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1948 - 21:41 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee RTV-N-8. LV Configuration: Aerobee RTV-N-8 A6.

  • B field Magnetosphere mission Nation: USA. Agency: APL. Apogee: 114 km (70 mi).

    Magnetic field research. Launched at 1551 local time. Reached 114.3 km.

1957 - Launch Site: Cape Canaveral. Launch Complex: LC3. Launch Pad: -. Launch Vehicle: X-17. LV Configuration: X-17 VI-1 4-204-1A?.
  • 4-204-1A? re-entry vehicle test flight Nation: USA. Agency: USN. Apogee: 100 km (60 mi).

1959 -
  • Mercury small-scale escape-tower combinations launched Nation: USA. Program: Mercury. Spacecraft: Mercury.

    Two small-scale spacecraft escape-tower combinations were launched successfully at Wallops Island. On the next day a full-scale spacecraft escape system was launched. The complete sequence of events - escape system firing, escape tower jettisoning, parachute deployment, landing, and helicopter recovery - was satisfactory.

1959 - 21:18 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena A. LV Configuration: Thor Agena A 170 / Agena A 1018.
  • Discoverer 2 Nation: USA. Payload: KH-1 prototype / Agena A 1022. Mass: 743 kg (1,638 lb). Class: Surveillance. Type: Military. Spacecraft: KH-1. Agency: DARPA. Perigee: 239 km (148 mi). Apogee: 346 km (214 mi). Inclination: 89.90 deg. Period: 90.40 min. COSPAR: 1959-Gamma-1. USAF Sat Cat: 14. Decay Date: 1959-04-26.

    KH-1 prototype; tested capsule recovery techniques; did not carry camera; capsule recovery failed. Because of a timing error, the US believed that the capsule landed somewhere on the island of Spitsbergen, north of Norway, instead of landing in the recovery zone near Hawaii. The capsule was never found; and CIA officials suspect it may have been snatched by the Soviets. The search for this capsule formed the basis of the book and film 'Ice Station Zebra'.

    In the winter of 1960/1961, a US Discovery spy satellite capsule was found by loggers near Kalinin, 200 km north of Moscow. The loggers cracked it open with an axe. Sergei Khrushchev believed this to be the Discoverer 2 capsule. What was left was examined by Soviet engineers but didn’t reveal much information - it was a polished aluminium sphere, 30 cm in diameter, gilded on the exterior. Some said it was found as early as the winter of 1959.

1960 - 12:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar 257 AB002?.
  • Transit 1B Nation: USA. Program: Transit. Mass: 121 kg (266 lb). Class: Navigation. Spacecraft: Transit. Agency: DARPA. Perigee: 363 km (225 mi). Apogee: 644 km (400 mi). Inclination: 51.20 deg. Period: 94.60 min. COSPAR: 1960-Gamma-2. USAF Sat Cat: 31. Duration: 89.00 days. Decay Date: 1967-10-05.

    The Able-Star second stage demonstrated the first engine restart in space and the feasibility of using satellites as navigational aids. The first experimental Transit satellite to achieve orbit operated for 89 days. It transmitted on two frequency pairs to test the technique for refraction correction and to determine if the transmitted frequencies should be close together or far apart. It also tested a magnetic torque device for spacecraft attitude control - the first satellite to do so.

  • Dummy subsatellite Nation: USA. Payload: GRAB dummy. Mass: 18 kg (39 lb). Class: Sigint. Spacecraft: GRAB. Agency: USAF. COSPAR: 1960-Gamma-3. USAF Sat Cat: 33. Decay Date: 1960-07-17.

1960 - 17:15 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 1-4-9.
  • X-15A test Nation: USA. Agency: NASA/USAF. Apogee: 14 km (8 mi).

    Maximum Speed - 2018 kph. Maximum Altitude - 14630 m.

1962 - Launch Vehicle: N1.
  • N1 development slowed. Nation: USSR.

    Decree 'On restriction of work on the N1' was issued.

1963 -
  • Vostok plans in 1963. Nation: USSR. Spacecraft: Vostok.

    Decree 'On plans for Vostok launches in 1963' was issued.

1963 -
  • At a meeting with the VVS, Korolev outlines his revised plans for the next fights. Nation: USSR. Flight: Vostok 5, Vostok 6.

    He plans a male flight for 8 days, during which a woman would be sent aloft for 2 to 3 days.

1963 -
  • Decree issued for four Vostok flights in 1963. Nation: USSR. Spacecraft: Vostok. Flight: Vostok 5, Vostok 6.

    Decree issued by the Soviet ministers and Central Committee setting out four Vostok flights in 1963. Two are to be launched by 15 June.

