1999 July 1 -
1999 July 1 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Malemute. LV Configuration: Malemute TMBD Target. -
Malemute II Slugger Target mission Nation: USA. Agency: USN. Apogee: 120 km (70 mi). References: 2.
1999 July 5 - 03:57 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.116GE. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 250 km (150 mi). References: 2.
1999 July 5 - 04:02 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: Taurus Orion. LV Configuration: Taurus Orion NASA 33.065UE. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1999 July 5 - 13:32 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/Briz-M. LV Configuration: Proton-K/Briz-M 389-01. FAILURE: Second stage explosion. -
Raduga Nation: Russia. Payload: Raduga s/n 45L. Class: Communications. Spacecraft: Raduga. Agency: RVSN. Apogee: 30 km (18 mi). COSPAR: F990705A. Carried a Russian Defence Ministry communications satellite. First attempted flight of the Khrunichev Briz-M upper stage in place of the usual Block DM. After the second stage explosion the remainder of the vehicle survived for 45 seconds before breaking up. Debris landed near Karaganda. As a result of this accident the Kazakh government suspended launches from Baikonur pending Russian agreement to pay back part of rent owed.
References: 2.
1999 July 5 - 23:36 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA NASA 21.123GE. -
MD-DR-04 DROPPS-1 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi). References: 2.
1999 July 8 - 08:45 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML. -
Molniya-3-50 Nation: Russia. Payload: Molniya-3 s/n 63. Class: Communications. Spacecraft: Molniya-3. Manufacturer: NPO Prikladnoi Mekhaniki, Zhelenogorsk. Agency: MO RF. Perigee: 1,811 km (1,125 mi). Apogee: 38,540 km (23,940 mi). Inclination: 63.50 deg. Period: 717.70 min. COSPAR: 1999-036A. USAF Sat Cat: 25847. The launch was from one of the three active R-7 class pads at Plesetsk (LC16/pad 2, LC43/pad 3, LC43/pad 4) and used the 8K78M launch vehicle, consisting of the 11S59 core packet, the 11S510 Block I third stage, and the Block-ML upper stage. The Block ML and the payload were placed in a 62.8 degree low parking orbit and then the ML fired to deliver the payload to a 12-hour operational orbit. This was the 52nd Molniya-3 to be launched (two were orbited under the Cosmos designation).
References: 2.
1999 July 9 -
1999 July 10 - 08:45 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: SLC17B. Launch Vehicle: Delta. Model: Delta 7420-10C. LV Configuration: Delta 7420-10C D272. -
Globalstar 32 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,413 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-037A. USAF Sat Cat: 25851. References: 2.
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Globalstar 30 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,413 km (877 mi). Apogee: 1,415 km (879 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-037B. USAF Sat Cat: 25852. References: 2.
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Globalstar 35 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,413 km (877 mi). Apogee: 1,415 km (879 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-037C. USAF Sat Cat: 25853. References: 2.
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Globalstar 51 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,413 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-037D. USAF Sat Cat: 25854. References: 2.
1999 July 11 - -
Project 921-2 Go-Ahead Nation: China. Spacecraft: Project 921-2. China initiated the second phase of the National Manned Space program - Project 921-2. Phase 2 would focus on a manned 'space lab' and related key technologies. A China Academy of Science research team, including six subgroups on specific topics, was established in February 1999 to issue a requirements document. The new Shanghai Institute for Biological Sciences was also involved.
References: 424.
1999 July 14 - 03:28 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA NASA 21.124GE. -
MD-DR-13 DROPPS-2 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 118 km (73 mi). References: 2.
1999 July 16 - -
Chinese Manned Program Announcement Nation: China. Spacecraft: Shenzhou. Zhang Lihui, Director of Research and Development at the China Aerospace Science and Technology Corporation (CASC), said that a development plan for manned-space flight technology was issued by the Chinese State Council in 1992 and that China was on track to launch a manned space flight by early in the next century. This was the first direct official acknowledgement of such a program.
References: 424.
