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On July 14 in Space History
1913 July 14 - .
- Birth of Gerald R Ford - .
Nation: USA.
Related Persons: Ford, Gerald.
American politician. House of Representatives 1948-1973; Vice President 1973-1974; President 1974-1977. No new space initiatives, stewarded Nixon's program of ending Apollo, single Apollo-Soyuz flight, continued Shuttle development..
1913 July 14 - .
- Birth of Leonid Aleksandrovich Voskresenskiy - .
Nation: Russia.
Related Persons: Voskresenskiy.
Russian engineer. Deputy Chief Designer 1953-1964 of Korolev design bureau..
1914 July 14 - .
- Goddard patents liquid fuel rocket - .
Nation: USA.
Related Persons: Goddard.
Goddard receives US Patent 1,103,503. Although mainly concerned with his concept of cartridge rockets, a brief section fully outlines the concept of liquid rocket propulsion..
1936 July 14 - .
- Birth of Robert Franklin 'Bob' Overmyer - .
Nation: USA.
Related Persons: Overmyer.
American test pilot astronaut 1966-1986. 2 spaceflights, 12.1 days in space. Flew to orbit on STS-5 (1982), STS-51B..
1941 July 14 - .
- Birth of Tatyana Dmitryevna nee Pitskhelauri Kuznetsova - .
Nation: Russia.
Related Persons: Kuznetsova.
Russian pilot cosmonaut, 1962-1969..
1946 July 14 - .
LV Family:
V-2.
Launch Vehicle:
R-1.
- First rocket unit of Soviet military formed. - .
Nation: Russia.
Decree 'On establishment of BON of Fourth Directorate of GAU in Ministry of Armed Forces' was issued..
1948 July 14 - .
- Samolyot 5 rocketplane first flight. - .
Crew: Pakhomov.
Nation: Russia.
Related Persons: Pakhomov.
Spacecraft Bus: Russian Rocket Fighters.
Spacecraft: Samolyot 5.
The first 5-1 aircraft, controlled on its first glide flight by A K Pakhomov, was dropped from a Pe-8 bomber..
1948 July 14 - .
01:05 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC33.
LV Family:
Atlas.
Launch Vehicle:
Hiroc.
FAILURE: Cutoff after half of the propellants were used..
Failed Stage: 1.
- MX-774 Flight 1 - .
Nation: USA.
Agency: USAF.
Apogee: 1.00 km (0.60 mi). First Convair MX-774 (RTV-A-2) test rocket was successfully launched, first demonstrating use of gimballed engines and design features later incorporated in the Atlas ICBM. This was the first of three Convair-sponsored test flights..
1949 July 14 - .
- First successful Soviet atomic test - .
Nation: Russia.
1950 July 14 - .
08:39 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC35.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee XASR-SC-1.
- Grenades Aeronomy mission - .
Nation: USA.
Agency: US Army.
Apogee: 69 km (42 mi). Temperature, winds research. Launched at 0139 local time. Reached 69.2 km..
1951 July 14 - .
- Birth of Esther Dyson - .
Nation: Switzerland,
USA.
Related Persons: Dyson.
American cosmonaut, 2008-2009. Internet entrepreneur, daughter of physicist and space visionary Freeman Dyson. Internet entrepreneur who paid $ 3 million to train as back-up to Charles Simonyi as a space tourist aboard Soyuz TMA-14..
1953 July 14 - .
15:30 GMT - .
Launch Site:
Holloman.
Launch Complex:
Holloman A.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee RTV-A-1a.
- Solar flux Solar ultraviolet mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 103 km (64 mi). Solar radiation research. Launched at 0830 local time. Reached 103 km..
1959 July 14 - .
03:40 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
LV Family:
V-2.
Launch Vehicle:
R-2A.
- Ionosphere / aeronomy mission - .
Nation: Russia.
Agency: MVS.
Apogee: 203 km (126 mi).
1959 July 14 - .
17:45 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LC-A.
LV Family:
Asp.
Launch Vehicle:
Nike Asp.
- Solar x-ray mission - .
Nation: USA.
Agency: USN.
Apogee: 200 km (120 mi).
1960 July 14 - .
02:43 GMT - .
Launch Site:
Wallops Island.
LV Family:
Honest John.
Launch Vehicle:
Strongarm.
FAILURE: Failure.
- Ionosphere mission - .
Nation: USA.
Agency: USA BRL.
Apogee: 710 km (440 mi).
1960 July 14 - .
10:05 GMT - .
Launch Site:
Eglin.
LV Family:
Deacon.
Launch Vehicle:
Nike Cajun.
- Firefly FRANCES Aeronomy mission - .
Nation: USA.
Agency: USAF.
Apogee: 148 km (91 mi).
1961 July 14 - .
02:57 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Magnetic Fields Magnetosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 196 km (121 mi).
1961 July 14 - .
15:00 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Magnetic Fields Magnetosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 200 km (120 mi).
