See also Born on this Day On this day in: 1944 - Launch Vehicle: Redstone.
1947 - Launch Vehicle: Atlas.
1947 - 23:47 GMT - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: V-2. LV Configuration: V-2 Special. FAILURE: Failure.
1953 - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: Hermes. Model: Hermes A-3A. LV Configuration: Hermes A-3A 6. -
Test mission Nation: USA. Agency: USA. Apogee: 30 km (18 mi).
1953 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Deacon. Model: Triple Deacon HPAG. -
E10 Hypersonic test Nation: USA. Agency: NACA. Apogee: 20 km (12 mi).
1954 - Launch Vehicle: Soyuz. Model: R-7.
1956 -
1957 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Double Cajun T40. -
MW-2 model test flight Nation: USA. Agency: NACA. Apogee: 10 km (6 mi).
1959 - 10:51 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.17CA. -
Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 236 km (146 mi).
1959 - 17:11 GMT - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1X-3. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1959 - 18:16 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AA6.164C. -
Diurnal density Aeronomy mission Nation: USA. Agency: USAF. Apogee: 119 km (73 mi).
1959 - 19:25 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena A. LV Configuration: Thor Agena A 212 / Agena A 1050.
1959 - 21:06 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7. LV Configuration: R-7 I2-1T.
1961 - Launch Vehicle: Saturn V. Model: Saturn C-5. -
Rosen Group recommends direct ascent for the lunar landing mission mode Nation: USA. Program: Apollo. Milton W. Rosen, Director of Launch Vehicles and Propulsion, NASA Office of Manned Space Flight (OMSF), submitted to D. Brainerd Holmes, Director, OMSF, the report of the working group which had been set up on November 6. - Additional details.
1961 - -
North American to proceed with the Paraglider Development Program. Nation: USA. Program: Gemini. Spacecraft: Gemini. Manned Spacecraft Center notified North American to proceed with Phase II-A of the Paraglider Development Program. A letter contract, NAS 9-167, followed on November 21; contract negotiations were completed February 9, 1962; and the final contract was awarded on April 16, 1962. Phase I, the design studies that ran from the beginning of June to mid-August 1961, had already demonstrated the feasibility of the paraglider concept. Phase II-A, System Research and Development, called for an eight-month effort to develop the design concept of a paraglider landing system and to determine its optimal performance configuration. This development would lay the groundwork for Phase II, Part B, comprising prototype fabrication, unmanned and manned flight testing, and the completion of the final system design. Ultimately Phase III-Implementation-would see the paraglider being manufactured and pilots trained to fly it.
1961 - Launch Site: Warren AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E.
1961 - 18:04 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2C. LV Configuration: Skylark-2C NASA 9.04GG. -
Southern Sky Survey Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 209 km (129 mi).
1962 - 21:41 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 300A. LV Configuration: Aerobee 300A NASA 06.06GA. -
Thermosphere Probe 1 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 345 km (214 mi).
1963 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-44. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1965 - 00:37 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache Ferdinand 12. -
Ferdinand 12 Ionosphere mission Nation: Norway. Agency: NDRE. Apogee: 122 km (75 mi).
1965 - 05:20 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.239UE. -
Auroral emissions Aurora mission Nation: USA. Agency: NASA. Apogee: 175 km (108 mi).
1965 - 08:28 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.8. -
Stellar Spectra Ultraviolet astronomy mission Nation: USA. Agency: KPNO. Apogee: 150 km (90 mi).
1965 - 17:53 GMT - Launch Site: Hammaguira. Launch Complex: Bechar. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-8. -
MPE Ba-16? Aeronomy mission Nation: France. Agency: CNES. Apogee: 404 km (251 mi).
1966 - 02:45 GMT - Launch Site: Yuma. Launch Complex: -. Launch Pad: -. Launch Vehicle: Martlet. Model: Martlet 2. -
Y-21 Meteorites mission Nation: USA. Agency: USA. Apogee: 142 km (88 mi).
1966 - 04:21 GMT - Launch Site: Yuma. Launch Complex: -. Launch Pad: -. Launch Vehicle: Martlet. Model: Martlet 2. -
Y-22 Meteorites mission Nation: USA. Agency: USA. Apogee: 111 km (68 mi).