1999 July 16 - 16:37 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. LV Configuration: Soyuz 11A511U 667. -
Progress M-42 Nation: Russia. Program: Mir. Payload: Progress M s/n 242. Class: Manned. Type: Logistics. Spacecraft: Progress M. Manufacturer: RKK Energiya im. S.P. Korolyov, Kaliningrad-Korolyov. Agency: RAKA. Perigee: 340 km (210 mi). Apogee: 348 km (216 mi). Inclination: 51.60 deg. Period: 91.42 min. COSPAR: 1999-038A. USAF Sat Cat: 25858. Duration: 200.57 days. Decay Date: 2000-02-04. Flight: Mir EO-27, Mir EO-26/-27. Delivered supplies to the crew of the Mir complex. Docked with the Kvant port at 17:53 GMT on July 18. Remained docked to the station after the departure of the last operational crew in September 1999. Undocked on February 2. 2000, to clear the port for Progress M1, at 0311:52 GMT. Deorbited over
the Pacific later the same day at 0610:40 UTC with an 8 minute burn.
References: 2.
1999 July 17 - -
Mayflower aerodynamic mndel tests. Nation: USA. Program: X-Prize. Advent Launch Systems (Houston, Texas, USA) successfully tests aerodynamic
engineering prototype model.
1999 July 17 - 06:38 GMT - Launch Site: Baikonur. Launch Complex: LC45/1. Launch Pad: -. Launch Vehicle: Zenit. Model: Zenit-2. LV Configuration: Zenit-2 17L. -
Okean-O Nation: Russia. Program: Okean. Payload: Okean-O no. 1. Mass: 4,360 kg (9,610 lb). Class: Earth. Type: Landsat. Spacecraft: Okean-O. Manufacturer: KB Yuzhnoe (Pivdenne?), Dnepropetrovsk, Ukraine. Agency: RAKA. Perigee: 660 km (410 mi). Apogee: 663 km (411 mi). Inclination: 98.00 deg. COSPAR: 1999-039A. USAF Sat Cat: 25860. First of a new generation of larger Okean oceanographic satellites, carried a side-looking radar (RSL-BO), and a set of visible and infrared scanners and radiometers. It is built by the Ukrainian Yuzhnoye company and is a joint project of the Russian Aviation/Space Agency (RAKA) and the Ukrainian National Space Agency (NKAU).
References: 2.
1999 July 18 - -
New Tracking Ship Joins Yuan Wang Fleet Nation: China. Spacecraft: Shenzhou. A new space tracking ship, Yuan Wang 4, was delivered to China Satellite Launch and Tracking Control General by the China State Shipbuilding Corporation. This was the fourth tracking ship in China's Yuan Wang space tracking fleet. The Yuan Wang 4 tracking ship was converted from the scientific survey ship Xiang Yang Hong 10. The announcment also contained the second announcement that the fleet would deploy for a major new operation (a test of a manned spacecraft) within the next year. The Yuan Wang 4 was 156.09 m long, 20.6 m wide along the mold-line, and had a displacement of 10,895 tons.
References: 424.
1999 July 18 - 03:41 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: Taurus Orion. LV Configuration: Taurus Orion NASA 33.066UE. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1999 July 20 - -
Retrieval of Liberty Bell 7 Capsule From Ocean Floor Nation: USA. Flight: Mercury MR-5.
1999 July 23 - 04:31 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39B. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-93. -
STS-93 Nation: USA. Program: STS. Payload: Columbia F26 / Chandra. Class: Manned. Type: Spaceplane. Spacecraft: Columbia. Manufacturer: Boeing Reusable Space Systems, Palmdale. Agency: NASA JSC. Perigee: 276 km (171 mi). Apogee: 276 km (171 mi). Inclination: 28.50 deg. COSPAR: 1999-040A. USAF Sat Cat: 25866. Duration: 4.95 days. Decay Date: 1999-07-28. Crew: Collins Eileen, Ashby, Hawley, Coleman, Tognini. Flight: STS-93. STS-93 was first rolled out to pad 39B on June 7 1999. The Chandra/IUS-27 vehicle was placed in the payload canister on June 19. The first launch attempt was on July 20, but controllers aborted the launch at T-6 seconds, just before main engine ignition, due to a data spike in hydrogen pressure data. This was determined to be due to a faulty sensor and a second attempt was on July 22. A lightning storm prevented launch during the 46 minute window, and the launch was again scrubbed. Finally the vehicle lifted off the pad on July 23, but five seconds after launch a short in an electrical bus brought down two of the three main engine controllers. Backup controllers took over, but a further failure on the backup controller bus would have resulted in engine shutdown and the first ever attempt at an RTLS (Return To Launch Site) abort. To further complicate matters engine 3 (SSME 2019) had a hydrogen leak throughout the ascent, causing the engine to run hot. Controllers sweated as temperatures neared redline. The hot engine’s controller compensated as programmed by using additional liquid oxygen propellant. The final result was that the shuttle ran out of gas - main engine cut-off (MECO) was at 04:39 GMT, putting Columbia into a 78 km x 276 km x 28.5 degree transfer orbit. Columbia was 1,700 kg short of oxygen propellant and 5 meters/sec slower than planned. The OMS-2 engine burn at 05:12 GMT circularised the orbit 10 km lower than planned.
