min. Area survey photo reconnaissance satellite. Also performed radiation measurements..
1963 January 7 - .
21:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9051 - .
Payload: KH-4 s/n 9051 / Agena D 1157 / OPS 0048. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-01-24 . USAF Sat Cat: 525 . COSPAR: 1963-002A. Apogee: 384 km (238 mi). Perigee: 202 km (125 mi). Inclination: 82.00 deg. Period: 90.30 min. KH-4. Erratic vehicle attitude. Frame ephemeris not created..
1963 January 16 - .
21:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena B.
- OPS 0180 - .
Payload: Ferret 3 / Agena B 2313. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-01-09 . USAF Sat Cat: 527 . COSPAR: 1963-003A. Apogee: 522 km (324 mi). Perigee: 461 km (286 mi). Inclination: 81.90 deg. Period: 94.40 min.
1963 February 28 - .
21:48 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-4 9052 - .
Payload: KH-4 s/n 9052. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-02-28 . KH-4. Mission failed..
1963 March 18 - .
21:13 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-6 8001 - .
Payload: KH-6 s/n 8001. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-6.
Decay Date: 1963-03-18 . First launch of KH-6. Mission failed..
- P-11 No. 1 - .
Payload: P-11 No. 1. Mass: 80 kg (176 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1963-03-18 . Ferret subsatellite aboard first launch of KH-6. Mission failed..
1963 March 21 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 13 - .
Payload: Zenit-2 11F61 s/n 9. Mass: 4,700 kg (10,300 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1963-03-29 . USAF Sat Cat: 554 . COSPAR: 1963-006A. Apogee: 303 km (188 mi). Perigee: 214 km (132 mi). Inclination: 65.20 deg. Period: 89.60 min. Area survey photo reconnaissance satellite. Also performed radiation measurements..
1963 April 1 - .
23:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9053 - .
Payload: KH-4 s/n 9053 / Agena D 1160 / OPS 0720. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-04-26 . USAF Sat Cat: 562 . COSPAR: 1963-007A. Apogee: 408 km (253 mi). Perigee: 198 km (123 mi). Inclination: 74.90 deg. Period: 90.50 min. KH-4; film capsule recovered 3.1 days later. Best imagery to date..
1963 April 22 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 15 - .
Payload: Zenit-2 11F61 s/n 8. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 5.00 days. Decay Date: 1963-04-27 . USAF Sat Cat: 569 . COSPAR: 1963-011A. Apogee: 336 km (208 mi). Perigee: 194 km (120 mi). Inclination: 65.00 deg. Period: 89.80 min. Area survey photo reconnaissance satellite. Also carried weather, radiation experiments..
1963 April 26 - .
20:13 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
FAILURE: Attitude sensors were misaligned. No orbit..
Failed Stage: U.
- KH-5 9055A - .
Payload: KH-5 s/n 9055A. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1963-04-26 . Mission failed..
1963 April 28 - .
08:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 16 - .
Payload: Zenit-2 11F61 s/n 10. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 10.00 days. Decay Date: 1963-05-08 . USAF Sat Cat: 571 . COSPAR: 1963-012A. Apogee: 379 km (235 mi). Perigee: 201 km (124 mi). Inclination: 64.70 deg. Period: 90.30 min. Program partially completed. Part of the information lost due to failure of engine block stabilization system. Area survey photo reconnaissance satellite. Also performed radiation measurements..
1963 May 9 - .
20:06 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Midas 7 - .
Payload: Midas / Agena TV 1206. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
USAF Sat Cat: 574 . COSPAR: 1963-014A. Apogee: 3,680 km (2,280 mi). Perigee: 3,609 km (2,242 mi). Inclination: 87.30 deg. Period: 166.40 min. MIDAS 7 was the first operational MIDAS mission and the first equipped with the W-37 sensor. During its six weeks of operation, MIDAS 7 recorded nine US ICBM launches, including the first missile launch ever detected from space..
1963 May 18 - .
22:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-6 8002 - .
Payload: KH-6 s/n 8002 / Agena D 1165 / OPS 0924. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-6.
Decay Date: 1963-05-27 . USAF Sat Cat: 578 . COSPAR: 1963-016A. Apogee: 506 km (314 mi). Perigee: 147 km (91 mi). Inclination: 74.50 deg. Period: 91.00 min. KH-6. Second launch of KH-6. Operation was successful but no film was used. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1963 May 24 - .
10:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 18 - .
Payload: Zenit-2 11F61 s/n 11. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 9.00 days. Decay Date: 1963-06-02 . USAF Sat Cat: 586 . COSPAR: 1963-018A. Apogee: 269 km (167 mi). Perigee: 212 km (131 mi). Inclination: 64.60 deg. Period: 89.30 min. Area survey photo reconnaissance satellite. Also performed radiation measurements..
1963 June 12 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
FAILURE: Failure.
Failed Stage: U.
- Midas 8 - .
Payload: Midas / Agena TV 1204. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
Decay Date: 1963-06-12 . Missile Defense Alarm System. Carried ERS-7, ERS-8 subsatellites..
1963 June 12 - .
23:58 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4 9054 - .
Payload: KH-4 s/n 9054 / Agena D 1161 / OPS 0954. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-07-11 . USAF Sat Cat: 590 . COSPAR: 1963-019A. Apogee: 416 km (258 mi). Perigee: 193 km (119 mi). Inclination: 81.80 deg. Period: 90.70 min. KH-4. Some imagery seriously affected by corona..
1963 June 15 - .
14:29 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- RADOSE 112 - .
Payload: NRL PL 112 / Poppy 2B (Poppy 20-inch). Mass: 25 kg (55 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
Decay Date: 1963-07-30 . USAF Sat Cat: 600 . COSPAR: 1963-021D. Apogee: 875 km (543 mi). Perigee: 170 km (100 mi). Inclination: 69.90 deg. Period: 95.10 min. Poppy naval signals intelligence satellite. Official and secondary mission: Radiation dosimeter measurements. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- USN satellite - .
Payload: NRL PL130 / Poppy 2C / RADOSE (Poppy 24-inch). Mass: 35 kg (77 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
Decay Date: 1963-07-27 . USAF Sat Cat: 598 . COSPAR: 1963-021E. Apogee: 859 km (533 mi). Perigee: 170 km (100 mi). Inclination: 69.90 deg. Period: 94.90 min. Poppy naval signals intelligence satellite..
- SURCAL 1B - .
Mass: 3.00 kg (6.60 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SURCAL.
Decay Date: 1963-07-05 . USAF Sat Cat: 597 . COSPAR: 1963-021F. Apogee: 802 km (498 mi). Perigee: 172 km (106 mi). Inclination: 69.90 deg. Period: 94.40 min. Surveillance Calibration. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1963 June 27 - .
00:37 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4 9056 - .
Payload: KH-4 s/n 9056 / Agena D 1166 / OPS 0999. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-07-26 . USAF Sat Cat: 609 . COSPAR: 1963-025A. Apogee: 338 km (210 mi). Perigee: 199 km (123 mi). Inclination: 81.60 deg. Period: 89.90 min. KH-4. Experimental camera carried. Film affected by light leaks..
- Hitch Hiker 1 - .
Payload: P-11 No. 2. Mass: 80 kg (176 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 614 . COSPAR: 1963-025B. Apogee: 2,506 km (1,557 mi). Perigee: 323 km (200 mi). Inclination: 82.10 deg. Period: 114.10 min. Radiation data. First successful flight of P-11 bus, mainly used for radar signals intelligence gathering..
1963 June 29 - .
22:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena B.
- OPS 1440 - .
Payload: Ferret 4 / Agena B 2314. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-10-26 . USAF Sat Cat: 613 . COSPAR: 1963-027A. Apogee: 530 km (320 mi). Perigee: 487 km (302 mi). Inclination: 82.30 deg. Period: 94.80 min.
An Air Force Thor/Agena B launched from Vandenberg established a number of distinctive records. It was the 200th Thor to be launched since Number 101 was launched at Cape Canaveral on 25 January 1957. It was the first, last and only-Thrust Augmented Thor/Agena B to be used by the Air Force. It was the final Agena B (#2314) to be employed with a Thor booster.
1963 July 10 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
FAILURE: Shutdown of Block B strap-on engine stage 1.9 seconds after liftoff. Pad damaged..
Failed Stage: 0.
- Zenit-2 11F61 s/n 12 - .
Payload: Zenit-2 11F61 s/n 12. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1963-07-10 . Area survey photo reconnaissance satellite..
1963 July 12 - .
20:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
1963 July 19 - .
00:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Agena D.
- KH-4 9057 - .
Payload: KH-4 s/n 9057 / Agena D 1412 / OPS 1266. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-08-13 . USAF Sat Cat: 621 . COSPAR: 1963-029A. Apogee: 382 km (237 mi). Perigee: 197 km (122 mi). Inclination: 82.90 deg. Period: 90.40 min. KH-4. Best mission to date..
1963 July 19 - .
03:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena B.
- Midas 9 - .
Payload: Midas / Agena TV 1207. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
USAF Sat Cat: 622 . COSPAR: 1963-030A. Apogee: 3,726 km (2,315 mi). Perigee: 3,676 km (2,284 mi). Inclination: 88.40 deg. Period: 167.90 min. The final Air Force Atlas D/Agena B (75D/1207) was launched from Vandenberg AFB. Missile Defense Alarm System. Did not eject ERS 10 subsatellite..
1963 July 31 - .
00:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH 4A-07 - .
Payload: KH-6 s/n 8003 / Agena D 1167 / OPS 1370. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-6.
Decay Date: 1963-08-12 . USAF Sat Cat: 626 . COSPAR: 1963-032A. Apogee: 455 km (282 mi). Perigee: 152 km (94 mi). Inclination: 74.90 deg. Period: 90.60 min. KH-6. Third and final KH-6 mission (LANYARD). Mission was successful but image quality was poor. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1963 August 25 - .
00:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1001 - .
Payload: KH-4A s/n 1001 / Agena D 1162 / OPS 1419. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1963-09-12 . USAF Sat Cat: 636 . COSPAR: 1963-034A. Apogee: 320 km (190 mi). Perigee: 161 km (100 mi). Inclination: 75.00 deg. Period: 89.40 min. KH-4A. First mission of KH-4A. Some film was fogged. Two buckets but 1001-2 was never recovered..
1963 August 29 - .
20:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2 Agena D.
- KH-4 9033 - .
Payload: KH-4 s/n 9033 & Lampo / Agena D 1169 / OPS 1561. Mass: 1,000 kg (2,200 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-11-07 . USAF Sat Cat: 637 . COSPAR: 1963-035A. Apogee: 324 km (201 mi). Perigee: 292 km (181 mi). Inclination: 81.90 deg. Period: 90.80 min. The first Thor standard launch vehicle, SLV-2, with an Agena D upper stage vehicle, was launched from Vandenberg AFB. KH-5; deployed ELINT subsatellite. Considered to be best mission to date in Argon program..
- LAMPO - .
Payload: 0.1 Square Meter Target. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: LAMPO.
Decay Date: 1963-09-29 . USAF Sat Cat: 638 . COSPAR: 1963-035B. Apogee: 422 km (262 mi). Perigee: 315 km (195 mi). Inclination: 81.90 deg. Period: 92.00 min. The first Thor standard launch vehicle, SLV-2, with an Agena D upper stage vehicle, was launched from Vandenberg AFB. Radar monitoring. Not identified as a subsatellite ferret by McDowell..
1963 September 6 - .
19:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-02 - .
Payload: KH-7 no. 2 / OPS 1947. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1963-09-13 . USAF Sat Cat: 641 . COSPAR: 1963-036A. Apogee: 243 km (150 mi). Perigee: 171 km (106 mi). Inclination: 94.40 deg. Period: 88.70 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1963 September 23 - .
23:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1002 - .
Payload: KH-4A s/n 1002 / Agena D 1163 / OPS 1353. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1963-10-12 . USAF Sat Cat: 668 . COSPAR: 1963-037A. Apogee: 442 km (274 mi). Perigee: 162 km (100 mi). Inclination: 74.80 deg. Period: 90.60 min. KH-4A. Severe light leaks, 1002-2 never recovered, indefinite postponement of KH-4A series..
1963 October 17 - .
02:37 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- Vela 2 - .
Payload: Vela 1B. Mass: 220 kg (480 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Vela.
USAF Sat Cat: 674 . COSPAR: 1963-039A. Apogee: 116,582 km (72,440 mi). Perigee: 101,081 km (62,808 mi). Inclination: 38.70 deg. Period: 6,486.20 min.
Space Systems Division, acting.as program manager for the Defense Department, launched two Vela nuclear radiation detection satellites from Cape Canaveral aboard the first Atlas D/Agena D (SLV-3/SS-01A) launch vehicle (197D). The Vela satellites were developed and produced by the TRW Systems and were the first pair in a series of satellites designed to provide information on nuclear detonations in the atmosphere or in outer space to a distance of 100 million miles. The 297-pound satellites were placed in near-circular orbits approximately 70,000 miles above the Earth's surface. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
- Vela 1 - .
Payload: Vela 1A. Mass: 220 kg (480 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Vela.
USAF Sat Cat: 692 . COSPAR: 1963-039C. Apogee: 116,528 km (72,407 mi). Perigee: 101,925 km (63,333 mi). Inclination: 37.80 deg. Period: 6,519.60 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1963 October 18 - .
09:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 20 - .
Payload: Zenit-2 11F61 s/n 13. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1963-10-26 . USAF Sat Cat: 673 . COSPAR: 1963-040A. Apogee: 296 km (183 mi). Perigee: 201 km (124 mi). Inclination: 64.80 deg. Period: 89.40 min. Area survey photo reconnaissance satellite..
1963 October 25 - .
18:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-03 - .
Payload: KH-7 no. 3 / OPS 2196. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1963-10-29 . USAF Sat Cat: 677 . COSPAR: 1963-041A. Apogee: 312 km (193 mi). Perigee: 123 km (76 mi). Inclination: 99.00 deg. Period: 88.80 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1963 October 29 - .
21:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-5 9059A - .
Payload: KH-5 s/n 9059A/Agena D 1601 / OPS 2437. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1964-01-21 . USAF Sat Cat: 681 . COSPAR: 1963-042A. Apogee: 318 km (197 mi). Perigee: 283 km (175 mi). Inclination: 89.90 deg. Period: 90.60 min. KH-5; deployed ELINT subsatellite. Fourth film payload retrieved in ARGON program. Film comparable to that of 9058A. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Hitch Hiker 2 - .
Payload: P-11 s/n A3. Mass: 80 kg (176 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1965-05-23 . USAF Sat Cat: 682 . COSPAR: 1963-042B. Apogee: 581 km (361 mi). Perigee: 288 km (178 mi). Inclination: 90.00 deg. Period: 93.30 min. Radar monitoring..
1963 November 9 - .
20:27 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2 Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-4 9060 - .
Payload: KH-4 s/n 9060. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-11-09 . KH-4. Mission failed..
1963 November 16 - .
10:34 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 22 - .
Payload: Zenit-4 no. 1. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 6.00 days. Decay Date: 1963-11-22 . USAF Sat Cat: 689 . COSPAR: 1963-045A. Apogee: 376 km (233 mi). Perigee: 193 km (119 mi). Inclination: 64.90 deg. Period: 90.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1963 November 27 - .
21:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2 Agena D.
- KH-4 9061 - .
Payload: KH-4 s/n 9061 / Agena D 1172 / OPS 2260. Mass: 1,150 kg (2,530 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1963-12-15 . USAF Sat Cat: 695 . COSPAR: 1963-048A. Apogee: 368 km (228 mi). Perigee: 182 km (113 mi). Inclination: 69.60 deg. Period: 90.00 min. KH-4. Mission failed. Return capsule separated from satellite but remained in orbit..
1963 November 28 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
FAILURE: Failure of block E upper stage. Spacecraft liquidated by APO destruct system..
Failed Stage: 2.
- Zenit-2 11F61 s/n 14 - .
Payload: Zenit-2 11F61 s/n 14. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1963-11-28 . Area survey photo reconnaissance satellite..
1963 December 18 - .
21:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-04 - .
Payload: KH-7 no. 4 / OPS 2372. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1963-12-20 . USAF Sat Cat: 711 . COSPAR: 1963-051A. Apogee: 266 km (165 mi). Perigee: 122 km (75 mi). Inclination: 97.90 deg. Period: 88.50 min.
Atlas 109F was the final Atlas research and development flight test missile to be launched. Since the first attempted launch of a Series A Atlas on 11 June 1957, 95 Atlas missiles had been used in the R&D program - eight As, nine Bs, six Cs, 32 Ds, 24 Es, and 16 Fs. All but 12 of these were launched from Cape Canaveral. Of the 95 launches, 57 were considered successful while 38 were failures. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
1963 December 19 - .
09:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 24 - .
Payload: Zenit-2 11F61 s/n 15. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 9.00 days. Decay Date: 1963-12-28 . USAF Sat Cat: 712 . COSPAR: 1963-052A. Apogee: 391 km (242 mi). Perigee: 204 km (126 mi). Inclination: 65.00 deg. Period: 90.50 min. Area survey photo reconnaissance satellite..
1963 December 21 - .
21:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4 9062 - .
Payload: KH-4 s/n 9062 / Agena D 1168 / OPS 1388. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4.
Decay Date: 1964-01-08 . USAF Sat Cat: 718 . COSPAR: 1963-055A. Apogee: 337 km (209 mi). Perigee: 178 km (110 mi). Inclination: 64.80 deg. Period: 89.70 min. KH-4; deployed ELINT subsatellite. Corona static fogged much of film..
- Hitch Hiker 3 - .
Payload: P-11 s/n A4. Mass: 80 kg (176 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1964-11-07 . USAF Sat Cat: 719 . COSPAR: 1963-055B. Apogee: 394 km (244 mi). Perigee: 316 km (196 mi). Inclination: 64.50 deg. Period: 91.70 min. Radar monitoring..
1964 January 11 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- Agena D 2354 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
USAF Sat Cat: 727 . COSPAR: 1964-001A. Apogee: 937 km (582 mi). Perigee: 906 km (562 mi). Inclination: 69.90 deg. Period: 103.50 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Unidentified - .
Payload: NRL PL135 / Poppy 3B (Poppy 20-inch). Mass: 40 kg (88 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 731 . COSPAR: 1964-001E. Apogee: 919 km (571 mi). Perigee: 902 km (560 mi). Inclination: 69.90 deg. Period: 103.20 min. Poppy naval signals intelligence satellite..
- Solrad 7A - .
Payload: NRL PL124 / Poppy 3A (Poppy 24-inch). Mass: 45 kg (99 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 730 . COSPAR: 1964-001D. Apogee: 920 km (570 mi). Perigee: 902 km (560 mi). Inclination: 69.90 deg. Period: 103.20 min. Poppy naval signals intelligence satellite. Official and secondary mission: Solar radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1964 February 15 - .
21:38 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1004 - .
Payload: KH-4A s/n 1004 / Agena D 1174 / OPS 3444. Mass: 1,590 kg (3,500 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-03-09 . USAF Sat Cat: 752 . COSPAR: 1964-008A. Apogee: 429 km (266 mi). Perigee: 172 km (106 mi). Inclination: 74.90 deg. Period: 90.50 min. KH-4A. Main cameras operated satisfactorily. Minor degradations due to static and light leaks..
1964 February 25 - .
18:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-05 - .
Payload: KH-7 no. 5 / OPS 2423. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-03-01 . USAF Sat Cat: 754 . COSPAR: 1964-009A. Apogee: 135 km (83 mi). Perigee: 135 km (83 mi). Inclination: 95.60 deg. Period: 87.20 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1964 February 28 - .
03:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 3722 - .
Payload: Ferret 5 / Agena D 2316. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-02-19 . USAF Sat Cat: 759 . COSPAR: 1964-011A. Apogee: 516 km (320 mi). Perigee: 491 km (305 mi). Inclination: 82.10 deg. Period: 94.70 min.
1964 March 11 - .
20:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-06 - .
Payload: KH-7 no. 6 / OPS 3435. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-03-16 . USAF Sat Cat: 764 . COSPAR: 1964-012A. Apogee: 203 km (126 mi). Perigee: 163 km (101 mi). Inclination: 95.70 deg. Period: 88.20 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1964 March 24 - .
22:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-4A 1003 - .
Payload: KH-4A s/n 1003. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-03-24 . KH-4A. Mission failed..
1964 April 4 - .
09:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 28 - .
Payload: Zenit-2 11F61 s/n 16. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1964-04-12 . USAF Sat Cat: 779 . COSPAR: 1964-017A. Apogee: 373 km (231 mi). Perigee: 213 km (132 mi). Inclination: 65.00 deg. Period: 90.40 min. Area survey photo reconnaissance satellite..
1964 April 23 - .
16:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-07 - .
Payload: KH-7 no. 7 / OPS 3743. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-04-29 . USAF Sat Cat: 786 . COSPAR: 1964-020A. Apogee: 336 km (208 mi). Perigee: 150 km (90 mi). Inclination: 103.60 deg. Period: 89.40 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1964 April 25 - .
10:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 29 - .
Payload: Zenit-2 11F61 s/n 19. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 7.00 days. Decay Date: 1964-05-02 . USAF Sat Cat: 791 . COSPAR: 1964-021A. Apogee: 292 km (181 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite..
1964 April 27 - .
23:23 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1005 - .
Payload: KH-4A s/n 1005 / Agena D 1604 / OPS 2921. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-05-26 . USAF Sat Cat: 796 . COSPAR: 1964-022A. Apogee: 445 km (276 mi). Perigee: 175 km (108 mi). Inclination: 79.90 deg. Period: 90.80 min. KH-4A. Mission failed. Recovery vehicle impacted in Venezuela..
1964 May 18 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 30 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1964-05-26 . USAF Sat Cat: 797 . COSPAR: 1964-023A. Apogee: 366 km (227 mi). Perigee: 206 km (128 mi). Inclination: 64.90 deg. Period: 90.30 min. High resolution photo reconnaissance satellite; returned film capsule.
1964 May 19 - .
19:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-08 - .
Payload: KH-7 no. 8 / OPS 3592. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-05-22 . USAF Sat Cat: 799 . COSPAR: 1964-024A. Apogee: 380 km (230 mi). Perigee: 141 km (87 mi). Inclination: 101.10 deg. Period: 89.70 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1964 June 4 - .
22:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1006 - .
Payload: KH-4A s/n 1006 / Agena D 1176 / OPS 3483. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-06-18 . USAF Sat Cat: 802 . COSPAR: 1964-027A. Apogee: 429 km (266 mi). Perigee: 149 km (92 mi). Inclination: 80.00 deg. Period: 90.30 min. KH-4A. Highest quality imagery attained to date from the KH-4 system..
1964 June 10 - .
10:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 32 - .
Payload: Zenit-2 11F61 s/n 18. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1964-06-18 . USAF Sat Cat: 807 . COSPAR: 1964-029A. Apogee: 322 km (200 mi). Perigee: 205 km (127 mi). Inclination: 51.30 deg. Period: 89.80 min. Area survey photo reconnaissance satellite..
1964 June 13 - .
15:47 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-5 9065A - .
Payload: KH-5 s/n 9065A / OPS 3236. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1965-06-02 . USAF Sat Cat: 811 . COSPAR: 1964-030A. Apogee: 362 km (224 mi). Perigee: 352 km (218 mi). Inclination: 114.90 deg. Period: 91.70 min. KH-5; carried Star Flash experiment. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1964 June 19 - .
23:18 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1007 - .
Payload: KH-4A s/n 1007 / Agena D 1609 / OPS 3754. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-07-16 . USAF Sat Cat: 814 . COSPAR: 1964-032A. Apogee: 451 km (280 mi). Perigee: 180 km (110 mi). Inclination: 85.00 deg. Period: 90.90 min. KH-4A. Out-of-focus area on some film..
1964 June 23 - .
10:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 33 - .
Payload: Zenit-2 11F61 s/n 20. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1964-07-01 . USAF Sat Cat: 816 . COSPAR: 1964-033A. Apogee: 279 km (173 mi). Perigee: 205 km (127 mi). Inclination: 64.90 deg. Period: 89.40 min. Area survey photo reconnaissance satellite..
1964 July 1 - .
11:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 34 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1964-07-09 . USAF Sat Cat: 822 . COSPAR: 1964-034A. Apogee: 342 km (212 mi). Perigee: 201 km (124 mi). Inclination: 64.90 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1964 July 2 - .
23:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 3395 - .
Payload: Ferret 6 / Agena D 2315. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-08-07 . USAF Sat Cat: 824 . COSPAR: 1964-035A. Apogee: 520 km (320 mi). Perigee: 502 km (311 mi). Inclination: 82.10 deg. Period: 94.90 min.
1964 July 6 - .
18:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-09 - .
Payload: KH-7 no. 9 / OPS 3684. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-07-08 . USAF Sat Cat: 825 . COSPAR: 1964-036A. Apogee: 345 km (214 mi). Perigee: 121 km (75 mi). Inclination: 92.90 deg. Period: 89.10 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 4923 - .
Payload: EHH A3. Mass: 80 kg (176 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1965-01-03 . USAF Sat Cat: 826 . COSPAR: 1964-036B. Apogee: 505 km (313 mi). Perigee: 156 km (96 mi). Inclination: 92.90 deg. Period: 91.10 min. Radar monitoring..
1964 July 10 - .
23:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1008 - .
Payload: KH-4A s/n 1008 / Agena D 1117 / OPS 3491. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-08-06 . USAF Sat Cat: 828 . COSPAR: 1964-037A. Apogee: 346 km (214 mi). Perigee: 173 km (107 mi). Inclination: 84.90 deg. Period: 89.70 min. KH-4A. Cameras operated satisfactorily, some light leaks..
1964 July 15 - .
11:31 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 35 - .
Payload: Zenit-2 11F61 s/n 21. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1964-07-23 . USAF Sat Cat: 833 . COSPAR: 1964-039A. Apogee: 258 km (160 mi). Perigee: 218 km (135 mi). Inclination: 51.30 deg. Period: 89.20 min. Area survey photo reconnaissance satellite..
1964 July 17 - .
08:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- Vela 3 - .
Payload: Vela 2A / OPS 3662. Mass: 220 kg (480 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Vela.
USAF Sat Cat: 836 . COSPAR: 1964-040A. Apogee: 104,101 km (64,685 mi). Perigee: 102,500 km (63,600 mi). Inclination: 39.10 deg. Period: 6,024.80 min.
An Atlas D/Agena D launch vehicle (Atlas 216D), carrying the second set of Vela Nuclear Detection Satellites, was launched from Cape Canaveral and placed the satellites in their prescribed orbits. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
- Vela 4 - .
Payload: Vela 2B / OPS 3674. Mass: 220 kg (480 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Vela.
USAF Sat Cat: 837 . COSPAR: 1964-040B. Apogee: 114,000 km (70,000 mi). Perigee: 92,103 km (57,230 mi). Inclination: 40.80 deg. Period: 6,004.30 min.
An Atlas D/Agena D launch vehicle (Atlas 216D), carrying the second set of Vela Nuclear Detection Satellites, was launched from Cape Canaveral and placed the satellites in their prescribed orbits. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
1964 August 5 - .
23:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1009 - .
Payload: KH-4A s/n 1009 / Agena D 1605 / OPS 3042. Mass: 1,540 kg (3,390 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-09-01 . USAF Sat Cat: 846 . COSPAR: 1964-043A. Apogee: 436 km (270 mi). Perigee: 182 km (113 mi). Inclination: 80.00 deg. Period: 90.70 min. KH-4A. Cameras operated successfully..
1964 August 14 - .
09:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 37 - .
Payload: Zenit-2 11F61 s/n 22. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1964-08-22 . USAF Sat Cat: 848 . COSPAR: 1964-044A. Apogee: 240 km (140 mi). Perigee: 208 km (129 mi). Inclination: 64.90 deg. Period: 88.90 min. Area survey photo reconnaissance satellite. Program partially completed. Break in the film fof the SA-10 camera..
1964 August 14 - .
22:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-10 - .
Payload: KH-7 no. 10 / OPS 3802. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-08-23 . USAF Sat Cat: 850 . COSPAR: 1964-045A. Apogee: 300 km (180 mi). Perigee: 165 km (102 mi). Inclination: 95.40 deg. Period: 89.10 min.
The first Atlas/Agena D standard launch vehicle (SLV-3, 7100 Series) was successfully launched from Vandenberg AFB. This vehicle, Number 7101, was the first Atlas booster to be designed and produced to fully standardized specifications. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
- OPS 3316 - .
Payload: P-11 s/n 4202. Mass: 79 kg (174 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1979-03-08 . USAF Sat Cat: 851 . COSPAR: 1964-045B. Apogee: 3,751 km (2,330 mi). Perigee: 272 km (169 mi). Inclination: 95.70 deg. Period: 127.40 min. The first Atlas/Agena D standard launch vehicle (SLV-3, 7100 Series) was successfully launched from Vandenberg AFB. This vehicle, Number 7101, was the first Atlas booster to be designed and produced to fully standardized specifications. .
1964 August 21 - .
15:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-5 9066A - .
Payload: KH-5 s/n 9066A / Agena D 1603 / OPS 2739. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-5.
Decay Date: 1965-03-31 . USAF Sat Cat: 861 . COSPAR: 1964-048A. Apogee: 363 km (225 mi). Perigee: 351 km (218 mi). Inclination: 114.90 deg. Period: 91.70 min. KH-5. 15% of stellar film degraded by flare. Image smearing on leading edge of main camera film. Final ARGON mission. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
1964 September 13 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
1964 September 14 - .
22:53 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1010 - .
Payload: KH-4A s/n 1010 / Agena D 1178 / OPS 3497. Mass: 1,330 kg (2,930 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-10-06 . USAF Sat Cat: 882 . COSPAR: 1964-056A. Apogee: 455 km (282 mi). Perigee: 174 km (108 mi). Inclination: 84.90 deg. Period: 90.90 min. KH-4A. Small out of focus areas on both cameras at random times throughout the mission..
1964 September 23 - .
20:06 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-11 - .
Payload: KH-7 no. 11 / OPS 4262. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-09-28 . USAF Sat Cat: 884 . COSPAR: 1964-058A. Apogee: 303 km (188 mi). Perigee: 143 km (88 mi). Inclination: 92.90 deg. Period: 88.90 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1964 September 24 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 46 - .
Payload: Zenit-2 11F61 s/n 23. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1964-10-02 . USAF Sat Cat: 885 . COSPAR: 1964-059A. Apogee: 264 km (164 mi). Perigee: 211 km (131 mi). Inclination: 51.30 deg. Period: 89.20 min. Area survey photo reconnaissance satellite. Demonstration launch witnessed by Khrushchev..
1964 October 5 - .
21:50 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
1964 October 6 - .
17:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor Ablestar.
- Calsphere 2 - .
Payload: Dragsphere 2. Mass: 10 kg (22 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
USAF Sat Cat: 902 . COSPAR: 1964-063E. Apogee: 1,078 km (669 mi). Perigee: 1,049 km (651 mi). Inclination: 90.20 deg. Period: 106.50 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Calsphere 1 - .
Payload: Dragsphere 1. Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
USAF Sat Cat: 900 . COSPAR: 1964-063C. Apogee: 1,034 km (642 mi). Perigee: 997 km (619 mi). Inclination: 90.10 deg. Period: 105.50 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1964 October 8 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-7 12 - .
Payload: KH-7 no. 12. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-10-08 . KH-7 type satellite..
1964 October 14 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 48 - .
Payload: Zenit-2 11F61 s/n 24. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 6.00 days. Decay Date: 1964-10-20 . USAF Sat Cat: 908 . COSPAR: 1964-066A. Apogee: 284 km (176 mi). Perigee: 204 km (126 mi). Inclination: 65.10 deg. Period: 89.30 min. Area survey photo reconnaissance satellite. Program partially completed. Returned early due to failure of spacecraft thermoregulation system; internal temperature rose to 43 degrees C..
1964 October 17 - .
22:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1012 - .
Payload: KH-4A s/n 1012 / Agena D 1179 / OPS 3559. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-11-04 . USAF Sat Cat: 911 . COSPAR: 1964-067A. Apogee: 416 km (258 mi). Perigee: 189 km (117 mi). Inclination: 75.00 deg. Period: 90.60 min. KH-4A. Vehicle attitude became erratic on the second portion of the mission necessitating an early recovery..
1964 October 23 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- KH 7-13 - .
Payload: KH-7 no. 13 / OPS 4384. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-10-28 . USAF Sat Cat: 912 . COSPAR: 1964-068A. Apogee: 267 km (165 mi). Perigee: 140 km (80 mi). Inclination: 95.50 deg. Period: 88.50 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- SRV - .
Nation: USA.
Agency: USAF AFSC.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1965-02-23 . USAF Sat Cat: 914 . COSPAR: 1964-068xx. Apogee: 185 km (114 mi). Perigee: 185 km (114 mi). Inclination: 95.40 deg. Period: 88.20 min.
1964 October 28 - .
10:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 50 - .
Payload: Zenit-2 11F61 s/n 25. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1964-11-05 . USAF Sat Cat: 919 . COSPAR: 1964-070A. Apogee: 232 km (144 mi). Perigee: 190 km (110 mi). Inclination: 51.20 deg. Period: 88.70 min. Area survey photo reconnaissance satellite. Unsuccessful mission. Failure of the braking engine system. Spacecraft ordered to self destruct..
1964 November 2 - .
21:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1013 - .
Payload: KH-4A s/n 1013 - Agena D 1173 / OPS 5434. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-11-28 . USAF Sat Cat: 921 . COSPAR: 1964-071A. Apogee: 210 km (130 mi). Perigee: 181 km (112 mi). Inclination: 51.20 deg. Period: 88.40 min. KH-4A. Program anomaly occurred immediately after launch when both cameras operated for 417 frames. Main cameras ceased operation on rev 52D of first portion of mission negating second portion. About 65% of aft camera film is out of focus..
1964 November 4 - .
02:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 3062 - .
Payload: Ferret 7 / Agena D 2317. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-11-05 . USAF Sat Cat: 922 . COSPAR: 1964-072A. Apogee: 526 km (326 mi). Perigee: 512 km (318 mi). Inclination: 82.00 deg. Period: 95.00 min.
1964 November 18 - .
20:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1014 (ORBIS) - .
Payload: KH-4A s/n 1014 & Orbis / Agena D 1180 / OPS 3360. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-12-06 . USAF Sat Cat: 930 . COSPAR: 1964-075A. Apogee: 329 km (204 mi). Perigee: 177 km (109 mi). Inclination: 70.00 deg. Period: 89.60 min. KH-4A. Cameras operated successfully..
1964 December 4 - .
18:57 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-14 - .
Payload: KH-7 no. 14 / OPS 4439. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1964-12-05 . USAF Sat Cat: 946 . COSPAR: 1964-079A. Apogee: 357 km (221 mi). Perigee: 158 km (98 mi). Inclination: 97.00 deg. Period: 89.70 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1964 December 19 - .
21:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1015 - .
Payload: KH-4A s/n 1015 / Agena D 1607 / OPS 3358. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-01-14 . USAF Sat Cat: 961 . COSPAR: 1964-085A. Apogee: 405 km (251 mi). Perigee: 193 km (119 mi). Inclination: 74.90 deg. Period: 90.50 min. KH-4A. Discrepancies in planned and actual coverage due to telemetry problems during the first 6 revolutions. Small out-of-focus areas on film from aft camera..
1965 January 11 - .
09:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 52 - .
Payload: Zenit-2 11F61 s/n 26. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1965-01-19 . USAF Sat Cat: 968 . COSPAR: 1965-001A. Apogee: 298 km (185 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite..
1965 January 15 - .
21:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1016 - .
Payload: KH-4A s/n 1016 / Agena D 1608 / OPS 3928. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-02-09 . USAF Sat Cat: 972 . COSPAR: 1965-002A. Apogee: 420 km (260 mi). Perigee: 180 km (110 mi). Inclination: 75.00 deg. Period: 90.50 min. KH-4A. Smearing of highly reflective images due to reflections within camera..
1965 January 23 - .
20:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-15 - .
Payload: KH-7 no. 15 / OPS 4703. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-01-29 . USAF Sat Cat: 980 . COSPAR: 1965-005A. Apogee: 291 km (180 mi). Perigee: 146 km (90 mi). Inclination: 102.50 deg. Period: 88.90 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1965 February 25 - .
21:44 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1017 - .
Payload: KH-4A s/n 1017 / Agena D 1611 / OPS 4782. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-03-18 . USAF Sat Cat: 1096 . COSPAR: 1965-013A. Apogee: 377 km (234 mi). Perigee: 177 km (109 mi). Inclination: 75.10 deg. Period: 90.10 min. KH-4A. Capping shutter malfunction occurred during last 5 passes of mission..
1965 March 7 - .
09:07 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 59 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-03-15 . USAF Sat Cat: 1191 . COSPAR: 1965-015A. Apogee: 321 km (199 mi). Perigee: 205 km (127 mi). Inclination: 64.90 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule fitted with airlock mating ring planned for Voskhod-2 spacecraft..
1965 March 9 - .
18:29 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2 Agena D.
- Solrad 6B - .
Payload: NRL PL142 / OPS 4988 / Poppy 4B (Poppy 24-inch). Mass: 40 kg (88 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 1271 . COSPAR: 1965-016A. Apogee: 924 km (574 mi). Perigee: 896 km (556 mi). Inclination: 70.10 deg. Period: 103.20 min.
A Thor/Agena D booster was employed to launch eight military satellites into orbit from Vandenberg AFB. This was the largest number of individual payloads yet orbited by the United States with one launch vehicle. First launch of a quadruplet of Poppy naval signals intelligence satellites, which would lead to the NOSS production series. Official and secondary mission: Solar radiation data.
- GGSE 3 - .
Payload: NRL PL144 / Poppy 4D (Poppy 24-inch). Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 1292 . COSPAR: 1965-016C. Apogee: 915 km (568 mi). Perigee: 886 km (550 mi). Inclination: 70.10 deg. Period: 103.00 min. Poppy naval signals intelligence satellite. Official and secondary mission: Gravity gradient stabilization tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Solrad 7B - .
Payload: NRL PL141 / Poppy 4A (Poppy 24-inch). Mass: 47 kg (103 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 1291 . COSPAR: 1965-016D. Apogee: 928 km (576 mi). Perigee: 901 km (559 mi). Inclination: 70.10 deg. Period: 103.30 min. Solar radiation monitoring. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- GGSE 2 - .
Payload: NRL PL143 / Poppy 4C (Poppy 24-inch). Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 1244 . COSPAR: 1965-016B. Apogee: 925 km (574 mi). Perigee: 898 km (557 mi). Inclination: 70.10 deg. Period: 103.20 min. Poppy naval signals intelligence satellite. Official and secondary mission: Gravity gradient stabilization tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- SURCAL 2B - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SURCAL.
Decay Date: 1981-03-27 . USAF Sat Cat: 1310 . COSPAR: 1965-016G. Apogee: 947 km (588 mi). Perigee: 902 km (560 mi). Inclination: 70.10 deg. Period: 103.50 min. Surveillance Calibration. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1965 March 12 - .
19:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-16 - .
Payload: KH-7 no. 16 / OPS 4920. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-03-17 . USAF Sat Cat: 1247 . COSPAR: 1965-019A. Apogee: 358 km (222 mi). Perigee: 223 km (138 mi). Inclination: 107.50 deg. Period: 90.30 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1965 March 25 - .
10:04 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 64 - .
Payload: Zenit-2 11F61 s/n 17. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1965-04-02 . USAF Sat Cat: 1305 . COSPAR: 1965-025A. Apogee: 250 km (150 mi). Perigee: 205 km (127 mi). Inclination: 65.00 deg. Period: 89.10 min. Area survey photo reconnaissance satellite..
1965 March 25 - .
21:11 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1018 - .
Payload: KH-4A s/n 1018 / Agena D 1612 / OPS 4803. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-04-04 . USAF Sat Cat: 1307 . COSPAR: 1965-026A. Apogee: 381 km (236 mi). Perigee: 237 km (147 mi). Inclination: 96.00 deg. Period: 90.70 min. KH-4A. Cameras operated successfully. First KH-4A reconnaissance system to be launched into a retrograde orbit..
1965 April 17 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 65 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-04-25 . USAF Sat Cat: 1320 . COSPAR: 1965-029A. Apogee: 315 km (195 mi). Perigee: 207 km (128 mi). Inclination: 65.00 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; also carried weather experiments..
1965 April 28 - .
20:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-17 - .
Payload: KH-7 no. 17 / OPS 4983. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-05-03 . USAF Sat Cat: 1327 . COSPAR: 1965-031A. Apogee: 259 km (160 mi). Perigee: 180 km (110 mi). Inclination: 95.60 deg. Period: 89.00 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6717 - .
Payload: EHH B1. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1969-10-31 . USAF Sat Cat: 1329 . COSPAR: 1965-031B. Apogee: 547 km (339 mi). Perigee: 506 km (314 mi). Inclination: 95.20 deg. Period: 95.10 min. Radar monitoring..
1965 April 29 - .
21:44 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1019 - .
Payload: KH-4A s/n 1019 / Agena D 1614 / OPS 5023. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-05-26 . USAF Sat Cat: 1330 . COSPAR: 1965-033A. Apogee: 461 km (286 mi). Perigee: 181 km (112 mi). Inclination: 85.00 deg. Period: 91.00 min. KH-4A. Cameras operated successfully. Malfunction in recovery mode on 1019-2 negated recovery..
1965 May 6 - .
15:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC20.
LV Family:
Titan.
Launch Vehicle:
Titan IIIA.
- LCS 1 - .
Mass: 34 kg (74 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: LCS.
USAF Sat Cat: 1361 . COSPAR: 1965-034C. Apogee: 2,795 km (1,736 mi). Perigee: 2,786 km (1,731 mi). Inclination: 32.10 deg. Period: 145.60 min.
The fourth Titan IIIA flight test missile (Vehicle #6) was launched from Complex 20 at Cape Canaveral in a maneuverability test for the Transtage. The primary aim was for the Transtage engine to accomplish four separate ignitions, something never before attempted. In the process of successfully completing its four programmed ignitions and burns, the Transtage placed two satellites into orbit - a Lincoln Experimental Satellite (LES-2) and a hollow aluminum radar calibration sphere (LCS-1). By completing its assigned tasks, the Transtage extended the capabilities of the Titan IIIA beyond it's specific requirements. Because of this highly productive mission, the planned fifth Titan IIIA (Vehicle 7/4) launch was cancelled and the booster was converted to a Titan IIIC configuration. Aluminum sphere used for radar calibration. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
1965 May 7 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 66 - .
Payload: Zenit-2 11F61 s/n 27. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1965-05-15 . USAF Sat Cat: 1362 . COSPAR: 1965-035A. Apogee: 397 km (246 mi). Perigee: 285 km (177 mi). Inclination: 64.90 deg. Period: 91.30 min. Returned after 8 days. Unsuccessful mission. Parachute deployment failure. Spacecraft destroyed in crash..
1965 May 18 - .
18:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1021 - .
Payload: KH-4A s/n 1021 / Agena D 1615 / OPS 8431. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-06-15 . USAF Sat Cat: 1374 . COSPAR: 1965-037A. Apogee: 399 km (247 mi). Perigee: 321 km (199 mi). Inclination: 75.00 deg. Period: 91.70 min. KH-4A. Aft camera ceased operation on pass 102..
1965 May 25 - .
10:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 67 - .
Payload: Zenit-4. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-06-02 . USAF Sat Cat: 1382 . COSPAR: 1965-040A. Apogee: 351 km (218 mi). Perigee: 203 km (126 mi). Inclination: 51.80 deg. Period: 90.10 min. High resolution photo reconnaissance satellite; returned film capsule.
1965 May 27 - .
19:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-18 - .
Payload: KH-7 no. 18 / OPS 5236. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-06-01 . USAF Sat Cat: 1386 . COSPAR: 1965-041A. Apogee: 267 km (165 mi). Perigee: 149 km (92 mi). Inclination: 95.60 deg. Period: 88.70 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1965 June 9 - .
21:58 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1020 - .
Payload: KH-4A s/n 1020 / Agena D 1613 / OPS 8425. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-06-15 . USAF Sat Cat: 1396 . COSPAR: 1965-045A. Apogee: 355 km (220 mi). Perigee: 176 km (109 mi). Inclination: 75.10 deg. Period: 89.90 min. KH-4A. All cameras operated satisfactorily. Erratic attitude caused an early recovery after the second day of 1020-2..
1965 June 15 - .
10:04 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 68 - .
Payload: Zenit-2 11F61 s/n 29. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1965-06-23 . USAF Sat Cat: 1404 . COSPAR: 1965-046A. Apogee: 306 km (190 mi). Perigee: 208 km (129 mi). Inclination: 65.00 deg. Period: 89.70 min. Area survey photo reconnaissance satellite..
1965 June 25 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 69 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-07-03 . USAF Sat Cat: 1421 . COSPAR: 1965-049A. Apogee: 310 km (190 mi). Perigee: 206 km (128 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1965 June 25 - .
19:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- OPS 6749 - .
Payload: EHH B2. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1968-08-22 . USAF Sat Cat: 1422 . COSPAR: 1965-050A. Apogee: 510 km (310 mi). Perigee: 496 km (308 mi). Inclination: 107.60 deg. Period: 94.70 min. Radar monitoring..
- KH 7-19 - .
Payload: KH-7 no. 19 / OPS 5501. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-06-30 . USAF Sat Cat: 1424 . COSPAR: 1965-050B. Apogee: 349 km (216 mi). Perigee: 254 km (157 mi). Inclination: 107.60 deg. Period: 90.50 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1965 July 12 - .
19:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-7-20 - .
Payload: KH-7 no. 20. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-07-12 . KH-7 type satellite..
1965 July 13 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
FAILURE: Second stage guidance failure..
Failed Stage: 2.
- Zenit-2 11F61 s/n 28 - .
Payload: Zenit-2 11F61 s/n 28. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1965-07-13 . Area survey photo reconnaissance satellite..
1965 July 17 - .
05:55 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 8411 - .
Payload: Ferret 8 / Agena D 2702. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1968-12-18 . USAF Sat Cat: 1447 . COSPAR: 1965-055A. Apogee: 512 km (318 mi). Perigee: 471 km (292 mi). Inclination: 70.20 deg. Period: 94.50 min.
1965 July 19 - .
22:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1022 - .
Payload: KH-4A s/n 1022 / Agena D 1617 / OPS 5543. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-08-18 . USAF Sat Cat: 1457 . COSPAR: 1965-057A. Apogee: 461 km (286 mi). Perigee: 189 km (117 mi). Inclination: 85.10 deg. Period: 91.00 min. KH-4A. All cameras operated satisfactorily..
1965 July 20 - .
08:27 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas Agena D.
- Vela 5 - .
Payload: Vela 3A / OPS 6577. Mass: 235 kg (518 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Vela.
USAF Sat Cat: 1458 . COSPAR: 1965-058A. Apogee: 115,839 km (71,978 mi). Perigee: 106,367 km (66,093 mi). Inclination: 35.20 deg. Period: 6,679.00 min. Air Force Atlas/Agena D lifted the third pair of Vela nuclear detection satellites into their 70,000-mile, nearly circular orbits. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Vela 6 - .
Payload: Vela 3B / OPS 6564. Mass: 235 kg (518 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Vela.
USAF Sat Cat: 1459 . COSPAR: 1965-058B. Apogee: 121,281 km (75,360 mi). Perigee: 101,715 km (63,202 mi). Inclination: 34.20 deg. Period: 6,712.70 min. An Air Force Atlas/Agena D lifted the third pair of Vela nuclear detection satellites into their 70,000-mile, nearly circular orbits. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1965 August 3 - .
11:02 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 77 - .
Payload: Zenit-4. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-08-11 . USAF Sat Cat: 1469 . COSPAR: 1965-061A. Apogee: 281 km (174 mi). Perigee: 200 km (120 mi). Inclination: 51.80 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule.
1965 August 3 - .
19:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-21 - .
Payload: KH-7 no. 21 / OPS 5698. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-08-07 . USAF Sat Cat: 1471 . COSPAR: 1965-062A. Apogee: 352 km (218 mi). Perigee: 278 km (172 mi). Inclination: 107.40 deg. Period: 90.80 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6761 - .
Payload: EHH B3. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1968-06-17 . USAF Sat Cat: 1472 . COSPAR: 1965-062B. Apogee: 515 km (320 mi). Perigee: 501 km (311 mi). Inclination: 107.40 deg. Period: 94.80 min. Radar monitoring..
1965 August 13 - .
22:11 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2E.
LV Family:
Thor.
Launch Vehicle:
Thor Ablestar.
- Dodecapole 2 - .
Payload: PORCUPINE 2. Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: DODECAPOLE.
USAF Sat Cat: 1510 . COSPAR: 1965-065C. Apogee: 1,051 km (653 mi). Perigee: 979 km (608 mi). Inclination: 90.00 deg. Period: 105.40 min. Surveillance Calibration; dodecahedron; extended 12 25 ft. antennas. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Long Rod - .
Payload: Navspasur Rod. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Surcal.
USAF Sat Cat: 1515 . COSPAR: 1965-065G. Apogee: 1,194 km (741 mi). Perigee: 1,090 km (670 mi). Inclination: 90.00 deg. Period: 108.10 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- SURCAL 5 - .
Payload: NRL PL150C?. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SURCAL.
USAF Sat Cat: 1521 . COSPAR: 1965-065K. Apogee: 1,196 km (743 mi). Perigee: 1,083 km (672 mi). Inclination: 90.00 deg. Period: 108.11 min.
- Calsphere 4A - .
Payload: NRL PL 158?. Mass: 2.00 kg (4.40 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
USAF Sat Cat: 1520 . COSPAR: 1965-065H. Apogee: 1,179 km (732 mi). Perigee: 1,077 km (669 mi). Inclination: 90.10 deg. Period: 107.90 min. Surveillance Calibration; white 14 inch dia. sphere. .
- Tempsat 1 - .
Mass: 9.00 kg (19.80 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Tempsat.
USAF Sat Cat: 1512 . COSPAR: 1965-065E. Apogee: 1,188 km (738 mi). Perigee: 1,082 km (672 mi). Inclination: 89.90 deg. Period: 108.00 min. Surveillance Calibration; black 14 inch dia. sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1965 August 14 - .
11:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 78 - .
Payload: Zenit-2 11F61 s/n 30. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1965-08-22 . USAF Sat Cat: 1505 . COSPAR: 1965-066A. Apogee: 379 km (235 mi). Perigee: 330 km (200 mi). Inclination: 69.00 deg. Period: 91.60 min. Area survey photo reconnaissance satellite..
1965 August 17 - .
20:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1023 - .
Payload: KH-4A s/n 1023 / Agena D 1618 / OPS 7208. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-10-11 . USAF Sat Cat: 1513 . COSPAR: 1965-067A. Apogee: 399 km (247 mi). Perigee: 179 km (111 mi). Inclination: 70.00 deg. Period: 90.30 min. KH-4A. Program anomaly caused the fore camera to cease operation during revolutions 103-132..
1965 August 25 - .
10:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 79 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-09-02 . USAF Sat Cat: 1523 . COSPAR: 1965-069A. Apogee: 338 km (210 mi). Perigee: 206 km (128 mi). Inclination: 64.90 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1965 September 9 - .
09:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 85 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-09-17 . USAF Sat Cat: 1578 . COSPAR: 1965-071A. Apogee: 291 km (180 mi). Perigee: 202 km (125 mi). Inclination: 64.90 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule.
1965 September 22 - .
21:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 102 - .
Payload: KH-4A s/n 102 / Agena D 1619 / OPS 7221. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-10-11 . USAF Sat Cat: 1602 . COSPAR: 1965-074A. Apogee: 364 km (226 mi). Perigee: 191 km (118 mi). Inclination: 80.00 deg. Period: 90.00 min. KH-4A. All cameras operated satisfactorily. Cameras not operated on passes 88D-93D..
1965 September 23 - .
09:07 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 91 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-10-01 . USAF Sat Cat: 1603 . COSPAR: 1965-075A. Apogee: 324 km (201 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1965 September 30 - .
19:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-22 - .
Payload: KH-7 no. 22 / OPS 7208. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-10-05 . USAF Sat Cat: 1609 . COSPAR: 1965-076A. Apogee: 361 km (224 mi). Perigee: 237 km (147 mi). Inclination: 95.60 deg. Period: 90.50 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1965 October 5 - .
17:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1025 - .
Payload: KH-4A s/n 1025 / Agena D 1616 / OPS 5325. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-10-29 . USAF Sat Cat: 1615 . COSPAR: 1965-079A. Apogee: 322 km (200 mi). Perigee: 202 km (125 mi). Inclination: 75.10 deg. Period: 89.70 min. KH-4A. Main cameras operated satisfactorily..
1965 October 15 - .
17:23 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
FAILURE: Partial Failure..
Failed Stage: U.
- LCS 2 - .
Payload: OV2-01 / Transtage 4. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: LCS.
Decay Date: 1965-10-15 . USAF Sat Cat: 1624 . COSPAR: 1965-082A. Apogee: 785 km (487 mi). Perigee: 730 km (450 mi). Inclination: 32.30 deg. Period: 99.98 min.
The second Titan IIIC (Vehicle #4) was successfully launched from Cape Canaveral. This was the first Titan IIIC to carry an operational payload. Three satellites were placed in orbit - an LCS-2 radar calibration sphere, an OV 2-1 radiation sensor, and a metal-ballasted dummy payload. All systems performed well until the second planned burn of the Transtage engines just prior to the injection of the multiple payload into orbit. At this point in the mission, the Transtage exploded due to a malfunction, abruptly terminating the mission. Dual launch with OV2-1; upper stage broke up.
1965 October 16 - .
08:09 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 92 - .
Payload: Bion precursor. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-10-24 . USAF Sat Cat: 1626 . COSPAR: 1965-083A. Apogee: 331 km (205 mi). Perigee: 204 km (126 mi). Inclination: 64.90 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule; also carried weather and biological experiments..
1965 October 28 - .
08:24 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 94 - .
Payload: Bion precursor. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1965-11-05 . USAF Sat Cat: 1636 . COSPAR: 1965-085A. Apogee: 271 km (168 mi). Perigee: 205 km (127 mi). Inclination: 65.00 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; also carried biological experiments..
1965 October 28 - .
21:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1026 - .
Payload: KH-4A s/n 1026 / Agena D 1620 / OPS 2155. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-11-17 . USAF Sat Cat: 1637 . COSPAR: 1965-086A. Apogee: 432 km (268 mi). Perigee: 173 km (107 mi). Inclination: 74.90 deg. Period: 90.50 min. KH-4A. All cameras operated satisfactorily..
1965 November 8 - .
19:26 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-23 - .
Payload: KH-7 no. 23 / OPS 8293. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1965-11-11 . USAF Sat Cat: 1727 . COSPAR: 1965-090A. Apogee: 352 km (218 mi). Perigee: 280 km (170 mi). Inclination: 93.90 deg. Period: 90.80 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6232/Agena D - .
Payload: Agena Pickaback / OPS 6232. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1965-11-09 . USAF Sat Cat: 1728 . COSPAR: 1965-090B. Apogee: 284 km (176 mi). Perigee: 155 km (96 mi). Inclination: 93.90 deg. Period: 88.90 min. Not identified as a subsatellite ferret by McDowell..
1965 November 27 - .
08:24 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 98 - .
Payload: Zenit-2 11F61 s/n 31. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1965-12-05 . USAF Sat Cat: 1780 . COSPAR: 1965-097A. Apogee: 547 km (339 mi). Perigee: 205 km (127 mi). Inclination: 65.00 deg. Period: 92.10 min. Area survey photo reconnaissance satellite..
1965 December 9 - .
21:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1027 - .
Payload: KH-4A s/n 1027 / Agena D 1621 / OPS 7249. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1965-12-26 . USAF Sat Cat: 1816 . COSPAR: 1965-102A. Apogee: 439 km (272 mi). Perigee: 186 km (115 mi). Inclination: 80.10 deg. Period: 90.80 min. KH-4A. Erratic attitude necessitated recovery after two days of operation. All cameras operated satisfactorily..
1965 December 10 - .
08:09 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 99 - .
Payload: Zenit-2 11F61 s/n 32. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1965-12-18 . USAF Sat Cat: 1817 . COSPAR: 1965-103A. Apogee: 309 km (192 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1965 December 24 - .
21:06 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1028 - .
Payload: KH-4A s/n 1028 / Agena D 1610 / OPS 4639. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-01-20 . USAF Sat Cat: 1866 . COSPAR: 1965-110A. Apogee: 443 km (275 mi). Perigee: 181 km (112 mi). Inclination: 80.00 deg. Period: 90.70 min. KH-4A. Cameras operated satisfactorily..
1965 December 27 - .
22:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A510.
- Cosmos 102 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1966-01-13 . USAF Sat Cat: 1867 . COSPAR: 1965-111A. Apogee: 267 km (165 mi). Perigee: 205 km (127 mi). Inclination: 64.90 deg. Period: 89.20 min. Prototype RORSAT hardware using chemical batteries in place of nuclear reactor..
1966 January 7 - .
08:24 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 104 - .
Payload: Zenit-2 11F61 s/n 36. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-01-15 . USAF Sat Cat: 1903 . COSPAR: 1966-001A. Apogee: 379 km (235 mi). Perigee: 195 km (121 mi). Inclination: 65.00 deg. Period: 90.20 min. Area survey photo reconnaissance satellite. Program not completely met. Spacecraft put into incorrect orbit by abnormal function of second and third stages of booster..
1966 January 19 - .
20:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-24 - .
Payload: KH-7 no. 24 / OPS 7253. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-01-25 . USAF Sat Cat: 1939 . COSPAR: 1966-002A. Apogee: 259 km (160 mi). Perigee: 138 km (85 mi). Inclination: 93.80 deg. Period: 88.40 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 3179/Agena D - .
Payload: Agena Pickaback / OPS 3179. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1966-01-23 . USAF Sat Cat: 1940 . COSPAR: 1966-002B. Apogee: 149 km (92 mi). Perigee: 120 km (70 mi). Inclination: 93.80 deg. Period: 87.20 min. Not identified as a subsatellite ferret by McDowell..
1966 January 22 - .
08:38 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 105 - .
Payload: Zenit-2 11F61 s/n 38. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-01-30 . USAF Sat Cat: 1945 . COSPAR: 1966-003A. Apogee: 311 km (193 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1966 February 2 - .
21:32 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1029 - .
Payload: KH-4A s/n 1029 / Agena D 1623 / OPS 7291. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-02-27 . USAF Sat Cat: 1968 . COSPAR: 1966-007A. Apogee: 428 km (265 mi). Perigee: 182 km (113 mi). Inclination: 75.00 deg. Period: 90.60 min. KH-4A. Both panoramic cameras were operational throughout..
1966 February 9 - .
19:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 1439 - .
Payload: Ferret 9 / Agena D 2703. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-09-26 . USAF Sat Cat: 1997 . COSPAR: 1966-009A. Apogee: 511 km (317 mi). Perigee: 507 km (315 mi). Inclination: 82.00 deg. Period: 94.70 min.
1966 February 10 - .
08:52 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 107 - .
Payload: Zenit-2 11F61 s/n 34. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-02-18 . USAF Sat Cat: 1998 . COSPAR: 1966-010A. Apogee: 313 km (194 mi). Perigee: 216 km (134 mi). Inclination: 65.00 deg. Period: 89.70 min. Area survey photo reconnaissance satellite..
1966 February 15 - .
20:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-25 - .
Payload: KH-7 no. 25 / OPS 1184. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-02-22 . USAF Sat Cat: 2012 . COSPAR: 1966-012A. Apogee: 290 km (180 mi). Perigee: 142 km (88 mi). Inclination: 96.50 deg. Period: 88.90 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Bluebell 2C (Cylinder) - .
Payload: OPS 3011. Mass: 9.00 kg (19.80 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Bluebell.
Decay Date: 1966-02-16 . USAF Sat Cat: 2014 . COSPAR: 1966-012B. Apogee: 253 km (157 mi). Perigee: 115 km (71 mi). Inclination: 96.50 deg. Period: 88.10 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Bluebell 2S (Sphere) - .
Payload: OPS 3031. Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Bluebell.
Decay Date: 1966-02-22 . USAF Sat Cat: 2015 . COSPAR: 1966-012C. Apogee: 268 km (166 mi). Perigee: 147 km (91 mi). Inclination: 96.50 deg. Period: 88.60 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1966 February 19 - .
08:52 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 109 - .
Payload: Bion precursor. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-02-27 . USAF Sat Cat: 2019 . COSPAR: 1966-014A. Apogee: 288 km (178 mi). Perigee: 204 km (126 mi). Inclination: 64.90 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; also carried biological experiments..
1966 March 9 - .
22:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1030 - .
Payload: KH-4A s/n 1030 / Agena D 1622 / OPS 3488. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-03-29 . USAF Sat Cat: 2099 . COSPAR: 1966-018A. Apogee: 418 km (259 mi). Perigee: 180 km (110 mi). Inclination: 75.00 deg. Period: 90.40 min. KH-4A. All cameras operated satisfactorily..
1966 March 17 - .
10:28 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 112 - .
Payload: Zenit-2 11F61 s/n 37. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-03-25 . USAF Sat Cat: 2107 . COSPAR: 1966-021A. Apogee: 664 km (412 mi). Perigee: 214 km (132 mi). Inclination: 72.00 deg. Period: 93.30 min. Area survey photo reconnaissance satellite..
1966 March 18 - .
20:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-26 - .
Payload: KH-7 no. 26 / OPS 0879. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-03-24 . USAF Sat Cat: 2109 . COSPAR: 1966-022A. Apogee: 308 km (191 mi). Perigee: 162 km (100 mi). Inclination: 101.00 deg. Period: 89.30 min. Not identified as a subsatellite ferret by McDowell..
- OPS 0974/Agena D - .
Payload: NRL PL137 / OPS 0974. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1966-03-23 . USAF Sat Cat: 2112 . COSPAR: 1966-022B. Apogee: 285 km (177 mi). Perigee: 149 km (92 mi). Inclination: 101.00 deg. Period: 88.80 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1966 March 21 - .
09:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 113 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-03-29 . USAF Sat Cat: 2114 . COSPAR: 1966-023A. Apogee: 314 km (195 mi). Perigee: 202 km (125 mi). Inclination: 64.90 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 April 6 - .
11:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 114 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-04-14 . USAF Sat Cat: 2133 . COSPAR: 1966-028A. Apogee: 337 km (209 mi). Perigee: 202 km (125 mi). Inclination: 72.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 April 7 - .
22:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1031 - .
Payload: KH-4A s/n 1031 / Agena D 1627 / OPS 1612. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-04-26 . USAF Sat Cat: 2136 . COSPAR: 1966-029A. Apogee: 312 km (193 mi). Perigee: 193 km (119 mi). Inclination: 75.10 deg. Period: 89.60 min. KH-4A. The aft-looking camera malfunctioned after the recovery of bucket '1'. No material was received in bucket '2' (1031-2)..
1966 April 19 - .
19:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-27 - .
Payload: KH-7 no. 27 / OPS 0910. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-04-26 . USAF Sat Cat: 2146 . COSPAR: 1966-032A. Apogee: 375 km (233 mi). Perigee: 139 km (86 mi). Inclination: 116.90 deg. Period: 89.60 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1966 April 20 - .
10:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 115 - .
Payload: Zenit-2 11F61 s/n 35. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-04-28 . USAF Sat Cat: 2147 . COSPAR: 1966-033A. Apogee: 283 km (175 mi). Perigee: 189 km (117 mi). Inclination: 65.00 deg. Period: 89.20 min. . Program partially completed. Abnormal operation of SA-10 camera..
1966 May 3 - .
19:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-4A 1032 - .
Payload: KH-4A s/n 1032. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-05-04 .
1966 May 6 - .
11:02 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 117 - .
Payload: Zenit-2 11F61 s/n 39. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-05-14 . USAF Sat Cat: 2163 . COSPAR: 1966-037A. Apogee: 314 km (195 mi). Perigee: 200 km (120 mi). Inclination: 64.90 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1966 May 14 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-28 - .
Payload: KH-7 no. 28 / OPS 1950. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-05-21 . USAF Sat Cat: 2171 . COSPAR: 1966-039A. Apogee: 319 km (198 mi). Perigee: 130 km (80 mi). Inclination: 110.50 deg. Period: 89.00 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6785 - .
Payload: EHH B4. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1970-10-27 . USAF Sat Cat: 2172 . COSPAR: 1966-039B. Apogee: 555 km (344 mi). Perigee: 519 km (322 mi). Inclination: 110.00 deg. Period: 95.40 min. Radar monitoring..
1966 May 24 - .
02:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1033 - .
Payload: KH-4A s/n 1033 / Agena D 1630 / OPS 1778. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-06-09 . USAF Sat Cat: 2181 . COSPAR: 1966-042A. Apogee: 271 km (168 mi). Perigee: 179 km (111 mi). Inclination: 66.00 deg. Period: 89.00 min. KH-4A. The stellar camera shutter of bucket '2' remained open for approximately 200 frames..
1966 June 3 - .
19:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-29 - .
Payload: KH-7 no. 29 / OPS 1577. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-06-09 . USAF Sat Cat: 2192 . COSPAR: 1966-048A. Apogee: 288 km (178 mi). Perigee: 143 km (88 mi). Inclination: 87.00 deg. Period: 88.90 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 1856/Agena D - .
Payload: [AAS 6] / OPS 1856. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1966-06-09 . USAF Sat Cat: 2194 . COSPAR: 1966-048B. Apogee: 230 km (140 mi). Perigee: 148 km (91 mi). Inclination: 86.90 deg. Period: 88.20 min. Not identified as a subsatellite ferret by McDowell..
1966 June 8 - .
11:02 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 120 - .
Payload: Zenit-2 11F61 s/n 41. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-06-16 . USAF Sat Cat: 2196 . COSPAR: 1966-050A. Apogee: 331 km (205 mi). Perigee: 201 km (124 mi). Inclination: 51.70 deg. Period: 89.80 min. Area survey photo reconnaissance satellite..
1966 June 9 - .
20:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- Midas 10 - .
Payload: Midas RTS 1 / Agena TV 1351 / Agena D 1351 / OPS 1. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
Decay Date: 1966-12-03 . USAF Sat Cat: 2200 . COSPAR: 1966-051A. Apogee: 3,678 km (2,285 mi). Perigee: 154 km (95 mi). Inclination: 90.00 deg. Period: 125.20 min. The first Atlas SLV-3/Agena D (7200 Series, Vehicle #7201) standard booster was successfully launched from Vandenberg. Missile Defense Alarm System. Left in transfer orbit..
1966 June 17 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 121 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-06-25 . USAF Sat Cat: 2210 . COSPAR: 1966-054A. Apogee: 327 km (203 mi). Perigee: 205 km (127 mi). Inclination: 72.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 June 21 - .
21:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1034 - .
Payload: KH-4A s/n 1034 / Agena D 1626 / OPS 1599. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-07-14 . USAF Sat Cat: 2227 . COSPAR: 1966-055A. Apogee: 359 km (223 mi). Perigee: 207 km (128 mi). Inclination: 80.10 deg. Period: 90.10 min. KH-4A. Failure of velocity/altitude programmer produced poor imagery after revolution 5..
1966 July 12 - .
17:57 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-30 - .
Payload: KH-7 no. 30 / OPS 1850. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-07-20 . USAF Sat Cat: 2322 . COSPAR: 1966-062A. Apogee: 261 km (162 mi). Perigee: 150 km (90 mi). Inclination: 95.50 deg. Period: 88.70 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1966 July 14 - .
10:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 124 - .
Payload: Zenit-2 11F61 s/n 42. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-07-22 . USAF Sat Cat: 2325 . COSPAR: 1966-064A. Apogee: 282 km (175 mi). Perigee: 205 km (127 mi). Inclination: 51.80 deg. Period: 89.40 min. Area survey photo reconnaissance satellite..
1966 July 20 - .
09:07 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A510.
- Cosmos 125 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1966-08-02 . USAF Sat Cat: 2351 . COSPAR: 1966-067A. Apogee: 260 km (160 mi). Perigee: 204 km (126 mi). Inclination: 64.90 deg. Period: 89.10 min. Prototype RORSAT hardware using chemical batteries in place of nuclear reactor. Lost on the 52nd revolution as a result of a possible failure in the chemical power units placed on board instead of the nuclear BES-5..
1966 July 28 - .
10:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 126 - .
Payload: Zenit-4. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 9.00 days. Decay Date: 1966-08-06 . USAF Sat Cat: 2368 . COSPAR: 1966-068A. Apogee: 343 km (213 mi). Perigee: 209 km (129 mi). Inclination: 51.80 deg. Period: 90.10 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 July 29 - .
18:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 3014 - .
Payload: KH-8 no. 01 (Gambit) / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1966-08-06 . USAF Sat Cat: 2376 . COSPAR: 1966-069A. Apogee: 252 km (156 mi). Perigee: 154 km (95 mi). Inclination: 94.20 deg. Period: 88.50 min.
After the initial launch attempt oil the 28th was held at T minus 12 seconds, the first Titan IIIB/Agena D was successfully launched from Vandenberg AFB. All primary and secondary test objectives were met during the launch and flight which completed the research and development program for the Titan IIIB. This newest member of the Titan III (SLV-5) KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
1966 August 8 - .
11:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 127 - .
Payload: Zenit-4. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-08-16 . USAF Sat Cat: 2391 . COSPAR: 1966-071A. Apogee: 263 km (163 mi). Perigee: 201 km (124 mi). Inclination: 51.80 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 August 9 - .
20:46 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1036 - .
Payload: KH-4A s/n 1036 / Agena D 1631 / OPS 1545. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-09-11 . USAF Sat Cat: 2393 . COSPAR: 1966-072A. Apogee: 284 km (176 mi). Perigee: 190 km (110 mi). Inclination: 100.10 deg. Period: 89.20 min. KH-4A. All cameras operated satisfactorily..
1966 August 16 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-31 - .
Payload: KH-7 no. 31 / OPS 1832. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-08-24 . USAF Sat Cat: 2396 . COSPAR: 1966-074A. Apogee: 330 km (200 mi). Perigee: 143 km (88 mi). Inclination: 93.20 deg. Period: 89.20 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6810 - .
Payload: SSF-B No. 5. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1970-03-05 . USAF Sat Cat: 2397 . COSPAR: 1966-074B. Apogee: 522 km (324 mi). Perigee: 511 km (317 mi). Inclination: 93.20 deg. Period: 94.90 min. Radar monitoring..
1966 August 19 - .
19:26 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- Midas 11 - .
Payload: Midas RTS 2 / Agena TV 1352 / Agena D / OPS 0856. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
USAF Sat Cat: 2403 . COSPAR: 1966-077A. Apogee: 3,708 km (2,304 mi). Perigee: 3,658 km (2,272 mi). Inclination: 89.70 deg. Period: 167.40 min. Missile Defense Alarm System..
1966 August 27 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1?.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 128 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-09-04 . USAF Sat Cat: 2409 . COSPAR: 1966-079A. Apogee: 343 km (213 mi). Perigee: 207 km (128 mi). Inclination: 64.90 deg. Period: 90.00 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 September 16 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
FAILURE: Launch vehicle destroyed. Failure of Block D core stage..
Failed Stage: 1.
- Zenit-2 11F61 s/n 40 - .
Payload: Zenit-2 11F61 s/n 40. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1966-09-16 . Area survey photo reconnaissance satellite..
1966 September 16 - .
17:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-32 - .
Payload: KH-7 no. 32 / OPS 1686. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-09-23 . USAF Sat Cat: 2419 . COSPAR: 1966-083A. Apogee: 328 km (203 mi). Perigee: 146 km (90 mi). Inclination: 93.90 deg. Period: 89.20 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6874 - .
Payload: EHH B5. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1968-05-09 . USAF Sat Cat: 2420 . COSPAR: 1966-083B. Apogee: 501 km (311 mi). Perigee: 461 km (286 mi). Inclination: 94.10 deg. Period: 94.20 min. Radar monitoring..
1966 September 20 - .
21:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1035 - .
Payload: KH-4A s/n 1035 / Agena D 1628 / OPS 1703. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-10-12 . USAF Sat Cat: 2427 . COSPAR: 1966-085A. Apogee: 430 km (260 mi). Perigee: 182 km (113 mi). Inclination: 85.10 deg. Period: 90.60 min. KH-4A. All cameras operated satisfactorily. First mission flown with pan geometry modification..
1966 September 28 - .
19:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 4096 - .
Payload: KH-8 no. 02 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1966-10-07 . USAF Sat Cat: 2433 . COSPAR: 1966-086A. Apogee: 287 km (178 mi). Perigee: 146 km (90 mi). Inclination: 93.90 deg. Period: 88.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1966 October 5 - .
22:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- Midas 12 - .
Payload: Midas RTS 3 / Agena TV 1353 / Agena D / OPS 1920. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: WS-117.
Spacecraft: Midas.
USAF Sat Cat: 2481 . COSPAR: 1966-089A. Apogee: 3,724 km (2,313 mi). Perigee: 3,657 km (2,272 mi). Inclination: 89.80 deg. Period: 167.60 min. Missile Defense Alarm System..
1966 October 12 - .
19:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-33 - .
Payload: KH-7 no. 33 / OPS 2055. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-10-20 . USAF Sat Cat: 2489 . COSPAR: 1966-090A. Apogee: 287 km (178 mi). Perigee: 155 km (96 mi). Inclination: 91.00 deg. Period: 89.00 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 5345/Agena D - .
Payload: SGLS 1 / OPS 5345. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1966-10-21 . USAF Sat Cat: 2490 . COSPAR: 1966-090B. Apogee: 258 km (160 mi). Perigee: 181 km (112 mi). Inclination: 90.90 deg. Period: 89.00 min. Not identified as a subsatellite ferret by McDowell..
1966 October 14 - .
12:13 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 129 - .
Payload: Zenit-2 11F61 s/n 33. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 7.00 days. Decay Date: 1966-10-21 . USAF Sat Cat: 2491 . COSPAR: 1966-091A. Apogee: 288 km (178 mi). Perigee: 199 km (123 mi). Inclination: 65.40 deg. Period: 89.40 min. Area survey photo reconnaissance satellite..
1966 October 20 - .
08:52 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 130 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-10-28 . USAF Sat Cat: 2502 . COSPAR: 1966-093A. Apogee: 316 km (196 mi). Perigee: 204 km (126 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 November 2 - .
20:23 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-34 - .
Payload: KH-7 no. 34 / OPS 2070. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-11-10 . USAF Sat Cat: 2523 . COSPAR: 1966-098A. Apogee: 305 km (189 mi). Perigee: 159 km (98 mi). Inclination: 91.00 deg. Period: 89.20 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 5424/Agena D - .
Payload: Agena Pickaback / OPS 5424. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1966-11-16 . USAF Sat Cat: 2525 . COSPAR: 1966-098B. Apogee: 324 km (201 mi). Perigee: 208 km (129 mi). Inclination: 91.00 deg. Period: 89.90 min. Not identified as a subsatellite ferret by McDowell..
1966 November 8 - .
19:53 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1037 - .
Payload: KH-4A s/n 1037 / Agena D 1632 / OPS 1866. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1966-11-29 . USAF Sat Cat: 2537 . COSPAR: 1966-102A. Apogee: 300 km (180 mi). Perigee: 179 km (111 mi). Inclination: 100.00 deg. Period: 89.20 min. KH-4A. Second pan geometry mission. Higher than normal base plus fog encountered on both main camera records..
1966 November 12 - .
09:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 131 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-11-20 . USAF Sat Cat: 2568 . COSPAR: 1966-105A. Apogee: 335 km (208 mi). Perigee: 202 km (125 mi). Inclination: 72.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1966 November 19 - .
08:09 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 132 - .
Payload: Zenit-2 11F61 s/n 46. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-11-27 . USAF Sat Cat: 2599 . COSPAR: 1966-106A. Apogee: 257 km (159 mi). Perigee: 202 km (125 mi). Inclination: 65.00 deg. Period: 89.10 min. Area survey photo reconnaissance satellite..
1966 December 3 - .
08:09 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 134 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1966-12-11 . USAF Sat Cat: 2603 . COSPAR: 1966-108A. Apogee: 286 km (177 mi). Perigee: 206 km (128 mi). Inclination: 64.90 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; also carried scientific experiments..
1966 December 5 - .
21:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-35 - .
Payload: KH-7 no. 35 / OPS 1890. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1966-12-14 . USAF Sat Cat: 2606 . COSPAR: 1966-109A. Apogee: 341 km (211 mi). Perigee: 137 km (85 mi). Inclination: 104.60 deg. Period: 89.20 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1966 December 14 - .
18:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 8968 - .
Payload: KH-8 no. 03 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1966-12-24 . USAF Sat Cat: 2618 . COSPAR: 1966-113A. Apogee: 392 km (243 mi). Perigee: 147 km (91 mi). Inclination: 109.50 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1966 December 19 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 136 - .
Payload: Zenit-2 11F61 s/n 47. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1966-12-27 . USAF Sat Cat: 2624 . COSPAR: 1966-115A. Apogee: 281 km (174 mi). Perigee: 197 km (122 mi). Inclination: 64.60 deg. Period: 89.30 min. Area survey photo reconnaissance satellite. Also carried science package..
1966 December 29 - .
12:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 1584 - .
Payload: Ferret 10 / Agena D 2731. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-04-05 . USAF Sat Cat: 2634 . COSPAR: 1966-118A. Apogee: 495 km (307 mi). Perigee: 487 km (302 mi). Inclination: 75.00 deg. Period: 94.40 min.
1967 January 14 - .
21:28 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1038 - .
Payload: KH-4A s/n 1038 / Agena D 1629 / OPS 1664. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1967-02-02 . USAF Sat Cat: 2642 . COSPAR: 1967-002A. Apogee: 355 km (220 mi). Perigee: 177 km (109 mi). Inclination: 80.10 deg. Period: 89.80 min. KH-4A. Fair image quality..
1967 January 19 - .
12:39 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 138 - .
Payload: Zenit-2 11F61 s/n 43. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-01-27 . USAF Sat Cat: 2646 . COSPAR: 1967-004A. Apogee: 273 km (169 mi). Perigee: 190 km (110 mi). Inclination: 64.60 deg. Period: 89.10 min. Area survey photo reconnaissance satellite..
1967 February 2 - .
20:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-36 - .
Payload: KH-7 no. 36 / OPS 4399. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1967-02-12 . USAF Sat Cat: 2664 . COSPAR: 1967-007A. Apogee: 357 km (221 mi). Perigee: 136 km (84 mi). Inclination: 103.00 deg. Period: 89.50 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 February 8 - .
10:19 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 141 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-02-16 . USAF Sat Cat: 2670 . COSPAR: 1967-012A. Apogee: 316 km (196 mi). Perigee: 205 km (127 mi). Inclination: 72.90 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 February 22 - .
22:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1039 - .
Payload: KH-4A s/n 1039 / Agena D 1635 / OPS 4750. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1967-03-11 . USAF Sat Cat: 2686 . COSPAR: 1967-015A. Apogee: 380 km (230 mi). Perigee: 180 km (110 mi). Inclination: 80.00 deg. Period: 90.10 min. KH-4A. Normal KH-4 mission. Light from horizon camera on both main camera records during 1039-1..
1967 February 24 - .
19:55 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 4204 - .
Payload: KH-8 no. 04 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1967-03-06 . USAF Sat Cat: 2687 . COSPAR: 1967-016A. Apogee: 414 km (257 mi). Perigee: 135 km (83 mi). Inclination: 107.00 deg. Period: 90.00 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 February 27 - .
08:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 143 - .
Payload: Zenit-2 11F61 s/n 45. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-03-07 . USAF Sat Cat: 2693 . COSPAR: 1967-017A. Apogee: 390 km (240 mi). Perigee: 202 km (125 mi). Inclination: 64.90 deg. Period: 90.50 min. Placed into orbit with 22.8 second period different from that planned. Area survey photo reconnaissance satellite. Also carried science package..
1967 March 13 - .
12:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 147 - .
Payload: Zenit-2 11F61 s/n 44. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-03-21 . USAF Sat Cat: 2710 . COSPAR: 1967-022A. Apogee: 298 km (185 mi). Perigee: 195 km (121 mi). Inclination: 64.50 deg. Period: 89.40 min. Area survey photo reconnaissance satellite. Program partially completed..
1967 March 22 - .
12:44 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 150 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-03-30 . USAF Sat Cat: 2715 . COSPAR: 1967-025A. Apogee: 341 km (211 mi). Perigee: 178 km (110 mi). Inclination: 65.40 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 March 30 - .
18:54 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1040 - .
Payload: KH-4A s/n 1040 / Agena D 1636 / OPS 4779. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1967-04-17 . USAF Sat Cat: 2736 . COSPAR: 1967-029A. Apogee: 326 km (202 mi). Perigee: 167 km (103 mi). Inclination: 85.00 deg. Period: 89.50 min. KH-4A. Satellite flown nose first, all cameras operated satisfactorily..
1967 April 4 - .
14:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 153 - .
Payload: Zenit-2 11F61 s/n 48. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-04-12 . USAF Sat Cat: 2740 . COSPAR: 1967-030A. Apogee: 279 km (173 mi). Perigee: 199 km (123 mi). Inclination: 64.60 deg. Period: 89.30 min. Area survey photo reconnaissance satellite. Program partially completed. Failure of primary SA-20 camera..
1967 April 12 - .
10:51 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 155 - .
Payload: Zenit-4. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-04-20 . USAF Sat Cat: 2750 . COSPAR: 1967-033A. Apogee: 267 km (165 mi). Perigee: 200 km (120 mi). Inclination: 51.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 April 26 - .
18:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
FAILURE: Stage 2 engine lost thrust..
Failed Stage: 2.
- OPS 4243 - .
Payload: KH-8 no. 05 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1967-04-26 . KH-8 type satellite..
1967 April 28 - .
10:01 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- Vela 7 - .
Payload: Vela 4A / OPS 6638. Mass: 317 kg (698 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Advanced Vela.
USAF Sat Cat: 2765 . COSPAR: 1967-040A. Apogee: 112,627 km (69,983 mi). Perigee: 108,948 km (67,697 mi). Inclination: 32.10 deg. Period: 6,652.10 min.
Two new and heavier Vela Nuclear Detection Satellites and three scientific satellites were placed in orbit by a Titan IIIC (Vehicle #10) launched from Cape Canaveral. The two Vela satellites joined six other Vela spacecraft already on sentry duty 69,000 miles above the earth. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
- Vela 8 - .
Payload: Vela 4B / OPS 6679. Mass: 317 kg (698 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Advanced Vela.
USAF Sat Cat: 2766 . COSPAR: 1967-040B. Apogee: 114,578 km (71,195 mi). Perigee: 107,372 km (66,717 mi). Inclination: 33.10 deg. Period: 6,668.10 min.
Two new and heavier Vela Nuclear Detection Satellites and three scientific satellites were placed in orbit by a Titan IIIC (Vehicle #10) launched from Cape Canaveral. The two Vela satellites joined six other Vela spacecraft already on sentry duty 69,000 miles above the earth. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
1967 May 9 - .
21:50 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
FAILURE: Failure of the booster cut-off switch..
Failed Stage: 1.
- KH-4A 1041 - .
Payload: KH-4A s/n 1041 / Agena D 1634 / OPS 4696. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1967-07-13 . USAF Sat Cat: 2779 . COSPAR: 1967-043A. Apogee: 791 km (491 mi). Perigee: 183 km (113 mi). Inclination: 85.00 deg. Period: 94.30 min. KH-4A. Due to the failure of the booster cut-off switch, the satellite went into a highly eccentric orbit. Significant image degradation..
- SRV 731 - .
Payload: SRV 1041-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1993-03-14 . USAF Sat Cat: 2780 . COSPAR: 1967-043xx. Apogee: 145 km (90 mi). Perigee: 131 km (81 mi). Inclination: 84.90 deg. Period: 87.20 min.
1967 May 12 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92.
- Cosmos 157 - .
Payload: Zenit-2 11F61 s/n 49. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-05-20 . USAF Sat Cat: 2781 . COSPAR: 1967-044A. Apogee: 262 km (162 mi). Perigee: 249 km (154 mi). Inclination: 51.30 deg. Period: 89.60 min. Area survey photo reconnaissance satellite. Program partially completed. Bad quality film loaded into SA-20 camera..
1967 May 22 - .
14:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 161 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-05-30 . USAF Sat Cat: 2812 . COSPAR: 1967-049A. Apogee: 321 km (199 mi). Perigee: 201 km (124 mi). Inclination: 65.60 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 May 22 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-37 - .
Payload: KH-7 no. 37 / OPS 4321. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1967-05-30 . USAF Sat Cat: 2813 . COSPAR: 1967-050A. Apogee: 293 km (182 mi). Perigee: 135 km (83 mi). Inclination: 91.50 deg. Period: 88.80 min. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 5557/Agena D - .
Payload: LOGACS / OPS 5557. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1967-05-27 . USAF Sat Cat: 2816 . COSPAR: 1967-050B. Apogee: 240 km (140 mi). Perigee: 148 km (91 mi). Inclination: 91.50 deg. Period: 88.40 min. Not identified as a subsatellite ferret by McDowell..
1967 May 31 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2 Agena D.
- Surcal 160 - .
Payload: NRL PL160 / Agena D 2704. Mass: 2.00 kg (4.40 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Surcal.
USAF Sat Cat: 2825 . COSPAR: 1967-053B. Apogee: 927 km (576 mi). Perigee: 923 km (573 mi). Inclination: 69.90 deg. Period: 103.50 min. 20 inch dia. calibration sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Calsphere 4 - .
Payload: Agena D 2704 / OPS 5712. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
USAF Sat Cat: 2826 . COSPAR: 1967-053A. Apogee: 834 km (518 mi). Perigee: 815 km (506 mi). Inclination: 69.90 deg. Period: 101.40 min. The last Air Force Thor/Agena D, SLV-2 #443 and SS-01B #2704, was launched from Vandenberg. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- GGSE 5 - .
Payload: NRL PL154 / Poppy 5D (Poppy multifaceted). Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 2834 . COSPAR: 1967-053D. Apogee: 913 km (567 mi). Perigee: 906 km (562 mi). Inclination: 70.00 deg. Period: 103.20 min. Poppy naval signals intelligence satellite. Official and secondary mission: Gravity gradient stabilization tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Calsphere 3 - .
Payload: NRL PL159. Mass: 38 kg (83 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
USAF Sat Cat: 2872 . COSPAR: 1967-053F. Apogee: 906 km (562 mi). Perigee: 900 km (550 mi). Inclination: 70.00 deg. Period: 103.10 min. Surveillance Calibration. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Surcal (151) - .
Payload: NRL PL151 / OPS 5712 / Poppy 5A (Poppy 24-inch). Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 2873 . COSPAR: 1967-053G. Apogee: 910 km (560 mi). Perigee: 902 km (560 mi). Inclination: 70.00 deg. Period: 103.10 min. Poppy naval signals intelligence satellite. Official and secondary mission: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Surcal (153) - .
Payload: NRL PL153 / OPS 5712 / Poppy 5C (Poppy multifacete. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 2874 . COSPAR: 1967-053H. Apogee: 912 km (566 mi). Perigee: 905 km (562 mi). Inclination: 70.00 deg. Period: 103.20 min. Poppy naval signals intelligence satellite. Official and secondary mission: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- SURCAL 150B - .
Payload: NRL PL150B. Mass: 2.00 kg (4.40 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SURCAL.
USAF Sat Cat: 2909 . COSPAR: 1967-053J. Apogee: 816 km (507 mi). Perigee: 805 km (500 mi). Inclination: 70.00 deg. Period: 101.10 min. The last Air Force Thor/Agena D, SLV-2 #443 and SS-01B #2704, was launched from Vandenberg. 16 inch dia. calibration sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 June 1 - .
10:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 162 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-06-09 . USAF Sat Cat: 2827 . COSPAR: 1967-054A. Apogee: 275 km (170 mi). Perigee: 196 km (121 mi). Inclination: 51.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 June 4 - .
18:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-38 - .
Payload: KH-7 no. 38 / OPS 4360. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1967-06-12 . USAF Sat Cat: 2831 . COSPAR: 1967-055A. Apogee: 456 km (283 mi). Perigee: 149 km (92 mi). Inclination: 104.90 deg. Period: 90.60 min. The final Air Force Atlas/Agena D (SLV-3 #7128/SS-01B #4837) was successfully launched from Vandenberg AFB. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 June 8 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 164 - .
Payload: Zenit-2 11F61 s/n 50. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 6.00 days. Decay Date: 1967-06-14 . USAF Sat Cat: 2836 . COSPAR: 1967-057A. Apogee: 317 km (196 mi). Perigee: 185 km (114 mi). Inclination: 65.60 deg. Period: 89.50 min. Area survey photo reconnaissance satellite..
1967 June 16 - .
21:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1042 - .
Payload: KH-4A s/n 1042 / Agena D 1633 / OPS 3559. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1967-07-20 . USAF Sat Cat: 2850 . COSPAR: 1967-062A. Apogee: 380 km (230 mi). Perigee: 169 km (105 mi). Inclination: 80.00 deg. Period: 90.00 min. KH-4A. Small out-of-focus area in forward camera of 1042-1..
- SRV 725 - .
Payload: SRV 1042-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1968-10-22 . USAF Sat Cat: 2851 . COSPAR: 1967-062xx. Apogee: 197 km (122 mi). Perigee: 182 km (113 mi). Inclination: 80.20 deg. Period: 88.30 min.
1967 June 20 - .
16:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 4282 - .
Payload: KH-8 no. 06 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1967-06-30 . USAF Sat Cat: 2858 . COSPAR: 1967-064A. Apogee: 325 km (201 mi). Perigee: 127 km (78 mi). Inclination: 111.40 deg. Period: 89.00 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 June 26 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Launch vehicle failed to orbit - unknown cause..
Failed Stage: U.
1967 July 4 - .
05:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 168 - .
Payload: Zenit-2 11F61 s/n 52. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-07-12 . USAF Sat Cat: 2869 . COSPAR: 1967-067A. Apogee: 230 km (140 mi). Perigee: 223 km (138 mi). Inclination: 51.80 deg. Period: 89.10 min. Area survey photo reconnaissance satellite..
1967 July 25 - .
03:48 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 1879 - .
Payload: Ferret 11 / Agena D 2732. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1969-06-05 . USAF Sat Cat: 2890 . COSPAR: 1967-071A. Apogee: 608 km (377 mi). Perigee: 390 km (240 mi). Inclination: 75.10 deg. Period: 94.50 min.