1966 - 05:37 GMT - Launch Site: Yuma. Launch Complex: -. Launch Pad: -. Launch Vehicle: Martlet. Model: Martlet 2. -
Y-23 Meteorites mission Nation: USA. Agency: USA. Apogee: 111 km (68 mi).
1966 - 06:59 GMT - Launch Site: Yuma. Launch Complex: -. Launch Pad: -. Launch Vehicle: Martlet. Model: Martlet 2. -
Y-24 Meteorites mission Nation: USA. Agency: USA. Apogee: 147 km (91 mi).
1967 - 03:00 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: RH. Model: RH-75. LV Configuration: RH-75 1. -
TERLS-54 test Nation: India. Agency: ISRO. Apogee: 9.00 km (5.50 mi). First RH-75 launch.
1967 - 04:00 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: RH. Model: RH-75. LV Configuration: RH-75 2. -
Test mission Nation: India. Agency: ISRO. Apogee: 9.00 km (5.50 mi).
1967 - 10:42 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.228CG. -
AS&E X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 144 km (89 mi).
1968 - -
Soyuz spacesuit review Nation: USSR. Program: Lunar L1, Soyuz. Spacecraft: Yastreb, Soyuz 7K-L1. Flight: Soyuz 3, Soyuz 4, Soyuz 5, Soyuz 4/5. Kamanin attends an Yastreb spacesuit review with VVS doctors. The suit removes 200 cal/hour, but when the cosmonaut is exerting himself, he will generate 3 to 4 times more than this. So the cabin is chilled to 18 deg C prior to the EVA, and there will be lots of pauses during preparations to exit the spacecraft. The L1 cosmonaut-engineers at the meeting have little zero-G experience, and need to get a lot more. The new oxygen generating system for the L1 is still not complete. It will be 6 to 8 kg lighter than the old system (using calcium instead of the old material). Mishin insists that the new system should be completed and installed. Ground qualification testing will be completed on 1 January, but the system will not be flight-proven - Kamanin believes it needs test on low earth orbit missions before being adopted for lunar flights. Beregovoi's experience on Soyuz 3 is reviewed. He needed more time to adapt to zero-G before being required to attempt a docking. He had the impression he was upside-down and had intestinal tract problems.
1968 - -
Soviet manned circumlunar flight set for February Nation: USSR. Program: Soyuz, Lunar L1. Spacecraft: Soyuz 7K-OK, Soyuz 7K-L1. Flight: Soyuz 4, Soyuz 5, Soyuz 7K-L1 mission 1, Soyuz 4/5. Titov still would prefer to be a test pilot, not a cosmonaut. The Soyuz group is scheduled to complete their training and to depart for the cosmodrome on 20 December for final preparations. Leonov's L1 group is to complete their training on 20 January 1969, then depart to the cosmodrome for a flight to the moon in February.
1968 - 07:08 GMT - Launch Site: Johnston Island. Launch Complex: LE1. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2J. LV Configuration: Thor DSV-2J 252. -
AFP-437 combat evaluation interceptor mission Nation: USA. Agency: USAF. Apogee: 1,158 km (719 mi).
1968 - 11:24 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.283GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 120 km (70 mi).
1968 - 13:24 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.284GM. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi).
1968 - 22:45 GMT - Launch Site: Cape Canaveral. Launch Complex: LC43. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 75 km (46 mi).
1969 -
1969 - 00:30 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL801. -
Solar ultraviolet Spectrum / PHC Solar ultraviolet and x-ray mission Nation: UK. Agency: BAC. Apogee: 242 km (150 mi).
1969 - 03:54 GMT -
1970 -
1970 - 19:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.458UA. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1970 - 22:19 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.901-6. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 150 km (90 mi).
1970 - 22:19 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.917-1. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 170 km (100 mi).
1970 - 22:23 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.896. -
Mass spectrometer Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 130 km (80 mi).
1970 - 22:23 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.895. -
Mass spectrometer Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 121 km (75 mi).
1970 - 22:26 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.917-3. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 166 km (103 mi).
1970 - 22:26 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.917-2. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 158 km (98 mi).
1970 - 23:29 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.460UM. -
UM Pitot 52 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 181 km (112 mi).
1971 - 07:21 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.57GG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1971 - 08:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.58GG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1971 - 18:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47114-106.