The orbiter payload bay contained only the Chandra spacecraft, the IUS, and the IUS tilt tableTthe following payloads were carried in the shuttle’s cabin: STL-B (Space Tissue Loss), CCM (Cell culture module), SAREX-II (Shuttle Amateur Radio Experiment), EarthKam, PGIM (Plant Growth Investigations in Microgravity), CGBA (Commercial Generic Bioprocessing Apparatus), MEMS (Micro-electric Mechanical System), and BRIC (Biological Research in Canisters) and SWUIS (the Southwest Ultraviolet Imaging System, an 0.18-m UV telescope to be used for airglow and planetary observations); GOSAMR (the Gelation of Sols: Applied Microgravity Research experiment) and LFSAH, the Lightweight Flexible Solar Array Hinge. MSX and SIMPLEX experiments were also to be carried out.
Chandra/IUS-27 was deployed from Columbia at 11:47 GMT July 23. Flight duration was limited; this was the heaviest shuttle (122,534 kg) and heaviest payload (19,736 kg) to that date. Columbia landed at 03:20 GMT on July 28 on runway 33 at Kennedy Space Center. Post-flight inspection found the presence of holes in the cooling lines on the nozzle of SSME 2019 (engine 3) which caused a hydrogen leak. A loose repair pin in the engine broke free and caused the failure. The cause of the short was found to be chaffed wiring inside the shuttle. The entire fleet was grounded for inspection and replacement of wiring as necessary.
References: 2, 7.
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Chandra Nation: USA. Payload: OV-102. Class: Astronomy. Spacecraft: Chandra. Manufacturer: TRW, Redondo Beach. Agency: NASA MSF. Perigee: 20,046 km (12,455 mi). Apogee: 128,769 km (80,013 mi). Inclination: 45.10 deg. Period: 3,808.60 min. COSPAR: 1999-040B. USAF Sat Cat: 25867. The Chandra Advanced X-ray Astrophysics Facility was one of NASA’s four Great Observatories (along with Hubble Space Telescope, Compton Gamma Ray Observatory, and the SIRTF). Chandra will study the composition and nature of galaxies, stellar objects and interstellar phenomena as well as basic issues in theoretical physics using the most sensitive X-ray telescope ever built. The IUS under-performed and placed Chandra in an orbit about 900 km lower than planned. Therefore Chandra's own IPS propulsion system had to be used to make up the difference. The first such manoeuvre was at 01:11 GMT on July 25 when the IPS engines fired for 5 minutes to raise
perigee to 1192 km. Further perigee burns on July 31, August 4, and August 7 raised the orbit to its final 10,000 km x 140.000 km.
Additional Details: Chandra. References: 2.
1999 July 23 - 11:06 GMT - -
EVA Mir EO-27-2 Nation: Russia. Program: Mir. Class: Manned. Type: Space station. Spacecraft: Mir. Crew: Afanasyev, Avdeyev. Flight: Mir EO-27, Mir EO-26/-27. EVA Duration: 0.25 days. Mir spacewalk started at 11:06 GMT. Afanasyev and Avdeyev installed a new experimental 6-meter antenna but failed to deploy it.
1999 July 25 - 07:46 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: SLC17A. Launch Vehicle: Delta. Model: Delta 7420-10C. LV Configuration: Delta 7420-10C D273. -
Globalstar 26 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,413 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-041A. USAF Sat Cat: 25872. References: 2.
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Globalstar 28 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. COSPAR: 1999-041B. USAF Sat Cat: 25873. References: 2.
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Globalstar 43 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. COSPAR: 1999-041C. USAF Sat Cat: 25874. References: 2.
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Globalstar 48 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,415 km (879 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-041D. USAF Sat Cat: 25875. References: 2.
1999 July 27 - 22:48 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB NASA 21.122GE. -
ICON Ionosphere mission Nation: USA. Agency: NASA. Apogee: 104 km (64 mi). References: 2.