1961 July 14 - .
16:02 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Cajun.
- Grenades Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 101 km (62 mi).
1962 July 14 - .
- Titov again - .
Nation: Russia.
Related Persons: Titov.
Titov is involved in another automobile accident at 4 am in the morning. Kamanin tries to contact him, but he has gone to Kiev and won't return his calls. .
1963 July 14 - .
21:03 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Eclipse cal Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 172 km (106 mi).
1964 July 14 - .
- Douglas six-man space research station. - .
Nation: USA.
Spacecraft: MORL.
A study submitted to NASA by Douglas Aircraft Company concluded that a six-man space research station, capable of orbiting for one year, could be orbiting the Earth within five years. The crew, serving on a staggered schedule, would travel to and from the station on modified Gemini or Apollo spacecraft. The station would provide a small degree of artificial gravity by rotating slowly and would include a centrifuge to simulate reentry forces.
1964 July 14 - .
03:00 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA2.
LV Family:
Lupus.
Launch Vehicle:
HAD.
- Aeronomy mission - .
Nation: Australia.
Agency: WRE.
Apogee: 122 km (75 mi).
1965 July 14 - .
1965 July 14 - .
11:08 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA2.
Launch Pad: LA2 SL.
Launch Vehicle:
Skylark.
1966 July 14 - .
Launch Site:
Green River.
Launch Complex:
Green River Pad 2.
LV Family:
Athena RTV.
Launch Vehicle:
Athena RTV.
- ARPA C015 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF.
Apogee: 200 km (120 mi).
1966 July 14 - .
Launch Site:
Shijiedu.
LV Family:
T-7.
Launch Vehicle:
T-7A-S2.
- Life Science (dog) Biological mission - .
Nation: China.
Agency: Shanghai.
Apogee: 100 km (60 mi).
1966 July 14 - .
02:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576B3.
LV Family:
Atlas.
Launch Vehicle:
Atlas D.
FAILURE: Partial Failure..
Failed Stage: 1.
- OV1-07 - .
Payload: PasComSat. Mass: 10 kg (22 lb). Nation: USA.
Agency: USAF OAR.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: OV1.
Decay Date: 1978-01-04 . USAF Sat Cat: 2324 . COSPAR: 1966-063A. Apogee: 1,022 km (635 mi). Perigee: 985 km (612 mi). Inclination: 144.20 deg. Period: 105.20 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
- OV1-08 PasComSat - .
Mass: 555 kg (1,223 lb). Nation: USA.
Agency: USAF AFSC.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: OV1.
Decay Date: 1978-01-04 . USAF Sat Cat: 2324 . COSPAR: 1966-063xx. Apogee: 410 km (250 mi). Perigee: 393 km (244 mi). Inclination: 144.20 deg. Period: 92.60 min.
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 14 - .
15:15 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 195 km (121 mi).
1967 July 14 - .
Launch Site:
Whiteman AFB.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
- Whiteman AFB - .
The final squadron of Wing IV at Whiteman AFB was received from SAC's 351st Strategic Missile Wing for Force Modernization..
1967 July 14 - .
Launch Site:
Green River.
Launch Complex:
Green River Pad 2.
LV Family:
Athena RTV.
Launch Vehicle:
Athena RTV.
- USAF D050 re-entry vehicle test flight - .
Nation: USA.
Agency: USAF.
Apogee: 200 km (120 mi).
1967 July 14 - .
11:53 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC36A.
LV Family:
Atlas.
Launch Vehicle:
Atlas Centaur D.
- Surveyor 4 - .
Payload: Surveyor SC-4. Mass: 283 kg (623 lb). Nation: USA.
Agency: JPL,
NASA.
Class: Moon.
Type: Lunar probe. Spacecraft: Surveyor.
Decay Date: 1967-07-17 . USAF Sat Cat: 2875 . COSPAR: 1967-068A. Soft lunar landing attempt failed..
1969 July 14 - .
23:53 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA2.
Launch Pad: LA2 SL.
Launch Vehicle:
Skylark.
- Electron profile Ionosphere mission - .
Nation: UK.
Agency: BAC.
Apogee: 216 km (134 mi).
1970 July 14 - .
1970 July 14 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF09.
Launch Pad: LF09?.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- FOT GT71B-2 Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1970 July 14 - .
04:52 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA2.
Launch Pad: LA2 SL.
LV Family:
Skylark.
Launch Vehicle:
Skylark 6.
- X-ray RMC X-ray astronomy mission - .
Nation: UK.
Agency: BAC.
Apogee: 223 km (138 mi).
1970 July 14 - .
07:04 GMT - .
Launch Pad: Atlantic Ocean, 39.0 N x 30.0 W.
Launch Platform: VISE.
Launch Vehicle:
MR-12.
- Ionosphere mission - .
Nation: Russia.
Apogee: 171 km (106 mi).
1971 July 14 - .
21:00 GMT - .