1972 - 04:54 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 S94. -
ESRO S94 X-ray Astronomy mission Nation: Europe. Agency: ESRO. Apogee: 210 km (130 mi).
1972 - 17:07 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.13GT. -
Test mission Nation: USA. Agency: NASA. Apogee: 250 km (150 mi).
1973 - Launch Site: Baikonur. Launch Complex: LC104. Launch Pad: -. Launch Vehicle: R-36M. -
Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1973 - 12:29 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1974 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 HRV. Launch Vehicle: Jaguar. Model: Jabiru 3. LV Configuration: Jabiru 3 J-7. -
Test mission Nation: UK. Agency: RAE. Apogee: 30 km (18 mi).
1974 - 09:46 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Chemical release/Plasma mission Nation: USSR. Apogee: 150 km (90 mi).
1974 - 11:59 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1975 - 02:06 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2910. LV Configuration: Delta 2910 604/D117.
1978 - 17:23 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3TA. -
Demonstration and shakedown operations launch Nation: USA. Agency: RN. Apogee: 1,000 km (600 mi).
1981 - 01:37 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 3910/PAM. LV Configuration: Delta 3910/PAM 640/D158.
1981 - 08:30 GMT - Launch Site: Kapustin Yar. Launch Complex: LC107/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47193-468.
1985 - 10:19 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Taurus Nike Tomahawk. LV Configuration: Taurus Nike Tomahawk NASA 38.09UE. -
CRRES Test Plasma mission Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).
1986 - 12:09 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
1987 - 23:47 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2.
1988 - 18:30 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.44DS. -
HRTS 6 / ASL-San Marco Test / solar mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).
1989 - 02:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 8B. LV Configuration: Black Brant 8B NASA 27.123UG. -
Astronomy mission Nation: USA. Agency: NASA. Apogee: 340 km (210 mi).
1990 - Launch Vehicle: Shuttle. -
Backup shuttle carrier aircraft. Nation: USA. In the event of loss of N905NA, which has been in service for 15 years, NASA purchases a second 747, N911NA, for use as a shuttle carrier.
1990 - 02:33 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
1990 - 04:00 GMT - Launch Site: Baikonur. Launch Complex: LC131. Launch Pad: -. Launch Vehicle: UR-100N. Model: Rokot. LV Configuration: Rokot-K No. 1L.
1990 - 23:11 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 42P. LV Configuration: Ariane 42P V40.
1990 -
1991 - 08:05 GMT - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-36M. Model: R-36M2 15A18M. -
Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1991 - 19:15 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1992 - 15:29 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1993 - 01:17 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 44LP. LV Configuration: Ariane 44LP+ V61.
1994 - 00:39 GMT - Launch Site: Baikonur. Launch Complex: LC200/39. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 371-01.
1995 - 17:00 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 N. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.126UG. -
Astronomy mission Nation: USA. Agency: NASA GSFC. Apogee: 300 km (180 mi).
1995 -
1998 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aries. LV Configuration: Aries TTV-1. -
TTV-1 Target mission Nation: USA. Agency: USA SMDC. Apogee: 322 km (200 mi).
1998 - 06:40 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K. LV Configuration: Proton-K 395-01. -
Zarya Nation: USA. Program: ISS. Payload: FGB 77KM s/n 175-01. Class: Manned. Type: Space station. Spacecraft: ISS Zarya. Manufacturer: Khrunichev. Agency: NASA. Perigee: 397 km (246 mi). Apogee: 402 km (249 mi). Inclination: 51.60 deg. COSPAR: 1998-067A. USAF Sat Cat: 25544. This was the first launch in the assembly of the International Space Station. The Zarya FGB was funded by NASA and built by Khrunichev in Moscow under subcontract from Boeing for NASA. Its design from the TKS military station resupply spacecraft of the 1970’s and the later 77KS Mir modules. Zarya included a multiple docking adapter, a pressurised cabin section, and a propulsion/instrument section with a rear docking port. Initial orbit was 176 lm x 343 km x 51.6 degrees. By November 25 it had manoeuvred to a 383 km x 396 km x 51.7 degree orbit, awaiting the launch of Shuttle mission STS-88 which docked the Unity node to it.