1999 July 28 - 09:37 GMT - -
EVA Mir EO-27-3 Nation: Russia. Program: Mir. Class: Manned. Type: Space station. Spacecraft: Mir. Crew: Afanasyev, Avdeyev. Flight: Mir EO-27, Mir EO-26/-27. EVA Duration: 0.22 days. The spacewalk started at 09:37 GMT. Afanasyev and Avdeyev erected an experimental 6-meter antenna. At the end of the experiment the antenna was jettisoned.
1999 July 28 - -
Landing of STS-93 Nation: USA. Program: STS. Flight: STS-93. STS-93 landed at 03:17 GMT.
1999 July 29 - -
Deep Space 1, Asteroid Braille Flyby Nation: USA. Spacecraft: Deep Space 1.
1999 July 31 - -
Lunar Prospector, Moon Impact Nation: USA. Spacecraft: Lunar Prospector. A two year extended mission following the original one-year mission was possible, during which the orbit was to be lowered to 50 km and then 10 km altitude to obtain higher resolution measurements. However this was not funded, and the spacecraft was commanded to crash into the moon.
1999 August 2 - Launch Site: Taiyuan. Launch Complex: -. Launch Pad: -. Launch Vehicle: DF-31. -
Test mission Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). References: 2.
1999 August 2 - 11:37 GMT - Launch Site: White Sands. Launch Complex: LC94. Launch Pad: FIX. Launch Vehicle: Hera. LV Configuration: Hera 16. -
BRV/THAAD Target mission Nation: USA. Agency: USA. Apogee: 270 km (160 mi). References: 2.
1999 August 2 - 11:44 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: THAAD. LV Configuration: THAAD FT-11. -
ABM test Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1999 August 12 - 22:52 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 42P. LV Configuration: Ariane 42P-3 V118. -
Telkom 1 Nation: Indonesia. Program: Palapa. Mass: 2,763 kg (6,091 lb). Class: Communications. Spacecraft: AS 2100. Manufacturer: Lockheed Martin, Sunnyvale. Agency: PT Telko. Perigee: 35,781 km (22,233 mi). Apogee: 35,794 km (22,241 mi). Inclination: 0.10 deg. COSPAR: 1999-042A. USAF Sat Cat: 25880. The launch vehicle delivered its H-10-3 third stage and the Telkom 1 payload into a 221 km x 35687 km x 7.0 degree geosynchronous transfer orbit 21 minutes after launch. Telkom 1 was owned by PT Telkomunikasi of Indonesia and was a successor to the Palapa series of satellites. Mass of Telkom 1 was 1700 kg in geosynchronous orbit after its on-board engine made the apogee burn. Stationed at 108 deg E. Positioned in geosynchronous orbit at 108 deg E in 1999. As of 3 September 2001 located at 107.98 deg E drifting at 0.011 deg W per day. As of 2007 Mar 11 located at 107.98E drifting at 0.014W degrees per day.
References: 2.
1999 August 14 - -
Galileo, Callisto 22 Flyby Nation: USA. Spacecraft: Galileo.
1999 August 15 - Launch Vehicle: CZ. Model: CZ-2F. -
China Upgrades Launch Facilities Nation: China. Tang Xianming, Director of the Xichang Launch Center, confirmed the construction of a new Vertical Assembly Facility at the Jiuquan Launch Center. He also affirmed that China would continue to use the Xichang Launch Center, which would be upgraded with improved data processing and control equipment.
References: 424.
1999 August 17 - 04:37 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: SLC17B. Launch Vehicle: Delta. Model: Delta 7420-10C. LV Configuration: Delta 7420-10C D274. -
Globalstar 24 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. COSPAR: 1999-043A. USAF Sat Cat: 25883. References: 2.
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Globalstar 27 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,415 km (879 mi). Inclination: 52.00 deg. COSPAR: 1999-043B. USAF Sat Cat: 25884. References: 2.
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Globalstar 53 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. COSPAR: 1999-043C. USAF Sat Cat: 25885. References: 2.
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Globalstar 54 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,413 km (877 mi). Apogee: 1,414 km (878 mi). Inclination: 52.00 deg. COSPAR: 1999-043D. USAF Sat Cat: 25886. References: 2.
1999 August 18 - -
Cassini, Earth Flyby Nation: USA. Spacecraft: Cassini.