1963 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • K-21 Titan Intercept Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1963 - Launch Site: Vandenberg. Launch Complex: 395-A3. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-1.
  • NTMP K-21 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi).

1963 - 11:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1.
  • Cosmos 14 Nation: USSR. Payload: DS-U / Omega-1. Class: Technology. Spacecraft: Omega. Agency: MO SSSR. Perigee: 250 km (150 mi). Apogee: 410 km (250 mi). Inclination: 48.90 deg. Period: 91.10 min. COSPAR: 1963-010A. USAF Sat Cat: 567. Decay Date: 1963-08-29.

    Tested VNIIEM electric gyrodyne satellite orientation technology.

1964 -
  • Construction of nine Voskhod spacecraft approved. Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1, Voskhod 2.

    Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On approval of work on four Voskhods and five EVA-equipped Vykhods' was issued. Work on the 3KV (three crew) and 3KD (two crew plus inflatable airlock) versions of the basic Vostok spacecraft began.

1964 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-06.
  • FU-104B Probe / Na Aeronomy mission Nation: France. Agency: CNES. Apogee: 425 km (264 mi).

1964 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C59.
  • Sodium / TMA release Aeronomy mission Nation: France. Agency: CNES. Apogee: 151 km (93 mi).

1964 - 19:00 GMT - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 734.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1965 - 04:05 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 60.0 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.67UA.
  • UM Pitot 13 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 150 km (90 mi).

    Launched at 1965 Croatan MRF Expedition LP39 - - Latitude: 60.00 S - Longitude: 78.00 W.

1965 - 16:00 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 60.0 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.27UA.
  • UM Pitot 14 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 146 km (90 mi).

    Launched at 1965 Croatan MRF Expedition LP39 - - Latitude: 60.00 S - Longitude: 78.00 W.

1965 - 17:10 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 60.0 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.186UE.
  • UNH Particles Plasma mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

    Launched at 1965 Croatan MRF Expedition LP39 - - Latitude: 60.00 S - Longitude: 78.00 W.

1965 - 19:06 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 59.9 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.101UA.
  • Composition Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

    Launched at 1965 Croatan MRF Expedition LP40 - - Latitude: 59.92 S - Longitude: 77.97 W.

1965 - 21:00 GMT - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1165.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1965 - 21:00 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 851.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1966 - Launch Vehicle: Titan. Model: Titan 2.
  • The Electrical Interface Integrated Validation and Joint Guidance and Control Test began. Nation: USA. Flight: Gemini 9.

    The Electrical Interface Integrated Validation and Joint Guidance and Control Test began after Gemini launch vehicle 9 and spacecraft No. 9 were electrically mated. These activities were completed April 15. The Joint Combined Systems Test was run April 19.

1967 - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 4S. LV Configuration: Lambda 4S L-4S-3. FAILURE: Fourth stage failed to ignite.
  • Ohsumi 3 Nation: Japan. Payload: L-4S-3. Mass: 26 kg (57 lb). Class: Technology. Spacecraft: Ohsumi. Agency: ISAS. Apogee: 200 km (120 mi). COSPAR: F670413A. Decay Date: 1967-04-13.

1967 - 06:22 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AF6.561.
  • Ion trap Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 116 km (72 mi).

1967 - 07:24 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL AF08.647.
  • Sphere / TMA Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 175 km (108 mi).

1969 - 00:33 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 2B. LV Configuration: Dragon 2B D-255.
  • FU-182 Ions / Electric field Ionosphere mission Nation: France. Agency: CNES. Apogee: 399 km (247 mi).

1969 - 02:24 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3A Agena D. LV Configuration: SLV-3A Agena D 5502A / Agena D 2802.
  • Canyon 2 Nation: USA. Payload: Canyon 2 / Agena D. Mass: 700 kg (1,540 lb). Class: Sigint. Spacecraft: Canyon. Agency: USAF. Perigee: 32,670 km (20,300 mi). Apogee: 39,270 km (24,400 mi). Inclination: 9.90 deg. Period: 1,445.00 min. COSPAR: 1969-036A. USAF Sat Cat: 3889.

    Positioned in geosynchronous orbit over the Indian Ocean. Last known longitude (31 December 1969) 99.24 deg W drifting at 2.246 deg W per day.

1969 - 14:04 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.326GE.
  • Magnetospheric mission Nation: USA. Agency: NASA. Apogee: 155 km (96 mi).

1970 -
  • Tenth anniversary of the Gagarin Centre. Nation: USSR.

    A big celebration is held at Star City on the occasion of the tenth anniversary of the founding of the Gagarin Centre.