1967 August 7 - .
21:44 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1043 - .
Payload: KH-4A s/n 1043 / Agena D 1637 / OPS 4827. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1967-09-01 . USAF Sat Cat: 2910 . COSPAR: 1967-076A. Apogee: 346 km (214 mi). Perigee: 174 km (108 mi). Inclination: 79.90 deg. Period: 89.70 min. KH-4A. Forward camera film came out of the rails on pass 230D. Film degraded past this point..
1967 August 9 - .
05:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1/LC31?.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 172 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-08-17 . USAF Sat Cat: 2914 . COSPAR: 1967-078A. Apogee: 277 km (172 mi). Perigee: 206 km (128 mi). Inclination: 51.70 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 August 16 - .
17:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 4886 - .
Payload: KH-8 no. 07 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1967-08-28 . USAF Sat Cat: 2919 . COSPAR: 1967-079A. Apogee: 445 km (276 mi). Perigee: 123 km (76 mi). Inclination: 111.50 deg. Period: 90.10 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 September 1 - .
10:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
FAILURE: Failure of Block I stage at 296 seconds. Remnants of spacecraft and stage fell near Novaya Zemlya..
Failed Stage: 2.
- Zenit-2 11F61 s/n 51 - .
Payload: Zenit-2 11F61 s/n 51. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Decay Date: 1967-09-01 . Area survey photo reconnaissance satellite..
1967 September 11 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 175 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-09-19 . USAF Sat Cat: 2939 . COSPAR: 1967-085A. Apogee: 356 km (221 mi). Perigee: 181 km (112 mi). Inclination: 72.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 September 15 - .
19:41 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4B 1101 - .
Payload: KH-4B s/n 1101 / Agena D 1641 / OPS 5089. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1967-10-04 . USAF Sat Cat: 2946 . COSPAR: 1967-087A. Apogee: 372 km (231 mi). Perigee: 156 km (96 mi). Inclination: 80.00 deg. Period: 89.70 min. KH-4B. First mission of the KH-4B series. Best film to date..
1967 September 16 - .
06:06 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 177 - .
Payload: Zenit-2 11F61 s/n 53. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-09-24 . USAF Sat Cat: 2947 . COSPAR: 1967-088A. Apogee: 267 km (165 mi). Perigee: 201 km (124 mi). Inclination: 51.70 deg. Period: 89.10 min. Area survey photo reconnaissance satellite..
1967 September 19 - .
18:28 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 4941 - .
Payload: KH-8 no. 08 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1967-09-30 . USAF Sat Cat: 2952 . COSPAR: 1967-090A. Apogee: 401 km (249 mi). Perigee: 122 km (75 mi). Inclination: 106.00 deg. Period: 89.70 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 September 26 - .
10:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 180 - .
Payload: Zenit-2 11F61 s/n 54. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-10-04 . USAF Sat Cat: 2966 . COSPAR: 1967-093A. Apogee: 350 km (210 mi). Perigee: 206 km (128 mi). Inclination: 72.80 deg. Period: 90.10 min. Area survey photo reconnaissance satellite..
1967 October 11 - .
11:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 181 - .
Payload: Zenit-2 11F61 s/n 55. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-10-19 . USAF Sat Cat: 2981 . COSPAR: 1967-097A. Apogee: 325 km (201 mi). Perigee: 198 km (123 mi). Inclination: 65.60 deg. Period: 89.70 min. Area survey photo reconnaissance satellite..
1967 October 16 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 182 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-10-24 . USAF Sat Cat: 2995 . COSPAR: 1967-098A. Apogee: 374 km (232 mi). Perigee: 197 km (122 mi). Inclination: 64.90 deg. Period: 90.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 October 25 - .
19:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 4995 - .
Payload: KH-8 no. 09 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1967-11-05 . USAF Sat Cat: 3012 . COSPAR: 1967-103A. Apogee: 431 km (267 mi). Perigee: 134 km (83 mi). Inclination: 111.50 deg. Period: 90.10 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 October 30 - .
17:59 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 189 - .
Payload: Tselina-O Mass Model. Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1978-06-08 . USAF Sat Cat: 3021 . COSPAR: 1967-108A. Apogee: 599 km (372 mi). Perigee: 510 km (310 mi). Inclination: 73.80 deg. Period: 95.70 min. Possible ELINT satellite test..
1967 November 2 - .
21:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1044 - .
Payload: KH-4A s/n 1044 / OPS 0562. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1967-12-02 . USAF Sat Cat: 3024 . COSPAR: 1967-109A. Apogee: 410 km (250 mi). Perigee: 184 km (114 mi). Inclination: 81.50 deg. Period: 90.40 min. KH-4A. All cameras operated fine..
- SRV 733 - .
Payload: SRV 1044-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1969-03-28 . USAF Sat Cat: 3025 . COSPAR: 1967-109xx. Apogee: 208 km (129 mi). Perigee: 179 km (111 mi). Inclination: 81.60 deg. Period: 88.40 min.
1967 November 3 - .
11:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 190 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-11-11 . USAF Sat Cat: 3026 . COSPAR: 1967-110A. Apogee: 327 km (203 mi). Perigee: 197 km (122 mi). Inclination: 65.60 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 November 25 - .
11:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 193 - .
Payload: Zenit-2 11F61 s/n 58. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-12-03 . USAF Sat Cat: 3052 . COSPAR: 1967-117A. Apogee: 756 km (469 mi). Perigee: 745 km (462 mi). Inclination: 74.00 deg. Period: 99.90 min. Area survey photo reconnaissance satellite..
1967 December 3 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 194 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1967-12-11 . USAF Sat Cat: 3055 . COSPAR: 1967-119A. Apogee: 312 km (193 mi). Perigee: 201 km (124 mi). Inclination: 65.60 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1967 December 5 - .
18:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5000 - .
Payload: KH-8 no. 10 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1967-12-16 . USAF Sat Cat: 3058 . COSPAR: 1967-121A. Apogee: 428 km (265 mi). Perigee: 141 km (87 mi). Inclination: 109.50 deg. Period: 90.20 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1967 December 9 - .
22:26 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4B 1102 - .
Payload: KH-4B s/n 1102 / Agena D 1642 / OPS 1001. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1967-12-25 . USAF Sat Cat: 3063 . COSPAR: 1967-122A. Apogee: 248 km (154 mi). Perigee: 151 km (93 mi). Inclination: 81.60 deg. Period: 88.40 min. KH-4B. Noticeable image smear for forward camera, but best imagery to date..
1967 December 16 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 195 - .
Payload: Zenit-2 11F61 s/n 57. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1967-12-24 . USAF Sat Cat: 3071 . COSPAR: 1967-124A. Apogee: 352 km (218 mi). Perigee: 204 km (126 mi). Inclination: 65.60 deg. Period: 90.00 min. Area survey photo reconnaissance satellite..
1967 December 27 - .
11:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2A.
- Cosmos 198 - .
Payload: US-A no. 1. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1968-01-21 . USAF Sat Cat: 3082 . COSPAR: 1967-127B. Apogee: 927 km (576 mi). Perigee: 907 km (563 mi). Inclination: 65.10 deg. Period: 103.40 min. Prototype RORSAT hardware using chemical batteries in place of BES-5 nuclear reactor. First satellite to be boosted to 900 km storage orbit..
1968 January 16 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 199 - .
Payload: Zenit-2 11F61 s/n 59. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 16.00 days. Decay Date: 1968-02-01 . USAF Sat Cat: 3099 . COSPAR: 1968-003C. Apogee: 363 km (225 mi). Perigee: 206 km (128 mi). Inclination: 65.60 deg. Period: 90.20 min.
Area survey photo reconnaissance satellite. Unsuccessful mission. Spacecraft failed to separate from Block I stage. Attempt was made to conduct mission without orientation system. APO self destruct system destroyed spacecraft on 126th revolution over Sea of Okhotsk. First generation, low resolution photo surveillance; recovery probably failed.
1968 January 17 - .
10:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- OPS 1965 - .
Payload: Ferret 12 / Agena D 2733. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1970-07-07 . USAF Sat Cat: 3097 . COSPAR: 1968-004A. Apogee: 536 km (333 mi). Perigee: 462 km (287 mi). Inclination: 75.10 deg. Period: 94.60 min.
The last scheduled Air Force Thrust Augmented Thor/Agena (SLV-2A //498/SS-01B #2733) to be launched from Vandenberg AFB was the 150th Thor/ Agena vehicle fired from there since Discoverer I was launched on 28 February 1959. From now on, the Air Force would use the more advanced Long Tank Thrust Augmented Thor (SLV-2G) - Thorad - and the newer SLV-2H.
1968 January 18 - .
19:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5028 - .
Payload: KH-8 no. 11 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-02-04 . USAF Sat Cat: 3098 . COSPAR: 1968-005A. Apogee: 405 km (251 mi). Perigee: 137 km (85 mi). Inclination: 111.50 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 January 19 - .
21:59 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 200 - .
Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1973-02-24 . USAF Sat Cat: 3100 . COSPAR: 1968-006A. Apogee: 539 km (334 mi). Perigee: 518 km (321 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible navigation satellite..
1968 January 24 - .
22:26 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1045 - .
Payload: KH-4A s/n 1045 / Agena D 1640 / OPS 2243. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1968-02-27 . USAF Sat Cat: 3113 . COSPAR: 1968-008A. Apogee: 438 km (272 mi). Perigee: 179 km (111 mi). Inclination: 81.50 deg. Period: 90.70 min. KH-4A. All cameras operated satisfactorily..
- SRV 741 - .
Payload: SRV 1045-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1970-03-04 . USAF Sat Cat: 3114 . COSPAR: 1968-008xx. Apogee: 186 km (115 mi). Perigee: 185 km (114 mi). Inclination: 81.60 deg. Period: 88.20 min.
1968 February 6 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 201 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-02-14 . USAF Sat Cat: 3118 . COSPAR: 1968-009A. Apogee: 334 km (207 mi). Perigee: 207 km (128 mi). Inclination: 64.90 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 March 5 - .
12:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 205 - .
Payload: Zenit-2 11F61 s/n 56. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-03-13 . USAF Sat Cat: 3140 . COSPAR: 1968-016A. Apogee: 293 km (182 mi). Perigee: 197 km (122 mi). Inclination: 65.70 deg. Period: 89.40 min. Area survey photo reconnaissance satellite..
1968 March 13 - .
19:55 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5057 - .
Payload: KH-8 no. 12 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-03-24 . USAF Sat Cat: 3148 . COSPAR: 1968-018A. Apogee: 407 km (252 mi). Perigee: 128 km (79 mi). Inclination: 99.90 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 March 14 - .
22:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1046 - .
Payload: KH-4A s/n 1046 / Agena D 1638 / OPS 4849. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1968-04-10 . USAF Sat Cat: 3152 . COSPAR: 1968-020A. Apogee: 390 km (240 mi). Perigee: 183 km (113 mi). Inclination: 83.00 deg. Period: 90.20 min. KH-4A. Image quality good for 1046-1 and fair for 1046-2..
- SRV 747 - .
Payload: SRV 1046-1 / OPS 7076. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1970-01-03 . USAF Sat Cat: 3153 . COSPAR: 1968-020xx. Apogee: 189 km (117 mi). Perigee: 189 km (117 mi). Inclination: 83.00 deg. Period: 88.30 min.
1968 March 16 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 207 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-03-24 . USAF Sat Cat: 3154 . COSPAR: 1968-021A. Apogee: 320 km (190 mi). Perigee: 201 km (124 mi). Inclination: 65.60 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 March 21 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 208 - .
Payload: Zenit-2M. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1968-04-02 . USAF Sat Cat: 3156 . COSPAR: 1968-022A. Apogee: 287 km (178 mi). Perigee: 205 km (127 mi). Inclination: 64.90 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule; deployed high energy gamma ray experiment capsule. First flight of modernised Zenit-2 area survey reconnaissance satellite..
1968 March 22 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2A.
- Cosmos 209 - .
Payload: US-A no. 2. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1968-04-10 . USAF Sat Cat: 3162 . COSPAR: 1968-023C. Apogee: 927 km (576 mi). Perigee: 876 km (544 mi). Inclination: 65.30 deg. Period: 103.00 min. RORSAT hardware, representative of production hardware, but using chemical batteries in place of BES-5 nuclear reactor..
1968 April 3 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 210 - .
Payload: Zenit-2 11F61 s/n 60. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-04-11 . USAF Sat Cat: 3168 . COSPAR: 1968-024A. Apogee: 373 km (231 mi). Perigee: 200 km (120 mi). Inclination: 81.40 deg. Period: 90.30 min. Area survey photo reconnaissance satellite..
1968 April 17 - .
17:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5105 - .
Payload: KH-8 no. 13 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-04-29 . USAF Sat Cat: 3199 . COSPAR: 1968-031A. Apogee: 421 km (261 mi). Perigee: 127 km (78 mi). Inclination: 111.40 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 April 18 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 214 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-04-26 . USAF Sat Cat: 3203 . COSPAR: 1968-032A. Apogee: 373 km (231 mi). Perigee: 200 km (120 mi). Inclination: 81.40 deg. Period: 90.30 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 April 20 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 216 - .
Payload: Zenit-2 11F61 s/n 62. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-04-28 . USAF Sat Cat: 3207 . COSPAR: 1968-034A. Apogee: 267 km (165 mi). Perigee: 198 km (123 mi). Inclination: 51.00 deg. Period: 89.20 min. Area survey photo reconnaissance satellite. Unsuccessful mission. Spacecraft landed in River Volga 1 km from shore and sank after 42 minutes. 85% of the data was ruined..
1968 May 1 - .
21:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4B 1103 - .
Payload: KH-4B s/n 1103 / OPS 1419. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1968-05-15 . USAF Sat Cat: 3228 . COSPAR: 1968-039B. Apogee: 243 km (150 mi). Perigee: 164 km (101 mi). Inclination: 83.10 deg. Period: 88.60 min. KH-4B. Out-of-focus imagery is present on both main camera records..
1968 June 1 - .
10:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 223 - .
Payload: Zenit-2 11F61 s/n 63. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Completed Operations Date: 1968-06-09 . Decay Date: 1968-06-09 . USAF Sat Cat: 3274 . COSPAR: 1968-045A. Apogee: 317 km (196 mi). Perigee: 221 km (137 mi). Inclination: 72.90 deg. Period: 89.90 min. Area survey photo reconnaissance satellite..
1968 June 4 - .
06:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 224 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-06-12 . USAF Sat Cat: 3276 . COSPAR: 1968-046A. Apogee: 256 km (159 mi). Perigee: 203 km (126 mi). Inclination: 51.80 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; also measured atmospheric composition..
1968 June 5 - .
17:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5138 - .
Payload: KH-8 no. 14 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-06-17 . USAF Sat Cat: 3278 . COSPAR: 1968-047A. Apogee: 456 km (283 mi). Perigee: 123 km (76 mi). Inclination: 110.50 deg. Period: 90.30 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 June 18 - .
06:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 227 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-06-26 . USAF Sat Cat: 3294 . COSPAR: 1968-051A. Apogee: 271 km (168 mi). Perigee: 202 km (125 mi). Inclination: 51.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 June 20 - .
21:46 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1047 - .
Payload: KH-4A s/n 1047 / Agena D 1645 / OPS 5343. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1968-07-16 . USAF Sat Cat: 3296 . COSPAR: 1968-052A. Apogee: 402 km (249 mi). Perigee: 183 km (113 mi). Inclination: 85.00 deg. Period: 90.30 min. KH-4A. Out-of-focus imagery is present on both main camera records..
- SRV 745 - .
Payload: SRV 1047-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1970-01-11 . USAF Sat Cat: 3297 . COSPAR: 1968-052xx. Apogee: 180 km (110 mi). Perigee: 180 km (110 mi). Inclination: 85.10 deg. Period: 88.10 min.
1968 June 21 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 228 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1968-07-03 . USAF Sat Cat: 3298 . COSPAR: 1968-053A. Apogee: 245 km (152 mi). Perigee: 205 km (127 mi). Inclination: 51.60 deg. Period: 89.00 min. Area survey photo reconnaissance satellite; returned film capsule; deployed cosmic ray experiment capsule..
1968 June 26 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 229 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-07-04 . USAF Sat Cat: 3304 . COSPAR: 1968-054A. Apogee: 327 km (203 mi). Perigee: 207 km (128 mi). Inclination: 72.90 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 July 10 - .
19:49 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 231 - .
Payload: Zenit-2 11F61 s/n 64. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-07-18 . USAF Sat Cat: 3316 . COSPAR: 1968-058A. Apogee: 311 km (193 mi). Perigee: 206 km (128 mi). Inclination: 64.90 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1968 July 16 - .
13:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 232 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-07-24 . USAF Sat Cat: 3322 . COSPAR: 1968-060A. Apogee: 348 km (216 mi). Perigee: 189 km (117 mi). Inclination: 65.30 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule; also performed weather experiments..
1968 July 30 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 234 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 6.00 days. Decay Date: 1968-08-05 . USAF Sat Cat: 3332 . COSPAR: 1968-062A. Apogee: 288 km (178 mi). Perigee: 208 km (129 mi). Inclination: 51.80 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 August 6 - .
11:16 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- Canyon 1 - .
Payload: Canyon 1 / Agena D / OPS 2222. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Canyon.
USAF Sat Cat: 3334 . COSPAR: 1968-063A. Apogee: 39,860 km (24,760 mi). Perigee: 31,680 km (19,680 mi). Inclination: 9.90 deg. Period: 1,436.00 min.
The first "stretched" Atlas SLV-3A/ Agena D was launched from the Eastern Test Range. The "stretched" Atlas had an additional 117-inch tank section to provide more fuel, a longer burn time, and increased payload capability. First launch in a communications intelligence program operated by the USAF within the National Reconnaissance Office, on behalf of the National Security Agency. The first generation series, CANYON, was based on the Agena vehicle. The Agena D remained attached to the spacecraft. Positioned in geosynchronous orbit over the Indian Ocean. Last known longitude (30 December 1968) 98.50 deg W drifting at 0.166 deg E per day.
1968 August 6 - .
16:33 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5187 - .
Payload: KH-8 no. 15 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-08-16 . USAF Sat Cat: 3335 . COSPAR: 1968-064A. Apogee: 395 km (245 mi). Perigee: 142 km (88 mi). Inclination: 110.00 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 August 7 - .
21:36 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4B 1104 - .
Payload: KH-4B s/n 1104 / Agena D 1644 / OPS 5955. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1968-08-27 . USAF Sat Cat: 3336 . COSPAR: 1968-065A. Apogee: 259 km (160 mi). Perigee: 160 km (90 mi). Inclination: 82.10 deg. Period: 88.70 min. KH-4B. Best imagery to date on any KH-4 systems. Bicolor and color infrared experiments were conducted on this mission..
1968 August 9 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 235 - .
Payload: Zenit-2 11F61 s/n 61. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-08-17 . USAF Sat Cat: 3339 . COSPAR: 1968-067A. Apogee: 281 km (174 mi). Perigee: 201 km (124 mi). Inclination: 51.80 deg. Period: 89.30 min. Area survey photo reconnaissance satellite. Partially successful. Hard landing due to parachute sytem failure. 30% of the film damaged..
1968 August 27 - .
12:29 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 237 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-09-04 . USAF Sat Cat: 3348 . COSPAR: 1968-071A. Apogee: 320 km (190 mi). Perigee: 200 km (120 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 September 5 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 239 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-09-13 . USAF Sat Cat: 3353 . COSPAR: 1968-073A. Apogee: 274 km (170 mi). Perigee: 201 km (124 mi). Inclination: 51.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 September 10 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5247 - .
Payload: KH-8 no. 16 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-09-25 . USAF Sat Cat: 3375 . COSPAR: 1968-074A. Apogee: 404 km (251 mi). Perigee: 125 km (77 mi). Inclination: 106.10 deg. Period: 89.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 September 14 - .
06:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 240 - .
Payload: Zenit-2 11F61 s/n 66. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 7.00 days. Decay Date: 1968-09-21 . USAF Sat Cat: 3388 . COSPAR: 1968-075A. Apogee: 283 km (175 mi). Perigee: 203 km (126 mi). Inclination: 51.80 deg. Period: 89.30 min. Area survey photo reconnaissance satellite..
1968 September 16 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 241 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-09-24 . USAF Sat Cat: 3398 . COSPAR: 1968-077A. Apogee: 326 km (202 mi). Perigee: 198 km (123 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 September 18 - .
21:32 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1E.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1048 - .
Payload: KH-4A s/n 1048 / Agena D 1647 / OPS 0165. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1968-10-08 . USAF Sat Cat: 3408 . COSPAR: 1968-078A. Apogee: 393 km (244 mi). Perigee: 167 km (103 mi). Inclination: 83.00 deg. Period: 90.10 min. KH-4A. Film in the forward camera separated and camera failed on mission 1048-2, also the stellar/index camera unit failed..
- SRV 749 - .
Payload: SRV 1048-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1969-09-28 . USAF Sat Cat: 3409 . COSPAR: 1968-078xx. Apogee: 236 km (146 mi). Perigee: 211 km (131 mi). Inclination: 83.20 deg. Period: 89.00 min.
1968 September 23 - .
07:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 243 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 9.00 days. Decay Date: 1968-10-04 . USAF Sat Cat: 3418 . COSPAR: 1968-080A. Apogee: 293 km (182 mi). Perigee: 213 km (132 mi). Inclination: 71.30 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; deployed passive microwave radio telescope capsule..
1968 October 5 - .
11:16 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- OPS 0964 - .
Payload: Ferret 13 / Agena D 2734. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1971-03-26 . USAF Sat Cat: 3472 . COSPAR: 1968-086A. Apogee: 511 km (317 mi). Perigee: 483 km (300 mi). Inclination: 75.00 deg. Period: 94.60 min.
1968 October 7 - .
12:05 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 246 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 5.00 days. Decay Date: 1968-10-12 . USAF Sat Cat: 3473 . COSPAR: 1968-087A. Apogee: 321 km (199 mi). Perigee: 149 km (92 mi). Inclination: 65.40 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 October 11 - .
12:05 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 247 - .
Payload: Zenit-2 11F61 s/n 65. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-10-19 . USAF Sat Cat: 3484 . COSPAR: 1968-088A. Apogee: 345 km (214 mi). Perigee: 199 km (123 mi). Inclination: 65.40 deg. Period: 89.90 min. Area survey photo reconnaissance satellite..
1968 October 30 - .
22:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 250 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1978-02-15 . USAF Sat Cat: 3526 . COSPAR: 1968-095A. Apogee: 542 km (336 mi). Perigee: 522 km (324 mi). Inclination: 74.00 deg. Period: 95.30 min. Possible navigation satellite..
1968 October 31 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 251 - .
Payload: Zenit-4M no. 1. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 18.00 days. Decay Date: 1968-11-18 . USAF Sat Cat: 3528 . COSPAR: 1968-096A. Apogee: 255 km (158 mi). Perigee: 201 km (124 mi). Inclination: 64.90 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; deployed radio astronony and gamma ray experiment capsule; maneuverable..
1968 November 3 - .
21:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4B 1105 - .
Payload: KH-4B s/n 1105 / Agena D 1646 / OPS 1315. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1968-11-23 . USAF Sat Cat: 3531 . COSPAR: 1968-098A. Apogee: 288 km (178 mi). Perigee: 150 km (90 mi). Inclination: 82.20 deg. Period: 88.90 min. KH-4B. Image quality is variable and displays areas of soft focus and image smear..
1968 November 6 - .
19:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5296 - .
Payload: KH-8 no. 17 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-11-20 . USAF Sat Cat: 3532 . COSPAR: 1968-099A. Apogee: 390 km (240 mi). Perigee: 130 km (80 mi). Inclination: 106.00 deg. Period: 89.70 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 November 13 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 253 - .
Payload: Zenit-2 11F61 s/n 67. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 5.00 days. Decay Date: 1968-11-18 . USAF Sat Cat: 3542 . COSPAR: 1968-102A. Apogee: 337 km (209 mi). Perigee: 216 km (134 mi). Inclination: 65.40 deg. Period: 90.00 min. Area survey photo reconnaissance satellite. Unsuccessful mission. On 13th orbit the SA-20-1 camera's shutter responded to an uncommanded order to open. Radiation levels inside reached 3 times normal levels. 53% of the data was lost..
1968 November 21 - .
12:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 254 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-11-29 . USAF Sat Cat: 3562 . COSPAR: 1968-104A. Apogee: 335 km (208 mi). Perigee: 197 km (122 mi). Inclination: 65.40 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1968 November 29 - .
12:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 255 - .
Payload: Zenit-2 11F61 s/n 68. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-12-07 . USAF Sat Cat: 3574 . COSPAR: 1968-105A. Apogee: 317 km (196 mi). Perigee: 197 km (122 mi). Inclination: 65.40 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1968 December 4 - .
19:23 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 6518 - .
Payload: KH-8 no. 18 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1968-12-12 . USAF Sat Cat: 3594 . COSPAR: 1968-108A. Apogee: 735 km (456 mi). Perigee: 137 km (85 mi). Inclination: 106.20 deg. Period: 93.30 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 December 10 - .
08:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 258 - .
Payload: Zenit-2 11F61 s/n 69. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1968-12-18 . USAF Sat Cat: 3602 . COSPAR: 1968-111A. Apogee: 298 km (185 mi). Perigee: 205 km (127 mi). Inclination: 65.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1968 December 12 - .
22:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1049 - .
Payload: KH-4A s/n 1049 / Agena D 1648 / OPS 4740. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1968-12-28 . USAF Sat Cat: 3604 . COSPAR: 1968-112A. Apogee: 248 km (154 mi). Perigee: 169 km (105 mi). Inclination: 81.00 deg. Period: 88.70 min. KH-4A. Degraded film.
- OPS 7684 - .
Payload: EHH C1 / OPS 7684. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 3605 . COSPAR: 1968-112B. Apogee: 1,466 km (910 mi). Perigee: 1,378 km (856 mi). Inclination: 80.40 deg. Period: 114.30 min. ABM monitoring..
1969 January 12 - .
12:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 263 - .
Payload: Zenit-2 11F61 s/n 70. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-01-20 . USAF Sat Cat: 3651 . COSPAR: 1969-003A. Apogee: 325 km (201 mi). Perigee: 200 km (120 mi). Inclination: 65.40 deg. Period: 89.70 min. Area survey photo reconnaissance satellite..
1969 January 22 - .
19:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 7585 - .
Payload: KH-8 no. 19 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1969-02-03 . USAF Sat Cat: 3665 . COSPAR: 1969-007A. Apogee: 1,090 km (670 mi). Perigee: 142 km (88 mi). Inclination: 106.20 deg. Period: 97.00 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1969 January 23 - .
09:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 264 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1969-02-05 . USAF Sat Cat: 3667 . COSPAR: 1969-008A. Apogee: 295 km (183 mi). Perigee: 209 km (129 mi). Inclination: 69.90 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; carried radio astronony and gamma ray experiments; maneuverable..
1969 January 25 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2A.
FAILURE: Payload propulsion system failed; no orbit..
Failed Stage: P.
- US-A Mass Model - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: RVSN.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1969-01-24 . COSPAR: F690125A. Apogee: 100 km (60 mi). RORSAT hardware, representative of production hardware, but using chemical batteries in place of BES-5 nuclear reactor..
1969 February 5 - .
21:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4B 1106 - .
Payload: KH-4B s/n 1106 / Agena D 1650 / OPS 3890. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1969-02-24 . USAF Sat Cat: 3672 . COSPAR: 1969-010A. Apogee: 275 km (170 mi). Perigee: 147 km (91 mi). Inclination: 81.60 deg. Period: 88.70 min. KH-4B. The best image quality to date..
- OPS 2644 - .
Payload: EHH C2 / OPS 2644. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 3673 . COSPAR: 1969-010B. Apogee: 1,429 km (887 mi). Perigee: 1,391 km (864 mi). Inclination: 80.40 deg. Period: 114.00 min. ABM monitoring..
1969 February 25 - .
10:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 266 - .
Payload: Zenit-2 11F61 s/n 71. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-03-05 . USAF Sat Cat: 3761 . COSPAR: 1969-015A. Apogee: 336 km (208 mi). Perigee: 202 km (125 mi). Inclination: 72.00 deg. Period: 89.80 min. Area survey photo reconnaissance satellite..
1969 February 26 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 267 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-03-06 . USAF Sat Cat: 3765 . COSPAR: 1969-017A. Apogee: 331 km (205 mi). Perigee: 202 km (125 mi). Inclination: 70.00 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 March 4 - .
19:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 4248 - .
Payload: KH-8 no. 20 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1969-03-18 . USAF Sat Cat: 3772 . COSPAR: 1969-019A. Apogee: 461 km (286 mi). Perigee: 134 km (83 mi). Inclination: 92.00 deg. Period: 90.50 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1969 March 5 - .
17:25 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 269 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1978-10-21 . USAF Sat Cat: 3775 . COSPAR: 1969-021A. Apogee: 543 km (337 mi). Perigee: 525 km (326 mi). Inclination: 74.10 deg. Period: 95.30 min. Possible ELINT satellite..
1969 March 6 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 270 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-03-14 . USAF Sat Cat: 3777 . COSPAR: 1969-022A. Apogee: 331 km (205 mi). Perigee: 200 km (120 mi). Inclination: 65.40 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 March 15 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 271 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-03-23 . USAF Sat Cat: 3807 . COSPAR: 1969-023A. Apogee: 324 km (201 mi). Perigee: 196 km (121 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 March 19 - .
21:38 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1050 - .
Payload: KH-4A s/n 1050 / Agena D 1651 / OPS 3722. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1969-03-24 . USAF Sat Cat: 3829 . COSPAR: 1969-026A. Apogee: 252 km (156 mi). Perigee: 165 km (102 mi). Inclination: 82.90 deg. Period: 88.60 min. KH-4A. Due to abnormal rotational rates after revolution 22, the mission was terminated after a total of three days collecting photography..
- SRV 737 - .
Payload: SRV 1050-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1971-12-06 . USAF Sat Cat: 3830 . COSPAR: 1969-026xx. Apogee: 168 km (104 mi). Perigee: 168 km (104 mi). Inclination: 83.00 deg. Period: 87.90 min.
1969 March 22 - .
12:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 273 - .
Payload: Zenit-2 11F61 s/n 77. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-03-30 . USAF Sat Cat: 3831 . COSPAR: 1969-027A. Apogee: 336 km (208 mi). Perigee: 200 km (120 mi). Inclination: 65.40 deg. Period: 89.80 min. Area survey photo reconnaissance satellite..
1969 March 24 - .
10:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 274 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-04-01 . USAF Sat Cat: 3833 . COSPAR: 1969-028A. Apogee: 300 km (180 mi). Perigee: 206 km (128 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; also carried science package..
1969 April 4 - .
10:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 276 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 7.00 days. Decay Date: 1969-04-11 . USAF Sat Cat: 3854 . COSPAR: 1969-032A. Apogee: 371 km (230 mi). Perigee: 200 km (120 mi). Inclination: 81.40 deg. Period: 90.30 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 April 9 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 278 - .
Payload: Zenit-2 11F61 s/n 78. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-04-17 . USAF Sat Cat: 3883 . COSPAR: 1969-034A. Apogee: 310 km (190 mi). Perigee: 198 km (123 mi). Inclination: 65.40 deg. Period: 89.60 min. Area survey photo reconnaissance satellite..
1969 April 13 - .
02:24 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- Canyon 2 - .
Payload: Canyon 2 / Agena D / OPS 3148. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Canyon.
USAF Sat Cat: 3889 . COSPAR: 1969-036A. Apogee: 39,270 km (24,400 mi). Perigee: 32,670 km (20,300 mi). Inclination: 9.90 deg. Period: 1,445.00 min. Positioned in geosynchronous orbit over the Indian Ocean. Last known longitude (31 December 1969) 99.24 deg W drifting at 2.246 deg W per day..
1969 April 15 - .
08:14 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 279 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-04-23 . USAF Sat Cat: 3893 . COSPAR: 1969-038A. Apogee: 267 km (165 mi). Perigee: 192 km (119 mi). Inclination: 51.70 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 April 15 - .
17:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 5310 - .
Payload: KH-8 no. 21 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1969-04-30 . USAF Sat Cat: 3895 . COSPAR: 1969-039A. Apogee: 410 km (250 mi). Perigee: 135 km (83 mi). Inclination: 108.80 deg. Period: 90.00 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1969 April 23 - .
09:55 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 280 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1969-05-06 . USAF Sat Cat: 3906 . COSPAR: 1969-040A. Apogee: 250 km (150 mi). Perigee: 207 km (128 mi). Inclination: 51.60 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; carried weather experiments; maneuverable..
1969 May 2 - .
01:46 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1051 - .
Payload: KH-4A s/n 1051 / Agena D 1649 / OPS 1101. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1969-05-23 . USAF Sat Cat: 3914 . COSPAR: 1969-041A. Apogee: 325 km (201 mi). Perigee: 168 km (104 mi). Inclination: 64.90 deg. Period: 89.50 min. KH-4A. Imagery of both pan camera records is soft and lacks crispness and edge sharpness..
- SRV 739 - .
Payload: SRV 1051-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1970-02-16 . USAF Sat Cat: 3915 . COSPAR: 1969-041xx. Apogee: 193 km (119 mi). Perigee: 177 km (109 mi). Inclination: 65.70 deg. Period: 88.20 min.
1969 May 13 - .
09:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 281 - .
Payload: Zenit-2 11F61 s/n 72. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-05-21 . USAF Sat Cat: 3939 . COSPAR: 1969-042A. Apogee: 303 km (188 mi). Perigee: 191 km (118 mi). Inclination: 65.40 deg. Period: 89.40 min. Area survey photo reconnaissance satellite..
1969 May 20 - .
08:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 282 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-05-28 . USAF Sat Cat: 3944 . COSPAR: 1969-044A. Apogee: 321 km (199 mi). Perigee: 202 km (125 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 May 23 - .
07:57 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- Vela 9 - .
Payload: Vela 5A / OPS 6909. Mass: 317 kg (698 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Advanced Vela.
Decay Date: 1992-12-31 . USAF Sat Cat: 3954 . COSPAR: 1969-046D. Apogee: 145,638 km (90,495 mi). Perigee: 77,082 km (47,896 mi). Inclination: 61.60 deg. Period: 6,700.90 min. Solar flare particle detectors. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Vela 10 - .
Payload: Vela 5B / OPS 6911. Mass: 317 kg (698 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Advanced Vela.
Decay Date: 1992-12-31 . USAF Sat Cat: 3955 . COSPAR: 1969-046E. Apogee: 150,633 km (93,598 mi). Perigee: 72,080 km (44,780 mi). Inclination: 61.00 deg. Period: 6,700.70 min.
The 13th, and final, Titan IIIC research and development booster (Vehicle #15) lifted two Vela satellites, the fifth pair of such nuclear detection spacecraft, and three experimental satellites into orbit from Cape Canaveral. This launch concluded the highly successful Titan III research and development program initiated in 1962. Out of 13 Titan IIIC and four Titan IITA vehicles launched, 10 Titan IITCs were complete successes, two were partial successes, and only one was a failure, while three of the four Titan IITA launches were rated successful. Radiation, low-energy particle, solar flare data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
1969 May 29 - .
06:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 284 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-06-06 . USAF Sat Cat: 3971 . COSPAR: 1969-048A. Apogee: 297 km (184 mi). Perigee: 204 km (126 mi). Inclination: 51.70 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 June 3 - .
16:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan IIIB.
- OPS 1077 - .
Payload: KH-8 no. 22 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1969-06-14 . USAF Sat Cat: 3984 . COSPAR: 1969-050A. Apogee: 414 km (257 mi). Perigee: 137 km (85 mi). Inclination: 110.00 deg. Period: 90.00 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1969 June 15 - .
08:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 286 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-06-23 . USAF Sat Cat: 3988 . COSPAR: 1969-052A. Apogee: 322 km (200 mi). Perigee: 197 km (122 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 June 24 - .
06:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 287 - .
Payload: Zenit-2 11F61 s/n 76. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-07-02 . USAF Sat Cat: 3991 . COSPAR: 1969-054A. Apogee: 265 km (164 mi). Perigee: 189 km (117 mi). Inclination: 51.80 deg. Period: 89.00 min. Area survey photo reconnaissance satellite..
1969 June 27 - .
06:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 288 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-07-05 . USAF Sat Cat: 3994 . COSPAR: 1969-055A. Apogee: 273 km (169 mi). Perigee: 199 km (123 mi). Inclination: 51.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 July 10 - .
09:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 289 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 5.00 days. Decay Date: 1969-07-15 . USAF Sat Cat: 4034 . COSPAR: 1969-057A. Apogee: 324 km (201 mi). Perigee: 194 km (120 mi). Inclination: 65.30 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 July 22 - .
12:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 290 - .
Payload: Zenit-2 11F61 s/n 75. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-07-30 . USAF Sat Cat: 4042 . COSPAR: 1969-060A. Apogee: 332 km (206 mi). Perigee: 195 km (121 mi). Inclination: 65.40 deg. Period: 89.70 min. Area survey photo reconnaissance satellite..
1969 July 24 - .
01:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1107 - .
Payload: KH-4B s/n 1107 / Agena D 1652 / OPS 3654. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1969-08-23 . USAF Sat Cat: 4050 . COSPAR: 1969-063A. Apogee: 203 km (126 mi). Perigee: 182 km (113 mi). Inclination: 74.90 deg. Period: 88.40 min. KH-4B. Forward camera failed on pass 1 and remained inoperative throughout the rest of the mission..
1969 July 31 - .
10:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- OPS 8285 - .
Payload: Ferret 14 / Agena D 2735. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1973-01-04 . USAF Sat Cat: 4054 . COSPAR: 1969-065A. Apogee: 536 km (333 mi). Perigee: 465 km (288 mi). Inclination: 75.00 deg. Period: 94.60 min.
1969 August 16 - .
11:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 293 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1969-08-28 . USAF Sat Cat: 4072 . COSPAR: 1969-071A. Apogee: 244 km (151 mi). Perigee: 215 km (133 mi). Inclination: 51.70 deg. Period: 89.10 min. Area survey photo reconnaissance satellite; returned film capsule; carried science package..
1969 August 19 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 294 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-08-27 . USAF Sat Cat: 4074 . COSPAR: 1969-072A. Apogee: 329 km (204 mi). Perigee: 200 km (120 mi). Inclination: 65.40 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 August 23 - .
16:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 7807 - .
Payload: KH-8 no. 23 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1969-09-07 . USAF Sat Cat: 4078 . COSPAR: 1969-074A. Apogee: 377 km (234 mi). Perigee: 138 km (85 mi). Inclination: 108.10 deg. Period: 89.60 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1969 August 29 - .
09:05 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 296 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-09-06 . USAF Sat Cat: 4080 . COSPAR: 1969-075A. Apogee: 302 km (187 mi). Perigee: 207 km (128 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 September 2 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 297 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-09-10 . USAF Sat Cat: 4082 . COSPAR: 1969-076A. Apogee: 314 km (195 mi). Perigee: 207 km (128 mi). Inclination: 72.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 September 18 - .
08:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 299 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 4.00 days. Decay Date: 1969-09-22 . USAF Sat Cat: 4097 . COSPAR: 1969-078A. Apogee: 284 km (176 mi). Perigee: 207 km (128 mi). Inclination: 65.00 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 September 22 - .
21:11 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- KH-4A 1052 - .
Payload: KH-4A s/n 1052 / Agena D 1653 / OPS 3531. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1969-10-12 . USAF Sat Cat: 4102 . COSPAR: 1969-079A. Apogee: 253 km (157 mi). Perigee: 178 km (110 mi). Inclination: 85.00 deg. Period: 88.80 min. KH-4A. Last of the KH-4A missions, all camera systems operated satisfactorily..
- SRV 743R - .
Payload: SRV 1052-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1971-05-16 . USAF Sat Cat: 4103 . COSPAR: 1969-079xx. Apogee: 211 km (131 mi). Perigee: 211 km (131 mi). Inclination: 85.10 deg. Period: 88.70 min.
1969 September 24 - .
12:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 301 - .
Payload: Zenit-2 11F61 s/n 79. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-10-02 . USAF Sat Cat: 4106 . COSPAR: 1969-081A. Apogee: 271 km (168 mi). Perigee: 203 km (126 mi). Inclination: 65.40 deg. Period: 89.30 min. Area survey photo reconnaissance satellite..
1969 September 30 - .
13:40 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- OPS 1807 - .
Payload: EHH B17. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1970-10-30 . USAF Sat Cat: 4111 . COSPAR: 1969-082A. Apogee: 484 km (300 mi). Perigee: 446 km (277 mi). Inclination: 69.60 deg. Period: 93.90 min.
- Surcal - .
Payload: NRL PL164 / OPS 7613 / Poppy 6D (Poppy multifacete. Mass: 40 kg (88 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 4295 . COSPAR: 1969-082G. Apogee: 926 km (575 mi). Perigee: 899 km (558 mi). Inclination: 70.00 deg. Period: 103.30 min. Poppy naval signals intelligence satellite..
- SOICAL Cone - .
Payload: S69-4 Cone. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SOICAL.
USAF Sat Cat: 4132 . COSPAR: 1969-082K. Apogee: 870 km (540 mi). Perigee: 844 km (524 mi). Inclination: 70.00 deg. Period: 102.10 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Tempsat 2 - .
Mass: 9.00 kg (19.80 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Tempsat.
USAF Sat Cat: 4168 . COSPAR: 1969-082H. Apogee: 924 km (574 mi). Perigee: 899 km (558 mi). Inclination: 70.00 deg. Period: 103.20 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Surcal - .
Payload: NRL PL163 / OPS 7613 / Poppy 6C (Poppy multifacete. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 4247 . COSPAR: 1969-082F. Apogee: 925 km (574 mi). Perigee: 898 km (557 mi). Inclination: 70.00 deg. Period: 103.20 min. Poppy naval signals intelligence satellite. Official and secondary mission: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Surcal - .
Payload: NRL PL162 / OPS 7613 / Poppy 6B (Poppy multifacet. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 4237 . COSPAR: 1969-082E. Apogee: 925 km (574 mi). Perigee: 899 km (558 mi). Inclination: 70.00 deg. Period: 103.30 min. Poppy naval signals intelligence satellite. Official and secondary mission:Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Surcal - .
Payload: NRL PL161 / OPS 7613 / Poppy 6A (Poppy multifacet. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 4259 . COSPAR: 1969-082D. Apogee: 928 km (576 mi). Perigee: 899 km (558 mi). Inclination: 70.00 deg. Period: 103.30 min. Launch of a quadruplet of Poppy naval signals intelligence satellites. Official and secondary mission: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Surcal - .
Payload: NRL PL176 / OPS 7613 P/L 1. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Surcal.
USAF Sat Cat: 4256 . COSPAR: 1969-082B. Apogee: 918 km (570 mi). Perigee: 893 km (554 mi). Inclination: 70.00 deg. Period: 103.10 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- SOICAL Cylinder - .
Payload: S69-4 Cylinder. Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SOICAL.
USAF Sat Cat: 4166 . COSPAR: 1969-082J. Apogee: 812 km (504 mi). Perigee: 791 km (491 mi). Inclination: 70.00 deg. Period: 100.90 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1969 October 17 - .
11:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 302 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-10-25 . USAF Sat Cat: 4130 . COSPAR: 1969-089A. Apogee: 321 km (199 mi). Perigee: 198 km (123 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 October 24 - .
09:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 306 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1969-11-05 . USAF Sat Cat: 4182 . COSPAR: 1969-093A. Apogee: 299 km (185 mi). Perigee: 215 km (133 mi). Inclination: 65.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1969 October 24 - .
18:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 8455 - .
Payload: KH-8 no. 24 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1969-11-08 . USAF Sat Cat: 4186 . COSPAR: 1969-095A. Apogee: 740 km (450 mi). Perigee: 136 km (84 mi). Inclination: 108.00 deg. Period: 93.40 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1969 November 12 - .
11:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 309 - .
Payload: Zenit-2 11F61 s/n 80. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1969-11-20 . USAF Sat Cat: 4223 . COSPAR: 1969-098A. Apogee: 364 km (226 mi). Perigee: 185 km (114 mi). Inclination: 64.50 deg. Period: 90.00 min. Area survey photo reconnaissance satellite. First flight with Nauka external experiment container..
1969 November 15 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 310 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1969-11-23 . USAF Sat Cat: 4232 . COSPAR: 1969-100A. Apogee: 336 km (208 mi). Perigee: 204 km (126 mi). Inclination: 65.00 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 December 3 - .
13:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 313 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1969-12-15 . USAF Sat Cat: 4262 . COSPAR: 1969-104A. Apogee: 335 km (208 mi). Perigee: 198 km (123 mi). Inclination: 65.40 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1969 December 4 - .
21:37 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1108 - .
Payload: KH-4B s/n 1108 / Agena D 1655 / OPS 6617. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1970-01-10 . USAF Sat Cat: 4264 . COSPAR: 1969-105A. Apogee: 229 km (142 mi). Perigee: 161 km (100 mi). Inclination: 81.40 deg. Period: 88.40 min. KH-4B. Cameras operated satisfactorily and the mission carried 811 ft of aerial color film added to the end of the film supply..
1969 December 20 - .
03:26 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/pad?.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 315 - .
Mass: 325 kg (716 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1979-03-25 . USAF Sat Cat: 4273 . COSPAR: 1969-107A. Apogee: 542 km (336 mi). Perigee: 518 km (321 mi). Inclination: 74.00 deg. Period: 95.30 min. Possible navigation satellite..
1969 December 23 - .
13:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 317 - .
Payload: Zenit-4MK no. 1. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1970-01-05 . USAF Sat Cat: 4280 . COSPAR: 1969-109A. Apogee: 280 km (170 mi). Perigee: 205 km (127 mi). Inclination: 65.40 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; carried charged particle experiments; maneuverable..
1970 January 9 - .
09:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 318 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-01-21 . USAF Sat Cat: 4292 . COSPAR: 1970-001A. Apogee: 379 km (235 mi). Perigee: 206 km (128 mi). Inclination: 65.00 deg. Period: 90.30 min. Area survey photo reconnaissance satellite; returned film capsule..
1970 January 14 - .
18:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 6531 - .
Payload: KH-8 no. 25 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1970-02-01 . USAF Sat Cat: 4296 . COSPAR: 1970-002A. Apogee: 383 km (237 mi). Perigee: 134 km (83 mi). Inclination: 110.00 deg. Period: 89.70 min. The 25th Air Force Titan IIIB/Agena D space booster was launched from Vandenberg AFB. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1970 January 21 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 322 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1970-01-29 . USAF Sat Cat: 4315 . COSPAR: 1970-007A. Apogee: 298 km (185 mi). Perigee: 216 km (134 mi). Inclination: 65.30 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 February 10 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 323 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1970-02-18 . USAF Sat Cat: 4328 . COSPAR: 1970-010A. Apogee: 314 km (195 mi). Perigee: 201 km (124 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 March 4 - .
12:14 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 325 - .
Payload: Zenit-2 11F61 s/n 73. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1970-03-12 . USAF Sat Cat: 4340 . COSPAR: 1970-015A. Apogee: 327 km (203 mi). Perigee: 200 km (120 mi). Inclination: 65.40 deg. Period: 89.80 min. Area survey photo reconnaissance satellite..
1970 March 4 - .
22:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1109 - .
Payload: KH-4B s/n 1109 / Agena D 1657 / OPS 0440. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1970-03-26 . USAF Sat Cat: 4342 . COSPAR: 1970-016A. Apogee: 257 km (159 mi). Perigee: 167 km (103 mi). Inclination: 88.00 deg. Period: 88.80 min. KH-4B. Cameras operated satisfactorily but the overall image quality of both the forward and aft records is variable..
- SRV 819 - .
Payload: SRV 1109-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1971-11-10 . USAF Sat Cat: 4343 . COSPAR: 1970-016xx. Apogee: 164 km (101 mi). Perigee: 164 km (101 mi). Inclination: 88.10 deg. Period: 87.80 min.
1970 March 13 - .
08:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 326 - .
Payload: Zenit-2 11F61 s/n 74. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1970-03-21 . USAF Sat Cat: 4346 . COSPAR: 1970-018A. Apogee: 232 km (144 mi). Perigee: 208 km (129 mi). Inclination: 81.30 deg. Period: 88.90 min. Area survey photo reconnaissance satellite..
1970 March 27 - .
11:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 328 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1970-04-09 . USAF Sat Cat: 4355 . COSPAR: 1970-022A. Apogee: 299 km (185 mi). Perigee: 203 km (126 mi). Inclination: 72.90 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 April 3 - .
08:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 329 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-04-15 . USAF Sat Cat: 4357 . COSPAR: 1970-023A. Apogee: 228 km (141 mi). Perigee: 198 km (123 mi). Inclination: 81.30 deg. Period: 88.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1970 April 7 - .
11:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 330 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1979-06-12 . USAF Sat Cat: 4360 . COSPAR: 1970-024A. Apogee: 543 km (337 mi). Perigee: 514 km (319 mi). Inclination: 74.10 deg. Period: 95.20 min. Possible navigation satellite. Replaced Cosmos 250..
1970 April 8 - .
10:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 331 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1970-04-16 . USAF Sat Cat: 4364 . COSPAR: 1970-026A. Apogee: 320 km (190 mi). Perigee: 206 km (128 mi). Inclination: 65.00 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 April 8 - .
10:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- Vela 12 - .
Payload: Vela 6A / OPS 7044. Mass: 317 kg (698 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Advanced Vela.
Decay Date: 1992-12-31 . USAF Sat Cat: 4366 . COSPAR: 1970-027A. Apogee: 121,227 km (75,326 mi). Perigee: 101,261 km (62,920 mi). Inclination: 61.20 deg. Period: 6,691.00 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- Vela 11 - .
Payload: Vela 6B / OPS 7033. Mass: 317 kg (698 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Nuclear detection surveillance satellite. Spacecraft: Advanced Vela.
Decay Date: 1992-12-31 . USAF Sat Cat: 4368 . COSPAR: 1970-027B. Apogee: 119,313 km (74,137 mi). Perigee: 103,570 km (64,350 mi). Inclination: 57.40 deg. Period: 6,707.90 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1970 April 15 - .
09:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 333 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1970-04-28 . USAF Sat Cat: 4373 . COSPAR: 1970-030A. Apogee: 239 km (148 mi). Perigee: 219 km (136 mi). Inclination: 81.30 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 April 15 - .
15:52 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 2863 - .
Payload: KH-8 no. 26 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1970-05-06 . USAF Sat Cat: 4375 . COSPAR: 1970-031A. Apogee: 388 km (241 mi). Perigee: 130 km (80 mi). Inclination: 111.00 deg. Period: 89.70 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1970 May 12 - .
10:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 344 - .
Payload: Zenit-2 11F61 s/n 81. Mass: 4,720 kg (10,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2 satellite.
Duration: 8.00 days. Decay Date: 1970-05-20 . USAF Sat Cat: 4401 . COSPAR: 1970-038A. Apogee: 326 km (202 mi). Perigee: 204 km (126 mi). Inclination: 72.90 deg. Period: 89.80 min. Area survey photo reconnaissance satellite. Partially successful. Failure of SA-10B camera on 42nd orbit..
1970 May 20 - .
09:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 345 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1970-05-28 . USAF Sat Cat: 4403 . COSPAR: 1970-039A. Apogee: 296 km (183 mi). Perigee: 153 km (95 mi). Inclination: 52.00 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 May 20 - .
21:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1110 - .
Payload: KH-4B s/n 1110 / Agena D 1656 / OPS 4720. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1970-06-17 . USAF Sat Cat: 4405 . COSPAR: 1970-040A. Apogee: 247 km (153 mi). Perigee: 162 km (100 mi). Inclination: 83.00 deg. Period: 88.60 min. KH-4B. The overall image quality is less than that provided by recent missions and 2,000 feet of S0-349.
- OPS 8520 - .
Payload: EHH B19. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1974-03-08 . USAF Sat Cat: 4406 . COSPAR: 1970-040B. Apogee: 499 km (310 mi). Perigee: 490 km (300 mi). Inclination: 83.10 deg. Period: 94.50 min. Radar monitoring; may or may not have existed!!!..
1970 June 10 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 346 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 7.00 days. Decay Date: 1970-06-17 . USAF Sat Cat: 4409 . COSPAR: 1970-042A. Apogee: 351 km (218 mi). Perigee: 206 km (128 mi). Inclination: 51.80 deg. Period: 90.00 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 June 17 - .
12:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 349 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1970-06-25 . USAF Sat Cat: 4416 . COSPAR: 1970-045A. Apogee: 332 km (206 mi). Perigee: 199 km (123 mi). Inclination: 65.40 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 June 19 - .
11:37 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- OPS 5346 - .
Payload: AFP-720 Rhyolite 1. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Rhyolite.
USAF Sat Cat: 4418 . COSPAR: 1970-046A. Apogee: 33,685 km (20,930 mi). Perigee: 178 km (110 mi). Inclination: 28.20 deg. Period: 588.90 min. First launch of Rhyolite geostationary ELINT satellite. Reportedly left in transfer orbit; other sources indicate a successful mission. Positioned in geosynchronous orbit over the Indian Ocean..
1970 June 25 - .
14:50 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 6820 - .
Payload: KH-8 no. 27 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1970-07-06 . USAF Sat Cat: 4422 . COSPAR: 1970-048A. Apogee: 393 km (244 mi). Perigee: 144 km (89 mi). Inclination: 108.90 deg. Period: 89.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1970 June 26 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 350 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-07-08 . USAF Sat Cat: 4425 . COSPAR: 1970-050A. Apogee: 274 km (170 mi). Perigee: 180 km (110 mi). Inclination: 51.70 deg. Period: 89.00 min. Area survey photo reconnaissance satellite; returned film capsule..
1970 July 7 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 352 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1970-07-15 . USAF Sat Cat: 4446 . COSPAR: 1970-052A. Apogee: 340 km (210 mi). Perigee: 203 km (126 mi). Inclination: 51.80 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 July 9 - .
13:35 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 353 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-07-21 . USAF Sat Cat: 4455 . COSPAR: 1970-053A. Apogee: 304 km (188 mi). Perigee: 205 km (127 mi). Inclination: 65.40 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1970 July 23 - .
01:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1111 - .
Payload: KH-4B s/n 1111 / Agena D 1654 / OPS 4324. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1970-08-19 . USAF Sat Cat: 4477 . COSPAR: 1970-054A. Apogee: 379 km (235 mi). Perigee: 156 km (96 mi). Inclination: 59.90 deg. Period: 89.80 min. KH-4B. The overall image quality is good..
1970 August 7 - .
09:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 355 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1970-08-15 . USAF Sat Cat: 4484 . COSPAR: 1970-058A. Apogee: 321 km (199 mi). Perigee: 198 km (123 mi). Inclination: 65.30 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule.
1970 August 18 - .
14:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 7874 - .
Payload: KH-8 no. 28 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1970-09-03 . USAF Sat Cat: 4492 . COSPAR: 1970-061A. Apogee: 377 km (234 mi). Perigee: 149 km (92 mi). Inclination: 111.10 deg. Period: 89.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1970 August 26 - .
10:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- OPS 8329 - .
Payload: Ferret 15. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1975-03-26 . USAF Sat Cat: 4503 . COSPAR: 1970-066A. Apogee: 499 km (310 mi). Perigee: 496 km (308 mi). Inclination: 75.00 deg. Period: 94.50 min.
1970 August 29 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 360 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 10.00 days. Decay Date: 1970-09-08 . USAF Sat Cat: 4508 . COSPAR: 1970-068A. Apogee: 287 km (178 mi). Perigee: 207 km (128 mi). Inclination: 65.00 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable; deployed capsule..
1970 September 1 - .
01:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- Canyon 3 - .
Payload: Canyon 3 / Agena D / OPS 7329. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Canyon.
USAF Sat Cat: 4510 . COSPAR: 1970-069A. Apogee: 39,855 km (24,764 mi). Perigee: 31,947 km (19,850 mi). Inclination: 10.30 deg. Period: 1,441.90 min. Positioned in geosynchronous orbit over the Indian Ocean. Last known longitude (31 December 1970) 99.01 deg W drifting at 1.490 deg W per day..
1970 September 8 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 361 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1970-09-21 . USAF Sat Cat: 4524 . COSPAR: 1970-071A. Apogee: 338 km (210 mi). Perigee: 195 km (121 mi). Inclination: 72.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 September 17 - .
08:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 363 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-09-29 . USAF Sat Cat: 4538 . COSPAR: 1970-074A. Apogee: 294 km (182 mi). Perigee: 207 km (128 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1970 September 22 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 364 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 10.00 days. Decay Date: 1970-10-02 . USAF Sat Cat: 4553 . COSPAR: 1970-075A. Apogee: 297 km (184 mi). Perigee: 202 km (125 mi). Inclination: 65.40 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 October 1 - .
08:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 366 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-10-13 . USAF Sat Cat: 4561 . COSPAR: 1970-078A. Apogee: 284 km (176 mi). Perigee: 216 km (134 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1970 October 3 - .
10:26 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 367 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: PKO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1970-10-31 . USAF Sat Cat: 4566 . COSPAR: 1970-079C. Apogee: 1,022 km (635 mi). Perigee: 915 km (568 mi). Inclination: 65.30 deg. Period: 104.50 min. Ocean surveillance; probably used chemical batteries..
1970 October 8 - .
12:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 368 - .
Payload: Bion precursor. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 6.00 days. Decay Date: 1970-10-14 . USAF Sat Cat: 4571 . COSPAR: 1970-080A. Apogee: 383 km (237 mi). Perigee: 202 km (125 mi). Inclination: 65.00 deg. Period: 90.40 min. Bion precursor mission. Conducted biological investigations and study of the physical characteristics of outer space..
1970 October 9 - .
11:04 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 370 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1970-10-22 . USAF Sat Cat: 4576 . COSPAR: 1970-082A. Apogee: 280 km (170 mi). Perigee: 203 km (126 mi). Inclination: 64.90 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 October 23 - .
17:40 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 7568 - .
Payload: KH-8 no. 29 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1970-11-11 . USAF Sat Cat: 4596 . COSPAR: 1970-090A. Apogee: 396 km (246 mi). Perigee: 135 km (83 mi). Inclination: 111.10 deg. Period: 89.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1970 October 30 - .
13:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 376 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1970-11-12 . USAF Sat Cat: 4599 . COSPAR: 1970-092A. Apogee: 286 km (177 mi). Perigee: 207 km (128 mi). Inclination: 65.40 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 November 6 - .
10:35 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
FAILURE: Partial Failure..
Failed Stage: U.
- IMEWS 1 - .
Payload: DSP Phase 1 s/n 1 / OPS 5960. Mass: 900 kg (1,980 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1973-12-31 . USAF Sat Cat: 4630 . COSPAR: 1970-093A. Apogee: 36,128 km (22,448 mi). Perigee: 25,840 km (16,050 mi). Inclination: 16.40 deg. Period: 1,197.90 min.
An Air Force Titan IIIC launched the 500th satellite to be placed in orbit successfully by a vehicle launched from Cape Canaveral. First generation geosynchronous ballistic missile launch detection satellite; placed in incorrect subsynchronous orbit. One account claimed that it exhausted its propellant before it could be put into operation, but a 2007service history chart showed that is was considered operational for three years, well beyond its planned life.
1970 November 11 - .
09:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 377 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-11-23 . USAF Sat Cat: 4695 . COSPAR: 1970-096A. Apogee: 286 km (177 mi). Perigee: 204 km (126 mi). Inclination: 65.00 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule..
1970 November 18 - .
21:29 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1112 - .
Payload: KH-4B s/n 1112 / Agena D 1658 / OPS 4992. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1970-12-11 . USAF Sat Cat: 4721 . COSPAR: 1970-098A. Apogee: 227 km (141 mi). Perigee: 180 km (110 mi). Inclination: 82.90 deg. Period: 88.50 min. KH-4B. The forward camera failed on pass 104 and remained inoperative throughout the rest of the mission..
- SRV 827 - .
Payload: SRV 1112-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1977-09-14 . USAF Sat Cat: 4722 . COSPAR: 1970-098xx. Apogee: 206 km (128 mi). Perigee: 195 km (121 mi). Inclination: 83.20 deg. Period: 88.50 min.
1970 December 3 - .
13:55 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 383 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1970-12-16 . USAF Sat Cat: 4787 . COSPAR: 1970-104A. Apogee: 279 km (173 mi). Perigee: 204 km (126 mi). Inclination: 65.40 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 December 10 - .
11:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 384 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1970-12-22 . USAF Sat Cat: 4791 . COSPAR: 1970-105A. Apogee: 292 km (181 mi). Perigee: 203 km (126 mi). Inclination: 72.90 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; deployed science capsule..
1970 December 15 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 386 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1970-12-28 . USAF Sat Cat: 4804 . COSPAR: 1970-110A. Apogee: 242 km (150 mi). Perigee: 222 km (137 mi). Inclination: 65.00 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1970 December 16 - .
04:29 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 387 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-01-19 . USAF Sat Cat: 4806 . COSPAR: 1970-111A. Apogee: 543 km (337 mi). Perigee: 525 km (326 mi). Inclination: 74.00 deg. Period: 95.30 min. Possible navigation satellite. Replaced Cosmos 269..
1970 December 18 - .
16:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 389 - .
Payload: Tselina-D no. 1. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2003-11-24 . USAF Sat Cat: 4813 . COSPAR: 1970-113A. Apogee: 568 km (352 mi). Perigee: 543 km (337 mi). Inclination: 81.20 deg. Period: 95.80 min.
1971 January 12 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 390 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-01-25 . USAF Sat Cat: 4845 . COSPAR: 1971-001A. Apogee: 276 km (171 mi). Perigee: 196 km (121 mi). Inclination: 65.00 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 January 21 - .
08:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 392 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1971-02-02 . USAF Sat Cat: 4872 . COSPAR: 1971-004A. Apogee: 278 km (172 mi). Perigee: 204 km (126 mi). Inclination: 65.00 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule..
1971 January 21 - .
18:28 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 7776 - .
Payload: KH-8 no. 30 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1971-02-09 . USAF Sat Cat: 4874 . COSPAR: 1971-005A. Apogee: 418 km (259 mi). Perigee: 139 km (86 mi). Inclination: 110.90 deg. Period: 90.10 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1971 February 17 - .
03:52 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC10W.
LV Family:
Thor.
Launch Vehicle:
Thor Burner 2.
- Calsphere 5 - .
Payload: NRL PL170C / OPS 5268. Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
Decay Date: 1990-01-07 . USAF Sat Cat: 4963 . COSPAR: 1971-012E. Apogee: 360 km (220 mi). Perigee: 340 km (210 mi). Inclination: 98.20 deg. Period: 91.50 min. Radar calibarion sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Calsphere 3A - .
Payload: NRL PL170A / OPS 5268. Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
Decay Date: 1989-10-17 . USAF Sat Cat: 4957 . COSPAR: 1971-012C. Apogee: 531 km (329 mi). Perigee: 509 km (316 mi). Inclination: 98.40 deg. Period: 95.00 min. Radar calibarion sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Calsphere 4 - .
Payload: NRL PL170B / OPS 5268. Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Calsphere.
Decay Date: 1989-09-20 . USAF Sat Cat: 4958 . COSPAR: 1971-012D. Apogee: 502 km (311 mi). Perigee: 486 km (301 mi). Inclination: 98.40 deg. Period: 94.50 min. Radar calibarion sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1971 February 17 - .
20:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
FAILURE: Failure.
Failed Stage: U.
- KH-4B 1113 - .
Payload: KH-4B s/n 1113. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1971-02-17 .
KH-4B. The launch vehicle had a very cold boattail due to a hose discovered to be leaking away warming air to the boattail. The boattail was colder than usual, below freezing. Based on earlier tests of the Thor for just that condition, as relayed by Ed Dierdorf, Thor chief engineer at the time, the temp low was of no concern.
The only problem was that those tests were made with a Thor that carried a Rocketdyne engine lubricated with "lube oil". The Thor being launched used a fuel additive, "Orinite" (like STP "super snot"). The technician that pumped the Orinite into its cannister later stated, "It wasn't for lack of orinite. I put it in just like the procedure said, and I could feel when it was full (with the hand pump). To make sure, I gave it another slug."
That "other slug" cracked the output valve that was only supposed to be cracked by turbopump output pressure. When it cracked the output valve a bit of the "honey" squirted down the tube toward engine bearing jets. This line had a low spot in it by design. The Orinite settled there. When it was chilled by the low temp air at lox loading, the Orinite formed a plug.
Unaware of this chain of circumstances, Launch Director Philip Payne made the decision to launch. The rocket (carrying Agena D and payload) flew for 18 seconds, then wiped out its gears, causing the turbine to overspeed and shed its vanes. These punctured various parts in the boattail like machine gun bullets. With loss of power, the rocket fell not far from the launch pad into Bear Creek canyon.
The final cause was therefore found to be loss of engine lubrication at startup.
1971 February 17 - .
21:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 395 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-04-06 . USAF Sat Cat: 4955 . COSPAR: 1971-013A. Apogee: 546 km (339 mi). Perigee: 529 km (328 mi). Inclination: 74.00 deg. Period: 95.40 min. Possible ELINT satellite..
1971 February 18 - .
13:59 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 396 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-03-03 . USAF Sat Cat: 4959 . COSPAR: 1971-014A. Apogee: 285 km (177 mi). Perigee: 204 km (126 mi). Inclination: 65.40 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 March 3 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 399 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 14.00 days. Decay Date: 1971-03-17 . USAF Sat Cat: 5003 . COSPAR: 1971-017A. Apogee: 285 km (177 mi). Perigee: 200 km (120 mi). Inclination: 64.90 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 March 21 - .
03:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 33B.
- Jumpseat 1 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Jumpseat.
USAF Sat Cat: 5053 . COSPAR: 1971-021A. Apogee: 33,800 km (21,000 mi). Perigee: 390 km (240 mi). Inclination: 63.20 deg. Period: 596.70 min.
1971 March 24 - .
21:05 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1114 - .
Payload: KH-4B s/n 1114 / Agena D 1660 / OPS 5300. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1971-04-12 . USAF Sat Cat: 5059 . COSPAR: 1971-022A. Apogee: 245 km (152 mi). Perigee: 156 km (96 mi). Inclination: 81.50 deg. Period: 88.40 min. KH-4B. The overall image quality is good and comparable to the best of past missions. On-board program failed.
1971 March 27 - .
10:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 401 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-04-09 . USAF Sat Cat: 5086 . COSPAR: 1971-023A. Apogee: 290 km (180 mi). Perigee: 185 km (114 mi). Inclination: 72.80 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 April 1 - .
11:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 402 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1971-05-06 . USAF Sat Cat: 5107 . COSPAR: 1971-025B. Apogee: 1,011 km (628 mi). Perigee: 965 km (599 mi). Inclination: 65.00 deg. Period: 104.90 min. Ocean surveillance; probably used chemical batteries..
1971 April 2 - .
08:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 403 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1971-04-14 . USAF Sat Cat: 5108 . COSPAR: 1971-026A. Apogee: 229 km (142 mi). Perigee: 216 km (134 mi). Inclination: 81.30 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule..
1971 April 7 - .
07:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 405 - .
Payload: Tselina-D no. 2. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 5117 . COSPAR: 1971-028A. Apogee: 603 km (374 mi). Perigee: 594 km (369 mi). Inclination: 81.20 deg. Period: 96.70 min.
1971 April 14 - .
08:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 406 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 10.00 days. Decay Date: 1971-04-24 . USAF Sat Cat: 5124 . COSPAR: 1971-029A. Apogee: 246 km (152 mi). Perigee: 217 km (134 mi). Inclination: 81.30 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 April 22 - .
15:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 23B.
- OPS 7899 - .
Payload: KH-8 no. 31 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1971-05-13 . USAF Sat Cat: 5171 . COSPAR: 1971-033A. Apogee: 403 km (250 mi). Perigee: 132 km (82 mi). Inclination: 110.60 deg. Period: 89.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1971 May 5 - .
07:43 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
1971 May 6 - .
06:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 410 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1971-05-18 . USAF Sat Cat: 5207 . COSPAR: 1971-040A. Apogee: 280 km (170 mi). Perigee: 205 km (127 mi). Inclination: 65.00 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule; deployed science capsule..
1971 May 18 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 420 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 11.00 days. Decay Date: 1971-05-29 . USAF Sat Cat: 5230 . COSPAR: 1971-043A. Apogee: 257 km (159 mi). Perigee: 199 km (123 mi). Inclination: 51.80 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 May 28 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 424 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-06-10 . USAF Sat Cat: 5248 . COSPAR: 1971-048A. Apogee: 282 km (175 mi). Perigee: 204 km (126 mi). Inclination: 65.40 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 May 29 - .
03:49 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 425 - .
Mass: 820 kg (1,800 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1979-11-30 . USAF Sat Cat: 5253 . COSPAR: 1971-050A. Apogee: 553 km (343 mi). Perigee: 506 km (314 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible ELINT satellite..
1971 June 11 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 427 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1971-06-23 . USAF Sat Cat: 5289 . COSPAR: 1971-055A. Apogee: 314 km (195 mi). Perigee: 204 km (126 mi). Inclination: 72.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 June 15 - .
18:41 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 01 (Big Bird) - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1971-08-06 . USAF Sat Cat: 5297 . COSPAR: 1971-056A. Apogee: 300 km (180 mi). Perigee: 180 km (110 mi). Inclination: 96.40 deg. Period: 89.30 min. The 6595th Space Test Group at Vandenberg AFB launched the first Titan HID space booster (Vehicle D-l). KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1971 June 24 - .
07:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 428 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1971-07-06 . USAF Sat Cat: 5305 . COSPAR: 1971-057A. Apogee: 257 km (159 mi). Perigee: 205 km (127 mi). Inclination: 51.70 deg. Period: 89.10 min. Area survey photo reconnaissance satellite; returned film capsule; deployed electron and gamma ray science capsule..
1971 July 16 - .
10:50 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- OPS 8373 - .
Payload: Ferret 16 / Agena D 2737?. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Ferret.
Decay Date: 1978-08-31 . USAF Sat Cat: 5329 . COSPAR: 1971-060A. Apogee: 460 km (280 mi). Perigee: 450 km (270 mi). Inclination: 74.90 deg. Period: 93.60 min.
1971 July 20 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 429 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-08-02 . USAF Sat Cat: 5331 . COSPAR: 1971-061A. Apogee: 252 km (156 mi). Perigee: 202 km (125 mi). Inclination: 51.80 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 July 22 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Launch vehicle failed to orbit - unknown cause..
Failed Stage: U.
1971 July 23 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 430 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-08-05 . USAF Sat Cat: 5340 . COSPAR: 1971-062A. Apogee: 305 km (189 mi). Perigee: 199 km (123 mi). Inclination: 65.40 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 July 30 - .
08:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 431 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1971-08-11 . USAF Sat Cat: 5364 . COSPAR: 1971-065A. Apogee: 284 km (176 mi). Perigee: 165 km (102 mi). Inclination: 51.70 deg. Period: 89.00 min. Area survey photo reconnaissance satellite; returned film capsule..
1971 August 5 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 432 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-08-18 . USAF Sat Cat: 5379 . COSPAR: 1971-066A. Apogee: 252 km (156 mi). Perigee: 200 km (120 mi). Inclination: 51.70 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 August 7 - .
00:11 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576A2.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
- Cannonball 2 - .
Payload: LOADS 2. Mass: 364 kg (802 lb). Nation: USA.
Agency: USAF STP.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Cannonball.
Decay Date: 1972-01-31 . USAF Sat Cat: 5382 . COSPAR: 1971-067C. Apogee: 1,970 km (1,220 mi). Perigee: 133 km (82 mi). Inclination: 92.00 deg. Period: 106.30 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- LCS 4 - .
Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: US Army.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: LCS.
Decay Date: 1972-06-11 . USAF Sat Cat: 5396 . COSPAR: 1971-067F. Apogee: 910 km (560 mi). Perigee: 779 km (484 mi). Inclination: 87.60 deg. Period: 101.80 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- Rigidsphere - .
Payload: AVL-802 Rigid Sphere. Mass: 6.00 kg (13.20 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Rigidsphere.
Decay Date: 1979-11-02 . USAF Sat Cat: 5406 . COSPAR: 1971-067H. Apogee: 916 km (569 mi). Perigee: 781 km (485 mi). Inclination: 87.60 deg. Period: 101.80 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1971 August 12 - .
15:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 8607 - .
Payload: KH-8 no. 32 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1971-09-03 . USAF Sat Cat: 5409 . COSPAR: 1971-070A. Apogee: 424 km (263 mi). Perigee: 137 km (85 mi). Inclination: 111.00 deg. Period: 90.10 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1971 September 7 - .
01:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 436 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-01-04 . USAF Sat Cat: 5461 . COSPAR: 1971-074A. Apogee: 543 km (337 mi). Perigee: 510 km (310 mi). Inclination: 74.00 deg. Period: 95.10 min. Possible ELINT satellite..
1971 September 10 - .
03:37 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 437 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-03-29 . USAF Sat Cat: 5466 . COSPAR: 1971-075A. Apogee: 539 km (334 mi). Perigee: 517 km (321 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 436. Possible ELINT satellite..
1971 September 10 - .
21:33 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1115 - .
Payload: KH-4B s/n 1115 / Agena D 1662 / OPS 5454. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1971-10-05 . USAF Sat Cat: 5468 . COSPAR: 1971-076A. Apogee: 234 km (145 mi). Perigee: 157 km (97 mi). Inclination: 74.90 deg. Period: 88.30 min. KH-4B. Overall image quality is good..
- SRV 831 - .
Payload: SRV 1115-1. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1976-02-03 . USAF Sat Cat: 5469 . COSPAR: 1971-076xx. Apogee: 197 km (122 mi). Perigee: 187 km (116 mi). Inclination: 75.00 deg. Period: 88.30 min.
1971 September 14 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 438 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1971-09-27 . USAF Sat Cat: 5475 . COSPAR: 1971-077A. Apogee: 279 km (173 mi). Perigee: 205 km (127 mi). Inclination: 65.40 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 September 21 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 439 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 11.00 days. Decay Date: 1971-10-02 . USAF Sat Cat: 5478 . COSPAR: 1971-078A. Apogee: 263 km (163 mi). Perigee: 226 km (140 mi). Inclination: 65.40 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule..
1971 September 28 - .
07:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 441 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 12.00 days. Decay Date: 1971-10-10 . USAF Sat Cat: 5486 . COSPAR: 1971-081A. Apogee: 266 km (165 mi). Perigee: 207 km (128 mi). Inclination: 65.00 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 September 29 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 442 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-10-12 . USAF Sat Cat: 5493 . COSPAR: 1971-084A. Apogee: 313 km (194 mi). Perigee: 182 km (113 mi). Inclination: 72.90 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 October 7 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 443 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1971-10-19 . USAF Sat Cat: 5536 . COSPAR: 1971-085A. Apogee: 300 km (180 mi). Perigee: 204 km (126 mi). Inclination: 65.40 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; deployed science capsule..
1971 October 14 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 452 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-10-27 . USAF Sat Cat: 5558 . COSPAR: 1971-088A. Apogee: 248 km (154 mi). Perigee: 193 km (119 mi). Inclination: 64.90 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 October 23 - .
17:16 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 7616 - .
Payload: KH-8 no. 33 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1971-11-17 . USAF Sat Cat: 5575 . COSPAR: 1971-092A. Apogee: 369 km (229 mi). Perigee: 135 km (83 mi). Inclination: 110.90 deg. Period: 89.50 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1971 November 2 - .
14:25 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 454 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 14.00 days. Decay Date: 1971-11-16 . USAF Sat Cat: 5585 . COSPAR: 1971-094A. Apogee: 346 km (214 mi). Perigee: 204 km (126 mi). Inclination: 65.40 deg. Period: 90.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 November 19 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 456 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1971-12-02 . USAF Sat Cat: 5611 . COSPAR: 1971-098A. Apogee: 304 km (188 mi). Perigee: 178 km (110 mi). Inclination: 72.90 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 November 30 - .
16:39 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 460 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-03-05 . USAF Sat Cat: 5628 . COSPAR: 1971-103A. Apogee: 541 km (336 mi). Perigee: 517 km (321 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible ELINT satellite..
1971 December 4 - .
22:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
FAILURE: First stage failure..
Failed Stage: 1.
- AFP-827 / Canyon 4 - .
Payload: Canyon 4 / Agena D. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Canyon.
Decay Date: 1971-12-04 .
1971 December 6 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 463 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 5.00 days. Decay Date: 1971-12-11 . USAF Sat Cat: 5661 . COSPAR: 1971-107A. Apogee: 272 km (169 mi). Perigee: 202 km (125 mi). Inclination: 64.00 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 December 10 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 464 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 6.00 days. Decay Date: 1971-12-16 . USAF Sat Cat: 5670 . COSPAR: 1971-108A. Apogee: 311 km (193 mi). Perigee: 180 km (110 mi). Inclination: 72.00 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 December 14 - .
12:13 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC1W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2G Agena D.
- OPS 7898 P/L 1 - .
Payload: NRL PL171 / OPS 7898 / Poppy 7A (Poppy multifacete. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 5678 . COSPAR: 1971-110A. Apogee: 999 km (620 mi). Perigee: 983 km (610 mi). Inclination: 70.00 deg. Period: 104.90 min. Launch of a quadruplet of Poppy naval signals intelligence satellites. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- OPS 7898 P/L 2 - .
Payload: NRL PL172 / OPS 7898 / Poppy 7B (Poppy multifacete. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 5680 . COSPAR: 1971-110C. Apogee: 999 km (620 mi). Perigee: 983 km (610 mi). Inclination: 70.00 deg. Period: 104.90 min. Poppy naval signals intelligence satellite. Official and secondary mission: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- OPS 7898 P/L 3 - .
Payload: NRL PL173 / OPS 7898 / Poppy 7C (Poppy multifacete. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 5681 . COSPAR: 1971-110D. Apogee: 997 km (619 mi). Perigee: 982 km (610 mi). Inclination: 70.00 deg. Period: 104.90 min. Poppy naval signals intelligence satellite. Official and secondary mission: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
- OPS 7898 P/L 4 - .
Payload: NRL PL174 / OPS 7898 / Poppy 7D (Poppy multifacete. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRL.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: Poppy.
USAF Sat Cat: 5682 . COSPAR: 1971-110E. Apogee: 997 km (619 mi). Perigee: 981 km (609 mi). Inclination: 70.00 deg. Period: 104.90 min. Poppy naval signals intelligence satellite. Official and secondary mission: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1971 December 16 - .
09:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 466 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 11.00 days. Decay Date: 1971-12-27 . USAF Sat Cat: 5687 . COSPAR: 1971-112A. Apogee: 375 km (233 mi). Perigee: 175 km (108 mi). Inclination: 64.00 deg. Period: 90.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1971 December 25 - .
11:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 469 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1972-02-09 . USAF Sat Cat: 5737 . COSPAR: 1971-117B. Apogee: 1,006 km (625 mi). Perigee: 948 km (589 mi). Inclination: 64.50 deg. Period: 104.60 min. Ocean surveillance; nuclear powered. First RORSAT flight confirmed by Russian source to have had BES-5 nuclear reactor..
1971 December 27 - .
14:04 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 470 - .
Payload: Zenit-4MT no. 1. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 10.00 days. Decay Date: 1972-01-06 . USAF Sat Cat: 5727 . COSPAR: 1971-118A. Apogee: 259 km (160 mi). Perigee: 192 km (119 mi). Inclination: 65.00 deg. Period: 89.00 min. Military topography satellite; returned film capsule; deployed science capsule..
1972 January 12 - .
09:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 471 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-01-25 . USAF Sat Cat: 5764 . COSPAR: 1972-001A. Apogee: 316 km (196 mi). Perigee: 201 km (124 mi). Inclination: 65.00 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 January 20 - .
18:36 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 02 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1972-02-29 . USAF Sat Cat: 5769 . COSPAR: 1972-002A. Apogee: 330 km (200 mi). Perigee: 153 km (95 mi). Inclination: 97.00 deg. Period: 89.30 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 7719 - .
Payload: SSF-B No. 22. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1979-04-17 . USAF Sat Cat: 5772 . COSPAR: 1972-002D. Apogee: 545 km (338 mi). Perigee: 474 km (294 mi). Inclination: 96.00 deg. Period: 94.80 min. Radar monitoring..
1972 February 3 - .
08:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 473 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-02-15 . USAF Sat Cat: 5821 . COSPAR: 1972-006A. Apogee: 309 km (192 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1972 February 16 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 474 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-02-29 . USAF Sat Cat: 5839 . COSPAR: 1972-008A. Apogee: 325 km (201 mi). Perigee: 177 km (109 mi). Inclination: 64.90 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 February 16 - .
09:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 33B.
FAILURE: Failure.
- Jumpseat 2 - .
Payload: OPS 1844. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Jumpseat.
1972 March 1 - .
09:39 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- IMEWS 3 - .
Payload: DSP Phase 1 s/n 3 / OPS 1570. Mass: 900 kg (1,980 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1981-08-03 . USAF Sat Cat: 5851 . COSPAR: 1972-010A. Apogee: 35,962 km (22,345 mi). Perigee: 35,416 km (22,006 mi). Inclination: 0.20 deg. Period: 1,429.90 min. First generation geosynchronous ballistic missile launch detection satellite, remained in service for over nine years. Positioned over the Pacific Ocean at 165 deg E in 1979-1980. As of 2003 Mar 5 located at 74.63E drifting at 0.712W degrees per day..
1972 March 1 - .
11:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 476 - .
Payload: Tselina-D no. 3. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1991-10-25 . USAF Sat Cat: 5852 . COSPAR: 1972-011A. Apogee: 388 km (241 mi). Perigee: 379 km (235 mi). Inclination: 81.20 deg. Period: 92.20 min.
1972 March 4 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 477 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-03-16 . USAF Sat Cat: 5862 . COSPAR: 1972-013A. Apogee: 306 km (190 mi). Perigee: 202 km (125 mi). Inclination: 72.90 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule; separated particle flux and radiation experiment capsule..
1972 March 15 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 478 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-03-28 . USAF Sat Cat: 5885 . COSPAR: 1972-015A. Apogee: 282 km (175 mi). Perigee: 176 km (109 mi). Inclination: 65.00 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 March 17 - .
17:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 1678 - .
Payload: KH-8 no. 34 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1972-04-11 . USAF Sat Cat: 5888 . COSPAR: 1972-016A. Apogee: 409 km (254 mi). Perigee: 131 km (81 mi). Inclination: 111.00 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1972 March 22 - .
20:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 479 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-04-13 . USAF Sat Cat: 5894 . COSPAR: 1972-017A. Apogee: 537 km (333 mi). Perigee: 517 km (321 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible ELINT satellite..
1972 March 26 - .
- Tselina-O accepted into military service. - .
Nation: Russia.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On adoption of Tselina-O into armaments' was issued..
1972 April 3 - .
10:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 483 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 12.00 days. Decay Date: 1972-04-15 . USAF Sat Cat: 5924 . COSPAR: 1972-024A. Apogee: 313 km (194 mi). Perigee: 209 km (129 mi). Inclination: 72.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 April 6 - .
08:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 484 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-04-18 . USAF Sat Cat: 5933 . COSPAR: 1972-026A. Apogee: 223 km (138 mi). Perigee: 194 km (120 mi). Inclination: 81.00 deg. Period: 88.60 min. Area survey photo reconnaissance satellite; returned film capsule; separated cosmic ray experiment capsule..
1972 April 14 - .
08:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 486 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-04-27 . USAF Sat Cat: 5945 . COSPAR: 1972-030A. Apogee: 234 km (145 mi). Perigee: 178 km (110 mi). Inclination: 81.30 deg. Period: 88.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 April 19 - .
21:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1116 - .
Payload: KH-4B s/n 1116 / Agena D 1661 / OPS 5640. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1972-05-12 . USAF Sat Cat: 6003 . COSPAR: 1972-032A. Apogee: 276 km (171 mi). Perigee: 154 km (95 mi). Inclination: 81.00 deg. Period: 88.80 min. KH-4B. Very successful mission and image quality was good..
1972 May 5 - .
11:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 488 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1972-05-18 . USAF Sat Cat: 6016 . COSPAR: 1972-034A. Apogee: 294 km (182 mi). Perigee: 207 km (128 mi). Inclination: 65.40 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 May 17 - .
10:19 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 490 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-05-29 . USAF Sat Cat: 6021 . COSPAR: 1972-036A. Apogee: 285 km (177 mi). Perigee: 205 km (127 mi). Inclination: 65.00 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule; separated electron flux cosmic ray experiment capsule..
1972 May 20 - .
15:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
FAILURE: Failure.
Failed Stage: U.
- OPS 6574 - .
Payload: KH-8 no. 35 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
1972 May 25 - .
06:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 491 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 14.00 days. Decay Date: 1972-06-08 . USAF Sat Cat: 6035 . COSPAR: 1972-038A. Apogee: 268 km (166 mi). Perigee: 177 km (109 mi). Inclination: 64.90 deg. Period: 88.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 May 25 - .
18:41 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thorad SLV-2H Agena D.
- KH-4B 1117 - .
Payload: KH-4B s/n 1117 / Agena D 1663 / OPS 6371. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4B.
Decay Date: 1972-06-04 . USAF Sat Cat: 6037 . COSPAR: 1972-039A. Apogee: 305 km (189 mi). Perigee: 158 km (98 mi). Inclination: 96.30 deg. Period: 89.20 min. KH-4B. Last KH-4B mission. Very successful mission, image quality was good. Final CORONA mission..
1972 June 9 - .
06:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 492 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-06-22 . USAF Sat Cat: 6049 . COSPAR: 1972-040A. Apogee: 323 km (200 mi). Perigee: 204 km (126 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 June 21 - .
06:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 493 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-07-03 . USAF Sat Cat: 6053 . COSPAR: 1972-042A. Apogee: 267 km (165 mi). Perigee: 202 km (125 mi). Inclination: 64.90 deg. Period: 89.10 min. Area survey photo reconnaissance satellite; returned film capsule..
1972 June 23 - .
11:19 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 495 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-07-06 . USAF Sat Cat: 6060 . COSPAR: 1972-044A. Apogee: 277 km (172 mi). Perigee: 202 km (125 mi). Inclination: 65.40 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 July 6 - .
10:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 499 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 11.00 days. Decay Date: 1972-07-17 . USAF Sat Cat: 6090 . COSPAR: 1972-051A. Apogee: 283 km (175 mi). Perigee: 204 km (126 mi). Inclination: 51.80 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 July 7 - .
17:46 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 03 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1972-09-13 . USAF Sat Cat: 6094 . COSPAR: 1972-052A. Apogee: 254 km (157 mi). Perigee: 176 km (109 mi). Inclination: 96.00 deg. Period: 88.70 min. KH-9 type satellite. Investigation of the upper atmosphere and outer space. .
- OPS 7803 - .
Payload: SSF-B No. 23. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1978-05-06 . USAF Sat Cat: 6096 . COSPAR: 1972-052C. Apogee: 504 km (313 mi). Perigee: 498 km (309 mi). Inclination: 96.20 deg. Period: 94.70 min. Radar monitoring..
1972 July 10 - .
16:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 500 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-03-29 . USAF Sat Cat: 6097 . COSPAR: 1972-053A. Apogee: 548 km (340 mi). Perigee: 505 km (313 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible navigation satellite. Replaced Cosmos 425..
1972 July 13 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 502 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1972-07-25 . USAF Sat Cat: 6105 . COSPAR: 1972-055A. Apogee: 262 km (162 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.10 min. Military topography satellite; returned film capsule; carried science package..
1972 July 19 - .
13:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 503 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-08-01 . USAF Sat Cat: 6114 . COSPAR: 1972-056A. Apogee: 288 km (178 mi). Perigee: 202 km (125 mi). Inclination: 65.40 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 July 28 - .
10:19 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 512 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-08-09 . USAF Sat Cat: 6130 . COSPAR: 1972-059A. Apogee: 273 km (169 mi). Perigee: 202 km (125 mi). Inclination: 65.30 deg. Period: 89.20 min. Area survey photo reconnaissance satellite; returned film capsule..
1972 August 2 - .
08:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 513 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 14.00 days. Decay Date: 1972-08-15 . USAF Sat Cat: 6135 . COSPAR: 1972-060A. Apogee: 307 km (190 mi). Perigee: 172 km (106 mi). Inclination: 64.90 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 August 18 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 515 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1972-08-31 . USAF Sat Cat: 6150 . COSPAR: 1972-063A. Apogee: 309 km (192 mi). Perigee: 203 km (126 mi). Inclination: 72.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 August 21 - .
10:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 516 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1972-10-20 . USAF Sat Cat: 6199 . COSPAR: 1972-066C. Apogee: 1,038 km (644 mi). Perigee: 906 km (562 mi). Inclination: 64.80 deg. Period: 104.50 min. Ocean surveillance; nuclear powered..
1972 August 30 - .
08:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 517 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-09-11 . USAF Sat Cat: 6168 . COSPAR: 1972-067A. Apogee: 285 km (177 mi). Perigee: 203 km (126 mi). Inclination: 64.90 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule..
1972 September 1 - .
17:44 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 8888 - .
Payload: KH-8 no. 36 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1972-09-30 . USAF Sat Cat: 6172 . COSPAR: 1972-068A. Apogee: 381 km (236 mi). Perigee: 142 km (88 mi). Inclination: 110.40 deg. Period: 89.70 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1972 September 15 - .
09:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 518 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 9.00 days. Decay Date: 1972-09-24 . USAF Sat Cat: 6186 . COSPAR: 1972-070A. Apogee: 306 km (190 mi). Perigee: 203 km (126 mi). Inclination: 72.80 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1972 September 16 - .
08:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 519 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 10.00 days. Decay Date: 1972-09-26 . USAF Sat Cat: 6188 . COSPAR: 1972-071A. Apogee: 360 km (220 mi). Perigee: 207 km (128 mi). Inclination: 71.30 deg. Period: 90.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 September 19 - .
19:19 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 520 - .
Payload: Oko #1. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 6192 . COSPAR: 1972-072A. Apogee: 33,393 km (20,749 mi). Perigee: 6,841 km (4,250 mi). Inclination: 69.90 deg. Period: 715.30 min. Covered Oko constellation plane 3 - 355 degree longitude of ascending node..
1972 October 4 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 522 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-10-17 . USAF Sat Cat: 6219 . COSPAR: 1972-077A. Apogee: 309 km (192 mi). Perigee: 212 km (131 mi). Inclination: 72.00 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 October 10 - .
18:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 04 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1973-01-08 . USAF Sat Cat: 6227 . COSPAR: 1972-079A. Apogee: 281 km (174 mi). Perigee: 160 km (90 mi). Inclination: 96.50 deg. Period: 88.90 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 8314/2 - .
Payload: SSF-C No. 3 / OPS 8314. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 6822 . COSPAR: 1972-079C. Apogee: 1,464 km (909 mi). Perigee: 1,420 km (880 mi). Inclination: 95.60 deg. Period: 114.70 min. ABM monitoring..
1972 October 18 - .
11:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 525 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 11.00 days. Decay Date: 1972-10-29 . USAF Sat Cat: 6248 . COSPAR: 1972-083A. Apogee: 268 km (166 mi). Perigee: 207 km (128 mi). Inclination: 65.00 deg. Period: 89.20 min. Area survey photo reconnaissance satellite; returned film capsule; separated Nauka autonomous subsatellite 16KS No 161 / 1L which tested Kondor control system for Yantar satellite..
1972 October 31 - .
13:29 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 527 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1972-11-13 . USAF Sat Cat: 6260 . COSPAR: 1972-086A. Apogee: 306 km (190 mi). Perigee: 207 km (128 mi). Inclination: 65.40 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 November 3 - .
01:34 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/1?.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 536 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-07-20 . USAF Sat Cat: 6272 . COSPAR: 1972-088A. Apogee: 539 km (334 mi). Perigee: 522 km (324 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible navigation satellite..
1972 November 25 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 537 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1972-12-07 . USAF Sat Cat: 6287 . COSPAR: 1972-093A. Apogee: 303 km (188 mi). Perigee: 203 km (126 mi). Inclination: 64.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1972 December 14 - .
13:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 538 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1972-12-27 . USAF Sat Cat: 6311 . COSPAR: 1972-099A. Apogee: 283 km (175 mi). Perigee: 205 km (127 mi). Inclination: 65.40 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1972 December 20 - .
22:20 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- Canyon 5 - .
Payload: Canyon Improved / OPS 9390. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Canyon.
USAF Sat Cat: 6317 . COSPAR: 1972-101A. Apogee: 40,728 km (25,307 mi). Perigee: 31,012 km (19,269 mi). Inclination: 9.70 deg. Period: 1,440.40 min. First launch of improved ELINT satellite. In comparison to earlier Canyon ELINT satellites, Improved Canyon had a similar but heavier payload which separated from the Agena D final stage..
1972 December 21 - .
17:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 3978 - .
Payload: KH-8 no. 37 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1973-01-23 . USAF Sat Cat: 6321 . COSPAR: 1972-103A. Apogee: 378 km (234 mi). Perigee: 139 km (86 mi). Inclination: 110.50 deg. Period: 89.70 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1972 December 27 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 541 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1973-01-08 . USAF Sat Cat: 6326 . COSPAR: 1972-105A. Apogee: 348 km (216 mi). Perigee: 218 km (135 mi). Inclination: 81.00 deg. Period: 90.20 min. Military topography satellite; returned film capsule; separated science capsule..
1972 December 28 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 542 - .
Payload: Tselina-D no. 4. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1983-10-09 . USAF Sat Cat: 6328 . COSPAR: 1972-106A. Apogee: 640 km (390 mi). Perigee: 527 km (327 mi). Inclination: 81.00 deg. Period: 96.30 min.
1973 January 11 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 543 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-01-24 . USAF Sat Cat: 6339 . COSPAR: 1973-002A. Apogee: 274 km (170 mi). Perigee: 191 km (118 mi). Inclination: 64.90 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 January 20 - .
03:36 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 544 - .
Mass: 750 kg (1,650 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-06-15 . USAF Sat Cat: 6343 . COSPAR: 1973-003A. Apogee: 535 km (332 mi). Perigee: 528 km (328 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 460. Possible ELINT satellite..
1973 February 1 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 547 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1973-02-13 . USAF Sat Cat: 6353 . COSPAR: 1973-006A. Apogee: 309 km (192 mi). Perigee: 203 km (126 mi). Inclination: 64.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1973 February 8 - .
13:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 548 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-02-21 . USAF Sat Cat: 6359 . COSPAR: 1973-008A. Apogee: 300 km (180 mi). Perigee: 205 km (127 mi). Inclination: 65.40 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 February 28 - .
04:37 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 549 - .
Mass: 750 kg (1,650 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-06-29 . USAF Sat Cat: 6373 . COSPAR: 1973-010A. Apogee: 545 km (338 mi). Perigee: 513 km (318 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible ELINT satellite..
1973 March - .
- Tselina-2 ELINT satellite authorised - .
Nation: Russia.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
The improved model had an increased frequency range and on-board method of determining the position of fixed transmitters. The Tselina-2 prime contractors were TsNIRTI Minradioprom (M E Zaslovskiy) for the ELINT equipment and KB Yuzhnoye (KB-3, B S Khimrov) for the spacecraft bus. The launch vehicle was by OKB MEI Minvuza (A F Bogomolov) and the encrypted communications system by 0-TsNII KS MO.
1973 March 1 - .
12:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 550 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 10.00 days. Decay Date: 1973-03-11 . USAF Sat Cat: 6376 . COSPAR: 1973-011A. Apogee: 317 km (196 mi). Perigee: 206 km (128 mi). Inclination: 65.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 March 6 - .
09:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 551 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 14.00 days. Decay Date: 1973-03-20 . USAF Sat Cat: 6378 . COSPAR: 1973-012A. Apogee: 296 km (183 mi). Perigee: 206 km (128 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 March 6 - .
09:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- OPS 6063 - .
Payload: AFP-720 Rhyolite 2. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Rhyolite.
USAF Sat Cat: 6380 . COSPAR: 1973-013A. Apogee: 35,855 km (22,279 mi). Perigee: 35,679 km (22,169 mi). Inclination: 0.20 deg. Period: 1,435.10 min. Second launch of Rhyolite geostationary ELINT satellite..
1973 March 9 - .
21:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 05 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1973-05-17 . USAF Sat Cat: 6382 . COSPAR: 1973-014A. Apogee: 262 km (162 mi). Perigee: 150 km (90 mi). Inclination: 95.70 deg. Period: 88.70 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1973 March 22 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 552 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1973-04-03 . USAF Sat Cat: 6394 . COSPAR: 1973-016A. Apogee: 308 km (191 mi). Perigee: 202 km (125 mi). Inclination: 72.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule; separated Nauka autonomous subsatellite 16KS No 162 / 2L which tested Kondor control system for Yantar satellite..
1973 April 19 - .
08:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 554 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 38.00 days. Decay Date: 1973-05-07 . USAF Sat Cat: 6432 . COSPAR: 1973-021A. Apogee: 304 km (188 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable; exploded in orbit..
1973 April 25 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
FAILURE: Payload propulsion system failed; no orbit..
Failed Stage: P.
- RORSAT failure - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: RVSN.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1973-04-25 . COSPAR: F730425A. Ocean surveillance; nuclear powered. Last launch of original US-A design by Savin's KB. American 'sniffer' aircraft flew over the Pacific after this failure looking for radioisotopes traces in order to characterise the reactor..
1973 April 25 - .
10:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 555 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1973-05-07 . USAF Sat Cat: 6440 . COSPAR: 1973-024A. Apogee: 230 km (140 mi). Perigee: 216 km (134 mi). Inclination: 81.00 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1973 May 5 - .
07:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 556 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 9.00 days. Decay Date: 1973-05-14 . USAF Sat Cat: 6446 . COSPAR: 1973-025A. Apogee: 240 km (140 mi). Perigee: 199 km (123 mi). Inclination: 81.30 deg. Period: 88.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 May 16 - .
16:40 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 2093 - .
Payload: KH-8 no. 38 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1973-06-13 . USAF Sat Cat: 6640 . COSPAR: 1973-028A. Apogee: 352 km (218 mi). Perigee: 136 km (84 mi). Inclination: 110.50 deg. Period: 89.40 min. The 40th Titan IIIB/Agena D was launched from Vandenberg AFB by the Space and Missile Test Center's 6595th Space Test Group. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1973 May 18 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 559 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 5.00 days. Decay Date: 1973-05-23 . USAF Sat Cat: 6647 . COSPAR: 1973-030A. Apogee: 325 km (201 mi). Perigee: 204 km (126 mi). Inclination: 65.40 deg. Period: 89.80 min. First flight of Soyuz U launch vehicle. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 May 23 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 560 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-06-05 . USAF Sat Cat: 6652 . COSPAR: 1973-031A. Apogee: 314 km (195 mi). Perigee: 203 km (126 mi). Inclination: 72.90 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 May 25 - .
13:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 561 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1973-06-06 . USAF Sat Cat: 6657 . COSPAR: 1973-033A. Apogee: 295 km (183 mi). Perigee: 206 km (128 mi). Inclination: 65.40 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; separated gamma ray telescope experiment capsule..
1973 June 6 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 563 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 12.00 days. Decay Date: 1973-06-18 . USAF Sat Cat: 6667 . COSPAR: 1973-036A. Apogee: 298 km (185 mi). Perigee: 206 km (128 mi). Inclination: 65.40 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 June 10 - .
10:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 572 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-06-23 . USAF Sat Cat: 6684 . COSPAR: 1973-038A. Apogee: 281 km (174 mi). Perigee: 206 km (128 mi). Inclination: 51.70 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 June 12 - .
07:14 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- IMEWS 4 - .
Payload: DSP Phase 1 s/n 4 / OPS 6157. Mass: 900 kg (1,980 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1980-11-01 . USAF Sat Cat: 6691 . COSPAR: 1973-040A. Apogee: 35,786 km (22,236 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.30 deg. Period: 1,435.90 min.
First generation geosynchronous ballistic missile launch detection satellite, remained in service for over seven years. Positioned in geosynchronous orbit over the Indian Ocean at 75E in 1973; over the Americas at 105 deg W in 1979-1980. As of 1983 Jan 3 located at 73.21W drifting at 1.648W degrees per day.
1973 June 21 - .
13:29 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 575 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1973-07-03 . USAF Sat Cat: 6709 . COSPAR: 1973-043A. Apogee: 271 km (168 mi). Perigee: 204 km (126 mi). Inclination: 65.40 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule; separated capsule..
1973 June 26 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
FAILURE: Agena upper stage failed to orbit..
Failed Stage: U.
- OPS 4018 - .
Payload: KH-8 no. 39 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1973-06-26 .
1973 June 26 - .
01:22 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Nine persons were killed in the explosion of the vehicle..
Failed Stage: U.
- Nine killed in fuelling accident at Plesetsk - .
Nation: Russia.
Agency: RVSN.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
COSPAR: F730626BA. Nine were killed at the LC-133 Voskhod complex during preparation of a Kosmos-3M booster. Oxidiser and propellant were accidentally mixed together during fuelling..
1973 June 27 - .
11:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 576 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1973-07-09 . USAF Sat Cat: 6713 . COSPAR: 1973-044A. Apogee: 332 km (206 mi). Perigee: 204 km (126 mi). Inclination: 72.90 deg. Period: 89.80 min. Military topography satellite; returned film capsule; separated science capsule..
1973 July 4 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
Launch Pad: LC43/pad?.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
FAILURE: Failure.
Failed Stage: U.
- Zenit-4M - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
High resolution photo reconnaissance mission..
1973 July 13 - .
20:24 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 06 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1973-10-12 . USAF Sat Cat: 6727 . COSPAR: 1973-046A. Apogee: 291 km (180 mi). Perigee: 143 km (88 mi). Inclination: 96.20 deg. Period: 88.80 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1973 July 25 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 577 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-08-07 . USAF Sat Cat: 6745 . COSPAR: 1973-048A. Apogee: 309 km (192 mi). Perigee: 175 km (108 mi). Inclination: 65.40 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 August 1 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 578 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1973-08-13 . USAF Sat Cat: 6759 . COSPAR: 1973-051A. Apogee: 292 km (181 mi). Perigee: 200 km (120 mi). Inclination: 65.40 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule..
1973 August 21 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 579 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-09-03 . USAF Sat Cat: 6789 . COSPAR: 1973-055A. Apogee: 270 km (160 mi). Perigee: 171 km (106 mi). Inclination: 65.40 deg. Period: 88.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 August 21 - .
16:07 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 33B.
- Jumpseat 3 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Jumpseat.
USAF Sat Cat: 6791 . COSPAR: 1973-056A. Apogee: 39,296 km (24,417 mi). Perigee: 460 km (280 mi). Inclination: 63.30 deg. Period: 705.70 min.
1973 August 24 - .
10:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 581 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-09-06 . USAF Sat Cat: 6798 . COSPAR: 1973-059A. Apogee: 276 km (171 mi). Perigee: 177 km (109 mi). Inclination: 51.60 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 August 28 - .
10:08 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 582 - .
Mass: 750 kg (1,650 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-09-05 . USAF Sat Cat: 6802 . COSPAR: 1973-060A. Apogee: 543 km (337 mi). Perigee: 519 km (322 mi). Inclination: 74.00 deg. Period: 95.30 min. Possible ELINT satellite..
1973 August 30 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 583 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1973-09-12 . USAF Sat Cat: 6809 . COSPAR: 1973-062A. Apogee: 298 km (185 mi). Perigee: 204 km (126 mi). Inclination: 64.90 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; separated capsule..
1973 September 6 - .
10:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 584 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 14.00 days. Decay Date: 1973-09-20 . USAF Sat Cat: 6818 . COSPAR: 1973-063A. Apogee: 336 km (208 mi). Perigee: 205 km (127 mi). Inclination: 72.90 deg. Period: 90.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 September 21 - .
13:05 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 587 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1973-10-04 . USAF Sat Cat: 6832 . COSPAR: 1973-066A. Apogee: 301 km (187 mi). Perigee: 205 km (127 mi). Inclination: 65.40 deg. Period: 89.60 min. Second flight of Soyuz U launch vehicle. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 September 27 - .
17:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 6275 - .
Payload: KH-8 no. 40 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1973-10-29 . USAF Sat Cat: 6837 . COSPAR: 1973-068A. Apogee: 385 km (239 mi). Perigee: 131 km (81 mi). Inclination: 110.50 deg. Period: 89.70 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1973 October 3 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 596 - .
Payload: FEU-170 s/n 1L. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 6.00 days. Decay Date: 1973-10-09 . USAF Sat Cat: 6856 . COSPAR: 1973-070A. Apogee: 287 km (178 mi). Perigee: 206 km (128 mi). Inclination: 65.40 deg. Period: 89.40 min.
Area survey photo reconnaissance satellite; returned film capsule. First test of small film return capsules planned for Yantar spacecraft. SpK capsule FEU-170 No. 1L experienced an electrical short circuit, which led to failure to separate the shell of the capsule after reentry, preventing parachute deployment. The capsule crashed into the ground.
1973 October 6 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 597 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 6.00 days. Decay Date: 1973-10-12 . USAF Sat Cat: 6858 . COSPAR: 1973-071A. Apogee: 290 km (180 mi). Perigee: 206 km (128 mi). Inclination: 65.40 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 October 10 - .
10:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 598 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 6.00 days. Decay Date: 1973-10-16 . USAF Sat Cat: 6862 . COSPAR: 1973-072A. Apogee: 334 km (207 mi). Perigee: 208 km (129 mi). Inclination: 72.80 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 October 15 - .
08:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 599 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1973-10-28 . USAF Sat Cat: 6867 . COSPAR: 1973-073A. Apogee: 280 km (170 mi). Perigee: 202 km (125 mi). Inclination: 64.90 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule..
1973 October 16 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 600 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 7.00 days. Decay Date: 1973-10-23 . USAF Sat Cat: 6873 . COSPAR: 1973-074A. Apogee: 340 km (210 mi). Perigee: 205 km (127 mi). Inclination: 72.80 deg. Period: 90.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 October 20 - .
10:14 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 602 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 9.00 days. Decay Date: 1973-10-29 . USAF Sat Cat: 6885 . COSPAR: 1973-077A. Apogee: 309 km (192 mi). Perigee: 169 km (105 mi). Inclination: 72.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 October 27 - .
11:09 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 603 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-11-09 . USAF Sat Cat: 6900 . COSPAR: 1973-079A. Apogee: 357 km (221 mi). Perigee: 205 km (127 mi). Inclination: 72.90 deg. Period: 90.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 October 29 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 604 - .
Payload: Tselina-D no. 5. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1992-01-19 . USAF Sat Cat: 6907 . COSPAR: 1973-080A. Apogee: 424 km (263 mi). Perigee: 413 km (256 mi). Inclination: 81.20 deg. Period: 92.90 min.
1973 November 2 - .
13:01 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 606 - .
Payload: Oko #2. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 6916 . COSPAR: 1973-084A. Apogee: 35,385 km (21,987 mi). Perigee: 4,964 km (3,084 mi). Inclination: 69.50 deg. Period: 717.70 min. Replaced Cosmos 520. Covered Oko constellation plane 3 - 359 degree longitude of ascending node..
1973 November 10 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- Titan 23D no. 8 stage - .
Payload: SSF 32. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1973-11-13 . USAF Sat Cat: 6929 . COSPAR: 1973-088C. Apogee: 508 km (315 mi). Perigee: 486 km (301 mi). Inclination: 96.30 deg. Period: 94.50 min. ABM monitoring. .
1973 November 10 - .
12:38 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 607 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1973-11-22 . USAF Sat Cat: 6926 . COSPAR: 1973-087A. Apogee: 341 km (211 mi). Perigee: 203 km (126 mi). Inclination: 72.80 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable (?)..
1973 November 10 - .
20:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 07 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1974-03-13 . USAF Sat Cat: 6928 . COSPAR: 1973-088A. Apogee: 275 km (170 mi). Perigee: 158 km (98 mi). Inclination: 96.90 deg. Period: 88.80 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 7705 - .
Payload: SSF-B No. 24. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1978-12-26 . USAF Sat Cat: 6931 . COSPAR: 1973-088B. Apogee: 505 km (313 mi). Perigee: 488 km (303 mi). Inclination: 96.30 deg. Period: 94.50 min. Radar monitoring..
- OPS 6630 P/L 2 - .
Payload: SSF-C No. 4 / OPS 6630. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 6938 . COSPAR: 1973-088D. Apogee: 1,457 km (905 mi). Perigee: 1,414 km (878 mi). Inclination: 97.00 deg. Period: 114.60 min.
1973 November 21 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 609 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1973-12-04 . USAF Sat Cat: 6943 . COSPAR: 1973-092A. Apogee: 335 km (208 mi). Perigee: 175 km (108 mi). Inclination: 69.90 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 November 27 - .
00:08 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 610 - .
Mass: 750 kg (1,650 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-09-15 . USAF Sat Cat: 6950 . COSPAR: 1973-093A. Apogee: 545 km (338 mi). Perigee: 515 km (320 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible ELINT satellite..
1973 November 28 - .
11:43 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 612 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1973-12-11 . USAF Sat Cat: 6953 . COSPAR: 1973-095A. Apogee: 339 km (210 mi). Perigee: 188 km (116 mi). Inclination: 72.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 December 17 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 616 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 11.00 days. Decay Date: 1973-12-28 . USAF Sat Cat: 6979 . COSPAR: 1973-102A. Apogee: 332 km (206 mi). Perigee: 206 km (128 mi). Inclination: 72.90 deg. Period: 89.90 min. Military topography satellite; returned film capsule; separated science capsule..
1973 December 21 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 625 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1974-01-03 . USAF Sat Cat: 6995 . COSPAR: 1973-105A. Apogee: 321 km (199 mi). Perigee: 204 km (126 mi). Inclination: 72.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1973 December 27 - .
20:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 626 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1974-03-22 . USAF Sat Cat: 7115 . COSPAR: 1973-108D. Apogee: 982 km (610 mi). Perigee: 907 km (563 mi). Inclination: 65.40 deg. Period: 103.90 min. Ocean surveillance; nuclear powered. First test of modernised design by KB Arsenal..
1974 January 24 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 629 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-02-05 . USAF Sat Cat: 7100 . COSPAR: 1974-003A. Apogee: 289 km (179 mi). Perigee: 197 km (122 mi). Inclination: 62.80 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule. First successful test of SpK small film return capsule planned for Yantar. SpK capsule FEU-170-13 No. 1702 / 2L successfully recovered..
1974 January 30 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 630 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1974-02-13 . USAF Sat Cat: 7104 . COSPAR: 1974-004A. Apogee: 346 km (214 mi). Perigee: 203 km (126 mi). Inclination: 72.80 deg. Period: 90.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 February 6 - .
00:34 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 631 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-10-03 . USAF Sat Cat: 7109 . COSPAR: 1974-005A. Apogee: 545 km (338 mi). Perigee: 519 km (322 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 479. Possible ELINT satellite..
1974 February 12 - .
08:56 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 632 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 14.00 days. Decay Date: 1974-02-26 . USAF Sat Cat: 7117 . COSPAR: 1974-006A. Apogee: 303 km (188 mi). Perigee: 176 km (109 mi). Inclination: 65.00 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 February 13 - .
18:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 6889 - .
Payload: KH-8 no. 41 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1974-03-17 . USAF Sat Cat: 7121 . COSPAR: 1974-007A. Apogee: 396 km (246 mi). Perigee: 135 km (83 mi). Inclination: 110.40 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1974 March 14 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 635 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-03-26 . USAF Sat Cat: 7216 . COSPAR: 1974-014A. Apogee: 322 km (200 mi). Perigee: 204 km (126 mi). Inclination: 72.80 deg. Period: 89.70 min. Area survey photo reconnaissance satellite; returned film capsule; separated Nauka autonomous subsatellite 17KS M15000-171 / 1L which tested astro-visir and radio altimeter systems for Yantar..
1974 March 20 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 636 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1974-04-03 . USAF Sat Cat: 7225 . COSPAR: 1974-016A. Apogee: 302 km (187 mi). Perigee: 169 km (105 mi). Inclination: 65.00 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 April 4 - .
08:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 639 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 11.00 days. Decay Date: 1974-04-15 . USAF Sat Cat: 7240 . COSPAR: 1974-019A. Apogee: 226 km (140 mi). Perigee: 206 km (128 mi). Inclination: 81.30 deg. Period: 88.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 April 10 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 08 Capsule - .
Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
COSPAR: 1974-020xx. Apogee: 830 km (510 mi). Perigee: 786 km (488 mi). Inclination: 94.60 deg. Period: 101.10 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- KH-9 no. 08 - .
Payload: OPS 6245. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1974-07-28 . USAF Sat Cat: 7242 . COSPAR: 1974-020A. Apogee: 285 km (177 mi). Perigee: 153 km (95 mi). Inclination: 94.50 deg. Period: 88.90 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 4547 - .
Payload: OPS 4547 / SSF-B No. 25. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1980-02-22 . USAF Sat Cat: 7247 . COSPAR: 1974-020C. Apogee: 531 km (329 mi). Perigee: 503 km (312 mi). Inclination: 94.00 deg. Period: 95.00 min. Radar monitoring..
1974 April 11 - .
12:23 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 640 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-04-23 . USAF Sat Cat: 7245 . COSPAR: 1974-021A. Apogee: 225 km (139 mi). Perigee: 201 km (124 mi). Inclination: 81.30 deg. Period: 88.80 min. Area survey photo reconnaissance satellite; returned film capsule; separated capsule (?)..
1974 April 29 - .
13:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 649 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1974-05-11 . USAF Sat Cat: 7280 . COSPAR: 1974-027A. Apogee: 299 km (185 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 May - .
- Tselina-2 specifications approved. - .
Nation: Russia.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
The draft project was drawn up in the first quarter of 1974 and the MO approved the TTZ in May 1974..
1974 May 15 - .
07:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 651 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1974-09-05 . USAF Sat Cat: 7388 . COSPAR: 1974-029C. Apogee: 946 km (587 mi). Perigee: 890 km (550 mi). Inclination: 65.00 deg. Period: 103.40 min. Ocean surveillance; nuclear powered..
1974 May 15 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 652 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 8.00 days. Decay Date: 1974-05-23 . USAF Sat Cat: 7292 . COSPAR: 1974-030A. Apogee: 343 km (213 mi). Perigee: 173 km (107 mi). Inclination: 51.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 May 15 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 653 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-05-27 . USAF Sat Cat: 7293 . COSPAR: 1974-031A. Apogee: 287 km (178 mi). Perigee: 192 km (119 mi). Inclination: 62.80 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule..
1974 May 17 - .
06:53 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 654 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1974-09-07 . USAF Sat Cat: 7397 . COSPAR: 1974-032D. Apogee: 1,006 km (625 mi). Perigee: 924 km (574 mi). Inclination: 64.90 deg. Period: 104.40 min. Ocean surveillance; nuclear powered..
1974 May 21 - .
06:16 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 655 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-11-19 . USAF Sat Cat: 7306 . COSPAR: 1974-035A. Apogee: 542 km (336 mi). Perigee: 523 km (324 mi). Inclination: 74.10 deg. Period: 95.30 min. Replaced Cosmos 536. Possible ELINT satellite..
1974 May 23 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
Launch Pad: LC43/pad?.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
FAILURE: A problem in separation of the second and third stages of resulted in radio contact being lost with the spacecraft at T+439.6 sec. This automatically triggered the destruct charge in the Yantar OSA Descent Module, destroying the spacecraft and booster..
Failed Stage: 3.
- Yantar-2K failure. - .
Payload: Yantar-2K s/n 1. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
First test launch of Yantar second generation reconnaissance spacecraft..
1974 May 30 - .
12:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 657 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1974-06-13 . USAF Sat Cat: 7317 . COSPAR: 1974-038A. Apogee: 296 km (183 mi). Perigee: 177 km (109 mi). Inclination: 62.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 June 6 - .
06:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 658 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-06-18 . USAF Sat Cat: 7328 . COSPAR: 1974-041A. Apogee: 286 km (177 mi). Perigee: 204 km (126 mi). Inclination: 65.00 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule..
1974 June 6 - .
16:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 1776 - .
Payload: KH-8 no. 42 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1974-07-23 . USAF Sat Cat: 7330 . COSPAR: 1974-042A. Apogee: 394 km (244 mi). Perigee: 136 km (84 mi). Inclination: 110.50 deg. Period: 89.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1974 June 13 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 659 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1974-06-26 . USAF Sat Cat: 7334 . COSPAR: 1974-043A. Apogee: 329 km (204 mi). Perigee: 153 km (95 mi). Inclination: 62.80 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 June 18 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 660 - .
Mass: 650 kg (1,430 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 7337 . COSPAR: 1974-044A. Apogee: 1,536 km (954 mi). Perigee: 383 km (237 mi). Inclination: 83.00 deg. Period: 104.30 min. Radar calibration mission..
1974 June 21 - .
09:03 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 661 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-08-27 . USAF Sat Cat: 7339 . COSPAR: 1974-045A. Apogee: 548 km (340 mi). Perigee: 511 km (317 mi). Inclination: 74.00 deg. Period: 95.20 min. Possible ELINT satellite..
1974 June 29 - .
12:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 664 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1974-07-11 . USAF Sat Cat: 7351 . COSPAR: 1974-049A. Apogee: 341 km (211 mi). Perigee: 205 km (127 mi). Inclination: 72.90 deg. Period: 90.00 min. Military topography satellite; returned film capsule; separated science capsule..
1974 June 29 - .
15:59 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 665 - .
Payload: Oko #3. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 1990-07-06 . USAF Sat Cat: 7352 . COSPAR: 1974-050A. Apogee: 39,653 km (24,639 mi). Perigee: 298 km (185 mi). Inclination: 61.80 deg. Period: 709.60 min. Covered Oko constellation plane 2 - 315 degree longitude of ascending node..
1974 July 12 - .
12:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 666 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1974-07-25 . USAF Sat Cat: 7367 . COSPAR: 1974-053A. Apogee: 328 km (203 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 July 25 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 667 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4M.
Duration: 13.00 days. Decay Date: 1974-08-07 . USAF Sat Cat: 7383 . COSPAR: 1974-057A. Apogee: 320 km (190 mi). Perigee: 176 km (109 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 July 26 - .
07:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 669 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1974-08-08 . USAF Sat Cat: 7389 . COSPAR: 1974-059A. Apogee: 229 km (142 mi). Perigee: 207 km (128 mi). Inclination: 81.30 deg. Period: 88.80 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1974 August 7 - .
12:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 671 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1974-08-20 . USAF Sat Cat: 7409 . COSPAR: 1974-062A. Apogee: 304 km (188 mi). Perigee: 168 km (104 mi). Inclination: 62.80 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 August 14 - .
15:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 3004 - .
Payload: KH-8 no. 43 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1974-09-29 . USAF Sat Cat: 7416 . COSPAR: 1974-065A. Apogee: 402 km (249 mi). Perigee: 135 km (83 mi). Inclination: 110.50 deg. Period: 89.90 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1974 August 16 - .
03:41 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 673 - .
Payload: Tselina-D no. 6. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1991-06-01 . USAF Sat Cat: 7417 . COSPAR: 1974-066A. Apogee: 416 km (258 mi). Perigee: 399 km (247 mi). Inclination: 81.20 deg. Period: 92.70 min.
1974 August 29 - .
07:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 674 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 9.00 days. Decay Date: 1974-09-07 . USAF Sat Cat: 7423 . COSPAR: 1974-068A. Apogee: 323 km (200 mi). Perigee: 175 km (108 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 September 20 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 685 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-10-02 . USAF Sat Cat: 7445 . COSPAR: 1974-073A. Apogee: 281 km (174 mi). Perigee: 209 km (129 mi). Inclination: 64.90 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule..
1974 October 11 - .
11:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 687 - .
Mass: 400 kg (880 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1978-02-05 . USAF Sat Cat: 7469 . COSPAR: 1974-076A. Apogee: 698 km (433 mi). Perigee: 286 km (177 mi). Inclination: 74.00 deg. Period: 94.50 min. Radar calibration mission..
1974 October 18 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 688 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1974-10-30 . USAF Sat Cat: 7473 . COSPAR: 1974-078A. Apogee: 349 km (216 mi). Perigee: 179 km (111 mi). Inclination: 62.80 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 October 25 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 691 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1974-11-06 . USAF Sat Cat: 7483 . COSPAR: 1974-082A. Apogee: 317 km (196 mi). Perigee: 187 km (116 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 October 29 - .
19:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 09 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1975-03-18 . USAF Sat Cat: 7495 . COSPAR: 1974-085A. Apogee: 272 km (169 mi). Perigee: 115 km (71 mi). Inclination: 96.70 deg. Period: 88.40 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6239 - .
Payload: SSF-B No. 26. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1980-01-23 . USAF Sat Cat: 7498 . COSPAR: 1974-085B. Apogee: 531 km (329 mi). Perigee: 521 km (323 mi). Inclination: 96.00 deg. Period: 95.10 min. Radar monitoring; may or may not have existed!!!..
1974 November 1 - .
14:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 692 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-11-13 . USAF Sat Cat: 7502 . COSPAR: 1974-087A. Apogee: 295 km (183 mi). Perigee: 197 km (122 mi). Inclination: 62.80 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule. Second successful test of SpK small film return capsule planned for Yantar. SpK capsule FEU-170 No. 4L successfully recovered..
1974 November 4 - .
10:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 693 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1974-11-16 . USAF Sat Cat: 7509 . COSPAR: 1974-088A. Apogee: 243 km (150 mi). Perigee: 219 km (136 mi). Inclination: 81.30 deg. Period: 89.10 min. Military topography satellite; returned film capsule; separated science capsule..
1974 November 5 - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2.
FAILURE: Cable carrying pitch rate gyro signal disconnected..
Failed Stage: G.
- FSW-0 - .
Payload: FSW-0 No. A. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: PRC.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Decay Date: 1974-11-05 .
1974 November 16 - .
11:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 694 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1974-11-29 . USAF Sat Cat: 7533 . COSPAR: 1974-090A. Apogee: 336 km (208 mi). Perigee: 172 km (106 mi). Inclination: 72.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1974 November 27 - .
11:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 696 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1974-12-09 . USAF Sat Cat: 7551 . COSPAR: 1974-095A. Apogee: 321 km (199 mi). Perigee: 205 km (127 mi). Inclination: 72.90 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1974 December 13 - .
13:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 697 - .
Payload: Yantar-2K s/n 2. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 12.00 days. Decay Date: 1974-12-25 . USAF Sat Cat: 7571 . COSPAR: 1974-098A. Apogee: 392 km (243 mi). Perigee: 174 km (108 mi). Inclination: 62.80 deg. Period: 90.20 min.
Yantar second generation reconnaissance spacecraft. After failure of the first Yantar-2K launch, a review board recommended modifications to the Soyuz U launch vehicle. This second Yantar still used the Sokol control system from the Zenit and lacked the SpK small film recovery capsules. As planned, after 12 days, the main descent capsule was successfully recovered with its film.
1974 December 18 - .
14:12 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 698 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-12-09 . USAF Sat Cat: 7576 . COSPAR: 1974-100A. Apogee: 552 km (342 mi). Perigee: 515 km (320 mi). Inclination: 74.00 deg. Period: 95.30 min. Replaced Cosmos 549. Possible ELINT satellite..
1974 December 24 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 699 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1977-10-16 . USAF Sat Cat: 7587 . COSPAR: 1974-103A. Apogee: 440 km (270 mi). Perigee: 428 km (265 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring; exploded 4/17/75..
1974 December 27 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 701 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-01-09 . USAF Sat Cat: 7596 . COSPAR: 1974-106A. Apogee: 319 km (198 mi). Perigee: 205 km (127 mi). Inclination: 71.40 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 January 17 - .
09:07 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 702 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-01-29 . USAF Sat Cat: 7606 . COSPAR: 1975-002A. Apogee: 313 km (194 mi). Perigee: 205 km (127 mi). Inclination: 71.30 deg. Period: 89.70 min. Area survey photo reconnaissance satellite; returned film capsule..
1975 January 23 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 704 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1975-02-06 . USAF Sat Cat: 7617 . COSPAR: 1975-005A. Apogee: 305 km (189 mi). Perigee: 205 km (127 mi). Inclination: 72.90 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 January 30 - .
15:02 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 706 - .
Payload: Oko #4. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 7625 . COSPAR: 1975-007A. Apogee: 35,365 km (21,974 mi). Perigee: 4,977 km (3,092 mi). Inclination: 67.80 deg. Period: 717.60 min. Covered Oko constellation planes 7/8 - 182 degree longitude of ascending node..
1975 February 5 - .
13:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 707 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-09-07 . USAF Sat Cat: 7637 . COSPAR: 1975-008A. Apogee: 548 km (340 mi). Perigee: 491 km (305 mi). Inclination: 74.00 deg. Period: 95.00 min. Investigation of the upper atmosphere and outer space. .
1975 February 12 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 709 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-02-25 . USAF Sat Cat: 7664 . COSPAR: 1975-013A. Apogee: 310 km (190 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 February 26 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 710 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1975-03-12 . USAF Sat Cat: 7675 . COSPAR: 1975-015A. Apogee: 335 km (208 mi). Perigee: 176 km (109 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 March 10 - .
04:41 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 34B.
- Jumpseat 4 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Jumpseat.
USAF Sat Cat: 7687 . COSPAR: 1975-017A. Apogee: 39,337 km (24,442 mi). Perigee: 295 km (183 mi). Inclination: 63.50 deg. Period: 702.00 min.
1975 March 12 - .
08:55 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 719 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-03-25 . USAF Sat Cat: 7691 . COSPAR: 1975-018A. Apogee: 307 km (190 mi). Perigee: 175 km (108 mi). Inclination: 65.00 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 March 21 - .
06:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 720 - .
Payload: Zenit-4MT Mod. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 11.00 days. Decay Date: 1975-04-01 . USAF Sat Cat: 7696 . COSPAR: 1975-019A. Apogee: 273 km (169 mi). Perigee: 212 km (131 mi). Inclination: 62.80 deg. Period: 89.30 min. Military topography satellite; returned film capsule..
1975 March 26 - .
08:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 721 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-04-07 . USAF Sat Cat: 7705 . COSPAR: 1975-020A. Apogee: 228 km (141 mi). Perigee: 208 km (129 mi). Inclination: 81.30 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1975 March 27 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 722 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-04-09 . USAF Sat Cat: 7709 . COSPAR: 1975-021A. Apogee: 337 km (209 mi). Perigee: 204 km (126 mi). Inclination: 71.40 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 April 2 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 723 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1975-07-15 . USAF Sat Cat: 7797 . COSPAR: 1975-024D. Apogee: 961 km (597 mi). Perigee: 899 km (558 mi). Inclination: 64.70 deg. Period: 103.60 min. Ocean surveillance; nuclear powered..
1975 April 7 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 724 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1975-08-07 . USAF Sat Cat: 7922 . COSPAR: 1975-025B. Apogee: 943 km (585 mi). Perigee: 852 km (529 mi). Inclination: 65.60 deg. Period: 102.90 min. Ocean surveillance; nuclear powered..
1975 April 16 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 727 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1975-04-28 . USAF Sat Cat: 7742 . COSPAR: 1975-030A. Apogee: 334 km (207 mi). Perigee: 172 km (106 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 April 18 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 728 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 11.00 days. Decay Date: 1975-04-29 . USAF Sat Cat: 7745 . COSPAR: 1975-031A. Apogee: 311 km (193 mi). Perigee: 209 km (129 mi). Inclination: 72.80 deg. Period: 89.70 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1975 April 18 - .
16:48 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 4883 - .
Payload: KH-8 no. 44 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1975-06-05 . USAF Sat Cat: 7747 . COSPAR: 1975-032A. Apogee: 398 km (247 mi). Perigee: 133 km (82 mi). Inclination: 110.50 deg. Period: 89.80 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1975 April 24 - .
08:05 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 730 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1975-05-06 . USAF Sat Cat: 7770 . COSPAR: 1975-035A. Apogee: 234 km (145 mi). Perigee: 210 km (130 mi). Inclination: 81.30 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 May 21 - .
06:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 731 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-06-02 . USAF Sat Cat: 7810 . COSPAR: 1975-041A. Apogee: 296 km (183 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1975 May 28 - .
07:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 740 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-06-10 . USAF Sat Cat: 7821 . COSPAR: 1975-046A. Apogee: 327 km (203 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 May 30 - .
06:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
1975 June 3 - .
13:21 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 742 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1975-06-15 . USAF Sat Cat: 7900 . COSPAR: 1975-048A. Apogee: 355 km (220 mi). Perigee: 178 km (110 mi). Inclination: 62.90 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 June 8 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 10 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1975-11-05 . USAF Sat Cat: 7918 . COSPAR: 1975-051A. Apogee: 272 km (169 mi). Perigee: 157 km (97 mi). Inclination: 96.30 deg. Period: 88.70 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1975 June 12 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 743 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-06-25 . USAF Sat Cat: 7925 . COSPAR: 1975-053A. Apogee: 331 km (205 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 June 18 - .
09:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- Canyon 6 - .
Payload: Canyon Improved / OPS 4966. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Canyon.
USAF Sat Cat: 7963 . COSPAR: 1975-055A. Apogee: 40,800 km (25,300 mi). Perigee: 30,200 km (18,700 mi). Inclination: 9.00 deg. Period: 1,422.00 min.
1975 June 20 - .
06:54 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 744 - .
Payload: Tselina-D no. 7. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1991-10-12 . USAF Sat Cat: 7968 . COSPAR: 1975-056A. Apogee: 380 km (230 mi). Perigee: 367 km (228 mi). Inclination: 81.20 deg. Period: 92.00 min.
1975 June 25 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 746 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-07-08 . USAF Sat Cat: 7985 . COSPAR: 1975-059A. Apogee: 325 km (201 mi). Perigee: 180 km (110 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 June 27 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 747 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-07-09 . USAF Sat Cat: 7990 . COSPAR: 1975-060A. Apogee: 280 km (170 mi). Perigee: 204 km (126 mi). Inclination: 62.80 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1975 July 3 - .
13:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 748 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-07-16 . USAF Sat Cat: 8006 . COSPAR: 1975-061A. Apogee: 303 km (188 mi). Perigee: 190 km (110 mi). Inclination: 62.80 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 July 4 - .
00:56 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 749 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-09-26 . USAF Sat Cat: 8009 . COSPAR: 1975-062A. Apogee: 550 km (340 mi). Perigee: 509 km (316 mi). Inclination: 74.00 deg. Period: 95.30 min. Replaced Cosmos 610. Possible ELINT satellite..
1975 July 23 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 751 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-08-04 . USAF Sat Cat: 8040 . COSPAR: 1975-068A. Apogee: 313 km (194 mi). Perigee: 197 km (122 mi). Inclination: 62.80 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1975 July 24 - .
19:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 752 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1981-02-28 . USAF Sat Cat: 8043 . COSPAR: 1975-069A. Apogee: 514 km (319 mi). Perigee: 481 km (298 mi). Inclination: 65.80 deg. Period: 94.50 min. Radar calibration mission..
1975 July 26 - .
13:28 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Feng Bao 1.
- JSSW 3 - .
Payload: JSSW 3. Mass: 1,107 kg (2,440 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: JSSW.
Decay Date: 1975-09-14 . USAF Sat Cat: 8053 . COSPAR: 1975-070A. Apogee: 455 km (282 mi). Perigee: 190 km (110 mi). Inclination: 69.00 deg. Period: 90.90 min. Photo surveillance; radio transmission. .
1975 July 31 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 753 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-08-13 . USAF Sat Cat: 8059 . COSPAR: 1975-071A. Apogee: 330 km (200 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 August 13 - .
07:21 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 754 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-08-26 . USAF Sat Cat: 8069 . COSPAR: 1975-073A. Apogee: 326 km (202 mi). Perigee: 204 km (126 mi). Inclination: 71.40 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 August 22 - .
02:11 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 756 - .
Payload: Tselina-D no. 8. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1992-11-05 . USAF Sat Cat: 8127 . COSPAR: 1975-076A. Apogee: 403 km (250 mi). Perigee: 394 km (244 mi). Inclination: 81.20 deg. Period: 92.50 min.
1975 August 27 - .
14:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 757 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-09-09 . USAF Sat Cat: 8147 . COSPAR: 1975-078A. Apogee: 316 km (196 mi). Perigee: 182 km (113 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 September 5 - .
14:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 758 - .
Payload: Yantar-2K s/n 3. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 1.00 days. Decay Date: 1975-09-25 . USAF Sat Cat: 8191 . COSPAR: 1975-080A. Apogee: 326 km (202 mi). Perigee: 174 km (108 mi). Inclination: 67.10 deg. Period: 89.50 min.
Third Yantar-2K second generation reconnaissance flight, the first with the new Kondor attitude control system. This system experienced problems and failed on the second day of flight. The spacecraft's destruct package was activated by ground command and the spacecraft was destroyed on 6 September 1975 in its second day of flight.
1975 September 12 - .
05:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 759 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 11.00 days. Decay Date: 1975-09-23 . USAF Sat Cat: 8275 . COSPAR: 1975-084A. Apogee: 276 km (171 mi). Perigee: 231 km (143 mi). Inclination: 62.80 deg. Period: 89.60 min. Military topography satellite; returned film capsule; separated science capsule..
1975 September 16 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 760 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1975-09-30 . USAF Sat Cat: 8281 . COSPAR: 1975-085A. Apogee: 335 km (208 mi). Perigee: 174 km (108 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 September 23 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 769 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-10-05 . USAF Sat Cat: 8322 . COSPAR: 1975-088A. Apogee: 307 km (190 mi). Perigee: 203 km (126 mi). Inclination: 72.80 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule. Third successful test of SpK small film return capsule planned for Yantar. SpK capsule FEU-170-13 No. 5L successfully recovered..
1975 September 25 - .
09:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 771 - .
Payload: Zenit-4MKT no. 1. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1975-10-08 . USAF Sat Cat: 8327 . COSPAR: 1975-090A. Apogee: 219 km (136 mi). Perigee: 203 km (126 mi). Inclination: 81.30 deg. Period: 88.70 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1975 October 1 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 774 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1975-10-15 . USAF Sat Cat: 8345 . COSPAR: 1975-095A. Apogee: 315 km (195 mi). Perigee: 204 km (126 mi). Inclination: 71.40 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 October 8 - .
00:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/23.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM.
- Cosmos 775 - .
Payload: SPRN No. 1. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Prognoz SPRN.
Completed Operations Date: 1975-10-08 . USAF Sat Cat: 8357 . COSPAR: 1975-097A. Apogee: 35,853 km (22,277 mi). Perigee: 35,749 km (22,213 mi). Inclination: 14.90 deg. Period: 1,436.80 min.
First launch of a prototype for a new geosynchronous ballistic missile early warning satellite. Exploded in orbit. The next launch did not come until nine years later, so this may have been a version of the Oko elliptical orbit early warning satellite. As of 29 August 2001 located at 113.71 deg E drifting at 0.044 deg W per day. As of 2007 Mar 10 located at 54.82E drifting at 0.255W degrees per day.
1975 October 9 - .
19:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 5499 - .
Payload: KH-8 no. 45 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1975-11-30 . USAF Sat Cat: 8360 . COSPAR: 1975-098A. Apogee: 274 km (170 mi). Perigee: 145 km (90 mi). Inclination: 96.40 deg. Period: 88.60 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1975 October 17 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 776 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-10-29 . USAF Sat Cat: 8369 . COSPAR: 1975-101A. Apogee: 288 km (178 mi). Perigee: 200 km (120 mi). Inclination: 62.80 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1975 October 29 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 777 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1976-06-03 . USAF Sat Cat: 8416 . COSPAR: 1975-102A. Apogee: 442 km (274 mi). Perigee: 425 km (264 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring; exploded 1/76..
1975 November 4 - .
15:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 779 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1975-11-18 . USAF Sat Cat: 8420 . COSPAR: 1975-104A. Apogee: 341 km (211 mi). Perigee: 182 km (113 mi). Inclination: 62.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1975 November 21 - .
09:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 780 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-12-03 . USAF Sat Cat: 8442 . COSPAR: 1975-108A. Apogee: 278 km (172 mi). Perigee: 201 km (124 mi). Inclination: 65.00 deg. Period: 89.30 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1975 November 21 - .
17:11 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 781 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-11-26 . USAF Sat Cat: 8444 . COSPAR: 1975-109A. Apogee: 563 km (349 mi). Perigee: 499 km (310 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 698. Investigation of the upper atmosphere and outer space. .
1975 November 26 - .
03:29 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 1 - .
Payload: FSW-0 No. 01. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 2.00 days. Decay Date: 1975-12-29 . USAF Sat Cat: 8452 . COSPAR: 1975-111A. Apogee: 483 km (300 mi). Perigee: 183 km (113 mi). Inclination: 63.00 deg. Period: 91.10 min.
First orbital test of Chinese recoverable photo surveillance satellite. The spacecraft was brought down early, after three days in orbit, due to problems with the attitude control system cold gas supply. Along the skirt of the return capsule some wires and instruments were burnt during re-entry and capsule impacted far from its planned landing point. However usable film was obtained from the capsule. The Chinese Academy of Space Technology organised a team to determine the cause, and improvements were made in the next spacecraft of the model. Additional Details: here....
1975 December 3 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 784 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1975-12-15 . USAF Sat Cat: 8463 . COSPAR: 1975-113A. Apogee: 231 km (143 mi). Perigee: 215 km (133 mi). Inclination: 81.30 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1975 December 4 - .
20:38 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 11 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1976-04-01 . USAF Sat Cat: 8467 . COSPAR: 1975-114A. Apogee: 234 km (145 mi). Perigee: 157 km (97 mi). Inclination: 96.30 deg. Period: 88.40 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- KH 9-11 Subsatellite - .
Payload: SSF 9 / OPS 5547. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1978-05-01 . USAF Sat Cat: 8468 . COSPAR: 1975-114B. Apogee: 1,558 km (968 mi). Perigee: 236 km (146 mi). Inclination: 96.30 deg. Period: 103.00 min. Not identified as a subsatellite ferret by McDowell..
1975 December 12 - .
12:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 785 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1976-02-05 . USAF Sat Cat: 8480 . COSPAR: 1975-116C. Apogee: 1,004 km (623 mi). Perigee: 907 km (563 mi). Inclination: 65.10 deg. Period: 104.20 min. Ocean surveillance; nuclear powered; failed immediately after reaching orbit..
1975 December 14 - .
05:15 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- IMEWS 5 - .
Payload: DSP Phase 2 s/n 7 / OPS 3165. Mass: 1,040 kg (2,290 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1987-12-31 . USAF Sat Cat: 8482 . COSPAR: 1975-118A. Apogee: 35,785 km (22,235 mi). Perigee: 35,671 km (22,164 mi). Inclination: 3.00 deg. Period: 1,436.00 min. Second generation geosynchronous ballistic missile launch detection satellite, remained in service for over twelve years. As of 1982 Dec 16 located at 34.61E drifting at 0.823E degrees per day..
1975 December 16 - .
09:19 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Feng Bao 1.
- JSSW 4 - .
Payload: JSSW 4. Mass: 1,110 kg (2,440 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: JSSW.
Decay Date: 1976-01-27 . USAF Sat Cat: 8488 . COSPAR: 1975-119A. Apogee: 387 km (240 mi). Perigee: 186 km (115 mi). Inclination: 69.00 deg. Period: 90.30 min. Photo surveillance; radio transmission. .
1975 December 16 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 786 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1975-12-29 . USAF Sat Cat: 8489 . COSPAR: 1975-120A. Apogee: 325 km (201 mi). Perigee: 184 km (114 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 January 6 - .
04:52 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 787 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-12-12 . USAF Sat Cat: 8530 . COSPAR: 1976-001A. Apogee: 565 km (351 mi). Perigee: 509 km (316 mi). Inclination: 74.00 deg. Period: 95.30 min. Replaced Cosmos 655. Possible ELINT satellite..
1976 January 7 - .
15:35 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 788 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-01-20 . USAF Sat Cat: 8551 . COSPAR: 1976-002A. Apogee: 321 km (199 mi). Perigee: 183 km (113 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 January 22 - .
22:26 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 790 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-11-12 . USAF Sat Cat: 8604 . COSPAR: 1976-007A. Apogee: 548 km (340 mi). Perigee: 511 km (317 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 631. Possible ELINT satellite..
1976 January 29 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 799 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1976-02-10 . USAF Sat Cat: 8616 . COSPAR: 1976-009A. Apogee: 306 km (190 mi). Perigee: 205 km (127 mi). Inclination: 71.40 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1976 February 11 - .
08:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 802 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1976-02-25 . USAF Sat Cat: 8681 . COSPAR: 1976-013A. Apogee: 334 km (207 mi). Perigee: 172 km (106 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 February 20 - .
14:01 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 805 - .
Payload: Yantar-2K s/n 4. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 20.00 days. Decay Date: 1976-03-11 . USAF Sat Cat: 8699 . COSPAR: 1976-018A. Apogee: 351 km (218 mi). Perigee: 171 km (106 mi). Inclination: 67.10 deg. Period: 89.70 min.
Fourth Yantar-2K second generation reconnaissance flight and the first with two SpK small film recovery capsules. First flight of the completely equipped satellite. The main reentry capsule and its film cargo were returned successfully. Both SpK capsules successfully separated from the Yantar in the course of the flight, but neither was recovered. The parachutes of the first did not deploy and the capsule crashed into the ground. The solid motor of the second capsule did not fire as programmed and the capsule did not deorbit at the expected time.
1976 March 10 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 806 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-03-23 . USAF Sat Cat: 8737 . COSPAR: 1976-020A. Apogee: 328 km (203 mi). Perigee: 188 km (116 mi). Inclination: 71.40 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 March 12 - .
13:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 807 - .
Mass: 400 kg (880 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 8744 . COSPAR: 1976-022A. Apogee: 1,568 km (974 mi). Perigee: 384 km (238 mi). Inclination: 82.90 deg. Period: 104.60 min. Radar calibration mission..
1976 March 16 - .
17:22 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 808 - .
Payload: Tselina-D no. 9. Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1993-11-20 . USAF Sat Cat: 8754 . COSPAR: 1976-024A. Apogee: 370 km (220 mi). Perigee: 363 km (225 mi). Inclination: 81.20 deg. Period: 91.90 min.
1976 March 18 - .
09:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 809 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1976-03-30 . USAF Sat Cat: 8758 . COSPAR: 1976-025A. Apogee: 300 km (180 mi). Perigee: 205 km (127 mi). Inclination: 65.00 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule..
1976 March 22 - .
18:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 7600 - .
Payload: KH-8 no. 46 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1976-05-18 . USAF Sat Cat: 8770 . COSPAR: 1976-027A. Apogee: 347 km (215 mi). Perigee: 125 km (77 mi). Inclination: 96.40 deg. Period: 89.30 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1976 March 26 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 810 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-04-08 . USAF Sat Cat: 8772 . COSPAR: 1976-028A. Apogee: 338 km (210 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 March 31 - .
12:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511M.
- Cosmos 811 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1976-04-12 . USAF Sat Cat: 8781 . COSPAR: 1976-030A. Apogee: 338 km (210 mi). Perigee: 206 km (128 mi). Inclination: 72.90 deg. Period: 90.00 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources; deployed capsule..
1976 April 6 - .
04:14 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 812 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-10-30 . USAF Sat Cat: 8794 . COSPAR: 1976-031A. Apogee: 548 km (340 mi). Perigee: 508 km (315 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 544. Possible ELINT satellite..
1976 April 9 - .
08:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 813 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1976-04-21 . USAF Sat Cat: 8801 . COSPAR: 1976-033A. Apogee: 236 km (146 mi). Perigee: 209 km (129 mi). Inclination: 81.30 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule..
1976 April 28 - .
09:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 815 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-05-11 . USAF Sat Cat: 8811 . COSPAR: 1976-036A. Apogee: 231 km (143 mi). Perigee: 218 km (135 mi). Inclination: 81.30 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 April 28 - .
13:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 816 - .
Mass: 950 kg (2,090 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1979-11-24 . USAF Sat Cat: 8812 . COSPAR: 1976-037A. Apogee: 566 km (351 mi). Perigee: 453 km (281 mi). Inclination: 65.90 deg. Period: 94.80 min. Released 24 Romb radar calibration subsatellites..
1976 April 30 - .
19:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas F/MSD.
- NOSS 1 (Whitecloud 1) - .
Payload: PARCAE 1 / OPS 6431. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 8818 . COSPAR: 1976-038A. Apogee: 1,128 km (700 mi). Perigee: 1,092 km (678 mi). Inclination: 63.50 deg. Period: 107.50 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- SSU 2 (NOSS 1) - .
Payload: NOSS-Subsat 1-2. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 8836 . COSPAR: 1976-038D. Apogee: 1,286 km (799 mi). Perigee: 931 km (578 mi). Inclination: 63.40 deg. Period: 107.40 min. Deployed from NOSS 1..
- SSU 3 (NOSS 1) - .
Payload: NOSS-Subsat 1-3. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 8884 . COSPAR: 1976-038J. Apogee: 1,324 km (822 mi). Perigee: 893 km (554 mi). Inclination: 63.40 deg. Period: 107.40 min. Deployed from NOSS 1..
- SSU 1 (NOSS 1) - .
Payload: NOSS-Subsat 1-1. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 8835 . COSPAR: 1976-038C. Apogee: 1,284 km (797 mi). Perigee: 932 km (579 mi). Inclination: 63.40 deg. Period: 107.40 min. Deployed from NOSS 1..
1976 May 5 - .
07:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 817 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-05-18 . USAF Sat Cat: 8823 . COSPAR: 1976-040A. Apogee: 324 km (201 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 May 20 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 819 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 11.00 days. Decay Date: 1976-06-01 . USAF Sat Cat: 8853 . COSPAR: 1976-045A. Apogee: 293 km (182 mi). Perigee: 207 km (128 mi). Inclination: 64.90 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1976 May 21 - .
07:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 820 - .
Payload: Zenit-4MKT no. 2. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 12.00 days. Decay Date: 1976-06-02 . USAF Sat Cat: 8856 . COSPAR: 1976-046A. Apogee: 217 km (134 mi). Perigee: 209 km (129 mi). Inclination: 81.40 deg. Period: 88.80 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1976 May 26 - .
09:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 821 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-06-08 . USAF Sat Cat: 8862 . COSPAR: 1976-048A. Apogee: 314 km (195 mi). Perigee: 204 km (126 mi). Inclination: 72.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 May 28 - .
15:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 822 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1978-08-08 . USAF Sat Cat: 8865 . COSPAR: 1976-049A. Apogee: 711 km (441 mi). Perigee: 280 km (170 mi). Inclination: 74.10 deg. Period: 94.50 min. Radar calibration mission..
1976 June 8 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 824 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-06-21 . USAF Sat Cat: 8877 . COSPAR: 1976-052A. Apogee: 325 km (201 mi). Perigee: 204 km (126 mi). Inclination: 71.40 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 June 16 - .
13:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 833 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-06-29 . USAF Sat Cat: 8898 . COSPAR: 1976-055A. Apogee: 316 km (196 mi). Perigee: 180 km (110 mi). Inclination: 62.80 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 June 24 - .
07:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 834 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1976-07-06 . USAF Sat Cat: 8914 . COSPAR: 1976-058A. Apogee: 237 km (147 mi). Perigee: 216 km (134 mi). Inclination: 81.40 deg. Period: 89.10 min. Area survey photo reconnaissance satellite; returned film capsule..
1976 June 26 - .
03:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- IMEWS 6 - .
Payload: DSP Phase 2 s/n 8 / OPS 2112. Mass: 1,040 kg (2,290 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1984-07-01 . USAF Sat Cat: 8916 . COSPAR: 1976-059A. Apogee: 35,860 km (22,280 mi). Perigee: 35,620 km (22,130 mi). Inclination: 0.50 deg. Period: 1,433.30 min.
Second generation geosynchronous ballistic missile launch detection satellite, remained in service for over eight years. Positioned over the Atlantic Ocean from 1976 to 1981: at 35 deg W in 1976-1977; at 65 deg W in 1977-1979; and 35 deg W in 1979-1980; and 65 deg W in 1980-1981. Then moved over the Pacific Ocean at 125 deg W, then 140 deg W in 1981-1982; then over the Indian Ocean at 75 deg E in 1982-1984.
1976 June 29 - .
07:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 835 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-07-12 . USAF Sat Cat: 8922 . COSPAR: 1976-060A. Apogee: 317 km (196 mi). Perigee: 174 km (108 mi). Inclination: 65.00 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 July 2 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 838 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1977-08-23 . USAF Sat Cat: 8932 . COSPAR: 1976-063A. Apogee: 440 km (270 mi). Perigee: 428 km (265 mi). Inclination: 65.10 deg. Period: 93.30 min. Ocean surveillance. Exploded June/July '76..
1976 July 8 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 12 - .
Mass: 13,000 kg (28,000 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1976-12-13 . USAF Sat Cat: 9006 . COSPAR: 1976-065A. Apogee: 242 km (150 mi). Perigee: 159 km (98 mi). Inclination: 97.00 deg. Period: 88.50 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 5366 - .
Payload: SSF-D No. 1. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 9008 . COSPAR: 1976-065C. Apogee: 632 km (392 mi). Perigee: 628 km (390 mi). Inclination: 96.40 deg. Period: 97.30 min. Radar monitoring..
1976 July 14 - .
09:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 840 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1976-07-26 . USAF Sat Cat: 9019 . COSPAR: 1976-068A. Apogee: 319 km (198 mi). Perigee: 203 km (126 mi). Inclination: 72.90 deg. Period: 89.70 min. Area survey photo reconnaissance satellite; returned film capsule..
1976 July 22 - .
15:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 844 - .
Payload: Yantar-2K s/n 5. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 3.00 days. Decay Date: 1976-08-30 . USAF Sat Cat: 9046 . COSPAR: 1976-072A. Apogee: 353 km (219 mi). Perigee: 172 km (106 mi). Inclination: 67.20 deg. Period: 89.80 min. Fifth Yantar second generation reconnaissance test flight. One of the solar panels would not unfold. Ground control activiated the destruct package and the spacecraft was destroyed on 25 July..
1976 July 27 - .
05:21 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
Launch Pad: LC132/2?.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 845 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-11-15 . USAF Sat Cat: 9053 . COSPAR: 1976-075A. Apogee: 597 km (370 mi). Perigee: 487 km (302 mi). Inclination: 74.00 deg. Period: 95.40 min. Replaced Cosmos 812. Investigation of the upper atmosphere and outer space. .
1976 August 4 - .
13:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 847 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-08-17 . USAF Sat Cat: 9214 . COSPAR: 1976-079A. Apogee: 321 km (199 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 August 12 - .
13:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 848 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1976-08-25 . USAF Sat Cat: 9280 . COSPAR: 1976-082A. Apogee: 303 km (188 mi). Perigee: 206 km (128 mi). Inclination: 62.80 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1976 August 27 - .
14:35 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 851 - .
Payload: Tselina-D no. 10. Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1989-08-05 . USAF Sat Cat: 9389 . COSPAR: 1976-085A. Apogee: 313 km (194 mi). Perigee: 300 km (180 mi). Inclination: 81.20 deg. Period: 90.70 min.
1976 August 28 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 852 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-09-10 . USAF Sat Cat: 9391 . COSPAR: 1976-086A. Apogee: 332 km (206 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 August 30 - .
11:53 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Feng Bao 1.
- JSSW 5 - .
Payload: JSSW 5. Mass: 1,108 kg (2,442 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: JSSW.
Decay Date: 1978-11-25 . USAF Sat Cat: 9394 . COSPAR: 1976-087A. Apogee: 2,145 km (1,332 mi). Perigee: 195 km (121 mi). Inclination: 69.20 deg. Period: 108.80 min.
1976 September 3 - .
09:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 854 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-09-16 . USAF Sat Cat: 9405 . COSPAR: 1976-090A. Apogee: 308 km (191 mi). Perigee: 167 km (103 mi). Inclination: 81.40 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 September 15 - .
18:50 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 8533 - .
Payload: KH-8 no. 47 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1976-11-05 . USAF Sat Cat: 9426 . COSPAR: 1976-094A. Apogee: 337 km (209 mi). Perigee: 142 km (88 mi). Inclination: 96.40 deg. Period: 89.20 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1976 September 21 - .
11:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 855 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1976-10-03 . USAF Sat Cat: 9433 . COSPAR: 1976-095A. Apogee: 321 km (199 mi). Perigee: 221 km (137 mi). Inclination: 72.90 deg. Period: 89.90 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources; deployed capsule..
1976 September 22 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 856 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1976-10-05 . USAF Sat Cat: 9435 . COSPAR: 1976-096A. Apogee: 300 km (180 mi). Perigee: 203 km (126 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1976 September 24 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 857 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1976-10-07 . USAF Sat Cat: 9439 . COSPAR: 1976-097A. Apogee: 331 km (205 mi). Perigee: 177 km (109 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 October 4 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
FAILURE: Launch vehicle destroyed at T+95 seconds..
Failed Stage: 0.
- Zenit-4MKT no. 3 - .
Payload: Zenit-4MKT no. 3. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: RVSN.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1976 October 10 - .
09:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 859 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 11.00 days. Decay Date: 1976-10-21 . USAF Sat Cat: 9471 . COSPAR: 1976-099A. Apogee: 337 km (209 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable; also performed earth resources tasks..
1976 October 17 - .
18:06 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 860 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1976-12-29 . USAF Sat Cat: 9531 . COSPAR: 1976-103B. Apogee: 995 km (618 mi). Perigee: 923 km (573 mi). Inclination: 64.70 deg. Period: 104.30 min. Ocean surveillance; nuclear powered..
1976 October 21 - .
16:53 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 861 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1977-02-04 . USAF Sat Cat: 9631 . COSPAR: 1976-104C. Apogee: 987 km (613 mi). Perigee: 928 km (576 mi). Inclination: 64.90 deg. Period: 104.20 min. Ocean surveillance; nuclear powered..
1976 October 22 - .
09:12 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 862 - .
Payload: Oko #5. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 9495 . COSPAR: 1976-105A. Apogee: 36,759 km (22,840 mi). Perigee: 3,620 km (2,240 mi). Inclination: 68.30 deg. Period: 718.30 min. Covered Oko constellation plane 5 - 86 degree longitude of ascending node..
1976 October 25 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 863 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 11.00 days. Decay Date: 1976-11-05 . USAF Sat Cat: 9499 . COSPAR: 1976-106A. Apogee: 348 km (216 mi). Perigee: 178 km (110 mi). Inclination: 62.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 November 1 - .
11:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 865 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1976-11-13 . USAF Sat Cat: 9515 . COSPAR: 1976-109A. Apogee: 326 km (202 mi). Perigee: 203 km (126 mi). Inclination: 72.90 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1976 November 11 - .
10:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 866 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1976-11-23 . USAF Sat Cat: 9532 . COSPAR: 1976-110A. Apogee: 287 km (178 mi). Perigee: 180 km (110 mi). Inclination: 65.00 deg. Period: 89.20 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 November 23 - .
16:27 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 867 - .
Payload: Zenit-6 no. 1. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 12.00 days. Decay Date: 1976-12-06 . USAF Sat Cat: 9552 . COSPAR: 1976-111A. Apogee: 402 km (249 mi). Perigee: 250 km (150 mi). Inclination: 62.80 deg. Period: 91.10 min. Photo surveillance; returned film capsule..
1976 November 26 - .
14:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 868 - .
Mass: 1,400 kg (3,000 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1978-07-08 . USAF Sat Cat: 9561 . COSPAR: 1976-113A. Apogee: 444 km (275 mi). Perigee: 422 km (262 mi). Inclination: 65.00 deg. Period: 93.30 min.
1976 December - .
- Military-Industrial Commission approves Tselina-2 development plan. - .
Nation: Russia.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
After a long review process the VPK issued the project plan for development of the system in December 1976. It would now use the new Zenit launch vehicle..
1976 December 2 - .
00:17 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 870 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-12-20 . USAF Sat Cat: 9573 . COSPAR: 1976-115A. Apogee: 563 km (349 mi). Perigee: 504 km (313 mi). Inclination: 74.00 deg. Period: 95.30 min. Replaced Cosmos 500. Possible ELINT satellite..
1976 December 7 - .
04:38 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 2 - .
Payload: FSW-0 No. 02. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 2.00 days. Decay Date: 1977-01-02 . USAF Sat Cat: 9587 . COSPAR: 1976-117A. Apogee: 489 km (303 mi). Perigee: 172 km (106 mi). Inclination: 59.40 deg. Period: 91.10 min. Photo surveillance; film capsule recovered 9 December. First completely successful test of the FSW spy satellite. Many improvements in comparison to the first FSW orbited..
1976 December 9 - .
10:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 879 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1976-12-22 . USAF Sat Cat: 9599 . COSPAR: 1976-119A. Apogee: 225 km (139 mi). Perigee: 213 km (132 mi). Inclination: 81.40 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule..
1976 December 10 - .
- Tselina-D accepted for military service. - .
Nation: Russia.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On adoption of the Tselina-D into armaments' was issued..
1976 December 17 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 884 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 12.00 days. Decay Date: 1976-12-29 . USAF Sat Cat: 9614 . COSPAR: 1976-123A. Apogee: 345 km (214 mi). Perigee: 169 km (105 mi). Inclination: 65.10 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1976 December 17 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 885 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1979-10-14 . USAF Sat Cat: 9615 . COSPAR: 1976-124A. Apogee: 520 km (320 mi). Perigee: 433 km (269 mi). Inclination: 65.90 deg. Period: 94.10 min. Released 18 Romb radar calibration subsatellites..
1976 December 19 - .
18:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-11 no. 1 - .
Payload: KH-11 no. 1 / OPS 5705. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
Decay Date: 1979-01-28 . USAF Sat Cat: 9627 . COSPAR: 1976-125A. Apogee: 531 km (329 mi). Perigee: 246 km (152 mi). Inclination: 96.90 deg. Period: 92.30 min. KH-11 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A)..
1977 January 6 - .
09:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 888 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1977-01-19 . USAF Sat Cat: 9658 . COSPAR: 1977-001A. Apogee: 325 km (201 mi). Perigee: 170 km (100 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 January 20 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 889 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1977-02-01 . USAF Sat Cat: 9735 . COSPAR: 1977-003A. Apogee: 329 km (204 mi). Perigee: 202 km (125 mi). Inclination: 71.40 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1977 February 2 - .
12:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 891 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1981-02-04 . USAF Sat Cat: 9801 . COSPAR: 1977-006A. Apogee: 516 km (320 mi). Perigee: 472 km (293 mi). Inclination: 65.80 deg. Period: 94.50 min. Radar calibration mission..
1977 February 6 - .
06:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- IMEWS 7 - .
Payload: DSP Phase 2 s/n 9 / OPS 3151. Mass: 1,040 kg (2,290 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1984-01-01 . USAF Sat Cat: 9803 . COSPAR: 1977-007A. Apogee: 35,860 km (22,280 mi). Perigee: 35,620 km (22,130 mi). Inclination: 0.50 deg. Period: 1,433.30 min. Second generation geosynchronous ballistic missile launch detection satellite, remained in service for nearly seven years. Positioned in geosynchronous orbit over the Pacific Ocean at 135 deg W in 1977-1979; over the Indian Ocean 70 deg E in 1979-1984..
1977 February 9 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 892 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1977-02-22 . USAF Sat Cat: 9812 . COSPAR: 1977-009A. Apogee: 427 km (265 mi). Perigee: 159 km (98 mi). Inclination: 72.90 deg. Period: 90.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 February 22 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
FAILURE: Failure.
Failed Stage: U.
- Zenit-4MK - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Decay Date: 1977-03-30 . High resolution photo reconnaissance mission..
1977 February 26 - .
21:18 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 895 - .
Payload: Tselina-D no. 11. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1992-03-22 . USAF Sat Cat: 9853 . COSPAR: 1977-015A. Apogee: 442 km (274 mi). Perigee: 433 km (269 mi). Inclination: 81.20 deg. Period: 93.30 min.
1977 March 3 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 896 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1977-03-16 . USAF Sat Cat: 9857 . COSPAR: 1977-016A. Apogee: 206 km (128 mi). Perigee: 202 km (125 mi). Inclination: 72.90 deg. Period: 88.60 min. Photo surveillance; returned film capsule; maneuverable..
1977 March 10 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 897 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1977-03-23 . USAF Sat Cat: 9860 . COSPAR: 1977-017A. Apogee: 340 km (210 mi). Perigee: 171 km (106 mi). Inclination: 72.90 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 March 13 - .
18:41 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 4915 - .
Payload: KH-8 no. 48 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1977-05-26 . USAF Sat Cat: 9863 . COSPAR: 1977-019A. Apogee: 329 km (204 mi). Perigee: 141 km (87 mi). Inclination: 96.40 deg. Period: 89.10 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1977 March 17 - .
08:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 898 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1977-03-30 . USAF Sat Cat: 9871 . COSPAR: 1977-020A. Apogee: 230 km (140 mi). Perigee: 216 km (134 mi). Inclination: 81.40 deg. Period: 89.00 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1977 March 24 - .
22:11 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 899 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-10-19 . USAF Sat Cat: 9883 . COSPAR: 1977-022A. Apogee: 547 km (339 mi). Perigee: 503 km (312 mi). Inclination: 74.10 deg. Period: 95.20 min. Replaced Cosmos 437. Possible ELINT satellite..
1977 April 7 - .
08:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 902 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1977-04-20 . USAF Sat Cat: 9908 . COSPAR: 1977-026A. Apogee: 279 km (173 mi). Perigee: 168 km (104 mi). Inclination: 81.40 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 April 11 - .
01:38 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 903 - .
Payload: Oko #6. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2014-08-04 . USAF Sat Cat: 9911 . COSPAR: 1977-027A. Apogee: 35,796 km (22,242 mi). Perigee: 4,559 km (2,832 mi). Inclination: 67.40 deg. Period: 717.80 min. Covered Oko constellation plane 7 - 163 degree longitude of ascending node..
1977 April 20 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 904 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 14.00 days. Decay Date: 1977-05-04 . USAF Sat Cat: 9930 . COSPAR: 1977-028A. Apogee: 328 km (203 mi). Perigee: 203 km (126 mi). Inclination: 71.40 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1977 April 26 - .
14:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 905 - .
Payload: Yantar-2K s/n 6. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1977-05-26 . USAF Sat Cat: 9937 . COSPAR: 1977-030A. Apogee: 413 km (256 mi). Perigee: 170 km (100 mi). Inclination: 67.10 deg. Period: 90.30 min.
Sixth Yantar second generation reconnaissance test flight and first completely successful flight. Both small SpK film capsules successfully recovered during course of flight, as was the main OSA cabin with its camera, computer, and main film cannisters. First full duration Yantar flight.
1977 April 27 - .
03:30 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 906 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1980-03-23 . USAF Sat Cat: 9938 . COSPAR: 1977-031A. Apogee: 515 km (320 mi). Perigee: 464 km (288 mi). Inclination: 50.60 deg. Period: 94.40 min. Released 1 Romb radar calibration subsatellite. Possible partially failed spacecraft bus..
1977 May 5 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 907 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 11.00 days. Decay Date: 1977-05-16 . USAF Sat Cat: 9944 . COSPAR: 1977-033A. Apogee: 364 km (226 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 May 17 - .
10:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 908 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 14.00 days. Decay Date: 1977-05-31 . USAF Sat Cat: 10007 . COSPAR: 1977-035A. Apogee: 288 km (178 mi). Perigee: 174 km (108 mi). Inclination: 51.80 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 May 23 - .
18:13 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- Canyon 7 - .
Payload: Canyon Improved / OPS 9751. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Canyon.
USAF Sat Cat: 10016 . COSPAR: 1977-038A. Apogee: 35,855 km (22,279 mi). Perigee: 35,679 km (22,169 mi). Inclination: 0.20 deg. Period: 1,435.10 min.
1977 May 26 - .
07:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 912 - .
Payload: Zenit-4MKT no. 4. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1977-06-08 . USAF Sat Cat: 10021 . COSPAR: 1977-040A. Apogee: 225 km (139 mi). Perigee: 217 km (134 mi). Inclination: 81.30 deg. Period: 88.90 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1977 May 30 - .
22:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 913 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1979-12-29 . USAF Sat Cat: 10028 . COSPAR: 1977-042A. Apogee: 520 km (320 mi). Perigee: 474 km (294 mi). Inclination: 74.00 deg. Period: 94.50 min. Released 21 Romb radar calibration subsatellites..
1977 May 31 - .
07:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 914 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1977-06-13 . USAF Sat Cat: 10030 . COSPAR: 1977-043A. Apogee: 284 km (176 mi). Perigee: 202 km (125 mi). Inclination: 65.00 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1977 June 8 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 915 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1977-06-21 . USAF Sat Cat: 10038 . COSPAR: 1977-045A. Apogee: 289 km (179 mi). Perigee: 173 km (107 mi). Inclination: 62.80 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 June 10 - .
08:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 916 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 11.00 days. Decay Date: 1977-06-21 . USAF Sat Cat: 10040 . COSPAR: 1977-046A. Apogee: 304 km (188 mi). Perigee: 255 km (158 mi). Inclination: 62.70 deg. Period: 90.10 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources; deployed capsule..
1977 June 16 - .
01:58 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 917 - .
Payload: Oko #7. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 10059 . COSPAR: 1977-047A. Apogee: 36,143 km (22,458 mi). Perigee: 4,196 km (2,607 mi). Inclination: 67.60 deg. Period: 717.50 min. Covered Oko constellation plane 9 - 245 degree longitude of ascending node..
1977 June 22 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 920 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MK.
Duration: 13.00 days. Decay Date: 1977-07-05 . USAF Sat Cat: 10086 . COSPAR: 1977-052A. Apogee: 342 km (212 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 June 24 - .
10:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 921 - .
Payload: Tselina-D Mass model. Mass: 5,000 kg (11,000 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 10095 . COSPAR: 1977-055A. Apogee: 651 km (404 mi). Perigee: 587 km (364 mi). Inclination: 75.80 deg. Period: 97.10 min. Launch vehicle test. Dummy payload. Investigation of the upper atmosphere and outer space..
1977 June 27 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 13 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1977-12-23 . USAF Sat Cat: 10111 . COSPAR: 1977-056A. Apogee: 239 km (148 mi). Perigee: 155 km (96 mi). Inclination: 97.00 deg. Period: 88.50 min. KH-9 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1977 June 30 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 922 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1977-07-13 . USAF Sat Cat: 10115 . COSPAR: 1977-058A. Apogee: 283 km (175 mi). Perigee: 221 km (137 mi). Inclination: 62.80 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1977 July 4 - .
22:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 924 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1981-02-10 . USAF Sat Cat: 10129 . COSPAR: 1977-060A. Apogee: 552 km (342 mi). Perigee: 513 km (318 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 436. Possible ELINT satellite..
1977 July 7 - .
07:25 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 925 - .
Payload: Tselina-D no. 12. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1993-04-29 . USAF Sat Cat: 10134 . COSPAR: 1977-061A. Apogee: 275 km (170 mi). Perigee: 269 km (167 mi). Inclination: 81.20 deg. Period: 90.00 min.
1977 July 12 - .
09:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 927 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1977-07-25 . USAF Sat Cat: 10139 . COSPAR: 1977-063A. Apogee: 361 km (224 mi). Perigee: 153 km (95 mi). Inclination: 72.90 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 July 19 - .
08:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 930 - .
Mass: 2,750 kg (6,060 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1980-05-12 . USAF Sat Cat: 10149 . COSPAR: 1977-067A. Apogee: 515 km (320 mi). Perigee: 482 km (299 mi). Inclination: 74.00 deg. Period: 94.60 min. Radar calibration mission..
1977 July 20 - .
04:44 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 931 - .
Payload: Oko #8. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 10150 . COSPAR: 1977-068A. Apogee: 36,549 km (22,710 mi). Perigee: 3,770 km (2,340 mi). Inclination: 66.50 deg. Period: 717.10 min. Replaced Cosmos 665. Covered Oko constellation plane 2 - 323 degree longitude of ascending node..
1977 July 20 - .
07:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 932 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1977-08-02 . USAF Sat Cat: 10153 . COSPAR: 1977-069A. Apogee: 358 km (222 mi). Perigee: 150 km (90 mi). Inclination: 65.00 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 July 22 - .
10:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 933 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1978-11-01 . USAF Sat Cat: 10157 . COSPAR: 1977-070A. Apogee: 431 km (267 mi). Perigee: 369 km (229 mi). Inclination: 65.80 deg. Period: 92.50 min. Radar calibration mission..
1977 July 27 - .
18:07 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 934 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1977-08-09 . USAF Sat Cat: 10164 . COSPAR: 1977-072A. Apogee: 255 km (158 mi). Perigee: 231 km (143 mi). Inclination: 62.80 deg. Period: 89.40 min. Photo surveillance; returned film capsule; maneuverable..
1977 July 29 - .
08:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 935 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1977-08-11 . USAF Sat Cat: 10168 . COSPAR: 1977-073A. Apogee: 251 km (155 mi). Perigee: 217 km (134 mi). Inclination: 81.30 deg. Period: 89.20 min. Area survey photo reconnaissance satellite; returned film capsule..
1977 August 10 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
FAILURE: Failure.
Failed Stage: U.
- Zenit-4MKM - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Decay Date: 1977-08-30 . High resolution photo reconnaissance mission..
1977 August 24 - .
07:07 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 937 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1978-10-19 . USAF Sat Cat: 10278 . COSPAR: 1977-077A. Apogee: 444 km (275 mi). Perigee: 424 km (263 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring..
1977 August 24 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 938 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1977-09-06 . USAF Sat Cat: 10281 . COSPAR: 1977-078A. Apogee: 340 km (210 mi). Perigee: 181 km (112 mi). Inclination: 62.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 August 27 - .
10:09 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 947 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1977-09-09 . USAF Sat Cat: 10299 . COSPAR: 1977-081A. Apogee: 321 km (199 mi). Perigee: 203 km (126 mi). Inclination: 72.90 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1977 September 2 - .
09:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 948 - .
Payload: Zenit-4MKT no. 5. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1977-09-15 . USAF Sat Cat: 10319 . COSPAR: 1977-083A. Apogee: 235 km (146 mi). Perigee: 217 km (134 mi). Inclination: 81.40 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1977 September 6 - .
17:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1977 September 13 - .
15:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 950 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 14.00 days. Decay Date: 1977-09-27 . USAF Sat Cat: 10351 . COSPAR: 1977-086A. Apogee: 282 km (175 mi). Perigee: 205 km (127 mi). Inclination: 62.80 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule..
1977 September 16 - .
14:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 952 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1977-11-07 . USAF Sat Cat: 10399 . COSPAR: 1977-088B. Apogee: 990 km (610 mi). Perigee: 911 km (566 mi). Inclination: 64.90 deg. Period: 104.10 min. Ocean surveillance; nuclear powered..
1977 September 16 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 953 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1977-09-29 . USAF Sat Cat: 10359 . COSPAR: 1977-089A. Apogee: 330 km (200 mi). Perigee: 180 km (110 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 September 18 - .
13:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 954 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1978-01-24 . USAF Sat Cat: 10361 . COSPAR: 1977-090A. Apogee: 265 km (164 mi). Perigee: 251 km (155 mi). Inclination: 65.00 deg. Period: 89.70 min. Ocean surveillance; nuclear powered; re-entered over Canada, spreading radioactive debris..
1977 September 20 - .
01:01 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 955 - .
Payload: Tselina-D no. 13. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2000-09-07 . USAF Sat Cat: 10362 . COSPAR: 1977-091A. Apogee: 501 km (311 mi). Perigee: 493 km (306 mi). Inclination: 81.20 deg. Period: 94.60 min.
1977 September 23 - .
18:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 7471 - .
Payload: KH-8 no. 49 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1977-12-08 . USAF Sat Cat: 10374 . COSPAR: 1977-094A. Apogee: 335 km (208 mi). Perigee: 134 km (83 mi). Inclination: 96.50 deg. Period: 89.10 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1977 September 24 - .
10:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
FAILURE: Probable failure of launch vehicle stage to reach proper orbit..
Failed Stage: 3.
- Cosmos 956 - .
Payload: Tselina-D Mass model. Mass: 5,000 kg (11,000 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1982-06-27 . USAF Sat Cat: 10375 . COSPAR: 1977-095A. Apogee: 864 km (536 mi). Perigee: 355 km (220 mi). Inclination: 75.80 deg. Period: 96.80 min. Launch vehicle test. Dummy payload. Probable failure of launch vehicle stage to reach proper orbit. Investigation of the upper atmosphere and outer space..
1977 September 30 - .
09:46 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 957 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1977-10-13 . USAF Sat Cat: 10385 . COSPAR: 1977-098A. Apogee: 361 km (224 mi). Perigee: 171 km (106 mi). Inclination: 65.00 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule.
1977 October 11 - .
15:14 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 958 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1977-10-24 . USAF Sat Cat: 10403 . COSPAR: 1977-100A. Apogee: 351 km (218 mi). Perigee: 257 km (159 mi). Inclination: 62.80 deg. Period: 90.60 min. Photo surveillance; returned film capsule..
1977 October 25 - .
05:25 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132/1?.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 960 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-10-22 . USAF Sat Cat: 10430 . COSPAR: 1977-103A. Apogee: 546 km (339 mi). Perigee: 502 km (311 mi). Inclination: 74.00 deg. Period: 95.10 min. Replaced Cosmos 870. Possible ELINT satellite..
1977 December 4 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 964 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1977-12-17 . USAF Sat Cat: 10498 . COSPAR: 1977-110A. Apogee: 362 km (224 mi). Perigee: 171 km (106 mi). Inclination: 72.90 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 December 8 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 965 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1979-12-16 . USAF Sat Cat: 10501 . COSPAR: 1977-111A. Apogee: 516 km (320 mi). Perigee: 465 km (288 mi). Inclination: 74.00 deg. Period: 94.40 min. Released 24 Romb radar calibration subsatellites..
1977 December 8 - .
17:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas F/MSD.
- NOSS 2 - .
Payload: PARCAE 2 / OPS 8781. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 10502 . COSPAR: 1977-112A. Apogee: 1,169 km (726 mi). Perigee: 1,054 km (654 mi). Inclination: 63.40 deg. Period: 107.50 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- SS 2 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 10544 . COSPAR: 1977-112E. Apogee: 1,168 km (725 mi). Perigee: 1,055 km (655 mi). Inclination: 63.40 deg. Period: 107.50 min. Deployed from NOSS 2..
- SS 1 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 10529 . COSPAR: 1977-112D. Apogee: 1,169 km (726 mi). Perigee: 1,054 km (654 mi). Inclination: 63.40 deg. Period: 107.50 min. Deployed from NOSS 2..
- SS 3 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 10594 . COSPAR: 1977-112F. Apogee: 1,168 km (725 mi). Perigee: 1,055 km (655 mi). Inclination: 63.40 deg. Period: 107.50 min. Deployed from NOSS 2..
1977 December 11 - .
22:45 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- OPS 4258 - .
Payload: AFP-472 AQUACADE 3. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Rhyolite.
USAF Sat Cat: 10508 . COSPAR: 1977-114A. Apogee: 35,855 km (22,279 mi). Perigee: 35,679 km (22,169 mi). Inclination: 0.20 deg. Period: 1,435.10 min. Third launch of Rhyolite geostationary ELINT satellite. Code name changed to Aquacade after Rhyolite name came out in trial of spy Boyce..
1977 December 12 - .
09:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 966 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 12.00 days. Decay Date: 1977-12-24 . USAF Sat Cat: 10510 . COSPAR: 1977-115A. Apogee: 296 km (183 mi). Perigee: 204 km (126 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1977 December 20 - .
15:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 969 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 14.00 days. Decay Date: 1978-01-03 . USAF Sat Cat: 10527 . COSPAR: 1977-120A. Apogee: 317 km (196 mi). Perigee: 180 km (110 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1977 December 27 - .
08:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
FAILURE: Probable failure of launch vehicle stage to reach proper orbit..
Failed Stage: 3.
- Cosmos 972 - .
Payload: Tselina-D Mass model. Mass: 5,000 kg (11,000 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 10539 . COSPAR: 1977-123A. Apogee: 1,157 km (718 mi). Perigee: 712 km (442 mi). Inclination: 75.80 deg. Period: 103.70 min. Launch vehicle test. Dummy payload. Probable failure of launch vehicle stage to reach proper orbit. Investigation of the upper atmosphere and outer space..
1977 December 27 - .
09:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 973 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-01-09 . USAF Sat Cat: 10540 . COSPAR: 1977-124A. Apogee: 325 km (201 mi). Perigee: 203 km (126 mi). Inclination: 71.50 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1978 January 6 - .
15:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 974 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-01-19 . USAF Sat Cat: 10554 . COSPAR: 1978-001A. Apogee: 334 km (207 mi). Perigee: 178 km (110 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 January 10 - .
13:23 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 975 - .
Payload: Tselina-D no. 14. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2001-09-19 . USAF Sat Cat: 10561 . COSPAR: 1978-004A. Apogee: 522 km (324 mi). Perigee: 513 km (318 mi). Inclination: 81.20 deg. Period: 95.00 min.
1978 January 13 - .
15:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 984 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-01-26 . USAF Sat Cat: 10592 . COSPAR: 1978-006A. Apogee: 291 km (180 mi). Perigee: 206 km (128 mi). Inclination: 62.80 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 January 24 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 986 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 14.00 days. Decay Date: 1978-02-07 . USAF Sat Cat: 10607 . COSPAR: 1978-010A. Apogee: 318 km (197 mi). Perigee: 172 km (106 mi). Inclination: 65.00 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 January 26 - .
04:58 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 3 - .
Payload: FSW-0 No. 03. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 5.00 days. Decay Date: 1978-02-07 . USAF Sat Cat: 10611 . COSPAR: 1978-011A. Apogee: 507 km (315 mi). Perigee: 186 km (115 mi). Inclination: 57.00 deg. Period: 91.40 min. Photo surveillance; film capsule; capsule returned January 30. Second fully successful FSW mission..
1978 January 31 - .
14:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 987 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 14.00 days. Decay Date: 1978-02-14 . USAF Sat Cat: 10639 . COSPAR: 1978-013A. Apogee: 322 km (200 mi). Perigee: 189 km (117 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 February 8 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 988 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1978-02-20 . USAF Sat Cat: 10666 . COSPAR: 1978-015A. Apogee: 335 km (208 mi). Perigee: 201 km (124 mi). Inclination: 72.80 deg. Period: 89.90 min. Military topography satellite; returned film capsule; maneuverable; also performed mapping, geodesy, earth resources tasks..
1978 February 14 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 989 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 14.00 days. Decay Date: 1978-02-28 . USAF Sat Cat: 10672 . COSPAR: 1978-017A. Apogee: 318 km (197 mi). Perigee: 169 km (105 mi). Inclination: 65.10 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 February 25 - .
05:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 34B.
- Jumpseat 5 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Jumpseat.
USAF Sat Cat: 10688 . COSPAR: 1978-021A. Apogee: 39,377 km (24,467 mi). Perigee: 311 km (193 mi). Inclination: 63.20 deg. Period: 703.70 min. Or Quasar..
1978 March 4 - .
07:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 992 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-03-17 . USAF Sat Cat: 10699 . COSPAR: 1978-025A. Apogee: 323 km (200 mi). Perigee: 203 km (126 mi). Inclination: 71.30 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 March 10 - .
10:42 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 993 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-03-23 . USAF Sat Cat: 10725 . COSPAR: 1978-027A. Apogee: 325 km (201 mi). Perigee: 190 km (110 mi). Inclination: 72.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 March 16 - .
18:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 14 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1978-09-11 . USAF Sat Cat: 10733 . COSPAR: 1978-029A. Apogee: 240 km (140 mi). Perigee: 160 km (90 mi). Inclination: 96.40 deg. Period: 88.50 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 7858 - .
Payload: SSF-D No. 2. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 10734 . COSPAR: 1978-029B. Apogee: 645 km (400 mi). Perigee: 639 km (397 mi). Inclination: 95.80 deg. Period: 97.60 min. Radar monitoring..
1978 March 17 - .
10:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 995 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-03-30 . USAF Sat Cat: 10735 . COSPAR: 1978-030A. Apogee: 227 km (141 mi). Perigee: 209 km (129 mi). Inclination: 81.30 deg. Period: 88.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 March 30 - .
07:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 999 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-04-12 . USAF Sat Cat: 10773 . COSPAR: 1978-033A. Apogee: 352 km (218 mi). Perigee: 174 km (108 mi). Inclination: 71.40 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 April 6 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1002 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-04-19 . USAF Sat Cat: 10785 . COSPAR: 1978-037A. Apogee: 283 km (175 mi). Perigee: 205 km (127 mi). Inclination: 65.10 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 April 7 - .
