See also Born on this Day On this day in: 1946 -
1947 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: FFAR. -
RM-10 model test flight Nation: USA. Agency: NACA. Apogee: 5.00 km (3.10 mi).
1952 - Launch Vehicle: Von Braun 1952.
1953 - Launch Site: Cape Canaveral. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hermes. Model: Hermes A-2. LV Configuration: RV-A-10 1. -
Test mission Nation: USA. Agency: USA. Apogee: 50 km (31 mi).
1960 - 18:15 GMT - Launch Site: Rosamund Dry Lake DZ. Launch Complex: -. Launch Pad: 34.7 N x 118.1 W. Launch Vehicle: X-15. LV Configuration: X-15 2-4-11.
1961 - 10:41 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI27. -
Airglow Aeronomy mission Nation: France. Agency: FR. Apogee: 91 km (56 mi).
1962 - Launch Site: Kapustin Yar. Launch Complex: silo. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: R-14U. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 675 km (419 mi).
1963 - Launch Site: Baikonur. Launch Complex: LC70. Launch Pad: -. Launch Vehicle: R-9. Model: Desna. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,160 km (720 mi).
1963 - 15:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-7. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1964 - -
Apollo LEM to use an inertial reference system Nation: USA. Program: Apollo. Spacecraft: Apollo LM. ASPO directed Grumman to provide an abort guidance system (AGS) in the LEM using an inertial reference system attached to the structure of the vehicle. Should the spacecraft's navigation and guidance system fail, the crew could use the AGS to effect an abort. Such a device eliminated the need for redundancy in the primary guidance system (and proved to be a lighter and simpler arrangement).
1964 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 692. -
Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1965 - -
Drogue parachutes tested to ultimate load Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A drop test at EI Centro, Calif., demonstrated the ability of the drogue parachutes to sustain the ultimate disreefed load that would be imposed upon them during reentry. (For the current CM weight, that maximum load would be 7,711 kg (17,000 lbs) per parachute.) Preliminary data indicated that the two drogues had withstood loads of 8,803 and 8,165 kg (19,600 and 18,000 lbs). One of the drogues emerged unscathed; the other suffered only minor damage near the pocket of the reefing cutter.
1965 - 15:19 GMT - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3A. LV Configuration: Titan IIIA 3A-3.
1965 - 17:55 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AE3.153. -
Solar spectrum Solar ultraviolet / solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).
1966 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1387. -
Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1966 - 01:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 460. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1966 - 13:04 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 86D. -
NTMP KX-51 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).
1966 - 18:00 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1.
1969 - -
Unmanned Apollo LM landing discussed Nation: USA. Program: Apollo. Spacecraft: Apollo LM. The possibility of an unmanned LM landing was discussed at NASA Hq. The consensus was that such a landing would be a risky venture. Proposals had been made which included an unmanned LM landing as a prerequisite to a manned landing on the moon. However, the capability to land the LM unmanned did not exist and development of the capability would seriously delay the program.
1969 - Launch Vehicle: N1. -
Military space objectives Nation: USSR. Program: Lunar L3, Luna. Spacecraft: Luna Ye-8. The Ye-8 and N1 are on schedule for their respective launches. Kamanin discusses the cosmonaut training curriculum with Kerimov. No one has ever defined what it is cosmonauts are actually supposed to do in space. No one really knows what their purpose is --- not Keldysh, not Mishin, not Smirnov, not Ustinov. Kerimov agrees to put together a state commission to define the role of man in space and draw up plans for future space missions.
1969 - 21:09 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P23K. -
Electrons Ionosphere mission Nation: UK. Agency: SRC. Apogee: 157 km (97 mi).
1970 -
1970 - 04:25 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 4S. LV Configuration: Lambda 4S L-4S-5.
1970 - 08:40 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 2. LV Configuration: Thor Burner 2 287.
1972 - 03:20 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Ionosphere/Plasma mission Nation: USSR. Apogee: 177 km (109 mi).
1972 - 12:00 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Plasma mission Nation: USSR. Apogee: 173 km (107 mi).
1972 - 12:00 GMT - Launch Site: Syowa Base. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210JA-12. -
Mass spectrometer Ionosphere mission Nation: Japan. Agency: NIPR. Apogee: 108 km (67 mi).
1974 - 13:48 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3E. LV Configuration: Titan IIIE 23E-1 / Centaur D-1T E-1. FAILURE: Centaur LOX pump failure.
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Viking Dynamic Simulator Nation: USA. Payload: VDS. Spacecraft: Viking. Agency: USAF. COSPAR: F740211B.
1975 - 02:16 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.65UE.
1976 - 08:50 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
1977 - 04:48 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.1012UE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 212 km (131 mi).
1977 - 12:33 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P194H. -
Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi).