Launch Site:
South Uist.
Launch Vehicle:
Petrel.
- Electron analyser Ionosphere mission - .
Nation: UK.
Agency: SRC.
Apogee: 143 km (88 mi).
1971 July 14 - .
22:04 GMT - .
Launch Site:
South Uist.
Launch Vehicle:
Petrel.
- Electron analyser Ionosphere mission - .
Nation: UK.
Agency: SRC.
Apogee: 142 km (88 mi).
1972 July 14 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC142/34.
LV Family:
R-36.
Launch Vehicle:
R-36 8K67MA.
- State trials missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1972 July 14 - .
06:01 GMT - .
Launch Site:
White Sands.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 170.
- Astronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 200 km (120 mi).
1974 July 14 - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan LA2B.
LV Family:
CZ.
Launch Vehicle:
Feng Bao 1.
FAILURE: Vehicle lost attitude stability and destroyed by range safety..
Failed Stage: G.
- JSSW 2 - .
Payload: JSSW 2. Mass: 1,100 kg (2,400 lb). Nation: China.
Agency: PRC.
Spacecraft: JSSW.
1974 July 14 - .
05:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas F/PTS.
1975 July 14 - .
14:04 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC43.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Arcasonde - .
Nation: USA.
Agency: MRN.
Apogee: 63 km (39 mi).
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..
1977 July 14 - .
- Deliver third main engine to NSTL (MPTA-098) - .
Nation: USA.
Program: STS.
1977 July 14 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: UK S22.
LV Family:
Polaris.
Launch Vehicle:
Polaris A3.
- Demonstration and shakedown operations launch - .
Nation: UK.
Agency: RN.
Apogee: 1,000 km (600 mi).
1977 July 14 - .
10:39 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Delta 2914.
1978 July 14 - .
10:43 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17A.
LV Family:
Thor.
Launch Vehicle:
Delta 2914.
- ESA-Geos 2 - .
Payload: ESA GEOS 2. Mass: 573 kg (1,263 lb). Nation: Europe.
Agency: ESA.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: ESA-Geos.
Completed Operations Date: 1984-01-24 . USAF Sat Cat: 10981 . COSPAR: 1978-071A. Apogee: 36,049 km (22,399 mi). Perigee: 36,027 km (22,386 mi). Inclination: 14.60 deg. Period: 1,449.00 min.
Magnetospheric research. European Space Agency satellite. Launch time 1043 GMT. Reached initial operational position of 6 deg East on 26 Jul 1978. During the two years of its mission, it will be maintained in position between longitude 0 and 35 deg east in geosynchronous orbit. Positioned in geosynchronous orbit over the Atlantic Ocean at 36 deg E in 1978-1979 over the Atlantic Ocean 6-36 deg E in 1979-1981; over the Atlantic Ocean 24 deg E in 1981; over the Atlantic Ocean 33-37 deg E in 1981-1984 As of 3 September 2001 located at 177.77 deg W drifting at 3.212 deg W per day. As of 2007 Mar 9 located at 179.12E drifting at 3.212W degrees per day.
1978 July 14 - .
15:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Molniya 1-41 - .
Payload: Molniya-1T. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MOM.
Program: Molniya.
Class: Communications.
Type: Military communications satellite. Spacecraft Bus: KAUR-2.
Spacecraft: Molniya-1T.
Decay Date: 1992-02-08 . USAF Sat Cat: 10984 . COSPAR: 1978-072A. Apogee: 38,306 km (23,802 mi). Perigee: 260 km (160 mi). Inclination: 61.80 deg. Period: 681.90 min. Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of the long-range telephone and telegraph radiocommunications system in the USSR; transmission of television programmes to stations in the Orbita network..
1979 July 14 - .
18:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 657.
LV Family:
Trident.
Launch Vehicle:
Trident C-4.
- PEM-4 test launch - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1980 July 14 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg.
- Fifth and final launch of a Thor/Block 5D-I - .
Nation: USA.
Fifth and final launch of a Thor/Block 5D-I from Vandenberg AFB (first launch on 11 September 1976)..
1980 July 14 - .
22:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 634.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- DASO-48 demonstration and shakedown operations launch - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1980 July 14 - .
22:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM.
1982 July 14 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg BOM2.
Launch Vehicle:
Bomarc.
- Target - .
Nation: USA.
Agency: USN.
Apogee: 20 km (12 mi). Last two launches of the Navy's Bomarc target missile from Vandenberg AFB (first Bomarc launch from Vandenberg on 25 August 19656)..
1983 July 14 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
LV Family:
R-36M.
Launch Vehicle:
R-36M 15A14.
- Joint flight trials launch - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1983 July 14 - .
10:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Atlas.
Launch Vehicle:
Atlas E/SGS-2.
- Navstar 8 - .
Payload: GPS SVN 8 / OPS 9794. Mass: 770 kg (1,690 lb). Nation: USA.
Agency: USAF.