1999 August 18 - 18:00 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. -
Cosmos 2365 Nation: Russia. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-4K1. Manufacturer: TsSKB-Progress, Samara. Agency: MO RF. Perigee: 184 km (114 mi). Apogee: 338 km (210 mi). Inclination: 67.10 deg. Period: 89.73 min. COSPAR: 1999-044A. USAF Sat Cat: 25889. Duration: 119.00 days. Decay Date: 1999-12-15. 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. References: 2.
1999 August 18 - 18:05 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9CM1. LV Configuration: Black Brant 9CM1 NASA 36.181US. -
USC-3 (SOHO Cal) Solar extreme ultraviolet mission Nation: USA. Agency: NASA GSFC. Apogee: 314 km (195 mi). References: 2.
1999 August 20 - -
Starchaser 3a launch. Nation: UK. Program: X-Prize. Spacecraft: Starchaser 5. Starchaser Industries (Hyde, England, UK) successfully launches Starchaser 3a vehicle.
1999 August 20 - 08:45 GMT - Launch Site: Vandenberg. Launch Complex: LF10. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT170GM. -
RCT-1 GT170GM/RRF-6 operational test launch Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi). References: 2.
1999 August 20 - 11:27 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT171GM. -
FOT GT171GM Follow-on Test launch Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi). References: 2.
1999 August 21 - -
Discovery of Dar al Gani 975 (Mars Meteorite) Nation: Libya.
1999 August 24 - 07:07 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.119UG. -
Ultraviolet astronomy mission Nation: USA. Agency: NASA GSFC. Apogee: 300 km (180 mi). References: 2.
1999 August 26 - 12:02 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. -
Cosmos 2366 Nation: Russia. Mass: 825 kg (1,818 lb). Class: Navigation. Spacecraft: Parus. Manufacturer: AKO Polyot, Omsk. Agency: MO RF. Perigee: 963 km (598 mi). Apogee: 1,007 km (625 mi). Inclination: 82.90 deg. Period: 104.80 min. COSPAR: 1999-045A. USAF Sat Cat: 25892. References: 2.
1999 August 28 - -
Landing of Soyuz TM-29 Nation: Russia. Program: Mir. Flight: Mir EO-27, Mir EO-26/-27. The hatch between Mir and Soyuz was closed at 18:12 GMT on August 27, 1999. Soyuz TM-29 undocked from Mir at 21:17 GMT with Afanasyev, Avdeyev and Haignere aboard. The Mir EO-27 crew landed in Kazakhstan at 00:35 GMT on August 28. Afanasyev had set a new cumulative time in space record, but for the first time since September 1989 there were no humans in space.
1999 August 29 - Launch Site: Kapustin Yar. Launch Complex: LC107/1. Launch Pad: LC107/pad?. Launch Vehicle: Kosmos 3. Model: K65M-R. FAILURE: Failure. -
Re-entry Vehicle test Nation: Russia. Agency: RVSN RF. Apogee: 675 km (419 mi). References: 2.
1999 August 31 - -
China and Russia Sign Space Co-operation Agreement Nation: China. China and Russia signed a new agreement in Beijing on the co-operation in the peaceful space exploration. Joint research would be conducted in telecommunication systems, Earth surface monitoring, and satellite navigation. The agreement also covered scientific research aboard the Mir space station, but not visits of Chinese cosmonauts to Mir. It was also reported that Russia was working with China not only on design of the new manned spacecraft, but also on the 921-2 space station.
References: 424.
1999 September - -
XMM integration/testing completed Nation: Europe. Spacecraft: XMM.
1999 September 3 - 11:44 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Topol. Model: Topol M. LV Configuration: Topol-M 8. -
Test mission Nation: Russia. Agency: RVSN RF. Apogee: 1,000 km (600 mi). References: 2.
1999 September 4 - 22:34 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 42P. LV Configuration: Ariane 42P-3 V120. -
Koreasat 3 Nation: Korea South. Payload: Mugunghwa 3. Class: Communications. Spacecraft: AS 2100. Manufacturer: Lockheed Martin, Sunnyvale. Agency: Korea Te. Perigee: 35,786 km (22,236 mi). Apogee: 35,789 km (22,238 mi). Inclination: 0.00 deg. COSPAR: 1999-046A. USAF Sat Cat: 25894. Geosynchronous communications satellite. Stationed at 112 deg E. Positioned in geosynchronous orbit at 112 deg E in 1999. As of 31 August 2001 located at 115.99 deg E drifting at 0.014 deg W per day. As of 2007 Mar 10 located at 116.12E drifting at 0.008W degrees per day.