1977 - 13:18 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P191H. -
Ionosphere mission Nation: UK. Agency: SRC. Apogee: 132 km (82 mi).
1977 - 13:59 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P189H. -
Atomic oxygen Atmospheric mission Nation: UK. Agency: SRC. Apogee: 142 km (88 mi).
1977 - 14:57 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
1977 - 20:49 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.213IE. -
SSC S21 / 2 TRIGGER Aurora mission Nation: Sweden. Agency: NASA/SSC. Apogee: 220 km (130 mi).
1978 - Launch Site: Baikonur. Launch Complex: LC109. Launch Pad: -. Launch Vehicle: R-36M. -
Missile accuracy test launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1980 - 23:32 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53772-402.
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Cosmos 1157 Nation: USSR. Program: Strela. Payload: Strela-1M no. 186. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,415 km (879 mi). Apogee: 1,477 km (917 mi). Inclination: 74.00 deg. Period: 114.80 min. COSPAR: 1980-012B. USAF Sat Cat: 11692.
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Cosmos 1158 Nation: USSR. Program: Strela. Payload: Strela-1M no. 187. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,434 km (891 mi). Apogee: 1,476 km (917 mi). Inclination: 74.00 deg. Period: 115.00 min. COSPAR: 1980-012C. USAF Sat Cat: 11693.
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Cosmos 1159 Nation: USSR. Program: Strela. Payload: Strela-1M no. 188. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,450 km (900 mi). Apogee: 1,479 km (919 mi). Inclination: 74.00 deg. Period: 115.20 min. COSPAR: 1980-012D. USAF Sat Cat: 11694.
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Cosmos 1160 Nation: USSR. Program: Strela. Payload: Strela-1M no. 189. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,465 km (910 mi). Apogee: 1,484 km (922 mi). Inclination: 74.00 deg. Period: 115.40 min. COSPAR: 1980-012E. USAF Sat Cat: 11695.
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Cosmos 1161 Nation: USSR. Program: Strela. Payload: Strela-1M no. 190. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,468 km (912 mi). Apogee: 1,502 km (933 mi). Inclination: 74.00 deg. Period: 115.70 min. COSPAR: 1980-012F. USAF Sat Cat: 11696.
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Cosmos 1162 Nation: USSR. Program: Strela. Payload: Strela-1M no. 191. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,472 km (914 mi). Apogee: 1,519 km (943 mi). Inclination: 74.00 deg. Period: 115.90 min. COSPAR: 1980-012G. USAF Sat Cat: 11697.
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Cosmos 1163 Nation: USSR. Program: Strela. Payload: Strela-1M no. 192. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,471 km (914 mi). Apogee: 1,543 km (958 mi). Inclination: 74.00 deg. Period: 116.10 min. COSPAR: 1980-012H. USAF Sat Cat: 11698.
1981 - -
Production of the Production of four 37KS modules for Mir approved Nation: USSR. Spacecraft: 37KS. Production of the four 37KS modules was approved following review of the draft projects. The four modules would be placed into orbit by a Proton launch vehicle. An FGO tug section, connected to the 37KS module by a light lattice structure, would rendezvous with the Mir station and dock the module to one of the radial ports of the Mir station. It would then separate and deorbit itself into the earth's atmosphere. The plan was that production of all of the modules would be completed in 1984. They would be assembled with the Mir base block in one year and have an operational lifetime of five years.
1981 - 08:30 GMT - Launch Site: Tanegashima. Launch Complex: N. Launch Pad: -. Launch Vehicle: Delta. Model: N-2. LV Configuration: N-2 N-7(F).
1982 - 01:11 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2. -
Cosmos 1337 Nation: USSR. Program: EORSAT. Mass: 3,000 kg (6,600 lb). Class: Sigint. Type: Naval reconnaisance. Spacecraft: US-P. Agency: MO SSSR. Perigee: 426 km (264 mi). Apogee: 444 km (275 mi). Inclination: 65.00 deg. Period: 93.30 min. COSPAR: 1982-010A. USAF Sat Cat: 13061. Decay Date: 1982-07-25. Ocean monitoring.
1984 - 12:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki T 1-0784. -
Aeronomy mission Nation: USA. Agency: NASA WFC. Apogee: 109 km (67 mi).
1984 -
1985 - 10:30 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: K. Launch Vehicle: S. Model: S-520. LV Configuration: S-520-7. -
Aeronomy / ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 362 km (224 mi).
1986 - 06:56 GMT - Launch Site: Plesetsk. Launch Complex: LC32/2. Launch Pad: -. Launch Vehicle: Tsiklon. Model: Tsiklon-3.
1987 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B.