00:45 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC13.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3A Agena D.
- OPS 8790 - .
Payload: AFP-472 AQUACADE 4. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Rhyolite.
USAF Sat Cat: 10787 . COSPAR: 1978-038A. Apogee: 35,855 km (22,279 mi). Perigee: 35,679 km (22,169 mi). Inclination: 0.20 deg. Period: 1,435.10 min. Fourth and final launch of Rhyolite geostationary ELINT satellite. Code name changed to Aquacade after Rhyolite name came out in trial of spy Boyce..
1978 April 20 - .
15:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1003 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 14.00 days. Decay Date: 1978-05-04 . USAF Sat Cat: 10811 . COSPAR: 1978-040A. Apogee: 328 km (203 mi). Perigee: 178 km (110 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 May 5 - .
15:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1004 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-05-18 . USAF Sat Cat: 10846 . COSPAR: 1978-043A. Apogee: 290 km (180 mi). Perigee: 205 km (127 mi). Inclination: 62.80 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule; separated science capsule..
1978 May 12 - .
04:07 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1005 - .
Payload: Tselina-D no. 15. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2000-06-15 . USAF Sat Cat: 10860 . COSPAR: 1978-045A. Apogee: 494 km (306 mi). Perigee: 485 km (301 mi). Inclination: 81.20 deg. Period: 94.40 min.
1978 May 12 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1006 - .
Mass: 1,120 kg (2,460 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1979-03-14 . USAF Sat Cat: 10862 . COSPAR: 1978-046A. Apogee: 407 km (252 mi). Perigee: 384 km (238 mi). Inclination: 65.80 deg. Period: 92.40 min. Radar calibration mission..
1978 May 16 - .
10:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1007 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-05-29 . USAF Sat Cat: 10895 . COSPAR: 1978-048A. Apogee: 350 km (210 mi). Perigee: 168 km (104 mi). Inclination: 72.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable; also performed earth resources tasks..
1978 May 17 - .
14:39 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1008 - .
Mass: 1,080 kg (2,380 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1981-01-08 . USAF Sat Cat: 10898 . COSPAR: 1978-049A. Apogee: 549 km (341 mi). Perigee: 499 km (310 mi). Inclination: 74.00 deg. Period: 95.10 min. Replaced Cosmos 845. Investigation of the upper atmosphere and outer space. .
1978 May 23 - .
07:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1010 - .
Payload: Zenit-4MKT no. 6. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1978-06-05 . USAF Sat Cat: 10915 . COSPAR: 1978-052A. Apogee: 230 km (140 mi). Perigee: 217 km (134 mi). Inclination: 81.40 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1978 May 25 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1012 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-06-07 . USAF Sat Cat: 10919 . COSPAR: 1978-054A. Apogee: 265 km (164 mi). Perigee: 202 km (125 mi). Inclination: 62.80 deg. Period: 89.20 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 June 10 - .
08:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1021 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-06-23 . USAF Sat Cat: 10939 . COSPAR: 1978-057A. Apogee: 313 km (194 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 June 10 - .
19:12 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- Chalet 1 - .
Payload: Chalet 1 (Vortex 1) / OPS 9454. Mass: 820 kg (1,800 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Chalet.
USAF Sat Cat: 10941 . COSPAR: 1978-058A. Apogee: 42,039 km (26,121 mi). Perigee: 29,929 km (18,596 mi). Inclination: 12.00 deg. Period: 1,446.30 min. First launch of the heavier, mored advanced CHALET ELINT satellites. (the project was renamed VORTEX when the code name CHALET appeared in the New York Times)..
1978 June 12 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1022 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-06-25 . USAF Sat Cat: 10944 . COSPAR: 1978-059A. Apogee: 344 km (213 mi). Perigee: 171 km (106 mi). Inclination: 72.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 June 14 - .
18:28 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
1978 June 28 - .
02:59 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1024 - .
Payload: Oko #9. Mass: 2,030 kg (4,470 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 10970 . COSPAR: 1978-066A. Apogee: 35,365 km (21,974 mi). Perigee: 4,984 km (3,096 mi). Inclination: 67.30 deg. Period: 717.70 min. Replaced Cosmos 931. Covered Oko constellation plane 2 - 323 degree longitude of ascending node..
1978 June 28 - .
17:35 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1025 - .
Payload: Tselina-D Mass model no. 16. Mass: 4,375 kg (9,645 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2007-03-10 . USAF Sat Cat: 10973 . COSPAR: 1978-067A. Apogee: 567 km (352 mi). Perigee: 551 km (342 mi). Inclination: 82.50 deg. Period: 95.80 min.
1978 August 5 - .
15:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1028 - .
Payload: Yantar-2K s/n 14. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1978-09-04 . USAF Sat Cat: 10995 . COSPAR: 1978-076A. Apogee: 247 km (153 mi). Perigee: 170 km (100 mi). Inclination: 67.10 deg. Period: 88.70 min. Successful full duration flight. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1978 August 29 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1029 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 10.00 days. Decay Date: 1978-09-08 . USAF Sat Cat: 11012 . COSPAR: 1978-082A. Apogee: 316 km (196 mi). Perigee: 194 km (120 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 September 6 - .
03:04 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1030 - .
Payload: Oko #10. Mass: 2,030 kg (4,470 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2004-08-17 . USAF Sat Cat: 11015 . COSPAR: 1978-083A. Apogee: 36,185 km (22,484 mi). Perigee: 4,131 km (2,566 mi). Inclination: 66.20 deg. Period: 717.00 min. Covered Oko constellation plane 4 - 39 degree longitude of ascending node..
1978 September 9 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1031 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-09-22 . USAF Sat Cat: 11022 . COSPAR: 1978-085A. Apogee: 329 km (204 mi). Perigee: 182 km (113 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 September 19 - .
08:05 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1032 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-10-02 . USAF Sat Cat: 11029 . COSPAR: 1978-088A. Apogee: 226 km (140 mi). Perigee: 215 km (133 mi). Inclination: 81.30 deg. Period: 88.90 min. Area survey photo reconnaissance satellite; returned film capsule; separated capsule..
1978 October 3 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1033 - .
Payload: Zenit-4MKT no. 7. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1978-10-16 . USAF Sat Cat: 11039 . COSPAR: 1978-089A. Apogee: 231 km (143 mi). Perigee: 212 km (131 mi). Inclination: 81.40 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1978 October 6 - .
15:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1042 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-10-19 . USAF Sat Cat: 11052 . COSPAR: 1978-092A. Apogee: 299 km (185 mi). Perigee: 179 km (111 mi). Inclination: 62.80 deg. Period: 89.30 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 October 10 - .
19:44 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1043 - .
Payload: Tselina-D no. 17. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1998-02-27 . USAF Sat Cat: 11055 . COSPAR: 1978-094A. Apogee: 433 km (269 mi). Perigee: 425 km (264 mi). Inclination: 81.20 deg. Period: 93.20 min.
1978 October 17 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1044 - .
Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-10-30 . USAF Sat Cat: 11065 . COSPAR: 1978-097A. Apogee: 295 km (183 mi). Perigee: 203 km (126 mi). Inclination: 62.80 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 November 1 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1046 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1978-11-13 . USAF Sat Cat: 11098 . COSPAR: 1978-102A. Apogee: 324 km (201 mi). Perigee: 202 km (125 mi). Inclination: 72.90 deg. Period: 89.80 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources tasks; deployed capsule..
1978 November 15 - .
11:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1047 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-11-28 . USAF Sat Cat: 11108 . COSPAR: 1978-104A. Apogee: 354 km (219 mi). Perigee: 171 km (106 mi). Inclination: 72.90 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 November 21 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1049 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-12-04 . USAF Sat Cat: 11118 . COSPAR: 1978-107A. Apogee: 338 km (210 mi). Perigee: 169 km (105 mi). Inclination: 72.90 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 November 28 - .
16:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1050 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1978-12-12 . USAF Sat Cat: 11121 . COSPAR: 1978-108A. Apogee: 341 km (211 mi). Perigee: 194 km (120 mi). Inclination: 62.80 deg. Period: 89.80 min. Photo surveillance; returned film capsule; maneuverable..
1978 December 7 - .
15:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1059 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1978-12-20 . USAF Sat Cat: 11137 . COSPAR: 1978-110A. Apogee: 338 km (210 mi). Perigee: 180 km (110 mi). Inclination: 62.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 December 8 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1060 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-12-21 . USAF Sat Cat: 11139 . COSPAR: 1978-111A. Apogee: 291 km (180 mi). Perigee: 216 km (134 mi). Inclination: 65.00 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1978 December 14 - .
15:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1061 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1978-12-27 . USAF Sat Cat: 11148 . COSPAR: 1978-114A. Apogee: 310 km (190 mi). Perigee: 203 km (126 mi). Inclination: 62.80 deg. Period: 89.60 min. Area survey photo reconnaissance satellite; returned film capsule; deployed capsule..
1978 December 15 - .
13:19 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1062 - .
Mass: 810 kg (1,780 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1981-04-20 . USAF Sat Cat: 11150 . COSPAR: 1978-115A. Apogee: 549 km (341 mi). Perigee: 504 km (313 mi). Inclination: 74.00 deg. Period: 95.10 min. Replaced Cosmos 899. Possible ELINT satellite..
1978 December 19 - .
01:35 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1063 - .
Payload: Tselina-D no. 18. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2001-11-25 . USAF Sat Cat: 11155 . COSPAR: 1978-117A. Apogee: 524 km (325 mi). Perigee: 518 km (321 mi). Inclination: 81.20 deg. Period: 95.10 min.
1978 December 22 - .
22:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1065 - .
Mass: 1,170 kg (2,570 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1979-08-01 . USAF Sat Cat: 11163 . COSPAR: 1978-120A. Apogee: 544 km (338 mi). Perigee: 348 km (216 mi). Inclination: 50.60 deg. Period: 93.50 min. Radar calibration. Released 7 Romb radar calibration subsatellites. Possible partially failed spacecraft bus..
1978 December 26 - .
15:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1068 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-01-08 . USAF Sat Cat: 11169 . COSPAR: 1978-123A. Apogee: 389 km (241 mi). Perigee: 191 km (118 mi). Inclination: 62.80 deg. Period: 90.40 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1978 December 28 - .
16:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1069 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 13.00 days. Decay Date: 1979-01-10 . USAF Sat Cat: 11173 . COSPAR: 1978-124A. Apogee: 289 km (179 mi). Perigee: 254 km (157 mi). Inclination: 62.90 deg. Period: 89.90 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources tasks; separated capsule..
1979 January 11 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1070 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 9.00 days. Decay Date: 1979-01-20 . USAF Sat Cat: 11229 . COSPAR: 1979-001A. Apogee: 293 km (182 mi). Perigee: 205 km (127 mi). Inclination: 62.80 deg. Period: 89.50 min. Area survey photo reconnaissance satellite; returned film capsule..
1979 January 13 - .
15:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1071 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-01-26 . USAF Sat Cat: 11233 . COSPAR: 1979-002A. Apogee: 339 km (210 mi). Perigee: 179 km (111 mi). Inclination: 62.80 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 January 30 - .
15:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1073 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 29.00 days. Decay Date: 1979-02-12 . USAF Sat Cat: 11255 . COSPAR: 1979-006A. Apogee: 328 km (203 mi). Perigee: 182 km (113 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 February 8 - .
10:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1075 - .
Mass: 1,080 kg (2,380 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1981-10-19 . USAF Sat Cat: 11262 . COSPAR: 1979-010A. Apogee: 516 km (320 mi). Perigee: 473 km (293 mi). Inclination: 65.80 deg. Period: 94.40 min. Radar calibration mission..
1979 February 13 - .
21:41 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1077 - .
Payload: Tselina-D no. 19. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2000-06-26 . USAF Sat Cat: 11268 . COSPAR: 1979-012A. Apogee: 491 km (305 mi). Perigee: 485 km (301 mi). Inclination: 81.20 deg. Period: 94.40 min.
1979 February 22 - .
12:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1078 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 8.00 days. Decay Date: 1979-03-02 . USAF Sat Cat: 11276 . COSPAR: 1979-016A. Apogee: 280 km (170 mi). Perigee: 168 km (104 mi). Inclination: 72.90 deg. Period: 89.00 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 February 27 - .
15:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1079 - .
Payload: Yantar-2K s/n 15. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 12.00 days. Decay Date: 1979-03-11 . USAF Sat Cat: 11283 . COSPAR: 1979-019A. Apogee: 337 km (209 mi). Perigee: 174 km (108 mi). Inclination: 67.10 deg. Period: 89.60 min. Area survey photo reconnaissance. Spacecraft depressurization led to malfunction of spacecraft. Deorbited after 12 days..
1979 March 14 - .
10:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1080 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 14.00 days. Decay Date: 1979-03-28 . USAF Sat Cat: 11294 . COSPAR: 1979-023A. Apogee: 294 km (182 mi). Perigee: 169 km (105 mi). Inclination: 72.90 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 March 16 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 15 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1979-09-22 . USAF Sat Cat: 11305 . COSPAR: 1979-025A. Apogee: 258 km (160 mi). Perigee: 170 km (100 mi). Inclination: 96.40 deg. Period: 88.80 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 6675 - .
Payload: SSF-D No. 3. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 11306 . COSPAR: 1979-025B. Apogee: 628 km (390 mi). Perigee: 621 km (385 mi). Inclination: 95.80 deg. Period: 97.20 min.
1979 March 31 - .
10:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1090 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-2M satellite.
Duration: 13.00 days. Decay Date: 1979-04-13 . USAF Sat Cat: 11313 . COSPAR: 1979-027A. Apogee: 320 km (190 mi). Perigee: 217 km (134 mi). Inclination: 72.80 deg. Period: 89.80 min. Area survey photo reconnaissance satellite; returned film capsule..
1979 April 14 - .
05:27 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1093 - .
Payload: Tselina-D no. 20. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2000-03-23 . USAF Sat Cat: 11331 . COSPAR: 1979-032A. Apogee: 487 km (302 mi). Perigee: 474 km (294 mi). Inclination: 81.20 deg. Period: 94.20 min.
1979 April 18 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1094 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1979-09-30 . USAF Sat Cat: 11333 . COSPAR: 1979-033A. Apogee: 442 km (274 mi). Perigee: 426 km (264 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring..
1979 April 20 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1095 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1979-05-04 . USAF Sat Cat: 11335 . COSPAR: 1979-034A. Apogee: 379 km (235 mi). Perigee: 199 km (123 mi). Inclination: 72.80 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1979 April 25 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1096 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1979-11-24 . USAF Sat Cat: 11346 . COSPAR: 1979-036A. Apogee: 442 km (274 mi). Perigee: 428 km (265 mi). Inclination: 65.10 deg. Period: 93.30 min. Ocean monitoring..
1979 April 27 - .
17:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1097 - .
Payload: Yantar-4K1 s/n 1. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 30.00 days. Decay Date: 1979-05-27 . USAF Sat Cat: 11348 . COSPAR: 1979-037A. Apogee: 331 km (205 mi). Perigee: 173 km (107 mi). Inclination: 62.80 deg. Period: 89.50 min. First flight test of Yantar-4K1 satellite. Returned as planned after 30 days. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1979 May 15 - .
11:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1098 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-05-28 . USAF Sat Cat: 11358 . COSPAR: 1979-040A. Apogee: 354 km (219 mi). Perigee: 170 km (100 mi). Inclination: 72.90 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable; also performed earth resources tasks..
1979 May 17 - .
07:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1099 - .
Payload: Zenit-4MKT no. 8. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1979-05-30 . USAF Sat Cat: 11360 . COSPAR: 1979-041A. Apogee: 247 km (153 mi). Perigee: 215 km (133 mi). Inclination: 81.40 deg. Period: 89.10 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1979 May 25 - .
07:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1979 May 28 - .
18:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 7164 - .
Payload: KH-8 no. 50 / Agena D. Mass: 4,000 kg (8,800 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1979-08-26 . USAF Sat Cat: 11372 . COSPAR: 1979-044A. Apogee: 285 km (177 mi). Perigee: 131 km (81 mi). Inclination: 96.40 deg. Period: 88.70 min. KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1979 May 31 - .
16:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1103 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1979-06-14 . USAF Sat Cat: 11376 . COSPAR: 1979-045A. Apogee: 375 km (233 mi). Perigee: 257 km (159 mi). Inclination: 62.80 deg. Period: 90.80 min. Photo surveillance; returned film capsule..
1979 June 8 - .
07:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1105 - .
Payload: Zenit-4MKT no. 9. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1979-06-21 . USAF Sat Cat: 11394 . COSPAR: 1979-052A. Apogee: 254 km (157 mi). Perigee: 212 km (131 mi). Inclination: 81.40 deg. Period: 89.20 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1979 June 10 - .
13:39 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
1979 June 12 - .
07:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1979 June 15 - .
10:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1107 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1979-06-29 . USAF Sat Cat: 11404 . COSPAR: 1979-055A. Apogee: 301 km (187 mi). Perigee: 198 km (123 mi). Inclination: 72.90 deg. Period: 89.50 min. Photo surveillance; returned film capsule; maneuverable..
1979 June 22 - .
07:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1108 - .
Payload: Zenit-4MKT no. 10. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1979-07-05 . USAF Sat Cat: 11413 . COSPAR: 1979-056A. Apogee: 245 km (152 mi). Perigee: 214 km (132 mi). Inclination: 81.30 deg. Period: 89.10 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1979 June 27 - .
18:11 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1109 - .
Payload: Oko #11. Mass: 2,030 kg (4,470 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 11417 . COSPAR: 1979-058A. Apogee: 36,998 km (22,989 mi). Perigee: 3,228 km (2,005 mi). Inclination: 68.20 deg. Period: 715.20 min. Covered Oko constellation plane 9 - 237 degree longitude of ascending node..
1979 June 29 - .
16:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1111 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 15.00 days. Decay Date: 1979-07-14 . USAF Sat Cat: 11429 . COSPAR: 1979-061A. Apogee: 354 km (219 mi). Perigee: 255 km (158 mi). Inclination: 62.80 deg. Period: 90.60 min. Photo surveillance; returned film capsule..
1979 July 6 - .
08:20 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1112 - .
Mass: 1,190 kg (2,620 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1980-01-21 . USAF Sat Cat: 11443 . COSPAR: 1979-063A. Apogee: 541 km (336 mi). Perigee: 357 km (221 mi). Inclination: 50.60 deg. Period: 93.50 min. Radar calibration. Released 25 Romb radar calibration subsatellites..
1979 July 10 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1113 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-07-23 . USAF Sat Cat: 11447 . COSPAR: 1979-064A. Apogee: 330 km (200 mi). Perigee: 173 km (107 mi). Inclination: 65.00 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 July 11 - .
15:41 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1114 - .
Mass: 1,080 kg (2,380 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1981-12-26 . USAF Sat Cat: 11449 . COSPAR: 1979-065A. Apogee: 552 km (342 mi). Perigee: 506 km (314 mi). Inclination: 74.10 deg. Period: 95.20 min. Replaced Cosmos 924. Possible ELINT satellite..
1979 July 13 - .
08:25 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1115 - .
Payload: Zenit-4MKT no. 11. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1979-07-26 . USAF Sat Cat: 11451 . COSPAR: 1979-066A. Apogee: 235 km (146 mi). Perigee: 217 km (134 mi). Inclination: 81.40 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1979 July 20 - .
11:58 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1116 - .
Payload: Tselina-D no. 21. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1993-03-11 . USAF Sat Cat: 11457 . COSPAR: 1979-067A. Apogee: 408 km (253 mi). Perigee: 396 km (246 mi). Inclination: 81.20 deg. Period: 92.60 min.
1979 July 25 - .
15:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1117 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-08-07 . USAF Sat Cat: 11463 . COSPAR: 1979-068A. Apogee: 325 km (201 mi). Perigee: 177 km (109 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 July 27 - .
07:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1979 August 3 - .
10:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1119 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1979-08-15 . USAF Sat Cat: 11478 . COSPAR: 1979-071A. Apogee: 245 km (152 mi). Perigee: 213 km (132 mi). Inclination: 81.40 deg. Period: 89.00 min. Military topography satellite; returned film capsule; separated capsule..
1979 August 11 - .
09:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1120 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-08-24 . USAF Sat Cat: 11485 . COSPAR: 1979-073A. Apogee: 362 km (224 mi). Perigee: 170 km (100 mi). Inclination: 70.60 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 August 14 - .
15:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1121 - .
Payload: Yantar-2K s/n 929. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1979-09-13 . USAF Sat Cat: 11487 . COSPAR: 1979-074A. Apogee: 348 km (216 mi). Perigee: 171 km (106 mi). Inclination: 67.20 deg. Period: 89.70 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1979 August 17 - .
07:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1979 August 21 - .
11:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1123 - .
Payload: Zenit-4MKT no. 12. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1979-09-03 . USAF Sat Cat: 11496 . COSPAR: 1979-076A. Apogee: 236 km (146 mi). Perigee: 211 km (131 mi). Inclination: 81.30 deg. Period: 88.90 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1979 August 28 - .
00:17 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1124 - .
Payload: Oko #12. Mass: 2,030 kg (4,470 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 11509 . COSPAR: 1979-077A. Apogee: 35,403 km (21,998 mi). Perigee: 4,913 km (3,052 mi). Inclination: 67.30 deg. Period: 717.00 min. Replaced Cosmos 1030. Covered Oko constellation plane 4 - 36 degree longitude of ascending node..
1979 August 31 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1126 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1979-09-14 . USAF Sat Cat: 11515 . COSPAR: 1979-079A. Apogee: 391 km (242 mi). Perigee: 194 km (120 mi). Inclination: 72.80 deg. Period: 90.40 min. Photo surveillance; returned film capsule..
1979 September 14 - .
15:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1128 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1979-09-27 . USAF Sat Cat: 11529 . COSPAR: 1979-081A. Apogee: 328 km (203 mi). Perigee: 173 km (107 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1979 September 28 - .
12:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1138 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1979-10-12 . USAF Sat Cat: 11548 . COSPAR: 1979-085A. Apogee: 373 km (231 mi). Perigee: 199 km (123 mi). Inclination: 72.90 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1979 October 1 - .
11:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- Chalet 2 - .
Payload: Chalet 2 (Vortex 2) / OPS 1948. Mass: 820 kg (1,800 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Chalet.
USAF Sat Cat: 11558 . COSPAR: 1979-086A. Apogee: 41,497 km (25,784 mi). Perigee: 30,443 km (18,916 mi). Inclination: 7.50 deg. Period: 1,445.50 min. Chalet ELINT satellite..
1979 October 5 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1139 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 13.00 days. Decay Date: 1979-10-18 . USAF Sat Cat: 11564 . COSPAR: 1979-088A. Apogee: 329 km (204 mi). Perigee: 199 km (123 mi). Inclination: 72.80 deg. Period: 89.80 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources tasks; separated capsule..
1979 October 22 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1142 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1979-11-04 . USAF Sat Cat: 11592 . COSPAR: 1979-092A. Apogee: 382 km (237 mi). Perigee: 198 km (123 mi). Inclination: 72.90 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1979 October 26 - .
18:12 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1143 - .
Payload: Tselina-D no. 22. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2002-02-17 . USAF Sat Cat: 11600 . COSPAR: 1979-093A. Apogee: 533 km (331 mi). Perigee: 524 km (325 mi). Inclination: 81.30 deg. Period: 95.20 min.
1979 November 2 - .
16:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1144 - .
Payload: Yantar-2K s/n 939. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 32.00 days. Decay Date: 1979-12-04 . USAF Sat Cat: 11611 . COSPAR: 1979-097A. Apogee: 337 km (209 mi). Perigee: 158 km (98 mi). Inclination: 67.20 deg. Period: 89.40 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1979 November 27 - .
09:55 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1145 - .
Payload: Tselina-D no. 23. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2000-06-16 . USAF Sat Cat: 11629 . COSPAR: 1979-099A. Apogee: 495 km (307 mi). Perigee: 484 km (300 mi). Inclination: 81.20 deg. Period: 94.40 min.
1979 December 5 - .
09:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1146 - .
Mass: 1,000 kg (2,200 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1981-11-25 . USAF Sat Cat: 11632 . COSPAR: 1979-100A. Apogee: 493 km (306 mi). Perigee: 438 km (272 mi). Inclination: 65.90 deg. Period: 93.90 min. Radar calibration..
1979 December 12 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1147 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1979-12-26 . USAF Sat Cat: 11638 . COSPAR: 1979-102A. Apogee: 377 km (234 mi). Perigee: 192 km (119 mi). Inclination: 72.90 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1979 December 28 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1148 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1980-01-10 . USAF Sat Cat: 11649 . COSPAR: 1979-106A. Apogee: 340 km (210 mi). Perigee: 170 km (100 mi). Inclination: 67.10 deg. Period: 89.60 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1980 January 9 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1149 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-01-23 . USAF Sat Cat: 11652 . COSPAR: 1980-001A. Apogee: 384 km (238 mi). Perigee: 191 km (118 mi). Inclination: 72.90 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1980 January 24 - .
15:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1152 - .
Payload: Yantar-2K s/n 928. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 13.00 days. Decay Date: 1980-02-06 . USAF Sat Cat: 11678 . COSPAR: 1980-006A. Apogee: 341 km (211 mi). Perigee: 169 km (105 mi). Inclination: 67.10 deg. Period: 89.60 min. Area survey photo reconnaissance. Mission terminated early for unknown reasons (normally 30 day duration)..
1980 January 30 - .
12:51 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1154 - .
Payload: Tselina-D no. 24. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2002-11-05 . USAF Sat Cat: 11682 . COSPAR: 1980-008A. Apogee: 545 km (338 mi). Perigee: 540 km (330 mi). Inclination: 81.20 deg. Period: 95.50 min.
1980 February 7 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1155 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-02-21 . USAF Sat Cat: 11685 . COSPAR: 1980-009A. Apogee: 393 km (244 mi). Perigee: 191 km (118 mi). Inclination: 72.80 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1980 February 7 - .
21:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-11 no. 3 - .
Payload: KH-11 no. 3 / OPS 2581. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
Decay Date: 1982-10-30 . USAF Sat Cat: 11687 . COSPAR: 1980-010A. Apogee: 498 km (309 mi). Perigee: 220 km (130 mi). Inclination: 97.00 deg. Period: 91.70 min. KH-11 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1980 February 12 - .
00:53 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
FAILURE: Fourth stage failure..
Failed Stage: U.
- Cosmos 1164 - .
Payload: Oko #13. Mass: 1,890 kg (4,160 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 1980-02-12 . USAF Sat Cat: 11700 . COSPAR: 1980-013A. Apogee: 40,856 km (25,386 mi). Perigee: 434 km (269 mi). Inclination: 62.80 deg. Period: 736.80 min. Left in parking orbit. Decay date suspect Investigation of the upper atmosphere and outer space. Was intended to cover Oko constellation plane 9 - 241 degree longitude of ascending node..
1980 February 21 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1165 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1980-03-05 . USAF Sat Cat: 11713 . COSPAR: 1980-017A. Apogee: 350 km (210 mi). Perigee: 170 km (100 mi). Inclination: 72.90 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule.
1980 March 3 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas F/MSD.
- EP-2 (NOSS 3) - .
Payload: Plume shield / OPS 7245 DEB. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 11733 . COSPAR: 1980-019E. Apogee: 1,166 km (724 mi). Perigee: 1,048 km (651 mi). Inclination: 63.50 deg. Period: 107.40 min.
- NOSS 3 - .
Payload: PARCAE 3 / OPS 7245. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 11720 . COSPAR: 1980-019A. Apogee: 1,150 km (710 mi). Perigee: 1,035 km (643 mi). Inclination: 63.00 deg. Period: 107.10 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- EP 3 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 11745 . COSPAR: 1980-019G. Apogee: 1,166 km (724 mi). Perigee: 1,048 km (651 mi). Inclination: 63.50 deg. Period: 107.40 min. Deployed from NOSS 3. .
- EP 2 - .
Payload: SSU. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 11732 . COSPAR: 1980-019D. Apogee: 1,484 km (922 mi). Perigee: 730 km (450 mi). Inclination: 63.40 deg. Period: 107.41 min.
- EP 1 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 11731 . COSPAR: 1980-019C. Apogee: 1,166 km (724 mi). Perigee: 1,048 km (651 mi). Inclination: 63.50 deg. Period: 107.40 min. Deployed from NOSS 3..
1980 March 4 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1166 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-03-18 . USAF Sat Cat: 11722 . COSPAR: 1980-020A. Apogee: 371 km (230 mi). Perigee: 194 km (120 mi). Inclination: 72.80 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1980 March 14 - .
10:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1167 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1981-10-01 . USAF Sat Cat: 11729 . COSPAR: 1980-021A. Apogee: 442 km (274 mi). Perigee: 426 km (264 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring..
1980 March 18 - .
16:01 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
FAILURE: Booster exploded on pad during servicing. Severe pad damage, 48 people killed. Cause found to be change in solder with tin to that with lead in H2O2 filters, causing decomposition and explosion..
Failed Stage: 0.
- Tselina-D - .
Nation: Russia.
Agency: RVSN.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 1980-03-18 . COSPAR: F800318A.
This was the worst disaster since the Nedelin Catastrophe on 24 October 1964. A commission of military officers and chief designers reviewed the incident and requested changes to equipment and procedures, especially as regarded liquid oxygen handling. Another source reports that the explosion occurred during the fuelling of the Block E upper stage, and was due to hydrogen peroxide being present in a lox line filter and a confusion between fuel and lox lines. This error had always been possible, but had never happened in the 20 years of use of the booster before the explosion. The launch pad was badly damaged and not put back into service until April 1983.
1980 March 27 - .
07:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1169 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1983-03-03 . USAF Sat Cat: 11741 . COSPAR: 1980-023A. Apogee: 513 km (318 mi). Perigee: 466 km (289 mi). Inclination: 65.80 deg. Period: 94.40 min. Radar calibration mission..
1980 April 1 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1170 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 11.00 days. Decay Date: 1980-04-12 . USAF Sat Cat: 11747 . COSPAR: 1980-025A. Apogee: 379 km (235 mi). Perigee: 178 km (110 mi). Inclination: 70.40 deg. Period: 90.10 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1980 April 12 - .
20:18 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1172 - .
Payload: Oko #14. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 1997-12-26 . USAF Sat Cat: 11758 . COSPAR: 1980-028A. Apogee: 38,809 km (24,114 mi). Perigee: 1,476 km (917 mi). Inclination: 64.70 deg. Period: 716.40 min. Replaced Cosmos 1109. Covered Oko constellation plane 9 - 240 degree longitude of ascending node..
1980 April 17 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1173 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 11.00 days. Decay Date: 1980-04-28 . USAF Sat Cat: 11763 . COSPAR: 1980-029A. Apogee: 352 km (218 mi). Perigee: 174 km (108 mi). Inclination: 70.30 deg. Period: 89.80 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1980 April 29 - .
11:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1176 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1980-10-04 . USAF Sat Cat: 11968 . COSPAR: 1980-034B. Apogee: 962 km (597 mi). Perigee: 873 km (542 mi). Inclination: 64.80 deg. Period: 103.40 min. Ocean surveillance; nuclear powered; test flight of modified safer design..
1980 April 29 - .
13:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1177 - .
Payload: Yantar-4K1 s/n 2. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 44.00 days. Decay Date: 1980-06-12 . USAF Sat Cat: 11789 . COSPAR: 1980-035A. Apogee: 331 km (205 mi). Perigee: 167 km (103 mi). Inclination: 67.20 deg. Period: 89.50 min. Second flight test of Yantar-4K1 satellite. Demonstrated full spacecraft design duration of 45 days. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1980 May 7 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1178 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 15.00 days. Decay Date: 1980-05-22 . USAF Sat Cat: 11793 . COSPAR: 1980-036A. Apogee: 386 km (239 mi). Perigee: 193 km (119 mi). Inclination: 72.80 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1980 May 14 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1179 - .
Mass: 650 kg (1,430 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1989-07-18 . USAF Sat Cat: 11796 . COSPAR: 1980-037A. Apogee: 307 km (190 mi). Perigee: 202 km (125 mi). Inclination: 82.90 deg. Period: 89.60 min. Failure. Radar calibration mission..
1980 May 15 - .
05:35 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1180 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 11.00 days. Decay Date: 1980-05-26 . USAF Sat Cat: 11798 . COSPAR: 1980-038A. Apogee: 279 km (173 mi). Perigee: 245 km (152 mi). Inclination: 62.80 deg. Period: 89.80 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources tasks; separated capsule..
1980 May 23 - .
07:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1182 - .
Payload: Zenit-4MKT no. 13. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1980-06-05 . USAF Sat Cat: 11808 . COSPAR: 1980-040A. Apogee: 251 km (155 mi). Perigee: 211 km (131 mi). Inclination: 82.30 deg. Period: 89.10 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1980 May 28 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1183 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-06-11 . USAF Sat Cat: 11816 . COSPAR: 1980-042A. Apogee: 384 km (238 mi). Perigee: 196 km (121 mi). Inclination: 72.80 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1980 June 4 - .
07:34 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1184 - .
Payload: Tselina-D no. 25. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2002-04-29 . USAF Sat Cat: 11821 . COSPAR: 1980-044A. Apogee: 535 km (332 mi). Perigee: 532 km (330 mi). Inclination: 81.20 deg. Period: 95.30 min.
1980 June 6 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1186 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1982-01-01 . USAF Sat Cat: 11829 . COSPAR: 1980-047A. Apogee: 414 km (257 mi). Perigee: 388 km (241 mi). Inclination: 74.00 deg. Period: 92.60 min. Released 25 Romb radar calibration subsatellites..
1980 June 12 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1187 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-06-26 . USAF Sat Cat: 11837 . COSPAR: 1980-048A. Apogee: 294 km (182 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 89.40 min. Photo surveillance; returned film capsule; maneuverable..
1980 June 14 - .
20:52 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1188 - .
Payload: Oko #15. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2013-05-24 . USAF Sat Cat: 11844 . COSPAR: 1980-050A. Apogee: 36,280 km (22,540 mi). Perigee: 4,103 km (2,549 mi). Inclination: 68.00 deg. Period: 718.40 min. Replaced Cosmos 1024. Covered Oko constellation plane 2 - 319 degree longitude of ascending node..
1980 June 18 - .
18:29 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 16 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1981-03-06 . USAF Sat Cat: 11850 . COSPAR: 1980-052A. Apogee: 262 km (162 mi). Perigee: 164 km (101 mi). Inclination: 96.40 deg. Period: 88.80 min. KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OPS 1292 - .
Payload: SSF-C No. 6. Mass: 60 kg (132 lb). Nation: USA.
Agency: CIA,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 11852 . COSPAR: 1980-052C. Apogee: 1,333 km (828 mi). Perigee: 1,331 km (827 mi). Inclination: 96.60 deg. Period: 112.30 min. ABM monitoring; may or may not have existed!!!..
1980 June 26 - .
12:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1189 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-07-10 . USAF Sat Cat: 11863 . COSPAR: 1980-054A. Apogee: 305 km (189 mi). Perigee: 198 km (123 mi). Inclination: 72.90 deg. Period: 89.60 min. Photo surveillance; returned film capsule; maneuverable..
1980 July 2 - .
00:54 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1191 - .
Payload: Oko #16. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 11871 . COSPAR: 1980-057A. Apogee: 34,907 km (21,690 mi). Perigee: 5,403 km (3,357 mi). Inclination: 67.50 deg. Period: 716.90 min. Replaced Cosmos 1124. Covered Oko constellation plane 4 - 39 degree longitude of ascending node..
1980 July 9 - .
12:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1200 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-07-23 . USAF Sat Cat: 11884 . COSPAR: 1980-059A. Apogee: 298 km (185 mi). Perigee: 195 km (121 mi). Inclination: 72.90 deg. Period: 89.40 min. Photo surveillance; returned film capsule; maneuverable..
1980 July 15 - .
07:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1201 - .
Payload: Zenit-4MKT no. 14. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1980-07-28 . USAF Sat Cat: 11894 . COSPAR: 1980-061A. Apogee: 243 km (150 mi). Perigee: 213 km (132 mi). Inclination: 82.30 deg. Period: 89.10 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1980 July 24 - .
12:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1202 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-08-07 . USAF Sat Cat: 11907 . COSPAR: 1980-065A. Apogee: 307 km (190 mi). Perigee: 198 km (123 mi). Inclination: 72.90 deg. Period: 89.60 min. Photo surveillance; returned film capsule; maneuverable..
1980 July 31 - .
10:20 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1204 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1981-02-23 . USAF Sat Cat: 11917 . COSPAR: 1980-067A. Apogee: 546 km (339 mi). Perigee: 349 km (216 mi). Inclination: 50.70 deg. Period: 93.50 min. Radar calibration. Released 25 Romb radar calibration subsatellites..
1980 August 12 - .
11:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1205 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-08-26 . USAF Sat Cat: 11924 . COSPAR: 1980-068A. Apogee: 302 km (187 mi). Perigee: 195 km (121 mi). Inclination: 72.80 deg. Period: 89.50 min. Photo surveillance; returned film capsule; maneuverable..
1980 August 15 - .
05:34 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1206 - .
Payload: Tselina-D no. 26. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2002-01-14 . USAF Sat Cat: 11932 . COSPAR: 1980-069A. Apogee: 531 km (329 mi). Perigee: 525 km (326 mi). Inclination: 81.20 deg. Period: 95.20 min.
1980 August 22 - .
10:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1207 - .
Payload: Zenit-4MKT no. 15. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1980-09-04 . USAF Sat Cat: 11938 . COSPAR: 1980-070A. Apogee: 256 km (159 mi). Perigee: 211 km (131 mi). Inclination: 82.30 deg. Period: 89.20 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1980 August 26 - .
15:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1208 - .
Payload: Yantar-2K s/n 927. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 29.00 days. Decay Date: 1980-09-24 . USAF Sat Cat: 11945 . COSPAR: 1980-071A. Apogee: 339 km (210 mi). Perigee: 173 km (107 mi). Inclination: 67.10 deg. Period: 89.60 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1980 September 19 - .
10:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1210 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-10-03 . USAF Sat Cat: 11980 . COSPAR: 1980-076A. Apogee: 239 km (148 mi). Perigee: 175 km (108 mi). Inclination: 82.30 deg. Period: 88.60 min. Photo surveillance; returned film capsule; maneuverable..
1980 September 23 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1211 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 11.00 days. Decay Date: 1980-10-04 . USAF Sat Cat: 11982 . COSPAR: 1980-077A. Apogee: 236 km (146 mi). Perigee: 211 km (131 mi). Inclination: 82.40 deg. Period: 89.00 min. Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources tasks; separated capsule..
1980 September 26 - .
10:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1212 - .
Payload: Zenit-4MKT no. 16. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1980-10-09 . USAF Sat Cat: 11985 . COSPAR: 1980-078A. Apogee: 244 km (151 mi). Perigee: 205 km (127 mi). Inclination: 82.30 deg. Period: 88.90 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1980 October 3 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1213 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-10-17 . USAF Sat Cat: 11997 . COSPAR: 1980-080A. Apogee: 313 km (194 mi). Perigee: 192 km (119 mi). Inclination: 72.90 deg. Period: 89.60 min. Photo surveillance; returned film capsule; maneuverable..
1980 October 10 - .
13:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1214 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKM.
Duration: 13.00 days. Decay Date: 1980-10-23 . USAF Sat Cat: 12008 . COSPAR: 1980-082A. Apogee: 347 km (215 mi). Perigee: 170 km (100 mi). Inclination: 67.20 deg. Period: 89.70 min. High resolution photo reconnaissance satellite; returned film capsule; maneuverable..
1980 October 14 - .
20:41 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1215 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1983-05-12 . USAF Sat Cat: 12016 . COSPAR: 1980-083A. Apogee: 546 km (339 mi). Perigee: 493 km (306 mi). Inclination: 74.00 deg. Period: 95.00 min. Radar calibration. Investigation of the upper atmosphere and outer space. .
1980 October 16 - .
12:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1216 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-10-30 . USAF Sat Cat: 12019 . COSPAR: 1980-084A. Apogee: 367 km (228 mi). Perigee: 189 km (117 mi). Inclination: 72.90 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1980 October 24 - .
10:53 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1217 - .
Payload: Oko #17. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 12032 . COSPAR: 1980-085A. Apogee: 38,306 km (23,802 mi). Perigee: 2,007 km (1,247 mi). Inclination: 67.00 deg. Period: 716.90 min. Replaced Cosmos 1188. Covered Oko constellation plane 2 - 316 degree longitude of ascending node..
1980 October 30 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1980 October 31 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1219 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1980-11-13 . USAF Sat Cat: 12050 . COSPAR: 1980-088A. Apogee: 312 km (193 mi). Perigee: 189 km (117 mi). Inclination: 72.90 deg. Period: 89.50 min. Photo surveillance; returned film capsule; maneuverable..
1980 November 4 - .
15:04 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1220 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1982-06-20 . USAF Sat Cat: 12054 . COSPAR: 1980-089A. Apogee: 759 km (471 mi). Perigee: 526 km (326 mi). Inclination: 65.00 deg. Period: 97.60 min. Ocean monitoring..
1980 November 12 - .
12:21 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1221 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-11-26 . USAF Sat Cat: 12058 . COSPAR: 1980-090A. Apogee: 399 km (247 mi). Perigee: 196 km (121 mi). Inclination: 72.90 deg. Period: 90.50 min. Photo surveillance; returned film capsule..
1980 November 21 - .
11:53 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1222 - .
Payload: Tselina-D no. 27. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2011-04-27 . USAF Sat Cat: 12071 . COSPAR: 1980-093A. Apogee: 561 km (348 mi). Perigee: 557 km (346 mi). Inclination: 81.20 deg. Period: 95.90 min.
1980 November 27 - .
21:37 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1223 - .
Payload: Oko #18. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 12078 . COSPAR: 1980-095A. Apogee: 34,854 km (21,657 mi). Perigee: 5,517 km (3,428 mi). Inclination: 68.30 deg. Period: 718.10 min. Replaced Cosmos 903. Covered Oko constellation planes 7/8 - 177 degree longitude of ascending node..
1980 December - .
1980 December 1 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1224 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1980-12-15 . USAF Sat Cat: 12084 . COSPAR: 1980-096A. Apogee: 374 km (232 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1980 December 9 - .
07:18 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas E/MSD.
FAILURE: Premature shut down of one of the Atlas booster engines turned the vehicle around, thereafter the sustainer thrust it back toward the earth..
Failed Stage: 1.
- NOSS - .
Payload: PARCAE 4. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
Decay Date: 1980-12-08 . COSPAR: F801209A.
Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE. Other sources give the payload designation ABSAD. The failure was caused by a loss of lubricating oil to one of the booster engines, causing the engine to fail approx 200 milliseconds before it was to have shut down on guidance command. The asymmetric thrust pivoted the booster around approximately 180 degrees, where it stabilized in a retrofire attitude with the sustainer engine still firing. It descended back toward earth through its own exhaust flame and exploded a couple of minutes later.
1980 December 16 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1227 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 12.00 days. Decay Date: 1980-12-28 . USAF Sat Cat: 12100 . COSPAR: 1980-101A. Apogee: 296 km (183 mi). Perigee: 194 km (120 mi). Inclination: 72.80 deg. Period: 89.40 min. Photo surveillance; returned film capsule; maneuverable..
1980 December 26 - .
16:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1236 - .
Payload: Yantar-2K s/n 941. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 26.00 days. Decay Date: 1981-01-21 . USAF Sat Cat: 12121 . COSPAR: 1980-105A. Apogee: 362 km (224 mi). Perigee: 168 km (104 mi). Inclination: 67.10 deg. Period: 89.80 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 January 6 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1237 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-01-20 . USAF Sat Cat: 12130 . COSPAR: 1981-001A. Apogee: 382 km (237 mi). Perigee: 191 km (118 mi). Inclination: 72.90 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1981 January 16 - .
09:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1238 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 12138 . COSPAR: 1981-003A. Apogee: 1,706 km (1,060 mi). Perigee: 395 km (245 mi). Inclination: 83.00 deg. Period: 106.20 min. Radar calibration mission..
1981 January 16 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1239 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 12.00 days. Decay Date: 1981-01-28 . USAF Sat Cat: 12140 . COSPAR: 1981-004A. Apogee: 231 km (143 mi). Perigee: 210 km (130 mi). Inclination: 82.30 deg. Period: 88.90 min. Military topography satellite; returned film capsule; also performed mapping, geodesy..
1981 January 20 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1240 - .
Payload: Yantar-2K s/n 975. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 28.00 days. Decay Date: 1981-02-17 . USAF Sat Cat: 12143 . COSPAR: 1981-005A. Apogee: 359 km (223 mi). Perigee: 165 km (102 mi). Inclination: 64.90 deg. Period: 89.80 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 January 27 - .
14:58 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1242 - .
Payload: Tselina-D no. 28. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2014-05-08 . USAF Sat Cat: 12154 . COSPAR: 1981-008A. Apogee: 584 km (362 mi). Perigee: 568 km (352 mi). Inclination: 81.20 deg. Period: 96.20 min.
1981 February 13 - .
11:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1245 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-02-27 . USAF Sat Cat: 12299 . COSPAR: 1981-014A. Apogee: 374 km (232 mi). Perigee: 193 km (119 mi). Inclination: 72.80 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1981 February 18 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1246 - .
Payload: Yantar-1KFT no. 1. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 23.00 days. Decay Date: 1981-03-13 . USAF Sat Cat: 12301 . COSPAR: 1981-015A. Apogee: 263 km (163 mi). Perigee: 193 km (119 mi). Inclination: 64.90 deg. Period: 89.10 min. Military topographic / cartographic satellite..
1981 February 19 - .
10:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1247 - .
Payload: Oko #19. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 12303 . COSPAR: 1981-016A. Apogee: 35,529 km (22,076 mi). Perigee: 4,493 km (2,791 mi). Inclination: 67.20 deg. Period: 711.10 min. Covered Oko constellation plane 5 - 77 degree longitude of ascending node. First space launch from LC16/2, which had been cannabalised in the 1960's to reconstruct LC31 at Baikonur after the on-pad explosion of the second Soyuz in December 1966..
1981 February 28 - .
19:15 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 1166 - .
Payload: KH-8 no. 51 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1981-06-20 . USAF Sat Cat: 12315 . COSPAR: 1981-019A. Apogee: 336 km (208 mi). Perigee: 138 km (85 mi). Inclination: 96.40 deg. Period: 89.30 min. KH-8 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1981 March 5 - .
15:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1248 - .
Payload: Yantar-2K s/n 940. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1981-04-04 . USAF Sat Cat: 12317 . COSPAR: 1981-020A. Apogee: 531 km (329 mi). Perigee: 112 km (69 mi). Inclination: 68.10 deg. Period: 91.00 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 March 5 - .
18:09 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1249 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1981-07-19 . USAF Sat Cat: 12552 . COSPAR: 1981-021D. Apogee: 976 km (606 mi). Perigee: 904 km (561 mi). Inclination: 65.00 deg. Period: 103.90 min. Ocean surveillance; nuclear powered..
1981 March 16 - .
19:24 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- IMEWS 11 - .
Payload: DSP MOS/PIM s/n 10 / OPS 7350. Mass: 1,170 kg (2,570 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1992-01-01 . USAF Sat Cat: 12339 . COSPAR: 1981-025A. Apogee: 35,527 km (22,075 mi). Perigee: 35,463 km (22,035 mi). Inclination: 2.00 deg. Period: 1,421.20 min.
Multi-Orbit Satellite / Performance Improvement ballistic missile launch detection satellite, remained in service for nearly eleven years. Positioned in geosynchronous orbit over the Pacific Ocean at 69 deg W in 1981-1982; 135 deg W in 1982-1984; 75 deg E in 1984-1985. As of 2003 Mar 6 located at 40.27E drifting at 0.598E degrees per day.
1981 March 17 - .
08:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1259 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-03-31 . USAF Sat Cat: 12341 . COSPAR: 1981-026A. Apogee: 379 km (235 mi). Perigee: 204 km (126 mi). Inclination: 70.30 deg. Period: 90.40 min. Photo surveillance; returned film capsule..
1981 March 20 - .
23:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1260 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1982-05-22 . USAF Sat Cat: 12364 . COSPAR: 1981-028A. Apogee: 444 km (275 mi). Perigee: 425 km (264 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring..
1981 March 28 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
FAILURE: Failure of launch vehicle..
Failed Stage: 2.
- Yantar-2K s/n 979 - .
Payload: Yantar-2K s/n 979. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: RVSN.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Yantar Area survey photo reconnaissance spacecraft failed to achieve orbit..
1981 March 31 - .
09:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1261 - .
Payload: Oko #20. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 12376 . COSPAR: 1981-031A. Apogee: 35,583 km (22,110 mi). Perigee: 4,742 km (2,946 mi). Inclination: 67.20 deg. Period: 717.20 min. Covered Oko constellation plane 6 - 115 degree longitude of ascending node..
1981 April 7 - .
10:51 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1262 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-04-21 . USAF Sat Cat: 12385 . COSPAR: 1981-032A. Apogee: 372 km (231 mi). Perigee: 191 km (118 mi). Inclination: 72.90 deg. Period: 90.20 min. Photo surveillance; returned film capsule; maneuverable..
1981 April 9 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1263 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 12388 . COSPAR: 1981-033A. Apogee: 1,684 km (1,046 mi). Perigee: 387 km (240 mi). Inclination: 83.00 deg. Period: 105.90 min. Radar calibration mission..
1981 April 15 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1264 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-04-29 . USAF Sat Cat: 12400 . COSPAR: 1981-035A. Apogee: 382 km (237 mi). Perigee: 205 km (127 mi). Inclination: 70.40 deg. Period: 90.40 min. Photo surveillance; returned film capsule..
1981 April 16 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1265 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 12.00 days. Decay Date: 1981-04-28 . USAF Sat Cat: 12402 . COSPAR: 1981-036A. Apogee: 267 km (165 mi). Perigee: 197 km (122 mi). Inclination: 72.90 deg. Period: 89.20 min. Photo surveillance; returned film capsule; maneuverable..
1981 April 21 - .
03:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1266 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1981-05-20 . USAF Sat Cat: 12429 . COSPAR: 1981-037B. Apogee: 941 km (584 mi). Perigee: 911 km (566 mi). Inclination: 64.80 deg. Period: 103.60 min. Ocean surveillance; nuclear powered..
1981 April 24 - .
21:32 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 34B.
- Jumpseat 6 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Jumpseat.
USAF Sat Cat: 12418 . COSPAR: 1981-038A. Apogee: 708 km (439 mi). Perigee: 188 km (116 mi). Inclination: 62.70 deg. Period: 93.00 min. SDS 4 not deployed..
1981 April 28 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1268 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-05-12 . USAF Sat Cat: 12423 . COSPAR: 1981-040A. Apogee: 366 km (227 mi). Perigee: 206 km (128 mi). Inclination: 70.40 deg. Period: 90.30 min. Photo surveillance; returned film capsule; maneuverable..
1981 May 18 - .
11:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1270 - .
Payload: Yantar-2K s/n 980. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1981-06-17 . USAF Sat Cat: 12461 . COSPAR: 1981-045A. Apogee: 345 km (214 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.70 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 May 19 - .
03:49 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1271 - .
Payload: Tselina-D no. 29. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2013-05-03 . USAF Sat Cat: 12464 . COSPAR: 1981-046A. Apogee: 582 km (361 mi). Perigee: 565 km (351 mi). Inclination: 81.20 deg. Period: 96.20 min. Replaced Cosmos 1077..
1981 May 21 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1272 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-06-04 . USAF Sat Cat: 12466 . COSPAR: 1981-047A. Apogee: 376 km (233 mi). Perigee: 206 km (128 mi). Inclination: 70.40 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1981 May 22 - .
07:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1273 - .
Payload: Zenit-4MKT no. 17. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1981-06-04 . USAF Sat Cat: 12469 . COSPAR: 1981-048A. Apogee: 258 km (160 mi). Perigee: 205 km (127 mi). Inclination: 82.30 deg. Period: 89.10 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1981 June 3 - .
14:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1274 - .
Payload: Yantar-2K s/n 942. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1981-07-03 . USAF Sat Cat: 12495 . COSPAR: 1981-052A. Apogee: 291 km (180 mi). Perigee: 144 km (89 mi). Inclination: 67.20 deg. Period: 88.90 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 June 16 - .
07:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1276 - .
Payload: Zenit-4MKT no. 18. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1981-06-29 . USAF Sat Cat: 12517 . COSPAR: 1981-055A. Apogee: 233 km (144 mi). Perigee: 211 km (131 mi). Inclination: 82.40 deg. Period: 88.90 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1981 June 17 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1277 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-07-01 . USAF Sat Cat: 12520 . COSPAR: 1981-056A. Apogee: 373 km (231 mi). Perigee: 204 km (126 mi). Inclination: 70.40 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1981 June 19 - .
19:37 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1278 - .
Payload: Oko #21. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2000-09-02 . USAF Sat Cat: 12547 . COSPAR: 1981-058A. Apogee: 37,962 km (23,588 mi). Perigee: 2,452 km (1,523 mi). Inclination: 67.00 deg. Period: 719.00 min. Covered Oko constellation plane 3 - 357 degree longitude of ascending node..
1981 July 1 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1279 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-07-15 . USAF Sat Cat: 12571 . COSPAR: 1981-062A. Apogee: 364 km (226 mi). Perigee: 206 km (128 mi). Inclination: 70.40 deg. Period: 90.20 min. Photo surveillance; returned film capsule; maneuverable..
1981 July 7 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1281 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-07-21 . USAF Sat Cat: 12583 . COSPAR: 1981-064A. Apogee: 389 km (241 mi). Perigee: 193 km (119 mi). Inclination: 72.80 deg. Period: 90.40 min. Photo surveillance; returned film capsule..
1981 July 15 - .
13:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1282 - .
Payload: Yantar-2K s/n 951. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1981-08-14 . USAF Sat Cat: 12588 . COSPAR: 1981-066A. Apogee: 332 km (206 mi). Perigee: 170 km (100 mi). Inclination: 64.90 deg. Period: 89.50 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 August 4 - .
00:13 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1285 - .
Payload: Oko #22. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 12627 . COSPAR: 1981-071A. Apogee: 36,086 km (22,422 mi). Perigee: 4,721 km (2,933 mi). Inclination: 67.20 deg. Period: 727.00 min. Replaced Cosmos 1261. Covered Oko constellation plane 6 - 116 degree longitude of ascending node..
1981 August 4 - .
08:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1286 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1982-10-16 . USAF Sat Cat: 12631 . COSPAR: 1981-072A. Apogee: 442 km (274 mi). Perigee: 430 km (260 mi). Inclination: 65.00 deg. Period: 93.20 min. Ocean monitoring..
1981 August 13 - .
16:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1296 - .
Payload: Yantar-2K s/n 943. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 31.00 days. Decay Date: 1981-09-13 . USAF Sat Cat: 12687 . COSPAR: 1981-078A. Apogee: 354 km (219 mi). Perigee: 167 km (103 mi). Inclination: 67.10 deg. Period: 89.70 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 August 18 - .
09:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1297 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 12.00 days. Decay Date: 1981-08-30 . USAF Sat Cat: 12716 . COSPAR: 1981-079A. Apogee: 360 km (220 mi). Perigee: 194 km (120 mi). Inclination: 72.80 deg. Period: 90.10 min. Photo surveillance; returned film capsule; maneuverable..
1981 August 21 - .
10:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1298 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 42.00 days. Decay Date: 1981-10-02 . USAF Sat Cat: 12776 . COSPAR: 1981-080A. Apogee: 328 km (203 mi). Perigee: 170 km (100 mi). Inclination: 64.80 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 August 24 - .
16:37 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1299 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: RVSN.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1981-09-27 . USAF Sat Cat: 12809 . COSPAR: 1981-081E. Apogee: 962 km (597 mi). Perigee: 926 km (575 mi). Inclination: 65.10 deg. Period: 103.90 min. Ocean surveillance; nuclear powered..
1981 August 24 - .
21:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1300 - .
Payload: Tselina-D no. 30. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 12785 . COSPAR: 1981-082A. Apogee: 609 km (378 mi). Perigee: 589 km (365 mi). Inclination: 82.50 deg. Period: 96.70 min.
1981 September 3 - .
18:29 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-11 no. 4 - .
Payload: KH-11 no. 4 / OPS 3984. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
Decay Date: 1984-11-23 . USAF Sat Cat: 12799 . COSPAR: 1981-085A. Apogee: 526 km (326 mi). Perigee: 244 km (151 mi). Inclination: 97.00 deg. Period: 92.30 min. KH-11 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1981 September 4 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1303 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-09-18 . USAF Sat Cat: 12801 . COSPAR: 1981-086A. Apogee: 363 km (225 mi). Perigee: 208 km (129 mi). Inclination: 70.40 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1981 September 14 - .
20:31 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1306 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: RVSN.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1982-07-16 . USAF Sat Cat: 12828 . COSPAR: 1981-089A. Apogee: 424 km (263 mi). Perigee: 168 km (104 mi). Inclination: 65.00 deg. Period: 90.40 min. Ocean monitoring; replaced Cosmos 1260..
1981 September 15 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1307 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1981-09-28 . USAF Sat Cat: 12830 . COSPAR: 1981-090A. Apogee: 390 km (240 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 90.40 min. Photo surveillance; returned film capsule..
1981 September 18 - .
09:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1309 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 13.00 days. Decay Date: 1981-10-01 . USAF Sat Cat: 12837 . COSPAR: 1981-092A. Apogee: 257 km (159 mi). Perigee: 212 km (131 mi). Inclination: 82.30 deg. Period: 89.20 min. Military topography satellite; returned film capsule; also performed mapping, geodesy..
1981 September 23 - .
08:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1310 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1989-04-03 . USAF Sat Cat: 12852 . COSPAR: 1981-095A. Apogee: 423 km (262 mi). Perigee: 394 km (244 mi). Inclination: 65.80 deg. Period: 92.70 min. Radar calibration mission..
1981 September 28 - .
21:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1311 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1983-08-28 . USAF Sat Cat: 12871 . COSPAR: 1981-097A. Apogee: 513 km (318 mi). Perigee: 462 km (287 mi). Inclination: 82.90 deg. Period: 94.30 min. Released 25 Romb radar calibration subsatellites..
1981 October 1 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1313 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-10-15 . USAF Sat Cat: 12881 . COSPAR: 1981-099A. Apogee: 286 km (177 mi). Perigee: 203 km (126 mi). Inclination: 70.40 deg. Period: 89.40 min. Photo surveillance; returned film capsule; maneuverable..
1981 October 9 - .
10:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1314 - .
Payload: Zenit-4MKT no. 19. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1981-10-22 . USAF Sat Cat: 12895 . COSPAR: 1981-101A. Apogee: 223 km (138 mi). Perigee: 209 km (129 mi). Inclination: 82.30 deg. Period: 88.90 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1981 October 13 - .
23:01 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1315 - .
Payload: Tselina-D no. 31. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2015-08-31 . USAF Sat Cat: 12903 . COSPAR: 1981-103A. Apogee: 599 km (372 mi). Perigee: 571 km (354 mi). Inclination: 81.20 deg. Period: 96.40 min. Replaced Cosmos 1154..
1981 October 15 - .
09:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1316 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-10-29 . USAF Sat Cat: 12905 . COSPAR: 1981-104A. Apogee: 381 km (236 mi). Perigee: 205 km (127 mi). Inclination: 70.30 deg. Period: 90.40 min. Photo surveillance; returned film capsule; maneuverable..
1981 October 31 - .
09:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- Chalet 3 - .
Payload: Chalet 3 (Vortex 3) / OPS 4029. Mass: 820 kg (1,800 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Chalet.
USAF Sat Cat: 12930 . COSPAR: 1981-107A. Apogee: 382 km (237 mi). Perigee: 134 km (83 mi). Inclination: 29.30 deg. Period: 90.40 min. Chalet ELINT satellite..
1981 October 31 - .
22:54 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1317 - .
Payload: Oko #23. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 12933 . COSPAR: 1981-108A. Apogee: 34,987 km (21,739 mi). Perigee: 5,425 km (3,370 mi). Inclination: 68.30 deg. Period: 719.00 min. Covered Oko constellation plane 8 - 196 degree longitude of ascending node..
1981 November 3 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1318 - .
Payload: Yantar-2K s/n 944. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 31.00 days. Decay Date: 1981-12-04 . USAF Sat Cat: 12936 . COSPAR: 1981-109A. Apogee: 353 km (219 mi). Perigee: 172 km (106 mi). Inclination: 67.10 deg. Period: 89.80 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1981 November 13 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1319 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-11-27 . USAF Sat Cat: 12954 . COSPAR: 1981-112A. Apogee: 374 km (232 mi). Perigee: 204 km (126 mi). Inclination: 70.40 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1981 December 3 - .
11:47 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1328 - .
Payload: Tselina-D no. 32. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 12987 . COSPAR: 1981-117A. Apogee: 619 km (384 mi). Perigee: 597 km (370 mi). Inclination: 82.50 deg. Period: 96.90 min.
1981 December 4 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1329 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1981-12-18 . USAF Sat Cat: 12989 . COSPAR: 1981-118A. Apogee: 273 km (169 mi). Perigee: 231 km (143 mi). Inclination: 65.00 deg. Period: 89.50 min. Photo surveillance; returned film capsule; maneuverable..
1981 December 19 - .
11:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1330 - .
Payload: Yantar-2K s/n 952. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 31.00 days. Decay Date: 1982-01-19 . USAF Sat Cat: 13008 . COSPAR: 1981-121A. Apogee: 376 km (233 mi). Perigee: 164 km (101 mi). Inclination: 70.40 deg. Period: 89.90 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 January 12 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1332 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 13.00 days. Decay Date: 1982-01-25 . USAF Sat Cat: 13031 . COSPAR: 1982-002A. Apogee: 251 km (155 mi). Perigee: 207 km (128 mi). Inclination: 82.30 deg. Period: 89.00 min. Military topography satellite; returned film capsule; also performed mapping, geodesy..
1982 January 20 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1334 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-02-03 . USAF Sat Cat: 13036 . COSPAR: 1982-005A. Apogee: 286 km (177 mi). Perigee: 191 km (118 mi). Inclination: 72.90 deg. Period: 89.30 min. Photo surveillance; returned film capsule; maneuverable..
1982 January 21 - .
19:36 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 2849 - .
Payload: KH-8 no. 52 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1982-04-30 . USAF Sat Cat: 13040 . COSPAR: 1982-006A. Apogee: 527 km (327 mi). Perigee: 137 km (85 mi). Inclination: 97.30 deg. Period: 91.20 min. Possible test of KH-12 systems. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..
1982 January 29 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1335 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1987-04-05 . USAF Sat Cat: 13042 . COSPAR: 1982-007A. Apogee: 513 km (318 mi). Perigee: 476 km (295 mi). Inclination: 74.10 deg. Period: 94.50 min. Radar calibration; replaced Cosmos 1186. Released 25 Romb radar calibration subsatellites..
1982 January 30 - .
11:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1336 - .
Payload: Yantar-2K s/n 953. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 27.00 days. Decay Date: 1982-02-26 . USAF Sat Cat: 13045 . COSPAR: 1982-008A. Apogee: 352 km (218 mi). Perigee: 170 km (100 mi). Inclination: 70.30 deg. Period: 89.70 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 February 11 - .
01:11 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1337 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1982-07-25 . USAF Sat Cat: 13061 . COSPAR: 1982-010A. Apogee: 444 km (275 mi). Perigee: 426 km (264 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring..
1982 February 16 - .
11:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1338 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-03-02 . USAF Sat Cat: 13063 . COSPAR: 1982-011A. Apogee: 376 km (233 mi). Perigee: 186 km (115 mi). Inclination: 72.80 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1982 February 19 - .
01:42 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1340 - .
Payload: Tselina-D no. 33. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 13067 . COSPAR: 1982-013A. Apogee: 604 km (375 mi). Perigee: 590 km (360 mi). Inclination: 81.20 deg. Period: 96.60 min. Replaced Cosmos 1206..
1982 March 3 - .
05:44 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1341 - .
Payload: Oko #24. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 13080 . COSPAR: 1982-016A. Apogee: 36,092 km (22,426 mi). Perigee: 4,229 km (2,627 mi). Inclination: 67.50 deg. Period: 717.10 min. Replaced Cosmos 1247. Covered Oko constellation plane 5 - 79 degree longitude of ascending node..
1982 March 4 - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Launch vehicle failed to orbit - unknown cause..
Failed Stage: U.
- Romb - .
Nation: Russia.
Agency: UNKS.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Released 25 Romb radar calibration subsatellites..
1982 March 5 - .
10:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1342 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-03-19 . USAF Sat Cat: 13084 . COSPAR: 1982-018A. Apogee: 297 km (184 mi). Perigee: 191 km (118 mi). Inclination: 72.90 deg. Period: 89.40 min. Photo surveillance; returned film capsule; maneuverable..
1982 March 6 - .
19:25 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
1982 March 17 - .
10:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1343 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-03-31 . USAF Sat Cat: 13096 . COSPAR: 1982-021A. Apogee: 284 km (176 mi). Perigee: 194 km (120 mi). Inclination: 72.80 deg. Period: 89.30 min. Photo surveillance; returned film capsule; maneuverable..
1982 March 31 - .
09:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1345 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1989-09-27 . USAF Sat Cat: 13118 . COSPAR: 1982-026A. Apogee: 369 km (229 mi). Perigee: 355 km (220 mi). Inclination: 74.00 deg. Period: 91.80 min. Investigation of the upper atmosphere and outer space. .
1982 March 31 - .
16:27 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1346 - .
Payload: Tselina-D no. 34. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2017-12-17 . USAF Sat Cat: 13120 . COSPAR: 1982-027A. Apogee: 602 km (374 mi). Perigee: 572 km (355 mi). Inclination: 81.20 deg. Period: 96.40 min. Replaced Cosmos 1222..
1982 April 2 - .
10:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1347 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 49.00 days. Decay Date: 1982-05-21 . USAF Sat Cat: 13122 . COSPAR: 1982-028A. Apogee: 337 km (209 mi). Perigee: 172 km (106 mi). Inclination: 70.40 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 April 7 - .
13:42 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1348 - .
Payload: Oko #25. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 13124 . COSPAR: 1982-029A. Apogee: 35,126 km (21,826 mi). Perigee: 5,269 km (3,273 mi). Inclination: 68.40 deg. Period: 718.60 min. Replaced Cosmos 1172. Covered Oko constellation plane 9 - 236 degree longitude of ascending node..
1982 April 15 - .
14:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1350 - .
Payload: Yantar-2K s/n 978. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 31.00 days. Decay Date: 1982-05-16 . USAF Sat Cat: 13134 . COSPAR: 1982-032A. Apogee: 355 km (220 mi). Perigee: 172 km (106 mi). Inclination: 67.10 deg. Period: 89.80 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 April 21 - .
01:40 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1351 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1983-03-14 . USAF Sat Cat: 13142 . COSPAR: 1982-034A. Apogee: 548 km (340 mi). Perigee: 348 km (216 mi). Inclination: 50.70 deg. Period: 93.60 min. Released 25 Romb radar calibration subsatellites..
1982 April 21 - .
09:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1352 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-05-05 . USAF Sat Cat: 13144 . COSPAR: 1982-035A. Apogee: 364 km (226 mi). Perigee: 204 km (126 mi). Inclination: 70.40 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1982 April 23 - .
09:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1353 - .
Payload: Zenit-4MKT no. 20. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1982-05-06 . USAF Sat Cat: 13146 . COSPAR: 1982-036A. Apogee: 238 km (147 mi). Perigee: 207 km (128 mi). Inclination: 82.40 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1982 April 29 - .
09:55 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1355 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1984-03-07 . USAF Sat Cat: 13150 . COSPAR: 1982-038A. Apogee: 295 km (183 mi). Perigee: 277 km (172 mi). Inclination: 65.00 deg. Period: 90.20 min. Ocean monitoring..
1982 May 5 - .
08:01 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1356 - .
Payload: Tselina-D no. 35. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 13153 . COSPAR: 1982-039A. Apogee: 612 km (380 mi). Perigee: 587 km (364 mi). Inclination: 81.20 deg. Period: 96.70 min. Replaced Cosmos 1184..
1982 May 11 - .
18:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-9 no. 17 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1982-12-05 . USAF Sat Cat: 13170 . COSPAR: 1982-041A. Apogee: 262 km (162 mi). Perigee: 177 km (109 mi). Inclination: 96.40 deg. Period: 88.90 min. KH-9 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
- OPS 6553 - .
Payload: SSF-D No. 4. Mass: 60 kg (132 lb). Nation: USA.
Agency: CIA,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 13172 . COSPAR: 1982-041C. Apogee: 707 km (439 mi). Perigee: 701 km (435 mi). Inclination: 96.00 deg. Period: 98.90 min. Radar monitoring; may or may not have existed!!!..
1982 May 14 - .
19:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1365 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1982-10-19 . USAF Sat Cat: 13593 . COSPAR: 1982-043C. Apogee: 979 km (608 mi). Perigee: 881 km (547 mi). Inclination: 65.10 deg. Period: 103.60 min. Ocean surveillance; nuclear powered..
1982 May 20 - .
13:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1367 - .
Payload: Oko #26. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 13205 . COSPAR: 1982-045A. Apogee: 35,764 km (22,222 mi). Perigee: 4,640 km (2,880 mi). Inclination: 67.90 deg. Period: 718.80 min. Covered Oko constellation plane 1 - 276 degree longitude of ascending node..
1982 May 21 - .
12:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1368 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1982-06-03 . USAF Sat Cat: 13208 . COSPAR: 1982-046A. Apogee: 338 km (210 mi). Perigee: 204 km (126 mi). Inclination: 70.40 deg. Period: 89.90 min. Photo surveillance; returned film capsule; maneuverable..
1982 May 28 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1370 - .
Payload: Yantar-1KFT no. 2. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 44.00 days. Decay Date: 1982-07-11 . USAF Sat Cat: 13219 . COSPAR: 1982-049A. Apogee: 273 km (169 mi). Perigee: 195 km (121 mi). Inclination: 64.90 deg. Period: 89.20 min. Military topographic / cartographic satellite..
1982 June 1 - .
13:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1372 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1982-09-09 . USAF Sat Cat: 13411 . COSPAR: 1982-052B. Apogee: 966 km (600 mi). Perigee: 919 km (571 mi). Inclination: 64.90 deg. Period: 103.90 min. Ocean surveillance; nuclear powered..
1982 June 2 - .
12:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1373 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-06-16 . USAF Sat Cat: 13244 . COSPAR: 1982-053A. Apogee: 347 km (215 mi). Perigee: 210 km (130 mi). Inclination: 70.40 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1982 June 8 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1377 - .
Payload: Yantar-4K1 s/n 215. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 44.00 days. Decay Date: 1982-07-22 . USAF Sat Cat: 13265 . COSPAR: 1982-057A. Apogee: 363 km (225 mi). Perigee: 173 km (107 mi). Inclination: 64.90 deg. Period: 89.90 min. Photo surveillance; 2 small film capsules recovered in course of flight and main reentry capsule with remaining film, camera, and computer systems at end of flight..
1982 June 10 - .
17:37 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1378 - .
Payload: Tselina-D no. 36. Mass: 2,200 kg (4,800 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 13271 . COSPAR: 1982-059A. Apogee: 618 km (384 mi). Perigee: 593 km (368 mi). Inclination: 82.50 deg. Period: 96.80 min.
1982 June 18 - .
13:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1381 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Decay Date: 1982-07-01 . USAF Sat Cat: 13283 . COSPAR: 1982-062A. Apogee: 374 km (232 mi). Perigee: 199 km (123 mi). Inclination: 70.40 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1982 June 25 - .
02:28 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1382 - .
Payload: Oko #27. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 13295 . COSPAR: 1982-064A. Apogee: 34,865 km (21,664 mi). Perigee: 5,465 km (3,395 mi). Inclination: 68.00 deg. Period: 717.30 min. Replaced Cosmos 1223. Covered Oko constellation plane 7 - 154 degree longitude of ascending node..
1982 June 30 - .
15:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1384 - .
Payload: Yantar-2K s/n 954. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1982-07-30 . USAF Sat Cat: 13303 . COSPAR: 1982-067A. Apogee: 353 km (219 mi). Perigee: 168 km (104 mi). Inclination: 67.20 deg. Period: 89.70 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 July 13 - .
08:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1387 - .
Payload: Zenit-4MKT no. 21. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1982-07-26 . USAF Sat Cat: 13365 . COSPAR: 1982-071A. Apogee: 229 km (142 mi). Perigee: 201 km (124 mi). Inclination: 82.30 deg. Period: 88.80 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1982 July 27 - .
12:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1396 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-08-10 . USAF Sat Cat: 13391 . COSPAR: 1982-075A. Apogee: 294 km (182 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 89.40 min. Photo surveillance; returned film capsule; maneuverable..
1982 July 29 - .
19:40 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1397 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1983-05-18 . USAF Sat Cat: 13394 . COSPAR: 1982-076A. Apogee: 539 km (334 mi). Perigee: 343 km (213 mi). Inclination: 50.70 deg. Period: 93.40 min. Released 25 Romb radar calibration subsatellites..
1982 August 3 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1398 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MT.
Duration: 10.00 days. Decay Date: 1982-08-13 . USAF Sat Cat: 13396 . COSPAR: 1982-077A. Apogee: 231 km (143 mi). Perigee: 211 km (131 mi). Inclination: 82.40 deg. Period: 88.90 min. Military topography satellite; returned film capsule; also performed mapping, geodesy..
1982 August 4 - .
11:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1399 - .
Payload: Yantar-4K1 s/n 216. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 43.00 days. Decay Date: 1982-09-16 . USAF Sat Cat: 13399 . COSPAR: 1982-078A. Apogee: 344 km (213 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 August 5 - .
06:56 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1400 - .
Payload: Tselina-D no. 37. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2014-09-13 . USAF Sat Cat: 13402 . COSPAR: 1982-079A. Apogee: 590 km (360 mi). Perigee: 575 km (357 mi). Inclination: 81.20 deg. Period: 96.30 min. Replaced Cosmos 1315..
1982 August 30 - .
10:06 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1402 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1983-01-23 . USAF Sat Cat: 13441 . COSPAR: 1982-084A. Apogee: 266 km (165 mi). Perigee: 250 km (150 mi). Inclination: 65.00 deg. Period: 89.60 min. Ocean surveillance; nuclear powered..
1982 September 1 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1403 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-09-15 . USAF Sat Cat: 13448 . COSPAR: 1982-085A. Apogee: 353 km (219 mi). Perigee: 205 km (127 mi). Inclination: 70.40 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1982 September 1 - .
11:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1404 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-09-15 . USAF Sat Cat: 13449 . COSPAR: 1982-086A. Apogee: 354 km (219 mi). Perigee: 196 km (121 mi). Inclination: 72.80 deg. Period: 90.00 min. Photo surveillance; returned film capsule..
1982 September 4 - .
17:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1405 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1984-01-31 . USAF Sat Cat: 13508 . COSPAR: 1982-088A. Apogee: 443 km (275 mi). Perigee: 425 km (264 mi). Inclination: 65.00 deg. Period: 93.30 min. Ocean monitoring..
1982 September 8 - .
10:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
Launch Pad: LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1406 - .
Payload: Zenit-4MKT no. 22. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1982-09-21 . USAF Sat Cat: 13519 . COSPAR: 1982-089A. Apogee: 227 km (141 mi). Perigee: 208 km (129 mi). Inclination: 82.30 deg. Period: 88.80 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1982 September 9 - .
07:19 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 4 - .
Payload: FSW-0 No. 04. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 5.00 days. Decay Date: 1982-09-21 . USAF Sat Cat: 13521 . COSPAR: 1982-090A. Apogee: 392 km (243 mi). Perigee: 172 km (106 mi). Inclination: 63.00 deg. Period: 90.20 min. Photo surveillance; film capsule recovered 14 September..
1982 September 15 - .
15:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1407 - .
Payload: Yantar-2K s/n 955. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 31.00 days. Decay Date: 1982-10-16 . USAF Sat Cat: 13546 . COSPAR: 1982-091A. Apogee: 309 km (192 mi). Perigee: 169 km (105 mi). Inclination: 67.20 deg. Period: 89.30 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 September 16 - .
04:55 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1408 - .
Payload: Tselina-D no. 38. Mass: 2,200 kg (4,800 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 13552 . COSPAR: 1982-092A. Apogee: 617 km (383 mi). Perigee: 587 km (364 mi). Inclination: 82.60 deg. Period: 96.70 min. Replaced Cosmos 1378..
1982 September 22 - .
06:23 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1409 - .
Payload: Oko #28. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2009-06-08 . USAF Sat Cat: 13585 . COSPAR: 1982-095A. Apogee: 36,670 km (22,780 mi). Perigee: 3,715 km (2,308 mi). Inclination: 66.70 deg. Period: 718.40 min. Replaced Cosmos 1217. Covered Oko constellation plane 2 - 317 degree longitude of ascending node..
1982 September 30 - .
11:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1411 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-10-14 . USAF Sat Cat: 13597 . COSPAR: 1982-098A. Apogee: 354 km (219 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 90.00 min. Photo surveillance; returned film capsule; maneuverable..
1982 October 2 - .
00:01 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1412 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1982-12-04 . USAF Sat Cat: 13645 . COSPAR: 1982-099B. Apogee: 998 km (620 mi). Perigee: 886 km (550 mi). Inclination: 64.80 deg. Period: 103.90 min. Ocean surveillance; nuclear powered..
1982 October 14 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1416 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-10-28 . USAF Sat Cat: 13611 . COSPAR: 1982-101A. Apogee: 278 km (172 mi). Perigee: 231 km (143 mi). Inclination: 70.40 deg. Period: 89.60 min. Photo surveillance; returned film capsule; maneuverable..
1982 October 21 - .
14:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1418 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1983-09-30 . USAF Sat Cat: 13627 . COSPAR: 1982-104A. Apogee: 414 km (257 mi). Perigee: 370 km (220 mi). Inclination: 50.70 deg. Period: 92.40 min. Radar calibration mission..
1982 November 2 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1419 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-11-16 . USAF Sat Cat: 13641 . COSPAR: 1982-108A. Apogee: 264 km (164 mi). Perigee: 206 km (128 mi). Inclination: 70.30 deg. Period: 89.20 min. Photo surveillance; returned film capsule; maneuverable..
1982 November 17 - .
21:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan IIID.
- KH-11 no. 5 - .
Payload: KH-11 no. 5 / OPS 9627. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
Decay Date: 1985-08-13 . USAF Sat Cat: 13659 . COSPAR: 1982-111A. Apogee: 520 km (320 mi). Perigee: 280 km (170 mi). Inclination: 97.00 deg. Period: 92.60 min. KH-11 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1982 November 18 - .
09:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1421 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-12-02 . USAF Sat Cat: 13661 . COSPAR: 1982-112A. Apogee: 259 km (160 mi). Perigee: 206 km (128 mi). Inclination: 70.30 deg. Period: 89.20 min. Photo surveillance; returned film capsule; maneuverable..
1982 December 3 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1422 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1982-12-17 . USAF Sat Cat: 13677 . COSPAR: 1982-114A. Apogee: 288 km (178 mi). Perigee: 228 km (141 mi). Inclination: 72.90 deg. Period: 89.70 min. Photo surveillance; returned film capsule; maneuverable..
1982 December 16 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1424 - .
Payload: Yantar-4K1 s/n 217. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 43.00 days. Decay Date: 1983-01-28 . USAF Sat Cat: 13725 . COSPAR: 1982-117A. Apogee: 349 km (216 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1982 December 23 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Cosmos 1425 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-01-06 . USAF Sat Cat: 13739 . COSPAR: 1982-119A. Apogee: 352 km (218 mi). Perigee: 220 km (130 mi). Inclination: 70.00 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1982 December 28 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1426 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 69.00 days. Decay Date: 1983-03-05 . USAF Sat Cat: 13745 . COSPAR: 1982-120A. Apogee: 384 km (238 mi). Perigee: 200 km (120 mi). Inclination: 50.60 deg. Period: 90.40 min. Photo/digital surveillance..
1982 December 29 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1427 - .
Mass: 2,200 kg (4,800 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1989-10-05 . USAF Sat Cat: 13750 . COSPAR: 1982-121A. Apogee: 351 km (218 mi). Perigee: 319 km (198 mi). Inclination: 65.80 deg. Period: 91.20 min. Radar calibration mission..
1983 January 20 - .
17:26 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1437 - .
Payload: Tselina-D no. 39. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 13770 . COSPAR: 1983-003A. Apogee: 604 km (375 mi). Perigee: 581 km (361 mi). Inclination: 81.20 deg. Period: 96.50 min.
1983 January 25 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Launch vehicle failed to orbit - unknown cause..
Failed Stage: U.
- Romb - .
Nation: Russia.
Agency: UNKS.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Carried Romb radar calibration subsatellites..
1983 January 27 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1438 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 11.00 days. Decay Date: 1983-02-07 . USAF Sat Cat: 13779 . COSPAR: 1983-005A. Apogee: 226 km (140 mi). Perigee: 205 km (127 mi). Inclination: 70.40 deg. Period: 88.80 min. Photo surveillance; returned film capsule; maneuverable..
1983 February 6 - .
11:31 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1439 - .
Payload: Yantar-2K s/n 956. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 16.00 days. Decay Date: 1983-02-22 . USAF Sat Cat: 13784 . COSPAR: 1983-007A. Apogee: 344 km (213 mi). Perigee: 168 km (104 mi). Inclination: 70.40 deg. Period: 89.60 min. Area survey photo reconnaissance; film capsule; also performed earth resources tasks. Returned in less than usual 30 day full duration..
1983 February 9 - .
13:47 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas H.
- NOSS 4 - .
Payload: PARCAE 5 / OPS 0252. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 13791 . COSPAR: 1983-008A. Apogee: 1,186 km (736 mi). Perigee: 1,063 km (660 mi). Inclination: 63.40 deg. Period: 107.80 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- SSC - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 13874 . COSPAR: 1983-008H. Apogee: 1,173 km (728 mi). Perigee: 1,043 km (648 mi). Inclination: 63.50 deg. Period: 107.40 min. Released from NOSS 4..
- SSD (NOSS 4) - .
Payload: NOSS-Subsat 4-4. Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 13834 . COSPAR: 1983-008C. Apogee: 1,419 km (881 mi). Perigee: 796 km (494 mi). Inclination: 63.40 deg. Period: 107.42 min. Released from NOSS 4. .
- SSA - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 13844 . COSPAR: 1983-008E. Apogee: 1,166 km (724 mi). Perigee: 1,051 km (653 mi). Inclination: 63.40 deg. Period: 107.40 min. Released from NOSS 4..
- SSA (NOSS 4) - .
Payload: NOSS-Subsat 4-1 / OPS 0252 DEB. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 13835 . COSPAR: 1983-008D. Apogee: 1,164 km (723 mi). Perigee: 1,051 km (653 mi). Inclination: 63.50 deg. Period: 107.40 min. Released from NOSS 4..
- SSB - .
Payload: SSU. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 13845 . COSPAR: 1983-008F. Apogee: 1,489 km (925 mi). Perigee: 733 km (456 mi). Inclination: 63.40 deg. Period: 107.42 min.
1983 February 16 - .
10:03 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1441 - .
Payload: Tselina-D no. 40. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2014-11-08 . USAF Sat Cat: 13818 . COSPAR: 1983-010A. Apogee: 587 km (364 mi). Perigee: 578 km (359 mi). Inclination: 81.10 deg. Period: 96.30 min.
1983 February 25 - .
12:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1442 - .
Payload: Yantar-4K1 s/n 248. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 45.00 days. Decay Date: 1983-04-11 . USAF Sat Cat: 13850 . COSPAR: 1983-012A. Apogee: 339 km (210 mi). Perigee: 169 km (105 mi). Inclination: 67.10 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1983 March 2 - .
10:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1444 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-03-16 . USAF Sat Cat: 13870 . COSPAR: 1983-014A. Apogee: 384 km (238 mi). Perigee: 189 km (117 mi). Inclination: 72.90 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1983 March 16 - .
08:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Cosmos 1446 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-03-30 . USAF Sat Cat: 13886 . COSPAR: 1983-018A. Apogee: 343 km (213 mi). Perigee: 223 km (138 mi). Inclination: 69.90 deg. Period: 90.20 min. Photo surveillance; returned film capsule; maneuverable..
1983 March 31 - .
10:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1449 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 15.00 days. Decay Date: 1983-04-15 . USAF Sat Cat: 13955 . COSPAR: 1983-024A. Apogee: 372 km (231 mi). Perigee: 197 km (122 mi). Inclination: 72.70 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1983 April 6 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
Launch Pad: LC132?/pad?.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1450 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1990-05-30 . USAF Sat Cat: 13972 . COSPAR: 1983-027A. Apogee: 385 km (239 mi). Perigee: 357 km (221 mi). Inclination: 65.80 deg. Period: 92.00 min. Possibly ASAT related. Radar calibration mission..
1983 April 8 - .
08:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1451 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-04-22 . USAF Sat Cat: 13975 . COSPAR: 1983-029A. Apogee: 232 km (144 mi). Perigee: 178 km (110 mi). Inclination: 82.40 deg. Period: 88.60 min. Photo surveillance; returned film capsule; maneuverable. First launch from LC43/4 since on-pad explosion in March 1980..
1983 April 15 - .
18:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 2925 - .
Payload: KH-8 no. 53 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1983-08-21 . USAF Sat Cat: 14001 . COSPAR: 1983-032A. Apogee: 305 km (189 mi). Perigee: 131 km (81 mi). Inclination: 96.50 deg. Period: 88.90 min. KH-8 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1983 April 19 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1453 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1989-05-08 . USAF Sat Cat: 14006 . COSPAR: 1983-034A. Apogee: 466 km (289 mi). Perigee: 434 km (269 mi). Inclination: 74.00 deg. Period: 93.60 min. Released 25 Romb radar calibration subsatellites..
1983 April 22 - .
14:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1454 - .
Payload: Yantar-2K s/n 957. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1983-05-22 . USAF Sat Cat: 14017 . COSPAR: 1983-036A. Apogee: 345 km (214 mi). Perigee: 167 km (103 mi). Inclination: 67.10 deg. Period: 89.70 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1983 April 23 - .
14:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1455 - .
Payload: Tselina-D no. 41. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 14032 . COSPAR: 1983-037A. Apogee: 617 km (383 mi). Perigee: 592 km (367 mi). Inclination: 82.50 deg. Period: 96.80 min.
1983 April 25 - .
19:34 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1456 - .
Payload: Oko #29. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 1998-05-11 . USAF Sat Cat: 14034 . COSPAR: 1983-038A. Apogee: 38,464 km (23,900 mi). Perigee: 1,871 km (1,162 mi). Inclination: 66.60 deg. Period: 717.40 min. Replaced Cosmos 1191. Covered Oko constellation plane 4 - 37 degree longitude of ascending node..
1983 April 26 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1457 - .
Payload: Yantar-4K1 s/n 214. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 45.00 days. Decay Date: 1983-06-08 . USAF Sat Cat: 14039 . COSPAR: 1983-039A. Apogee: 354 km (219 mi). Perigee: 164 km (101 mi). Inclination: 70.40 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1983 April 28 - .
08:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
Launch Pad: LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1458 - .
Payload: Zenit-4MKT no. 23. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1983-05-11 . USAF Sat Cat: 14044 . COSPAR: 1983-040A. Apogee: 243 km (150 mi). Perigee: 208 km (129 mi). Inclination: 82.30 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1983 May 6 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1460 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-05-20 . USAF Sat Cat: 14058 . COSPAR: 1983-043A. Apogee: 344 km (213 mi). Perigee: 207 km (128 mi). Inclination: 70.30 deg. Period: 90.00 min. Photo surveillance; returned film capsule..
1983 May 7 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1461 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1985-05-31 . USAF Sat Cat: 14064 . COSPAR: 1983-044A. Apogee: 803 km (498 mi). Perigee: 574 km (356 mi). Inclination: 65.00 deg. Period: 98.50 min. Ocean monitoring..
1983 May 19 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1463 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1993-01-24 . USAF Sat Cat: 14075 . COSPAR: 1983-046A. Apogee: 602 km (374 mi). Perigee: 254 km (157 mi). Inclination: 82.80 deg. Period: 93.10 min. Radar calibration mission..
1983 May 26 - .
05:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1465 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1985-01-23 . USAF Sat Cat: 14087 . COSPAR: 1983-049A. Apogee: 541 km (336 mi). Perigee: 349 km (216 mi). Inclination: 50.70 deg. Period: 93.50 min. Released 25 Romb radar calibration subsatellites..
1983 May 26 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1466 - .
Payload: Yantar-4K1 s/n 250. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 41.00 days. Decay Date: 1983-07-06 . USAF Sat Cat: 14089 . COSPAR: 1983-050A. Apogee: 315 km (195 mi). Perigee: 166 km (103 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1983 May 31 - .
11:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1467 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 12.00 days. Decay Date: 1983-06-12 . USAF Sat Cat: 14100 . COSPAR: 1983-052A. Apogee: 361 km (224 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1983 June 9 - .
23:23 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas H.
- NOSS 5 - .
Payload: PARCAE 6 / OPS 6432. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 14112 . COSPAR: 1983-056A. Apogee: 1,167 km (725 mi). Perigee: 1,049 km (651 mi). Inclination: 63.40 deg. Period: 107.40 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- GB1 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 14143 . COSPAR: 1983-056C. Apogee: 1,167 km (725 mi). Perigee: 1,049 km (651 mi). Inclination: 63.40 deg. Period: 107.40 min. Deployed from NOSS 5..
- GB2 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 14144 . COSPAR: 1983-056D. Apogee: 1,167 km (725 mi). Perigee: 1,049 km (651 mi). Inclination: 63.40 deg. Period: 107.40 min. Deployed from NOSS 5..
- GB3 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 14180 . COSPAR: 1983-056G. Apogee: 1,166 km (724 mi). Perigee: 1,049 km (651 mi). Inclination: 63.40 deg. Period: 107.40 min.
1983 June 14 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1469 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 10.00 days. Decay Date: 1983-06-24 . USAF Sat Cat: 14123 . COSPAR: 1983-057A. Apogee: 357 km (221 mi). Perigee: 193 km (119 mi). Inclination: 72.80 deg. Period: 90.00 min. Photo surveillance; returned film capsule; maneuverable..
1983 June 20 - .
18:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 34D.