Manufacturer: Seal Beach.
Program: Navstar.
Class: Navigation.
Type: Navigation satellite. Spacecraft Bus: Navstar.
Spacecraft: GPS Block 1.
USAF Sat Cat: 14189 . COSPAR: 1983-072A. Apogee: 21,229 km (13,191 mi). Perigee: 20,757 km (12,897 mi). Inclination: 64.20 deg. Period: 751.10 min. Global Positioning System..
1985 July 14 - .
15:05 GMT - .
Launch Site:
Barking Sands.
Launch Complex:
Barking Sands KP.
LV Family:
Malemute.
Launch Vehicle:
Terrier Malemute.
- ACE I Target - .
Nation: USA.
Agency: Lincoln,
SDIO.
Type: ABM Target. Apogee: 497 km (308 mi).
1987 July 14 - .
08:11 GMT - .
Launch Site:
Andoya.
LV Family:
Viper.
Launch Vehicle:
Viper 3A.
- MAC-SINE S-F19 Aeronomy mission - .
Nation: USA.
Agency: DLR.
Apogee: 108 km (67 mi).
1987 July 14 - .
08:32 GMT - .
Launch Site:
Andoya.
LV Family:
Viper.
Launch Vehicle:
Viper 3A.
- MAC-SINE S-F20 Aeronomy mission - .
Nation: USA.
Agency: DLR.
Apogee: 115 km (71 mi).
1987 July 14 - .
11:02 GMT - .
Launch Site:
Andoya.
LV Family:
Viper.
Launch Vehicle:
Viper 3A.
- MAC-SINE S-F21 Aeronomy mission - .
Nation: USA.
Agency: DLR.
Apogee: 116 km (72 mi).
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..
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..
1992 July 14 - .
22:02 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/23.
LV Family:
Proton.
Launch Vehicle:
Proton-K/DM-2.
1993 July 14 - .
03:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF05.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 1,000 km (600 mi).
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..
1994 July 14 - .
05:13 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Nadezhda 4 - .
Payload: Tsikada-Kospas. Mass: 825 kg (1,818 lb). Nation: Russia.
Agency: MO.
Class: Navigation.
Type: Navigation satellite. Spacecraft Bus: KAUR-1.
Spacecraft: Nadezhda.
USAF Sat Cat: 23179 . COSPAR: 1994-041A. Apogee: 1,007 km (625 mi). Perigee: 951 km (590 mi). Inclination: 82.94 deg. Period: 104.68 min. Carried COSPAS/SARSAT search and rescue package. Civilian navigation satellite. Positioned in plane 14 of constellation. Maritime navigation. Signals at 150,00 MHz and 400.00 MHz..
1995 July 14 - .
03:56 GMT - .
1996 July 14 - .
07:15 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC36.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant 9CM1.
- NUVIEWS 1 Ultraviolet astronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 300 km (180 mi).
1999 July 14 - .
03:28 GMT - .
Launch Site:
Andoya.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant VA.
- MD-DR-13 DROPPS-2 Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 118 km (73 mi).
2000 July 14 - .
05:21 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC36B.
Launch Pad: SLC36B.
LV Family:
Atlas.
Launch Vehicle:
Atlas IIAS.
- Echostar 6 - .
Mass: 3,700 kg (8,100 lb). Nation: USA.
Agency: PanAmSat.
Manufacturer: Palo Alto.
Program: Echostar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: FS-1300.
USAF Sat Cat: 26402 . COSPAR: 2000-038A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Communications satellite, positioned in geosynchronous orbit at 149 deg W. By 5 September 2001 located at 119.07 deg W drifting at 0.002 deg W per day. As of 2007 Mar 10 located at 110.39W drifting at 0.006W degrees per day..
2001 July 14 - .
- STS-104 Mission Status Report #05 - .
Nation: USA.
Related Persons: Gernhardt,
Helms,
Hobaugh,
Kavandi,
Lindsey,
Reilly,
Voss.
Program: ISS.
Flight: STS-102 ISS EO-2,
STS-104.
Atlantis Commander Steve Lindsey smoothly docked the space shuttle with the International Space Station late Friday about 240 statute miles above the northeastern coast of South America. With both spacecraft moving at about 17,500 mph, Lindsey moved Atlantis to the station at a relative speed of about a tenth of a foot per second. Docking occurred at 10:08 p.m. CDT. Additional Details: here....
2001 July 14 - .
- STS-104 - Wakeup Song: Space Cowboy - .
Flight: STS-104.
"Space Cowboy" by N'Sync for Mission Specialist Janet Kavandi..
2002 July 14 - .
01:34 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA1.
LV Family:
SB-735.
Launch Vehicle:
NAL-735.
FAILURE: Failure.
- National Experimental Supersonic Transport NEXST-1 test - .
Nation: Japan.
Agency: NAL.