1999 - 01:35 GMT - Launch Site: Sriharikota. Launch Complex: -. Launch Pad: -. Launch Vehicle: RH. Model: RH-300 Mk II. -
LMS Ionosphere / meteorology mission Nation: India. Agency: ISRO. Apogee: 135 km (83 mi).
2000 - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47165-631. FAILURE: Second stage failed to restart at apogee. -
QuickBird 1 Nation: USA. Mass: 950 kg (2,090 lb). Class: Surveillance. Type: Civilian. Spacecraft: Early Bird. Manufacturer: Ball Aerospace, Boulder. Agency: EarthWat. Perigee: 80 km (49 mi). Apogee: 614 km (381 mi). Inclination: 65.70 deg. Period: 91.49 min. COSPAR: 2000-074A. USAF Sat Cat: 26617. Decay Date: 2000-11-21. The Kosmos-3M second stage entered an 81 x 614 km x 65.8 deg orbit but failed to restart at apogee, and reentered at the next perigee over Uruguay. The loss of the QuickBird 1 satellite was a heavy blow to EarthWatch Inc. QuickBird1 was a 1-m resolution commerical imaging satellite using a Ball Aerospace BCP-2000 bus. Their earlier satellite, EarlyBird, failed after a few days in orbit in December 1997. EarthWatch's rival, SpaceImaging, lost one satellite as well but its second Ikonos was operating in orbit.
2002 - 01:33 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Orion. LV Configuration: Terrier Orion NASA 41.039DP. -
VALPE (fairing) test Nation: USA. Agency: NASA GSFC. Apogee: 135 km (83 mi).
2002 - 22:39 GMT - Launch Site: Cape Canaveral. Launch Complex: LC37B. Launch Pad: SLC37B. Launch Vehicle: Delta IV. Model: Delta IV Medium+ (4.2). LV Configuration: Delta 4M+(4,2) D4-1 (293) 4240. -
Eutelsat W5 Nation: Europe. Program: Eutelsat. Payload: W1A. Mass: 3,170 kg (6,980 lb). Class: Communications. Spacecraft: Spacebus 3000. Manufacturer: Alcatel Space. Agency: Eutelsat. Perigee: 35,788 km (22,237 mi). Apogee: 35,801 km (22,245 mi). Inclination: 0.10 deg. Period: 1,436.50 min. COSPAR: 2002-051A. USAF Sat Cat: 27554. Maiden flight of the Delta 4 EELV booster, delayed due to development problems from January and November 2001, April 30, July 15, August 31, October 9, November 3, 16 and 19. EUTELSAT W5 was a European (EUTELSAT Consortium) geostationary communication spacecraft. EUTELSAT W5 was to provide voice, video, and Internet services to all countries in western Europe, central Asia, and the Indian subcontinent through its 24 Ku-band transponders after being parked over 70.5° E longitude. As of 2007 Mar 10 located at 70.55E drifting at 0.004W degrees per day.
2004 - -
Cassini, Post Titan A Apoapsis Maneuver (OTM-6), Successful Nation: USA. Spacecraft: Cassini.
2004 - 17:16 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: SLC17A. Launch Vehicle: Delta. Model: Delta 7320-10C. LV Configuration: Delta 7320-10C D309. -
Swift Nation: USA. Payload: SA-200LL. Mass: 1,331 kg (2,934 lb). Class: Astronomy. Type: Gamma. Spacecraft: Swift. Manufacturer: Spectrum Astro. Agency: NASA. Perigee: 584 km (362 mi). Apogee: 604 km (375 mi). Inclination: 20.60 deg. Period: 96.60 min. COSPAR: 2004-047A. USAF Sat Cat: 28485. NASA Medium-class Explorer satellite dedicated to study of gamma ray bursts, the third after the IMAGE and WMAP satellites. Delayed from December 5 and 29, 2003, January 14, April 29, July 15, September 1, October 7 and 26, November 8, 11, 17, 18 and 19.
2005 - -
Hayabusa (MUSES-C), first Asteroid 25143 Itokawa Sample Collection, Failed Nation: Japan. Spacecraft: Hayabusa.
Born on this day in: - 1913 - Li Xun. Chinese Engineer. Birth City: Shaoyang. Birth State: Hunan. Birth Country: China.
- 1968 - James Patrick Dutton Jr. American Pilot Astronaut. Birth City: Eugene. Birth State: Oregon. Birth Country: USA.
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