- KH-9 no. 18 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1984-03-21 . USAF Sat Cat: 14137 . COSPAR: 1983-060A. Apogee: 259 km (160 mi). Perigee: 159 km (98 mi). Inclination: 96.50 deg. Period: 88.80 min. KH-9 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
- OPS 3899 - .
Payload: SSF-C No. 7. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 14139 . COSPAR: 1983-060C. Apogee: 1,296 km (805 mi). Perigee: 1,278 km (794 mi). Inclination: 96.60 deg. Period: 111.31 min. ABM monitoring; may or may not have existed!!!. .
1983 June 22 - .
23:58 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1470 - .
Payload: Tselina-D no. 42. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 14147 . COSPAR: 1983-061A. Apogee: 626 km (388 mi). Perigee: 596 km (370 mi). Inclination: 82.50 deg. Period: 96.90 min.
1983 June 28 - .
15:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1471 - .
Payload: Yantar-2K s/n 958. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 30.00 days. Decay Date: 1983-07-28 . USAF Sat Cat: 14156 . COSPAR: 1983-064A. Apogee: 343 km (213 mi). Perigee: 170 km (100 mi). Inclination: 67.10 deg. Period: 89.70 min. Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission. Final Yantar-2K mission..
1983 July 8 - .
19:21 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1481 - .
Payload: Oko #30. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 14182 . COSPAR: 1983-070A. Apogee: 36,924 km (22,943 mi). Perigee: 2,912 km (1,809 mi). Inclination: 67.30 deg. Period: 707.30 min. Intended to replace Cosmos 1285; last stage exploded. Was intended to cover Oko constellation plane 6 - 118 degree longitude of ascending node..
1983 July 26 - .
12:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1485 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-08-09 . USAF Sat Cat: 14210 . COSPAR: 1983-076A. Apogee: 366 km (227 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1983 July 31 - .
15:41 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 34B.
- Jumpseat 7 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Jumpseat.
USAF Sat Cat: 14237 . COSPAR: 1983-078A. Apogee: 39,321 km (24,432 mi). Perigee: 1,028 km (638 mi). Inclination: 63.40 deg. Period: 717.10 min. Or Quasar.
1983 August 9 - .
11:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1488 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-08-23 . USAF Sat Cat: 14251 . COSPAR: 1983-082A. Apogee: 368 km (228 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1983 August 10 - .
13:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1489 - .
Payload: Yantar-4K1 s/n 252. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 44.00 days. Decay Date: 1983-09-23 . USAF Sat Cat: 14256 . COSPAR: 1983-083A. Apogee: 299 km (185 mi). Perigee: 173 km (107 mi). Inclination: 64.70 deg. Period: 89.20 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1983 August 19 - .
06:00 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 5 - .
Payload: FSW-0 No. 05. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 5.00 days. Decay Date: 1983-09-03 . USAF Sat Cat: 14288 . COSPAR: 1983-086A. Apogee: 493 km (306 mi). Perigee: 170 km (100 mi). Inclination: 63.30 deg. Period: 91.20 min. Photo surveillance; film capsule recovered 24 August..
1983 August 23 - .
11:05 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1493 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-09-06 . USAF Sat Cat: 14299 . COSPAR: 1983-087A. Apogee: 362 km (224 mi). Perigee: 188 km (116 mi). Inclination: 72.90 deg. Period: 90.00 min. Photo surveillance; returned film capsule..
1983 August 31 - .
06:30 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1494 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1985-09-26 . USAF Sat Cat: 14316 . COSPAR: 1983-091A. Apogee: 413 km (256 mi). Perigee: 309 km (192 mi). Inclination: 50.70 deg. Period: 91.80 min. Released 25 Romb radar calibration subsatellites..
1983 September 3 - .
10:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1495 - .
Payload: Zenit-4MKT no. 24. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1983-09-16 . USAF Sat Cat: 14320 . COSPAR: 1983-092A. Apogee: 221 km (137 mi). Perigee: 205 km (127 mi). Inclination: 82.30 deg. Period: 88.80 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1983 September 7 - .
13:24 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1496 - .
Payload: Yantar-4K1 s/n 251. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 42.00 days. Decay Date: 1983-10-19 . USAF Sat Cat: 14326 . COSPAR: 1983-093A. Apogee: 338 km (210 mi). Perigee: 167 km (103 mi). Inclination: 67.20 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1983 September 9 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1497 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-09-23 . USAF Sat Cat: 14330 . COSPAR: 1983-095A. Apogee: 372 km (231 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1983 September 17 - .
11:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1499 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-10-01 . USAF Sat Cat: 14339 . COSPAR: 1983-097A. Apogee: 367 km (228 mi). Perigee: 193 km (119 mi). Inclination: 72.80 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1983 September 30 - .
11:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1501 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1989-05-26 . USAF Sat Cat: 14380 . COSPAR: 1983-101A. Apogee: 472 km (293 mi). Perigee: 437 km (271 mi). Inclination: 82.90 deg. Period: 93.70 min. Released 25 Romb radar calibration subsatellites..
1983 October 5 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1502 - .
Mass: 750 kg (1,650 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1985-08-29 . USAF Sat Cat: 14395 . COSPAR: 1983-102A. Apogee: 409 km (254 mi). Perigee: 366 km (227 mi). Inclination: 65.80 deg. Period: 92.30 min. Possibly ASAT related. Radar calibration mission..
1983 October 14 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1504 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 53.00 days. Decay Date: 1983-12-06 . USAF Sat Cat: 14403 . COSPAR: 1983-104A. Apogee: 304 km (188 mi). Perigee: 172 km (106 mi). Inclination: 64.90 deg. Period: 89.30 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1983 October 21 - .
12:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1505 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-11-04 . USAF Sat Cat: 14425 . COSPAR: 1983-107A. Apogee: 337 km (209 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 89.80 min. Photo surveillance; returned film capsule..
1983 October 29 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1507 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1987-08-19 . USAF Sat Cat: 14455 . COSPAR: 1983-110A. Apogee: 325 km (201 mi). Perigee: 298 km (185 mi). Inclination: 65.00 deg. Period: 90.80 min. Ocean monitoring..
1983 November 11 - .
12:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1508 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 14483 . COSPAR: 1983-111A. Apogee: 1,640 km (1,010 mi). Perigee: 392 km (243 mi). Inclination: 82.90 deg. Period: 105.50 min. Radar calibration mission..
1983 November 17 - .
12:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1509 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-12-01 . USAF Sat Cat: 14490 . COSPAR: 1983-112A. Apogee: 280 km (170 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 89.20 min. Photo surveillance; returned film capsule; maneuverable..
1983 November 30 - .
13:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1511 - .
Payload: Yantar-4K1 s/n 249. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 44.00 days. Decay Date: 1984-01-13 . USAF Sat Cat: 14530 . COSPAR: 1983-117A. Apogee: 332 km (206 mi). Perigee: 182 km (113 mi). Inclination: 67.10 deg. Period: 89.60 min.
Photo surveillance; 2 small film capsules recovered in course of flight and main reentry capsule with remaining film, camera, and computer systems at end of flight. Final flight of the Yantar-2K/Yantar-4K1 series. All 12 Yantar-4K1 flights were completely successful.
1983 December 7 - .
12:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1512 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1983-12-21 . USAF Sat Cat: 14542 . COSPAR: 1983-119A. Apogee: 380 km (230 mi). Perigee: 192 km (119 mi). Inclination: 72.80 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1983 December 15 - .
12:25 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1515 - .
Payload: Tselina-D no. 43. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 14551 . COSPAR: 1983-122A. Apogee: 620 km (380 mi). Perigee: 595 km (369 mi). Inclination: 82.50 deg. Period: 96.90 min.
1983 December 27 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1516 - .
Payload: Yantar-1KFT no. 3. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 49.00 days. Decay Date: 1984-02-09 . USAF Sat Cat: 14583 . COSPAR: 1983-124A. Apogee: 274 km (170 mi). Perigee: 194 km (120 mi). Inclination: 64.90 deg. Period: 89.20 min. Military topographic / cartographic satellite..
1983 December 28 - .
03:48 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1518 - .
Payload: Oko #31. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 1998-09-19 . USAF Sat Cat: 14587 . COSPAR: 1983-126A. Apogee: 38,145 km (23,702 mi). Perigee: 2,019 km (1,254 mi). Inclination: 66.90 deg. Period: 713.90 min. Replaced Cosmos 1341. Covered Oko constellation plane 5 - 72 degree longitude of ascending node..
1984 January 11 - .
12:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1530 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1984-01-25 . USAF Sat Cat: 14622 . COSPAR: 1984-002A. Apogee: 362 km (224 mi). Perigee: 189 km (117 mi). Inclination: 72.90 deg. Period: 90.00 min. Photo surveillance; returned film capsule..
1984 January 13 - .
14:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1532 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 44.00 days. Decay Date: 1984-02-26 . USAF Sat Cat: 14634 . COSPAR: 1984-004A. Apogee: 357 km (221 mi). Perigee: 163 km (101 mi). Inclination: 67.10 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 January 26 - .
08:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Cosmos 1533 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1984-02-09 . USAF Sat Cat: 14666 . COSPAR: 1984-006A. Apogee: 354 km (219 mi). Perigee: 222 km (137 mi). Inclination: 70.40 deg. Period: 90.30 min. Photo surveillance; returned film capsule..
1984 January 26 - .
12:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1534 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1990-09-19 . USAF Sat Cat: 14668 . COSPAR: 1984-007A. Apogee: 334 km (207 mi). Perigee: 305 km (189 mi). Inclination: 65.80 deg. Period: 90.90 min. Radar calibration mission..
1984 January 31 - .
03:08 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 34D/Transtage.
- Chalet 4 - .
Payload: OPS 0441. Mass: 1,043 kg (2,299 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Chalet.
USAF Sat Cat: 14675 . COSPAR: 1984-009A. Apogee: 1,023 km (635 mi). Perigee: 146 km (90 mi). Inclination: 29.40 deg. Period: 96.40 min. Chalet ELINT satellite..
1984 February 5 - .
18:44 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas H.
- NOSS 6 - .
Payload: PARCAE 7 / OPS 8737. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 14690 . COSPAR: 1984-012A. Apogee: 1,172 km (728 mi). Perigee: 1,052 km (653 mi). Inclination: 63.40 deg. Period: 107.00 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- JD2 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 14729 . COSPAR: 1984-012D. Apogee: 1,172 km (728 mi). Perigee: 1,052 km (653 mi). Inclination: 63.40 deg. Period: 107.00 min. Deployed from NOSS 6..
- JD1 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 14728 . COSPAR: 1984-012C. Apogee: 1,172 km (728 mi). Perigee: 1,052 km (653 mi). Inclination: 63.40 deg. Period: 107.00 min. Deployed from NOSS 6..
- JD3 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 14795 . COSPAR: 1984-012F. Apogee: 1,172 km (728 mi). Perigee: 1,052 km (653 mi). Inclination: 63.40 deg. Period: 107.00 min.
1984 February 8 - .
09:23 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1536 - .
Payload: Tselina-D no. 44. Mass: 2,200 kg (4,800 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 14699 . COSPAR: 1984-013A. Apogee: 631 km (392 mi). Perigee: 602 km (374 mi). Inclination: 82.50 deg. Period: 97.00 min.
1984 February 28 - .
13:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1539 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 41.00 days. Decay Date: 1984-04-09 . USAF Sat Cat: 14763 . COSPAR: 1984-020A. Apogee: 338 km (210 mi). Perigee: 167 km (103 mi). Inclination: 67.20 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 March 6 - .
17:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1541 - .
Payload: Oko #32. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 14790 . COSPAR: 1984-024A. Apogee: 35,015 km (21,757 mi). Perigee: 5,297 km (3,291 mi). Inclination: 68.00 deg. Period: 716.90 min. Replaced Cosmos 1278. Covered Oko constellation plane 3 - 355 degree longitude of ascending node..
1984 March 7 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Cosmos 1542 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1984-03-21 . USAF Sat Cat: 14793 . COSPAR: 1984-025A. Apogee: 346 km (214 mi). Perigee: 223 km (138 mi). Inclination: 70.30 deg. Period: 90.20 min. Photo surveillance; returned film capsule..
1984 March 15 - .
17:05 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1544 - .
Payload: Tselina-D no. 45. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 14819 . COSPAR: 1984-027A. Apogee: 618 km (384 mi). Perigee: 591 km (367 mi). Inclination: 82.50 deg. Period: 96.80 min.
1984 March 21 - .
11:05 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1545 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 15.00 days. Decay Date: 1984-04-05 . USAF Sat Cat: 14849 . COSPAR: 1984-030A. Apogee: 367 km (228 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1984 March 29 - .
05:53 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM.
1984 April 4 - .
01:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1547 - .
Payload: Oko #33. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 14884 . COSPAR: 1984-033A. Apogee: 36,507 km (22,684 mi). Perigee: 3,819 km (2,373 mi). Inclination: 67.50 deg. Period: 717.20 min. Replaced Cosmos 1382. Covered Oko constellation plane 7 - 154 degree longitude of ascending node..
1984 April 10 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1548 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 45.00 days. Decay Date: 1984-05-25 . USAF Sat Cat: 14902 . COSPAR: 1984-036A. Apogee: 331 km (205 mi). Perigee: 165 km (102 mi). Inclination: 67.20 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 April 14 - .
16:52 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 34D/Transtage.
1984 April 17 - .
18:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan 24B.
- OPS 8424 - .
Payload: KH-8 no. 54 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-8.
Decay Date: 1984-08-13 . USAF Sat Cat: 14935 . COSPAR: 1984-039A. Apogee: 311 km (193 mi). Perigee: 127 km (78 mi). Inclination: 96.40 deg. Period: 88.90 min. KH-8 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1984 April 19 - .
11:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1549 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 14.00 days. Decay Date: 1984-05-03 . USAF Sat Cat: 14938 . COSPAR: 1984-040A. Apogee: 364 km (226 mi). Perigee: 194 km (120 mi). Inclination: 72.80 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1984 May 11 - .
13:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1551 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 12.00 days. Decay Date: 1984-05-23 . USAF Sat Cat: 14967 . COSPAR: 1984-044A. Apogee: 276 km (171 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 89.20 min. Photo surveillance; returned film capsule; maneuverable..
1984 May 14 - .
14:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1552 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 173.00 days. Decay Date: 1984-11-03 . USAF Sat Cat: 14971 . COSPAR: 1984-045A. Apogee: 320 km (190 mi). Perigee: 180 km (110 mi). Inclination: 64.90 deg. Period: 89.50 min. Photo/digital surveillance..
1984 May 22 - .
08:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1557 - .
Payload: Zenit-4MKT no. 25. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1984-06-04 . USAF Sat Cat: 14982 . COSPAR: 1984-048A. Apogee: 245 km (152 mi). Perigee: 208 km (129 mi). Inclination: 82.30 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1984 May 25 - .
11:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1558 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 44.00 days. Decay Date: 1984-07-08 . USAF Sat Cat: 14993 . COSPAR: 1984-050A. Apogee: 293 km (182 mi). Perigee: 163 km (101 mi). Inclination: 67.10 deg. Period: 89.10 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 May 30 - .
18:46 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1567 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1988-04-03 . USAF Sat Cat: 15009 . COSPAR: 1984-053A. Apogee: 369 km (229 mi). Perigee: 353 km (219 mi). Inclination: 65.00 deg. Period: 91.80 min. Ocean monitoring..
1984 June 1 - .
13:50 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1568 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 13.00 days. Decay Date: 1984-06-14 . USAF Sat Cat: 15011 . COSPAR: 1984-054A. Apogee: 365 km (226 mi). Perigee: 193 km (119 mi). Inclination: 72.90 deg. Period: 90.10 min. Photo surveillance; returned film capsule..
1984 June 6 - .
15:34 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1569 - .
Payload: Oko #34. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2001-05-07 . USAF Sat Cat: 15027 . COSPAR: 1984-055A. Apogee: 37,578 km (23,349 mi). Perigee: 2,729 km (1,695 mi). Inclination: 66.10 deg. Period: 716.80 min. Replaced Cosmos 1518. Covered Oko constellation plane 5 - 74 degree longitude of ascending node..
1984 June 19 - .
10:55 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1573 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-6U.
Duration: 9.00 days. Decay Date: 1984-06-28 . USAF Sat Cat: 15051 . COSPAR: 1984-061A. Apogee: 287 km (178 mi). Perigee: 194 km (120 mi). Inclination: 72.90 deg. Period: 89.30 min. Photo surveillance; returned film capsule; maneuverable..
1984 June 25 - .
18:43 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 34D.
- USA 2 - .
Payload: KH-9 no. 19. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1984-10-18 . USAF Sat Cat: 15063 . COSPAR: 1984-065A. Apogee: 230 km (140 mi). Perigee: 170 km (100 mi). Inclination: 96.50 deg. Period: 88.50 min. KH-9 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
- USA 3 - .
Payload: SSF-D No. 5. Mass: 60 kg (132 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
USAF Sat Cat: 15071 . COSPAR: 1984-065C. Apogee: 710 km (440 mi). Perigee: 690 km (420 mi). Inclination: 96.10 deg. Period: 98.80 min. Radar monitoring..
1984 June 26 - .
15:35 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1576 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1984-08-24 . USAF Sat Cat: 15070 . COSPAR: 1984-066A. Apogee: 348 km (216 mi). Perigee: 167 km (103 mi). Inclination: 67.10 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 June 28 - .
13:10 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1578 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1993-01-10 . USAF Sat Cat: 15080 . COSPAR: 1984-068A. Apogee: 639 km (397 mi). Perigee: 255 km (158 mi). Inclination: 50.70 deg. Period: 93.50 min. Radar calibration mission..
1984 June 29 - .
00:21 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1579 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1984-11-05 . USAF Sat Cat: 15328 . COSPAR: 1984-069C. Apogee: 970 km (600 mi). Perigee: 914 km (567 mi). Inclination: 65.10 deg. Period: 103.90 min. Ocean surveillance; nuclear powered..
1984 July 3 - .
21:31 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1581 - .
Payload: Oko #35. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 15095 . COSPAR: 1984-071A. Apogee: 36,014 km (22,378 mi). Perigee: 4,498 km (2,794 mi). Inclination: 67.80 deg. Period: 721.00 min. Replaced Cosmos 1317. Covered Oko constellation plane 8 - 194 degree longitude of ascending node..
1984 July 31 - .
12:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1585 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1984-09-28 . USAF Sat Cat: 15142 . COSPAR: 1984-077A. Apogee: 300 km (180 mi). Perigee: 172 km (106 mi). Inclination: 64.70 deg. Period: 89.20 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 August 2 - .
08:38 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1586 - .
Payload: Oko #36. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2016-01-06 . USAF Sat Cat: 15147 . COSPAR: 1984-079A. Apogee: 36,751 km (22,835 mi). Perigee: 3,607 km (2,241 mi). Inclination: 66.40 deg. Period: 717.90 min. Replaced Cosmos 1456. Covered Oko constellation plane 4 - 35 degree longitude of ascending node..
1984 August 7 - .
22:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1588 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1986-02-28 . USAF Sat Cat: 15167 . COSPAR: 1984-083A. Apogee: 347 km (215 mi). Perigee: 331 km (205 mi). Inclination: 65.00 deg. Period: 91.30 min. Ocean monitoring..
1984 September 7 - .
19:13 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1596 - .
Payload: Oko #37. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 15267 . COSPAR: 1984-096A. Apogee: 35,908 km (22,312 mi). Perigee: 4,503 km (2,798 mi). Inclination: 67.80 deg. Period: 718.90 min. Replaced Cosmos 1348. Covered Oko constellation plane 9 - 238 degree longitude of ascending node..
1984 September 12 - .
05:44 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 6 - .
Payload: FSW-0 No. 06. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 5.00 days. Decay Date: 1984-09-29 . USAF Sat Cat: 15279 . COSPAR: 1984-098A. Apogee: 398 km (247 mi). Perigee: 172 km (106 mi). Inclination: 67.90 deg. Period: 90.20 min. Photo surveillance; film capsule recovered 17 September..
1984 September 13 - .
10:25 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1597 - .
Payload: Zenit-4MKT no. 26. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1984-09-26 . USAF Sat Cat: 15287 . COSPAR: 1984-099A. Apogee: 241 km (149 mi). Perigee: 208 km (129 mi). Inclination: 82.30 deg. Period: 89.00 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1984 September 25 - .
14:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1599 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 56.00 days. Decay Date: 1984-11-20 . USAF Sat Cat: 15318 . COSPAR: 1984-102A. Apogee: 247 km (153 mi). Perigee: 164 km (101 mi). Inclination: 67.10 deg. Period: 88.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 September 27 - .
09:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1601 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1989-11-29 . USAF Sat Cat: 15326 . COSPAR: 1984-104A. Apogee: 414 km (257 mi). Perigee: 387 km (240 mi). Inclination: 65.80 deg. Period: 92.60 min. Released 25 Romb radar calibration subsatellites..
1984 September 28 - .
14:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
- Cosmos 1603 - .
Payload: Tselina-2 no. 1. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 15333 . COSPAR: 1984-106A. Apogee: 863 km (536 mi). Perigee: 832 km (516 mi). Inclination: 71.00 deg. Period: 101.90 min. First launch of new Tselina-2 ELINT satellite. .
1984 October 4 - .
19:49 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1604 - .
Payload: Oko #38. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 15350 . COSPAR: 1984-107A. Apogee: 36,050 km (22,400 mi). Perigee: 4,359 km (2,708 mi). Inclination: 67.90 deg. Period: 718.90 min. Replaced Cosmos 1367. Covered Oko constellation plane 1 - 274 degree longitude of ascending node..
1984 October 18 - .
17:46 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1606 - .
Payload: Tselina-D no. 46. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 15369 . COSPAR: 1984-111A. Apogee: 623 km (387 mi). Perigee: 592 km (367 mi). Inclination: 82.50 deg. Period: 96.90 min. Replaced Cosmos 1455..
1984 October 31 - .
12:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1607 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1985-03-28 . USAF Sat Cat: 15502 . COSPAR: 1984-112B. Apogee: 994 km (617 mi). Perigee: 908 km (564 mi). Inclination: 65.00 deg. Period: 104.10 min. Ocean surveillance; nuclear powered..
1984 November 14 - .
07:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1608 - .
Payload: Yantar-1KFT no. 4. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 33.00 days. Decay Date: 1984-12-17 . USAF Sat Cat: 15393 . COSPAR: 1984-116A. Apogee: 248 km (154 mi). Perigee: 195 km (121 mi). Inclination: 70.00 deg. Period: 88.90 min. Military topographic / cartographic satellite..
1984 November 21 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1611 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 51.00 days. Decay Date: 1985-01-11 . USAF Sat Cat: 15403 . COSPAR: 1984-119A. Apogee: 299 km (185 mi). Perigee: 172 km (106 mi). Inclination: 64.70 deg. Period: 89.20 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1984 December 4 - .
18:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 34D.
- USA 6 - .
Payload: KH-11 no. 6. Mass: 13,000 kg (28,000 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
Decay Date: 1990-12-31 . USAF Sat Cat: 15423 . COSPAR: 1984-122A. Apogee: 650 km (400 mi). Perigee: 300 km (180 mi). Inclination: 97.10 deg. Period: 93.50 min. KH-11 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1984 December 20 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1615 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1990-04-15 . USAF Sat Cat: 15446 . COSPAR: 1984-127A. Apogee: 362 km (224 mi). Perigee: 328 km (203 mi). Inclination: 65.80 deg. Period: 91.40 min. Radar calibration mission..
1984 December 22 - .
00:02 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 34D/Transtage.
- USA 7 - .
Payload: DSP Phase 2 Upgrade s/n 6R. Mass: 1,670 kg (3,680 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1994-12-31 . USAF Sat Cat: 15453 . COSPAR: 1984-129A. Apogee: 35,915 km (22,316 mi). Perigee: 35,619 km (22,132 mi). Inclination: 3.40 deg. Period: 1,445.80 min.
Reserve Phase 2 DSP ballistic missile launch detection satellite fitted with Block 14 sensors, remained in service for nearly eighteen years. Observed Scud launches during Gulf War. Positioned in geosynchronous orbit at 155 deg W in 1985-1988; 65 deg E in 1988-1991; 145 deg E in 1991-1992; 105 deg E in 1992-1993; 5 deg E in 1993-1994.
1985 January 9 - .
10:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1616 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 54.00 days. Decay Date: 1985-03-04 . USAF Sat Cat: 15467 . COSPAR: 1985-002A. Apogee: 356 km (221 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.80 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1985 January 23 - .
19:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1625 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1985-01-25 . USAF Sat Cat: 15492 . COSPAR: 1985-008A. Apogee: 390 km (240 mi). Perigee: 118 km (73 mi). Inclination: 65.00 deg. Period: 89.60 min. Ocean monitoring..
1985 January 24 - .
16:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1626 - .
Payload: Tselina-D no. 47. Mass: 2,200 kg (4,800 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 15494 . COSPAR: 1985-009A. Apogee: 618 km (384 mi). Perigee: 590 km (360 mi). Inclination: 82.50 deg. Period: 96.80 min. Replaced Cosmos 1408..
1985 January 24 - .
19:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP1.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- USA 8 - .
Payload: Orion 1. Mass: 2,500 kg (5,500 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Magnum.
USAF Sat Cat: 15543 . COSPAR: 1985-010B. Apogee: 35,800 km (22,200 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,440.00 min. New Magnum model geostationary ELINT satellite model replaced earlier Rhyolite/Aquacade. Deployed from STS-51C 24 January 1985. Boosted to geostationary orbit. As of 2003 Apr 30 located at 69.16E drifting at 0.038W degrees per day..
1985 February 21 - .
07:57 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM.
1985 February 27 - .
11:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1630 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 55.00 days. Decay Date: 1985-04-23 . USAF Sat Cat: 15582 . COSPAR: 1985-017A. Apogee: 332 km (206 mi). Perigee: 173 km (107 mi). Inclination: 64.90 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1985 February 27 - .
12:56 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1631 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1990-12-08 . USAF Sat Cat: 15584 . COSPAR: 1985-018A. Apogee: 376 km (233 mi). Perigee: 349 km (216 mi). Inclination: 65.80 deg. Period: 91.80 min. Radar calibration mission..
1985 March 5 - .
15:39 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1633 - .
Payload: Tselina-D no. 48. Mass: 2,200 kg (4,800 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 15592 . COSPAR: 1985-020A. Apogee: 613 km (380 mi). Perigee: 595 km (369 mi). Inclination: 82.50 deg. Period: 96.80 min. Replaced Cosmos 1470..
1985 March 25 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1643 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 207.00 days. Decay Date: 1985-10-18 . USAF Sat Cat: 15634 . COSPAR: 1985-026A. Apogee: 276 km (171 mi). Perigee: 182 km (113 mi). Inclination: 64.80 deg. Period: 89.10 min. Photo/digital surveillance..
1985 April 18 - .
21:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1646 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1987-11-30 . USAF Sat Cat: 15653 . COSPAR: 1985-030A. Apogee: 399 km (247 mi). Perigee: 378 km (234 mi). Inclination: 65.00 deg. Period: 92.30 min. Ocean monitoring..
1985 April 19 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1647 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 53.00 days. Decay Date: 1985-06-11 . USAF Sat Cat: 15655 . COSPAR: 1985-031A. Apogee: 321 km (199 mi). Perigee: 167 km (103 mi). Inclination: 67.10 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1985 April 29 - .
16:02 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP2.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- NUSAT-1 - .
Payload: Challenger F7 / Nusat / GLOMR [1]. Mass: 52 kg (114 lb). Nation: USA.
Agency: Weber.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: NUSAT.
Decay Date: 1986-12-15 . USAF Sat Cat: 15666 . COSPAR: 1985-034B. Apogee: 354 km (219 mi). Perigee: 345 km (214 mi). Inclination: 57.00 deg. Period: 91.50 min. Air traffic control radar calibration. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1985 May 23 - .
12:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1654 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 29.00 days. Decay Date: 1985-06-30 . USAF Sat Cat: 15734 . COSPAR: 1985-039A. Apogee: 341 km (211 mi). Perigee: 170 km (100 mi). Inclination: 64.90 deg. Period: 89.60 min. High resolution photo reconnaissance. Spacecraft failed. Blown up in orbit on June 21..
1985 May 30 - .
14:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
- Cosmos 1656 - .
Payload: Tselina-2 no. 2. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 15755 . COSPAR: 1985-042A. Apogee: 852 km (529 mi). Perigee: 802 km (498 mi). Inclination: 71.10 deg. Period: 101.40 min.
1985 June 11 - .
14:27 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1658 - .
Payload: Oko #39. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2005-11-12 . USAF Sat Cat: 15808 . COSPAR: 1985-045A. Apogee: 36,933 km (22,949 mi). Perigee: 3,366 km (2,091 mi). Inclination: 65.60 deg. Period: 716.70 min. Replaced Cosmos 1481. Covered Oko constellation plane 6 - 114 degree longitude of ascending node..
1985 June 18 - .
00:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1661 - .
Payload: Oko #40. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 15827 . COSPAR: 1985-049A. Apogee: 36,253 km (22,526 mi). Perigee: 4,148 km (2,577 mi). Inclination: 67.40 deg. Period: 718.70 min. Covered Oko constellation plane 1 - 275 degree longitude of ascending node..
1985 June 19 - .
11:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1662 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1989-11-16 . USAF Sat Cat: 15833 . COSPAR: 1985-050A. Apogee: 410 km (250 mi). Perigee: 386 km (239 mi). Inclination: 65.80 deg. Period: 92.50 min. Released 25 Romb radar calibration subsatellites..
1985 July 8 - .
23:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1666 - .
Payload: Tselina-D no. 49. Mass: 1,500 kg (3,300 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 15889 . COSPAR: 1985-058A. Apogee: 622 km (386 mi). Perigee: 595 km (369 mi). Inclination: 82.50 deg. Period: 96.90 min.
1985 August 1 - .
05:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1670 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1985-12-08 . USAF Sat Cat: 16196 . COSPAR: 1985-064C. Apogee: 1,007 km (625 mi). Perigee: 893 km (554 mi). Inclination: 64.90 deg. Period: 104.10 min. Ocean surveillance; nuclear powered..
1985 August 8 - .
10:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1673 - .
Payload: Yantar-1KFT no. 5. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 42.00 days. Decay Date: 1985-09-19 . USAF Sat Cat: 15942 . COSPAR: 1985-068A. Apogee: 271 km (168 mi). Perigee: 195 km (121 mi). Inclination: 64.80 deg. Period: 89.20 min. Military topographic / cartographic satellite..
1985 August 8 - .
11:49 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1674 - .
Payload: Tselina-D no. 50. Mass: 1,500 kg (3,300 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 15944 . COSPAR: 1985-069A. Apogee: 620 km (380 mi). Perigee: 594 km (369 mi). Inclination: 82.50 deg. Period: 96.80 min. Replaced Cosmos 1536..
1985 August 12 - .
15:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1675 - .
Payload: Oko #41. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 15952 . COSPAR: 1985-071A. Apogee: 36,967 km (22,970 mi). Perigee: 3,363 km (2,089 mi). Inclination: 67.40 deg. Period: 717.30 min. Replaced Cosmos 1581. Covered Oko constellation plane 8 - 195 degree longitude of ascending node..
1985 August 16 - .
15:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1676 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1985-10-14 . USAF Sat Cat: 15959 . COSPAR: 1985-072A. Apogee: 332 km (206 mi). Perigee: 169 km (105 mi). Inclination: 67.10 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1985 August 23 - .
22:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1677 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1985-12-14 . USAF Sat Cat: 16192 . COSPAR: 1985-075B. Apogee: 1,001 km (621 mi). Perigee: 880 km (540 mi). Inclination: 64.70 deg. Period: 103.90 min. Ocean surveillance; nuclear powered..
1985 August 28 - .
21:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 34D.
FAILURE: Stage 1 propellant feed system failure forced premature engine shutdown..
Failed Stage: 1.
- KH-11 no. 7 - .
Payload: KH-11 no. 7. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
Decay Date: 1985-08-28 . KH-11 type satellite..
1985 August 29 - .
11:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1679 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 50.00 days. Decay Date: 1985-10-18 . USAF Sat Cat: 15999 . COSPAR: 1985-078A. Apogee: 341 km (211 mi). Perigee: 172 km (106 mi). Inclination: 64.90 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1985 September 6 - .
10:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1681 - .
Payload: Zenit-4MKT no. 27. Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Program: Resurs.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4MKT.
Duration: 13.00 days. Decay Date: 1985-09-19 . USAF Sat Cat: 16018 . COSPAR: 1985-080A. Apogee: 225 km (139 mi). Perigee: 206 km (128 mi). Inclination: 82.30 deg. Period: 88.80 min. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..
1985 September 19 - .
01:32 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1682 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1986-12-31 . USAF Sat Cat: 16054 . COSPAR: 1985-082A. Apogee: 446 km (277 mi). Perigee: 341 km (211 mi). Inclination: 65.00 deg. Period: 92.40 min. Ocean surveillance..
1985 September 24 - .
01:18 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1684 - .
Payload: Oko #42. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 16064 . COSPAR: 1985-084A. Apogee: 32,715 km (20,328 mi). Perigee: 7,606 km (4,726 mi). Inclination: 67.90 deg. Period: 717.10 min. Replaced Cosmos 1586. Covered Oko constellation plane 4 - 35 degree longitude of ascending node..
1985 September 30 - .
19:23 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1687 - .
Payload: Oko #43. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 16103 . COSPAR: 1985-088A. Apogee: 36,187 km (22,485 mi). Perigee: 4,160 km (2,580 mi). Inclination: 67.70 deg. Period: 717.70 min. Replaced Cosmos 1401. Covered Oko constellation plane 2 - 314 degree longitude of ascending node..
1985 October 2 - .
06:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
Launch Pad: LC107/pad?.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1688 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1988-07-02 . USAF Sat Cat: 16107 . COSPAR: 1985-089A. Apogee: 434 km (269 mi). Perigee: 320 km (190 mi). Inclination: 50.70 deg. Period: 92.10 min. Released 25 Romb radar calibration subsatellites..
1985 October 21 - .
05:04 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 7 - .
Payload: FSW-0 No. 07. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 5.00 days. Decay Date: 1985-11-07 . USAF Sat Cat: 16177 . COSPAR: 1985-096A. Apogee: 393 km (244 mi). Perigee: 171 km (106 mi). Inclination: 63.00 deg. Period: 90.20 min. Fanhui Shi Weixing photo surveillance satellite; film capsule recovered 26 October..
1985 October 22 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 1697 - .
Payload: Tselina-2 no. 3 (Mass Model). Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 16181 . COSPAR: 1985-097A. Apogee: 853 km (530 mi). Perigee: 843 km (523 mi). Inclination: 71.00 deg. Period: 101.90 min. First launch of new Tselina-2 ELINT satellite on Zenit-2 launch vehicle..
1985 October 22 - .
20:24 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1698 - .
Payload: Oko #44. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 16183 . COSPAR: 1985-098A. Apogee: 35,412 km (22,003 mi). Perigee: 4,994 km (3,103 mi). Inclination: 67.80 deg. Period: 718.80 min. Replaced Cosmos 1541. Covered Oko constellation plane 3 - 351 degree longitude of ascending node..
1985 October 25 - .
14:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1699 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1985-12-23 . USAF Sat Cat: 16198 . COSPAR: 1985-101A. Apogee: 335 km (208 mi). Perigee: 166 km (103 mi). Inclination: 67.10 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1985 November 9 - .
08:25 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1701 - .
Payload: Oko #45. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2001-05-11 . USAF Sat Cat: 16235 . COSPAR: 1985-105A. Apogee: 36,974 km (22,974 mi). Perigee: 3,375 km (2,097 mi). Inclination: 67.20 deg. Period: 717.70 min. Replaced Cosmos 1675. Covered Oko constellation plane 8 - 192 degree longitude of ascending node..
1985 November 22 - .
22:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1703 - .
Payload: Tselina-D no. 51. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 16262 . COSPAR: 1985-108A. Apogee: 621 km (385 mi). Perigee: 596 km (370 mi). Inclination: 82.50 deg. Period: 96.90 min. Replaced Cosmos 1674..
1985 December 11 - .
14:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1706 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 60.00 days. Decay Date: 1986-02-09 . USAF Sat Cat: 16306 . COSPAR: 1985-112A. Apogee: 323 km (200 mi). Perigee: 175 km (108 mi). Inclination: 67.10 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1985 December 12 - .
15:51 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1707 - .
Payload: Tselina-D no. 52. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 16326 . COSPAR: 1985-113A. Apogee: 623 km (387 mi). Perigee: 596 km (370 mi). Inclination: 82.50 deg. Period: 96.90 min. Replaced Cosmos 1515..
1985 December 28 - .
09:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
Launch Pad: LC45/pad?.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
FAILURE: Second stage failed to ignite. Partial Failure..
Failed Stage: 2.
- Cosmos 1714 - .
Payload: Tselina-2 no. 4. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
Decay Date: 1986-02-27 . USAF Sat Cat: 16434 . COSPAR: 1985-121A. Apogee: 850 km (520 mi). Perigee: 160 km (90 mi). Inclination: 71.00 deg. Period: 94.70 min. Tselina-2 ELINT satellite placed in unusable orbit due to second stage failure..
1986 January 15 - .
14:20 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1724 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1986-03-15 . USAF Sat Cat: 16490 . COSPAR: 1986-004A. Apogee: 330 km (200 mi). Perigee: 167 km (103 mi). Inclination: 67.10 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 January 17 - .
07:21 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1726 - .
Payload: Tselina-D no. 53. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 16495 . COSPAR: 1986-006A. Apogee: 618 km (384 mi). Perigee: 590 km (360 mi). Inclination: 82.50 deg. Period: 96.80 min.
1986 February 1 - .
18:11 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1729 - .
Payload: Oko #46. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 16527 . COSPAR: 1986-011A. Apogee: 33,130 km (20,580 mi). Perigee: 7,251 km (4,505 mi). Inclination: 68.00 deg. Period: 718.30 min. Replaced Cosmos 1569. Covered Oko constellation plane 5 - 75 degree longitude of ascending node..
1986 February 7 - .
08:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1731 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 238.00 days. Decay Date: 1986-10-03 . USAF Sat Cat: 16589 . COSPAR: 1986-013A. Apogee: 263 km (163 mi). Perigee: 233 km (144 mi). Inclination: 64.70 deg. Period: 89.50 min. Photo/digital surveillance..
1986 February 9 - .
10:06 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas H.
- USA 15 - .
Payload: PARCAE 8. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 16591 . COSPAR: 1986-014A. Apogee: 1,166 km (724 mi). Perigee: 1,049 km (651 mi). Inclination: 63.00 deg. Period: 107.40 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- USA 16 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 16624 . COSPAR: 1986-014E. Apogee: 1,161 km (721 mi). Perigee: 1,055 km (655 mi). Inclination: 63.00 deg. Period: 107.40 min.
- USA 18 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 16631 . COSPAR: 1986-014H. Apogee: 1,407 km (874 mi). Perigee: 817 km (508 mi). Inclination: 63.41 deg. Period: 107.44 min.
- USA 17 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 16625 . COSPAR: 1986-014F. Apogee: 1,165 km (723 mi). Perigee: 1,055 km (655 mi). Inclination: 63.00 deg. Period: 107.40 min.
1986 February 19 - .
23:04 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1733 - .
Payload: Tselina-D no. 54. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 16611 . COSPAR: 1986-018A. Apogee: 618 km (384 mi). Perigee: 594 km (369 mi). Inclination: 82.50 deg. Period: 96.80 min. Replaced Cosmos 1544..
1986 February 26 - .
13:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1734 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1986-04-26 . USAF Sat Cat: 16618 . COSPAR: 1986-020A. Apogee: 343 km (213 mi). Perigee: 165 km (102 mi). Inclination: 67.10 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 February 27 - .
01:44 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1735 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1988-11-17 . USAF Sat Cat: 16620 . COSPAR: 1986-021A. Apogee: 442 km (274 mi). Perigee: 419 km (260 mi). Inclination: 65.00 deg. Period: 93.20 min. Ocean surveillance..
1986 March 21 - .
10:05 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1736 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1986-09-01 . USAF Sat Cat: 16806 . COSPAR: 1986-024B. Apogee: 995 km (618 mi). Perigee: 936 km (581 mi). Inclination: 65.00 deg. Period: 104.40 min. Ocean surveillance; nuclear powered..
1986 March 25 - .
19:26 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1737 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1986-12-03 . USAF Sat Cat: 16648 . COSPAR: 1986-025A. Apogee: 426 km (264 mi). Perigee: 414 km (257 mi). Inclination: 73.40 deg. Period: 93.00 min. Ocean surveillance..
1986 April 9 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1739 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1986-06-07 . USAF Sat Cat: 16677 . COSPAR: 1986-028A. Apogee: 326 km (202 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 April 18 - .
17:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 34D.
FAILURE: SRM case insulation burned through, causing case burn-through and catastrophic explosion over pad at T+8.5 seconds..
Failed Stage: 0.
- KH-9 no. 20 - .
Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-9.
Decay Date: 1986-04-18 . KH-9 type satellite..
- SSF-D No. 6 - .
Payload: SSF-D No. 6. Mass: 60 kg (132 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1986-04-18 .
1986 May 15 - .
04:26 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1743 - .
Payload: Tselina-D no. 55. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 16719 . COSPAR: 1986-034A. Apogee: 623 km (387 mi). Perigee: 594 km (369 mi). Inclination: 82.60 deg. Period: 96.90 min. Replaced Cosmos 1626..
1986 June 6 - .
12:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1756 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1986-08-04 . USAF Sat Cat: 16767 . COSPAR: 1986-043A. Apogee: 268 km (166 mi). Perigee: 172 km (106 mi). Inclination: 64.90 deg. Period: 88.90 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 June 12 - .
04:43 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1758 - .
Payload: Tselina-D no. 56. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 16791 . COSPAR: 1986-046A. Apogee: 636 km (395 mi). Perigee: 603 km (374 mi). Inclination: 82.50 deg. Period: 97.10 min. Replaced Cosmos 1666..
1986 July 5 - .
01:16 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1761 - .
Payload: Oko #47. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 16849 . COSPAR: 1986-050A. Apogee: 35,495 km (22,055 mi). Perigee: 4,856 km (3,017 mi). Inclination: 67.80 deg. Period: 717.70 min. Replaced Cosmos 1698. Covered Oko constellation plane 3 - 354 degree longitude of ascending node..
1986 July 17 - .
12:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1764 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 56.00 days. Decay Date: 1986-09-11 . USAF Sat Cat: 16861 . COSPAR: 1986-053A. Apogee: 339 km (210 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 July 30 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 1767 - .
Payload: Mass Model. Mass: 15,000 kg (33,000 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
Decay Date: 1986-08-16 . USAF Sat Cat: 16883 . COSPAR: 1986-056A. Apogee: 205 km (127 mi). Perigee: 194 km (120 mi). Inclination: 64.90 deg. Period: 88.50 min. Instrumented Tselina-2 mock-up, with mass to test maximum payload capacity of Zenit launch vehicle. Officially: Investigation of the upper atmosphere and outer space..
1986 August 4 - .
05:08 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1769 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1987-09-30 . USAF Sat Cat: 16895 . COSPAR: 1986-059A. Apogee: 383 km (237 mi). Perigee: 287 km (178 mi). Inclination: 65.00 deg. Period: 91.20 min. Ocean surveillance..
1986 August 6 - .
13:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1770 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 180.00 days. Decay Date: 1987-02-02 . USAF Sat Cat: 16897 . COSPAR: 1986-060A. Apogee: 292 km (181 mi). Perigee: 234 km (145 mi). Inclination: 64.70 deg. Period: 89.80 min. Photo/digital surveillance..
1986 August 20 - .
12:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1771 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1986-11-29 . USAF Sat Cat: 17036 . COSPAR: 1986-062D. Apogee: 1,000 km (600 mi). Perigee: 909 km (564 mi). Inclination: 65.00 deg. Period: 104.20 min. Ocean surveillance; nuclear powered..
1986 August 27 - .
11:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1773 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 55.00 days. Decay Date: 1986-10-21 . USAF Sat Cat: 16920 . COSPAR: 1986-064A. Apogee: 339 km (210 mi). Perigee: 171 km (106 mi). Inclination: 64.90 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 August 28 - .
08:02 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1774 - .
Payload: Oko #48. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2010-10-01 . USAF Sat Cat: 16922 . COSPAR: 1986-065A. Apogee: 36,998 km (22,989 mi). Perigee: 3,405 km (2,115 mi). Inclination: 65.00 deg. Period: 718.80 min. Replaced Cosmos 1547. Covered Oko constellation plane 7 - 156 degree longitude of ascending node..
1986 September 3 - .
09:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1776 - .
Mass: 700 kg (1,540 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1989-12-15 . USAF Sat Cat: 16928 . COSPAR: 1986-067A. Apogee: 417 km (259 mi). Perigee: 403 km (250 mi). Inclination: 74.00 deg. Period: 92.80 min. Released 25 Romb radar calibration subsatellites..
1986 September 30 - .
18:34 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1782 - .
Payload: Tselina-D no. 57. Mass: 1,400 kg (3,000 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 16986 . COSPAR: 1986-074A. Apogee: 628 km (390 mi). Perigee: 605 km (375 mi). Inclination: 82.50 deg. Period: 97.00 min.
1986 October 3 - .
13:05 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
FAILURE: Fourth stage failure..
Failed Stage: U.
- Cosmos 1783 - .
Payload: Oko #49. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 16993 . COSPAR: 1986-075A. Apogee: 18,679 km (11,606 mi). Perigee: 1,970 km (1,220 mi). Inclination: 64.60 deg. Period: 358.00 min. Unusable orbit. Was intended to cover Oko constellation plane 1 - 272 degree longitude of ascending node..
1986 October 6 - .
05:40 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 8 - .
Payload: FSW-0 No. 08. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 5.00 days. Decay Date: 1986-10-23 . USAF Sat Cat: 17001 . COSPAR: 1986-076A. Apogee: 337 km (209 mi). Perigee: 169 km (105 mi). Inclination: 57.00 deg. Period: 89.60 min. Fanhui Shi Weixing recoverable satellite; capsule re-entered October 11 after five day mission..
1986 October 6 - .
07:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1784 - .
Payload: Yantar-1KFT no. 6. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 36.00 days. Decay Date: 1986-11-11 . USAF Sat Cat: 17003 . COSPAR: 1986-077A. Apogee: 283 km (175 mi). Perigee: 190 km (110 mi). Inclination: 64.80 deg. Period: 89.20 min. Military topographic / cartographic satellite..
1986 October 15 - .
09:29 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1785 - .
Payload: Oko #50. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2002-02-28 . USAF Sat Cat: 17031 . COSPAR: 1986-078A. Apogee: 37,013 km (22,998 mi). Perigee: 3,408 km (2,117 mi). Inclination: 67.00 deg. Period: 719.10 min. Replaced Cosmos 1596. Covered Oko constellation plane 9 - 233 degree longitude of ascending node..
1986 October 22 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 1786 - .
Mass: 15,000 kg (33,000 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Koltso.
Decay Date: 1988-03-06 . USAF Sat Cat: 17042 . COSPAR: 1986-080A. Apogee: 1,054 km (654 mi). Perigee: 149 km (92 mi). Inclination: 64.80 deg. Period: 96.70 min. Radar calibration mission..
1986 October 27 - .
12:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1788 - .
Mass: 700 kg (1,540 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1991-01-21 . USAF Sat Cat: 17050 . COSPAR: 1986-083A. Apogee: 263 km (163 mi). Perigee: 262 km (162 mi). Inclination: 65.80 deg. Period: 89.80 min. Radar calibration mission..
1986 November 13 - .
10:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1792 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 53.00 days. Decay Date: 1987-01-05 . USAF Sat Cat: 17068 . COSPAR: 1986-087A. Apogee: 309 km (192 mi). Perigee: 184 km (114 mi). Inclination: 64.90 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 November 20 - .
12:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1793 - .
Payload: Oko #51. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2011-05-15 . USAF Sat Cat: 17134 . COSPAR: 1986-091A. Apogee: 36,922 km (22,942 mi). Perigee: 3,455 km (2,146 mi). Inclination: 67.20 deg. Period: 718.20 min. Replaced Cosmos 1687. Covered Oko constellation plane 2 - 313 degree longitude of ascending node..
1986 November 29 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K.
FAILURE: Second stage explosion..
Failed Stage: 2.
- Almaz-T s/n 303 Failure - .
Payload: Almaz-K s/n 303. Mass: 18,550 kg (40,890 lb). Nation: Russia.
Agency: UNKS.
Program: Almaz.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Almaz.
Spacecraft: Almaz-T.
Decay Date: 1986-12-29 . In the second half of 1986 the first Almaz-T s/n 303 was readied for launch. General V V Favorskiy ordered it to be completed and launched with a full-up lab module in place of trials equipment. Unfortunately did not reach orbit..
1986 December 10 - .
07:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1805 - .
Payload: Tselina-D no. 58. Mass: 1,400 kg (3,000 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 17191 . COSPAR: 1986-097A. Apogee: 622 km (386 mi). Perigee: 598 km (371 mi). Inclination: 82.50 deg. Period: 96.90 min.
1986 December 12 - .
18:35 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1806 - .
Payload: Oko #52. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 17213 . COSPAR: 1986-098A. Apogee: 32,850 km (20,410 mi). Perigee: 7,495 km (4,657 mi). Inclination: 67.90 deg. Period: 717.60 min. Replaced Cosmos 1729. Covered Oko constellation plane 5 - 73 degree longitude of ascending node..
1986 December 16 - .
14:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1807 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 38.00 days. Decay Date: 1987-01-23 . USAF Sat Cat: 17217 . COSPAR: 1986-099A. Apogee: 366 km (227 mi). Perigee: 165 km (102 mi). Inclination: 67.10 deg. Period: 89.80 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1986 December 26 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1810 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 259.00 days. Decay Date: 1987-09-11 . USAF Sat Cat: 17262 . COSPAR: 1986-102A. Apogee: 275 km (170 mi). Perigee: 224 km (139 mi). Inclination: 64.70 deg. Period: 89.50 min. Photo/digital surveillance..
1987 January 9 - .
12:38 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1811 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 35.00 days. Decay Date: 1987-02-13 . USAF Sat Cat: 17292 . COSPAR: 1987-002A. Apogee: 345 km (214 mi). Perigee: 169 km (105 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1987 January 14 - .
09:05 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1812 - .
Payload: Tselina-D no. 59. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 17295 . COSPAR: 1987-003A. Apogee: 622 km (386 mi). Perigee: 598 km (371 mi). Inclination: 82.50 deg. Period: 96.90 min. Ocean surveillance..
1987 January 22 - .
07:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar LC107/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1815 - .
Mass: 700 kg (1,540 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1988-11-15 . USAF Sat Cat: 17326 . COSPAR: 1987-007A. Apogee: 507 km (315 mi). Perigee: 336 km (208 mi). Inclination: 50.70 deg. Period: 93.00 min. Released 25 Romb radar calibration subsatellites..
1987 February 1 - .
23:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1818 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: Plazma-A.
USAF Sat Cat: 17369 . COSPAR: 1987-011A. Apogee: 803 km (498 mi). Perigee: 774 km (480 mi). Inclination: 65.00 deg. Period: 100.60 min. Test of new Topaz reactor, new systems, and ion engines aboard US-AM bus..
1987 February 26 - .
13:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1824 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 55.00 days. Decay Date: 1987-04-22 . USAF Sat Cat: 17559 . COSPAR: 1987-021A. Apogee: 352 km (218 mi). Perigee: 162 km (100 mi). Inclination: 67.20 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1987 March 3 - .
15:03 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1825 - .
Payload: Tselina-D no. 60. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 17566 . COSPAR: 1987-024A. Apogee: 621 km (385 mi). Perigee: 594 km (369 mi). Inclination: 82.50 deg. Period: 96.80 min. Ocean surveillance..
1987 March 18 - .
08:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 1833 - .
Payload: Tselina-2 no. 5 (Mass Model). Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 17589 . COSPAR: 1987-027A. Apogee: 855 km (531 mi). Perigee: 845 km (525 mi). Inclination: 70.90 deg. Period: 101.90 min.
1987 April 8 - .
03:51 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1834 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1988-10-14 . USAF Sat Cat: 17847 . COSPAR: 1987-031A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1987 April 9 - .
11:44 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1835 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 56.00 days. Decay Date: 1987-06-04 . USAF Sat Cat: 17849 . COSPAR: 1987-032A. Apogee: 343 km (213 mi). Perigee: 170 km (100 mi). Inclination: 64.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1987 April 16 - .
06:18 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1836 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 230.00 days. Decay Date: 1987-12-02 . USAF Sat Cat: 17876 . COSPAR: 1987-033A. Apogee: 289 km (179 mi). Perigee: 236 km (146 mi). Inclination: 64.80 deg. Period: 89.80 min. Photo/digital surveillance..
1987 April 27 - .
00:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1842 - .
Payload: Tselina-D no. 61. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 17911 . COSPAR: 1987-038A. Apogee: 628 km (390 mi). Perigee: 602 km (374 mi). Inclination: 82.50 deg. Period: 97.00 min.
1987 May 13 - .
05:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 1844 - .
Payload: Tselina-2 no. 6. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 17973 . COSPAR: 1987-041A. Apogee: 851 km (528 mi). Perigee: 844 km (524 mi). Inclination: 70.90 deg. Period: 101.90 min.
1987 May 15 - .
15:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas H.
- USA 22 - .
Payload: PARCAE 9. Mass: 700 kg (1,540 lb). Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft: NOSS.
USAF Sat Cat: 17997 . COSPAR: 1987-043A. Apogee: 1,179 km (732 mi). Perigee: 1,045 km (649 mi). Inclination: 62.90 deg. Period: 107.80 min. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE..
- USA 24 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 18010 . COSPAR: 1987-043F. Apogee: 1,184 km (735 mi). Perigee: 1,046 km (649 mi). Inclination: 63.20 deg. Period: 107.90 min.
- USA 25 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 18025 . COSPAR: 1987-043H. Apogee: 1,178 km (731 mi). Perigee: 1,035 km (643 mi). Inclination: 62.60 deg. Period: 107.60 min.
- USA 23 - .
Payload: SSU. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: NOSS.
Spacecraft: NOSS-Subsat.
USAF Sat Cat: 18009 . COSPAR: 1987-043E. Apogee: 1,170 km (720 mi). Perigee: 1,039 km (645 mi). Inclination: 63.40 deg. Period: 107.30 min.
1987 May 26 - .
13:39 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1847 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 57.00 days. Decay Date: 1987-07-22 . USAF Sat Cat: 18011 . COSPAR: 1987-046A. Apogee: 315 km (195 mi). Perigee: 175 km (108 mi). Inclination: 67.10 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1987 June 4 - .
18:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1849 - .
Payload: Oko #53. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2003-02-04 . USAF Sat Cat: 18083 . COSPAR: 1987-048A. Apogee: 37,311 km (23,183 mi). Perigee: 3,104 km (1,928 mi). Inclination: 67.10 deg. Period: 719.00 min. Covered Oko constellation plane 1 - 274 degree longitude of ascending node..
1987 June 12 - .
07:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1851 - .
Payload: Oko #54. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 18103 . COSPAR: 1987-050A. Apogee: 33,453 km (20,786 mi). Perigee: 6,926 km (4,303 mi). Inclination: 67.90 deg. Period: 718.30 min. Covered Oko constellation plane 6 - 113 degree longitude of ascending node..
1987 June 18 - .
21:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1860 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1987-09-16 . USAF Sat Cat: 18240 . COSPAR: 1987-052C. Apogee: 992 km (616 mi). Perigee: 900 km (550 mi). Inclination: 65.00 deg. Period: 104.00 min. Ocean surveillance; nuclear powered..
1987 July 1 - .
19:35 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1862 - .
Payload: Tselina-D no. 62. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 18152 . COSPAR: 1987-055A. Apogee: 636 km (395 mi). Perigee: 602 km (374 mi). Inclination: 82.50 deg. Period: 97.10 min.
1987 July 8 - .
10:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1865 - .
Payload: Yantar-1KFT no. 7. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 37.00 days. Decay Date: 1987-08-14 . USAF Sat Cat: 18162 . COSPAR: 1987-058A. Apogee: 297 km (184 mi). Perigee: 192 km (119 mi). Inclination: 64.80 deg. Period: 89.40 min. Military topographic / cartographic satellite..
1987 July 9 - .
16:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1866 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 17.00 days. Decay Date: 1987-08-31 . USAF Sat Cat: 18184 . COSPAR: 1987-059A. Apogee: 769 km (477 mi). Perigee: 223 km (138 mi). Inclination: 67.20 deg. Period: 94.50 min. High resolution photo reconnaissance. Engine failure prematurely depleted fuel supply. Blown up in orbit on July 26..
1987 July 10 - .
15:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1867 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: Plazma-A.
USAF Sat Cat: 18187 . COSPAR: 1987-060A. Apogee: 803 km (498 mi). Perigee: 776 km (482 mi). Inclination: 65.00 deg. Period: 100.70 min. Test of new Topaz reactor, new systems, and ion engines aboard US-AM bus - Tested Plasma-2 SPT electric engine..
1987 July 14 - .
14:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1868 - .
Mass: 700 kg (1,540 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1989-03-03 . USAF Sat Cat: 18192 . COSPAR: 1987-061A. Apogee: 669 km (415 mi). Perigee: 279 km (173 mi). Inclination: 74.00 deg. Period: 94.10 min. Radar calibration mission..
1987 July 25 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K.
- Cosmos 1870 - .
Payload: Almaz-K s/n 304. Mass: 18,550 kg (40,890 lb). Nation: Russia.
Agency: MOM.
Program: Almaz.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Almaz.
Spacecraft: Almaz-T.
Duration: 734.00 days. Decay Date: 1989-07-29 . USAF Sat Cat: 18225 . COSPAR: 1987-064A. Apogee: 278 km (172 mi). Perigee: 263 km (163 mi). Inclination: 71.90 deg. Period: 89.90 min.
First flight of Almaz radars imaging satellite taken out of mothballs after death of Ustinov. At the beginning of 1987 it was decided not to man the Almaz-T, instead operate it in a fully automatic mode. Thus the final Almaz cosmonaut training group was disbanded. Cosmos 1870 conducted remote sensing of the earth's surface, oceans and seas in the interests of various branches of science and the economy. Its side-looking radar had a 20-25 m ground resolution and functioned throughout its two year service life.
1987 August 5 - .
06:39 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-0 No. 9 - .
Payload: FSW-0 No. 09. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 5.00 days. Decay Date: 1987-08-23 . USAF Sat Cat: 18306 . COSPAR: 1987-067A. Apogee: 366 km (227 mi). Perigee: 169 km (105 mi). Inclination: 63.00 deg. Period: 89.90 min. Fanhui Shi Weixing recoverable satellite; carried microgravity experiments; return capsule recovered August 10 after five days in space..
1987 September 9 - .
07:15 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-1 No. 1 - .
Payload: FSW-1 No. 01. Mass: 2,100 kg (4,600 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 8.00 days. Decay Date: 1987-10-04 . USAF Sat Cat: 18341 . COSPAR: 1987-075A. Apogee: 222 km (137 mi). Perigee: 181 km (112 mi). Inclination: 63.00 deg. Period: 88.50 min. Fanhui Shi Weixing recoverable satellite; return capsule recovered September 17 after eight days in space..
1987 September 11 - .
02:06 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1881 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 201.00 days. Decay Date: 1988-03-30 . USAF Sat Cat: 18343 . COSPAR: 1987-076A. Apogee: 294 km (182 mi). Perigee: 228 km (141 mi). Inclination: 64.70 deg. Period: 89.70 min. Photo/digital surveillance..
1987 September 17 - .
14:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1886 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 46.00 days. Decay Date: 1987-11-02 . USAF Sat Cat: 18366 . COSPAR: 1987-081A. Apogee: 321 km (199 mi). Perigee: 170 km (100 mi). Inclination: 67.10 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1987 October 10 - .
21:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1890 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1988-12-26 . USAF Sat Cat: 18396 . COSPAR: 1987-086A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1987 October 20 - .
09:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1892 - .
Payload: Tselina-D no. 63. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 18421 . COSPAR: 1987-088A. Apogee: 623 km (387 mi). Perigee: 595 km (369 mi). Inclination: 82.50 deg. Period: 96.90 min.
1987 October 22 - .
14:25 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1893 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 55.00 days. Decay Date: 1987-12-16 . USAF Sat Cat: 18432 . COSPAR: 1987-089A. Apogee: 323 km (200 mi). Perigee: 162 km (100 mi). Inclination: 67.20 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1987 October 26 - .
21:32 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 34D.
- USA 27 - .
Payload: KH-11 no. 8. Mass: 13,300 kg (29,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
Decay Date: 1992-05-31 . USAF Sat Cat: 18441 . COSPAR: 1987-090A. Apogee: 1,029 km (639 mi). Perigee: 153 km (95 mi). Inclination: 97.80 deg. Period: 96.50 min. KH-11 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1987 October 28 - .
15:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1987 November 14 - .
09:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1896 - .
Payload: Yantar-1KFT no. 8. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 41.00 days. Decay Date: 1987-12-25 . USAF Sat Cat: 18535 . COSPAR: 1987-093A. Apogee: 263 km (163 mi). Perigee: 206 km (128 mi). Inclination: 64.80 deg. Period: 89.20 min. Military topographic / cartographic satellite..
1987 November 29 - .
03:28 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 34D/Transtage.
- USA 28 - .
Payload: DSP Phase 2 Upgrade s/n 5R. Mass: 1,670 kg (3,680 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1987-12-31 . USAF Sat Cat: 18583 . COSPAR: 1987-097A. Apogee: 35,558 km (22,094 mi). Perigee: 35,514 km (22,067 mi). Inclination: 2.90 deg. Period: 1,423.30 min.
Reserve DSP ballistic missile launch detection satellite fitted with Block 14 sensors, remained in service for only five years.. Observed Scud launches during Gulf War. Positioned in geosynchronous orbit at 35 deg W in 1988-1989; 10 deg E in 1989-1992; 35 deg W in 1992-1993; 105 deg E in 1993; 165 deg W in 1999.
1987 December 12 - .
05:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1900 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
USAF Sat Cat: 18665 . COSPAR: 1987-101A. Apogee: 735 km (456 mi). Perigee: 696 km (432 mi). Inclination: 66.10 deg. Period: 99.10 min. Ocean surveillance; nuclear powered..
- Cosmos 1900 - .
Mass: 4,300 kg (9,400 lb). Nation: Russia.
Agency: UNKS.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
COSPAR: 1987-101xx. Ocean surveillance; nuclear powered..
1987 December 14 - .
11:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1901 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 51.00 days. Decay Date: 1988-02-03 . USAF Sat Cat: 18666 . COSPAR: 1987-102A. Apogee: 343 km (213 mi). Perigee: 172 km (106 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1987 December 15 - .
13:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1902 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1988-12-30 . USAF Sat Cat: 18668 . COSPAR: 1987-103A. Apogee: 408 km (253 mi). Perigee: 364 km (226 mi). Inclination: 65.80 deg. Period: 92.30 min. Radar calibration mission..
1987 December 21 - .
22:35 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1903 - .
Payload: Oko #55. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 18701 . COSPAR: 1987-105A. Apogee: 33,733 km (20,960 mi). Perigee: 6,634 km (4,122 mi). Inclination: 67.70 deg. Period: 718.00 min. Covered Oko constellation plane 8 - 196 degree longitude of ascending node. It was reported that prior to this, on 8 November 1987 a Molniya booster was prepared for launch in a record four days at Plesetsk..
1988 January 6 - .
07:41 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1908 - .
Payload: Tselina-D no. 64. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 18748 . COSPAR: 1988-001A. Apogee: 626 km (388 mi). Perigee: 600 km (370 mi). Inclination: 82.50 deg. Period: 97.00 min.
1988 February 3 - .
12:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1916 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 24.00 days. Decay Date: 1988-02-29 . USAF Sat Cat: 18823 . COSPAR: 1988-007A. Apogee: 352 km (218 mi). Perigee: 168 km (104 mi). Inclination: 64.90 deg. Period: 89.70 min. High resolution photo reconnaissance. Spacecraft failed. Blown up in orbit on February 27..
1988 February 26 - .
09:31 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1922 - .
Payload: Oko #56. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 18881 . COSPAR: 1988-013A. Apogee: 34,181 km (21,239 mi). Perigee: 6,225 km (3,868 mi). Inclination: 67.60 deg. Period: 718.80 min. Covered Oko constellation plane 5 - 75 degree longitude of ascending node..
1988 March 14 - .
14:21 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1932 - .
Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MO.
Program: RORSAT.
Class: Surveillance.
Type: Naval Radarsat. Spacecraft Bus: Kosmoplan.
Spacecraft: US-A.
Decay Date: 1988-06-29 . USAF Sat Cat: 19160 . COSPAR: 1988-019B. Apogee: 1,008 km (626 mi). Perigee: 920 km (570 mi). Inclination: 65.10 deg. Period: 104.40 min. Ocean surveillance; nuclear powered - last launch of the US-AM. Programme cancelled by Gorbachev..
1988 March 15 - .
18:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1933 - .
Payload: Tselina-D no. 65. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 18958 . COSPAR: 1988-020A. Apogee: 629 km (390 mi). Perigee: 605 km (375 mi). Inclination: 82.50 deg. Period: 97.10 min.
1988 March 24 - .
14:10 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1935 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 15.00 days. Decay Date: 1988-04-08 . USAF Sat Cat: 19011 . COSPAR: 1988-025A. Apogee: 330 km (200 mi). Perigee: 166 km (103 mi). Inclination: 67.20 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1988 March 30 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1936 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 49.00 days. Decay Date: 1988-05-18 . USAF Sat Cat: 19015 . COSPAR: 1988-027A. Apogee: 266 km (165 mi). Perigee: 182 km (113 mi). Inclination: 64.80 deg. Period: 89.00 min. Photo/digital surveillance..
1988 May 12 - .
14:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1942 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 53.00 days. Decay Date: 1988-07-04 . USAF Sat Cat: 19115 . COSPAR: 1988-037A. Apogee: 356 km (221 mi). Perigee: 166 km (103 mi). Inclination: 67.10 deg. Period: 89.70 min.
1988 May 15 - .
09:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 1943 - .
Payload: Tselina-2 no. 7. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 19119 . COSPAR: 1988-039A. Apogee: 851 km (528 mi). Perigee: 837 km (520 mi). Inclination: 71.00 deg. Period: 101.80 min.
1988 May 18 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1944 - .
Payload: Yantar-1KFT no. 9. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 36.00 days. Decay Date: 1988-06-23 . USAF Sat Cat: 19123 . COSPAR: 1988-041A. Apogee: 288 km (178 mi). Perigee: 196 km (121 mi). Inclination: 64.80 deg. Period: 89.30 min. Military topographic / cartographic satellite..
1988 May 28 - .
02:49 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1949 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1990-04-23 . USAF Sat Cat: 19193 . COSPAR: 1988-045A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1988 June 14 - .
03:18 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1953 - .
Payload: Tselina-D no. 66. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 19210 . COSPAR: 1988-050A. Apogee: 637 km (395 mi). Perigee: 604 km (375 mi). Inclination: 82.50 deg. Period: 97.10 min. Outer space research. .
1988 June 22 - .
13:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1955 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1988-08-20 . USAF Sat Cat: 19258 . COSPAR: 1988-054A. Apogee: 357 km (221 mi). Perigee: 171 km (106 mi). Inclination: 64.80 deg. Period: 89.80 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1988 July 14 - .
11:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1958 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1989-03-21 . USAF Sat Cat: 19320 . COSPAR: 1988-060A. Apogee: 411 km (255 mi). Perigee: 360 km (220 mi). Inclination: 65.80 deg. Period: 92.30 min. Radar calibration mission..
1988 July 28 - .
11:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1960 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1990-04-09 . USAF Sat Cat: 19338 . COSPAR: 1988-065A. Apogee: 379 km (235 mi). Perigee: 369 km (229 mi). Inclination: 65.80 deg. Period: 92.00 min. Released 25 Romb radar calibration subsatellites..
1988 August 5 - .
07:29 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-1 No. 2 - .
Payload: FSW-1 No. 02. Mass: 2,100 kg (4,600 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 8.00 days. Decay Date: 1988-08-13 . USAF Sat Cat: 19368 . COSPAR: 1988-067A. Apogee: 311 km (193 mi). Perigee: 204 km (126 mi). Inclination: 63.00 deg. Period: 89.70 min. German crystal growth experiment in recoverable capsule. Results marred by hard landing..
1988 August 16 - .
13:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1963 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 47.00 days. Decay Date: 1988-10-02 . USAF Sat Cat: 19384 . COSPAR: 1988-070A. Apogee: 350 km (210 mi). Perigee: 176 km (109 mi). Inclination: 64.80 deg. Period: 89.80 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1988 August 30 - .
14:14 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1966 - .
Payload: Oko #57. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2005-11-10 . USAF Sat Cat: 19445 . COSPAR: 1988-076A. Apogee: 37,970 km (23,590 mi). Perigee: 2,436 km (1,513 mi). Inclination: 67.20 deg. Period: 718.80 min. Covered Oko constellation plane 3 - 355 degree longitude of ascending node..
1988 September 2 - .
12:05 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 34D/Transtage.
FAILURE: Broken Transtage pressurization feed lines prevented the geosynchronous orbit apogee burn from taking place..
Failed Stage: U.
- USA 31 - .
Payload: Chalet 5. Mass: 1,045 kg (2,303 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Chalet.
USAF Sat Cat: 19458 . COSPAR: 1988-077A. Apogee: 14,103 km (8,763 mi). Perigee: 151 km (93 mi). Inclination: 29.30 deg. Period: 99.80 min. Chalet ELINT satellite; upper stage failure left in lower than planned orbit..
1988 September 5 - .
09:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan II SLV.
- USA 32 - .
Payload: SBWASS R1. Mass: 1,700 kg (3,700 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Singleton.
USAF Sat Cat: 19460 . COSPAR: 1988-078A. Apogee: 292 km (181 mi). Perigee: 185 km (114 mi). Inclination: 85.00 deg. Period: 89.30 min. New class of signals intelligence satellite; possibly some kind of imaging also done. On-board propulsion boosts spacecraft to 800 km operating orbit. First Titan 2 standard launch vehicle launch..
1988 September 15 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1969 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1988-11-13 . USAF Sat Cat: 19495 . COSPAR: 1988-084A. Apogee: 344 km (213 mi). Perigee: 165 km (102 mi). Inclination: 67.10 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1988 October 3 - .
22:23 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1974 - .
Payload: Oko #58. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 19554 . COSPAR: 1988-092A. Apogee: 33,413 km (20,761 mi). Perigee: 6,942 km (4,313 mi). Inclination: 68.00 deg. Period: 717.80 min. Covered Oko constellation plane 7 - 157 degree longitude of ascending node..
1988 October 11 - .
08:01 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1975 - .
Payload: Tselina-D no. 67. Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 19573 . COSPAR: 1988-093A. Apogee: 636 km (395 mi). Perigee: 604 km (375 mi). Inclination: 82.50 deg. Period: 97.10 min. Investigation of outer space. .
1988 October 25 - .
18:02 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC41/1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1977 - .
Payload: Oko #59. Mass: 1,250 kg (2,750 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 19608 . COSPAR: 1988-096A. Apogee: 33,805 km (21,005 mi). Perigee: 6,559 km (4,075 mi). Inclination: 67.70 deg. Period: 718.00 min. Covered Oko constellation plane 6 - 116 degree longitude of ascending node..
1988 November 6 - .
18:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 34D.
- USA 33 - .
Payload: KH-11 no. 9. Mass: 13,500 kg (29,700 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: KH-11.
USAF Sat Cat: 19625 . COSPAR: 1988-099A. Apogee: 1,012 km (628 mi). Perigee: 156 km (96 mi). Inclination: 97.90 deg. Period: 96.40 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1988 November 18 - .
00:12 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 1979 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1989-12-25 . USAF Sat Cat: 19647 . COSPAR: 1988-101A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1988 November 23 - .
14:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 1980 - .
Payload: Tselina-2 no. 8. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 19649 . COSPAR: 1988-102A. Apogee: 849 km (527 mi). Perigee: 841 km (522 mi). Inclination: 71.00 deg. Period: 101.80 min.
1988 December 2 - .
14:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39B.
Launch Platform: MLP1.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- USA 34 - .
Payload: Lacrosse 1. Nation: USA.
Agency: CIA,
NRO.
Manufacturer: Martin.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Lacrosse satellite.
Decay Date: 1997-03-25 . USAF Sat Cat: 19671 . COSPAR: 1988-106B. Apogee: 447 km (277 mi). Perigee: 437 km (271 mi). Inclination: 57.00 deg. Period: 93.40 min. Deployed from STS-27. Operations completed March 1997..
1988 December 16 - .
19:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1984 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1989-02-13 . USAF Sat Cat: 19705 . COSPAR: 1988-110A. Apogee: 323 km (200 mi). Perigee: 186 km (115 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1988 December 23 - .
07:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 1985 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-3.
Decay Date: 1992-05-04 . USAF Sat Cat: 19720 . COSPAR: 1988-113A. Apogee: 220 km (130 mi). Perigee: 206 km (128 mi). Inclination: 73.50 deg. Period: 88.80 min. Radar calibration mission. Believed to be a modernised version of the Taifun-1 satellite. Released 36 Romb radar calibration subsatellites..
1988 December 29 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1986 - .
Payload: Yantar-1KFT no. 10. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 44.00 days. Decay Date: 1989-02-11 . USAF Sat Cat: 19734 . COSPAR: 1988-116A. Apogee: 289 km (179 mi). Perigee: 193 km (119 mi). Inclination: 64.80 deg. Period: 89.30 min. Topographic mapping for the Army General Staff..
1989 January 28 - .
12:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 1993 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 58.00 days. Decay Date: 1989-03-27 . USAF Sat Cat: 19774 . COSPAR: 1989-007A. Apogee: 347 km (215 mi). Perigee: 171 km (106 mi). Inclination: 64.80 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1989 February 14 - .
04:21 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2001 - .
Payload: Oko #60. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2008-09-22 . USAF Sat Cat: 19796 . COSPAR: 1989-011A. Apogee: 37,951 km (23,581 mi). Perigee: 2,441 km (1,516 mi). Inclination: 66.90 deg. Period: 718.50 min. Covered Oko constellation plane 4 - 32 degree longitude of ascending node..
1989 February 14 - .
17:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2002 - .
Mass: 500 kg (1,100 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1989-10-15 . USAF Sat Cat: 19800 . COSPAR: 1989-012A. Apogee: 1,525 km (947 mi). Perigee: 179 km (111 mi). Inclination: 65.80 deg. Period: 102.00 min. Released 10 Romb radar calibration subsatellites..
1989 March 2 - .
18:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2005 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 54.00 days. Decay Date: 1989-04-25 . USAF Sat Cat: 19862 . COSPAR: 1989-019A. Apogee: 324 km (201 mi). Perigee: 188 km (116 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1989 March 23 - .
12:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2007 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 180.00 days. Decay Date: 1989-09-22 . USAF Sat Cat: 19900 . COSPAR: 1989-024A. Apogee: 262 km (162 mi). Perigee: 224 km (139 mi). Inclination: 64.70 deg. Period: 89.40 min. Photo/digital surveillance..
1989 April 20 - .
18:29 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2018 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 60.00 days. Decay Date: 1989-06-19 . USAF Sat Cat: 19938 . COSPAR: 1989-031A. Apogee: 327 km (203 mi). Perigee: 185 km (114 mi). Inclination: 62.90 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1989 May 10 - .
19:47 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 34D/Transtage.
- USA 37 - .
Payload: Chalet 6. Mass: 1,045 kg (2,303 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Chalet.
USAF Sat Cat: 19976 . COSPAR: 1989-035A. Apogee: 40,073 km (24,900 mi). Perigee: 455 km (282 mi). Inclination: 27.50 deg. Period: 720.00 min. Chalet ELINT satellite..
1989 May 17 - .
13:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2020 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1989-07-15 . USAF Sat Cat: 19986 . COSPAR: 1989-036A. Apogee: 280 km (170 mi). Perigee: 178 km (110 mi). Inclination: 64.80 deg. Period: 89.10 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1989 May 24 - .
10:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2021 - .
Payload: Yantar-1KFT no. 11. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 43.00 days. Decay Date: 1989-07-06 . USAF Sat Cat: 20000 . COSPAR: 1989-037A. Apogee: 280 km (170 mi). Perigee: 204 km (126 mi). Inclination: 69.90 deg. Period: 89.40 min. Topographic mapping for the Army General Staff..
1989 June 14 - .
12:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2027 - .
Mass: 900 kg (1,980 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
Decay Date: 1992-04-14 . USAF Sat Cat: 20064 . COSPAR: 1989-045A. Apogee: 427 km (265 mi). Perigee: 394 km (244 mi). Inclination: 65.80 deg. Period: 92.80 min. Radar calibration mission..
1989 June 14 - .
13:18 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 402A/IUS.
1989 July 12 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2030 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 16.00 days. Decay Date: 1989-07-29 . USAF Sat Cat: 20124 . COSPAR: 1989-054A. Apogee: 349 km (216 mi). Perigee: 162 km (100 mi). Inclination: 67.20 deg. Period: 89.60 min. High resolution photo reconnaissance. Spacecraft failed. Blown up in orbit on July 28..
1989 July 18 - .
12:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2031 - .
Payload: Orlets-1 no. 1. Mass: 6,500 kg (14,300 lb). Nation: Russia.
Agency: MOM.
Program: Orlets.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Duration: 44.00 days. Decay Date: 1989-09-15 . USAF Sat Cat: 20136 . COSPAR: 1989-056A. Apogee: 264 km (164 mi). Perigee: 211 km (131 mi). Inclination: 50.40 deg. Period: 89.30 min. First launch of Orlets-1 long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited..
1989 July 24 - .
00:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2033 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1991-01-06 . USAF Sat Cat: 20147 . COSPAR: 1989-058A. Apogee: 322 km (200 mi). Perigee: 196 km (121 mi). Inclination: 65.00 deg. Period: 89.70 min. Ocean surveillance..
1989 August 8 - .
12:37 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39B.
Launch Platform: MLP2.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- USA 41 - .
Nation: USA.
Agency: DARPA.
Class: Surveillance.
Type: SIGINT. Spacecraft Bus: P 11.
Spacecraft: SSF.
Decay Date: 1989-12-31 . USAF Sat Cat: 20172 . COSPAR: 1989-061C. Apogee: 307 km (190 mi). Perigee: 296 km (183 mi). Inclination: 57.00 deg. Period: 90.50 min. Deployed from STS-28 8/8/89. Believed to be one-off ferret satellite under COBRA BRASS measurement and signature intelligence experiment..
1989 September 6 - .
01:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan II SLV.
- USA 45 - .
Payload: SBWASS R2. Mass: 1,700 kg (3,700 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Singleton.
USAF Sat Cat: 20220 . COSPAR: 1989-072A. Signals intelligence. Reentered from initial parking orbit of 200 km after failure of on-board boost motor..
1989 September 27 - .
16:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2046 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1991-04-16 . USAF Sat Cat: 20259 . COSPAR: 1989-079A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1989 October 3 - .
14:59 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2047 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 49.00 days. Decay Date: 1989-11-21 . USAF Sat Cat: 20279 . COSPAR: 1989-082A. Apogee: 330 km (200 mi). Perigee: 165 km (102 mi). Inclination: 67.10 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1989 November 17 - .
10:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2049 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 214.00 days. Decay Date: 1990-06-19 . USAF Sat Cat: 20320 . COSPAR: 1989-088A. Apogee: 251 km (155 mi). Perigee: 232 km (144 mi). Inclination: 64.80 deg. Period: 89.30 min. Photo/digital surveillance..
1989 November 23 - .
00:23 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39B.
Launch Platform: MLP2.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- USA 48 - .
Payload: Orion 2. Mass: 2,500 kg (5,500 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Magnum.
USAF Sat Cat: 20355 . COSPAR: 1989-090B. Apogee: 35,800 km (22,200 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,440.00 min. Second Magnum model ELINT satellite. Code name changed to Orion. Deployed from STS-33 November 23, 1989, and boosted to geostationary orbit. As of 2003 May 4 located at 88.13E drifting at 0.048W degrees per day..
1989 November 23 - .
20:35 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2050 - .
Payload: Oko #61. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 20330 . COSPAR: 1989-091A. Apogee: 34,182 km (21,239 mi). Perigee: 6,185 km (3,843 mi). Inclination: 67.50 deg. Period: 718.00 min. Covered Oko constellation plane 9 - 233 degree longitude of ascending node..
1989 November 24 - .
23:22 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2051 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1990-01-21 . USAF Sat Cat: 20334 . COSPAR: 1989-092A. Apogee: 310 km (190 mi). Perigee: 293 km (182 mi). Inclination: 64.90 deg. Period: 90.60 min. Ocean surveillance..
1989 November 30 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2052 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 55.00 days. Decay Date: 1990-01-24 . USAF Sat Cat: 20350 . COSPAR: 1989-095A. Apogee: 320 km (190 mi). Perigee: 174 km (108 mi). Inclination: 67.10 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1989 December 27 - .
00:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 2053 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-3.
Decay Date: 1997-09-02 . USAF Sat Cat: 20389 . COSPAR: 1989-100A. Apogee: 410 km (250 mi). Perigee: 405 km (251 mi). Inclination: 73.50 deg. Period: 92.70 min.
Believed to be a modernised version of the Taifun-1 satellite, built by NPO Yuzhnoe. The satellite carried 36 small Calibration Spherical Object subsatellites to test Russian radars. These were released between December 27, 1989 and November 1, 1991. While Cosmos 2053 re-entered in 1997, by May 1999 the S5M upper stage was still in a 471 km x 485 km x 73.5 deg orbit. An on-board explosion blew it into 25 new objects.
1990 January 25 - .
17:15 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2057 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 53.00 days. Decay Date: 1990-03-19 . USAF Sat Cat: 20457 . COSPAR: 1990-009A. Apogee: 330 km (200 mi). Perigee: 183 km (113 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1990 January 30 - .
11:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 2058 - .
Payload: Tselina-D no. 68. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 20465 . COSPAR: 1990-010A. Apogee: 645 km (400 mi). Perigee: 616 km (382 mi). Inclination: 82.50 deg. Period: 97.30 min. Investigation of outer space. .
1990 February 6 - .
16:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2059 - .
Mass: 500 kg (1,100 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1990-11-12 . USAF Sat Cat: 20476 . COSPAR: 1990-012A. Apogee: 1,585 km (984 mi). Perigee: 184 km (114 mi). Inclination: 65.80 deg. Period: 102.70 min. Released 10 Romb radar calibration subsatellites..
1990 February 28 - .
07:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP1.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- USA 53 - .
Payload: KH-12 no. 1. Mass: 19,600 kg (43,200 lb). Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Misty.
Decay Date: 1990-03-31 . USAF Sat Cat: 20516 . COSPAR: 1990-019B. Apogee: 207 km (128 mi). Perigee: 198 km (123 mi). Inclination: 62.00 deg. Period: 88.60 min.
Deployed from STS-36 February 28, 1990. Said to be designated 'Misty', and believed to be the first maneouvering stealth satellite. Barely visible, it was rediscovered by amateur observors in October 1990, with a ground track that repeated every nine days. It maneouvered again in early November 1990, changing its inclination by 1.2 degrees and entering a lower orbit with a three-day repeating ground track. Amateurs again found it in 1996 and 1997 in a 66.2 degree orbit with a 99.4 minute period. The decay date for the active satellite is believed to refer instead to debris; the actually satellite was probably deorbited after 1997, perhaps after USA 144 (Misty 2?) was put into operation.
1990 March 14 - .
15:27 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2060 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1991-09-01 . USAF Sat Cat: 20525 . COSPAR: 1990-022A. Apogee: 418 km (259 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.80 min. Ocean surveillance..
1990 March 27 - .
16:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2063 - .
Payload: Oko #62. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 20536 . COSPAR: 1990-026A. Apogee: 35,210 km (21,870 mi). Perigee: 5,329 km (3,311 mi). Inclination: 67.80 deg. Period: 721.50 min. Covered Oko constellation plane 2 - 317 degree longitude of ascending node..
1990 April 13 - .
18:53 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2072 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 225.00 days. Decay Date: 1990-11-21 . USAF Sat Cat: 20568 . COSPAR: 1990-033A. Apogee: 270 km (160 mi). Perigee: 232 km (144 mi). Inclination: 64.70 deg. Period: 89.50 min. Photo/digital surveillance..
1990 April 25 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2075 - .
Mass: 1,000 kg (2,200 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1992-02-20 . USAF Sat Cat: 20581 . COSPAR: 1990-038A. Apogee: 439 km (272 mi). Perigee: 418 km (259 mi). Inclination: 74.00 deg. Period: 93.20 min. Released 25 Romb radar calibration subsatellites..
1990 April 28 - .
11:37 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
- Cosmos 2076 - .
Payload: Oko #63. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 20596 . COSPAR: 1990-040A. Apogee: 34,572 km (21,482 mi). Perigee: 5,748 km (3,571 mi). Inclination: 68.00 deg. Period: 717.10 min. Covered Oko constellation plane 1 - 277 degree longitude of ascending node..
1990 May 7 - .
18:39 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2077 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 58.00 days. Decay Date: 1990-07-04 . USAF Sat Cat: 20604 . COSPAR: 1990-042A. Apogee: 328 km (203 mi). Perigee: 182 km (113 mi). Inclination: 62.90 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1990 May 15 - .
09:55 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2078 - .
Payload: Yantar-1KFT no. 12. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 44.00 days. Decay Date: 1990-06-28 . USAF Sat Cat: 20615 . COSPAR: 1990-044A. Apogee: 280 km (170 mi). Perigee: 196 km (121 mi). Inclination: 70.00 deg. Period: 89.30 min. Topographic mapping for the Army General Staff..
1990 May 22 - .
05:14 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/2.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2082 - .
Payload: Tselina-2 no. 9. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 20624 . COSPAR: 1990-046A. Apogee: 857 km (532 mi). Perigee: 838 km (520 mi). Inclination: 71.00 deg. Period: 101.90 min.
1990 June 8 - .
05:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 405A.
- USA 59 - .
Payload: Intruder 1. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 20641 . COSPAR: 1990-050A. Apogee: 284 km (176 mi). Perigee: 268 km (166 mi). Inclination: 61.00 deg. Period: 90.00 min. First launch by Titan 4 of new generation of NOSS naval reconnaissance satellites. However earlier NOSS weighed only 2,000 kg; Titan 4 booster has seven times this capacity. What else was launched?.
- USA 62 - .
Payload: Intruder 1. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 20692 . COSPAR: 1990-050D. Apogee: 1,303 km (810 mi). Perigee: 920 km (572 mi). Inclination: 63.42 deg. Period: 107.44 min.
- USA 61 - .
Payload: Intruder 1. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 20691 . COSPAR: 1990-050C. Apogee: 1,304 km (810 mi). Perigee: 920 km (571 mi). Inclination: 63.43 deg. Period: 107.44 min.
- USA 60 - .
Payload: Intruder 1. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 20682 . COSPAR: 1990-050B. Apogee: 1,146 km (712 mi). Perigee: 1,071 km (665 mi). Inclination: 63.40 deg. Period: 107.45 min.
1990 June 21 - .
20:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
FAILURE: Fourth stage failure..
Failed Stage: U.
- Cosmos 2084 - .
Payload: Oko #64. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 1990-06-21 . USAF Sat Cat: 20663 . COSPAR: 1990-055A. Apogee: 666 km (413 mi). Perigee: 582 km (361 mi). Inclination: 62.80 deg. Period: 97.20 min. Launched into an erroneous orbit. There was no communication with the satellite. Covered Oko constellation plane 6 - 115 degree longitude of ascending node..
1990 July 25 - .
18:13 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
- Cosmos 2087 - .
Payload: Oko #65. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 20707 . COSPAR: 1990-064A. Apogee: 36,991 km (22,985 mi). Perigee: 3,357 km (2,085 mi). Inclination: 67.50 deg. Period: 717.60 min. Replaced Cosmos 2084. Covered Oko constellation plane 6 - 117 degree longitude of ascending node..
1990 August 3 - .
19:45 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2089 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1990-10-01 . USAF Sat Cat: 20732 . COSPAR: 1990-069A. Apogee: 320 km (190 mi). Perigee: 187 km (116 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1990 August 23 - .
16:17 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2096 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1992-08-30 . USAF Sat Cat: 20765 . COSPAR: 1990-075A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1990 August 28 - .
07:49 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
- Cosmos 2097 - .
Payload: Oko #66. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2014-12-28 . USAF Sat Cat: 20767 . COSPAR: 1990-076A. Apogee: 37,021 km (23,003 mi). Perigee: 3,383 km (2,102 mi). Inclination: 66.50 deg. Period: 718.80 min. Covered Oko constellation plane 3 - 357 degree longitude of ascending node..
1990 August 28 - .
15:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2098 - .
Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 20774 . COSPAR: 1990-078A. Apogee: 1,747 km (1,085 mi). Perigee: 392 km (243 mi). Inclination: 83.00 deg. Period: 106.60 min. Radar calibration mission..
1990 October 1 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Cosmos 2101 - .
Payload: Orlets-1 no. 2. Mass: 6,700 kg (14,700 lb). Nation: Russia.
Agency: MOM.
Program: Orlets.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Duration: 60.00 days. Decay Date: 1990-11-30 . USAF Sat Cat: 20828 . COSPAR: 1990-087A. Apogee: 304 km (188 mi). Perigee: 162 km (100 mi). Inclination: 64.80 deg. Period: 89.20 min. Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited..
1990 October 4 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/2.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
FAILURE: First stage engine exploded after 3 seconds..
Failed Stage: 1.
1990 October 5 - .
06:14 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-1 No. 3 - .
Payload: FSW-1 No. 03. Mass: 2,100 kg (4,600 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Decay Date: 1990-10-23 . USAF Sat Cat: 20838 . COSPAR: 1990-089A. Apogee: 312 km (193 mi). Perigee: 208 km (129 mi). Inclination: 57.00 deg. Period: 89.70 min. Fanhui Shi Weixing recoverable satellite; carried biological research experiments..
1990 October 16 - .
19:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2102 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 57.00 days. Decay Date: 1990-12-12 . USAF Sat Cat: 20909 . COSPAR: 1990-092A. Apogee: 340 km (210 mi). Perigee: 184 km (114 mi). Inclination: 62.90 deg. Period: 89.80 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1990 November 13 - .