1970 - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67P.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 - 12:34 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.321UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1971 -
  • Cosmodrome jammed for series of historic launches. Nation: USSR. Program: Salyut, Lunar L3. Spacecraft: Salyut 1. Flight: Soyuz 10.

    Nikolayev and others are flying to the cosmodrome. All of the cosmonauts except Volynov will be present for the historic launch of the first space station., the first crew to the station, and the N1 launch planned for 1 May. Kamanin has an argument with the cosmonauts on the necessity of working out on the KTF trainer during the mission.

1972 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT88M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1972 - 01:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.107-1.
  • Mass Spectrometer Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 120 km (70 mi).

1972 - 01:16 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.894.
  • Mass Spectrometer Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 128 km (79 mi).

1972 - 01:30 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL A08.013-1.
  • Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 214 km (132 mi).

1972 - 01:45 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.217-2.
  • Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 190 km (110 mi).

1972 - 04:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.215-1.
  • Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 219 km (136 mi).

1972 - 04:15 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.921-4.
  • Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 164 km (101 mi).

1972 - 07:50 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.921-2.
  • TMA / Grenade Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 160 km (90 mi).

1972 - 09:30 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.921-6.
  • TMA Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 175 km (108 mi).

1974 - 23:33 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2914. LV Configuration: Delta 2914-C 588/D101.
  • Westar 1 Nation: USA. Program: Westar. Mass: 500 kg (1,100 lb). Class: Communications. Spacecraft: HS 333. Agency: WUTC. Perigee: 35,886 km (22,298 mi). Apogee: 35,900 km (22,300 mi). Inclination: 13.40 deg. Period: 1,441.50 min. COSPAR: 1974-022A. USAF Sat Cat: 7250. Completed Operations Date: 1983-05-02.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Americas at 99 deg W in 1974-1982; over the Americas at 100 deg W in 1982; over the Americas at 97 deg W in 1982; over the Americas at 79 deg W in 1982-1983 As of 5 September 2001 located at 85.83 deg W drifting at 1.372 deg W per day. As of 2007 Mar 10 located at 89.54E drifting at 1.381W degrees per day.

1975 - 00:51 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 71F / Star-17A. FAILURE: First stage failure due to explosion in flame pit at lift-off.
  • P 72-2 Nation: USA. Class: Technology. Type: Military. Spacecraft: P 72. Agency: U.S. Air Force. COSPAR: F750413A. Decay Date: 1975-04-12.

    A lack of deluge water and collection in the flame bucket of a kerosene/liquid oxygen gel led to the explosion of the gel on lift-off, damaging one of the Atlas engines and leading to complete engine failure during the ascent.

1975 - 08:15 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.174GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 299 km (185 mi).

1975 - 09:46 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Castor. LV Configuration: Castor DNA EX531.43-1.
  • EXCEDE Active plasma mission Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).

1975 - 10:38 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.173GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 299 km (185 mi).

1976 - 17:16 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 814 Nation: USSR. Mass: 1,400 kg (3,000 lb). Class: Military. Type: ASAT. Spacecraft: IS-A. Agency: PKO. Perigee: 118 km (73 mi). Apogee: 480 km (290 mi). Inclination: 65.10 deg. Period: 90.50 min. COSPAR: 1976-034A. USAF Sat Cat: 8806. Decay Date: 1976-04-13.

    ASAT interceptor. After intercept with target deorbited using on-board engine.

1978 - 19:22 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Orion. LV Configuration: Nike Orion NASA 31.06UE.
  • SSC S27 TWILIGHT Test / aeronomy mission Nation: USA. Agency: NASA. Apogee: 153 km (95 mi).

1979 - 22:05 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.33AS-US.
  • Solar mission Nation: USA. Agency: NASA. Apogee: 268 km (166 mi).

1983 - 09:06 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Sounding Rocket. LV Configuration: Sergeant GL A30.276.
  • FWIF VI Auroral mission Nation: USA. Agency: USAF GL. Apogee: 140 km (80 mi).

1984 - 13:14 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki T 1-0883.
  • Aeronomy mission Nation: USA. Agency: NASA WFC. Apogee: 110 km (60 mi).

1984 -
  • Landing of STS-41-C Nation: USA. Program: STS. Flight: STS-41-C.

    STS-41-C landed at 13:38 GMT.

1985 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: Zenit. Model: Zenit-2. FAILURE: Failure.
  • R&D suborbital Zenit launch vehicle test failure Nation: USSR. Agency: UNKS.

1986 - 09:14 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 10. LV Configuration: Black Brant X NASA 35.016GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 977 km (607 mi).