Apogee: 0 km (0 mi). The intention was that an 11.5-m-long, one tenth scale model of the aircraft would be propelled by the NAL-735 solid rocket booster to Mach 2 at 18 km altitude. Instead the vehicle lost stability and crashed near the launch point..
2005 July 14 - .
- Cassini, Enceladus Flyby, Successful - .
Nation: USA.
Spacecraft: Cassini.
2006 July 14 - .
- STS-121 MCC Status Report #20 - .
Nation: USA.
Related Persons: Fossum,
Kelly, Mark,
Lindsey,
Nowak,
Reiter,
Sellers,
Vinogradov,
Williams, Jeffrey,
Wilson.
Program: ISS.
Flight: Soyuz TMA-8,
STS-121,
STS-121 Astrolab.
It's back to work for the Space Shuttle Discovery crew..
Additional Details: here....
2006 July 14 - .
- STS-121 - Wakeup Song: Aggie War Hymn - .
Flight: STS-121.
"Aggie War Hymn" by the The Fightin' Texas Aggie Band for Mission Specialist Mike Fossum, a graduate of Texas A&M University. According to Mission Control, the selection was sent by Fossum's wife. He is the first Texas A&M graduate in space ..
2009 July 14 - .
Launch Site:
North Pole.
Launch Platform: TK-208.
LV Family:
Topol'.
Launch Vehicle:
Bulava.
- Sineva Test - .
Nation: Russia.
Apogee: 1,000 km (600 mi). Test.
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..
2014 July 14 - .
15:15 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
Launch Pad: SLC40.
LV Family:
Falcon.
Launch Vehicle:
Falcon 9.
- Orbcomm FM 107 - .
Mass: 172 kg (379 lb). Nation: USA.
Agency: SPX.
Spacecraft: SN-100.
USAF Sat Cat: 40087 . COSPAR: 2014-040B. Apogee: 738 km (458 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.32 min.
- Orbcomm FM 106 - .
Mass: 172 kg (379 lb). Nation: USA.
Agency: SPX.
Spacecraft: SN-100.
USAF Sat Cat: 40088 . COSPAR: 2014-040C. Apogee: 739 km (459 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.33 min.
- Orbcomm FM 111 - .
Mass: 172 kg (379 lb). Nation: USA.
Agency: SPX.
Spacecraft: SN-100.
USAF Sat Cat: 40089 . COSPAR: 2014-040D. Apogee: 740 km (450 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.35 min.
- Orbcomm FM 104 - .
Mass: 172 kg (379 lb). Nation: USA.
Agency: SPX.
Spacecraft: SN-100.
USAF Sat Cat: 40090 . COSPAR: 2014-040E. Apogee: 740 km (450 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.35 min.
- Orbcomm FM 103 - .
Mass: 172 kg (379 lb). Nation: USA.
Agency: SPX.
Spacecraft: SN-100.
USAF Sat Cat: 40091 . COSPAR: 2014-040F. Apogee: 741 km (460 mi). Perigee: 620 km (380 mi). Inclination: 47.01 deg. Period: 98.37 min.
2015 July 14 - .
- New Horizons flies by Pluto. - .
2015 July 14 - .
04:31 GMT - .
Launch Platform: ISS.
- 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..
2017 July 14 - .
06:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1A.
- Kanopus-V-IK No. 2 - .
Nation: Russia.
USAF Sat Cat: 42825 . COSPAR: 2017-042A. Apogee: 510 km (310 mi). Perigee: 507 km (315 mi). Inclination: 97.45 deg. Period: 94.79 min. See Kanopus-V-IK 1. ..
- NORSAT-1 - .
Nation: TBD.
USAF Sat Cat: 42826 . COSPAR: 2017-042B. Apogee: 606 km (376 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.59 min. See NORSAT 1. ..
- Flock 2k-43 - .
Payload: Dove 1056; FLOCK 2K 43. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42874 . COSPAR: 2017-042BB. Apogee: 468 km (290 mi). Perigee: 451 km (280 mi). Inclination: 96.96 deg. Period: 93.79 min. See Flock-2k 43 (Dove 1056). ..
- Flock 2k-3 - .
Payload: Dove 0F21; FLOCK 2K 03. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42850 . COSPAR: 2017-042AB. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 3 (Dove 0F21). ..
- Flock 2k-4 - .
Payload: Dove 0F24; FLOCK 2K 04. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42851 . COSPAR: 2017-042AC. Apogee: 457 km (283 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.58 min. See Flock-2k 4 (Dove 0F24). ..
- Flock 2k-41 - .
Payload: Dove 1054; FLOCK 2K 41. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42875 . COSPAR: 2017-042BC. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 41 (Dove 1054). ..
- Iskra-MAI-85 - .
Nation: TBD.
USAF Sat Cat: 42827 . COSPAR: 2017-042C. Apogee: 606 km (376 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.58 min. See Iskra-MAI-85. ..
- NORSAT-2 - .
Nation: TBD.