References: 2.
1999 September 6 - Launch Site: Wake Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: SR19/SR19. -
TCMP-3A re-entry vehicle test flight Nation: USA. Agency: OSC. Apogee: 300 km (180 mi). References: 2.
1999 September 6 - 16:36 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M 388-02. -
Yamal 101 Nation: Russia. Class: Communications. Spacecraft: Yamal. Manufacturer: RKK Energiya im. S.P. Korolyov, Kaliningrad-Korolyov. Agency: AO Gazco. Perigee: 35,503 km (22,060 mi). Apogee: 36,298 km (22,554 mi). Inclination: 2.40 deg. Period: 1,441.90 min. COSPAR: 1999-047A. USAF Sat Cat: 25896. The first two Yamal communications satellites were placed into a 197 km x 36,311 km x 49.3 degree transfer orbit The DM-2M fourth stage made two successful burns, placing the satellites in circular 36,000 km geosynchronous orbits. Yamal 101 reportedly ran into problems after it was deployed. RKK Energia built the new Yamal satellites for AO Gazcom of Moscow, a joint venture of RKKE and RAO Gazprom, the Russian natural gas monopoly. The two satellites will support internal communications for RAO Gazprom. Positioned in geosynchronous orbit at 89 deg E in 1999. As of 30 August 2001 located at 112.86 deg E drifting at 1.484 deg W per day. As of 2007 Mar 10 located at 42.96E drifting at 1.484W degrees per day.
References: 2.
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Yamal 102 Nation: Russia. Class: Communications. Spacecraft: Yamal. Manufacturer: RKK Energiya im. S.P. Korolyov, Kaliningrad-Korolyov. Agency: AO Gazco. Perigee: 35,772 km (22,227 mi). Apogee: 35,802 km (22,246 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 1999-047B. USAF Sat Cat: 25897. Completed Operations Date: 1999-09-01. Geosynchronous communications satellite. Stationed at 90 deg E. As of 5 September 2001 located at 89.85 deg E drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 89.78E drifting at 0.010W degrees per day. References: 2.
1999 September 9 - 18:00 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. -
Foton 12 Nation: Russia. Payload: Foton s/n 12. Class: Materials. Spacecraft: Foton. Manufacturer: TsSKB-Progress, Samara. Agency: RAKA. Perigee: 216 km (134 mi). Apogee: 379 km (235 mi). Inclination: 62.80 deg. COSPAR: 1999-048A. USAF Sat Cat: 25902. Duration: 14.64 days. Decay Date: 1999-09-24. Foton 12 carried European microgravity experiments. The spacecraft's descent module landed on Russian territory at 52.47 deg N 53.83 deg E on September 24, 1999. References: 2.
1999 September 15 - 21:00 GMT - Launch Site: Kodiak. Launch Complex: -. Launch Pad: -. Launch Vehicle: ait. Model: ait-2. LV Configuration: Castor-M57A1 ait-2. -
Test mission Nation: USA. Agency: USAF SMC. Apogee: 1,060 km (650 mi). References: 2.
1999 September 22 - 14:33 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. LV Configuration: Soyuz 11A511U/Ikar S15000-061 ST04. -
Globalstar 33 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,416 km (879 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-049A. USAF Sat Cat: 25907. The third stage put the complex into a 235 km x 906 km x 51.9 degree transfer orbit. The Ikar upper stage maneouvered, placed the four satellites into their final parking orbit, then made a deorbit burn and re-entered on September 24. References: 2.
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Globalstar 50 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,415 km (879 mi). Inclination: 52.00 deg. COSPAR: 1999-049B. USAF Sat Cat: 25908. References: 2.
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Globalstar 55 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,412 km (877 mi). Apogee: 1,416 km (879 mi). Inclination: 52.00 deg. Period: 114.10 min. COSPAR: 1999-049C. USAF Sat Cat: 25909. References: 2.
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Globalstar 58 Nation: USA. Class: Communications. Spacecraft: Globalstar. Agency: Globalst. Perigee: 1,413 km (877 mi). Apogee: 1,413 km (877 mi). Inclination: 52.00 deg. COSPAR: 1999-049D. USAF Sat Cat: 25910. References: 2.