1990 - 06:16 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2. -
Soyuz TM-9 Nation: USSR. Program: Mir. Payload: Soyuz TM 11F732 s/n 60. Mass: 7,150 kg (15,760 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TM. Agency: MOM. Perigee: 373 km (231 mi). Apogee: 387 km (240 mi). Inclination: 51.60 deg. Period: 92.20 min. COSPAR: 1990-014A. USAF Sat Cat: 20494. Duration: 179.05 days. Decay Date: 1990-08-09. Crew: Balandin, Solovyov. Flight: Mir EO-5, Mir EO-6. Manned two crew. Mir Expedition EO-06. Docked with Mir. Transported to the Mir orbital station a crew comprising the cosmonauts A Y Solovyov and A N Balandin to conduct an extensive programme of geophysical and astrophysical research, experiments on biology and biotechnology and work on space materials science.
1991 - Launch Site: Sriharikota. Launch Complex: -. Launch Pad: -. Launch Vehicle: Prithvi. LV Configuration: Prithvi 3. -
Test mission Nation: India. Agency: IDRDL. Apogee: 100 km (60 mi).
1991 - 19:20 GMT - Launch Site: Scud Batteries. Launch Complex: -. Launch Pad: IRAQ-S. Launch Vehicle: R-17. Model: Al Hussein. -
Riyadh Nation: Iraq. Agency: IRAQ. Apogee: 100 km (60 mi).
1992 - 00:41 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36A. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas II. LV Configuration: Atlas II AC-101 / Centaur II 8101.
1992 - 01:50 GMT - Launch Site: Tanegashima. Launch Complex: N. Launch Pad: -. Launch Vehicle: Delta. Model: H-1. LV Configuration: H-1 H-24(F). -
JERS-1 Nation: Japan. Payload: ERS-1. Mass: 1,340 kg (2,950 lb). Class: Earth. Type: Landsat. Spacecraft: JERS. Agency: NASDA. Perigee: 567 km (352 mi). Apogee: 568 km (352 mi). Inclination: 97.70 deg. Period: 96.00 min. COSPAR: 1992-007A. USAF Sat Cat: 21867. Completed Operations Date: 1998-10-12. Decay Date: 2001-12-03. Japanese Research Satellite-1. JERS-1 (FUYO-1). To verify functions and performance of optical sensors and a Synthetic Aperture Radar and to establish an integrated system for observing the Earth's resources; to perform observations and measurements for land survey, agriculture, forest ry, fishery, environmental preservation, disaster prevention and coastal surveillance. Launch time 0150 GMT. Launching organization NASDA. The Japanese Fuyo-1 (ERS-1) satellite failed on Oct 12, 1998 after six years
of operation.
1994 -
1995 -
1996 - 11:00 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: K. Launch Vehicle: S. Model: S-310. LV Configuration: S-310-24. -
NTV-1 Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 199 km (123 mi).
1996 - 23:00 GMT - Launch Site: Tanegashima. Launch Complex: N. Launch Pad: -. Launch Vehicle: J. Model: J-1. LV Configuration: J-1 J-1-1F. -
Hyflex Spacecraft test Nation: Japan. Agency: NASDA. Apogee: 110 km (60 mi).
1997 - 08:36 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 12. LV Configuration: Black Brant XII NASA 40.11UE. -
Auroral Turbulence 2 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 546 km (339 mi).
1997 - 08:55 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-82. -
STS-82 Nation: USA. Program: STS. Payload: Discovery F22 / SAC. Class: Manned. Type: Spaceplane. Spacecraft: Discovery. Manufacturer: Boeing North American, Palmdale (formerly Rockwell). Agency: NASA JSC. Perigee: 584 km (362 mi). Apogee: 618 km (384 mi). Inclination: 28.50 deg. Period: 96.70 min. COSPAR: 1997-004A. USAF Sat Cat: 24719. Duration: 9.98 days. Decay Date: 1997-02-21. Crew: Bowersox, Horowitz, Lee, Tanner, Hawley, Harbaugh, Smith Steven. Flight: STS-82. After a spectacular night launch, the Shuttle completed its rendezvous with Hubble Space Telescope on February 13. Over the next four days five spacewalks were undertaken to renovate Hubble.
The Hubble Space Telescope was released back into orbit at 06:41 GMT on February 19. Discovery landed on Runway 15 at Kennedy Space Center at 08:32 GMT on February 21.
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FSS Nation: USA. Program: STS. Agency: NASA. COSPAR: 1997-004xx. USAF Sat Cat: 24719. Decay Date: 1997-02-21.
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ORUC Nation: USA. Program: STS. Agency: NASA. COSPAR: 1997-004xx. USAF Sat Cat: 24719. Decay Date: 1997-02-21.
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SAC Nation: USA. Program: STS. Agency: NASA. COSPAR: 1997-004xx. USAF Sat Cat: 24719. Decay Date: 1997-02-21.