USAF Sat Cat: 42828 . COSPAR: 2017-042D. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See NORSAT 2. ..
- Flock 2k-36 - .
Payload: Dove 104F; FLOCK 2K 36. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42876 . COSPAR: 2017-042BD. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 36 (Dove 104F). ..
- Flock 2k-1 - .
Payload: Dove 0F1A; FLOCK 2K 01. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42852 . COSPAR: 2017-042AD. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 1 (Dove 0F1A). ..
- Technosat - .
Nation: Germany.
USAF Sat Cat: 42829 . COSPAR: 2017-042E. Apogee: 606 km (376 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.58 min. See TechnoSat (Tubsat 12). ..
- Flock 2k-2 - .
Payload: Dove 0F1E; FLOCK 2K 02. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42853 . COSPAR: 2017-042AE. Apogee: 465 km (288 mi). Perigee: 450 km (270 mi). Inclination: 96.96 deg. Period: 93.75 min. See Flock-2k 2 (Dove 0F1E). ..
- Flock 2k-35 - .
Payload: Dove 104E; FLOCK 2K 35. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42877 . COSPAR: 2017-042BE. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 35 (Dove 104E). ..
- Mayak - .
Nation: TBD.
USAF Sat Cat: 42830 . COSPAR: 2017-042F. Apogee: 604 km (375 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.54 min. See Mayak. ..
- Flock 2k-47 - .
Payload: Dove 1043; FLOCK 2K 47. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42854 . COSPAR: 2017-042AF. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 47 (Dove 1043). ..
- Flock 2k-34 - .
Payload: Dove 104D; FLOCK 2K 34. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42878 . COSPAR: 2017-042BF. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 34 (Dove 104D). ..
- Flock 2k-48 - .
Payload: Dove 101C; FLOCK 2K 48. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42855 . COSPAR: 2017-042AG. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 48 (Dove 101C). ..
- FLP - .
Payload: Flying Laptop. Nation: Germany.
USAF Sat Cat: 42831 . COSPAR: 2017-042G. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.58 min. See Flying Laptop. ..
- Flock 2k-33 - .
Payload: Dove 104C; FLOCK 2K 33. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42879 . COSPAR: 2017-042BG. Apogee: 454 km (282 mi). Perigee: 439 km (272 mi). Inclination: 96.96 deg. Period: 93.51 min. See Flock-2k 33 (Dove 104C). ..
- Flock 2k-28 - .
Payload: Dove 1047; FLOCK 2K 28. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42880 . COSPAR: 2017-042BH. Apogee: 468 km (290 mi). Perigee: 452 km (280 mi). Inclination: 96.96 deg. Period: 93.79 min. See Flock-2k 28 (Dove 1047). ..
- Flock 2k-45 - .
Payload: Dove 100D; FLOCK 2K 45. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42856 . COSPAR: 2017-042AH. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 45 (Dove 100D). ..
- Ekvador-UTE-YuZGU - .
Payload: UTE-UESOR. Nation: TBD.
USAF Sat Cat: 42832 . COSPAR: 2017-042H. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See UTE-UESOR (Ecuador-UTE-YuZGU). ..
- Flock 2k-24 - .
Payload: Dove 0F4F; FLOCK 2K 24. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42857 . COSPAR: 2017-042AJ. Apogee: 457 km (283 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 24 (Dove 0F4F). ..
- Lemur-2-ArtFisher - .
Payload: Lemur-2-43; LEMUR 2 ARTFISCHER. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42881 . COSPAR: 2017-042BJ. Apogee: 461 km (286 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.64 min. See Lemur-2 43 (Lemur-2 ArtFischer). ..
- MKA-N 1 - .
Payload: MKA-N No. 1. Nation: TBD.
USAF Sat Cat: 42834 . COSPAR: 2017-042K. Apogee: 605 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See MKA-N 1. ..
- Flock 2k-27 - .
Payload: Dove 0F54; FLOCK 2K 27. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42882 . COSPAR: 2017-042BK. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 27 (Dove 0F54). ..
- Flock 2k-46 - .
Payload: Dove 103F; FLOCK 2K 46. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42858 . COSPAR: 2017-042AK. Apogee: 457 km (283 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.60 min. See Flock-2k 46 (Dove 103F). ..
- Flock 2k-23 - .
Payload: Dove 0F4B; FLOCK 2K 23. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42859 . COSPAR: 2017-042AL. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 23 (Dove 0F4B). ..
- WNISAT-1R - .
Nation: Japan.
USAF Sat Cat: 42835 . COSPAR: 2017-042L. Apogee: 605 km (375 mi). Perigee: 585 km (363 mi). Inclination: 97.58 deg. Period: 96.57 min. See WNISAT 1R. ..
- Flock 2k-26 - .
Payload: Dove 0F53; FLOCK 2K 26. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42883 . COSPAR: 2017-042BL. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 26 (Dove 0F53). ..
- Flock 2k-25 - .