00:37 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 402A/IUS.
- USA 65 - .
Payload: DSP-1 Block 14 F15. Mass: 2,360 kg (5,200 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 2006-01-01 . USAF Sat Cat: 20929 . COSPAR: 1990-095A. Apogee: 35,699 km (22,182 mi). Perigee: 35,614 km (22,129 mi). Inclination: 3.10 deg. Period: 1,421.80 min. DSP-1 Block 14 ballistic missile launch detection satellite. Positioned in geosynchronous orbit at 105 deg E in 1991; 70 deg E in 1991-1992; 5 deg E in 1992-1993; 35 deg W in 1993; 38 deg W in 1999-2004. Believed to have been taken out of service in 2006..
1990 November 14 - .
06:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2103 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1991-04-03 . USAF Sat Cat: 20933 . COSPAR: 1990-096A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1990 November 15 - .
23:48 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP1.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- USA 67 - .
Mass: 2,500 kg (5,500 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: Quasar.
USAF Sat Cat: 20963 . COSPAR: 1990-097B. Apogee: 35,800 km (22,200 mi). Perigee: 35,800 km (22,200 mi). Inclination: 0.00 deg. Period: 1,440.00 min. Deployed from STS 38 15 November 1990. Boosted to geostationary orbit. Last known longitude (31 December 1990) 99.16 deg W drifting at 0.050 deg W per day..
1990 November 20 - .
02:33 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
- Cosmos 2105 - .
Payload: Oko #67. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2008-01-21 . USAF Sat Cat: 20941 . COSPAR: 1990-099A. Apogee: 38,453 km (23,893 mi). Perigee: 1,936 km (1,202 mi). Inclination: 65.00 deg. Period: 718.50 min. Covered Oko constellation planes 3/4 - 12 degree longitude of ascending node..
1990 December 4 - .
00:48 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2107 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1991-01-31 . USAF Sat Cat: 20985 . COSPAR: 1990-108A. Apogee: 416 km (258 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.80 min. Ocean surveillance..
1990 December 4 - .
18:30 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2108 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 55.00 days. Decay Date: 1991-01-28 . USAF Sat Cat: 21000 . COSPAR: 1990-109A. Apogee: 289 km (179 mi). Perigee: 164 km (101 mi). Inclination: 62.80 deg. Period: 89.00 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1990 December 21 - .
06:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1 or LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2113 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 172.00 days. Decay Date: 1991-06-11 . USAF Sat Cat: 21026 . COSPAR: 1990-113A. Apogee: 261 km (162 mi). Perigee: 225 km (139 mi). Inclination: 64.80 deg. Period: 89.40 min. Photo/digital surveillance..
1991 January 18 - .
11:34 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2122 - .
Mass: 3,000 kg (6,600 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-P.
Decay Date: 1993-03-28 . USAF Sat Cat: 21065 . COSPAR: 1991-005A. Apogee: 415 km (257 mi). Perigee: 401 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. Ocean surveillance..
1991 February 7 - .
18:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2124 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1991-04-07 . USAF Sat Cat: 21092 . COSPAR: 1991-008A. Apogee: 316 km (196 mi). Perigee: 186 km (115 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1991 February 14 - .
08:31 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1991 February 15 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC1/LC31?.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2134 - .
Payload: Yantar-1KFT no. 13. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 45.00 days. Decay Date: 1991-04-01 . USAF Sat Cat: 21116 . COSPAR: 1991-011A. Apogee: 306 km (190 mi). Perigee: 190 km (110 mi). Inclination: 64.70 deg. Period: 89.50 min. Topographic mapping for the Army General Staff..
1991 March 8 - .
12:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 403A.
- USA 69 - .
Payload: Lacrosse 2. Nation: USA.
Agency: CIA,
NRO.
Manufacturer: Martin.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Lacrosse satellite.
USAF Sat Cat: 21147 . COSPAR: 1991-017A. Apogee: 662 km (411 mi). Perigee: 420 km (260 mi). Inclination: 68.00 deg. Period: 95.50 min. Still operating December 1997. First West Coast launch of a Titan 4..
1991 March 19 - .
14:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2137 - .
Mass: 1,000 kg (2,200 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1995-04-03 . USAF Sat Cat: 21190 . COSPAR: 1991-021A. Apogee: 364 km (226 mi). Perigee: 356 km (221 mi). Inclination: 65.80 deg. Period: 91.70 min. Radar calibration mission..
1991 March 26 - .
13:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2138 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1991-05-24 . USAF Sat Cat: 21203 . COSPAR: 1991-023A. Apogee: 343 km (213 mi). Perigee: 161 km (100 mi). Inclination: 67.10 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1991 March 31 - .
15:12 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K.
- Almaz 1 - .
Payload: Almaz-K s/n 305. Mass: 18,550 kg (40,890 lb). Nation: Russia.
Agency: MOM.
Program: Almaz.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Almaz.
Spacecraft: Almaz-T.
Decay Date: 1992-10-17 . USAF Sat Cat: 21213 . COSPAR: 1991-024A. Apogee: 351 km (218 mi). Perigee: 337 km (209 mi). Inclination: 72.70 deg. Period: 91.40 min.
Second flight of Almaz radar imaging satellite. Surveyed the territory of the Soviet Union and of other countries for purposes of geology, cartography, oceanology, ecology and agriculture, and studied the ice situation at high latitudes. Launched eight months after its target date into an initial operational orbit of approximately 270 km with an inclination of 72.7 degrees, slightly higher than the 71.9 degrees inclination of Cosmos 1870. Unfortunately, the failure of one of the SAR antennas to deploy fully rendered that side inoperable. Returned images of 10 to 15 meter resolution through 17 October 1992. Its radiometer provided images of 10 to 30 km radiometer resolution over a 600 km swath. Its engines completed 760,000 firings during its 18 month service life.
1991 May 24 - .
15:29 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2149 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 41.00 days. Decay Date: 1991-07-04 . USAF Sat Cat: 21315 . COSPAR: 1991-036A. Apogee: 285 km (177 mi). Perigee: 173 km (107 mi). Inclination: 67.10 deg. Period: 89.10 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1991 June 13 - .
15:41 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 2151 - .
Payload: Tselina-D no. 70. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 21422 . COSPAR: 1991-042A. Apogee: 653 km (405 mi). Perigee: 625 km (388 mi). Inclination: 82.50 deg. Period: 97.50 min. Investigation of outer space. .
1991 June 25 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Second stage malfunction - no stable orbit..
Failed Stage: 2.
- Romb - .
Nation: Russia.
Agency: UNKS.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Released 25 Romb radar calibration subsatellites..
1991 July 10 - .
14:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2153 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 247.00 days. Decay Date: 1992-03-13 . USAF Sat Cat: 21560 . COSPAR: 1991-049A. Apogee: 267 km (165 mi). Perigee: 182 km (113 mi). Inclination: 64.90 deg. Period: 89.00 min. Photo/digital surveillance..
1991 August 30 - .
08:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
FAILURE: Second stage exploded due to heating problems in main engine..
Failed Stage: 2.
1991 September 13 - .
17:51 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/23.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1991 September 19 - .
16:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2156 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1991-11-17 . USAF Sat Cat: 21713 . COSPAR: 1991-066A. Apogee: 345 km (214 mi). Perigee: 160 km (90 mi). Inclination: 67.10 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1991 October 9 - .
13:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Cosmos 2163 - .
Payload: Orlets-1 no. 3. Mass: 6,500 kg (14,300 lb). Nation: Russia.
Agency: MOM.
Program: Orlets.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Duration: 58.00 days. Decay Date: 1991-12-07 . USAF Sat Cat: 21741 . COSPAR: 1991-071A. Apogee: 308 km (191 mi). Perigee: 169 km (105 mi). Inclination: 64.80 deg. Period: 89.30 min. Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited..
1991 October 10 - .
14:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2164 - .
Mass: 750 kg (1,650 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 1992-12-12 . USAF Sat Cat: 21743 . COSPAR: 1991-072A. Apogee: 541 km (336 mi). Perigee: 256 km (159 mi). Inclination: 74.00 deg. Period: 92.50 min. Radar calibration mission..
1991 November 8 - .
07:07 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 403A.
- USA 72 - .
Payload: Intruder 2. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 21775 . COSPAR: 1991-076A. Apogee: 1,321 km (820 mi). Perigee: 799 km (496 mi). Inclination: 63.40 deg. Period: 106.40 min. Second launch by Titan 4 of new generation of NOSS naval reconnaissance satellites. However earlier NOSS weighed only 2,000 kg; Titan 4 booster has seven times this capacity. What else was launched?.
- USA 76 - .
Payload: Intruder 2. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 21808 . COSPAR: 1991-076D. Apogee: 1,270 km (789 mi). Perigee: 954 km (593 mi). Inclination: 63.43 deg. Period: 107.44 min.
- USA 74 - .
Payload: Intruder 2. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 21799 . COSPAR: 1991-076C. Apogee: 1,270 km (789 mi). Perigee: 954 km (593 mi). Inclination: 63.43 deg. Period: 107.44 min.
- USA 77 - .
Payload: Intruder 2. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 21809 . COSPAR: 1991-076E. Apogee: 1,270 km (789 mi). Perigee: 954 km (593 mi). Inclination: 63.43 deg. Period: 107.44 min.
1991 November 20 - .
19:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2171 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1992-01-17 . USAF Sat Cat: 21787 . COSPAR: 1991-078A. Apogee: 321 km (199 mi). Perigee: 187 km (116 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1991 November 24 - .
23:44 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP1.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- USA 75 - .
Payload: DSP-1 Block 14 F16. Mass: 2,360 kg (5,200 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 21805 . COSPAR: 1991-080B. Apogee: 35,787 km (22,236 mi). Perigee: 35,795 km (22,241 mi). Inclination: 2.50 deg. Period: 1,421.90 min.
DSP-1 Block 14 ballistic missile launch detection satellite, deployed from shuttle STS-44 on 25 November 1991. Only DSP launched from the shuttle before the Challenger disaster moved the payload to the Titan 4. Positioned in geosynchronous orbit at 130 deg W in 1992; 70 deg E in 1992; 8 deg E in 1999; 40 deg W in 2000. Still in service as of March 2007.
1991 December 17 - .
11:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2174 - .
Payload: Yantar-1KFT no. 14. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 44.00 days. Decay Date: 1992-01-30 . USAF Sat Cat: 21816 . COSPAR: 1991-085A. Apogee: 306 km (190 mi). Perigee: 193 km (119 mi). Inclination: 64.90 deg. Period: 89.50 min. Topographic mapping for the Army General Staff..
1992 January 21 - .
15:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2175 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1992-03-20 . USAF Sat Cat: 21844 . COSPAR: 1992-001A. Apogee: 347 km (215 mi). Perigee: 158 km (98 mi). Inclination: 67.10 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1992 January 24 - .
01:18 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2176 - .
Payload: Oko #68. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2012-01-17 . USAF Sat Cat: 21847 . COSPAR: 1992-003A. Apogee: 37,349 km (23,207 mi). Perigee: 3,058 km (1,900 mi). Inclination: 66.10 deg. Period: 718.80 min. Covered Oko constellation plane 6 - 119 degree longitude of ascending node..
1992 February 5 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
FAILURE: Second stage malfunction due to heating problems in main engine..
Failed Stage: 2.
1992 April 1 - .
14:18 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2182 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1992-05-30 . USAF Sat Cat: 21920 . COSPAR: 1992-016A. Apogee: 284 km (176 mi). Perigee: 166 km (103 mi). Inclination: 67.10 deg. Period: 89.00 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1992 April 8 - .
12:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2183 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 314.00 days. Decay Date: 1993-02-16 . USAF Sat Cat: 21928 . COSPAR: 1992-018A. Apogee: 289 km (179 mi). Perigee: 237 km (147 mi). Inclination: 64.90 deg. Period: 89.80 min. Photo/digital surveillance..
1992 April 25 - .
08:53 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan II SLV.
- USA 81 - .
Payload: SBWASS R3. Mass: 1,700 kg (3,700 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Singleton.
USAF Sat Cat: 21949 . COSPAR: 1992-023A. Apogee: 175 km (108 mi). Perigee: 145 km (90 mi). Inclination: 84.90 deg. Period: 89.30 min. Signals intelligence satellite; possibly some kind of imaging also done. On-board propulsion boosts spacecraft to 800 km operating orbit..
1992 April 29 - .
10:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2185 - .
Payload: Yantar-1KFT no. 15. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 43.00 days. Decay Date: 1992-06-11 . USAF Sat Cat: 21953 . COSPAR: 1992-025A. Apogee: 274 km (170 mi). Perigee: 209 km (129 mi). Inclination: 70.00 deg. Period: 89.30 min. Topographic mapping for the Army General Staff..
1992 May 28 - .
19:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2186 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 57.00 days. Decay Date: 1992-07-24 . USAF Sat Cat: 21973 . COSPAR: 1992-029A. Apogee: 327 km (203 mi). Perigee: 187 km (116 mi). Inclination: 62.80 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1992 July 8 - .
09:53 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
- Cosmos 2196 - .
Payload: Oko #69. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2016-09-27 . USAF Sat Cat: 22017 . COSPAR: 1992-040A. Apogee: 36,915 km (22,937 mi). Perigee: 3,433 km (2,133 mi). Inclination: 67.10 deg. Period: 717.70 min. Covered Oko constellation plane 5 - 75 degree longitude of ascending node..
1992 July 24 - .
19:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2203 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 60.00 days. Decay Date: 1992-09-22 . USAF Sat Cat: 22052 . COSPAR: 1992-045A. Apogee: 311 km (193 mi). Perigee: 189 km (117 mi). Inclination: 62.80 deg. Period: 89.50 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1992 August 9 - .
08:00 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
Launch Pad: LA2B?.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- FSW-2 No. 1 - .
Payload: FSW-2 No. 01. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 15.00 days. Decay Date: 1992-09-01 . USAF Sat Cat: 22072 . COSPAR: 1992-051A. Apogee: 332 km (206 mi). Perigee: 171 km (106 mi). Inclination: 63.10 deg. Period: 89.50 min. Fanhui Shi Weixing recoverable imaging satellite; carried microgravity experiments; capsule returned August 25 after 15 days in orbit..
1992 September 10 - .
18:01 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/23.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1992 September 22 - .
16:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2210 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1992-11-20 . USAF Sat Cat: 22133 . COSPAR: 1992-062A. Apogee: 353 km (219 mi). Perigee: 160 km (90 mi). Inclination: 67.20 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1992 October 6 - .
06:20 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
Launch Pad: LA2B?.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-1 No. 4 - .
Payload: FSW-1 No. 04. Mass: 2,100 kg (4,600 lb). Nation: China.
Agency: MAI.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 6.00 days. Decay Date: 1992-10-31 . USAF Sat Cat: 22162 . COSPAR: 1992-064B. Apogee: 309 km (192 mi). Perigee: 213 km (132 mi). Inclination: 63.00 deg. Period: 89.70 min. Fanhui Shi Weixing recoverable imaging satellite; carried remote sensing, microgravity experiments; capsule recovered October 13 after 6 days in orbit..
1992 October 21 - .
10:21 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
- Cosmos 2217 - .
Payload: Oko #70. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2010-11-07 . USAF Sat Cat: 22189 . COSPAR: 1992-069A. Apogee: 36,700 km (22,800 mi). Perigee: 3,642 km (2,263 mi). Inclination: 67.10 deg. Period: 717.50 min. Covered Oko constellation plane 8 - 201 degree longitude of ascending node..
1992 November 17 - .
07:47 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2219 - .
Payload: Tselina-2 no. 13. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 22219 . COSPAR: 1992-076A. Apogee: 854 km (530 mi). Perigee: 845 km (525 mi). Inclination: 71.00 deg. Period: 101.90 min.
1992 November 20 - .
15:29 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2220 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 59.00 days. Decay Date: 1993-01-18 . USAF Sat Cat: 22226 . COSPAR: 1992-077A. Apogee: 341 km (211 mi). Perigee: 164 km (101 mi). Inclination: 67.20 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1992 November 24 - .
04:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 2221 - .
Payload: Tselina-D no. 71. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 22236 . COSPAR: 1992-080A. Apogee: 662 km (411 mi). Perigee: 630 km (390 mi). Inclination: 82.50 deg. Period: 97.70 min. Investigation of outer space. .
1992 November 25 - .
12:18 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M-PVB.
- Cosmos 2222 - .
Payload: Oko #71. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 22238 . COSPAR: 1992-081A. Apogee: 35,026 km (21,764 mi). Perigee: 5,330 km (3,310 mi). Inclination: 67.10 deg. Period: 717.80 min. Covered Oko constellation plane 1 - 270 degree longitude of ascending node..
1992 November 28 - .
21:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 404A.
- USA 86 - .
Payload: EIS-1. Mass: 19,600 kg (43,200 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: EIS.
Decay Date: 2000-06-05 . USAF Sat Cat: 22251 . COSPAR: 1992-083A. Apogee: 911 km (566 mi). Perigee: 256 km (159 mi). Inclination: 97.70 deg. Period: 96.40 min. Optical reconnaisance satellite built for the US National Reconnaissance Office..
1992 December 9 - .
11:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2223 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 372.00 days. Decay Date: 1993-12-16 . USAF Sat Cat: 22260 . COSPAR: 1992-087A. Apogee: 271 km (168 mi). Perigee: 238 km (147 mi). Inclination: 64.60 deg. Period: 89.60 min. Photo/digital surveillance..
1992 December 17 - .
12:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1992 December 22 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2225 - .
Payload: Orlets-1 no. 4. Mass: 6,500 kg (14,300 lb). Nation: Russia.
Agency: MOM.
Program: Orlets.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Duration: 58.00 days. Decay Date: 1993-02-18 . USAF Sat Cat: 22280 . COSPAR: 1992-091A. Apogee: 313 km (194 mi). Perigee: 169 km (105 mi). Inclination: 64.90 deg. Period: 89.30 min. Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited..
1992 December 25 - .
05:56 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2227 - .
Payload: Tselina-2 no. 14. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 22284 . COSPAR: 1992-093A. Apogee: 855 km (531 mi). Perigee: 845 km (525 mi). Inclination: 71.00 deg. Period: 101.90 min.
1992 December 25 - .
20:07 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 2228 - .
Payload: Tselina-D no. 72. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 22286 . COSPAR: 1992-094A. Apogee: 666 km (413 mi). Perigee: 628 km (390 mi). Inclination: 82.50 deg. Period: 97.70 min. Investigation of outer space. .
1993 January 19 - .
14:49 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2231 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 65.00 days. Decay Date: 1993-03-25 . USAF Sat Cat: 22317 . COSPAR: 1993-004A. Apogee: 342 km (212 mi). Perigee: 163 km (101 mi). Inclination: 67.20 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1993 January 26 - .
15:55 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2232 - .
Payload: Oko #72. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 22321 . COSPAR: 1993-006A. Apogee: 35,870 km (22,280 mi). Perigee: 4,502 km (2,797 mi). Inclination: 67.60 deg. Period: 718.10 min. Covered Oko constellation plane 4 - 34 degree longitude of ascending node..
1993 March 26 - .
02:21 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2237 - .
Payload: Tselina-2 no. 15. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 22565 . COSPAR: 1993-016A. Apogee: 855 km (531 mi). Perigee: 847 km (526 mi). Inclination: 70.90 deg. Period: 102.00 min.
1993 March 30 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2238 - .
Payload: US-PU s/n 1. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Duration: 567.00 days. Decay Date: 1994-12-10 . USAF Sat Cat: 22585 . COSPAR: 1993-018A. Apogee: 416 km (258 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.70 min. First launch of new EORSAT, first of at 120 degree intervals on the same orbit with a 0 degree ascending node. Ocean surveillance..
1993 April 2 - .
14:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2240 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 66.00 days. Decay Date: 1993-06-07 . USAF Sat Cat: 22592 . COSPAR: 1993-021A. Apogee: 320 km (190 mi). Perigee: 188 km (116 mi). Inclination: 62.80 deg. Period: 89.60 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1993 April 6 - .
19:07 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2241 - .
Payload: Oko #73. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 22594 . COSPAR: 1993-022A. Apogee: 36,804 km (22,868 mi). Perigee: 3,564 km (2,214 mi). Inclination: 66.00 deg. Period: 718.00 min. Covered Oko constellation plane 7 - 161 degree longitude of ascending node..
1993 April 16 - .
07:49 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Cosmos 2242 - .
Payload: Tselina-D no. 73. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
USAF Sat Cat: 22626 . COSPAR: 1993-024A. Apogee: 665 km (413 mi). Perigee: 629 km (390 mi). Inclination: 82.50 deg. Period: 97.70 min. Ocean surveillance. Investigation of outer space. .
1993 April 27 - .
10:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2243 - .
Payload: Yantar-1KFT no. 16. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 9.00 days. Decay Date: 1993-05-06 . USAF Sat Cat: 22641 . COSPAR: 1993-028A. Apogee: 233 km (144 mi). Perigee: 189 km (117 mi). Inclination: 70.40 deg. Period: 88.70 min. Topographic mapping for the Army General Staff. Mission normally would have run 44 days..
1993 April 28 - .
03:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2244 - .
Payload: US-PU s/n 2. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Duration: 657.00 days. Decay Date: 1995-03-18 . USAF Sat Cat: 22643 . COSPAR: 1993-029A. Apogee: 416 km (258 mi). Perigee: 402 km (249 mi). Inclination: 65.00 deg. Period: 92.80 min. Second launch of new EORSAT, second of three stationed at 120 degree intervals on the same orbit with a 0 degree ascending node..
1993 June 25 - .
23:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC5.
LV Family:
Scout.
Launch Vehicle:
Scout G-1.
- Radcal - .
Mass: 95 kg (209 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Radcal.
USAF Sat Cat: 22698 . COSPAR: 1993-041A. Apogee: 882 km (548 mi). Perigee: 753 km (467 mi). Inclination: 89.60 deg. Period: 101.20 min. Radar calibration. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .
1993 July 7 - .
07:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2258 - .
Payload: US-PY s/n 3. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Duration: 603.00 days. Decay Date: 1995-06-08 . USAF Sat Cat: 22709 . COSPAR: 1993-044A. Apogee: 417 km (259 mi). Perigee: 400 km (240 mi). Inclination: 65.00 deg. Period: 92.80 min. Third launch of new EORSAT, final of three stationed at 120 degree intervals on the same orbit with a 0 degree ascending node. Ocean surveillance..
1993 July 14 - .
16:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2259 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 11.00 days. Decay Date: 1993-07-25 . USAF Sat Cat: 22716 . COSPAR: 1993-045A. Apogee: 349 km (216 mi). Perigee: 168 km (104 mi). Inclination: 67.10 deg. Period: 89.70 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1993 August 2 - .
19:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 403A.
FAILURE: Radial cut inadvertently made in SRM during repairs resulted in explosion of SRM and vehicle at T+101 seconds..
Failed Stage: 0.
- NOSS 19 - .
Payload: Intruder 3. Nation: USA.
Agency: USN.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
Decay Date: 1993-08-02 . Apogee: 33 km (20 mi). Third attempted launch by Titan 4 of new generation of NOSS naval reconnaissance satellites. No known launches of this system thereafter..
1993 August 10 - .
14:53 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2261 - .
Payload: Oko #74. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2012-12-31 . USAF Sat Cat: 22741 . COSPAR: 1993-051A. Apogee: 35,967 km (22,348 mi). Perigee: 4,370 km (2,710 mi). Inclination: 66.60 deg. Period: 717.40 min. Covered Oko constellation plane 9 - 235 degree longitude of ascending node..
1993 September 7 - .
13:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Cosmos 2262 - .
Payload: Orlets-1 no. 5. Mass: 6,500 kg (14,300 lb). Nation: Russia.
Agency: MOM.
Program: Orlets.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Duration: 102.00 days. Decay Date: 1993-12-18 . USAF Sat Cat: 22789 . COSPAR: 1993-057A. Apogee: 261 km (162 mi). Perigee: 182 km (113 mi). Inclination: 64.90 deg. Period: 88.90 min. Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited. First launch that demonstrated doubled operational life..
1993 September 16 - .
07:36 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2263 - .
Payload: Tselina-2 no. 16. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 22802 . COSPAR: 1993-059A. Apogee: 857 km (532 mi). Perigee: 845 km (525 mi). Inclination: 70.90 deg. Period: 102.00 min.
1993 September 17 - .
00:43 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2264 - .
Payload: US-PM s/n 4. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Duration: 564.00 days. Decay Date: 1995-08-07 . USAF Sat Cat: 22808 . COSPAR: 1993-060A. Apogee: 417 km (259 mi). Perigee: 401 km (249 mi). Inclination: 65.00 deg. Period: 92.80 min. EORSAT, first of three to be stationed at 120 degree intervals on the same orbit with a 215 degree ascending node. However cutbacks in program resulted in the constellation not being completed. Ocean surveillance..
1993 October 8 - .
08:00 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
Launch Pad: LA2B?.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-1 No. 5 - .
Payload: Jian Bing 93. Mass: 2,099 kg (4,627 lb). Nation: China.
Agency: CASC.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Decay Date: 1993-10-28 . USAF Sat Cat: 22859 . COSPAR: 1993-063A. Apogee: 2,860 km (1,770 mi). Perigee: 181 km (112 mi). Inclination: 56.60 deg. Period: 116.50 min.
The only FSW-1 mission conducted during 1993-1994 was launched into an orbit of 209 km by 300 km at an inclination of 57.0 deg. In addition to an Earth observation Payload, FSW-1 5 carried microgravity research equipment and a diamond-studded medallion commemorating the 100th anniversary of Chairman Mao Tse-Tung's birth. The spacecraft operated normally until 16 October when an attempt to recover the satellite failed. An attitude control system failure aligned the spacecraft 90 deg from its desired position, causing the re-entry capsule to be pushed into a higher elliptical orbit (179 km by 3031 km) instead of returning to Earth. Natural decay did not bring the capsule back until March 12, 1996.
1993 October 26 - .
10:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2265 - .
Mass: 500 kg (1,100 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 2003-08-11 . USAF Sat Cat: 22875 . COSPAR: 1993-067A. Apogee: 1,557 km (967 mi). Perigee: 290 km (180 mi). Inclination: 82.90 deg. Period: 103.50 min. Radar calibration mission..
1993 November 5 - .
08:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2267 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 418.00 days. Decay Date: 1994-12-28 . USAF Sat Cat: 22904 . COSPAR: 1993-071A. Apogee: 281 km (174 mi). Perigee: 228 km (141 mi). Inclination: 70.40 deg. Period: 89.60 min. Photo/digital surveillance..
1994 February 3 - .
12:10 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP3.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- ODERACS C - .
Payload: Discovery F18 / WSF 1 / BremSat 1 / ODERACS A, .... Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1994-12-31 . USAF Sat Cat: 22992 . COSPAR: 1994-006D. Apogee: 353 km (219 mi). Perigee: 329 km (204 mi). Inclination: 56.90 deg. Period: 91.35 min. Orbital Debris Radar Calibration Sphere; deployed from STS-60. .
- ODERACS D - .
Payload: Discovery F18 / WSF 1 / BremSat 1 / ODERACS A, .... Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1994-12-31 . USAF Sat Cat: 22993 . COSPAR: 1994-006E. Apogee: 353 km (219 mi). Perigee: 329 km (204 mi). Inclination: 56.90 deg. Period: 91.35 min. Orbital Debris Radar Calibration Sphere; deployed from STS-60. .
- ODERACS B - .
Payload: Discovery F18 / WSF 1 / BremSat 1 / ODERACS A, .... Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1994-10-04 . USAF Sat Cat: 22991 . COSPAR: 1994-006C. Apogee: 352 km (218 mi). Perigee: 332 km (206 mi). Inclination: 57.00 deg. Period: 91.40 min. Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- ODERACS E - .
Payload: Discovery F18 / WSF 1 / BremSat 1 / ODERACS A, .... Mass: 5.00 kg (11.00 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1995-03-03 . USAF Sat Cat: 22994 . COSPAR: 1994-006F. Apogee: 356 km (221 mi). Perigee: 337 km (209 mi). Inclination: 57.00 deg. Period: 91.50 min. Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- ODERACS F - .
Payload: Discovery F18 / WSF 1 / BremSat 1 / ODERACS A, .... Mass: 5.00 kg (11.00 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1995-02-24 . USAF Sat Cat: 22995 . COSPAR: 1994-006G. Apogee: 356 km (221 mi). Perigee: 338 km (210 mi). Inclination: 57.00 deg. Period: 91.50 min. Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- ODERACS A - .
Payload: Discovery F18 / WSF 1 / BremSat 1 / ODERACS A, .... Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1994-10-02 . USAF Sat Cat: 22990 . COSPAR: 1994-006B. Apogee: 352 km (218 mi). Perigee: 327 km (203 mi). Inclination: 57.00 deg. Period: 91.30 min. Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1994 March 17 - .
16:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
Launch Pad: LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
1994 April 23 - .
08:01 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2278 - .
Payload: Tselina-2 no. 17. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 23087 . COSPAR: 1994-023A. Apogee: 857 km (532 mi). Perigee: 846 km (525 mi). Inclination: 71.00 deg. Period: 102.00 min.
1994 April 28 - .
17:14 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2280 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 316.00 days. Decay Date: 1995-03-10 . USAF Sat Cat: 23095 . COSPAR: 1994-025A. Apogee: 283 km (175 mi). Perigee: 233 km (144 mi). Inclination: 70.40 deg. Period: 89.70 min. Photo/digital surveillance..
1994 May 3 - .
15:55 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
- USA 103 - .
Payload: Raven 1. Mass: 5,200 kg (11,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: Raven satellite.
USAF Sat Cat: 23097 . COSPAR: 1994-026A. Apogee: 537 km (333 mi). Perigee: 518 km (321 mi). Inclination: 55.10 deg. Period: 95.20 min. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .
1994 May 25 - .
10:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
FAILURE: Stage 2 and 3 failed to separate due to a breakdown of the launch vehicle control system..
Failed Stage: 3.
1994 July 3 - .
08:00 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
Launch Pad: LA2B?.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- FSW-2 No. 2 - .
Payload: FSW-2 No. 02. Mass: 2,600 kg (5,700 lb). Nation: China.
Agency: CASC.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 15.00 days. Decay Date: 1994-09-13 . USAF Sat Cat: 23145 . COSPAR: 1994-037A. Apogee: 350 km (210 mi). Perigee: 207 km (128 mi). Inclination: 62.90 deg. Period: 90.08 min.
The second Fanhui Shi Weixing FSW-2 was launched on 3 July 1994 into an orbit of 173 km by 343 km at an inclination of 63.0 deg. The spacecraft remained in orbit for 15 days, making four small manoeuvres before successfully returning to Earth. The payload included Earth observation systems, a biological experiment, and microgravity research instruments. The retrievable capsule was recovered in China on July 18
1994 July 6 - .
23:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/23.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1994 July 20 - .
17:35 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
Launch Pad: LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2283 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 71.00 days. Decay Date: 1994-09-29 . USAF Sat Cat: 23182 . COSPAR: 1994-042A. Apogee: 313 km (194 mi). Perigee: 179 km (111 mi). Inclination: 67.10 deg. Period: 89.42 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1994 July 29 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2284 - .
Payload: Yantar-1KFT no. 17. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 44.00 days. Decay Date: 1994-09-11 . USAF Sat Cat: 23187 . COSPAR: 1994-044A. Apogee: 274 km (170 mi). Perigee: 211 km (131 mi). Inclination: 70.30 deg. Period: 89.35 min. Topographic mapping for the Army General Staff. Landed September 11 1994..
1994 August 2 - .
20:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2285 - .
Mass: 825 kg (1,818 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 23189 . COSPAR: 1994-045A. Apogee: 1,013 km (629 mi). Perigee: 974 km (605 mi). Inclination: 74.03 deg. Period: 104.98 min. Radar calibration mission..
1994 August 5 - .
01:12 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2286 - .
Payload: Oko #75. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 23194 . COSPAR: 1994-048A. Apogee: 36,384 km (22,607 mi). Perigee: 3,982 km (2,474 mi). Inclination: 67.50 deg. Period: 718.00 min. Covered Oko constellation plane 5 - 78 degree longitude of ascending node..
1994 August 26 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2290 - .
Payload: Orlets-2 no. 1. Mass: 13,000 kg (28,000 lb). Nation: Russia.
Agency: MO.
Program: Orlets.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-2.
Decay Date: 1995-04-04 . USAF Sat Cat: 23218 . COSPAR: 1994-053A. Apogee: 392 km (243 mi). Perigee: 181 km (112 mi). Inclination: 64.80 deg. Period: 90.25 min. Only flight of Orlets-2 long-duration military reconnaissance satellite with 22 film-return capsules..
1994 August 27 - .
08:58 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
- USA 105 - .
Payload: Mercury ELINT 1. Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Mercury ELINT.
USAF Sat Cat: 23223 . COSPAR: 1994-054A. Apogee: 35,790 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. First launch of Mercury ELINT satellite..
1994 September 27 - .
14:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2292 - .
Mass: 500 kg (1,100 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1.
USAF Sat Cat: 23278 . COSPAR: 1994-061A. Apogee: 1,951 km (1,212 mi). Perigee: 400 km (240 mi). Inclination: 82.99 deg. Period: 108.90 min. Radar calibration mission..
1994 November 2 - .
01:04 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2293 - .
Payload: US-PM s/n 5. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Duration: 497.00 days. Decay Date: 1996-05-13 . USAF Sat Cat: 23336 . COSPAR: 1994-072A. Apogee: 418 km (259 mi). Perigee: 402 km (249 mi). Inclination: 65.03 deg. Period: 92.78 min. Second launch of new EORSAT, second of three to be stationed at 120 degree intervals on the same orbit with a 215 degree ascending node. However cutbacks in program resulted in the constellation not being completed. Ocean surveillance..
1994 November 24 - .
09:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2297 - .
Payload: Tselina-2 no. 18. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 23404 . COSPAR: 1994-077A. Apogee: 857 km (532 mi). Perigee: 845 km (525 mi). Inclination: 71.01 deg. Period: 101.96 min.
1994 December 22 - .
22:19 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 402A/IUS.
- USA 107 - .
Payload: DSP-1 Block 14 F17. Mass: 2,360 kg (5,200 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 23435 . COSPAR: 1994-084A. Apogee: 35,790 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. DSP-1 Block 14 ballistic missile launch detection satellite. Positioned in geosynchronous orbit at 103 deg E in 1999. Still in service as of March 2007..
1994 December 29 - .
11:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2305 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 354.00 days. Decay Date: 1995-12-18 . USAF Sat Cat: 23453 . COSPAR: 1994-088A. Apogee: 288 km (178 mi). Perigee: 231 km (143 mi). Inclination: 64.90 deg. Period: 89.70 min. Photo/digital surveillance..
1995 February 3 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39B.
Launch Platform: MLP2.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- ODERACS IIF - .
Nation: USA.
Agency: NASA.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1996-11-26 . USAF Sat Cat: 23476 . COSPAR: 1995-004H. Apogee: 258 km (160 mi). Perigee: 250 km (150 mi). Inclination: 98.30 deg. Period: 89.60 min. Reentered? .
- ODERACS 2D - .
Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1995-03-02 . USAF Sat Cat: 23474 . COSPAR: 1995-004F. Apogee: 265 km (164 mi). Perigee: 246 km (152 mi). Inclination: 51.60 deg. Period: 89.60 min. Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered Mar 2 .
- ODERACS 2E - .
Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1995-02-27 . USAF Sat Cat: 23475 . COSPAR: 1995-004G. Apogee: 270 km (160 mi). Perigee: 261 km (162 mi). Inclination: 51.60 deg. Period: 89.80 min. Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered Feb 27 .
- ODERACS 2C - .
Mass: 1.00 kg (2.20 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1996-02-07 . USAF Sat Cat: 23473 . COSPAR: 1995-004E. Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered? .
- ODERACS 2B - .
Mass: 4.00 kg (8.80 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1995-09-29 . USAF Sat Cat: 23472 . COSPAR: 1995-004D. Apogee: 179 km (111 mi). Perigee: 177 km (109 mi). Inclination: 51.60 deg. Period: 88.10 min. Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered Sep 29 .
- ODERACS 2A - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Agency: NASA Houston.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: ODERACS.
Decay Date: 1996-03-13 . USAF Sat Cat: 23471 . COSPAR: 1995-004C. Apogee: 280 km (170 mi). Perigee: 268 km (166 mi). Inclination: 51.60 deg. Period: 87.10 min. Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95..
1995 March 2 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2306 - .
Mass: 1,000 kg (2,200 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 2000-10-30 . USAF Sat Cat: 23501 . COSPAR: 1995-008A. Apogee: 513 km (318 mi). Perigee: 466 km (289 mi). Inclination: 65.80 deg. Period: 94.20 min. Released 25 Romb radar calibration subsatellites. Reentered on October 30, 2000..
1995 March 22 - .
16:44 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2311 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 70.00 days. Decay Date: 1995-05-31 . USAF Sat Cat: 23530 . COSPAR: 1995-014A. Apogee: 316 km (196 mi). Perigee: 178 km (110 mi). Inclination: 67.10 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1995 April 5 - .
11:16 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-3 - .
Mass: 189 kg (416 lb). Nation: Israel.
Agency: ISA.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 3.
Decay Date: 2000-10-24 . USAF Sat Cat: 23549 . COSPAR: 1995-018A. Apogee: 694 km (431 mi). Perigee: 366 km (227 mi). Inclination: 143.40 deg. Period: 94.50 min.
1995 May 14 - .
13:45 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
- USA 110 - .
Payload: Orion 3. Mass: 5,200 kg (11,400 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Advanced Orion.
USAF Sat Cat: 23567 . COSPAR: 1995-022A. Apogee: 35,787 km (22,236 mi). Perigee: 35,787 km (22,236 mi). Inclination: 0.00 deg. Period: 1,440.00 min. First launch of 'Advanced Orion' (real code name unknown) new model geostationary ELINT satellite..
1995 May 24 - .
20:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2312 - .
Payload: Oko #76. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2013-09-23 . USAF Sat Cat: 23584 . COSPAR: 1995-026A. Apogee: 36,472 km (22,662 mi). Perigee: 3,890 km (2,410 mi). Inclination: 67.00 deg. Period: 717.90 min. Covered Oko constellation planes 2/3 - 332 degree longitude of ascending node..
1995 June 8 - .
04:43 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2313 - .
Payload: US-PM s/n 6. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Duration: 685.00 days. Decay Date: 1997-07-11 . USAF Sat Cat: 23596 . COSPAR: 1995-028A. Apogee: 419 km (260 mi). Perigee: 410 km (250 mi). Inclination: 65.00 deg. Period: 87.60 min. EORSAT, first of three to be stationed at 120 degree intervals on the same orbit with a 143 degree ascending node. However cutbacks in program resulted in the constellation not being completed. Ocean surveillance..
1995 June 28 - .
18:25 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2314 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 70.00 days. Decay Date: 1995-09-06 . USAF Sat Cat: 23601 . COSPAR: 1995-031A. Apogee: 316 km (196 mi). Perigee: 175 km (108 mi). Inclination: 67.10 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1995 July 7 - .
16:23 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA2.
LV Family:
Ariane.
Launch Vehicle:
Ariane 40.
- Helios 1A - .
Mass: 2,537 kg (5,593 lb). Nation: France.
Agency: CNES,
DGA.
Program: Helios.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: SPOT-4.
Spacecraft: Helios 1A-1B.
USAF Sat Cat: 23605 . COSPAR: 1995-033A. Apogee: 682 km (423 mi). Perigee: 680 km (420 mi). Inclination: 98.10 deg. Period: 98.40 min.
1995 July 10 - .
12:38 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
- USA 112 - .
Payload: Raven 2. Mass: 5,200 kg (11,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: Raven satellite.
USAF Sat Cat: 23609 . COSPAR: 1995-034A. Apogee: 39,000 km (24,000 mi). Perigee: 1,000 km (600 mi). Inclination: 64.00 deg. Period: 720.00 min.
1995 September 29 - .
04:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2320 - .
Mass: 7,000 kg (15,400 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Duration: 365.00 days. Decay Date: 1996-09-28 . USAF Sat Cat: 23674 . COSPAR: 1995-051A. Apogee: 372 km (231 mi). Perigee: 235 km (146 mi). Inclination: 64.90 deg. Period: 89.30 min. Photo/digital surveillance..
1995 October 31 - .
20:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2322 - .
Payload: Tselina-2 no. 19. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 23704 . COSPAR: 1995-058A. Apogee: 854 km (530 mi). Perigee: 847 km (526 mi). Inclination: 71.00 deg. Period: 102.00 min.
1995 December 5 - .
21:18 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 404A.
- USA 116 - .
Payload: EIS-2. Mass: 26,000 kg (57,000 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 23728 . COSPAR: 1995-066A. Apogee: 976 km (606 mi). Perigee: 250 km (150 mi). Inclination: 98.70 deg. Optical reconnaisance satellite built for the US National Reconnaissance Office. Instruments said to include a large telescope with visual and near infrared wavelength CCD sensors and the ICMS mapping system..
1995 December 20 - .
00:52 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2326 - .
Payload: US-PM s/n 7. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Duration: 660.00 days. Decay Date: 1997-11-08 . USAF Sat Cat: 23748 . COSPAR: 1995-071A. Apogee: 415 km (257 mi). Perigee: 406 km (252 mi). Inclination: 65.00 deg. Period: 87.20 min. EORSAT, placed in 215 degree ascending node orbital slot. Ocean surveillance; also performed astrophysics research..
1996 March 14 - .
17:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2331 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 89.00 days. Decay Date: 1996-06-11 . USAF Sat Cat: 23818 . COSPAR: 1996-016A. Apogee: 291 km (180 mi). Perigee: 159 km (98 mi). Inclination: 67.10 deg. Period: 89.00 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..
1996 April 24 - .
13:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2332 - .
Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Taifun-1Yu.
Decay Date: 2005-01-28 . USAF Sat Cat: 23853 . COSPAR: 1996-025A. Apogee: 1,548 km (961 mi). Perigee: 294 km (182 mi). Inclination: 82.90 deg. Period: 102.70 min. Radar calibration mission..
1996 April 24 - .
23:37 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
- USA 118 - .
Payload: Mercury ELINT 2. Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: SIGINT. Spacecraft: Mercury ELINT.
USAF Sat Cat: 23855 . COSPAR: 1996-026A. Apogee: 35,790 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.00 min. Second launch of Mercury ELINT satellite..
1996 May 12 - .
21:32 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 403A.
- USA 122 - .
Payload: Intruder 4. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 23862 . COSPAR: 1996-029D. Apogee: 1,156 km (718 mi). Perigee: 1,060 km (650 mi). Inclination: 63.40 deg. Period: 107.40 min.
- USA 121 - .
Payload: Intruder 4. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 23908 . COSPAR: 1996-029C. Apogee: 1,160 km (720 mi). Perigee: 1,055 km (655 mi). Inclination: 63.40 deg. Period: 107.40 min.
- USA 120 - .
Payload: Intruder 4. Nation: USA.
Agency: NRL,
NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 23907 . COSPAR: 1996-029B. Apogee: 1,157 km (718 mi). Perigee: 1,058 km (657 mi). Inclination: 63.40 deg. Period: 107.40 min.
1996 May 14 - .
08:55 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
FAILURE: Shroud broke up at T+49 seconds..
Failed Stage: S.
- Kometa - .
Payload: Yantar-1KFT no. 18. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: VKS.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Topographic mapping satellite failed to reach orbit..
1996 June 20 - .
18:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
FAILURE: Shroud broke up at T+50seconds..
Failed Stage: S.
- Yantar-4K1 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: VKS.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
High resolution photo reconnaissance mission..
1996 September 4 - .
09:01 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2333 - .
Payload: Tselina-2 no. 20. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 24297 . COSPAR: 1996-051A. Apogee: 852 km (529 mi). Perigee: 849 km (527 mi). Inclination: 70.90 deg. Period: 101.90 min. New heavy ELINT class..
1996 October 20 - .
07:20 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- FSW-2 No. 3 - .
Payload: FSW-2 No. 03. Mass: 2,600 kg (5,700 lb). Nation: China.
Agency: CASC.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 15.00 days. Decay Date: 1996-12-03 . USAF Sat Cat: 24634 . COSPAR: 1996-059A. Apogee: 133 km (82 mi). Perigee: 121 km (75 mi). Inclination: 63.00 deg. Period: 87.00 min. Final launch in the FSW series. Landed in China on November 4 after 15 days in orbit..
1996 December 11 - .
12:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2335 - .
Payload: US-PM s/n 8. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Decay Date: 1999-01-01 . USAF Sat Cat: 24670 . COSPAR: 1996-069A. Apogee: 418 km (259 mi). Perigee: 403 km (250 mi). Inclination: 65.00 deg. Period: 92.80 min. EORSAT, second of three to be stationed at 120 degree intervals on the same orbit with a 143 degree ascending node. However cutbacks in program resulted in the constellation not being completed. Still in operation as of December 1997..
1996 December 20 - .
18:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 404A.
- USA 129 - .
Payload: EIS-3. Mass: 19,600 kg (43,200 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 24680 . COSPAR: 1996-072A. Apogee: 949 km (589 mi). Perigee: 153 km (95 mi). Inclination: 97.90 deg. Optical reconnaisance satellite built for the US National Reconnaissance Office..
1997 January 10 - .
Launch Site:
Plesetsk .
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Oko launch abort - .
Mass: 1,900 kg (4,100 lb). Nation: USA.
Agency: MO.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Oko launch aborted at moment of engine ignition. Spacecraft was intended to cover Oko constellation planes 8/9 - 209 degree longitude of ascending node..
1997 February 23 - .
20:20 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 402B/IUS.
- USA 130 - .
Payload: DSP-1 Block 18 F18. Mass: 2,380 kg (5,240 lb). Nation: USA.
Agency: USAF.
Manufacturer: TRW.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 24737 . COSPAR: 1997-008A. Apogee: 35,790 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. DSP-1 Block 14 ballistic missile launch detection satellite. Positioned in geosynchronous orbit at 70 deg E in 1999. Still in service as of March 2007..
1997 April 9 - .
08:58 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2340 - .
Payload: Oko #77. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MO.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 24761 . COSPAR: 1997-015A. Apogee: 37,201 km (23,115 mi). Perigee: 3,164 km (1,966 mi). Inclination: 65.20 deg. Period: 718.00 min. Covered Oko constellation planes 8/9 - 217 degree longitude of ascending node..
1997 May 14 - .
00:33 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2342 - .
Payload: Oko #78. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MO.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 24800 . COSPAR: 1997-022A. Apogee: 37,820 km (23,500 mi). Perigee: 2,584 km (1,605 mi). Inclination: 66.70 deg. Period: 718.80 min. Covered Oko constellation planes 6/7 - 129 degree longitude of ascending node..
1997 May 15 - .
12:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2343 - .
Payload: Orlets-1 no. 6. Mass: 6,500 kg (14,300 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Program: Orlets.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Duration: 123.00 days. Decay Date: 1997-09-15 . USAF Sat Cat: 24805 . COSPAR: 1997-024A. Apogee: 343 km (213 mi). Perigee: 179 km (111 mi). Inclination: 64.90 deg. Period: 89.40 min.
Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited. This satellite provided Russia with the photo reconnaisance capability after a break of 7 1/2 months. This launch came on the 40th anniversary of the first successful launch of the R-7 rocket, from which the Soyuz-U was derived. It was the 250th launch of the Soyuz-U from Baikonur, the 350th launch from Launch Complex 31, and the 666th launch of a Soyuz-U.
1997 May 20 - .
07:07 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
FAILURE: Strut in first stage engine failed at T+48 seconds..
Failed Stage: 1.
1997 June 6 - .
16:56 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-K/17S40.
- Cosmos 2344 - .
Payload: Arkon-1 s/n 1. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Arkon-1.
USAF Sat Cat: 24827 . COSPAR: 1997-028A. Apogee: 2,739 km (1,701 mi). Perigee: 1,502 km (933 mi). Inclination: 63.40 deg. Period: 130.00 min. First launch in a new series of electro-optical military reconnaisance satellites. .
1997 August 1 - .
20:20 GMT - .
Launch Site:
Point Arguello.
Launch Complex:
Point Arguello WADZ.
Launch Pad: Aircraft from Vandenberg..
Launch Platform: L-1011.
LV Family:
Pegasus.
Launch Vehicle:
Pegasus XL.
- Orbview-2 - .
Payload: Seastar. Nation: USA.
Agency: Orbimage.
Manufacturer: Germantown.
Program: Orbview.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: PegaStar.
Spacecraft: Orbview-2.
USAF Sat Cat: 24883 . COSPAR: 1997-037A. Apogee: 708 km (439 mi). Perigee: 707 km (439 mi). Inclination: 98.20 deg. Period: 98.90 min. Air dropped in Point Arguello WADZ..
1997 August 14 - .
20:49 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1997 October 24 - .
02:32 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 403A.
- USA 133 - .
Payload: Lacrosse 3. Nation: USA.
Agency: CIA,
NRO.
Manufacturer: Martin.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Lacrosse satellite.
USAF Sat Cat: 25017 . COSPAR: 1997-064A. Apogee: 679 km (421 mi). Perigee: 666 km (413 mi). Inclination: 57.00 deg. Still operating December 1997..
1997 November 8 - .
02:05 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
- USA 136 - .
Payload: Raven 3. Mass: 5,200 kg (11,400 lb). Nation: USA.
Agency: NRO,
USAF.
Manufacturer: Kent.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: Raven satellite.
USAF Sat Cat: 25034 . COSPAR: 1997-068A. Apogee: 39,059 km (24,270 mi). Perigee: 1,100 km (600 mi). Inclination: 63.60 deg. Period: 720.00 min.
1997 December 9 - .
07:17 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/19.
Launch Pad: LC90/pad?.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2347 - .
Payload: US-PM s/n 9. Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: MO.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Decay Date: 1999-12-11 . USAF Sat Cat: 25088 . COSPAR: 1997-079A. Apogee: 417 km (259 mi). Perigee: 403 km (250 mi). Inclination: 65.00 deg. Period: 92.80 min. EORSAT, in the 217 degree ascending node slot. Still in operation as of December 1997..
1997 December 15 - .
15:40 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2348 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 120.00 days. Decay Date: 1998-04-14 . USAF Sat Cat: 25095 . COSPAR: 1997-080A. Apogee: 361 km (224 mi). Perigee: 175 km (108 mi). Inclination: 67.10 deg. Period: 89.40 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission. Landed 14 April 1998..
1997 December 24 - .
13:32 GMT - .
Launch Site:
Svobodniy.
Launch Complex:
Svobodniy LC5.
LV Family:
Topol'.
Launch Vehicle:
Start-1.
- Early Bird - .
Payload: EarlyBird. Nation: USA.
Agency: DigitalGlobe.
Manufacturer: McLean.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Early Bird.
Decay Date: 2000-07-27 . USAF Sat Cat: 25123 . COSPAR: 1997-085A. Apogee: 488 km (303 mi). Perigee: 479 km (297 mi). Inclination: 97.30 deg. Period: 94.10 min.
1998 January 22 - .
12:56 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
FAILURE: Launch vehicle failed during second stage burn..
Failed Stage: 2.
- Ofeq-4 - .
Mass: 189 kg (416 lb). Nation: Israel.
Agency: ISA.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 3.
Fell in Mediterranean Sea..
1998 February 17 - .
10:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2349 - .
Payload: Yantar-1KFT s/n 19. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: RAKA.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 44.00 days. Decay Date: 1998-04-02 . USAF Sat Cat: 25167 . COSPAR: 1998-009A. Apogee: 327 km (203 mi). Perigee: 212 km (131 mi). Inclination: 70.40 deg. Period: 89.90 min. Topographic mapping for the Army General Staff. Landed in Kazakhstan April 2 1998..
1998 May 7 - .
08:53 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2351 - .
Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: MO.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 25327 . COSPAR: 1998-027A. Apogee: 37,513 km (23,309 mi). Perigee: 2,806 km (1,743 mi). Inclination: 63.70 deg. Period: 717.10 min.
1998 May 9 - .
01:38 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 401B/Centaur.
- USA 139 - .
Payload: Orion 4. Mass: 5,200 kg (11,400 lb). Nation: USA.
Agency: NRO,
NSA.
Manufacturer: El Segundo.
Class: Surveillance.
Type: SIGINT. Spacecraft: Advanced Orion.
USAF Sat Cat: 25336 . COSPAR: 1998-029A. Apogee: 35,800 km (22,200 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,440.00 min.
1998 June 24 - .
18:29 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2358 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 120.00 days. Decay Date: 1998-10-22 . USAF Sat Cat: 25373 . COSPAR: 1998-038A. Apogee: 316 km (196 mi). Perigee: 167 km (103 mi). Inclination: 67.10 deg. Period: 89.30 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission. Landed October 22, 1998..
1998 June 25 - .
14:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2359 - .
Mass: 6,620 kg (14,590 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Decay Date: 1999-07-12 . USAF Sat Cat: 25376 . COSPAR: 1998-039A. Apogee: 300 km (180 mi). Perigee: 239 km (148 mi). Inclination: 64.90 deg. Period: 89.90 min. Photo/digital surveillance. Entered an initial 170 x 290 km x 64.9 deg initial orbit. It manoeuvred to its operational orbit of 240 x 302 km x 64.9 deg on June 27..
1998 July 28 - .
09:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2360 - .
Payload: Tselina-2 no. 22. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Agency: MO.
Manufacturer: Yuzhnoye.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 25406 . COSPAR: 1998-045A. Apogee: 855 km (531 mi). Perigee: 847 km (526 mi). Inclination: 71.00 deg. Period: 102.00 min.
1998 August 12 - .
11:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 401A/Centaur.
FAILURE: Due to guidance system loss of heading after power interrupt, booster pitched over 40 seconds after launch, and was destroyed by range safety..
Failed Stage: G.
- Mercury ELINT - .
Payload: Mercury ELINT 3. Nation: USA.
Agency: NRO,
NSA.
Manufacturer: TRW.
Class: Surveillance.
Type: SIGINT. Spacecraft: Mercury ELINT.
Third launch of Mercury ELINT satellite..
1999 April 9 - .
17:01 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
LV Family:
Titan.
Launch Vehicle:
Titan 402B/IUS.
FAILURE: IUS first and second stages failed to separate..
Failed Stage: U.
- USA 142 - .
Payload: DSP-1 Block 18 F19. Mass: 2,380 kg (5,240 lb). Nation: USA.
Agency: USAF.
Manufacturer: TRW.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 25669 . COSPAR: 1999-017A. Apogee: 35,800 km (22,200 mi). Perigee: 720 km (440 mi). Inclination: 28.00 deg.
The Titan 4B placed the IUS upper stages and DSP-1 Block 14 ballistic missile launch detection satellite. payload into a 188 km x 718 km x 28.6 deg parking orbit. The first stage of the IUS burned at 18:14 GMT and put the second stage and payload into a geosynchronous transfer orbit. The IUS second stage fired at 23:34 GMT in order to place the spacecraft in geosynchronous orbit. However, at least one connector remained attached between the stages, and the second stage motor nozzle did not extend properly. When the stage fired, the vehicle tumbled wildly during the burn. Separation of the DSP was achieved. Although it could not perform its primary mission, it did provide a good test case in that the effects of radiation on its systems could be monitored as they underwent twice-daily passages of the Van Allen Radiation Belts. However after some weeks the hydrazine propellant aboard the satellite vented into space due to a broken fuel line. It was believed this had been induced by the wild ride aboard the IUS-2 stage.
1999 April 27 - .
18:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Athena.
Launch Vehicle:
Athena-2.
FAILURE: Payload shroud failed to separate four minutes after launch..
Failed Stage: S.
1999 May 22 - .
09:36 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 404B.
- USA 144 - .
Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Misty.
USAF Sat Cat: 25744 . COSPAR: 1999-028A. Apogee: 3,100 km (1,900 mi). Perigee: 2,700 km (1,600 mi). Inclination: 63.50 deg.
This classified National Reconnaissance Office satellite represented the first successful Titan launch in four attempts. The payload had been reported to be a Lacrosse radar imaging reconnaissance satellite. However the short 50 foot Titan fairing was used instead of the 66 foot fairing used by Lacrosse. This only seems to be used previously for an Improved Crystal photo-reconnaissance satellite in November 1992. The payload therefore could be related to the ocean surveillance triplets, or be an Improved CRYSTAL derivative. Veteran amateur satellite-watchers believed it was the second launch of 'Misty', a stealthy optical reconnaisance satellite (the first launch being USA 53 in February 1990).
1999 August 18 - .
18:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2365 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 119.00 days. Decay Date: 1999-12-15 . USAF Sat Cat: 25889 . COSPAR: 1999-044A. Apogee: 338 km (210 mi). Perigee: 184 km (114 mi). Inclination: 67.10 deg. Period: 89.73 min. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission. Landed in Russia on December 15, 1999..
1999 September 24 - .
18:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Athena.
Launch Vehicle:
Athena-2.
- Ikonos - .
Mass: 726 kg (1,600 lb). Nation: USA.
Agency: SpaceIm.
Manufacturer: Lockheed.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: LM-900.
Spacecraft: Ikonos.
USAF Sat Cat: 25919 . COSPAR: 1999-051A. Apogee: 679 km (421 mi). Perigee: 678 km (421 mi). Inclination: 98.10 deg. Period: 98.30 min. Commercial / civilian high resolution (1 metre resolution) photograhic satellite..
1999 December 3 - .
16:22 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA2.
LV Family:
Ariane.
Launch Vehicle:
Ariane 40.
- Helios 1B - .
Mass: 2,750 kg (6,060 lb). Nation: France.
Agency: DGA.
Manufacturer: Toulouse.
Program: Helios.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: SPOT-4.
Spacecraft: Helios 1A-1B.
USAF Sat Cat: 25977 . COSPAR: 1999-064A. Apogee: 682 km (423 mi). Perigee: 680 km (420 mi). Inclination: 98.20 deg. Period: 98.40 min.
French optical military reconnaisance satellite based on Spot 4. Taken out of service in mid-October 2004, when the orbit of the satellite was lowered to 637 x 640 km, taking it out of the path of Helios 1A and the Helios 2A that would be launched in December 2004.
- Clementine - .
Mass: 50 kg (110 lb). Nation: France.
Agency: CNES,
DGA.
Manufacturer: Surrey.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: SSTL-70.
USAF Sat Cat: 25978 . COSPAR: 1999-064B. Apogee: 616 km (382 mi). Perigee: 602 km (374 mi). Inclination: 98.10 deg. Period: 96.90 min. Customer: Alcatel Espace(France). French government military electronic intelligence research payload incorporated into an advance microsatellite platform. Based on CERISE with enhanced EMC subsystem. Still operational as of 2000..
1999 December 26 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
1999 December 27 - .
19:12 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
2000 February 3 - .
09:26 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2369 - .
Mass: 3,200 kg (7,000 lb). Nation: Russia.
Agency: MO.
Manufacturer: Yuzhnoye.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 26069 . COSPAR: 2000-006A. Apogee: 860 km (534 mi). Perigee: 849 km (528 mi). Inclination: 71.00 deg. Period: 101.95 min. ELINT satellite..
2000 March 12 - .
09:29 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576E.
LV Family:
Taurus.
Launch Vehicle:
Taurus 1110.
- MTI - .
Mass: 587 kg (1,294 lb). Nation: USA.
Agency: Los Alamos.
Manufacturer: Sandia.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: BCP-600.
Spacecraft: MTI.
USAF Sat Cat: 26102 . COSPAR: 2000-014A. Apogee: 609 km (378 mi). Perigee: 574 km (357 mi). Inclination: 97.40 deg. Period: 96.42 min. Military Technology. Sandia Multispectral Thermal Imager (MTI), aka USAF Space Test Program mission P97-3. The satellite was equipped with a hyperspectral imager for military target recognition / treaty monitoring applications..
2000 May 3 - .
13:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2370 - .
Payload: Neman. Mass: 6,700 kg (14,700 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4KS1.
Decay Date: 2001-05-03 . USAF Sat Cat: 26354 . COSPAR: 2000-023A. Apogee: 312 km (194 mi). Perigee: 244 km (152 mi). Inclination: 64.73 deg. Period: 90.00 min.
Military Observation. Advanced imaging reconnaissance satellite. Relays digital imagery to earth via geostationary comsats. The last such satellite, Cosmos 2359, reentered in July 1999 after one year in orbit. The Soyuz-U launcher placed it in a 183 x 277 km x 64.8 deg initial orbit; it raised altitude to 240 x 300 km about 24 hr after launch.
2000 May 8 - .
16:01 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan 402B/IUS.
2000 June 7 - .
13:19 GMT - .
Launch Site:
Point Arguello.
Launch Complex:
Point Arguello WADZ.
Launch Pad: Aircraft from Vandenberg..
Launch Platform: L-1011.
LV Family:
Pegasus.
Launch Vehicle:
Pegasus XL.
- TSX 5 - .
Payload: P95-2. Mass: 247 kg (544 lb). Nation: USA.
Agency: USAF STP.
Manufacturer: McLean.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: STEP.
USAF Sat Cat: 26374 . COSPAR: 2000-030A. Apogee: 1,695 km (1,053 mi). Perigee: 412 km (256 mi). Inclination: 68.94 deg. Period: 106.19 min.
Military Technology satellite. Launch delayed from May 20 and June 6. Fifth STEP (Space Test Experiments Program) satellite. The satellite's main section was the STRV-2 experiment module, sponsored by the Ballistic Missile Defense Organization and the UK Ministry of Defense. This was to take infrared images of UK military aircraft at perigee, and then downlink data via laser. STRV-2 also carried vibration isolation and debris impact sensors. A secondary payload was the S97-1 CEASE (Compact Environmental Anomaly Sensor). This was an AFRL prototype sensor package to provide warning of spacecraft charging and radiation events. Air dropped in Point Arguello WADZ.
2000 July 19 - .
20:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC8.
LV Family:
Minuteman.
Launch Vehicle:
Minotaur 1.
- Mightysat 2.1 - .
Payload: SA-200B. Mass: 120 kg (260 lb). Nation: USA.
Agency: USAF STP.
Manufacturer: Gilbert.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: SA-200.
Decay Date: 2002-11-12 . USAF Sat Cat: 26414 . COSPAR: 2000-042A. Apogee: 581 km (361 mi). Perigee: 547 km (340 mi). Inclination: 97.78 deg. Period: 95.86 min.
Mightysat 2.1, also known as Sindri, used a Spectrum Astro SA-200B satellite bus. The spacecraft carried a hyperspectral imager for earth imaging and spectroscopy, as well as satellite technology experiments such as advanced solar arrays. An Aerospace Corp./DARPA picosatellite experiment, consisting of two small boxes connected by a deployable tether, was deployed later. Similar picosats were deployed on the previous Minotaur launch in January 2000.
2000 August 17 - .
23:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 403B.
2000 September 1 - .
03:25 GMT - .
Launch Site:
Taiyuan.
Launch Complex:
Taiyuan LC1.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- ZY-2C - .
Payload: Zi Yuan 2. Mass: 2,600 kg (5,700 lb). Nation: China.
Agency: SISE.
Manufacturer: CAST.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-3.
Decay Date: 2016-03-11 . USAF Sat Cat: 26481 . COSPAR: 2000-050A. Apogee: 501 km (311 mi). Perigee: 489 km (303 mi). Inclination: 97.40 deg. Period: 94.43 min.
The ZY-2 (Ziyuan-2 ('Resource-2'), while disguised as a civilian earth monitoring system, was actually code-named Jianbing-3 and was China's first high-resolution military imaging satellite. The cover story of the official Xinhua news agency was that the civilian remote sensing system would be used primarily in territorial surveying, city planning, crop yield assessment, disaster monitoring and space science experimentation. However the satellite was placed at a much lower altitude than the ZY-1 satellite and US intelligence sources indicated that it was a photo-reconnaissance satellite for exclusively military purposes, such as targeting missiles at US and Taiwanese forces. The new satellite was believed to employ digital-imaging technology and to have a resolution of 2 m or less. The satellite was designed and built by the Chinese Academy of Space Technology and was developed indigenously. It was said to be more advanced than earlier sensing satellites and was expected to have an orbital life of two years. The camera provided more than three times the resolution of the ZY-1 earth resources satellite. The Zi Yuan 2 satellite may have used the CBERS Sino-Brazilian bus of the earlier ZY-1. However it was also said to be of new design and demonstrated the capability to maneuver in orbit, adjusting its orbit after launch. In October 2000 Chinese scientists denied that the ZY-2 satellite had a military mission. It was said to be a remote-sensing satellite equipped with CCD cameras and an infrared multispectral scanner that could only identify objects on the ground with a resolution of several dozen meters to 1 km.
2000 September 25 - .
10:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2372 - .
Mass: 12,000 kg (26,000 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-2.
Duration: 269.00 days. Decay Date: 2001-04-20 . USAF Sat Cat: 26538 . COSPAR: 2000-056A. Apogee: 343 km (213 mi). Perigee: 211 km (131 mi). Inclination: 64.78 deg. Period: 89.97 min. Reported code name Yenisey. It is speculated that this is an improved version of the Orlets satellite launched as Cosmos 2290 in 1994. Re-entered on Apr 20, 2001 after a 7 month mission..
2000 September 29 - .
09:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2373 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 46.56 days. Decay Date: 2000-11-14 . USAF Sat Cat: 26552 . COSPAR: 2000-058A. Apogee: 285 km (177 mi). Perigee: 211 km (131 mi). Inclination: 70.30 deg. Period: 89.46 min.
Twentieth Kometa cartographic satellite, using the Yantar service module with a Vostok-type reentry vehicle. It was announced as a dual civil-military geodetic mission. After a day it raised its orbit to 211 x 285 km x 70.4 deg. Landed near Orenburg, Russia on November 14. Deorbit burn was probably around 2230 GMT; the Vostok-style sphere landed at 2253 GMT.
2000 November 20 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Second stage failed to restart at apogee..
Failed Stage: 2.
- QuickBird 1 - .
Mass: 950 kg (2,090 lb). Nation: USA.
Agency: DigitalGlobe.
Manufacturer: Ball.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: BCP-2000.
Decay Date: 2000-11-21 . USAF Sat Cat: 26617 . COSPAR: 2000-074A. Apogee: 614 km (381 mi). Perigee: 80 km (49 mi). Inclination: 65.70 deg. Period: 91.49 min.
The Kosmos-3M second stage entered an 81 x 614 km x 65.8 deg orbit but failed to restart at apogee, and reentered at the next perigee over Uruguay. The loss of the QuickBird 1 satellite was a heavy blow to EarthWatch Inc. QuickBird1 was a 1-m resolution commerical imaging satellite using a Ball Aerospace BCP-2000 bus. Their earlier satellite, EarlyBird, failed after a few days in orbit in December 1997. EarthWatch's rival, SpaceImaging, lost one satellite as well but its second Ikonos was operating in orbit.
2000 December 5 - .
Launch Site:
Svobodniy.
Launch Complex:
Svobodniy LC5.
LV Family:
Topol'.
Launch Vehicle:
Start-1.
- EROS A1 - .
Mass: 240 kg (520 lb). Nation: Israel.
Agency: ImageSat.
Manufacturer: IAI.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Ofeq 3.
Decay Date: 2016-07-07 . USAF Sat Cat: 26631 . COSPAR: 2000-079A. Apogee: 542 km (336 mi). Perigee: 533 km (331 mi). Inclination: 97.60 deg. Period: 95.40 min.
Launch delayed from November 28. The Israeli commercial imaging satellite EROS A1 was owned by ImageSat (an Israeli-led company registered in the Netherlands Antilles) and built by IAI using the Ofeq-3 design. EROS A1 was placed in a sun-synchronous orbit together with the DS 5th stage. The 250 kg (dry mass) triaxially stabilized spacecraft carried a black and white high resolution (1.8 m) CCD camera, to obtain images (with terrain width of 12.6 km) of locations chosen by Israeli military or world-wide commercial clients, and downlink them at one of the 14 ground stations.
2001 May 29 - .
17:55 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2377 - .
Mass: 6,500 kg (14,300 lb). Nation: Russia.
Agency: MO.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 131.00 days. Decay Date: 2001-10-10 . USAF Sat Cat: 26775 . COSPAR: 2001-022A. Apogee: 261 km (162 mi). Perigee: 170 km (100 mi). Inclination: 67.10 deg. Period: 88.80 min. The Kobalt-class imaging satellite landed on October 10, 2001 after a four month mission..
2001 August 6 - .
07:28 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
Launch Pad: SLC40.
LV Family:
Titan.
Launch Vehicle:
Titan 402B/IUS.
- USA 159 - .
Payload: DSP-1 Block 18 F21. Mass: 2,380 kg (5,240 lb). Nation: USA.
Agency: USAF.
Manufacturer: TRW.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 26880 . COSPAR: 2001-033A. Apogee: 35,780 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 2.90 deg. Period: 1,435.76 min.
Launch postponed from February, then delayed from July 27. USA 159 was a US Air Force Defense Support Program infrared missile early warning satellite was placed by the Titan core into a 328 x 663 km x 28.7 deg parking orbit. The Boeing IUS-16 upper stage then fired its first solid motor to enter geostationary transfer orbit. The second IUS solid motor fired at around 14:00 GMT placing DSP Flight 21 in near-geosynchronous orbit. Still in service as of March 2007.
2001 August 24 - .
20:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/24.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
- Cosmos 2379 - .
Payload: SPRN No. 9. Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Prognoz SPRN.
USAF Sat Cat: 26892 . COSPAR: 2001-037A. Apogee: 35,810 km (22,250 mi). Perigee: 35,768 km (22,225 mi). Inclination: 1.60 deg. Period: 1,436.20 min.
Launch delayed from August 23. Early-warning geosynchronous satellite. The Proton upper stage entered a geostationary transfer orbit after its first burn at 2152 GMT. A second burn was at 0310 GMT put the payload into its operational orbit. It was to provide early warning of missiles launched from the United States with the help of a heat-sensing array of detectors. According to the Moscow Kommersant newspaper, these early warning geosynchronous satellites belong to the US-KMO group, also known as Prognoz fleet, while the highly elliptical complement belongs to the US-KS group, also known as Oko fleet, both supplemented by about eight ground-based radars. As of 6 September 2001 located at 80.17 deg E drifting at 0.031 deg E per day. As of 2007 Mar 10 located at 23.84W drifting at 0.002W degrees per day.
2001 September 8 - .
15:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas IIAS.
- USA 160 - .
Payload: Intruder 5 / MLV-10. Mass: 5,000 kg (11,000 lb). Nation: USA.
Agency: NRO.
Manufacturer: Martin.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 26905 . COSPAR: 2001-040A. Apogee: 1,200 km (700 mi). Perigee: 1,060 km (650 mi). Inclination: 63.40 deg. Period: 107.40 min.
Launch delayed from July 31. Move of launch of the Intruder naval electronic intelligence satellites for the National Reconnaissance Office (NRO) from the Titan to the Atlas launch vehicle. The Lockheed Martin Atlas IIAS AC-160 put the vehicle in a transfer orbit. The phrasing of the launch commentary implied that the second burn left the payload in 'transfer orbit', but several observers saw the bright Centaur in the typical final deployment orbit of the earlier NOSS satellites. Therefore it seemed the first burn was to a transfer orbit of around 180 x 1100 km x 63 deg. The second burn at 1629 GMT put the Centaur and payload into an 1100 x 1100 km x 63 deg orbit. The design was apparently different from earlier generation NOSS satellites since only one companion satellite was deployed rather than two, in line with the lower payload capability of the Atlas. Prime contractor for the new satellites was again believed to be Lockheed Martin Astronautics at Denver. The NRL probably continued to have a management and technical role in the program under overall NRO auspices.
- USA 160 companion - .
Payload: Intruder 5 / MLV-10. Mass: 5,000 kg (11,000 lb). Nation: USA.
Agency: NRO.
Manufacturer: Martin.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 26907 . COSPAR: 2001-040C. Apogee: 1,200 km (700 mi). Perigee: 1,060 km (650 mi). Inclination: 63.40 deg. Period: 107.40 min.
2001 September 21 - .
18:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576E.
LV Family:
Taurus.
Launch Vehicle:
Taurus 2110.
FAILURE: A problem a few seconds after first stage separation caused the rocket to go off course; it recovered and the remainder of the stages fired, but final cutoff velocity was too low to reach a sustainable orbit..
Failed Stage: G.
- Orbview-4 - .
Mass: 368 kg (811 lb). Nation: USA.
Agency: Orbimage.
Manufacturer: OSC.
Program: Orbview.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: LEOStar.
Spacecraft: Orbview.
COSPAR: F010921A.
Launch delayed from June 27, July 18/22, August 12/21 and September1. The Orbital Sciences Taurus 2110 failed to remain in orbit. A problem a few seconds after first stage separation caused the T6 rocket to go off course; the rocket recovered and the remainder of the stages fired, but final cutoff velocity was too low to reach a sustainable orbit. The Castor 120 zero stage was on course but the Orion 50S first stage motor went off course. The satellites separated from the final stage as planned but burned up in the earth's atmosphere northeast of Madagascar before completing the first orbit. The final orbit was about 75-80 km x 425-430 km x 97 deg. The primary payload was the OrbView-4 imaging satellite. OrbView-4, built by Orbital, was a 368 kg box-shaped spacecraft carrying a 1-m resolution panchromatic camera and an 8-m resolution 200-channel hyperspectral imager with a 0.45-meter aperture. It was to be used by the US Air Force.
2001 October 5 - .
21:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 404B.
- USA 161 - .
Payload: EIS-4. Mass: 16,650 kg (36,700 lb). Nation: USA.
Agency: NRO.
Manufacturer: Lockheed.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 26934 . COSPAR: 2001-044A. Apogee: 1,050 km (650 mi). Perigee: 150 km (90 mi). Inclination: 97.90 deg.
Launch delayed from September 25, October1. National Reconnaissance Office payload that was placed into a sun-synchronous orbit. It was speculated that the payload was an Improved Crystal imaging satellite. That would imply an operational orbit of 150 x 1050 km x 97.9 deg orbit. The satellite belonged to the National Reconnaissance Office's fleet of Earth Imaging System (EIS) satellites. A BBC website reported a resolution of 10 cm in the images. (A commonly used name for the EIS satellites was Advanced Keyhole.) The first member of the EIS fleet was USA 144 (1999-028A), launched in May 1999.
2001 October 18 - .
18:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10.
- QuickBird 2 - .
Mass: 980 kg (2,160 lb). Nation: USA.
Agency: DigitalGlobe.
Manufacturer: Ball.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: BCP-2000.
Decay Date: 2015-01-27 . USAF Sat Cat: 26953 . COSPAR: 2001-047A. Apogee: 471 km (292 mi). Perigee: 471 km (292 mi). Inclination: 97.20 deg. Period: 94.00 min.
The QuickBird commercial imaging satellite was owned by DigitalGlobe (formerly EarthWatch) and used a Ball BCP2000 bus with a launch mass of 1028 kg and a dry mass of about 995 kg. The Delta upper stage entered a 185 x 472 km x 98.1 deg orbit at 1902 GMT. At 1948 GMT it reached apogee and fired again to deploy QuickBird into a 461 x 465 km x 97.2 deg orbit. The Delta then made a series of unusual depletion burns, lowering its perigee to 167 km and changing inclination to 108.9 deg.
Quickbird 2 was to be operational after a few months of calibration and "ground-truth" checkouts to market high resolution images. The 1.0 tonne satellite was reported to be capable of images with a resolution as small as 0.6 meter, though the standard products were to be coarser. Unlike the comparable quality images from IKONOS images, some of which are currently marketed exclusively to the US military, all Quickbird 2 images may be available in the open market.
2001 October 22 - .
04:53 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
Launch Vehicle:
PSLV.
- TES - .
Mass: 1,108 kg (2,442 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: IRS.
Spacecraft: TES.
USAF Sat Cat: 26957 . COSPAR: 2001-049A. Apogee: 592 km (367 mi). Perigee: 533 km (331 mi). Inclination: 97.60 deg. Period: 95.90 min.
Launch delayed from July 20. The PS4 upper stage deployed the 1108 kg Indian TES (Technology Experiment Satellite) into a sun-synchronous orbit at 05:09:10 GMT. TES was an imaging satellite equipped with cameras and instruments to test military reconnaissance satellite technology. It was probably based on the IRS remote sensing satellite and carried a one-meter resolution panchromatic camera. India decided to develop an independent indigenous reconnaissance satellite capability after the 1999 incursion of Pakistani troops into disputed territory in Kashmir caught it by surprise. TES was developed by ISRO, the Indian Space Research Organization.
2001 December 10 - .
17:18 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Badr B - .
Mass: 70 kg (154 lb). Nation: Pakistan.
Agency: RAKA.
Manufacturer: SIL.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Badr.
USAF Sat Cat: 27003 . COSPAR: 2001-056C. Apogee: 1,014 km (630 mi). Perigee: 985 km (612 mi). Inclination: 99.20 deg. Period: 105.10 min. Badr B was Pakistan's second satellite. Built in collaboration with the English company SIL, it had a mass of 70 kg and carried an Earth imager..
2001 December 21 - .
04:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
2002 February 25 - .
17:26 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/3.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2387 - .
Mass: 6,700 kg (14,700 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 122.00 days. Decay Date: 2002-06-27 . USAF Sat Cat: 27382 . COSPAR: 2002-008A. Apogee: 297 km (184 mi). Perigee: 168 km (104 mi). Inclination: 67.10 deg. Period: 89.20 min. The optical reconnaissance satellite carried two small film capsules and a large reentry module. The main recoverable section of Cosmos 2387 landed at about 0230 UTC on June 27..
2002 April 1 - .
22:07 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
2002 May 28 - .
15:25 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-5 - .
Mass: 300 kg (660 lb). Nation: Israel.
Agency: Tsahal.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
USAF Sat Cat: 27434 . COSPAR: 2002-025A. Apogee: 757 km (470 mi). Perigee: 370 km (220 mi). Inclination: 143.50 deg. Period: 95.90 min.
Military Observation satellite. Return to flight of the Shavit booster following a lauanch failure. Launch delayed from third quarter 2001. The three-stage Shavit rocket took off from Palmachim Air Force Base on the Israeli coast and flew westward to put the satellite in a retrograde orbit. The AUS-51 third stage solid motor entered a 262 x 774 km x 143.5 deg orbit and separated from the Ofeq satellite. Both coasted up to apogee at around 1620 UTC when Ofeq made a burn to increase its velocity by 33 m/s, raising the orbit to 369 x 771 km x 143.5 deg.
2002 July 25 - .
15:13 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/24.
LV Family:
Proton.
Launch Vehicle:
Proton-K/17S40.
2002 October 27 - .
03:17 GMT - .
Launch Site:
Taiyuan.
Launch Complex:
Taiyuan LC1.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- ZY-2B - .
Payload: Zi Yuan 2-2. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: CAST.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-3.
Decay Date: 2015-01-22 . USAF Sat Cat: 27550 . COSPAR: 2002-049A. Apogee: 483 km (300 mi). Perigee: 470 km (290 mi). Inclination: 97.40 deg. Period: 94.10 min.
JB-3 2 was nominally a Chinese (PRC) remote sensing satellite, although US intelligence sources indicated it had primarily an intelligence imaging mission. JB-3 2 was the name adopted by the USSPACECOM. Most news reports from China and elsewhere use different names: ZY-2B (acronym for ZiYuan-2B, translated as Resource-2B), and Zhong Guo Zi Yuan Er Hao, translated as China Resource 2. No information was available on the instruments onboard the JB-3 2, but officially it was intended 'for territorial survey, environment monitoring and protection, urban planning, crop yield assessment, disaster monitoring, and space scientific experiments'. The initial orbital parameters of this sun-synchronous satellite were period 94.1 min, apogee 483 km, perigee 470 km, and inclination 97.4°.
2002 November 28 - .
06:07 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- ALSAT-1 - .
Mass: 80 kg (176 lb). Nation: Algeria.
Agency: NCST.
Manufacturer: Surrey.
Program: Alsat.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: MicroSat-100.
USAF Sat Cat: 27559 . COSPAR: 2002-054A. Apogee: 745 km (462 mi). Perigee: 681 km (423 mi). Inclination: 98.20 deg. Period: 99.00 min.
Delayed from September 12, October 29. ALSAT 1 was an Algerian imaging minisatellite. The 90-kg satellite was the first part of an international Disaster Monitoring System (DMS) for alerting natural/man-made disasters. ALSAT was built by Surrey Satellite for the CNTS (Centre National des Techniques Spatiales) in Algiers. It carriee a 32-m resolution 3-band imager,
a 100 mN resistojet thruster for small orbit corrections, and a GPS receiver. The SSTL Microsat-100 class satellite was a 0.60m cube with a 6m gravity gradient boom. As well as gravity gradient stabilization, it used a momentum wheel to improve stability for
imaging.
2002 December 24 - .
12:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2393 - .
Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2013-12-22 . USAF Sat Cat: 27613 . COSPAR: 2002-059A. Apogee: 39,722 km (24,682 mi). Perigee: 542 km (336 mi). Inclination: 62.90 deg. Period: 716.00 min. Launch delayed from September, then October 22..
2003 March 28 - .
01:27 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 2024.
- IGS-1b - .
Mass: 1,200 kg (2,600 lb). Nation: Japan.
Agency: NASDA.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: IGS.
Decay Date: 2012-07-26 . USAF Sat Cat: 27699 . COSPAR: 2003-009B. Apogee: 500 km (310 mi). Perigee: 489 km (303 mi). Inclination: 97.30 deg. Period: 94.20 min. Radar satellite..
2003 April 24 - .
04:23 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/24.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
- Cosmos 2397 - .
Payload: US-KMO (Prognoz 2). Mass: 2,155 kg (4,750 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Prognoz SPRN.
USAF Sat Cat: 27775 . COSPAR: 2003-015A. Apogee: 35,928 km (22,324 mi). Perigee: 35,886 km (22,298 mi). Inclination: 2.20 deg. Period: 1,442.30 min. As of 2007 Mar 9 located at 60.65W drifting at 0.723E degrees per day..
2003 August 12 - .
14:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2399 - .
Mass: 6,750 kg (14,880 lb). Nation: Russia.
Agency: VKS.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Decay Date: 2003-12-09 . USAF Sat Cat: 27856 . COSPAR: 2003-035A. Apogee: 289 km (179 mi). Perigee: 180 km (110 mi). Inclination: 64.90 deg. Period: 89.20 min.
Originally to have launched September 2002; June 2003. A Russian newspaper report (Kommersant, 13 August) stated that Cosmos 2399 was a Neman (Yantar-4KS1M) imaging satellite, which used data relay satellites to return CCD imagery rather than physically recovering film. However some Western observors, when Cosmos 2399 raised its perigee on August 14 to 205 km and lowered the apogee to 330 km, believed this was more like the standard operational orbit for an Orlets-1 Don 17F12 film-return capsule imaging satellite. This seemed confirmed when debris was tracked around the satellite later on, which was then said to be due to a failed film capsule recovery attempt. Destroyed in orbit on December 9 after completing its mission.
2003 September 9 - .
04:29 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
Launch Pad: SLC40.
LV Family:
Titan.
Launch Vehicle:
Titan 401B/Centaur.
- USA 171 - .
Payload: Orion 5. Mass: 5,200 kg (11,400 lb). Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Advanced Orion.
USAF Sat Cat: 27937 . COSPAR: 2003-041A. Apogee: 35,800 km (22,200 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,440.00 min.
American signals intelligence satellite placed into geostationary orbit. It was believed the payload was a successor to the USA-110 and USA-139 satellites launched in May 1995 and May 1998, referred
to as 'Advanced ORION' by those not in the know. They were thought to be successors to the RHYOLITE missions of the 1970s. The satellite was originally to have launched April 28, 2002. Launch delayed seven times.
2003 October 15 - .
01:00 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2F.
2003 November 2 - .
07:20 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- FSW-3 No. 1 - .
Payload: FSW-18, FSW-3.1, Jianbing 4. Mass: 3,000 kg (6,600 lb). Nation: China.
Agency: SAST.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Decay Date: 2003-12-18 . USAF Sat Cat: 28078 . COSPAR: 2003-051A. Apogee: 165 km (102 mi). Perigee: 141 km (87 mi). Inclination: 63.00 deg. Period: 87.50 min. Expected to have been long-awaited 'seeds in space' mission but official announcements spoke only of photography..
2003 November 29 - .
04:33 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 2024.
FAILURE: Destroyed by range safety after solid booster nozzle burn-through resulted in motor not separating from core..
Failed Stage: 0.
- IGS-2a - .
Mass: 850 kg (1,870 lb). Nation: Japan.
Agency: NASDA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IGS.
The launch failure meant that Japan's planned intelligence satellite constellation was crippled. The system was already in trouble due to the reported poor performance of the first two elements launched..
- IGS-2b - .
Mass: 1,200 kg (2,600 lb). Nation: Japan.
Agency: NASDA.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: IGS.
2003 December 2 - .
10:04 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas.
Launch Vehicle:
Atlas IIAS.
- USA 173 - .
Payload: Intruder 6 / NROL-18. Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 28095 . COSPAR: 2003-054A. Apogee: 1,210 km (750 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg. Period: 107.40 min. Second launch of new generation paired satellites used for tracking, characterisation, and intelligence on naval vessels and civilian shipping worldwide..
- USA 173 companion - .
Payload: Intruder 6 / NROL-18. Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 28097 . COSPAR: 2003-054C. Apogee: 1,210 km (750 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg. Period: 107.40 min.
2004 February 14 - .
18:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
Launch Pad: SLC40.
LV Family:
Titan.
Launch Vehicle:
Titan 402B/IUS.
- USA 176 - .
Payload: DSP-1 Block 18 F22. Mass: 2,380 kg (5,240 lb). Nation: USA.
Agency: NSA.
Manufacturer: TRW.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 28158 . COSPAR: 2004-004A. Apogee: 36,105 km (22,434 mi). Perigee: 35,852 km (22,277 mi). Inclination: 0.68 deg. Period: 1,445.94 min.
DSP-1 Block 14 ballistic missile launch detection satellite. Last flight of the IUS upper stage. Launch delayed from November 4, 2003, and January 17, 2003. Planned IMEX piggyback payload cancelled. Still in service as of March 2007, expected to remain operational until 2017-2022. As of 2004 Feb 15 located at 96.66W drifting at 2.464W degrees per day.
2004 April 18 - .
15:59 GMT - .
Launch Site:
Xichang.
Launch Complex:
Xichang LC1.
Launch Pad: LC1?.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- Naxing 1 - .
Payload: CAST1000A, OlympivSat. Mass: 25 kg (55 lb). Nation: China.
Agency: Tsinghua.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: CAST1000.
USAF Sat Cat: 28221 . COSPAR: 2004-012B. Apogee: 616 km (382 mi). Perigee: 599 km (372 mi). Inclination: 97.70 deg. Period: 96.80 min. Naxing 1 (a contraction of Nami Weixing 'Nanosatellite') was designed for high-tech experiments. The satellite was developed and will be used by the elite Qinghua University and the Aerospace Qinghua Satellite Technologies Co. Ltd..
2004 May 20 - .
17:47 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576E.
LV Family:
Taurus.
Launch Vehicle:
Taurus 3210.
- ROCSAT 2 - .
Payload: LeoStar 500XO. Mass: 760 kg (1,670 lb). Nation: Taiwan.
Agency: NSPO.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: T200.
Spacecraft: ROCSAT.
USAF Sat Cat: 28254 . COSPAR: 2004-018A. Apogee: 891 km (553 mi). Perigee: 887 km (551 mi). Inclination: 99.10 deg. Period: 102.80 min. Delayed from October, November 25, 2003; January 17, February 26, April 9 and 22, May 17, 2004..
2004 May 28 - .
06:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2405 - .
Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: VMF.
Manufacturer: Arsenal.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Decay Date: 2006-06-16 . USAF Sat Cat: 28350 . COSPAR: 2004-020A. Apogee: 417 km (259 mi). Perigee: 405 km (251 mi). Inclination: 65.00 deg. Period: 92.80 min. Original reported name Cosmos 2407..
2004 June 10 - .
01:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Cosmos 2406 - .
Mass: 3,200 kg (7,000 lb). Nation: Russia.
Agency: VKA.
Manufacturer: Yuzhnoye.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 28352 . COSPAR: 2004-021A. Apogee: 866 km (538 mi). Perigee: 846 km (525 mi). Inclination: 71.00 deg. Period: 102.10 min. Delayed from February 17 and 18; March 17 and 31; April 6, 25 and 26..
2004 August 29 - .
07:50 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-3 No. 2 - .
Payload: FSW-19. Mass: 3,100 kg (6,800 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 26.67 days. Decay Date: 2004-11-07 . USAF Sat Cat: 28402 . COSPAR: 2004-033A. Apogee: 547 km (339 mi). Perigee: 168 km (104 mi). Inclination: 63.00 deg. Period: 91.70 min.
Recoverable satellite officially stated to be conducting space scientific research, land surveying, mapping and other scientific experiments. Said to have improved experimental technology, with higher orientation precision and more complex on-board computers and software. Controlled from the Xian Satellite Monitoring and Control Centre. Successfully re-entered and recovered after 27 days in space at 23:55 GMT on 24 September.
2004 September 6 - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
FAILURE: Third stage orientation failure at 270 seconds into the flight.
Failed Stage: 3.
- Ofeq-6 - .
Mass: 300 kg (660 lb). Nation: Israel.
Agency: Tsahal.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
Military observation satellite failed to reach orbit. Finanical loss estimated by Israeli press as $ 100 million..
2004 September 24 - .
16:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2410 - .
Mass: 6,700 kg (14,700 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 107.00 days. Decay Date: 2005-01-09 . USAF Sat Cat: 28396 . COSPAR: 2004-038A. Apogee: 348 km (216 mi). Perigee: 208 km (129 mi). Inclination: 67.10 deg. Period: 90.10 min.
Film-return reconnaisance satellite. Maneuvered on October 1 to a 213 x 330 km orbit. Believed to be an improved Yantar-4K1 with a longer lifetime - and given the code name 'Kobalt' previously applied to the defunct Yantar-4K2 system. When re-entry was commanded after only 107 days in orbit, there was speculation that problems had arisen with the satellite. Sources claimed the satellite had some kind of control problem, which was brought under control, and the two smaller film return capsules were successfully returned. But when the control problem reoccurred, it was decided to bring the main re-entry capsule down early. At retrofire, two objects were tracked as having separated from the spacecraft. Russian search teams were unable to locate the capsule after re-entry. Further launches of the satellite were put on hold until a State Commission could determine the causes of the failure.