1990 - 18:53 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 2072 Nation: USSR. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-4KS1. Agency: MOM. Perigee: 232 km (144 mi). Apogee: 270 km (160 mi). Inclination: 64.70 deg. Period: 89.50 min. COSPAR: 1990-033A. USAF Sat Cat: 20568. Duration: 225.00 days. Decay Date: 1990-11-21.

    Photo/digital surveillance.

1990 - 22:28 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 6925-8. LV Configuration: Delta 6925-8 D194.
  • Palapa B2R Nation: Indonesia. Program: Palapa. Mass: 1,200 kg (2,600 lb). Class: Communications. Spacecraft: HS 376. Agency: Perumtel. Perigee: 35,784 km (22,235 mi). Apogee: 35,795 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.30 min. COSPAR: 1990-034A. USAF Sat Cat: 20570.

    Refurbished Palapa B2 retrieved by STS-51A; 107.7 deg E. Communication services for Indonesia, the Association of South-East Asian Nations (ASEAN), and Papua New Guinea. Launch time 2227:59.719 Z. Launch complex 17, ETR. Positioned in geosynchronous orbit at 108 deg E in 1990-1999 As of 29 August 2001 located at 42.49 deg E drifting at 0.002 deg E per day. As of 2007 Mar 9 located at 163.55E drifting at 2.663W degrees per day.

1991 - 00:09 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925 D204.
  • ASC-2 / Spacenet F4 Nation: USA. Program: GTE. Mass: 1,350 kg (2,970 lb). Class: Communications. Spacecraft: ASC. Agency: Contel. Perigee: 35,780 km (22,230 mi). Apogee: 35,794 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.20 min. COSPAR: 1991-028A. USAF Sat Cat: 21227.

    Commercial business communications; stationed at 101 deg W. C, Ku band communications satellite. Positioned in geosynchronous orbit at 101 deg W in 1991-1999; 81 deg W in 2000. As of 6 September 2001 located at 172.04 deg E drifting at 0.007 deg W per day. As of 2007 Mar 9 located at 34.51E drifting at 2.539W degrees per day.

1994 - 06:04 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36B. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas I. LV Configuration: Atlas I AC-73 / Centaur I 5053.
  • GOES 8 Nation: USA. Payload: GOES I. Mass: 2,105 kg (4,640 lb). Class: Earth. Type: Weather. Spacecraft: GOES-Next. Agency: NOAA. Perigee: 35,770 km (22,220 mi). Apogee: 35,807 km (22,249 mi). Inclination: 0.10 deg. Period: 1,436.20 min. COSPAR: 1994-022A. USAF Sat Cat: 23051.

    Geostationary Environmental Satellite. Stationed at 75 deg W. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). Launch vehicle put payload into supersynchronous earth orbit with MRS trajectory option. Positioned in geosynchronous orbit at 90 deg W in 1994-1995; 75 deg W in 1995-1999 As of 5 September 2001 located at 74.78 deg W drifting at 0.019 deg E per day. NASA announced that GOES-8 was "de-orbited" (presumably moved to a sub-synchronous orbit) on May 5, 2004 after 10 years of service. As of 2007 Mar 11 located at 87.46E drifting at 4.935W degrees per day.

2002 - 14:09 GMT -
  • EVA STS-110-2 Nation: USA. Program: ISS. Crew: Ross, Morin. Flight: STS-110. EVA Duration: 0.32 days.

    The spacewalk was from 1405 to 2139 UTC. The astronauts attached the aft MTS struts and deployed the second trailing umbilical.

2004 - 03:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Mk 70 Orion. LV Configuration: Terrier Mk 70 Orion NASA 12.54GT.
  • NMACS test Nation: USA. Agency: NASA GSFC. Apogee: 122 km (75 mi).

2006 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: SR19/SR19.
  • CMCM-1 Target mission Nation: USA. Agency: USA SMDC/MDA. Apogee: 200 km (120 mi).

    A two-stage SR19 rocket was flown from the Kaui Test Facility in the Pacific Missile Range Facility. The payload included the deployment of complex countermeasures, a mock reentry vehicle, an onboard sensor package. This series of radar certification flight was initially part of the Block 2004 effort.


Born on this day in:

Died on this day in:
  • 2002 - Aleksandr Yakovlevich Kramarenko.  Ukrainian Pilot Cosmonaut. Cause of Death: Heart attack at a railway station.
  • 2004 - Joachim Wilhelm Muehlner.  German Rocket engineer.
  • 2008 - Vladimir Mkrtychovich Gevorkyan.  Russian Engineer Cosmonaut.

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