Payload: Dove 0F4D; FLOCK 2K 25. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42884 . COSPAR: 2017-042BM. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 25 (Dove 0F4D). ..
- Flock 2k-21 - .
Payload: Dove 0F49; FLOCK 2K 21. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42860 . COSPAR: 2017-042AM. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 21 (Dove 0F49). ..
- MKA-N 2 - .
Payload: MKA-N No. 2. Nation: TBD.
USAF Sat Cat: 42836 . COSPAR: 2017-042M. Apogee: 604 km (375 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.57 min. See MKA-N 2. ..
- Flock 2k-20 - .
Payload: Dove 0F47; FLOCK 2K 20. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42885 . COSPAR: 2017-042BN. Apogee: 459 km (285 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 20 (Dove 0F47). ..
- Lemur-2-Greenberg - .
Payload: Lemur-2-42; LEMUR 2 GREENBERG. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42837 . COSPAR: 2017-042N. Apogee: 602 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.53 min. See Lemur-2 42 (Lemur-2 Greenberg). ..
- Flock 2k-22 - .
Payload: Dove 0F4A; FLOCK 2K 22. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42861 . COSPAR: 2017-042AN. Apogee: 455 km (282 mi). Perigee: 442 km (274 mi). Inclination: 96.96 deg. Period: 93.55 min. See Flock-2k 22 (Dove 0F4A). ..
- Lemur-2-AndiS - .
Payload: Lemur-2-47; LEMUR 2 ANDIS. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42838 . COSPAR: 2017-042P. Apogee: 602 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.53 min. See Lemur-2 47 (Lemur-2 AndiS). ..
- Flock 2k-7 - .
Payload: Dove 0F2B; FLOCK 2K 07. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42862 . COSPAR: 2017-042AP. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 7 (Dove 0F2B). ..
- Flock 2k-19 - .
Payload: Dove 0F46; FLOCK 2K 19. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42886 . COSPAR: 2017-042BP. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 19 (Dove 0F46). ..
- Flock 2k-18 - .
Payload: Dove 0F44; FLOCK 2K 18. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42887 . COSPAR: 2017-042BQ. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 18 (Dove 0F44). ..
- Flock 2k-8 - .
Payload: Dove 0F2D; FLOCK 2K 08. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42863 . COSPAR: 2017-042AQ. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 8 (Dove 0F2D). ..
- Lemur-2-Monson - .
Payload: Lemur-2-44; LEMUR 2 MONSON. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42839 . COSPAR: 2017-042Q. Apogee: 603 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.54 min. See Lemur-2 44 (Lemur-2 Monson). ..
- Flock 2k-17 - .
Payload: Dove 0F40; FLOCK 2K 17. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42888 . COSPAR: 2017-042BR. Apogee: 458 km (284 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.59 min. See Flock-2k 17 (Dove 0F40). ..
- Flock 2k-5 - .
Payload: Dove 0F29; FLOCK 2K 05. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42864 . COSPAR: 2017-042AR. Apogee: 456 km (283 mi). Perigee: 442 km (274 mi). Inclination: 96.96 deg. Period: 93.57 min. See Flock-2k 5 (Dove 0F29). ..
- Lemur-2-Furiaus - .
Payload: Lemur-2-45; LEMUR 2 FURIAUS. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42840 . COSPAR: 2017-042R. Apogee: 602 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.53 min. See Lemur-2 45 (Lemur-2 Furiaus). ..
- Flock 2k-40 - .
Payload: Dove 1053; FLOCK 2K 40. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42865 . COSPAR: 2017-042AS. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 40 (Dove 1053). ..
- Flock 2k-16 - .
Payload: Dove 0F3D; FLOCK 2K 16. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42889 . COSPAR: 2017-042BS. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 16 (Dove 0F3D). ..
- Lemur-2-PeterG - .
Payload: Lemur-2-48; LEMUR 2 PETERG. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42841 . COSPAR: 2017-042S. Apogee: 601 km (373 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.52 min. See Lemur-2 48 (Lemur-2 PeterG). ..
- Flock 2k-15 - .
Payload: Dove 0F3C; FLOCK 2K 15. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42890 . COSPAR: 2017-042BT. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 15 (Dove 0F3C). ..
- Flock 2k-39 - .
Payload: Dove 1052; FLOCK 2K 39. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42866 . COSPAR: 2017-042AT. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 39 (Dove 1052). ..
- Lemur-2-Dembitz - .
Payload: Lemur-2-49; LEMUR 2 DEMBITZ. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42842 . COSPAR: 2017-042T. Apogee: 601 km (373 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.51 min. See Lemur-2 49 (Lemur-2 Dembitz). ..
- Flock 2k-13 - .
Payload: Dove 0F37; FLOCK 2K 13. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42891 . COSPAR: 2017-042BU. Apogee: 457 km (283 mi). Perigee: 442 km (274 mi). Inclination: 96.96 deg. Period: 93.58 min. See Flock-2k 13 (Dove 0F37). ..