2004 September 27 - .
08:00 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- FSW-3 No. 3 - .
Payload: FSW 20. Mass: 3,100 kg (6,800 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 17.78 days. Decay Date: 2004-11-09 . USAF Sat Cat: 28424 . COSPAR: 2004-039A. Apogee: 297 km (184 mi). Perigee: 205 km (127 mi). Inclination: 63.00 deg. Recoverable military satellite. Returned to Earth at 02:48 GMT on October 15, falling through the roof of a house in the village of Penglai, Sichuan province..
2004 December 18 - .
16:26 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5Gp.
- Helios 2A - .
Mass: 4,200 kg (9,200 lb). Nation: France.
Agency: DGA.
Manufacturer: EADS Astrium.
Program: Helios.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: SPOT-5A-5B.
Spacecraft: Helios 2.
USAF Sat Cat: 28492 . COSPAR: 2004-049A. Apogee: 690 km (420 mi). Perigee: 688 km (427 mi). Inclination: 98.08 deg. Period: 98.39 min. First of two new-generation French military surveillance satellites. Last flight of Ariane 5G model. Launch delayed from December 10..
- Parasol - .
Mass: 125 kg (275 lb). Nation: France.
Agency: CNES.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 28498 . COSPAR: 2004-049G. Apogee: 673 km (418 mi). Perigee: 659 km (409 mi). Inclination: 98.08 deg. Period: 97.91 min.
Parasol carried a wide-field imaging radiometer/polarimeter called POLDER (Polarization and Directionality of the Earth's Reflectances), designed in partnership with the LOA atmospheric optics laboratory in Lille (CNRS-USTL). POLDER was designed to improve the knowledge of the radiative and microphysical properties of clouds and aerosols by measuring the directionality and polarization of light reflected by the Earth-atmosphere system.
- Essaim 1 - .
Mass: 120 kg (260 lb). Nation: France.
Agency: DGA.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 28494 . COSPAR: 2004-049C. Apogee: 673 km (418 mi). Perigee: 663 km (411 mi). Inclination: 98.08 deg. Period: 97.96 min.
The Essaim demonstrator was a system of several micro-satellites (Essaim means 'swarm' in French) for 'analysis of the electro-magnetic environment of the Earth's surface' (electronic intelligence). DGA, the French Ministry of Defence's procurement agency, developed the project. The system also comprised a ground control segment and a ground station for data processing. It was called a 'demonstrator' since the mission's objective was to assess the operational capability of such a system, paving the way for the next generation. The Essaim satellites were based on EADS Astrium's Myriade multipurpose micro-satellite. In early 2000, the DGA awarded the contract for the development, manufacturing of this turnkey system of micro-satellites and associated ground segment. Under the contract, EADS Astrium was also responsible for personnel training and system operations during the three-year life duration of the programme.
- Essaim 2 - .
Mass: 120 kg (260 lb). Nation: France.
Agency: DGA.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 28495 . COSPAR: 2004-049D. Apogee: 664 km (412 mi). Perigee: 657 km (408 mi). Inclination: 98.10 deg. Period: 98.00 min.
- Essaim 3 - .
Mass: 120 kg (260 lb). Nation: France.
Agency: DGA.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 28496 . COSPAR: 2004-049E. Apogee: 667 km (414 mi). Perigee: 654 km (406 mi). Inclination: 98.10 deg. Period: 98.00 min.
- Essaim 4 - .
Mass: 120 kg (260 lb). Nation: France.
Agency: DGA.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 28497 . COSPAR: 2004-049F. Apogee: 670 km (410 mi). Perigee: 651 km (404 mi). Inclination: 98.10 deg. Period: 98.00 min.
2005 February 3 - .
07:41 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC36B.
Launch Pad: SLC36B.
LV Family:
Atlas.
Launch Vehicle:
Atlas 3B.
- USA 181 - .
Payload: Intruder 7. Nation: USA.
Agency: ILS.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 28537 . COSPAR: 2005-004A. Apogee: 1,209 km (751 mi). Perigee: 1,011 km (628 mi). Inclination: 63.40 deg. Period: 107.40 min.
Last launch of an Atlas model using the original, innovative, balloon propellant tanks conceived in 1947. Third launch of new generation paired satellites used for tracking, characterisation, and intelligence on naval vessels and civilian shipping worldwide.
- USA 181 companion - .
Payload: Intruder 7. Nation: USA.
Agency: ILS.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 28541 . COSPAR: 2005-004C. Apogee: 1,209 km (751 mi). Perigee: 1,011 km (628 mi). Inclination: 63.40 deg. Period: 107.40 min.
2005 April 30 - .
00:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
Launch Pad: SLC40.
LV Family:
Titan.
Launch Vehicle:
Titan 405B.
- USA 182 - .
Mass: 14,500 kg (31,900 lb). Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Lacrosse satellite.
USAF Sat Cat: 28646 . COSPAR: 2005-016A. Apogee: 705 km (438 mi). Perigee: 481 km (298 mi). Inclination: 57.00 deg. Last East Coast Titan launch. Delayed from December 18, 2001; July 3, 2002; October 2004; February 20, April 6, 10 and 11, 2005. Amateur observors believed this to be the fifth in the Lacrosse/Onyx radar spy satellite series built by Lockheed Martin..
2005 August 2 - .
07:30 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- FSW-3 No. 4 - .
Payload: FSW-21. Mass: 3,100 kg (6,800 lb). Nation: China.
Agency: CAST.
Manufacturer: SAST.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 27.00 days. Decay Date: 2005-08-29 . USAF Sat Cat: 28776 . COSPAR: 2005-027A. Apogee: 259 km (160 mi). Perigee: 153 km (95 mi). Inclination: 63.00 deg. Period: 88.60 min. Military reconnaisance satellite, which maneuvered to raise its apogee on Aug 5 and 7 to a 166 x 552 km x 63.0 orbit; and again to the same altitude on Aug 19 after the apogee decayed to 535 km. Return capsule with film aboard recovered on 29 August..
2005 August 29 - .
08:45 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- FSW-3 No. 5 - .
Payload: FSW-22. Mass: 3,100 kg (6,800 lb). Nation: China.
Agency: CAST.
Manufacturer: SAST.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: FSW.
Duration: 49.00 days. Decay Date: 2005-10-17 . USAF Sat Cat: 28824 . COSPAR: 2005-033A. Apogee: 224 km (139 mi). Perigee: 178 km (110 mi). Inclination: 63.00 deg. Period: 88.50 min. Decayed 17 October 2005..
2005 September 2 - .
09:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2415 - .
Payload: Kometa s/n 21. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-1KFT.
Duration: 44.00 days. Decay Date: 2005-10-16 . USAF Sat Cat: 28841 . COSPAR: 2005-034A. Apogee: 272 km (169 mi). Perigee: 205 km (127 mi). Inclination: 64.90 deg. Period: 89.30 min. 1,700th launch of a vehicle derived from the R-7 ICBM put a Kometa-type cartographic satellite into orbit. The surveillance satellite's primary camera and film payload was recovered at 21:44 on 15 or 16 October..
2005 October 19 - .
18:05 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 404B.
- USA 186 - .
Payload: EIS-5 / NROL-20. Mass: 20,000 kg (44,000 lb). Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 28888 . COSPAR: 2005-042A. Apogee: 1,050 km (650 mi). Perigee: 264 km (164 mi). Inclination: 97.90 deg.
Delayed from 2003; February 2004; and June 30, July 10, September 9, 2005. Last launch of the Titan series put a classified National Reconnaisance Office satellite into polar orbit. Its orbital parameters, as determined by amateur observors, suggested it was an Improved Crystal electronic imaging reconnaissace satellite, replacing USA 129, which was launched in 1996.
2005 October 27 - .
06:52 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Topsat - .
Payload: Heavily modified Surrey MicroSat-100. Mass: 108 kg (238 lb). Nation: UK.
Agency: Qinetiq.
Manufacturer: Surrey.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SSTL-150.
USAF Sat Cat: 28891 . COSPAR: 2005-043B. Apogee: 707 km (439 mi). Perigee: 682 km (423 mi). Inclination: 98.20 deg. Period: 98.70 min. Delayed from May 18, mid-July, August 25, September 27 and 30, 2005. UK military surveillance research satellite..
- Sinah-1 - .
Mass: 160 kg (350 lb). Nation: Iran.
Agency: AKO Polyot.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Sterkh.
USAF Sat Cat: 28893 . COSPAR: 2005-043D. Apogee: 705 km (438 mi). Perigee: 682 km (423 mi). Inclination: 98.20 deg. Period: 98.60 min.
First Iranian satellite, with an experimental surveillance camera payload. It may have used the Russian Polyot enterprise's Sterkh satellite bus. The same bus was to be used in future Nadezhda satellites. The Strekh bus was said to accomodate 80-100 kg satellites, and be 1.0 m high and 0.4 m in diameter, with a design life of 5 years. Sinah was 160 kg, and 0.8 x 1.3 x 1.6 m in dimensions. Or it may have been a version of the previously-announced satellite dubbed Mesbah-2.
- SSETI Express - .
Mass: 80 kg (176 lb). Nation: Europe.
Agency: SSETI.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SSETI Express.
USAF Sat Cat: 28894 . COSPAR: 2005-043E. Apogee: 708 km (439 mi). Perigee: 682 km (423 mi). Inclination: 98.20 deg. Period: 98.70 min. Student-built technology satellite sponsored by the European Space Agency. It ejected three 1-kg Cubesats after separating from the booster, but then itself lost power less than 14 hours later..
2006 January 24 - .
01:33 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 2022.
- Daichi - .
Payload: ALOS-1. Mass: 3,850 kg (8,480 lb). Nation: Japan.
Agency: JAXA.
Manufacturer: Toshiba.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Daichi.
USAF Sat Cat: 28931 . COSPAR: 2006-002A. Apogee: 697 km (433 mi). Perigee: 693 km (430 mi). Inclination: 98.20 deg. Period: 98.70 min. Advanced Land Observing Satellite, which carried an L-band synthetic aperture radar, an optical 2.5-meter resolution mapping camera, and a 10-meter resolution visible/near-infrared radiometer..
2006 April 25 - .
16:47 GMT - .
Launch Site:
Svobodniy.
Launch Complex:
Svobodniy LC5.
LV Family:
Topol'.
Launch Vehicle:
Start-1.
- EROS-B - .
Mass: 350 kg (770 lb). Nation: Israel.
Agency: ImageSat.
Manufacturer: IAI.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Ofeq 3.
USAF Sat Cat: 29079 . COSPAR: 2006-014A. Apogee: 514 km (319 mi). Perigee: 505 km (313 mi). Inclination: 97.30 deg. Period: 94.80 min. Combined civilian/military imaging satellite operated by an Israeli company incorporated in the Cayman Islands. Its capability was demonstrated when, within days of launch, sharp photographs of people and motor vehicles on a Syrian dam were released..
2006 April 26 - .
22:48 GMT - .
Launch Site:
Taiyuan.
Launch Complex:
Taiyuan LC1.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 1 - .
Payload: Jianbing 5. Mass: 2,700 kg (5,900 lb). Nation: China.
Agency: CNSA.
Manufacturer: CASC.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-5.
USAF Sat Cat: 29092 . COSPAR: 2006-015A. Apogee: 630 km (390 mi). Perigee: 627 km (389 mi). Inclination: 97.80 deg. Period: 97.30 min. Remote sensing satellite built by the Shanghai SAST Group. In reality it was the first Chinese synthetic aperture radar military surveillance satellite..
2006 May 3 - .
17:38 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2420 - .
Payload: Yantar 4K-2M. Mass: 6,700 kg (14,700 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Decay Date: 2006-07-19 . USAF Sat Cat: 29111 . COSPAR: 2006-017A. Apogee: 349 km (216 mi). Perigee: 178 km (110 mi). Inclination: 67.10 deg. Period: 89.80 min. Imaging reconnaissance satellite, probably the second Kobalt-M satellite, built by the Arsenal factory. The satellite carried small film recovery capsules and one large reentry vehicle, recovered at the end of the mission with the camera and more film..
2006 June 24 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC90/20.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-2.
- Cosmos 2421 - .
Mass: 3,150 kg (6,940 lb). Nation: Russia.
Agency: VMF.
Manufacturer: Arsenal.
Program: EORSAT.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Kosmoplan.
Spacecraft: US-PU.
Decay Date: 2006-06-24 . USAF Sat Cat: 29246 . COSPAR: 2006-026A. Apogee: 414 km (257 mi). Perigee: 384 km (238 mi). Inclination: 65.00 deg. Period: 92.50 min.
2006 June 25 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(4,2).
- USA 184 - .
Payload: Raven 4 / NROL-22. Mass: 4,500 kg (9,900 lb). Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: ELINT. Spacecraft: Raven satellite.
USAF Sat Cat: 29249 . COSPAR: 2006-027A. Apogee: 39,000 km (24,000 mi). Perigee: 1,100 km (600 mi). Inclination: 63.60 deg. Period: 720.00 min.
Secret payload for the National Reconnaissance Office. The intended orbit was thought to be a "Molniya" elliptical 12-hour orbit with an inclination of 63 degrees. American data relay and signals intelligence satellites have used this orbit in the past, notably the Jumpseat series of 1971-1983. A secondary payload was later confirmed to be the first SBIRS-HEO (Space-based Infrared System) sensor. SBIRS was the successor to the DSP (Defence Support Program), which provided early warning of missile launches. Also carried the NASA/Los Alamos TWINS-A magnetospheric research payload
2006 July 21 - .
04:20 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2422 - .
Mass: 1,750 kg (3,850 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 29260 . COSPAR: 2006-030A. Apogee: 39,741 km (24,693 mi). Perigee: 616 km (382 mi). Inclination: 62.90 deg. Period: 717.80 min. Missile early warning satellite.
2006 September 11 - .
04:35 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS-3A - .
Mass: 850 kg (1,870 lb). Nation: Japan.
Agency: JIDF.
Manufacturer: Melco.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IGS.
Decay Date: 2016-10-29 . USAF Sat Cat: 29393 . COSPAR: 2006-037A. Apogee: 491 km (305 mi). Perigee: 484 km (300 mi). Inclination: 97.30 deg. Information Gathering Satellite / Optical-2 military surveillance satellite, launched to replace IGS O-1 launched in 2003, which demonstrated technical problems. The first replacement, IGS-O-2, was lost in a launch failure in 2003..
2006 September 14 - .
13:41 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2423 - .
Mass: 6,750 kg (14,880 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Orlets-1.
Duration: 64.00 days. Decay Date: 2006-11-17 . USAF Sat Cat: 29402 . COSPAR: 2006-039A. Apogee: 306 km (190 mi). Perigee: 208 km (129 mi). Inclination: 64.90 deg. Period: 89.70 min. Military surveillance; believed to be a derivative of the Orlets-1 multiple-capsule-return reconnaisance sattelite. Destroyed in orbit on November 17 at the end of its mission..
2006 October 23 - .
23:34 GMT - .
Launch Site:
Taiyuan.
Launch Complex:
Taiyuan LC1.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- SJ-6-02A SJ-6C - .
Mass: 2,700 kg (5,900 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: SJ-6.
USAF Sat Cat: 29505 . COSPAR: 2006-046A. Apogee: 598 km (371 mi). Perigee: 594 km (369 mi). Inclination: 97.70 deg. Period: 96.60 min. Replaced the SJ-6 Group 1 satellites A and B. Official purpose was to measure the space environment, but foreign analysts suspected a SIGINT role..
- SJ-6-02B SJ-6D - .
Mass: 2,700 kg (5,900 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Naval signals intelligence satellite. Spacecraft: CAST2000.
USAF Sat Cat: 29506 . COSPAR: 2006-046B. Apogee: 599 km (372 mi). Perigee: 598 km (371 mi). Inclination: 97.70 deg. Period: 96.70 min.
2006 December 16 - .
12:00 GMT - .
Launch Site:
Wallops Island.
Launch Complex:
Wallops Island LA0B.
LV Family:
Minuteman.
Launch Vehicle:
Minotaur 1.
- Tacsat-2 - .
Mass: 370 kg (810 lb). Nation: USA.
Agency: USAF RL.
Manufacturer: MicroSats.
Program: Tacsat.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Road Runner.
Spacecraft: Tacsat ORS.
Decay Date: 2011-02-05 . USAF Sat Cat: 29653 . COSPAR: 2006-058A. Apogee: 426 km (264 mi). Perigee: 410 km (250 mi). Inclination: 40.01 deg. Period: 92.93 min.
Tacsat-2 was a prototype rapid development/rapid deployment tactical military satellite that provided American Joint Task Force commanders direct control of a satellite providing both SIGINT and imagery with a resolution of better than 1-m. The known communications payload used an 8 GHz (X-band) downlink. This was the first orbital launch from Wallops Island since 1985. TacSat-2 was to have been launched by a Falcon-1 from Vandenberg into a sun-synchronous orbit. However, the failure of Falcon-1 on its long-delayed maiden in March 2006 caused AFRL to award a new launch contract for TacSat-2 and TacSat-3 to OSC in May 2006. The launch was achieved using OSC's Minotaur launch vehicle only seven months after contract award.
2006 December 19 - .
14:03 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- SAR-Lupe 1 - .
Mass: 770 kg (1,690 lb). Nation: Germany.
Agency: BWB.
Manufacturer: Bremen.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: SAR-Lupe.
USAF Sat Cat: 29658 . COSPAR: 2006-060A. Apogee: 506 km (314 mi). Perigee: 467 km (290 mi). Inclination: 98.20 deg. Period: 94.30 min. First of five planned German military surveillance satellites using synthetic aperture radar for target coverage at night and in all weathers. Orbital plane ascending node 143 deg..
2007 January 10 - .
04:16 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
Launch Vehicle:
PSLV.
2007 February 24 - .
04:41 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 2024.
- IGS 2 - .
Payload: IGS 4A. Mass: 1,200 kg (2,600 lb). Nation: Japan.
Agency: CSICE,
JAXA.
Manufacturer: Melco.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: IGS.
Decay Date: 2014-04-13 . USAF Sat Cat: 30586 . COSPAR: 2007-005A. Information Gathering Satellite Radar-2. Japanese military satellite using a synthetic aperture radar for all-weather, 24-hour, high-resolution surveillance of the earth..
2007 April 17 - .
06:46 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
Launch Pad: LC109/95.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- MisrSat 1 - .
Payload: Egyptsat 1 / MS-1TK. Mass: 100 kg (220 lb). Nation: Egypt.
Agency: NARSSS.
Manufacturer: Yuzhnoye.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: MS-1.
USAF Sat Cat: 31117 . COSPAR: 2007-012A. Apogee: 667 km (414 mi). Perigee: 657 km (408 mi). Inclination: 98.10 deg. Period: 98.00 min. MisrSat/Egyptsat carried an imaging payload for Egypt's National Authority for Remote Sensing and Space Sciences..
- Saudisat 3 - .
Mass: 35 kg (77 lb). Nation: Saudi Arabia.
Agency: RSRI.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Saudisat.
USAF Sat Cat: 31118 . COSPAR: 2007-012B. Apogee: 679 km (421 mi). Perigee: 656 km (407 mi). Inclination: 98.10 deg. Period: 98.10 min. Saudisat 3 carried a suveillance instrument, backed by data collection and relay avionics, to work in concert with the five smaller SaudiComSats launched at the same time..
2007 May 25 - .
07:12 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Yaogan 2 - .
Payload: Jianbing 6. Mass: 1,300 kg (2,800 lb). Nation: China.
Agency: CNSA.
Manufacturer: CAST.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-6.
USAF Sat Cat: 31490 . COSPAR: 2007-019A. Apogee: 655 km (406 mi). Perigee: 631 km (392 mi). Inclination: 97.80 deg. Period: 97.60 min. Second Chinese synthetic aperture radar military surveillance satellite..
2007 June 7 - .
18:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2427 - .
Mass: 6,700 kg (14,700 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Kozlov bureau.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 76.13 days. Decay Date: 2007-08-22 . USAF Sat Cat: 31595 . COSPAR: 2007-022A. Apogee: 339 km (210 mi). Perigee: 167 km (103 mi). Inclination: 67.10 deg. Period: 89.80 min.
Recoverable capsule military optical reconnaisance satellite. Orbit was raised on 11 June to 182 km x 354 km; decayed until 19 June, when it was lowered to 175 km x 325 km. On 28 June the orbit was raised to 183 km x 348 km; on 5 July to 169 km x 375 km. Landed at 21:00 GMT on 22 August after a 76-day mission.
2007 June 8 - .
02:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7420-10C.
- Cosmo-SkyMed 1 - .
Mass: 1,700 kg (3,700 lb). Nation: Italy.
Agency: ASI.
Manufacturer: Alenia.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Prima.
Spacecraft: Cosmo-SkyMed.
USAF Sat Cat: 31598 . COSPAR: 2007-023A. Apogee: 626 km (388 mi). Perigee: 622 km (386 mi). Inclination: 97.90 deg. Period: 97.20 min. The first of four Constellation of Small Satellites for Mediterranean basin Observation, Synthetic Aperture Radar satellites for primarily Italian military surveillance, but with products made available to civilian users as well..
2007 June 10 - .
23:40 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-7 - .
Mass: 300 kg (660 lb). Nation: Israel.
Agency: Tsahal.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
USAF Sat Cat: 31601 . COSPAR: 2007-025A. Apogee: 576 km (357 mi). Perigee: 340 km (210 mi). Inclination: 141.80 deg. Period: 93.80 min. Israeli optical reconnaisance satellite, evidently using an improved version of the Shavit booster and probably heavier and more capable than its predecessors..
2007 June 15 - .
02:14 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
Launch Pad: LC109/95.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- TerraSAR-X - .
Mass: 1,346 kg (2,967 lb). Nation: Germany.
Agency: DLR.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Astrobus.
Spacecraft: TerraSAR-X.
USAF Sat Cat: 31698 . COSPAR: 2007-026A. Apogee: 510 km (310 mi). Perigee: 507 km (315 mi). Inclination: 97.45 deg. Period: 94.79 min. Scientific/commercial surveillance satellite. equipped with an X-band synthetic aperture radar with 1 meter resolution.
2007 June 15 - .
15:11 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
Launch Pad: SLC41.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 194 - .
Payload: Intruder 8. Nation: USA.
Agency: NRO.
Manufacturer: Lockheed.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 31701 . COSPAR: 2007-027A. Apogee: 1,246 km (774 mi). Perigee: 776 km (482 mi). Inclination: 63.40 deg.
Classified National Reconnaissance Office mission. There appeared to be problem in the second burn of the Centaur upper stage. Amateur observors believed that two satellites were to be have been deployed in 1150 km altitude, 63 deg inclination, but that only a 776 km x 1246 km was achieved. However it was believed that the payloads could reach the final intended orbits using on-board propulsion
2007 June 29 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2M.
- Cosmos 2428 - .
Mass: 3,200 kg (7,000 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Yuzhnoye.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-2.
USAF Sat Cat: 31792 . COSPAR: 2007-029A. Apogee: 857 km (532 mi). Perigee: 846 km (525 mi). Inclination: 71.00 deg. Period: 102.00 min. Signals intelligence satellite. First launch in three years, and first with the improved version of the Zenit-2 launch vehicle using components developed for the Zenit-3SL..
2007 July 2 - .
19:38 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- SAR-Lupe 2 - .
Mass: 770 kg (1,690 lb). Nation: Germany.
Agency: BWB.
Manufacturer: Bremen.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: SAR-Lupe.
USAF Sat Cat: 31797 . COSPAR: 2007-030A. Apogee: 508 km (315 mi). Perigee: 470 km (290 mi). Inclination: 98.20 deg. Period: 94.40 min. Second of five planned German military surveillance satellites using synthetic aperture radar for target coverage at night and in all weathers. Orbital plane ascending node 208 deg..
2007 September 18 - .
18:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7920-10C.
- WorldView 1 - .
Mass: 2,500 kg (5,500 lb). Nation: USA.
Agency: Martin.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: BCP-5000.
Spacecraft: WorldView.
USAF Sat Cat: 32060 . COSPAR: 2007-041A. Apogee: 496 km (308 mi). Perigee: 492 km (305 mi). Inclination: 97.50 deg. Period: 94.50 min. Spacecraft was equipped with a 0.6-m aperture telescope for high resolution surveillance. Civilian, but primary customer was to be the US National Geospatial Intelligence Agency..
2007 September 19 - .
03:26 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
2007 September 27 - .
11:34 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
Launch Pad: SLC17B.
LV Family:
Thor.
Launch Vehicle:
Delta 7925H.
- Dawn - .
Mass: 1,218 kg (2,685 lb). Nation: USA.
Agency: Martin.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Dawn.
USAF Sat Cat: 32249 . COSPAR: 2007-043A.
Asteroid belt unmanned probe designed to first orbit and survey the asteroid Vesta, and then fly on to the largest asteroid, Ceres. The Delta upper stage boosted the spacecraft and PAM-D solid third stage to 9.01 km/sec and a 185 km x 6835 km orbit. The PAM-D fired at 12:29 GMT and released Dawn after accelerating it to 11.50 km/sec and sending it into a 1.00 AU x 1.62 AU x 0.5 deg solar orbit. The ion engines were ignited on 6 October. Using its ion engines and a Mars flyby in February 2009, Dawn was scheduled to reach Vesta in 2011 and Ceres in 2015.
2007 October 23 - .
04:39 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2430 - .
Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Lavochkin bureau.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2019-01-05 . USAF Sat Cat: 32268 . COSPAR: 2007-049A. Apogee: 39,175 km (24,342 mi). Perigee: 520 km (320 mi). Inclination: 62.90 deg. Period: 704.50 min. Missile early warning satellite.
2007 November 1 - .
00:51 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- SAR-Lupe 3 - .
Mass: 770 kg (1,690 lb). Nation: Germany.
Agency: KVR.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: SAR-Lupe.
USAF Sat Cat: 32283 . COSPAR: 2007-053A. Apogee: 496 km (308 mi). Perigee: 474 km (294 mi). Inclination: 98.20 deg. Period: 94.30 min. Third SAR-Lupe radar satellite. The final stage also carried a small Automatic Identification System package by OHB/Bremen, designed to test a system for monitoring shipping traffic. Orbital plane ascending node 272 deg..
2007 November 11 - .
01:50 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC37B.
Launch Pad: SLC37B.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 197 - .
Payload: DSP-1 Block 18 F23. Mass: 2,270 kg (5,000 lb). Nation: USA.
Agency: NSA.
Manufacturer: TRW.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
USAF Sat Cat: 32287 . COSPAR: 2007-054A. Apogee: 36,325 km (22,571 mi). Perigee: 35,800 km (22,200 mi). Inclination: 0.00 deg. Period: 1,436.00 min.
Final DSP launch. The series was to be replaced by SBIRS, which was in the middle of a troubled development program. The Delta 4H performed well after problems on its first launch. The RL10-powered upper stage made three burns before releasing the early-warning satellite in its final geosynchronous orbit. Total cost of the flight was $700 million, with the DSP worth $400 million. The DSP carried a special 25 kg supplementary payload designed to detect extremely small nuclear tests in space. The payload was required by a secret White House/National Security Council directive to detect any attempted covert nuclear tests by Iran or North Korea.
2007 November 11 - .
22:48 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 3 - .
Payload: Jianbing 5. Mass: 2,700 kg (5,900 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-5.
USAF Sat Cat: 32289 . COSPAR: 2007-055A. Apogee: 629 km (390 mi). Perigee: 628 km (390 mi). Inclination: 97.80 deg. Period: 97.30 min. The military launch used a new version of the CZ-4 booster. The CZ-4C includes a restart capability in the upper stage and a new interstage adapter between the first and second stages..
2007 December 9 - .
02:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7420-10C.
- Cosmo-SkyMed 2 - .
Mass: 1,700 kg (3,700 lb). Nation: Italy.
Agency: ASI.
Manufacturer: Alenia.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Prima.
Spacecraft: Cosmo-SkyMed.
USAF Sat Cat: 32376 . COSPAR: 2007-059A. Apogee: 624 km (387 mi). Perigee: 621 km (385 mi). Inclination: 97.90 deg. Period: 97.20 min. Second Italian military radar satellite in the Cosmo-Skymed system..
2007 December 14 - .
13:17 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-FG.
- Radarsat-2 - .
Mass: 2,200 kg (4,800 lb). Nation: Canada.
Agency: Starsem.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: BCP-4000.
Spacecraft: Radarsat.
USAF Sat Cat: 32382 . COSPAR: 2007-061A. Apogee: 793 km (492 mi). Perigee: 791 km (491 mi). Inclination: 98.60 deg. Period: 100.70 min.
Follow-on to Canadian Radarsat-1 launched in 1995. Designed to provide C-band synthetic aperture radar mapping with resolution of 3 m to Canadian government users. Compared to the earlier model had greater resolution, vastly increased on-board data storage capacity, and capability to scan left or right of ground track. Planned lifetime of seven years.
2008 January 21 - .
Launch Vehicle:
PSLV.
- Tecsar - .
Mass: 260 kg (570 lb). Nation: Israel.
Agency: ISRO.
Manufacturer: IAI.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Tecsar.
USAF Sat Cat: 32476 . COSPAR: 2008-002A. Apogee: 580 km (360 mi). Perigee: 405 km (251 mi). Inclination: 41.00 deg. Period: 94.50 min. Israeli military radar/optical surveillance satellite using synthetic aperture X-band radar, with estimated 10 cm radar and 1 m optical ground resolution..
2008 March 13 - .
10:02 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 411.
2008 March 27 - .
17:15 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- SAR-Lupe 4 - .
Mass: 730 kg (1,600 lb). Nation: Germany.
Agency: KVR.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: SAR-Lupe.
USAF Sat Cat: 32750 . COSPAR: 2008-014A. Apogee: 502 km (311 mi). Perigee: 471 km (292 mi). Inclination: 98.20 deg. Period: 94.30 min. Fourth of five planned German military surveillance satellites using synthetic aperture radar for target coverage at night and in all weathers. Orbital plane ascending node 143 deg, same plane as SAR-Lupe 1..
2008 April 28 - .
03:53 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
Launch Vehicle:
PSLV.
- Cartosat 2A - .
Mass: 768 kg (1,693 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: IRS.
USAF Sat Cat: 32783 . COSPAR: 2008-021A. Apogee: 645 km (400 mi). Perigee: 623 km (387 mi). Inclination: 98.00 deg. Period: 97.40 min. Primary payload, an imaging satellite with a spatial resolution of better than one metre and a swath of 9.6 km. Data from the satellite was to be used for detailed mapping..
- IMS 1 - .
Mass: 60 kg (132 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: IMS.
USAF Sat Cat: 32786 . COSPAR: 2008-021D. Apogee: 638 km (396 mi). Perigee: 620 km (380 mi). Inclination: 98.00 deg. Period: 97.30 min. Indian Mini Satellite, a small imaging satellite..
2008 June 26 - .
23:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/24.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
- Cosmos 2440 - .
Mass: 2,600 kg (5,700 lb). Nation: Russia.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Prognoz SPRN.
USAF Sat Cat: 33108 . COSPAR: 2008-033A. Apogee: 35,799 km (22,244 mi). Perigee: 35,780 km (22,230 mi). Inclination: 2.10 deg. Period: 1,436.20 min.
2008 July 22 - .
02:40 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- SAR-Lupe 5 - .
Mass: 770 kg (1,690 lb). Nation: Germany.
Agency: KVR.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: SAR-Lupe.
USAF Sat Cat: 33244 . COSPAR: 2008-036A. Apogee: 501 km (311 mi). Perigee: 474 km (294 mi). Inclination: 98.20 deg. Period: 94.40 min. Fifth German SAR-Lupe radar surveillance satellite..
2008 July 26 - .
18:31 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
2008 August 29 - .
07:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
Launch Pad: LC109/95.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Tachys - .
Payload: RapidEye 1. Mass: 152 kg (335 lb). Nation: Germany.
Agency: Makeyev bureau.
Manufacturer: Surrey.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SSTL-150.
USAF Sat Cat: 33312 . COSPAR: 2008-040A. Apogee: 632 km (392 mi). Perigee: 606 km (376 mi). Inclination: 98.00 deg. Period: 97.10 min.
RapidEye AG of Brandenberg paid for launch of a constellation of five environmental monitoring satellites in a single launch, each with a mass of 152 kg including 12 kg of propellant. The satellites had an optical resolution of 6 meters, and were designed to provide on-demand images for agricultural storm damage assessment and support of emergency services.
- Mati - .
Payload: RapidEye 2. Mass: 152 kg (335 lb). Nation: Germany.
Agency: Makeyev bureau.
Manufacturer: Surrey.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SSTL-150.
USAF Sat Cat: 33313 . COSPAR: 2008-040B. Apogee: 654 km (406 mi). Perigee: 624 km (387 mi). Inclination: 98.00 deg. Period: 97.50 min.
- Choma - .
Payload: RapidEye 3. Mass: 152 kg (335 lb). Nation: Germany.
Agency: Makeyev bureau.
Manufacturer: Surrey.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SSTL-150.
USAF Sat Cat: 33314 . COSPAR: 2008-040C. Apogee: 631 km (392 mi). Perigee: 598 km (371 mi). Inclination: 98.00 deg. Period: 97.00 min.
- Choros - .
Payload: RapidEye 4. Mass: 152 kg (335 lb). Nation: Germany.
Agency: Makeyev bureau.
Manufacturer: Surrey.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SSTL-150.
USAF Sat Cat: 33315 . COSPAR: 2008-040D. Apogee: 639 km (397 mi). Perigee: 620 km (380 mi). Inclination: 98.00 deg. Period: 97.30 min.
- Trochia - .
Payload: RapidEye 5. Mass: 152 kg (335 lb). Nation: Germany.
Agency: Makeyev bureau.
Manufacturer: Surrey.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SSTL-150.
USAF Sat Cat: 33316 . COSPAR: 2008-040E. Apogee: 647 km (402 mi). Perigee: 623 km (387 mi). Inclination: 98.00 deg. Period: 97.40 min.
2008 September 6 - .
03:25 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- HJ-1A - .
Payload: Huan Jing-1A. Mass: 470 kg (1,030 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: CAST2000.
USAF Sat Cat: 33320 . COSPAR: 2008-041A. Apogee: 662 km (411 mi). Perigee: 628 km (390 mi). Inclination: 98.00 deg. Period: 97.60 min. 'Environment' satellites that carried visible and infrared sensors..
- HJ-1B - .
Payload: Huan Jing-1B. Mass: 470 kg (1,030 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: CAST2000.
USAF Sat Cat: 33321 . COSPAR: 2008-041B. Apogee: 672 km (417 mi). Perigee: 626 km (388 mi). Inclination: 98.00 deg. Period: 97.70 min.
2008 September 6 - .
18:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7420-10C.
- GeoEye-1 - .
Mass: 1,923 kg (4,239 lb). Nation: USA.
Agency: Martin.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: SA-200.
USAF Sat Cat: 33331 . COSPAR: 2008-042A. Apogee: 687 km (426 mi). Perigee: 670 km (410 mi). Inclination: 98.10 deg. Period: 98.30 min. Commercial optical surveillance satellite with an 0.4-meter resolution. Primary customer was the US National Geospatial Intelligence Agency..
2008 October 1 - .
Launch Site:
Dombarovskiy.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Theos - .
Mass: 715 kg (1,576 lb). Nation: Thailand.
Agency: Makeyev bureau.
Manufacturer: EADS Astrium.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: T200.
Spacecraft: ROCSAT.
USAF Sat Cat: 33396 . COSPAR: 2008-049A. Apogee: 693 km (430 mi). Perigee: 673 km (418 mi). Inclination: 98.80 deg. Period: 98.40 min. Thai surveillance satellite, based on EADS Astrium bus used for ROCSAT-2..
2008 October 25 - .
01:15 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- SJ-6-03A SJ-6E - .
Mass: 2,700 kg (5,900 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: SJ-6.
USAF Sat Cat: 33408 . COSPAR: 2008-053A. Apogee: 603 km (374 mi). Perigee: 584 km (362 mi). Inclination: 97.70 deg. Period: 96.50 min. Third pair in China's SJ military surveillance constellation. It has been suggested that each pair consists of two differing satellites, a smaller minisatellite built by SAST Shanghai and a larger 300-kg CAST-968 bus satellite from DFH..
- SJ-6-03B SJ-6F - .
Mass: 2,700 kg (5,900 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: CAST2000.
USAF Sat Cat: 33409 . COSPAR: 2008-053B. Apogee: 605 km (375 mi). Perigee: 582 km (361 mi). Inclination: 97.70 deg. Period: 96.50 min.
2008 October 25 - .
02:28 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7420-10C.
- COSMO 3 - .
Mass: 1,900 kg (4,100 lb). Nation: Italy.
Agency: Martin.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Prima.
Spacecraft: Cosmo-SkyMed.
USAF Sat Cat: 33412 . COSPAR: 2008-054A. Apogee: 623 km (387 mi). Perigee: 622 km (386 mi). Inclination: 97.90 deg. Period: 97.20 min. Part of Italy's all-weather military surveillance constellation; carried X-band synthetic aperture radar..
2008 November 14 - .
15:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2445 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Decay Date: 2009-02-23 . USAF Sat Cat: 33439 . COSPAR: 2008-058A. Apogee: 327 km (203 mi). Perigee: 181 km (112 mi). Inclination: 67.20 deg. Period: 89.60 min. Recoverable reconnaisance satellite. Launched annually since 2005 with a typical 75 to 100 day mission, with recovery on an interim basis of two film capsules and final deorbiting of the camera and main film magazine..
2008 December 1 - .
04:42 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Yaogan 4 - .
Payload: Jianbing 6. Mass: 1,300 kg (2,800 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-6.
USAF Sat Cat: 33446 . COSPAR: 2008-061A. Apogee: 654 km (406 mi). Perigee: 632 km (392 mi). Inclination: 97.90 deg. Period: 97.60 min. Fourth 'Remote Sensing Satellite'; presumed military mission..
2008 December 2 - .
05:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2446 - .
Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2017-05-06 . USAF Sat Cat: 33447 . COSPAR: 2008-062A. Apogee: 39,772 km (24,713 mi). Perigee: 625 km (388 mi). Inclination: 63.00 deg. Period: 718.60 min. Molniya-orbit early warning satellite..
2008 December 15 - .
03:22 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Yaogan 5 - .
Payload: Jianbing 8. Mass: 2,800 kg (6,100 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-10.
Decay Date: 2014-09-02 . USAF Sat Cat: 33456 . COSPAR: 2008-064A. Apogee: 496 km (308 mi). Perigee: 486 km (301 mi). Inclination: 97.40 deg. Period: 94.40 min.
One of the two different series of military surveillance satellites launched under the YW designation, although YW 5 was in a lower orbit similar to the ZY-2 satellites, lower than previous YW satellites. The launch vehicle was announced as a CZ-4B, but appeared to be a CZ-4B with the CZ-4C's restartable YF-40A upper stage under the larger CZ-4C nose fairing.
2009 January 18 - .
02:47 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC37B.
Launch Pad: SLC37B.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 202 - .
Payload: Orion 6 / NROL-26. Mass: 5,400 kg (11,900 lb). Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: SIGINT. Spacecraft: Advanced Orion.
USAF Sat Cat: 33490 . COSPAR: 2009-001A. Apogee: 38,077 km (23,659 mi). Perigee: 35,943 km (22,333 mi). Inclination: 3.00 deg. Period: 1,440.00 min. Classified signals intelligence satellite. It was speculated that it was a large-antenna spacecraft with the same mission as earlier Rhyolite, Aquacade, Magnum, and Orion missions..
2009 January 23 - .
03:54 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- PRISM - .
Mass: 5.00 kg (11.00 lb). Nation: Japan.
Agency: Mitsubishi.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: PRISM.
USAF Sat Cat: 33493 . COSPAR: 2009-002B. Apogee: 641 km (398 mi). Perigee: 614 km (381 mi). Inclination: 98.00 deg. Period: 97.30 min. Remote sensing picosatellite built by the University of Tokyo, with a 10-cm aperture Earth imager on a 1-meter deployable boom..
- KKS 1 - .
Mass: 3.00 kg (6.60 lb). Nation: Japan.
Agency: Mitsubishi.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: KKS.
USAF Sat Cat: 33499 . COSPAR: 2009-002H. Apogee: 667 km (414 mi). Perigee: 651 km (404 mi). Inclination: 98.00 deg. Period: 97.90 min. Picosatellite built by Kouku-kosen, the Tokyo Metropolitan College of Aeronautical Engineering, carrying an Earth imager..
2009 February 11 - .
22:09 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5ECA.
- Spirale A - .
Mass: 117 kg (257 lb). Nation: France.
Agency: Arianespace.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 33751 . COSPAR: 2009-008C. Apogee: 35,693 km (22,178 mi). Perigee: 631 km (392 mi). Inclination: 1.80 deg. Period: 637.60 min. Demonstrator to prove infrared sensors designed to detect ballistic missile launches and other military targets..
- Spirale B - .
Mass: 117 kg (257 lb). Nation: France.
Agency: Arianespace.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 33752 . COSPAR: 2009-008D. Apogee: 35,681 km (22,171 mi). Perigee: 641 km (398 mi). Inclination: 1.80 deg. Period: 637.60 min.
2009 April 20 - .
01:15 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
Launch Vehicle:
PSLV.
- Risat-2 - .
Mass: 340 kg (740 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Tecsar.
USAF Sat Cat: 34807 . COSPAR: 2009-019A. Apogee: 552 km (342 mi). Perigee: 446 km (277 mi). Inclination: 41.20 deg. Period: 94.60 min. Tecsar-class radar imaging satellite bought by India from Israel..
2009 April 22 - .
02:55 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- Yaogan 6 - .
Payload: Jianbing 7. Mass: 1,200 kg (2,600 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: ELINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-7.
USAF Sat Cat: 34839 . COSPAR: 2009-021A. Apogee: 512 km (318 mi). Perigee: 512 km (318 mi). Inclination: 97.60 deg. Period: 94.90 min.
2009 April 29 - .
16:58 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2450 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 90.00 days. Decay Date: 2009-07-27 . USAF Sat Cat: 34871 . COSPAR: 2009-022A. Apogee: 282 km (175 mi). Perigee: 180 km (110 mi). Inclination: 67.10 deg. Period: 89.10 min. Return film capsule optical reconnaisance satellite. Landed on 27 July..
2009 May 5 - .
20:24 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7920-10C.
- USA 205 - .
Payload: STSS-ATRR. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: Martin.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft: SA-200.
USAF Sat Cat: 34903 . COSPAR: 2009-023A. Space Tracking and Surveillance System Advanced Technology Risk Reduction satellite..
2009 July 14 - .
03:36 GMT - .
Launch Site:
Kwajalein.
Launch Complex:
Kwajalein OM.
LV Family:
Falcon.
Launch Vehicle:
Falcon 1.
- Razaksat - .
Mass: 180 kg (390 lb). Nation: Malaysia.
Agency: SpaceX.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Satrec.
USAF Sat Cat: 35578 . COSPAR: 2009-037A. Apogee: 690 km (420 mi). Perigee: 665 km (413 mi). Inclination: 9.00 deg. Period: 98.30 min. Malaysian imaging satellite..
2009 July 29 - .
18:46 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Dubaisat 1 - .
Mass: 190 kg (410 lb). Nation: UAE.
Agency: Makeyev bureau.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: SatRec.
USAF Sat Cat: 35682 . COSPAR: 2009-041B. Apogee: 682 km (423 mi). Perigee: 666 km (413 mi). Inclination: 98.10 deg. Period: 98.20 min. Emirates Institute of Advanced Science and Technology, Dubai..
2009 September 17 - .
15:55 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Sterkh 12L - .
Mass: 160 kg (350 lb). Nation: Russia.
Class: Surveillance.
Type: Search and rescue satellite. Spacecraft: Sterkh.
USAF Sat Cat: 35866 . COSPAR: 2009-049B. Apogee: 818 km (508 mi). Perigee: 814 km (505 mi). Inclination: 98.54 deg. Period: 101.22 min. Second dedicated Sterkh search-and-rescue satellite..
- UGATUSAT - .
Mass: 35 kg (77 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: UGATUSAT.
USAF Sat Cat: 35869 . COSPAR: 2009-049E. Apogee: 821 km (510 mi). Perigee: 815 km (506 mi). Inclination: 98.54 deg. Period: 101.25 min. Remote sensing satellite built by the Ufa State Aviation Technical University..
2009 September 23 - .
06:21 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
Launch Vehicle:
PSLV.
- Oceansat-2 - .
Mass: 1,000 kg (2,200 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: IRS.
Spacecraft: Oceansat.
USAF Sat Cat: 35931 . COSPAR: 2009-051A. Apogee: 726 km (451 mi). Perigee: 720 km (440 mi). Inclination: 98.30 deg. Period: 99.20 min. Remote sensing satellite with an 8-band ocean color monitor, a radar scatterometer and a radio occultation atmospheric sounder..
2009 October 8 - .
18:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7920-10C.
- WorldView-2 - .
Mass: 2,615 kg (5,765 lb). Nation: USA.
Agency: Martin.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: BCP-5000.
Spacecraft: WorldView.
USAF Sat Cat: 35946 . COSPAR: 2009-055A. Apogee: 769 km (477 mi). Perigee: 766 km (475 mi). Inclination: 98.50 deg. Period: 100.20 min. Commercial 0.5-meter-resolution, 8-band imaging
satellite..
2009 November 12 - .
02:45 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- SJ-11-01 - .
Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: SJ-11.
USAF Sat Cat: 36088 . COSPAR: 2009-061A. Apogee: 705 km (438 mi). Perigee: 688 km (427 mi). Inclination: 98.30 deg. Period: 98.70 min. Experimental Satellite, believed to carry infrared surveillance system sensors..
2009 November 20 - .
10:44 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2455 - .
Payload: Lotos-S. Mass: 6,620 kg (14,590 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: SIGINT. Spacecraft: Lotos-S.
USAF Sat Cat: 36095 . COSPAR: 2009-063A. Apogee: 908 km (564 mi). Perigee: 902 km (560 mi). Inclination: 67.20 deg. Period: 103.10 min.
First Lotos-S electronic intelligence satellite, built by TsSKB-Progress, Samara and KB Arsenal, Saint Petersburg, using the same bus as the Resurs-DK optical remote sensing satellites. Maneuvered from an initial orbit of 199 km x 904 km x 67.2 deg to operational orbit of 903 km x 906 km on 23 November.
2009 November 28 - .
01:21 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS O-3 - .
Nation: USA.
Agency: Mitsubishi.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IGS.
USAF Sat Cat: 36104 . COSPAR: 2009-066A. Information Gathering Satellite, an optical surveillance satellite operated by Japan's Cabinet Satellite Intelligence Center..
2009 December 9 - .
08:42 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Yaogan 7 - .
Payload: Jianbing 6. Mass: 1,300 kg (2,800 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-6.
USAF Sat Cat: 36110 . COSPAR: 2009-069A. Apogee: 659 km (409 mi). Perigee: 623 km (387 mi). Inclination: 97.80 deg. Period: 97.50 min. Remote-Sensing Satellite, apparently a military optical surveillance satellite similar to YW-2 and YW-4..
2009 December 15 - .
02:31 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 8 - .
Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-9.
USAF Sat Cat: 36121 . COSPAR: 2009-072A. Apogee: 1,204 km (748 mi). Perigee: 1,193 km (741 mi). Inclination: 100.50 deg. Period: 109.40 min. Sun-synchronous orbit low resolution imaging satellite, primarily for civilian Earth resource studies. Supplemental military missions may include weather forecasting..
2009 December 18 - .
16:26 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5GS.
- Helios 2B - .
Mass: 4,200 kg (9,200 lb). Nation: France.
Agency: Arianespace.
Program: Helios.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: SPOT-5A-5B.
USAF Sat Cat: 36124 . COSPAR: 2009-073A. Apogee: 680 km (420 mi). Perigee: 680 km (420 mi). Inclination: 98.00 deg. French military surveillance satellite..
2010 March 5 - .
04:55 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 9A - .
Mass: 200 kg (440 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 36413 . COSPAR: 2010-009A. Apogee: 1,107 km (687 mi). Perigee: 1,075 km (667 mi). Inclination: 63.40 deg. Period: 107.10 min.
- Yaogan 9B - .
Mass: 2,000 kg (4,400 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 36414 . COSPAR: 2010-009B. Apogee: 1,107 km (687 mi). Perigee: 1,075 km (667 mi). Inclination: 63.40 deg. Period: 107.10 min.
- Yaogan 9C - .
Mass: 200 kg (440 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 36415 . COSPAR: 2010-009C. Apogee: 1,107 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.40 deg. Period: 107.10 min.
2010 April 16 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2462 - .
Mass: 6,900 kg (15,200 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Duration: 95.76 days. Decay Date: 2010-07-21 . USAF Sat Cat: 36511 . COSPAR: 2010-014A. Apogee: 270 km (160 mi). Perigee: 180 km (110 mi). Inclination: 67.20 deg. Period: 89.00 min. Recoverable optical surveillance satellite. Secondary recoverable film capsules probably recovered on 9 June and 18 July. Main spacecraft reentry vehicle landed at 09:10 GMT on 21 July 2010..
2010 June 15 - .
14:42 GMT - .
Launch Site:
Dombarovskiy.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Picard - .
Mass: 100 kg (220 lb). Nation: France.
Agency: Makeyev bureau.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 36598 . COSPAR: 2010-028A. Apogee: 730 km (450 mi). Perigee: 725 km (450 mi). Inclination: 98.30 deg. Period: 99.30 min. Solar observation payload..
2010 June 21 - .
02:14 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Tandem X - .
Mass: 1,350 kg (2,970 lb). Nation: Germany.
Agency: Makeyev bureau.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Astrobus.
Spacecraft: TerraSar-X.
USAF Sat Cat: 36605 . COSPAR: 2010-030A. Apogee: 509 km (316 mi). Perigee: 507 km (315 mi). Inclination: 97.50 deg. Period: 94.80 min. Radar surveillance satellite with 1-m resolution in spotlight mode..
2010 June 22 - .
19:00 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq 9 - .
Mass: 189 kg (416 lb). Nation: Israel.
Agency: ISA.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
USAF Sat Cat: 36608 . COSPAR: 2010-031A. Apogee: 586 km (364 mi). Perigee: 400 km (240 mi). Inclination: 141.80 deg. Period: 94.50 min. Israeli optical surveillance satellite..
2010 July 12 - .
03:52 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
Launch Vehicle:
PSLV.
- Cartosat 2B - .
Mass: 694 kg (1,530 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft: IRS.
USAF Sat Cat: 36795 . COSPAR: 2010-035A. Apogee: 647 km (402 mi). Perigee: 629 km (390 mi). Inclination: 98.10 deg. Period: 97.50 min. Cartography satellite with 0.8 meter resolution..
- Alsat 2A - .
Mass: 116 kg (255 lb). Nation: Algeria.
Agency: ISRO.
Program: Alsat.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 36798 . COSPAR: 2010-035D. Apogee: 674 km (418 mi). Perigee: 672 km (417 mi). Inclination: 98.20 deg. Period: 98.20 min. Optical surveillance satellite with 2.5 meter panchromatic resolution and 10 meter in 4 band/multispectral mode..
2010 August 9 - .
22:49 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 10 - .
Payload: Yaogan Weixing 10 / Jianbing 5. Mass: 2,700 kg (5,900 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-5.
USAF Sat Cat: 36834 . COSPAR: 2010-038A. Apogee: 630 km (390 mi). Perigee: 627 km (389 mi). Inclination: 97.80 deg. Period: 97.30 min. Radar imaging satellite..
2010 August 24 - .
07:10 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Tianhui-1 Weixing - .
Mass: 2,000 kg (4,400 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Tianhui.
USAF Sat Cat: 36985 . COSPAR: 2010-040A. Apogee: 507 km (315 mi). Perigee: 484 km (300 mi). Inclination: 97.40 deg. Period: 94.50 min. Research, mapping and land resource survey satellite..
2010 September 21 - .
04:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 501.
- USA 215 - .
Payload: NROL-41. Nation: USA.
Agency: Martin.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Topaz.
USAF Sat Cat: 37162 . COSPAR: 2010-046A. Apogee: 1,105 km (686 mi). Perigee: 1,102 km (684 mi). Inclination: 123.00 deg. Believed to be a surveillance radarsat, in an unusual retrograde, higher altitude orbit than previous versions..
2010 September 22 - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Yaogan 11 - .
Payload: Zheda Pixing 1A / Jianbing 6. Mass: 1,300 kg (2,800 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-6.
USAF Sat Cat: 37165 . COSPAR: 2010-047A. Apogee: 669 km (415 mi). Perigee: 626 km (388 mi). Inclination: 98.00 deg. Period: 97.70 min. Carried earth imaging camera..
2010 September 30 - .
Launch Site:
Vandenberg.
LV Family:
Peacekeeper.
Launch Vehicle:
Minotaur IV.
- USA 216 - .
Payload: SBSS. Mass: 1,031 kg (2,272 lb). Nation: USA.
Agency: USAF.
Manufacturer: Ball.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft: BCP-2000.
USAF Sat Cat: 37168 . COSPAR: 2010-048A. Apogee: 633 km (393 mi). Perigee: 632 km (392 mi). Inclination: 98.00 deg. Period: 97.40 min. First Space-Based Surveillance Satellite; designed to track satellites and orbital junk from a space-based vantage point..
2010 September 30 - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 2469 - .
Mass: 1,900 kg (4,100 lb). Nation: Russia.
Agency: KVR.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
USAF Sat Cat: 37170 . COSPAR: 2010-049A. Apogee: 39,609 km (24,611 mi). Perigee: 745 km (462 mi). Inclination: 62.90 deg. Period: 717.80 min. Early warning satellite..
2010 October 6 - .
00:49 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- SJ-6-04A SJ-6G - .
Payload: SJ-6/4A. Mass: 1,000 kg (2,200 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: SJ-6.
USAF Sat Cat: 37179 . COSPAR: 2010-051A. Apogee: 606 km (376 mi). Perigee: 587 km (364 mi). Inclination: 97.70 deg. Period: 96.60 min. Fourth pair of SJ-6 military surveillance satellites..
- SJ-6-04B SJ-6H - .
Payload: SJ-6/4B. Mass: 200 kg (440 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: CAST2000.
USAF Sat Cat: 37180 . COSPAR: 2010-051B. Apogee: 604 km (375 mi). Perigee: 588 km (365 mi). Inclination: 97.70 deg. Period: 96.60 min.
2010 November 6 - .
02:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7420-10C.
- Cosmo-SkyMed 4 - .
Mass: 1,900 kg (4,100 lb). Nation: Italy.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Prima.
Spacecraft: Cosmo-SkyMed.
USAF Sat Cat: 37216 . COSPAR: 2010-060A. Apogee: 623 km (387 mi). Perigee: 622 km (386 mi). Inclination: 97.90 deg. Period: 97.20 min. X-band radar satellite..
2010 November 21 - .
22:58 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC37B.
Launch Pad: SLC37B.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 223 - .
Payload: Orion 7 / NROL-32. Mass: 5,400 kg (11,900 lb). Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Advanced Orion.
USAF Sat Cat: 37232 . COSPAR: 2010-063A. Apogee: 35,800 km (22,200 mi). Perigee: 35,800 km (22,200 mi). Inclination: 0.00 deg. Period: 1,436.00 min. Probable geosynchronous signals intelligence satellite..
2011 January 20 - .
21:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 224 - .
Payload: EIS-6 / NROL-49. Mass: 17,000 kg (37,000 lb). Nation: USA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 37348 . COSPAR: 2011-002A. National Reconnaissance Office satellite placed into 252 km x 1023 km x 97.9 deg polar orbit, consistent with reports that it is was an Improved CRYSTAL type (KH-11 derivative) imaging reconnaissance satellite..
2011 April 15 - .
04:24 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 411.
- USA 229 - .
Payload: Intruder 9 / NROL-34. Mass: 3,250 kg (7,160 lb). Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 37386 . COSPAR: 2011-014A. Apogee: 1,200 km (700 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg. Period: 107.40 min. Probable naval ocean surveillance satellite cluster; normally operate in 1100 km circular orbits with 63 deg inclination and carry equipment to track ships and aircraft via their radio transmissions..
- USA 229 P/L 2 - .
Payload: Intruder 9 / NROL-34. Mass: 3,250 kg (7,160 lb). Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 37391 . COSPAR: 2011-014B. Apogee: 1,200 km (700 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg. Period: 107.40 min. Probable naval ocean surveillance satellite cluster; normally operate in 1100 km circular orbits with 63 deg inclination and carry equipment to track ships and aircraft via their radio transmissions..
2011 April 20 - .
04:42 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
Launch Vehicle:
PSLV.
- Resourcesat 2 - .
Mass: 1,200 kg (2,600 lb). Nation: India.
Program: IRS.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IRS.
USAF Sat Cat: 37387 . COSPAR: 2011-015A. Apogee: 825 km (512 mi). Perigee: 820 km (500 mi). Inclination: 98.80 deg. Period: 101.30 min.
Surveillance satellite. Carried the LISS-4 camera, a 6-meter-resolution imager, which was to be used for both military reconnaissance and civilian remote sensing. It also carried the lower resolution LISS-3 (23 m resolution) and AWIFS (56 m resolution), and an AIS Automatic Identification System payload for Comdev of Canada for tracking ships at sea.
2011 May 7 - .
18:10 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
Launch Pad: SLC41.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 230 - .
Payload: SBIRS GEO-1 / A2100M. Mass: 4,500 kg (9,900 lb). Nation: USA.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: AS 2100.
USAF Sat Cat: 37481 . COSPAR: 2011-019A. Apogee: 35,872 km (22,289 mi). Perigee: 35,851 km (22,276 mi). Inclination: 6.26 deg. Period: 1,439.93 min.
First geosynchronous element of the Space-Based Infrared System, an expensive new multispectral early warning and tracking system that forms part of the American missile defense system. The system also include payloads installed on Molniya-orbit signals intelligence satellite (USA 184 and USA 200). The spacecraft carry an infrared telescope with a large focal plane infrared array to monitor large areas of the Earth at once. An internal moving mirror scans the visible disk of the Earth to detect and track possible missile launches. It also has capabilites to track high-altitude aircraft and thermal events on the surface. The new SBIRS network will succeed 23 DSP satellites launched from 1970 to 2007. GEO-1 was inserted into geostationary transfer orbit by the booster and used its own on Leros-1 apogee motor to maneuver into geosynchronous orbit.
2011 June 27 - .
16:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
2011 June 30 - .
03:09 GMT - .
Launch Site:
Wallops Island.
Launch Complex:
Wallops Island LA0B.
LV Family:
Minuteman.
Launch Vehicle:
Minotaur 1.
- USA 231 - .
Payload: ORS-1. Mass: 450 kg (990 lb). Nation: USA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Road Runner.
Spacecraft: Tacsat ORS.
Decay Date: 2018-03-12 . USAF Sat Cat: 37728 . COSPAR: 2011-029A. Apogee: 409 km (254 mi). Perigee: 396 km (246 mi). Inclination: 40.00 deg. Period: 92.60 min.
Prototype optical surveillance satellite developed under the USAF Operationally Responsive Space program. Derived from Tacsat 3. Objective is to deploy small satellites to support military operations on short notice, either to provide a surge capability or to replace malfunctioning or disabled primary assets.
2011 July 6 - .
04:28 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- SJ-11-03 - .
Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: SJ-11.
USAF Sat Cat: 37730 . COSPAR: 2011-030A. Apogee: 702 km (436 mi). Perigee: 691 km (429 mi). Inclination: 98.20 deg. Period: 98.70 min. Military satellite, believed to be equipped with infrared sensors, perhaps for ballistic missile launch detection..
2011 July 29 - .
07:42 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- SJ-11-02 - .
Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: SJ-11.
USAF Sat Cat: 37765 . COSPAR: 2011-039A. Apogee: 705 km (438 mi). Perigee: 688 km (427 mi). Inclination: 98.10 deg. Period: 98.70 min. Believed to carry infrared surveillance system sensors..
2011 August 17 - .
07:12 GMT - .
Launch Site:
Taiyuan.
Launch Complex:
Taiyuan LC2.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Nigeriasat 2 - .
Mass: 268 kg (590 lb). Nation: Nigeria.
Agency: NSRDA.
Manufacturer: Surrey.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 37789 . COSPAR: 2011-044B. Apogee: 718 km (446 mi). Perigee: 693 km (430 mi). Inclination: 98.20 deg. Period: 98.90 min. Observation satellite with a 2.5-m resolution imager for Nigeria's National Space Research Development Agency..
2011 August 18 - .
09:28 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
FAILURE: Second stage vernier engine suffered a mechanical failure..
Failed Stage: 2.
- SJ-11-04 - .
Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: SJ-11.
Fourth satellite of the SJ-11 infrared surveillance system failed to reach orbit when the second stage vernier engine suffered a mechanical failure..
2011 September 23 - .
04:36 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS 6A - .
Mass: 1,000 kg (2,200 lb). Nation: Japan.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IGS.
USAF Sat Cat: 37813 . COSPAR: 2011-050A. IGS Optical-4 satellite to replenish Japan's military reconnaisance satellite constellation..
2011 November 9 - .
03:21 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Yaogan 12 - .
Payload: Jianbing 8. Mass: 2,800 kg (6,100 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-10.
USAF Sat Cat: 37875 . COSPAR: 2011-066B. Apogee: 497 km (308 mi). Perigee: 486 km (301 mi). Inclination: 97.40 deg. Period: 94.40 min. Military optical surveillance satellite..
2011 November 29 - .
18:50 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- Yaogan 13 - .
Payload: Jianbing 7. Mass: 1,200 kg (2,600 lb). Nation: China.
Agency: SISE.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-7.
USAF Sat Cat: 37941 . COSPAR: 2011-072A. Apogee: 511 km (317 mi). Perigee: 504 km (313 mi). Inclination: 97.10 deg. Period: 94.80 min. Military optical surveillance satellite. Probably operating in conjunction with the YW-6 radar satellite..
2011 December 12 - .
01:21 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS 7A - .
Mass: 1,000 kg (2,200 lb). Nation: Japan.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: IGS.
USAF Sat Cat: 37954 . COSPAR: 2011-075A. Apogee: 500 km (310 mi). Perigee: 500 km (310 mi). Inclination: 97.00 deg. Military surveillance radarsat..
2011 December 17 - .
02:03 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELS.
LV Family:
R-7.
Launch Vehicle:
Soyuz-ST-A.
- Pleiades HR1 - .
Mass: 970 kg (2,130 lb). Nation: France.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Pleiades.
USAF Sat Cat: 38007 . COSPAR: 2011-076A. Apogee: 692 km (429 mi). Perigee: 676 km (420 mi). Inclination: 98.20 deg. Period: 98.50 min. High resolution military surveillance satellite..
- Elisa 1 - .
Mass: 120 kg (260 lb). Nation: France.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 38008 . COSPAR: 2011-076B. Apogee: 692 km (429 mi). Perigee: 675 km (419 mi). Inclination: 98.20 deg. Period: 98.40 min.
Quartet of electronic intelligence satellites, which succeed Essaim as France's next space-based SIGINT demonstrator. Like Essaim, Elisa consists of four Myriade microsatellites equipped with electronic intelligence instruments to intercept radar transmissions from space. Elisa was to offer a pre-operational capability until a fully operational space-based intelligence capability would be deployed in 2016.
- Elisa 2 - .
Mass: 120 kg (260 lb). Nation: France.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 38009 . COSPAR: 2011-076C. Apogee: 693 km (430 mi). Perigee: 681 km (423 mi). Inclination: 98.20 deg. Period: 98.50 min.
- Elisa 3 - .
Mass: 120 kg (260 lb). Nation: France.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 38010 . COSPAR: 2011-076D. Apogee: 693 km (430 mi). Perigee: 674 km (418 mi). Inclination: 98.20 deg. Period: 98.40 min.
- Elisa 4 - .
Mass: 120 kg (260 lb). Nation: France.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 38011 . COSPAR: 2011-076E. Apogee: 616 km (382 mi). Perigee: 601 km (373 mi). Inclination: 98.20 deg. Period: 96.90 min.
- Fasat-Charlie - .
Mass: 50 kg (110 lb). Nation: Chile.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 38012 . COSPAR: 2011-076F. Apogee: 612 km (380 mi). Perigee: 597 km (370 mi). Inclination: 98.20 deg. Period: 96.80 min. Imaging satellite for the Chilean Air Force..
2011 December 22 - .
03:26 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- ZY-1 02C - .
Mass: 2,100 kg (4,600 lb). Nation: China.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Phoenix Eye.
USAF Sat Cat: 38038 . COSPAR: 2011-079A. Apogee: 775 km (481 mi). Perigee: 773 km (480 mi). Inclination: 98.50 deg. Period: 100.30 min. Military imaging payload with a resolution of 2.4 m..
2012 January 9 - .
03:17 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- ZY 3 - .
Mass: 2,636 kg (5,811 lb). Nation: China.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Phoenix Eye.
USAF Sat Cat: 38046 . COSPAR: 2012-001A. Apogee: 508 km (315 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. Period: 94.70 min.
First Chinese civil high-resolution stereoscopic Earth mapping satellite. The mission objective was to produce 1:50,000 scale maps and data for resource mapping, environmental surveying, disaster monitoring, city planning and national security needs. Project go-ahead was March 2008. For this mission the satellite had better positioning and attitude accuracy, multispectral capabilitym and high-data-rate data transmission to the ground - 2 x 450 Mbit/s. The satellite had a swath width of 51 km with a resolution of 2.1 m. The orbit provided a revisit period of 59 days.
2012 March 30 - .
05:49 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/24.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
- Cosmos 2479 - .
Payload: US-KMO 71Kh6. Mass: 2,600 kg (5,700 lb). Nation: Russia.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Prognoz SPRN.
USAF Sat Cat: 38101 . COSPAR: 2012-012A. Apogee: 35,883 km (22,296 mi). Perigee: 35,692 km (22,177 mi). Inclination: 2.10 deg. Period: 1,436.20 min. Early warning satellite stationed in geosynchronous orbit at 80.1 deg E..
2012 April 3 - .
23:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(5,2).
- USA 234 - .
Payload: NROL-25. Nation: USA.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Topaz.
USAF Sat Cat: 38109 . COSPAR: 2012-014A. Second FIA Radarsat mission, following NROL-41 / USA-25 / 2010-46A..
2012 April 26 - .
00:17 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
LV Family:
PSLV.
Launch Vehicle:
PSLV-XL.
- RISAT-1 - .
Mass: 1,858 kg (4,096 lb). Nation: India.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: IRS.
USAF Sat Cat: 38248 . COSPAR: 2012-017A. Apogee: 550 km (340 mi). Perigee: 529 km (328 mi). Inclination: 97.60 deg. Period: 95.40 min. Radar Imaging Satellite with a C-band synthetic aperture radar payload mounted on an IRS-
derived bus..
2012 May 6 - .
07:10 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Tianhui 1-02 - .
Payload: Tianhui 1B. Mass: 2,000 kg (4,400 lb). Nation: China.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft: Tianhui.
USAF Sat Cat: 38256 . COSPAR: 2012-020A. Apogee: 506 km (314 mi). Perigee: 485 km (301 mi). Inclination: 97.40 deg. Period: 94.50 min. Mapping-1 Satellite 02; carried visible-band mapping cameras with 5 m resolution..
2012 May 10 - .
07:06 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Yaogan 14 - .
Payload: Jianbing 11. Mass: 2,800 kg (6,100 lb). Nation: China.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-11.
USAF Sat Cat: 38257 . COSPAR: 2012-021A. Apogee: 479 km (297 mi). Perigee: 471 km (292 mi). Inclination: 97.20 deg. Period: 94.10 min. Military remote sensing
satellite..
2012 May 17 - .
14:05 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U-PVB.
- Cosmos 2480 - .
Payload: Kobalt-M. Mass: 6,700 kg (14,700 lb). Nation: Russia.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Decay Date: 2012-09-24 . USAF Sat Cat: 38335 . COSPAR: 2012-024A. Apogee: 280 km (170 mi). Perigee: 199 km (123 mi). Inclination: 81.40 deg. Period: 89.30 min. Kobalt-M film reconnaisance satellite. A deorbit burn on 24 September at 16:39 GMT was followed by separation of the service module and reentry of the pressurized main payload section which contained cameras and film. Landed at 17:03 GMT..
2012 May 17 - .
16:39 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- Arirang-3 - .
Payload: Kompsat-3. Mass: 800 kg (1,760 lb). Nation: Korea South.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: T200.
Spacecraft: Kompsat.
USAF Sat Cat: 38338 . COSPAR: 2012-025B. Apogee: 677 km (420 mi). Perigee: 665 km (413 mi). Inclination: 98.10 deg. Period: 98.20 min. South Korean imaging satellite..
2012 May 29 - .
07:31 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 15 - .
Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-9.
USAF Sat Cat: 38354 . COSPAR: 2012-029A. Apogee: 1,207 km (749 mi). Perigee: 1,201 km (746 mi). Inclination: 100.10 deg. Period: 109.50 min.
2012 June 29 - .
13:15 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC37B.
Launch Pad: SLC37B.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 237 - .
Payload: Orion 8 / NROL-15. Mass: 5,400 kg (11,900 lb). Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Advanced Orion.
USAF Sat Cat: 38528 . COSPAR: 2012-034A. Apogee: 35,800 km (22,200 mi). Perigee: 35,800 km (22,200 mi). Inclination: 0.00 deg. Period: 1,440.00 min. Probable geosynchronous signals intelligence satellite..
2012 July 22 - .
06:41 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-FG.
- Kanopus-V 1 - .
Payload: Kanopus-V. Mass: 473 kg (1,042 lb). Nation: Russia.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Kanopus.
USAF Sat Cat: 38707 . COSPAR: 2012-039A. Apogee: 507 km (315 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. Period: 94.70 min. Remote sensing satellite. Imager provided a resolution of 2.5 m in a 20 km swath and 12.5 m in four spectral channels along the same swath. A separate imager provided optical resolution of 25 m in a 250 km swath..
- BKA 2 - .
Payload: BelKA-2. Mass: 473 kg (1,042 lb). Nation: Belarus.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: Kanopus.
USAF Sat Cat: 38708 . COSPAR: 2012-039B. Apogee: 507 km (315 mi). Perigee: 506 km (314 mi). Inclination: 97.50 deg. Period: 94.80 min. Remote sensing satellite; replaced BelKa 1 satellite lost in an launch failure. Imager provided a resolution of 2.1 m and four spectral channels..
2012 September 13 - .
21:39 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 238 - .
Payload: Intruder 10 / NROL-36. Mass: 6,500 kg (14,300 lb). Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 38758 . COSPAR: 2012-048A. Apogee: 1,200 km (700 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg. Period: 107.40 min. NROL-36 mission, believed to be a naval signals intelligence satellite.
- RE - .
Payload: Re/STARE. Mass: 4.00 kg (8.80 lb). Nation: USA.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft: Cubesat.
USAF Sat Cat: 38765 . COSPAR: 2012-048H. Lawrence Livermore Natlional Laboratory space debris tracking experiment..
2012 November 18 - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- HJ-1C - .
Mass: 890 kg (1,960 lb). Nation: China.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: CAST2000.
USAF Sat Cat: 38997 . COSPAR: 2012-064A. Apogee: 503 km (312 mi). Perigee: 489 km (303 mi). Inclination: 97.30 deg. Period: 94.50 min. Small Chinese S-band semi-active radar earth observation satellite providing all-weather imagery at 100 m resolution. Part of a constellation that includes of two small optical satellites, the HJ-1A and the HJ-1B..
2012 November 25 - .
04:06 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 16A - .
Mass: 2,000 kg (4,400 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 39011 . COSPAR: 2012-066A. Apogee: 1,096 km (681 mi). Perigee: 1,085 km (674 mi). Inclination: 63.40 deg. Period: 107.10 min. Believed to be a military naval SIGINT surveillance system, consisting of a main satellite and two subsatellites. Second such launch after 2010's Yaogan 9..
- Yaogan 16B - .
Mass: 200 kg (440 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 39012 . COSPAR: 2012-066B. Apogee: 1,095 km (680 mi). Perigee: 1,086 km (674 mi). Inclination: 63.40 deg. Period: 107.10 min.
- Yaogan 16C - .
Mass: 200 kg (440 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 39013 . COSPAR: 2012-066C. Apogee: 1,096 km (681 mi). Perigee: 1,085 km (674 mi). Inclination: 63.40 deg. Period: 107.10 min.
2012 December 2 - .
02:02 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELS.
LV Family:
R-7.
Launch Vehicle:
Soyuz-ST-A.
- Pleiades 1B - .
Mass: 970 kg (2,130 lb). Nation: France.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Pleiades.
USAF Sat Cat: 39019 . COSPAR: 2012-068A. Apogee: 699 km (434 mi). Perigee: 697 km (433 mi). Inclination: 98.20 deg. Period: 98.70 min. High resolution French military optical reconnaisance satellite..
2012 December 18 - .
16:12 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Gokturk 2 - .
Mass: 1,100 kg (2,400 lb). Nation: Turkey.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Proteus.
USAF Sat Cat: 39030 . COSPAR: 2012-073A. Apogee: 691 km (429 mi). Perigee: 668 km (415 mi). Inclination: 98.20 deg. Period: 98.30 min. Earth observation satellite for the Turkish Defense Ministry. Provides high-resolution imagery of 2.5 m esolution panchromatic, 10 m multispectral (VNIR) and 20 m SWIR..
2013 January 27 - .
04:40 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS 8A - .
Payload: JSE Reda-4. Mass: 1,000 kg (2,200 lb). Nation: Japan.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: IGS.
USAF Sat Cat: 39061 . COSPAR: 2013-002A. Apogee: 524 km (325 mi). Perigee: 512 km (318 mi). Inclination: 97.50 deg. Period: 94.90 min. IGS military radar satellite 4, with a synthetic aperture radar payload..
- IGS 8B (DEMO) - .
Payload: Jissho eisei. Mass: 1,000 kg (2,200 lb). Nation: Japan.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IGS.
USAF Sat Cat: 39062 . COSPAR: 2013-002B. Apogee: 524 km (325 mi). Perigee: 512 km (318 mi). Inclination: 97.50 deg. Period: 94.98 min. Demonstration satellite, with a test optical imaging payload..
2013 February 25 - .
12:31 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
Launch Vehicle:
PSLV.
- Sapphire - .
Mass: 150 kg (330 lb). Nation: Canada.
Agency: DND.
Manufacturer: Surrey.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft: SSTL-150.
USAF Sat Cat: 39088 . COSPAR: 2013-009C. Apogee: 787 km (489 mi). Perigee: 772 km (479 mi). Inclination: 98.63 deg. Period: 100.44 min. Canadian Forces satellite for space object surveillance and missile early warning, based with a 0.15m visible-light telescope..
2013 March 19 - .
21:21 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
Launch Pad: SLC41.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 241 - .
Payload: SBIRS GEO-2 / A2100M. Mass: 4,500 kg (9,900 lb). Nation: USA.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: AS 2100.
USAF Sat Cat: 39120 . COSPAR: 2013-011A. Apogee: 35,800 km (22,200 mi). Perigee: 35,775 km (22,229 mi). Inclination: 6.00 deg.
Second geosynchronous orbit in the Space-Based Infrared System for detecting missile launches and tracking missiles, air vehicles, and certain surface events. The Centaur upper stage placed the satellite in a 182 km x 35804 km x 22.2 deg transfer orbit. SBIR-2 used its own engines to reach its operational geosynchronous orbit.
2013 April 26 - .
04:13 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Gaofen 1 - .
Mass: 800 kg (1,760 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CAST2000.
USAF Sat Cat: 39150 . COSPAR: 2013-018A. Apogee: 656 km (407 mi). Perigee: 628 km (390 mi). Inclination: 98.06 deg. Period: 97.56 min. High resolution imaging satellite with a 2 m resolution pan-chromatic camera, an 8 m resolution multi-spectral camera and a 16 m resolution wide-angle multi-spectral camera..
2013 May 7 - .
02:06 GMT - .
Launch Site:
Xichang.
Launch Vehicle:
Vega.
- Proba-V - .
Mass: 158 kg (348 lb). Nation: Europe.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: PROBA.
USAF Sat Cat: 39159 . COSPAR: 2013-021A. Apogee: 819 km (508 mi). Perigee: 814 km (505 mi). Inclination: 98.72 deg. Period: 101.21 min. European Space Agency technology satellite; carryied the Vegetation sensor previously used on French SPOT remote sensing satellites..
- VNREDSAT-1 - .
Payload: AstroSat-100. Mass: 115 kg (253 lb). Nation: Vietnam.
Class: Surveillance.
Type: SIGINT. Spacecraft: Myriade.
USAF Sat Cat: 39160 . COSPAR: 2013-021B. Apogee: 685 km (425 mi). Perigee: 683 km (424 mi). Inclination: 98.13 deg. Period: 98.43 min. Remote sensing satellite for the Vietnam Academy of Science and Technology..
2013 June 7 - .
18:37 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43.
Launch Pad: LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Cosmos 2486 - .
Mass: 7,100 kg (15,600 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Persona.
USAF Sat Cat: 39177 . COSPAR: 2013-028A. Apogee: 733 km (455 mi). Perigee: 714 km (443 mi). Inclination: 98.30 deg. Period: 99.26 min. Second Persona reconnaisance satellite, in sun-synchronous orbit with 10:31 local time descending node. Said to have failed after a short time in orbit..
2013 June 25 - .
17:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
Launch Pad: LC31/6.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Resurs-P - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Resurs-Spektr.
USAF Sat Cat: 39186 . COSPAR: 2013-030A. Apogee: 473 km (293 mi). Perigee: 459 km (285 mi). Inclination: 97.28 deg. Period: 93.91 min. Civilian imaging satellite with a Geoton-L1 telescope with 1-meter resolution multispectral imager and a 25m resolution hyperspectral imager..
2013 July 15 - .
09:27 GMT - .
Launch Site:
Jiuquan.
Launch Pad: xxx.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- SJ-11-05 - .
Nation: China.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: SJ-11.
USAF Sat Cat: 39202 . COSPAR: 2013-035A. Apogee: 702 km (436 mi). Perigee: 687 km (426 mi). Inclination: 98.15 deg. Period: 98.66 min. Suspected infrared-telescope-equipped missile early warning satellite; replaces the fourth spacecraft was lost in a launch failure in 2011..
2013 July 19 - .
23:37 GMT - .
Launch Site:
Taiyuan.
Launch Pad: xxx.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Shiyan 7 - .
Mass: 800 kg (1,760 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CAST3000.
USAF Sat Cat: 39208 . COSPAR: 2013-037A. Apogee: 674 km (418 mi). Perigee: 660 km (410 mi). Inclination: 98.04 deg. Period: 98.09 min. Satellite inspector with robotic arm. After maneuvering close to Chuangxin-3 on 6 and 9 August, it completed an unexpected rendezvous in a 564 x 610 km x 97.7 deg orbit with the Shi Jian 7 (SJ-7), launched in 2005..
2013 August 22 - .
14:39 GMT - .
Launch Site:
Dombarovskiy.
Launch Pad: Yasniy Sh370/13.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Arirang-5 - .
Payload: Kompsat-5. Mass: 1,400 kg (3,000 lb). Nation: Korea South.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: T200.
Spacecraft: Kompsat.
USAF Sat Cat: 39227 . COSPAR: 2013-042A. Apogee: 560 km (340 mi). Perigee: 545 km (338 mi). Inclination: 97.60 deg. Period: 95.70 min. South Korea's first X-band SAR satellite..
2013 August 28 - .
18:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 245 - .
Payload: EIS- 7 / NROL-65. Mass: 15,000 kg (33,000 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 39232 . COSPAR: 2013-043A. Apogee: 1,002 km (622 mi). Perigee: 259 km (160 mi). Inclination: 97.90 deg. Secret payload for the National Reconnaissance Office; thought to be an imaging spy satellite of the EIS/Enhanced CRYSTAL type..
2013 September 1 - .
19:16 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 17A - .
Mass: 2,000 kg (4,400 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 39239 . COSPAR: 2013-046A. Apogee: 1,116 km (693 mi). Perigee: 1,065 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.
Triplet of naval surveillance satellites, believed to operate like the old US PARCAE/NOSS system, in which a group of loosely formation-flying spacecraft locate radio emitters using the difference in time of arrival of the radio signals at the different satellites.
- Yaogan 17B - .
Mass: 200 kg (440 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 39240 . COSPAR: 2013-046B. Apogee: 1,116 km (693 mi). Perigee: 1,065 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.
- Yaogan 17C - .
Mass: 200 kg (440 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 39241 . COSPAR: 2013-046C. Apogee: 1,116 km (693 mi). Perigee: 1,064 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.
2013 September 25 - .
04:37 GMT - .
Launch Site:
Jiuquan.
LV Family:
DF-21.
Launch Vehicle:
Kuaizhou.
- Kuaizhou-1 - .
Payload: KZ-1. Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Kuaizhou satellite.
Decay Date: 2015-09-01 . USAF Sat Cat: 39262 . COSPAR: 2013-053A. Apogee: 301 km (187 mi). Perigee: 279 km (173 mi). Inclination: 96.59 deg. Period: 90.31 min.
First launch of China's Kuaizhou small quick-response launch vehicle. "Kuaizhou" means "Swift Boat". The solid propellant vehicle is thought to be built by CASIC in collaboration with the Harbin Institute of Technology and may be a derivative of the DF-21 family, like the failed KT-1 launch vehicle of 2002-2003. Development of the rocket began in 2010. The satellite's initial orbit was 275 x 293 km x 96.7 deg, raised on 27 September to 299 x 306 km. The satellite payload is operated by the State Remote Sensing Center. The satellite maneuvered following launch: its initial 275 x 293 km orbit, was raised on September 27 to 299 x 306 km. The orbit decayed to 279 x 288 km and then was raised on October 17 to 288 x 321 km; after a further decay another reboost on November 1 restored the orbit to 290 x 317 km. The third reboost on November 19 raised the orbit from 267 x 294 km to 287 x 322 km.
2013 October 29 - .
02:50 GMT - .
Launch Site:
Taiyuan.
Launch Pad: xxx.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- Yaogan 18 - .
Payload: Jianbing 7. Mass: 1,200 kg (2,600 lb). Nation: China.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-7.
USAF Sat Cat: 39363 . COSPAR: 2013-059A. Apogee: 514 km (319 mi). Perigee: 510 km (310 mi). Inclination: 97.52 deg. Period: 94.87 min. The third in a satellite series that began with Yaogan 6 and 13..
2013 November 20 - .
01:15 GMT - .
Launch Site:
Wallops Island.
Launch Complex:
Wallops Island LA0B.
LV Family:
Minuteman.
Launch Vehicle:
Minotaur 1.
- Horus/STARE-B - .
Mass: 3.00 kg (6.60 lb). Nation: USA.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft: Cubesat.
Decay Date: 2018-04-26 . USAF Sat Cat: 39397 . COSPAR: 2013-064T. Apogee: 489 km (303 mi). Perigee: 482 km (299 mi). Inclination: 40.51 deg. Period: 94.32 min. Cubesat; a 3U Lawrence Livermore experiment for space debris monitoring..
- Ho oponopono 2 - .
Mass: 3.00 kg (6.60 lb). Nation: USA.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Cubesat.
USAF Sat Cat: 39403 . COSPAR: 2013-064Z. Apogee: 492 km (305 mi). Perigee: 485 km (301 mi). Inclination: 40.53 deg. Period: 94.38 min. 3U Cubesat for radar calibration, from University of Hawaii-Manoa..
2013 November 20 - .
03:31 GMT - .
Launch Site:
Taiyuan.
Launch Pad: xxx.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 19 - .
Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-9.
USAF Sat Cat: 39410 . COSPAR: 2013-065A. Apogee: 1,208 km (750 mi). Perigee: 1,201 km (746 mi). Inclination: 100.45 deg. Period: 109.51 min. Thought to be an imaging satellite similar to Yaogan 8..
2013 November 21 - .
07:10 GMT - .
Launch Site:
Dombarovskiy.
Launch Pad: xxx.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- SkySat-1 - .
Mass: 90 kg (198 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Skysat.
USAF Sat Cat: 39418 . COSPAR: 2013-066C. Apogee: 595 km (369 mi). Perigee: 564 km (350 mi). Inclination: 97.79 deg. Period: 96.26 min. Imaging satellite, the first for the US company Skybox..
- Dubaisat-2 - .
Mass: 300 kg (660 lb). Nation: UAE.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SI-300.
USAF Sat Cat: 39419 . COSPAR: 2013-066D. Apogee: 600 km (370 mi). Perigee: 583 km (362 mi). Inclination: 97.79 deg. Period: 96.51 min. Imaging satellite for the United Arab Emirates build by Satrec of South Korea..
- Dove-3 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 39429 . COSPAR: 2013-066P. Apogee: 809 km (502 mi). Perigee: 593 km (368 mi). Inclination: 97.76 deg. Period: 98.80 min. 3U imaging satellite from PlanetLabs, San Francisco..
- Dove-4 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 39434 . COSPAR: 2013-066U. Apogee: 624 km (387 mi). Perigee: 581 km (361 mi). Inclination: 97.78 deg. Period: 96.75 min. 3U Earth imaging satellite, deployed from Unisat-5 for PlanetLabs..
2013 December 6 - .
07:14 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 501.
- USA 247 - .
Payload: NROL-39. Nation: USA.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Topaz.
USAF Sat Cat: 39462 . COSPAR: 2013-072A. Apogee: 1,089 km (676 mi). Perigee: 1,075 km (667 mi). Inclination: 123.00 deg. Classified launch; appears to have been the third TOPAZ radar satellite..
2013 December 9 - .
03:26 GMT - .
Launch Site:
Taiyuan.
Launch Pad: xxx.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
FAILURE: Failed to reach orbit; third stage shut down 11 seconds early..
- CBERS-3 ZY-1 FM 3 - .
Mass: 1,450 kg (3,190 lb). Nation: Brazil.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Phoenix Eye.
China-Brazil Earth Resources Satellite. It was initially reported the launch was a success, but in fact the CZ-4B rocket failed to reach orbit..
2013 December 28 - .
12:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1V.
- Cosmos 2493 - .
Payload: SKRL-756 No. 2. Mass: 45 kg (99 lb). Nation: Russia.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: SKRL.
USAF Sat Cat: 39491 . COSPAR: 2013-078B. Apogee: 625 km (388 mi). Perigee: 590 km (360 mi). Inclination: 82.42 deg. Period: 96.85 min. Calibration sphere. Announced as 'SKRL-756 No. 2' at time of launch..
- Aist 1 - .
Mass: 53 kg (116 lb). Nation: Russia.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Aist.
USAF Sat Cat: 39492 . COSPAR: 2013-078C. Apogee: 626 km (388 mi). Perigee: 595 km (369 mi). Inclination: 82.42 deg. Period: 96.91 min. Small satellite developed by TsSKB-Progress and the Samara Aerospace University; carried a magnetometer, acclerometers and a micrometeor experiment..
2014 February 11 - .
08:31 GMT - .
Launch Platform: ISS.
- Flock1-1 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-05-15 . USAF Sat Cat: 39512 . COSPAR: 1998-067DG. Apogee: 195 km (121 mi). Perigee: 181 km (112 mi). Inclination: 51.62 deg. Period: 88.26 min.
Flock-1 satellites, 3U Dove-class Earth imaging cubesats, for the San Francisco based company PlanetLabs, were deployed by the ISS JEM RMS at about 08:31 GMT on February 11. By February 15 all 16 satellites from the first Nanoracks bag had been ejected; by 19 February all of the Flock-1 satellites had been ejected.