1999 September 23 - 06:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36A. Launch Pad: SLC36A. Launch Vehicle: Atlas. Model: Atlas IIAS. LV Configuration: Atlas IIAS AC-155. -
Echostar 5 Nation: USA. Program: Echostar. Class: Communications. Spacecraft: FS-1300. Manufacturer: Space Systems/Loral, Palo Alto. Agency: Echostar. Perigee: 35,777 km (22,230 mi). Apogee: 35,795 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 1999-050A. USAF Sat Cat: 25913. The Centaur second stage put Echostar 5 into a supersynchronous transfer orbit of 131 km x 45526 km x 26.6 degrees. The satellite's own engine put it into the final geosynchronous orbit. Echostar 5 was a Ku-band satellite, part of the Dish Network. Stationed at 110 deg W. Positioned in geosynchronous orbit at 110 deg W in 1999. As of 5 September 2001 located at 110.01 deg W drifting at 0.003 deg W per day. As of 2007 Mar 11 located at 128.86W drifting at 0.001E degrees per day.
References: 2.
1999 September 24 - Launch Site: Barking Sands. Launch Complex: POA. Launch Pad: -. Launch Vehicle: Standard-ER. Model: Standard SM-3. LV Configuration: SM-3 CTV-1A. -
Test mission Nation: USA. Agency: USN. Apogee: 100 km (60 mi). References: 2.
1999 September 24 - 18:21 GMT - Launch Site: Vandenberg. Launch Complex: SLC6. Launch Pad: -. Launch Vehicle: Athena. Model: Athena-2. LV Configuration: Athena-2 LM-007. -
Ikonos Nation: USA. Mass: 726 kg (1,600 lb). Class: Surveillance. Type: Civilian. Spacecraft: Ikonos. Manufacturer: Lockheed Martin, Sunnyvale. Agency: SpaceIm. Perigee: 678 km (421 mi). Apogee: 679 km (421 mi). Inclination: 98.20 deg. COSPAR: 1999-051A. USAF Sat Cat: 25919. Commercial / civilian high resolution (1 metre resolution) photograhic satellite. References: 2.
1999 September 25 - 06:29 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 44LP. LV Configuration: Ariane 44LP-3 V121. -
Telstar 7 Nation: USA. Mass: 3,790 kg (8,350 lb). Class: Communications. Spacecraft: FS-1300. Manufacturer: Space Systems/Loral, Palo Alto. Agency: Loral Sk. Perigee: 35,778 km (22,231 mi). Apogee: 35,794 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 1999-052A. USAF Sat Cat: 25922. Telstar 7, owned by Loral Skynet, had 24 C-band and 24 Ku-band transponders. Dry mass was 1537 kg. After placement in final geosynchronous orbit it provided communications for North America from a position at 129 degrees East longitude. Sold to Intelsat in March 2004 and renamed IA-7. The satellite had a power failure on November 28, 2004 and was briefly declared lost. Intelsat recovered control of the satellite by December 4. As of 2007 Mar 9 located at 129.01W drifting at 0.007W degrees per day.
References: 2.
1999 September 26 - 22:30 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 398-02. -
LMI-1 Nation: Russia. Class: Communications. Spacecraft: LMI. Manufacturer: Lockheed Martin, Sunnyvale. Agency: LMI. Perigee: 35,783 km (22,234 mi). Apogee: 35,789 km (22,238 mi). Inclination: 0.10 deg. COSPAR: 1999-053A. USAF Sat Cat: 25924. Geosynchronous communications satellite. Stationed at 75 deg E. Positioned in geosynchronous orbit at 75 deg E in 1999. As of 2 September 2001 located at 74.98 deg E drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 75.00E drifting at 0.004W degrees per day.
References: 2.
1999 September 27 - 10:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.168UG. -
Ultraviolet astronomy mission Nation: USA. Agency: NASA GSFC. Apogee: 329 km (204 mi). References: 2.
1999 September 28 - 11:00 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. -
Resurs F-1M Nation: Russia. Class: Earth. Type: Landsat. Spacecraft: Resurs F1M. Manufacturer: TsSKB-Progress, Samara. Agency: RKA. Perigee: 220 km (130 mi). Apogee: 231 km (143 mi). Inclination: 82.30 deg. COSPAR: 1999-054A. USAF Sat Cat: 25929. Duration: 24.00 days. Decay Date: 1999-10-22. Remote sensing film satellite. Recovered in Russia on October 22, 1999. References: 2.
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