- Flock 2k-37 - .
Payload: Dove 1050; FLOCK 2K 37. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42867 . COSPAR: 2017-042AU. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 37 (Dove 1050). ..
- CICERO-1 - .
Nation: TBD.
USAF Sat Cat: 42843 . COSPAR: 2017-042U. Apogee: 603 km (374 mi). Perigee: 583 km (362 mi). Inclination: 97.58 deg. Period: 96.54 min. See CICERO 1. ..
- Flock 2k-38 - .
Payload: Dove 1051; FLOCK 2K 38. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42868 . COSPAR: 2017-042AV. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 38 (Dove 1051). ..
- NanoACE - .
Nation: USA.
USAF Sat Cat: 42844 . COSPAR: 2017-042V. Apogee: 601 km (373 mi). Perigee: 582 km (361 mi). Inclination: 97.58 deg. Period: 96.52 min. See NanoACE. ..
- Flock 2k-14 - .
Payload: Dove 0F3B; FLOCK 2K 14. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42892 . COSPAR: 2017-042BV. Apogee: 459 km (285 mi). Perigee: 443 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 14 (Dove 0F3B). ..
- Flock 2k-31 - .
Payload: Dove 104A; FLOCK 2K 31. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42869 . COSPAR: 2017-042AW. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 31 (Dove 104A). ..
- Flock 2k-12 - .
Payload: Dove 0F36; FLOCK 2K 12. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42893 . COSPAR: 2017-042BW. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 12 (Dove 0F36). ..
- Lemur-2-Zachary - .
Payload: Lemur-2-46; LEMUR 2 ZACHARY. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42845 . COSPAR: 2017-042W. Apogee: 601 km (373 mi). Perigee: 581 km (361 mi). Inclination: 97.58 deg. Period: 96.50 min. See Lemur-2 46 (Lemur-2 Zachary). ..
- Flock 2k-32 - .
Payload: Dove 104B; FLOCK 2K 32. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42870 . COSPAR: 2017-042AX. Apogee: 458 km (284 mi). Perigee: 445 km (276 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 32 (Dove 104B). ..
- Landmapper-BC2 - .
Payload: Corvus-BC 2; CORVUS BC2. Nation: USA.
USAF Sat Cat: 42846 . COSPAR: 2017-042X. Apogee: 599 km (372 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.52 min. See Landmapper-BC 2 (Corvus-BC 2). ..
- Flock 2k-11 - .
Payload: Dove 0F33; FLOCK 2K 11. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42894 . COSPAR: 2017-042BX. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 11 (Dove 0F33). ..
- Landmapper-BC1 - .
Payload: Corvus-BC 1; CORVUS BC1. Nation: USA.
USAF Sat Cat: 42847 . COSPAR: 2017-042Y. Apogee: 599 km (372 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.51 min. See Landmapper-BC 1 (Corvus-BC 1). ..
- Flock 2k-29 - .
Payload: Dove 1048; FLOCK 2K 29. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42871 . COSPAR: 2017-042AY. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 29 (Dove 1048). ..
- Flock 2k-10 - .
Payload: Dove 0F32; FLOCK 2K 10. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42895 . COSPAR: 2017-042BY. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 10 (Dove 0F32). ..
- Flock 2k-30 - .
Payload: Dove 1049; FLOCK 2K 30. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42872 . COSPAR: 2017-042AZ. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 30 (Dove 1049). ..
- CICERO-2 - .
Nation: TBD.
USAF Sat Cat: 42848 . COSPAR: 2017-042Z. Apogee: 597 km (370 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.50 min. See CICERO 2. ..
- Flock 2k-9 - .
Payload: Dove 0F2E; FLOCK 2K 09. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42896 . COSPAR: 2017-042BZ. Apogee: 456 km (283 mi). Perigee: 441 km (274 mi). Inclination: 96.96 deg. Period: 93.56 min. See Flock-2k 9 (Dove 0F2E). ..
- Flock 2k-6 - .
Payload: Dove 0F2A; FLOCK 2K 06. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42897 . COSPAR: 2017-042CA. Apogee: 458 km (284 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.62 min. See Flock-2k 6 (Dove 0F2A). ..
- Flock 2k-44 - .
Payload: Dove 1020; FLOCK 2K 44. Nation: USA.
Spacecraft: Cubesat.
USAF Sat Cat: 42873 . COSPAR: 2017-042BA. Apogee: 459 km (285 mi). Perigee: 444 km (275 mi). Inclination: 96.96 deg. Period: 93.61 min. See Flock-2k 44 (Dove 1020). ..
- CICERO-3 - .
Nation: TBD.
USAF Sat Cat: 42849 . COSPAR: 2017-042AA. Apogee: 597 km (370 mi). Perigee: 584 km (362 mi). Inclination: 97.58 deg. Period: 96.49 min. See CICERO 3. ..
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