- Flock1-2 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-09 . USAF Sat Cat: 39513 . COSPAR: 1998-067DH. Apogee: 162 km (100 mi). Perigee: 155 km (96 mi). Inclination: 51.60 deg. Period: 87.65 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-3 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-05-25 . USAF Sat Cat: 39514 . COSPAR: 1998-067DJ. Apogee: 170 km (100 mi). Perigee: 162 km (100 mi). Inclination: 51.63 deg. Period: 87.81 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-4 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-18 . USAF Sat Cat: 39515 . COSPAR: 1998-067DK. Apogee: 185 km (114 mi). Perigee: 169 km (105 mi). Inclination: 51.62 deg. Period: 88.03 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-5 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-02 . USAF Sat Cat: 39518 . COSPAR: 1998-067DL. Apogee: 154 km (95 mi). Perigee: 148 km (91 mi). Inclination: 51.61 deg. Period: 87.51 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-6 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-15 . USAF Sat Cat: 39519 . COSPAR: 1998-067DM. Apogee: 169 km (105 mi). Perigee: 156 km (96 mi). Inclination: 51.62 deg. Period: 87.73 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-11 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-06 . USAF Sat Cat: 39520 . COSPAR: 1998-067DN. Apogee: 175 km (108 mi). Perigee: 133 km (82 mi). Inclination: 51.58 deg. Period: 87.57 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-12 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-05-25 . USAF Sat Cat: 39521 . COSPAR: 1998-067DP. Apogee: 159 km (98 mi). Perigee: 153 km (95 mi). Inclination: 51.62 deg. Period: 87.61 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-13 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-07-06 . USAF Sat Cat: 39525 . COSPAR: 1998-067DQ. Apogee: 291 km (180 mi). Perigee: 287 km (178 mi). Inclination: 51.63 deg. Period: 90.30 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-14 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-14 . USAF Sat Cat: 39526 . COSPAR: 1998-067DR. Apogee: 165 km (102 mi). Perigee: 157 km (97 mi). Inclination: 51.61 deg. Period: 87.70 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-15 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-13 . USAF Sat Cat: 39527 . COSPAR: 1998-067DS. Apogee: 172 km (106 mi). Perigee: 165 km (102 mi). Inclination: 51.62 deg. Period: 87.86 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-16 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-10-26 . USAF Sat Cat: 39528 . COSPAR: 1998-067DT. Apogee: 370 km (220 mi). Perigee: 368 km (228 mi). Inclination: 51.64 deg. Period: 91.93 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-7 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-07-02 . USAF Sat Cat: 39529 . COSPAR: 1998-067DU. Apogee: 288 km (178 mi). Perigee: 279 km (173 mi). Inclination: 51.64 deg. Period: 90.19 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-8 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-20 . USAF Sat Cat: 39530 . COSPAR: 1998-067DV. Apogee: 177 km (109 mi). Perigee: 162 km (100 mi). Inclination: 51.61 deg. Period: 87.88 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-9 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-05-21 . USAF Sat Cat: 39531 . COSPAR: 1998-067DW. Apogee: 181 km (112 mi). Perigee: 166 km (103 mi). Inclination: 51.60 deg. Period: 87.96 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-10 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-20 . USAF Sat Cat: 39532 . COSPAR: 1998-067DX. Apogee: 171 km (106 mi). Perigee: 157 km (97 mi). Inclination: 51.62 deg. Period: 87.77 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-17 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-05-19 . USAF Sat Cat: 39555 . COSPAR: 1998-067DY. Apogee: 187 km (116 mi). Perigee: 177 km (109 mi). Inclination: 51.64 deg. Period: 88.14 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-18 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-10-29 . USAF Sat Cat: 39556 . COSPAR: 1998-067DZ. Apogee: 374 km (232 mi). Perigee: 370 km (220 mi). Inclination: 51.64 deg. Period: 92.00 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-21 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-05-25 . USAF Sat Cat: 39557 . COSPAR: 1998-067EA. Apogee: 161 km (100 mi). Perigee: 150 km (90 mi). Inclination: 51.61 deg. Period: 87.59 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-22 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-05 . USAF Sat Cat: 39558 . COSPAR: 1998-067EB. Apogee: 178 km (110 mi). Perigee: 165 km (102 mi). Inclination: 51.64 deg. Period: 87.92 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-19 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-03 . USAF Sat Cat: 39559 . COSPAR: 1998-067EC. Apogee: 190 km (110 mi). Perigee: 186 km (115 mi). Inclination: 51.63 deg. Period: 88.26 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-20 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-10-09 . USAF Sat Cat: 39560 . COSPAR: 1998-067ED. Apogee: 367 km (228 mi). Perigee: 363 km (225 mi). Inclination: 51.65 deg. Period: 91.85 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-23 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-07-10 . USAF Sat Cat: 39561 . COSPAR: 1998-067EE. Apogee: 321 km (199 mi). Perigee: 315 km (195 mi). Inclination: 51.64 deg. Period: 90.89 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-24 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-16 . USAF Sat Cat: 39562 . COSPAR: 1998-067EF. Apogee: 183 km (113 mi). Perigee: 172 km (106 mi). Inclination: 51.62 deg. Period: 88.04 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-25 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-24 . USAF Sat Cat: 39563 . COSPAR: 1998-067EG. Apogee: 245 km (152 mi). Perigee: 236 km (146 mi). Inclination: 51.63 deg. Period: 89.31 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-26 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-10 . USAF Sat Cat: 39564 . COSPAR: 1998-067EH. Apogee: 183 km (113 mi). Perigee: 177 km (109 mi). Inclination: 51.61 deg. Period: 88.09 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-27 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-05-03 . USAF Sat Cat: 39565 . COSPAR: 1998-067EJ. Apogee: 193 km (119 mi). Perigee: 174 km (108 mi). Inclination: 51.62 deg. Period: 88.17 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock1-28 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-06-03 . USAF Sat Cat: 39566 . COSPAR: 1998-067EK. Apogee: 152 km (94 mi). Perigee: 146 km (90 mi). Inclination: 51.61 deg. Period: 87.47 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- SkyCube 1 - .
Mass: 2.00 kg (4.40 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2014-07-28 . USAF Sat Cat: 39569 . COSPAR: 1998-067EN. Apogee: 325 km (201 mi). Perigee: 320 km (190 mi). Inclination: 51.64 deg. Period: 90.98 min. Cubesat from Southern Stars Group LLC, San Francisco, with an Earth imager..
2014 March 31 - .
02:58 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- SJ-11-06 - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SJ-11.
USAF Sat Cat: 39624 . COSPAR: 2014-014A. Apogee: 704 km (437 mi). Perigee: 688 km (427 mi). Inclination: 98.25 deg. Period: 98.68 min. Sixth satellite in China's Shi Jian 11 constellation, replacing SJ11-01 in that orbital slot. The SJ11 satellites were rumoured to carry infrared sensors of some kind..
2014 April 3 - .
21:02 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELS.
LV Family:
R-7.
Launch Vehicle:
Soyuz-ST-A.
- Sentinel-1A - .
Mass: 2,157 kg (4,755 lb). Nation: Europe.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Prima.
USAF Sat Cat: 39634 . COSPAR: 2014-016A. Apogee: 692 km (429 mi). Perigee: 690 km (420 mi). Inclination: 98.16 deg. Period: 98.58 min.
First satellite in the European Commission's Sentinel/Copernicus Earth observing program. Sentinel-1A's C-band SAR was 13.3 x 0.8m in size. The satellite was only a quarter the mass of its predecessor Envisat which carried a wider array of instruments; in the Sentinel program there will be a series of smaller, more specialized satellites. At 05:14 GMT on April 5, Sentinel made a maneuver to avoid a very close pass by NASA's defunct ACRIMSAT satellite, which failed on December 14 2013 after suffering battery issues.
2014 April 9 - .
19:06 GMT - .
Launch Site:
Palmachim.
Launch Pad: xxx.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-10 - .
Mass: 260 kg (570 lb). Nation: Israel.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Tecsar.
USAF Sat Cat: 39650 . COSPAR: 2014-019A. Apogee: 598 km (371 mi). Perigee: 388 km (241 mi). Inclination: 140.94 deg. Period: 94.48 min. Reportedly carried a radar imaging (SAR) payload..
2014 April 10 - .
17:45 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
Launch Pad: SLC41.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 541.
- USA 250 - .
Payload: NROL-67. Mass: 3,600 kg (7,900 lb). Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Mercury ELINT.
USAF Sat Cat: 39652 . COSPAR: 2014-020A. Apogee: 35,790 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.00 min. It appeared likely that the Centaur stage made three burns to deploy the USA 250 payload in geosynchronous orbit. The payload was suspected to be a large NRO signals intelligence satellite..
2014 April 16 - .
16:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Egyptsat-2 - .
Mass: 1,050 kg (2,310 lb). Nation: Egypt.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: USP (Victoria).
Spacecraft: Yamal.
USAF Sat Cat: 39678 . COSPAR: 2014-021A. Apogee: 710 km (440 mi). Perigee: 649 km (403 mi). Inclination: 51.62 deg. Period: 98.34 min. Bult by RKK Energia for Egypt's National Authority for Remote Sensing and Space Science using the 559GK bus; carried a 1-meter resolution imager..
2014 April 30 - .
01:38 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELV.
Launch Vehicle:
Vega.
- KazEOSat-1 - .
Mass: 830 kg (1,820 lb). Nation: Kazakhstan.
Manufacturer: Surrey.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Leostar-2.
USAF Sat Cat: 39731 . COSPAR: 2014-024A. Apogee: 753 km (467 mi). Perigee: 751 km (466 mi). Inclination: 98.52 deg. Period: 99.86 min. Kazakh high resolution imaging satellite; built by Airbus Defense and Space Toulouse, based on the Astrosat bus and had an imager with 1 metre resolution. The third launch of Europe's Vega light launch vehicle..
2014 May 6 - .
13:49 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1A.
- Cosmos 2495 - .
Payload: Kobalt-M. Mass: 6,700 kg (14,700 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Decay Date: 2014-09-03 . USAF Sat Cat: 39732 . COSPAR: 2014-025A. Apogee: 253 km (157 mi). Perigee: 203 km (126 mi). Inclination: 81.40 deg. Period: 89.06 min. Kobalt-M spy satellite, serial number 564. Ninth launch of an 11F695M Kobalt-M film-return satellite and the first to use the Soyuz-2-1A rocket instead of the older Soyuz-U. By May 17 the satellite was in a 207 x 248 km x 81.4 deg orbit..
2014 May 24 - .
03:05 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- Daichi-2 - .
Payload: ALOS 2. Mass: 2,120 kg (4,670 lb). Nation: Japan.
Class: Surveillance.
Type: Military Radarsat. Spacecraft Bus: Daichi.
Spacecraft: Daichi-2.
USAF Sat Cat: 39766 . COSPAR: 2014-029A. Apogee: 632 km (392 mi). Perigee: 630 km (390 mi). Inclination: 97.92 deg. Period: 97.33 min. Advanced Land Observing Satellite 2, placed in a noon/midnight sun-synchronous orbit. Carried the PALSAR-2 radar imager with 1 to 3 meter resolution in spotlight mode and 3 to 10 m in high resolution mode..
2014 August 9 - .
05:45 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 20b - .
Mass: 200 kg (440 lb). Nation: China.
Agency: CASC.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 40110 . COSPAR: 2014-047B. Apogee: 1,094 km (679 mi). Perigee: 1,087 km (675 mi). Inclination: 63.40 deg. Period: 107.05 min.
- Yaogan 20c - .
Mass: 200 kg (440 lb). Nation: China.
Agency: CASC.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 40111 . COSPAR: 2014-047C. Apogee: 1,094 km (679 mi). Perigee: 1,087 km (675 mi). Inclination: 63.40 deg. Period: 107.05 min.
- Yaogan 20a - .
Mass: 2,000 kg (4,400 lb). Nation: China.
Agency: CASC.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 40109 . COSPAR: 2014-047A. Apogee: 1,066 km (662 mi). Perigee: 1,054 km (654 mi). Inclination: 63.40 deg. Period: 106.41 min. Triplet satellites, the fourth in a series; previous triplet clusters were Yaogan 9, 16 and 17. They were thought to be analogous to the old US NOSS/PARCAE ocean surveillance system..
2014 September 5 - .
09:29 GMT - .
Launch Platform: ISS.
- Flock 1b-17 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
COSPAR: 1998-067FF. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-18 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
COSPAR: 1998-067FE. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2014 September 8 - .
03:22 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Yaogan 21 - .
Payload: Jianbing 8. Mass: 2,800 kg (6,100 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-10.
USAF Sat Cat: 40143 . COSPAR: 2014-053A. Apogee: 498 km (309 mi). Perigee: 480 km (290 mi). Inclination: 97.39 deg. Period: 94.39 min. Imaging satellite in a sun synchronous orbit with a 10:30 local time descending node. The mission continued a series begun with the Zi Yuan 2 satellites..
- Tiantuo 2 - .
Mass: 67 kg (147 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Tiantuo.
USAF Sat Cat: 40144 . COSPAR: 2014-053B. Apogee: 485 km (301 mi). Perigee: 469 km (291 mi). Inclination: 97.39 deg. Period: 94.15 min. Satellites built by the National University for Defense Technology; this one carried video imaging experiments..
2014 September 17 - .
00:10 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
Launch Pad: Cape Canaveral SLC41.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 257 - .
Payload: CLIO. Mass: 5,000 kg (11,000 lb). Nation: USA.
Class: Surveillance.
Type: ELINT. Spacecraft: AS 2100.
USAF Sat Cat: 40208 . COSPAR: 2014-055A.
Classified satellite in an unusual high-perigee geostationary transfer orbit, possibly around 11,800 x 36,000 km, after an initial 174 km x 28,860 km x 28 deg orbit. CLIO's owner was an unidentified US government agency - possibly the National Reconnaissance Office. It may have a communications or signals
intelligence payload.
2014 September 28 - .
05:13 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- SJ-11-07 - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SJ-11.
USAF Sat Cat: 40261 . COSPAR: 2014-059A. Apogee: 700 km (430 mi). Perigee: 684 km (425 mi). Inclination: 98.10 deg. Period: 98.61 min. Seventh satellite in the Shi Jian 11 constellation, thought perhaps to be used for infrared missile tracking and early warning..
2014 October 20 - .
06:31 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 22 - .
Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-9.
USAF Sat Cat: 40275 . COSPAR: 2014-063A. Apogee: 1,207 km (749 mi). Perigee: 1,198 km (744 mi). Inclination: 100.36 deg. Period: 109.48 min. Sun synchronous orbit; 1330 GMT local time of the descending node..
2014 October 27 - .
06:59 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- SJ-11-08 - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SJ-11.
USAF Sat Cat: 40286 . COSPAR: 2014-066A. Apogee: 700 km (430 mi). Perigee: 681 km (423 mi). Inclination: 98.25 deg. Period: 98.58 min. Eighth and final satellite in the Shi Jian 11 series, believed to be a military surveillance satellite of some kind. Sun synchronous orbit; 1315 GMT local time of the descending node..
2014 October 28 - .
22:20 GMT - .
Launch Site:
Wallops Island.
Launch Complex:
Wallops Island LA0A.
Launch Pad: Wallops MARS 0A.
LV Family:
Antares LV.
Launch Vehicle:
Antares 130.
- Flock-1d 1 to 26 - .
Mass: 4.00 kg (8.80 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
26 PlanetLabs Flock-1d 3U cubesats. Lost in explosion of booster. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2014 November 6 - .
07:35 GMT - .
Launch Site:
Dombarovskiy.
Launch Complex:
Dombarovskiy.
Launch Pad: Yasniy.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- ASNARO - .
Mass: 495 kg (1,091 lb). Nation: Japan.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: NEXTAR NX-300L.
USAF Sat Cat: 40298 . COSPAR: 2014-070A. Apogee: 509 km (316 mi). Perigee: 506 km (314 mi). Inclination: 97.45 deg. Period: 94.77 min.
High resolution imaging satellite developed by NEC and managed by Japan Space Systems (formerly USEF, part of the Ministry of Trade and Industry) rather than by the main Japanese space agency JAXA. The ASNARO had 0.5m resolution on a 10 km nadir swath width. Sun synchronous orbit; 1100 GMT local time of the descending node.
- Hodoyoshi-1 - .
Mass: 50 kg (110 lb). Nation: Japan.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Hodoyoshi.
USAF Sat Cat: 40299 . COSPAR: 2014-070B. Apogee: 513 km (318 mi). Perigee: 496 km (308 mi). Inclination: 97.45 deg. Period: 94.70 min. Satellite of the University of Tokyo and AXELSPACE, carried an imager with 6.8m resolution and 28 km swath. Sun synchronous orbit; 1100 GMT local time of the descending node..
- Kinshachi-1 - .
Payload: CHUBUSAT 1. Mass: 50 kg (110 lb). Nation: Japan.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: ChubuSat.
USAF Sat Cat: 40300 . COSPAR: 2014-070C. Apogee: 524 km (325 mi). Perigee: 496 km (308 mi). Inclination: 97.44 deg. Period: 94.82 min.
Also known as also known as ChubuSat-1, a project of Nagoya and Daido universities. (The name Kinschachi refers to the golden sea-monster statues on Nagoya castle). It carries d 10m resolution, 14 km swath imager, a 130 m resolution, 7-13 micron infrared camera reported to be for atmosphere temperature profiles and space debris monitoring, and an amateur radio relay payload. Sun synchronous orbit; 1055 GMT local time of the descending node.
- Tsukushi - .
Payload: QSAT-EOS. Mass: 49 kg (108 lb). Nation: Japan.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Tsukushi.
USAF Sat Cat: 40301 . COSPAR: 2014-070D. Apogee: 530 km (320 mi). Perigee: 489 km (303 mi). Inclination: 97.44 deg. Period: 94.81 min.
'Horsetail'; also called QSAT-EOS, Kyushu Satellite for Earth Observation System Demonstration. The satellite carried a CMOS camera with 4 m resolution and 7 km swath, a magnetometer and an in-situ space debris detector, as well as a deployable 3-meter kapton sail used as a drag augmentation device. Sun synchronous orbit; 1055 GMT local time of the descending node.
2014 November 14 - .
18:53 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- Yaogan 23 - .
Payload: Jianbing 7. Mass: 1,200 kg (2,600 lb). Nation: China.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft Bus: Jianbing.
Spacecraft: JB-7.
USAF Sat Cat: 40305 . COSPAR: 2014-071A. Apogee: 513 km (318 mi). Perigee: 511 km (317 mi). Inclination: 97.37 deg. Period: 94.87 min. Sun synchronous orbit; 0200 GMT local time of the descending node..
2014 November 20 - .
07:12 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Yaogan 24 - .
Payload: Jianbing 6. Mass: 1,300 kg (2,800 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-6.
USAF Sat Cat: 40310 . COSPAR: 2014-072A. Apogee: 652 km (405 mi). Perigee: 627 km (389 mi). Inclination: 97.95 deg. Period: 97.51 min. Imaging spy satellite in the same series as Yaogan 2, 4, 7, and 11. The CZ-2D second stage was deorbited after deploying the satellite. Sun synchronous orbit; 1330 GMT local time of the descending node..
2014 November 21 - .
06:37 GMT - .
Launch Site:
Jiuquan.
LV Family:
DF-21.
Launch Vehicle:
Kuaizhou.
- Kuaizhou-2 - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Kuaizhou satellite.
Decay Date: 2016-10-09 . USAF Sat Cat: 40311 . COSPAR: 2014-073A. Apogee: 318 km (197 mi). Perigee: 283 km (175 mi). Inclination: 96.50 deg. Period: 90.53 min.
Second launch of the Chinese 2nd Artillery's operationally responsive Kuaizhou (Swift Boat) launch vehicle with a military payload. Kuaizhou 1 was launched to a similar sun synchronous orbit with 11:00 local time of the descending node in September 2013; after regular maintenance burns for a year, during October 2014 Kuaizhou 1's orbit was raised to 365 x 390 km. Kuaizhou-2 was in a sun synchronous orbit; 1300 GMT local time of the descending node.
2014 December 7 - .
03:26 GMT - .
Launch Site:
Taiyuan LC9.
Launch Complex:
Taiyuan LC9.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- CBERS-4 - .
Mass: 2,100 kg (4,600 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Phoenix Eye.
USAF Sat Cat: 40336 . COSPAR: 2014-079A. Apogee: 774 km (480 mi). Perigee: 773 km (480 mi). Inclination: 98.51 deg. Period: 100.32 min. China-Brazil Earth Resources Satellite 4. The uprated ZY-1 class satellite replaced CBERS 3 which was lost in a launch failure a year earlier. Sun synchronous orbit; 1030 GMT local time of the descending node..
2014 December 10 - .
19:33 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 25a - .
Mass: 2,000 kg (4,400 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 40338 . COSPAR: 2014-080A. Apogee: 1,106 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.41 deg. Period: 107.05 min. Fifth Yaogan mission. Each consisted of a main satellite and two subsatellites..
- Yaogan 25b - .
Mass: 200 kg (440 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 40339 . COSPAR: 2014-080B. Apogee: 1,106 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.41 deg. Period: 107.05 min.
- Yaogan 25c - .
Mass: 200 kg (440 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 40340 . COSPAR: 2014-080C. Apogee: 1,106 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.41 deg. Period: 107.05 min.
2014 December 13 - .
03:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 541.
2014 December 19 - .
04:43 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: Baikonur LC175.
LV Family:
UR-100N.
Launch Vehicle:
Strela launch vehicle.
- Kondor-E No. 2 - .
Mass: 1,100 kg (2,400 lb). Nation: South Africa.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: Kondor.
USAF Sat Cat: 40353 . COSPAR: 2014-084A. Apogee: 484 km (300 mi). Perigee: 481 km (298 mi). Inclination: 74.75 deg. Period: 94.26 min. Second Kondor radar imaging satellite built by NPO Mashinostroenie (Moscow/Reutov)This satellite was the export version of the spacecraft and was reportedly sold to the Defense Intelligence organization of the South African National Defense Force..
2014 December 25 - .
03:01 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Cosmos 2502 - .
Payload: Lotos-S No. 802. Mass: 6,000 kg (13,200 lb). Nation: Russia.
Class: Surveillance.
Type: SIGINT. Spacecraft: Lotos-S.
USAF Sat Cat: 40358 . COSPAR: 2014-086A. Apogee: 910 km (560 mi). Perigee: 901 km (559 mi). Inclination: 67.15 deg. Period: 103.10 min.
Russian military satellite that initially entered a 240 km x 899 km x 67.1 deg orbit. Russian press reports and official announcements did not give any name for the satellite, not even a Cosmos cover name, the first time this had happened since 1963. Believed to be the second Lotos-S signals intelligence satellite. The Lotos-S satellites had a payload similar to the Tselina-2, but used a Russian Yantar-type spacecraft bus from TsSKB-Progress instead of the Tselina-2's Okean class bus from the Ukranian Yuzhnoye organization. The spacecraft circularized its orbit to 899 km x 909 km on December 26, joining Lotos-S No. 801 which was in a 903 km x 907 km x 67 deg orbit.
2014 December 26 - .
18:55 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
Launch Pad: Baikonur LC31/6.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Resurs-P No. 2 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Resurs-Spektr.
USAF Sat Cat: 40360 . COSPAR: 2014-087A. Apogee: 475 km (295 mi). Perigee: 463 km (287 mi). Inclination: 97.29 deg. Period: 93.98 min.
Resurs-P 47KS No. 2 civil imaging spacecraft. The main payload was the Geoton-L1 imager with 0.5m aperture and 38 km swath, 1.0 m panchromatic and 3 to 4m color resolution. Geoton-L1 had 7 passbands and a 216-channel hyperspectral imager. The KShMSA wide field multispectral camera was also part of the Resurs-P primary payload; an AIS ship tracking receiver from OAO RKS and Lomonosov Federal State Univ.'s Nuklon cosmic ray detector were secondary payloads. Nuklon detected cosmic ray nuclei with atomic number 1 to 30 in the 1 to 1000 TeV energy range. Resurs-P went into a 190 km x 428 km initial orbit that was raised to its operational height of 330 km x 471 km on December 29. Sun synchronous orbit; 1150 GMT local time of the descending node.
2014 December 27 - .
03:22 GMT - .
Launch Site:
Taiyuan LC9.
Launch Complex:
Taiyuan LC9.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Yaogan 26 - .
Payload: Jianbing 8. Mass: 2,800 kg (6,100 lb). Nation: China.
Class: Surveillance.
Type: Naval SIGINT. Spacecraft Bus: Jianbing.
Spacecraft: JB-8.
USAF Sat Cat: 40362 . COSPAR: 2014-088A. Apogee: 489 km (303 mi). Perigee: 484 km (300 mi). Inclination: 97.41 deg. Period: 94.34 min. The profile was similar to the Yaogan 5 series of imaging satellites, but the rocket used a larger nose fairing, so this was likely an upgrade. Sun synchronous orbit; 1030 GMT local time of the descending node..
2015 February 1 - .
01:21 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS Radar Spare - .
Mass: 1,000 kg (2,200 lb). Nation: Japan.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: IGS.
USAF Sat Cat: 40381 . COSPAR: 2015-004A. Apogee: 511 km (317 mi). Perigee: 490 km (300 mi). Inclination: 97.50 deg. The Radar Spare satellite (Reda Yobiki) in the Information Gathering Satellite (Joho Shushu Eisei) series were operated by Japan's Cabinet Satellite Intelligence Center..
2015 February 2 - .
08:50 GMT - .
Launch Site:
Semnan.
Launch Complex:
Semnan.
LV Family:
Nodong 1.
Launch Vehicle:
Safir.
- Fajr - .
Mass: 52 kg (114 lb). Nation: Iran.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Fajr.
Decay Date: 2015-02-26 . USAF Sat Cat: 40387 . COSPAR: 2015-006A. Apogee: 469 km (291 mi). Perigee: 224 km (139 mi). Inclination: 55.50 deg.
Fourth Iranian satellite, and Iran's first successful orbital launch since February 2012. Fajr (Aurora) had a technology payload with a cold-gas thruster developed by Iran Electronics Industries. There is suggestive evidence (mostly based on satellite imagery of launch pad
damage revealed by the magazine Jane's Intelligence Review) that Iran had two launch failures in 2012, as well as more speculative evidence of further launch failures since then. The satellite did not seem to make any orbital maneuvers. The orbit decayed from an initial 223 km x 470 km to 196 km x 293 km by February 22, and then after falling to 134 km x 155 km early on February 26 it reentered. The Safir rocket stage orbit decayed a bit more slowly, and was at 203 km x 325 km on Feb 26.
2015 February 27 - .
11:01 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1A.
- Cosmos 2503 - .
Payload: COSMOS 2503. Mass: 4,000 kg (8,800 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Bars.
USAF Sat Cat: 40420 . COSPAR: 2015-009A. Apogee: 577 km (358 mi). Perigee: 566 km (351 mi). Inclination: 97.67 deg. Period: 96.09 min. Believed to be a new-generation electro-optical reconnaisance satellite based on a heavily modified Yantar bus. Sun synchronous orbit; 0245 GMT local time of the descending node..
2015 February 27 - .
14:30 GMT - .
Launch Platform: ISS.
- Flock 1b-27 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-10-14 . USAF Sat Cat: 40422 . COSPAR: 1998-067FN. Apogee: 404 km (251 mi). Perigee: 396 km (246 mi). Inclination: 51.70 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-28 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-08-07 . USAF Sat Cat: 40423 . COSPAR: 1998-067FP. Apogee: 404 km (251 mi). Perigee: 396 km (246 mi). Inclination: 51.70 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-21 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-10-12 . USAF Sat Cat: 40427 . COSPAR: 1998-067FQ. Apogee: 402 km (249 mi). Perigee: 395 km (245 mi). Inclination: 51.70 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-22 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-10-03 . USAF Sat Cat: 40428 . COSPAR: 1998-067FR. Apogee: 402 km (249 mi). Perigee: 395 km (245 mi). Inclination: 51.70 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-9 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-08-23 . USAF Sat Cat: 40429 . COSPAR: 1998-067FS. Apogee: 407 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-10 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-06-28 . USAF Sat Cat: 40430 . COSPAR: 1998-067FT. Apogee: 413 km (256 mi). Perigee: 398 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1d'-1 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-10-13 . USAF Sat Cat: 40451 . COSPAR: 1998-067FU. Apogee: 405 km (251 mi). Perigee: 393 km (244 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1d'-2 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-12-27 . USAF Sat Cat: 40452 . COSPAR: 1998-067FV. Apogee: 313 km (194 mi). Perigee: 301 km (187 mi). Inclination: 51.63 deg. Period: 90.67 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-5 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-08-17 . USAF Sat Cat: 40453 . COSPAR: 1998-067FW. Apogee: 407 km (252 mi). Perigee: 394 km (244 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-6 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-10-16 . USAF Sat Cat: 40454 . COSPAR: 1998-067FX. Apogee: 407 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-11 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-09-07 . USAF Sat Cat: 40459 . COSPAR: 1998-067GC. Apogee: 405 km (251 mi). Perigee: 395 km (245 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1b-12 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2015-09-29 . USAF Sat Cat: 40460 . COSPAR: 1998-067GD. Apogee: 405 km (251 mi). Perigee: 395 km (245 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2015 March 25 - .
22:08 GMT - .
Launch Site:
Dombarovskiy.
Launch Complex:
Yasniy Sh370/13.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Arirang-3A - .
Payload: KOMPSAT 3A. Mass: 800 kg (1,760 lb). Nation: Korea South.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: T200.
Spacecraft: Kompsat.
USAF Sat Cat: 40536 . COSPAR: 2015-014A. Apogee: 538 km (334 mi). Perigee: 522 km (324 mi). Inclination: 97.53 deg. Period: 95.23 min. South Korean imaging satellite with submeter resolution. Sun synchronous orbit; 0130 GMT local time of the descending node..
2015 March 26 - .
01:21 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS Optical 5 - .
Mass: 1,000 kg (2,200 lb). Nation: Japan.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: IGS.
USAF Sat Cat: 40538 . COSPAR: 2015-015A. Apogee: 515 km (320 mi). Perigee: 511 km (317 mi). Inclination: 97.50 deg. Information Gathering Satellite Optical-5. Military optical surveillance satellite operated by the Japanese government. Sun synchronous orbit; 1015 GMT local time of the descending node..
2015 May 20 - .
15:05 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
Launch Pad: Cape Canaveral SLC40.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 501.
- O/C-1 - .
Payload: OPTICUBE 01. Mass: 3.00 kg (6.60 lb). Nation: USA.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Cubesat.
USAF Sat Cat: 40653 . COSPAR: 2015-025C. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.00 deg. 3U Optical Cubesat sponsored by NRO and built by Cal Poly as targets for space surveillance calibration..
- O/C-2 - .
Payload: OPTICUBE 02. Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Cubesat.
USAF Sat Cat: 40656 . COSPAR: 2015-025F. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.00 deg. 3U Optical Cubesat sponsored by NRO and built by Cal Poly as targets for space surveillance calibration..
- O/C-3 - .
Payload: OPTICUBE 03. Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Cubesat.
USAF Sat Cat: 40658 . COSPAR: 2015-025H. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.00 deg. 3U Optical Cubesat sponsored by NRO and built by Cal Poly as targets for space surveillance calibration..
2015 June 5 - .
15:23 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1A.
- Cosmos 2505 - .
Mass: 6,700 kg (14,700 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-4K1.
Decay Date: 2015-09-18 . USAF Sat Cat: 40667 . COSPAR: 2015-027A. Apogee: 285 km (177 mi). Perigee: 177 km (109 mi). Inclination: 81.40 deg.
Kobal't-M spy satellite s/n 565, maneuvered on 8 and 13 June from an initial orbit of 177 km x 285 km x 81.4 deg to 203 km x 264 km. Current version of the Yantar satellite which returns its main section, with film and camera, to Earth at the end of its flight. It also carried two small ejectable film canisters which can return some data to Earth during the mission.
2015 June 23 - .
01:51 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ZLV.
Launch Vehicle:
Vega.
2015 June 23 - .
16:44 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Cosmos 2506 - .
Mass: 7,000 kg (15,400 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Persona.
USAF Sat Cat: 40699 . COSPAR: 2015-029A. Apogee: 725 km (450 mi). Perigee: 706 km (438 mi). Inclination: 98.29 deg. Period: 99.09 min.
Third Persona-1 spy satellite, built by TsSKB-Progress in Samara and equipped with electro-optical imaging cameras. Said to be the first to return its data via an optical communications link to an unidentified geosynchronous satellite. On June 28 the satellite manuevered from an elliptical transfer orbit to a circular sun synchronous orbit with 0840 GMT local time of the descending node.
2015 June 26 - .
06:22 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Gaofen 8 - .
Mass: 800 kg (1,760 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CAST2000.
USAF Sat Cat: 40701 . COSPAR: 2015-030A. Apogee: 490 km (300 mi). Perigee: 482 km (299 mi). Inclination: 97.32 deg. Period: 94.33 min.
High resolution imaging satellite. The previous two Gaofen satellites, 1 and 2, were civilian operated and extensively described before launch. GF-8 was said to be civilian as well, but was not discussed prior to the launch, indicating it was used for military imaging. Sun synchronous orbit; 1330 GMT local time of the descending node.
2015 July 10 - .
16:28 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
Launch Pad: Sriharikota FLP.
LV Family:
PSLV.
Launch Vehicle:
PSLV-XL.
- DMC3-1 - .
Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 40715 . COSPAR: 2015-032A. Apogee: 660 km (410 mi). Perigee: 638 km (396 mi). Inclination: 98.04 deg. Period: 97.71 min.
Third generation Disaster Monitoring Constellation. The three satellites were deployed on a single launch. DMC Imaging International was a
Surrey Satellite spinoff which operated the DMC imaging
satellites in collaboration with several developing countries. The
satellites have the capability to return prompt imaging of areas in
those countries affected by natural disasters. The SSTL-300S1 platform provided 45 degree fast slew off-pointing and was capable of acquiring multiple targets in one pass using multiple viewing modes. The high resolution imager on board the satellites was designed and manufactured by SSTL and provided 1 meter resolution in panchromatic mode, and 4 meter resolution in multispectral mode, with a swath width of 23.4km.
The three satellites were phased 120 degrees apart around the same sun synchronous orbit with a 22:10 local time longitude of descending node sun synchronous orbit. This was acommplished using their on board propulsion systems in the three months after the launch. With off-pointing capability, the DMC3/TripleSat Satellite Constellation was able to target anywhere on Earth once per day.
- DMC3-2 - .
Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 40716 . COSPAR: 2015-032B. Apogee: 659 km (409 mi). Perigee: 640 km (390 mi). Inclination: 98.03 deg. Period: 97.71 min. 22:10 local time longitude of descending node sun synchronous orbit..
- DMC3-3 - .
Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 40717 . COSPAR: 2015-032C. Apogee: 662 km (411 mi). Perigee: 637 km (395 mi). Inclination: 98.10 deg. Period: 97.71 min. 22:10 local time longitude of descending node sun synchronous orbit..
- CBNT-1 - .
Mass: 91 kg (200 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CBNT.
USAF Sat Cat: 40718 . COSPAR: 2015-032D. Apogee: 659 km (409 mi). Perigee: 636 km (395 mi). Inclination: 98.03 deg. Period: 97.67 min. Surrey Satellite Technology experimental imaging satellite. SSTL did not disclose the meaning of the CBNT abbreviation. 22:10 local time longitude of descending node sun synchronous orbit..
2015 July 13 - .
16:40 GMT - .
Launch Platform: ISS.
- Flock 1e-1 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-03-05 . USAF Sat Cat: 40722 . COSPAR: 1998-067GE. Apogee: 370 km (220 mi). Perigee: 361 km (224 mi). Inclination: 51.64 deg. Period: 91.86 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-2 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-05-18 . USAF Sat Cat: 40723 . COSPAR: 1998-067GF. Apogee: 381 km (236 mi). Perigee: 373 km (231 mi). Inclination: 51.64 deg. Period: 92.08 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-4 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-06-24 . USAF Sat Cat: 40724 . COSPAR: 1998-067GG. Apogee: 379 km (235 mi). Perigee: 375 km (233 mi). Inclination: 51.64 deg. Period: 92.09 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-3 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-05-29 . USAF Sat Cat: 40725 . COSPAR: 1998-067GH. Apogee: 374 km (232 mi). Perigee: 368 km (228 mi). Inclination: 51.64 deg. Period: 91.97 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-5 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-06-20 . USAF Sat Cat: 40728 . COSPAR: 1998-067GL. Apogee: 381 km (236 mi). Perigee: 373 km (231 mi). Inclination: 51.64 deg. Period: 92.09 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-6 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-07-21 . USAF Sat Cat: 40729 . COSPAR: 1998-067GM. Apogee: 380 km (230 mi). Perigee: 372 km (231 mi). Inclination: 51.64 deg. Period: 92.07 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-7 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-07-17 . USAF Sat Cat: 40726 . COSPAR: 1998-067GJ. Apogee: 381 km (236 mi). Perigee: 375 km (233 mi). Inclination: 51.64 deg. Period: 92.11 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-8 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-06-22 . USAF Sat Cat: 40727 . COSPAR: 1998-067GK. Apogee: 379 km (235 mi). Perigee: 371 km (230 mi). Inclination: 51.64 deg. Period: 92.05 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-9 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-02-08 . USAF Sat Cat: 40736 . COSPAR: 1998-067GN. Apogee: 381 km (236 mi). Perigee: 377 km (234 mi). Inclination: 51.64 deg. Period: 92.13 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-10 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-08-09 . USAF Sat Cat: 40737 . COSPAR: 1998-067GP. Apogee: 381 km (236 mi). Perigee: 375 km (233 mi). Inclination: 51.64 deg. Period: 92.11 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-11 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-08-09 . USAF Sat Cat: 40738 . COSPAR: 1998-067GQ. Apogee: 377 km (234 mi). Perigee: 371 km (230 mi). Inclination: 51.64 deg. Period: 92.02 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-12 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-08-09 . USAF Sat Cat: 40739 . COSPAR: 1998-067GR. Apogee: 382 km (237 mi). Perigee: 374 km (232 mi). Inclination: 51.64 deg. Period: 92.12 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-13 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-08-24 . USAF Sat Cat: 40740 . COSPAR: 1998-067GS. Apogee: 380 km (230 mi). Perigee: 374 km (232 mi). Inclination: 51.64 deg. Period: 92.09 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 1e-14 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-07-31 . USAF Sat Cat: 40741 . COSPAR: 1998-067GT. Apogee: 380 km (230 mi). Perigee: 374 km (232 mi). Inclination: 51.64 deg. Period: 92.08 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Centennial-1 - .
Mass: 1.00 kg (2.20 lb). Nation: USA.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Cubesat.
Decay Date: 2015-12-23 . USAF Sat Cat: 40742 . COSPAR: 1998-067GU. Apogee: 337 km (209 mi). Perigee: 328 km (203 mi). Inclination: 51.64 deg. Period: 91.18 min. 1U cubesat by Booz Allen, used as a space surveillance target by the USAF..
2015 August 27 - .
02:31 GMT - .
Launch Site:
Taiyuan.
Launch Complex:
Taiyuan LC9.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Yaogan 27 - .
Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-9.
USAF Sat Cat: 40878 . COSPAR: 2015-040A. Apogee: 1,207 km (749 mi). Perigee: 1,193 km (741 mi). Inclination: 100.48 deg. Period: 109.43 min. The 27th Yaogan remote sensing satellite. Fifth in the Yaogan High A series and appeared to replace the first, Yaogan 8, in a sun synchronous orbit with a 09:30 local time longitude of descending node..
2015 September 14 - .
04:42 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
Launch Pad: Jiuquan LC603.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Gaofen 9 - .
Mass: 800 kg (1,760 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CAST2000.
USAF Sat Cat: 40894 . COSPAR: 2015-047A. Apogee: 666 km (413 mi). Perigee: 617 km (383 mi). Inclination: 98.01 deg. Period: 97.55 min. High resolution imaging satellite. GF-9 have replaced GF-1, launched in 2013 to a similar sun synchronous orbit (11:00 local time longitude of descending node)..
2015 October 6 - .
01:15 GMT - .
Launch Platform: ISS.
- Flock 2b-1 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-09-22 . USAF Sat Cat: 40950 . COSPAR: 1998-067HB. Apogee: 391 km (242 mi). Perigee: 387 km (240 mi). Inclination: 51.64 deg. Period: 92.34 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-2 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-10-02 . USAF Sat Cat: 40951 . COSPAR: 1998-067HC. Apogee: 391 km (242 mi). Perigee: 387 km (240 mi). Inclination: 51.64 deg. Period: 92.33 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-3 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-10-14 . USAF Sat Cat: 40952 . COSPAR: 1998-067HD. Apogee: 391 km (242 mi). Perigee: 389 km (241 mi). Inclination: 51.64 deg. Period: 92.35 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-4 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-10-17 . USAF Sat Cat: 40953 . COSPAR: 1998-067HE. Apogee: 392 km (243 mi). Perigee: 389 km (241 mi). Inclination: 51.64 deg. Period: 92.36 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-5 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-09-25 . USAF Sat Cat: 40954 . COSPAR: 1998-067HF. Apogee: 394 km (244 mi). Perigee: 385 km (239 mi). Inclination: 51.64 deg. Period: 92.34 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-6 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-08-22 . USAF Sat Cat: 40955 . COSPAR: 1998-067HG. Apogee: 397 km (246 mi). Perigee: 389 km (241 mi). Inclination: 51.64 deg. Period: 92.41 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-7 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-09-21 . USAF Sat Cat: 40956 . COSPAR: 1998-067HH. Apogee: 392 km (243 mi). Perigee: 384 km (238 mi). Inclination: 51.64 deg. Period: 92.32 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-8 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-05-22 . USAF Sat Cat: 40957 . COSPAR: 1998-067HJ. Apogee: 387 km (240 mi). Perigee: 382 km (237 mi). Inclination: 51.64 deg. Period: 92.24 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-9 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-10-12 . USAF Sat Cat: 40962 . COSPAR: 1998-067HK. Apogee: 394 km (244 mi). Perigee: 385 km (239 mi). Inclination: 51.64 deg. Period: 92.34 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-10 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-10-16 . USAF Sat Cat: 40963 . COSPAR: 1998-067HL. Apogee: 394 km (244 mi). Perigee: 386 km (239 mi). Inclination: 51.64 deg. Period: 92.36 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2015 October 7 - .
04:13 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Jilin-1 Optical A - .
Payload: LQSAT. Mass: 420 kg (920 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Jilin.
USAF Sat Cat: 40958 . COSPAR: 2015-057A. Apogee: 666 km (413 mi). Perigee: 639 km (397 mi). Inclination: 98.04 deg. Period: 97.78 min.
Satellite cluster deployed in a single launch, described as China's first commercial imaging satellite system, built by the Chang Guang Satellite
Technology Company, a spinoff of the Changchun Institute of Optics, Fine Mechanics and Physics (CIOMP) in Jilin province. The 420-kg main satellite had an 0.7 m resolution imager. Two 92-kg 'smart video imaging satellites' and a single 50-kg 'smart imaging verification satellite' completed the cluster.
- Jilin-1 Video 1 - .
Payload: LINGQIAO VIDEO A. Mass: 95 kg (209 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Jilin.
USAF Sat Cat: 40959 . COSPAR: 2015-057B. Apogee: 665 km (413 mi). Perigee: 638 km (396 mi). Inclination: 98.04 deg. Period: 97.77 min. One of two 'smart video imaging' satellites in the Jilin cluster..
- Jilin-1 Video 2 - .
Payload: LINGQIAO VIDEO B. Mass: 95 kg (209 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Jilin.
USAF Sat Cat: 40960 . COSPAR: 2015-057C. Apogee: 665 km (413 mi). Perigee: 638 km (396 mi). Inclination: 98.04 deg. Period: 97.76 min. One of two 'smart video imaging' satellites in the Jilin cluster..
- Jilin-1 Tech Demo - .
Mass: 50 kg (110 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Jilin.
USAF Sat Cat: 40961 . COSPAR: 2015-057D. Apogee: 665 km (413 mi). Perigee: 637 km (395 mi). Inclination: 98.04 deg. Period: 97.75 min. 'Smart imaging verification satellite', part of the Jilin cluster..
2015 October 7 - .
12:25 GMT - .
Launch Platform: ISS.
- Flock 2b-13 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-10-11 . USAF Sat Cat: 40979 . COSPAR: 1998-067HM. Apogee: 394 km (244 mi). Perigee: 385 km (239 mi). Inclination: 51.64 deg. Period: 92.35 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2b-14 - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2016-09-12 . USAF Sat Cat: 40980 . COSPAR: 1998-067HN. Apogee: 391 km (242 mi). Perigee: 384 km (238 mi). Inclination: 51.64 deg. Period: 92.31 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2015 October 8 - .
12:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 264 - .
Payload: Intruder 11 / NROL-55. Mass: 6,500 kg (14,300 lb). Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 40964 . COSPAR: 2015-058A. Apogee: 1,201 km (746 mi). Perigee: 1,014 km (630 mi). Inclination: 63.40 deg.
The Atlas deployed two NRO satellites and a cluster of cubesats in orbit. Items listed as USA 264 and USA 264 'debris', thought to be a clandestine active payload, were deployed in a 1014 km x 1201 km x 63.4 deg orbit. The satellites were believed to be NRO/Navy signals intelligence satellites, the latest successors to the GRAB/POPPY series, and probably codenamed INTRUDER. Following deployment of the main payloads, the Centaur upper stage made two further burns to a 496 km x 800 km x 64.8 deg orbit and deployed the cubesats from GRACE, the fourth NPS Cubesat Launcher flown on an Atlas Aft Bulkhead Carrier.
- USA 264 Payload 2 - .
Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 40981 . COSPAR: 2015-058R. Apogee: 1,201 km (746 mi). Perigee: 1,014 km (630 mi). Inclination: 63.40 deg. Believed to be subsatellite of USA 246 sigint satellite..
2015 October 26 - .
07:10 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Tianhui 1-03 - .
Mass: 2,000 kg (4,400 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Tianhui.
USAF Sat Cat: 40988 . COSPAR: 2015-061A. Apogee: 501 km (311 mi). Perigee: 490 km (300 mi). Inclination: 97.36 deg. Period: 94.52 min. Third Tianhui-1 cartography satellite, launched into the same local-time orbital plane as the prior two, with a 03:30 local time longitude of descending node sun synchronous orbit..
2015 November 4 - .
03:45 GMT - .
Launch Site:
Barking Sands.
LV Family:
Strypi.
Launch Vehicle:
Super Strypi.
FAILURE: Went out of
control during first stage burn and was destroyed.
- STACEM - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Cubesat; lost when first stage failed..
2015 November 8 - .
07:06 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Yaogan 28 - .
Payload: Jianbing 11. Mass: 2,800 kg (6,100 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Jianbing.
Spacecraft: JB-11.
USAF Sat Cat: 41026 . COSPAR: 2015-064A. Apogee: 483 km (300 mi). Perigee: 459 km (285 mi). Inclination: 97.25 deg. Period: 94.03 min. Thought to be the second Jianbing-11 imaging reconnaissance satellite with an 0.8 m resolution imager. Appeared to be a replacement for the first Jianbing-11, codenamed Yaogan 14. 04:14 local time longitude of descending node sun synchronous orbit..
2015 November 17 - .
06:34 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Cosmos 2510 - .
Nation: Russia.
Class: Surveillance.
Type: Early warning satellite. Spacecraft Bus: USP (Victoria).
Spacecraft: Tundra.
USAF Sat Cat: 41032 . COSPAR: 2015-066A. Apogee: 38,551 km (23,954 mi). Perigee: 1,625 km (1,009 mi). Inclination: 63.80 deg. The first EKS early warning satellite, launched into a Molniya orbit. The satellite, developed by Energiya and Kometa, replaced the defunct Lavochkin/Kometa 'Oko' system..
2015 November 26 - .
21:24 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
2015 December 5 - .
14:09 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC43/4.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1V.
- Cosmos 2511 - .
Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Kanopus.
Decay Date: 2015-12-08 . USAF Sat Cat: 41098 . COSPAR: 2015-071A. Apogee: 694 km (431 mi). Perigee: 685 km (425 mi). Inclination: 98.20 deg.
Russia carried out the second launch of the Soyuz-2-1V rocket, carrying the 440 kg Kanopus-ST military satellite as its primary payload. Kanopus-ST carried optical, infrared and microwave imagers to test technology to locate submerged submarines. The two-stage core of Soyuz-2-1V reached a 208 x 681 km x 98.2 deg transfer orbit. The Volga upper stage coasted to apogee and at about 1503 UTC made a circularization burn to reach a 684 x 693 km sun-synchronous orbit. The KYuA-1 satellite was successfully ejected at about 1540 UTC, but one of several latches on the Kanopus-ST failed to open, and the payload failed to separate.The two payloads were given the public cover names Kosmos-2511 (Kanopus-ST/Volga) and Kosmos-2512 (KYuA-1). Following the failure, at about 0200 UTC Dec 6 the Volga reignited in an attempt to deorbit the Kanopus/Volga stack and prevent it becoming long-lived space debris. This burn reached an orbit of 106 x 655 km. Natural orbital decay from atmospheric drag quickly set in. On Dec 7, with the orbit at 90 x 348 km, the spacecraft split into two pieces, possibly but not certainly the Kanopus satelite and the Volga stage. The two pieces reached an orbit of 88 x 297 km on Dec 8 before reentry.
- Cosmos 2512 - .
Payload: KYuA-1. Nation: Russia.
Class: Surveillance.
Type: Radar calibration target. USAF Sat Cat: 41099 . COSPAR: 2015-071B. Apogee: 693 km (430 mi). Perigee: 684 km (425 mi). Inclination: 98.20 deg. Secondary payload; KYuA-1, a 16 kg sphere used to calibrate anti-ballistic-missile radars. Placed in sun synchronous orbit with 06:00 Equator crossing time..
2015 December 16 - .
12:30 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
LV Family:
PSLV.
Launch Vehicle:
PSLV CA.
- TeLEOS-1 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. COSPAR: 2015-077A. For AgilSpace, the 400 kg TeLEOS-1 satellite with a 1 meter resolution Earth imager. The satellite was built by Singapore Technologies Electronics, of which AgilSpace was a subsidiary..
- Kent Ridge 1 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. COSPAR: 2015-077C.
For the National University of Singapore, the 78 kg Kent Ridge 1 satellite developed using the TUBSAT LEOS-50 bus by Berlin Space Technologies, a spinoff of the old TUBSAT group at Technische Universitat Berlin. KR-1 carried two low-resoluton hyperspectral Earth imagers and a 6-meter-resolution imager.
- Athenoxat-1 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
COSPAR: 2015-077F. In a technology development test, the PSLV 4th stage was reignited briefly to test its ability to deliver payloads to multiple orbits. For Microsat Rapid Pte Ltd., the 3U cubesat Athenoxat-1 carried a payload to image the night side of the Earth..
2015 December 28 - .
16:04 GMT - .
Launch Site:
Xichang.
Launch Complex:
Xichang LC2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 3B.
- GaoFen 4 - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41194 . COSPAR: 2015-083A. Apogee: 35,806 km (22,248 mi). Perigee: 205 km (127 mi). Inclination: 23.00 deg. High resolution imaging satellite launched into geotransfer orbit. GF-4 has a 50-metre-resolution imager..
2016 February 7 - .
00:30 GMT - .
Launch Site:
Sohae.
LV Family:
Unha.
Launch Vehicle:
Unha-3.
- Kwangmyongsong-4 - .
Nation: Korea North.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Kwangmyongsong.
USAF Sat Cat: 41332 . COSPAR: 2016-009A. Apogee: 501 km (311 mi). Perigee: 465 km (288 mi). Inclination: 97.50 deg.
North Korea's National Aerospace Development Administration (NADA, Kukga uju gaebalkuk) carried out its second successful satellite launch . The satellite, Kwangmyongsong-4, entered a 500 km
polar orbit like the KMS-3-2 satellite launched in 2012. It appears both satellite and launch vehicle are very similar to the 2012 mission. The launch vehicle this time carried the name 'Kwangmyongsong' but appeared to be essentially identical to the Unha-3 launched in 2012. As of Feb 17, hobbyist
observers had not picked up any radio signals from it. 0840LT SSO.
2016 February 10 - .
11:40 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(5,2).
- USA 267 - .
Payload: TOPAZ 4?. Nation: USA.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Topaz.
USAF Sat Cat: 41334 . COSPAR: 2016-010A. Apogee: 1,085 km (674 mi). Perigee: 1,078 km (669 mi). Inclination: 123.00 deg. Satellite for the US National Reconnaissance Office. The launch was designated NRO L-45. The USA 267 payload was observed in a 1078 x 1085 km orbit with a retrograde 123 degree inclination, characteristic of the TOPAZ radar imaging satellites..
2016 February 16 - .
17:57 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
UR-100N.
Launch Vehicle:
Rokot.
- Sentinel-3A - .
Mass: 1,200 kg (2,600 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Prima.
USAF Sat Cat: 41335 . COSPAR: 2016-011A. Apogee: 806 km (500 mi). Perigee: 802 km (498 mi). Inclination: 98.60 deg.
Eurockot/Krunichev Rokot's Briz-KM upper stage entered a 153 x 785 km transfer orbit followed by an 802 x 806 km target orbit, deploying the Sentinel-3A satellite. It then lowered perigee to 411 x 744 km to reduce orbital lifetime. ESA's Sentinel-3A was part of the European Union's Copernicus remote
sensing program, and carried an ocean color imaging payload and an ocean-topography radar altimeter payload.
2016 February 17 - .
08:45 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- Kinshachi-2 - .
Nation: Japan.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: ChubuSat.
USAF Sat Cat: 41338 . COSPAR: 2016-012B. Apogee: 579 km (359 mi). Perigee: 559 km (347 mi). Inclination: 31.00 deg.
2016 March 13 - .
18:56 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1B.
- Resurs-P No. 3 - .
Mass: 6,600 kg (14,500 lb). Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Resurs-Spektr.
USAF Sat Cat: 41386 . COSPAR: 2016-016A. Apogee: 452 km (280 mi). Perigee: 279 km (173 mi). Inclination: 97.30 deg. Third Resurs-P civil remote sensing satellite. The first two satellites in the series were still operating; Resurs-P No. 1 made an orbit adjust burn on Feb 22. The Resurs-P No. 3 spacecraft, however, failed to deploy one of its solar panels..
2016 March 24 - .
09:42 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1A.
- Cosmos 2515 - .
Payload: Bars-M No. 2. Nation: Russia.
Class: Surveillance.
Type: Cartographic satellite. Spacecraft Bus: Yantar.
Spacecraft: Bars.
USAF Sat Cat: 41394 . COSPAR: 2016-020A. Apogee: 540 km (330 mi). Perigee: 332 km (206 mi). Inclination: 97.60 deg. Bars-M cartography satellite; joined the No. 1 satellite (Kosmos-2503) launched in 2015. 1325LT SSO..
2016 April 25 - .
21:02 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELS.
LV Family:
R-7.
Launch Vehicle:
Soyuz-ST-A.
- Sentinel-1B - .
Mass: 2,157 kg (4,755 lb). Nation: Europe.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Prima.
USAF Sat Cat: 41456 . COSPAR: 2016-025A. Apogee: 700 km (430 mi). Perigee: 695 km (431 mi). Inclination: 98.20 deg.
Arianespace flight VS14. The Fregat stage first burn reached an initial orbit of 695 x 700 km and deployed the Sentinel-1B radar imaging satellite for ESA. It then made a burn to 442 x 690 km and deployed three 1U cubesats. The ASAP-S adapter was ejected into the same orbit. Next, the Fregat stage made two more burns to reach 711 x 714 km and released the Microscope satellite. Finally, at 0118 UTC, Fregat made a deorbit burn and reentered over the S Atlantic. 1800LT SSO.
2016 April 27 - .
11:45 GMT - .
Launch Platform: ISS.
- Diwata-1 - .
Mass: 50 kg (110 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41463 . COSPAR: 1998-067HT. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. The 50 kg Diwata-1 satellite, launched on Cygnus OA-6, was removed from the Kibo airlock by the JRMS arm and released into orbit. Diwata-1 was an Earth observation satellite developed by the Phillipines..
2016 April 28 - .
02:01 GMT - .
Launch Site:
Vostochniy.
Launch Complex:
Vostochniy PU1S.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1A.
- AIST-2D - .
Nation: Russia.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41465 . COSPAR: 2016-026B. Apogee: 485 km (301 mi). Perigee: 471 km (292 mi). Inclination: 97.30 deg. Samara State Aerospace University's AIST-2D imaging satellite;, the student-built Samsat-218/D
failed to transmit properly..
2016 May 17 - .
08:45 GMT - .
Launch Platform: ISS.
- Flock 2e'-1/0D05 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-04-15 . USAF Sat Cat: 41479 . COSPAR: 1998-067HZ. Apogee: 402 km (249 mi). Perigee: 399 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-2/0C1B - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2017-12-01 . USAF Sat Cat: 41481 . COSPAR: 1998-067JB. Apogee: 401 km (249 mi). Perigee: 400 km (240 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-3/0D06 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-04-18 . USAF Sat Cat: 41480 . COSPAR: 1998-067JA. Apogee: 402 km (249 mi). Perigee: 398 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-4/0C22 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2017-11-08 . USAF Sat Cat: 41482 . COSPAR: 1998-067JC. Apogee: 402 km (249 mi). Perigee: 399 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-1/0C37 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-06-16 . USAF Sat Cat: 41483 . COSPAR: 1998-067JD. Apogee: 403 km (250 mi). Perigee: 398 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-2/0C78 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-01-23 . USAF Sat Cat: 41484 . COSPAR: 1998-067JE. Apogee: 402 km (249 mi). Perigee: 398 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-3/0C60 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-04-05 . USAF Sat Cat: 41486 . COSPAR: 1998-067JG. Apogee: 402 km (249 mi). Perigee: 399 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-4/0C41 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-03-11 . USAF Sat Cat: 41487 . COSPAR: 1998-067JH. Apogee: 403 km (250 mi). Perigee: 398 km (247 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2016 May 30 - .
03:17 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Ziyuan-3 02 - .
Payload: ZY 3 2. Nation: China.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41556 . COSPAR: 2016-033A. Apogee: 499 km (310 mi). Perigee: 484 km (300 mi). Inclination: 97.50 deg. 1024LT sun synchronous orbit satellitefor China's Satellite Surveying and Mapping Applications Center.
It carried a 2-meter-resolution Earth imaging cameras..
- Batata - .
Payload: NUSAT 2. Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41558 . COSPAR: 2016-033C. Apogee: 499 km (310 mi). Perigee: 481 km (298 mi). Inclination: 97.50 deg. 1024LT SSO.
2016 May 30 - .
11:40 GMT - .
Launch Platform: ISS.
- Flock 2e-6/0C75 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-02-12 . USAF Sat Cat: 41563 . COSPAR: 1998-067JM. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-5/0C43 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-08-14 . USAF Sat Cat: 41564 . COSPAR: 1998-067JN. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-7/0C24 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-04-06 . USAF Sat Cat: 41565 . COSPAR: 1998-067JP. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-8/0C2B - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2017-07-25 . USAF Sat Cat: 41566 . COSPAR: 1998-067JQ. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-5/0C59 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-06-27 . USAF Sat Cat: 41567 . COSPAR: 1998-067JR. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-6/0C46 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-04-05 . USAF Sat Cat: 41568 . COSPAR: 1998-067JS. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-7/0C42 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-04-05 . USAF Sat Cat: 41569 . COSPAR: 1998-067JT. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-8/0C76 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2017-10-03 . USAF Sat Cat: 41570 . COSPAR: 1998-067JU. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-9/0C14 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2017-12-25 . USAF Sat Cat: 41571 . COSPAR: 1998-067JV. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-10/0C82 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-02-28 . USAF Sat Cat: 41572 . COSPAR: 1998-067JW. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-12/0C79 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-03-04 . USAF Sat Cat: 41573 . COSPAR: 1998-067JX. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e-11/0C13 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-03-04 . USAF Sat Cat: 41574 . COSPAR: 1998-067JY. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-9/0C19 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-03-12 . USAF Sat Cat: 41575 . COSPAR: 1998-067JZ. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-10/0C65 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-02-17 . USAF Sat Cat: 41576 . COSPAR: 1998-067KA. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-11/0C27 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-03-11 . USAF Sat Cat: 41577 . COSPAR: 1998-067KB. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-12/0C81 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-02-28 . USAF Sat Cat: 41578 . COSPAR: 1998-067KC. Apogee: 404 km (251 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2016 June 11 - .
17:51 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC37B.
Launch Pad: Cape Canaveral SLC37.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 268 - .
Payload: SIGINT. Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Advanced Orion.
USAF Sat Cat: 41584 . COSPAR: 2016-036A. Apogee: 36,000 km (22,000 mi). Perigee: 35,612 km (22,128 mi). Inclination: 7.50 deg.
The NROL-37 mission was a large signals intelligence (SIGINT) satellite, placed in geosynchronous orbit at 103 deg E over the Indian Ocean. Possibly the second Orion/Sharp model. There were two main lineages of GEO SIGINT satellites operated by the US National Reconnaissance Office: MERCURY (originally CANYON); and RHYOLITE (later AQUACADE), which was replaced in the 1980s by ORION (whose other rumoured codenames include MAGNUM and MENTOR). Launches of the MERCURY series ended in 1998, at which time it was rumoured that its capabilites would be merged into the ORION series. A number of observers suggested that the 2014 GEO SIGINT launch of USA 250 on an Atlas V was a one-off mission not part of the ORION series, and that with an increase in mass ORION had moved to using the RS-68A-powered Delta 4 Heavy rockets. It was further been suggested that the 2014 launch might be the NEMESIS 2 satellite mentioned in leaked FY2013 budget documents; however a close reading of those documents showed that funding for the latter project was cut off after FY2011, which implies that it was either launched by then or cancelled (more likely given the sudden drop from half-billion-dollar-level funding to zero). The documents also mention
SHARP, the SIGINT High Altitude Replenishment Program, funded at a high level in FY2011-2013 and reportedly also since. It's possible the 2012 and 2016 launches may represent a new ORION/SHARP series, or that they are beefed up ORION and the 2014 launch was a SHARP prototype. The shorter fairing used for the 2014 launch suggests that it was not in fact an ORION.
2016 June 22 - .
03:55 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
Launch Vehicle:
PSLV.
- Cartosat-2 Series - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41599 . COSPAR: 2016-040A. Apogee: 518 km (321 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 0930LT SSO. Cartosat-2 series imaging satellite.
- LAPAN-A3 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41603 . COSPAR: 2016-040E. Apogee: 517 km (321 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 120 kg imaging satellite for Indonesia's LAPAN space agency.
- BIROS - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41604 . COSPAR: 2016-040F. Apogee: 516 km (320 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 130 kg infrared satellite to study fires, for Germany's DLR; also carried the BEESAT-4 cubesat to be ejected later..
- SkySat 2G-1 - .
Payload: SkySat C1. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Skysat.
USAF Sat Cat: 41601 . COSPAR: 2016-040C. Apogee: 515 km (320 mi). Perigee: 501 km (311 mi). Inclination: 97.50 deg. A 110 kg imaging satellite for TerraBella's constellation.
- Flock 2P-1 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41617 . COSPAR: 2016-040U. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-2 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41609 . COSPAR: 2016-040L. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-3 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41618 . COSPAR: 2016-040V. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-4 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41611 . COSPAR: 2016-040N. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-5 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41616 . COSPAR: 2016-040T. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-6 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41606 . COSPAR: 2016-040H. Apogee: 514 km (319 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 3U imaging cubesats for Planet (formerly PlanetLabs).
- Flock 2P-7 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41615 . COSPAR: 2016-040S. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-8 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41613 . COSPAR: 2016-040Q. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-9 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41610 . COSPAR: 2016-040M. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-10 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41612 . COSPAR: 2016-040P. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-11 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41608 . COSPAR: 2016-040K. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-12 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41614 . COSPAR: 2016-040R. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2016 June 29 - .
03:21 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4B.
- Shi Jian 16-02 - .
Payload: SJ 16-02. Nation: China.
Class: Surveillance.
Type: ELINT. Spacecraft: DFH-4.
USAF Sat Cat: 41634 . COSPAR: 2016-043A. Apogee: 616 km (382 mi). Perigee: 596 km (370 mi). Inclination: 75.00 deg. Chinese technology satellite..
2016 August 9 - .
22:55 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- Gaofen 3 - .
Nation: China.
Class: Surveillance.
Type: Military Radarsat. USAF Sat Cat: 41727 . COSPAR: 2016-049A. Apogee: 751 km (466 mi). Perigee: 750 km (460 mi). Inclination: 98.40 deg. A 1-meter-resolution C-band radar imaging satellite placed in 750 km 0600LT sun-synchronous orbit. Its primary user was the National Satellite Oceanic Applications Center in Mudanjiang..
2016 August 19 - .
04:52 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC37B.
Launch Pad: Cape Canaveral SLC37B.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(4,2).
- USA 270 - .
Payload: GSSAP 3. Nation: USA.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft Bus: GeoStar-1.
Spacecraft: GSSAP.
USAF Sat Cat: 41744 . COSPAR: 2016-052A. Apogee: 35,819 km (22,256 mi). Perigee: 35,749 km (22,213 mi). Inclination: 0.00 deg. Placed in geosynchronous orbit at 111 deg W. The satellites will drift in the geostationary ring making observations of the orbits of other satellites..
- USA 271 - .
Payload: GSSAP 4. Nation: USA.
Class: Surveillance.
Type: Orbital object tracking satellite. Spacecraft Bus: GeoStar-1.
Spacecraft: GSSAP.
USAF Sat Cat: 41745 . COSPAR: 2016-052B. Apogee: 35,856 km (22,279 mi). Perigee: 35,814 km (22,253 mi). Inclination: 0.00 deg. Placed in geosynchronous orbit at 118 deg W..
2016 August 31 - .
18:55 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 4C.
- GaoFen 10 - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. COSPAR: 2016-0F01. High resolution imaging satellite lost in the launch failure. Rumored third stage restart failure, which would have left the vehicle just short of a marginal orbit..
2016 September 13 - .
13:48 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shavit.
- 'Ofeq-11 - .
Nation: Israel.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Tecsar.
USAF Sat Cat: 41759 . COSPAR: 2016-056A. Apogee: 600 km (370 mi). Perigee: 250 km (150 mi). Inclination: 141.00 deg. Ofeq-11 spy satellite, thought to be ususal retrograde orbit. It was reported that Israeli mission controllers were working to correct unspecified technical problems with the payload..
2016 September 14 - .
15:25 GMT - .
Launch Platform: ISS.
- Flock 2e'-13 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-06-03 . USAF Sat Cat: 41761 . COSPAR: 1998-067KH. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg.
On Sep 14 the Nanoracks NRCSD-9 deployer was pulled from the Kibo airlock by the Japanese RMS arm, and at 1525 UTC two Flock 2E Prime satellites were ejected into space, with six more to come from the same deployer. These satellites have been aboard ISS since their delivery aboard Cygnus OA-6 in March.
- Flock 2e'-14 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-10-25 . USAF Sat Cat: 41762 . COSPAR: 1998-067KJ. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-16 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-06-01 . USAF Sat Cat: 41763 . COSPAR: 1998-067KK. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-15 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-11-10 . USAF Sat Cat: 41764 . COSPAR: 1998-067KL. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-18 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-11-07 . USAF Sat Cat: 41769 . COSPAR: 1998-067KM. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-17 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-06-26 . USAF Sat Cat: 41776 . COSPAR: 1998-067KN. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-19 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-05-12 . USAF Sat Cat: 41777 . COSPAR: 1998-067KP. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2e'-20 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
Decay Date: 2018-09-22 . USAF Sat Cat: 41782 . COSPAR: 1998-067KQ. Apogee: 409 km (254 mi). Perigee: 401 km (249 mi). Inclination: 51.60 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2016 September 16 - .
01:43 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELV.
Launch Vehicle:
Vega.
- PeruSAT-1 - .
Nation: Europe.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Astrobus.
USAF Sat Cat: 41770 . COSPAR: 2016-058A. Apogee: 678 km (421 mi). Perigee: 676 km (420 mi). Inclination: 98.20 deg. Optical surveillance satellite for the Peruvian military..
- SkySat-4 - .
Nation: Europe.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Skysat.
USAF Sat Cat: 41773 . COSPAR: 2016-058D. Apogee: 502 km (311 mi). Perigee: 501 km (311 mi). Inclination: 97.40 deg.
Arianespace's Vega rocket made its 7th flight from Kourou. The AVUM upper stage made two burns to deploy TerraBella's SkySat 4 to 7 in a 500 km orbit at 0224 UTC, and then two further burns to put PeruSAT-1 in a 677 km orbit at 0326 UTC. The AVUM made a final burn to deorbit itself in the Indian Ocean west of Sumatra.
- SkySat-5 - .
Nation: Europe.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Skysat.
USAF Sat Cat: 41774 . COSPAR: 2016-058E. Apogee: 502 km (311 mi). Perigee: 501 km (311 mi). Inclination: 97.40 deg.
- SkySat-6 - .
Nation: Europe.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Skysat.
USAF Sat Cat: 41771 . COSPAR: 2016-058B. Apogee: 506 km (314 mi). Perigee: 497 km (308 mi). Inclination: 97.40 deg.
- SkySat-7 - .
Nation: Europe.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Skysat.
USAF Sat Cat: 41772 . COSPAR: 2016-058C. Apogee: 503 km (312 mi). Perigee: 501 km (311 mi). Inclination: 97.40 deg.
2016 September 26 - .
03:42 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
Launch Vehicle:
PSLV.
- Pathfinder 1 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41787 . COSPAR: 2016-059E. Apogee: 703 km (436 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg. From Black Sky Global (Seattle) with a 1 meter imager 0930LT SSO.
- ALSAT-1B - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41785 . COSPAR: 2016-059C. Apogee: 704 km (437 mi). Perigee: 661 km (410 mi). Inclination: 98.20 deg. 0930LT SSO imaging satellites for the Algerian space agency ASAL: ALSAT-1B built by Surrey.
- ALSAT-2B - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41786 . COSPAR: 2016-059D. Apogee: 673 km (418 mi). Perigee: 672 km (417 mi). Inclination: 98.20 deg. 0930LT SSO built by Airbus/Toulouse.
2016 November 9 - .
23:42 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-E.
LV Family:
DF-31.
Launch Vehicle:
Chang Zheng 11.
- Lishui 1-01 - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41843 . COSPAR: 2016-066C. Apogee: 511 km (317 mi). Perigee: 491 km (305 mi). Inclination: 97.40 deg. Imaging satellite launched to begin a commercial constellation for Zhejiang LiYi Electronic Technology Co..
- KS-1Q - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41844 . COSPAR: 2016-066D. Apogee: 511 km (317 mi). Perigee: 491 km (305 mi). Inclination: 97.40 deg. Instrument package, attached to the CZ-11 final stage, measured the launch vehicle environment..
- CAS-2T - .
Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41844 . COSPAR: 2016-066D. Apogee: 511 km (317 mi). Perigee: 491 km (305 mi). Inclination: 97.40 deg. Amateur radio payload in a 1U cubesat; remained attached to the launch vehicle..
2016 November 11 - .
18:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- WorldView-4 - .
Mass: 2,800 kg (6,100 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: BCP-5000.
USAF Sat Cat: 41848 . COSPAR: 2016-067A. Apogee: 611 km (379 mi). Perigee: 607 km (377 mi). Inclination: 98.00 deg.
United Launch Alliance Atlas V, serial AV-062, placed the DigitalGlobe WorldView-4 commercial imaging satellite in orbit. WV-4 was originaly GeoEye-2 before the GeoEye/DG merger, and has a resolution of only 0.25 metres. AV-062 reached a 600 km orbit at 1846 UTC and deployed
WV-4 at 1849 UTC. AV-062 also carried four cubesat deployers on its Aft Bulkhead Carrier. At 2120 UTC AV-062 made its second burn, accelerating to escape velocity to avoid it contributing to LEO space junk. The stage departed the Earth's gravitational sphere of influence on Nov 15 to enter
a solar orbit of 0.93 x 1.57 AU x 3.4 deg.
- Opticube 4 - .
Nation: USA.
Class: Surveillance.
Type: Radar calibration target. Spacecraft: Cubesat.
USAF Sat Cat: 41851 . COSPAR: 2016-067D. Apogee: 585 km (363 mi). Perigee: 576 km (357 mi). Inclination: 98.00 deg. 2U tracking calibration satellite, CalPoly's Opticub..
2016 December 5 - .
13:51 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ZLV.
Launch Vehicle:
Vega.
- Gokturk-1 - .
Nation: Turkey.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41875 . COSPAR: 2016-073A. Apogee: 691 km (429 mi). Perigee: 679 km (421 mi). Inclination: 98.10 deg. Turkish Defense Ministry's Gokturk-1 high resolution (0.7m) imaging satellite. The satellite
was built by Thales Alenia (Cannes).. 2230LT SSO.
2016 December 7 - .
04:54 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
LV Family:
PSLV.
Launch Vehicle:
PSLV-XL.
- Resourcesat-2A - .
Nation: India.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41877 . COSPAR: 2016-074A. Apogee: 831 km (516 mi). Perigee: 814 km (505 mi). Inclination: 98.70 deg. 1030LT SSO imaging satellite to provide continuity of service for the system as 2011's Resourcesat-2 ages. The satellite has a 6 metre resolution imager..
2016 December 21 - .
19:22 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Spark-01 - .
Mass: 50 kg (110 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41900 . COSPAR: 2016-081C. Apogee: 720 km (440 mi). Perigee: 690 km (420 mi). Inclination: 98.10 deg. 50 kg satellite with hyperspectral imager..
- Spark-02 - .
Mass: 50 kg (110 lb). Nation: China.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41901 . COSPAR: 2016-081D. Apogee: 726 km (451 mi). Perigee: 690 km (420 mi). Inclination: 98.10 deg. About 50 kg each. Spark-01 and Spark-02
have hyperspectral imagers; the third, referred to as Chao fenbianlu duo
guangpu chengxiang weixing (Ultra-resolution multispectral imaging
satellite) has a 1.4m resolution imager.
- CFDG - .
Payload: YIJIAN. Nation: China.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41899 . COSPAR: 2016-081B. Apogee: 728 km (452 mi). Perigee: 690 km (420 mi). Inclination: 98.10 deg. 50 kg satellite, referred to as Chao fenbianlu duo guangpu chengxiang weixing (Ultra-resolution multispectral imaging satellite), with a 1.4m resolution imager..
2016 December 28 - .
03:23 GMT - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- Gaojing 1 - .
Payload: Superview-1 01. Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CAST3000.
USAF Sat Cat: 41907 . COSPAR: 2016-083A. Apogee: 523 km (324 mi). Perigee: 212 km (131 mi). Inclination: 97.60 deg.
The first time the CZ-2D booster was flown from their southern launch site. However, the rocket appeared to have run into problems and achieved orbit with an underspeed of 100 m/s, making
a 212 x 520 km orbit instead of a circular 500 km one. The main payloads were Gaojing 1 and 2, two commercial high resolution (0.5m) imaging satellites also called SuperView 1 and 2. The satellites
were owned by Beijing Aerospace World View Information Technology Co., Ltd (also called Beijing Space View Tech Co.Ltd.); the US company DigitalGlobe was a major investor. 1030LT SSO
- Gaojing 2 - .
Payload: Superview-1 02. Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: CAST3000.
USAF Sat Cat: 41908 . COSPAR: 2016-083B. Apogee: 523 km (324 mi). Perigee: 212 km (131 mi). Inclination: 97.60 deg. 1030LT SSO.
2017 January 5 - .
15:18 GMT - .
Launch Site:
Xichang.
Launch Complex:
Xichang LC2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 3B.
- Tongxin Jishu SW 2 - .
Payload: TJS-2. Nation: China.
Class: Surveillance.
Type: ELINT. Spacecraft: DFH-4.
USAF Sat Cat: 41911 . COSPAR: 2017-001A. Apogee: 35,801 km (22,245 mi). Perigee: 201 km (124 mi). Inclination: 27.50 deg.
See TJS 2 (Huoyan-1 ?). Tongxin Jishu Shiyan Weixing 2 (Communications Technology Experiment Satellite 2) was developed by the Shanghai team. The lack of public information about the TJSW satellites has led to the suspicion that they may really be for defense purposes, possibly for non-communications purposes such as signals intelligence or missile early warning. TJSW 2 made the burn to circularize its orbit on Jan 6 at 0730 UTC over 114E.
2017 January 9 - .
04:11 GMT - .
Launch Site:
Jiuquan.
LV Family:
DF-21.
Launch Vehicle:
Kuaizhou.
- Linye 1 (Jilin-1S3) - .
Payload: Jilin-1-03. Nation: China.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41914 . COSPAR: 2017-002B. Apogee: 545 km (338 mi). Perigee: 513 km (318 mi). Inclination: 97.50 deg.
See Jilin-1 Video-03 (Jilin Linye 1). Kuaizhou-1A quick-response rocket test. The earlier KZ-1 rocket was used for two low orbit imaging satellites which remained integrated with the upper stage; in the commercialized KZ-1A version the 4th stage separates from the payloads, and launch services are provided by EXPACE, the commercial arm of KZ-1A builder CASIC (which also builds the DF-21 missile that KZ-1/1A was based on). The main payload was Chang Guang Satellite Technology Ltd's "Jilin-1 linqiao shipin xing 03 xing", also called Jilin Linye 1 Weixing (Jilin Forestry 1 satellite). The 165 kg sat has a 1m resolution Earth imager. Two 2U cubesats were also carried. 1030LT SSO.
2017 January 21 - .
00:42 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC41.
Launch Pad: Cape Canaveral SLC41.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 273 - .
Payload: SBIRS GEO-3 / A2100M. Mass: 4,500 kg (9,900 lb). Nation: USA.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: AS 2100.
USAF Sat Cat: 41937 . COSPAR: 2017-004A. Apogee: 35,847 km (22,274 mi). Perigee: 195 km (121 mi). Inclination: 23.30 deg. See SBIRS-GEO 3 (USA 273). Atlas AV-066 launched the third SBIRS GEO early warning sat into geotransfer orbit. SBIRS GEO used an infrared telescope to detect missile launches..
2017 February 15 - .
03:58 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota PSLV.
LV Family:
PSLV.
Launch Vehicle:
PSLV-XL.
- Cartosat-2 Series/4 - .
Payload: Cartosat 2D. Nation: India.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41948 . COSPAR: 2017-008A. Apogee: 520 km (320 mi). Perigee: 505 km (313 mi). Inclination: 97.50 deg.
See Cartosat 2D. India's PSLV placed a record 104 payloads in orbit on Feb 15, 100 of them via 25 QuadPack cubesat dispensers from the Dutch company ISISSpace. The main payload was the 714 kg `Cartosat-2 series satellite', the fourth such imaging payload from ISRO.
- INS-1B - .
Nation: India.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41954 . COSPAR: 2017-008G. Apogee: 507 km (315 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See INS 1B. Two 10 kg INS-1 (Indian Nanosatellite) technology payloads..
- Flock 3p-1 - .
Payload: Dove 1000. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41967 . COSPAR: 2017-008V. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 1 (Dove 1000). ..
- Flock 3p-2 - .
Payload: Dove 1001. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41966 . COSPAR: 2017-008U. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 2 (Dove 1001). ..
- Flock 3p-3 - .
Payload: Dove 1002. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41968 . COSPAR: 2017-008W. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 3 (Dove 1002). ..
- Flock 3p-4 - .
Payload: Dove 1003. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41965 . COSPAR: 2017-008T. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 4 (Dove 1003). ..
- Flock 3p-5 - .
Payload: Dove 0F18. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41971 . COSPAR: 2017-008Z. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 5 (Dove 0F18). ..
- Flock 3p-6 - .
Payload: Dove 0F35. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41969 . COSPAR: 2017-008X. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 6 (Dove 0F35). ..
- Flock 3p-7 - .
Payload: Dove 100B. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41970 . COSPAR: 2017-008Y. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 7 (Dove 100B). ..
- Flock 3p-8 - .
Payload: Dove 100C. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41951 . COSPAR: 2017-008D. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 8 (Dove 100C). ..
- Flock 3p-9 - .
Payload: Dove 1021. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41973 . COSPAR: 2017-008AB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 9 (Dove 1021). ..
- Flock 3p-10 - .
Payload: Dove 1022. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41974 . COSPAR: 2017-008AC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 10 (Dove 1022). ..
- Flock 3p-11 - .
Payload: Dove 101F. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41975 . COSPAR: 2017-008AD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 11 (Dove 101F). ..
- Flock 3p-12 - .
Payload: Dove 1010. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41972 . COSPAR: 2017-008AA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 12 (Dove 1010). ..
- Flock 3p-13 - .
Payload: Dove 1016. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42040 . COSPAR: 2017-008CW. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 13 (Dove 1016). ..
- Flock 3p-14 - .
Payload: Dove 1018. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42012 . COSPAR: 2017-008BS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 14 (Dove 1018). ..
- Flock 3p-15 - .
Payload: Dove 101D. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42039 . COSPAR: 2017-008CV. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 15 (Dove 101D). ..
- Flock 3p-16 - .
Payload: Dove 100E. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42011 . COSPAR: 2017-008BR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 16 (Dove 100E). ..
- Flock 3p-17 - .
Payload: Dove 1023. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41962 . COSPAR: 2017-008Q. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 17 (Dove 1023). ..
- Flock 3p-18 - .
Payload: Dove 102B. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41957 . COSPAR: 2017-008K. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 18 (Dove 102B). ..
- Flock 3p-19 - .
Payload: Dove 1024. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41955 . COSPAR: 2017-008H. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 19 (Dove 1024). ..
- Flock 3p-20 - .
Payload: Dove 1029. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41950 . COSPAR: 2017-008C. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 20 (Dove 1029). ..
- Flock 3p-21 - .
Payload: Dove 102A. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41959 . COSPAR: 2017-008M. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 21 (Dove 102A). ..
- Flock 3p-22 - .
Payload: Dove 1028. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41958 . COSPAR: 2017-008L. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 22 (Dove 1028). ..
- Flock 3p-23 - .
Payload: Dove 1025. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42018 . COSPAR: 2017-008BY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 23 (Dove 1025). ..
- Flock 3p-24 - .
Payload: Dove 1026. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41956 . COSPAR: 2017-008J. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 24 (Dove 1026). ..
- Flock 3p-25 - .
Payload: Dove 102F. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41964 . COSPAR: 2017-008S. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 25 (Dove 102F). ..
- Flock 3p-26 - .
Payload: Dove 102D. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41961 . COSPAR: 2017-008P. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 26 (Dove 102D). ..
- Flock 3p-27 - .
Payload: Dove 1030. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41963 . COSPAR: 2017-008R. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 27 (Dove 1030). ..
- Flock 3p-28 - .
Payload: Dove 102C. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41960 . COSPAR: 2017-008N. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 28 (Dove 102C). ..
- Flock 3p-29 - .
Payload: Dove 1033. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42045 . COSPAR: 2017-008DB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 29 (Dove 1033). ..
- Flock 3p-30 - .
Payload: Dove 102E. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41987 . COSPAR: 2017-008AR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 30 (Dove 102E). ..
- Flock 3p-31 - .
Payload: Dove 1032. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42049 . COSPAR: 2017-008DF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 31 (Dove 1032). ..
- Flock 3p-32 - .
Payload: Dove 1035. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42023 . COSPAR: 2017-008CD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 32 (Dove 1035). ..
- Flock 3p-33 - .
Payload: Dove 103C. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41990 . COSPAR: 2017-008AU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 33 (Dove 103C). ..
- Flock 3p-34 - .
Payload: Dove 103B. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41988 . COSPAR: 2017-008AS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 34 (Dove 103B). ..
- Flock 3p-35 - .
Payload: Dove 103D. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41989 . COSPAR: 2017-008AT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 35 (Dove 103D). ..
- Flock 3p-36 - .
Payload: Dove 103A. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41986 . COSPAR: 2017-008AQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 36 (Dove 103A). ..
- Flock 3p-37 - .
Payload: Dove 1037. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41953 . COSPAR: 2017-008F. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 37 (Dove 1037). ..
- Flock 3p-38 - .
Payload: Dove 1036. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42037 . COSPAR: 2017-008CT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 38 (Dove 1036). ..
- Flock 3p-39 - .
Payload: Dove 103E. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42038 . COSPAR: 2017-008CU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 39 (Dove 103E). ..
- Flock 3p-40 - .
Payload: Dove 1039. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42010 . COSPAR: 2017-008BQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 40 (Dove 1039). ..
- Flock 3p-41 - .
Payload: Dove 1031. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42004 . COSPAR: 2017-008BJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 41 (Dove 1031). ..
- Flock 3p-42 - .
Payload: Dove 101E. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42008 . COSPAR: 2017-008BN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 42 (Dove 101E). ..
- Flock 3p-43 - .
Payload: Dove 1041. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42007 . COSPAR: 2017-008BM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 43 (Dove 1041). ..
- Flock 3p-44 - .
Payload: Dove 1019. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42033 . COSPAR: 2017-008CP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 44 (Dove 1019). ..
- Flock 3p-45 - .
Payload: Dove 101A. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42005 . COSPAR: 2017-008BK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 45 (Dove 101A). ..
- Flock 3p-46 - .
Payload: Dove 1011. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42031 . COSPAR: 2017-008CM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 46 (Dove 1011). ..
- Flock 3p-47 - .
Payload: Dove 1027. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42032 . COSPAR: 2017-008CN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 47 (Dove 1027). ..
- Flock 3p-48 - .
Payload: Dove 1042. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42006 . COSPAR: 2017-008BL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 48 (Dove 1042). ..
- Flock 3p-49 - .
Payload: Dove 1038. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42001 . COSPAR: 2017-008BF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 49 (Dove 1038). ..
- Flock 3p-50 - .
Payload: Dove 1034. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42029 . COSPAR: 2017-008CK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 50 (Dove 1034). ..
- Flock 3p-51 - .
Payload: Dove 1006. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41952 . COSPAR: 2017-008E. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 51 (Dove 1006). ..
- Flock 3p-52 - .
Payload: Dove 1044. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42030 . COSPAR: 2017-008CL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 52 (Dove 1044). ..
- Flock 3p-53 - .
Payload: Dove 1007. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42013 . COSPAR: 2017-008BT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 53 (Dove 1007). ..
- Flock 3p-54 - .
Payload: Dove 1005. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42014 . COSPAR: 2017-008BU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 54 (Dove 1005). ..
- Flock 3p-55 - .
Payload: Dove 1008. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42041 . COSPAR: 2017-008CX. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 55 (Dove 1008). ..
- Flock 3p-56 - .
Payload: Dove 100F. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42042 . COSPAR: 2017-008CY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 56 (Dove 100F). ..
- Flock 3p-57 - .
Payload: Dove 1014. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41978 . COSPAR: 2017-008AG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 57 (Dove 1014). ..
- Flock 3p-58 - .
Payload: Dove 1009. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41977 . COSPAR: 2017-008AF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 58 (Dove 1009). ..
- Flock 3p-59 - .
Payload: Dove 1045. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42021 . COSPAR: 2017-008CB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 59 (Dove 1045). ..
- Flock 3p-60 - .
Payload: Dove 101B. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41976 . COSPAR: 2017-008AE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 60 (Dove 101B). ..
- Flock 3p-61 - .
Payload: Dove 1012. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42009 . COSPAR: 2017-008BP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 61 (Dove 1012). ..
- Flock 3p-62 - .
Payload: Dove 1046. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42036 . COSPAR: 2017-008CS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 62 (Dove 1046). ..
- Flock 3p-63 - .
Payload: Dove 1015. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42035 . COSPAR: 2017-008CR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 63 (Dove 1015). ..
- Flock 3p-64 - .
Payload: Dove 100A. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42034 . COSPAR: 2017-008CQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 64 (Dove 100A). ..
- Flock 3p-65 - .
Payload: Dove 1040. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42028 . COSPAR: 2017-008CJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 65 (Dove 1040). ..
- Flock 3p-66 - .
Payload: Dove 1013. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42027 . COSPAR: 2017-008CH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 66 (Dove 1013). ..
- Flock 3p-67 - .
Payload: Dove 1017. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42002 . COSPAR: 2017-008BG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 67 (Dove 1017). ..
- Flock 3p-68 - .
Payload: Dove 1004. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42003 . COSPAR: 2017-008BH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 68 (Dove 1004). ..
- Flock 3p-69 - .
Payload: Dove 0F43. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42019 . COSPAR: 2017-008BZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 69 (Dove 0F43). ..
- Flock 3p-70 - .
Payload: Dove 0F15. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41980 . COSPAR: 2017-008AJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 70 (Dove 0F15). ..
- Flock 3p-71 - .
Payload: Dove 0F11. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42051 . COSPAR: 2017-008DH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 71 (Dove 0F11). ..
- Flock 3p-72 - .
Payload: Dove 0F10. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42024 . COSPAR: 2017-008CE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 72 (Dove 0F10). ..
- Flock 3p-73 - .
Payload: Dove 0F1B. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41981 . COSPAR: 2017-008AK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 73 (Dove 0F1B). ..
- Flock 3p-74 - .
Payload: Dove 0F22. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42048 . COSPAR: 2017-008DE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 74 (Dove 0F22). ..
- Flock 3p-75 - .
Payload: Dove 0F12. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41979 . COSPAR: 2017-008AH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 75 (Dove 0F12). ..
- Flock 3p-76 - .
Payload: Dove 0F17. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42020 . COSPAR: 2017-008CA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 76 (Dove 0F17). ..
- Flock 3p-77 - .
Payload: Dove 0F28. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42025 . COSPAR: 2017-008CF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 77 (Dove 0F28). ..
- Flock 3p-78 - .
Payload: Dove 0F51. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42047 . COSPAR: 2017-008DD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 78 (Dove 0F51). ..
- Flock 3p-79 - .
Payload: Dove 0F52. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41984 . COSPAR: 2017-008AN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 79 (Dove 0F52). ..
- Flock 3p-80 - .
Payload: Dove 0F4E. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42026 . COSPAR: 2017-008CG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 80 (Dove 0F4E). ..
- Flock 3p-81 - .
Payload: Dove 0F25. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42043 . COSPAR: 2017-008CZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 81 (Dove 0F25). ..
- Flock 3p-82 - .
Payload: Dove 0F41. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42046 . COSPAR: 2017-008DC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 82 (Dove 0F41). ..
- Flock 3p-83 - .
Payload: Dove 0F3F. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42050 . COSPAR: 2017-008DG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 83 (Dove 0F3F). ..
- Flock 3p-84 - .
Payload: Dove 0F42. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42022 . COSPAR: 2017-008CC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 84 (Dove 0F42). ..
- Flock 3p-85 - .
Payload: Dove 0F1D. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41983 . COSPAR: 2017-008AM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 85 (Dove 0F1D). ..
- Flock 3p-86 - .
Payload: Dove 0F34. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41985 . COSPAR: 2017-008AP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 86 (Dove 0F34). ..
- Flock 3p-87 - .
Payload: Dove 0F31. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 42044 . COSPAR: 2017-008DA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 87 (Dove 0F31). ..
- Flock 3p-88 - .
Payload: Dove 0F38. Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Cubesat.
USAF Sat Cat: 41982 . COSPAR: 2017-008AL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 88 (Dove 0F38). ..
2017 March 1 - .
17:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3E.
LV Family:
Atlas V.
Launch Vehicle:
Atlas V 401.
- USA 274 - .
Payload: INTRUDER. Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 42058 . COSPAR: 2017-011A. Apogee: 1,204 km (748 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg.
See Intruder 12A (NOSS-3 8A, USA 274, NROL 79). Atlas V serial AV-068 carried a National Reconnaissance Office payload to orbit on NRO launch NROL-79. The payload was thought to be an NRO/Navy signals intelligence system code-named INTRUDER consisting of a pair of satellites in 1010 x 1200 km x 63 deg orbit. Both satellites were observed by hobbyists on Mar 3. The Centaur second stage was deorbited south of Australia on the first orbit
with impact around 1956 UTC.
- USA 274 P/L 2 - .
Payload: NOSS-3 8B, USA 274-2, NROL 79. Nation: USA.
Class: Surveillance.
Type: SIGINT. Spacecraft: Intruder.
USAF Sat Cat: 42065 . COSPAR: 2017-011B. Apogee: 1,204 km (748 mi). Perigee: 1,009 km (626 mi). Inclination: 63.50 deg.
2017 March 7 - .
01:49 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ZLV.
Launch Vehicle:
Vega.
- Sentinel-2B - .
Mass: 1,130 kg (2,490 lb). Nation: Europe.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: Astrobus.
USAF Sat Cat: 42063 . COSPAR: 2017-013A. Apogee: 782 km (485 mi). Perigee: 776 km (482 mi). Inclination: 98.60 deg. See Sentinel 2B. ESA Sentinel-2B imaging satellite, part of the EU's Copernicus Earth observing system, launched by Vega VV09..
2017 March 17 - .
01:20 GMT - .
Launch Site:
Tanegashima.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS Radar 5 - .
Nation: Japan.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: IGS.
USAF Sat Cat: 42072 . COSPAR: 2017-015A. Apogee: 510 km (310 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. See IGS-Radar 5. Japan launched the Joho shushu eisei Reda 5-goki (IGS Radar 5) spy satellite into polar orbit..
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