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External Airlock Nation: USA. Program: STS. Payload: EAL. Agency: NASA. COSPAR: 1997-004xx. USAF Sat Cat: 24719. Decay Date: 1997-02-21.
1998 - 09:42 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Improved Orion. LV Configuration: Nike Improved Orion DLR K-NO2-232. -
Mini-Texus 5 Microgravity mission Nation: Germany. Agency: DLR. Apogee: 140 km (80 mi).
1999 - 06:45 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 10. LV Configuration: Black Brant X NASA 35.032UE. -
ENSTROPHY Ionosphere mission Nation: USA. Agency: NASA GSFC. Apogee: 1,071 km (665 mi).
2000 - 17:43 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-99. -
STS-99 Nation: USA. Program: STS. Payload: Endeavour F14. Class: Manned. Type: Spaceplane. Spacecraft: Endeavour. Manufacturer: Boeing. Agency: NASA JSC. Perigee: 233 km (144 mi). Apogee: 233 km (144 mi). Inclination: 57.00 deg. COSPAR: 2000-010A. USAF Sat Cat: 26088. Duration: 11.23 days. Decay Date: 2000-02-22. Crew: Kregel, Gorie, Kavandi, Voss Janice, Mohri, Thiele. Flight: STS-99. On an extremely successful mission the space shuttle Endeavour deployed the 61 metre long STRM mast. This was a side-looking radar that digitally mapped with unprecedented accuracy the entire land surface of the Earth between latitudes 60 deg N and 54 deg S. Sponsors of the flight included the US National Imagery and Mapping Agency (NIMA), NASA, and the German and Italian space agencies. Some of the NIMA data would remain classified for exclusive use by the US Department of Defense.
2002 - 17:43 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7920-10C. LV Configuration: Delta 7920-10C D290. -
Iridium Nation: USA. Program: Iridium. Payload: SV 90. Mass: 690 kg (1,520 lb). Class: Communications. Spacecraft: LM 700. Manufacturer: LM-S/Motorola. Agency: Iridium. Perigee: 660 km (410 mi). Apogee: 684 km (425 mi). Inclination: 86.60 deg. Period: 98.20 min. COSPAR: 2002-005A. USAF Sat Cat: 27372.
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Iridium Nation: USA. Program: Iridium. Payload: SV 91. Mass: 690 kg (1,520 lb). Class: Communications. Spacecraft: LM 700. Manufacturer: LM-S/Motorola. Agency: Iridium. Perigee: 665 km (413 mi). Apogee: 679 km (421 mi). Inclination: 86.60 deg. Period: 98.20 min. COSPAR: 2002-005B. USAF Sat Cat: 27373.
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Iridium Nation: USA. Program: Iridium. Payload: SV 94. Mass: 690 kg (1,520 lb). Class: Communications. Spacecraft: LM 700. Manufacturer: LM-S/Motorola. Agency: Iridium. Perigee: 667 km (414 mi). Apogee: 677 km (420 mi). Inclination: 86.60 deg. Period: 98.20 min. COSPAR: 2002-005C. USAF Sat Cat: 27374.
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Iridium Nation: USA. Program: Iridium. Payload: SV 95. Mass: 690 kg (1,520 lb). Class: Communications. Spacecraft: LM 700. Manufacturer: LM-S/Motorola. Agency: Iridium. Perigee: 665 km (413 mi). Apogee: 679 km (421 mi). Inclination: 86.60 deg. Period: 98.20 min. COSPAR: 2002-005D. USAF Sat Cat: 27375. Mobile Telephony satellite. Return to flight after GEM solid booster failure on GBI launch. Launch delayed from February 8, 9 and 10. Five Motorola Iridium satellites were launched for Iridium Satellite LLC, the new company that bought out the bankrupt Iridium LLC. This was the first system replenishment launch since the bankruptcy.
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Iridium Nation: USA. Program: Iridium. Payload: SV 96. Mass: 690 kg (1,520 lb). Class: Communications. Spacecraft: LM 700. Manufacturer: LM-S/Motorola. Agency: Iridium. Perigee: 665 km (413 mi). Apogee: 679 km (421 mi). Inclination: 86.60 deg. Period: 98.20 min. COSPAR: 2002-005E. USAF Sat Cat: 27376.
2008 - 11:34 GMT - Launch Site: Baikonur. Launch Vehicle: Proton. Model: Proton-M/Briz-M.
2008 - 14:13 GMT -
Born on this day in: - 1906 - Erich Kaschig. German Rocket engineer. Birth City: Breslau. Birth Country: Germany.
- 1921 - James Wesley Crooks. American Engineer. Birth City: Frankfort. Birth State: Kansas. Birth Country: USA.
- 1953 - Steven Douglas Thorne. American Mission Specialist Astronaut. Birth City: Frankfurt-an-Main. Birth Country: Germany.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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