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1877 -

  • Asaph Hall's Discovery of Phobos (Mars Moon) Nation: USA.

1933 - Launch Vehicle: GIRD-09.
  • First Russian hybrid rocket launch. Nation: USSR. Apogee: 0.40 km (0.25 mi).

    Russian hybrid propellant rocket, designed by M. K. Tikhonravov, successfully flown. Reached 400 m; design altitude of 5000 m not reached due to loss of pressure integrity of the motor flank.

1943 - Launch Site: Peenemuende. Launch Complex: -. Launch Pad: -. Launch Vehicle: V-2.
  • Peenemünde attacked by RAF. Nation: Germany.

    The Royal Air Force attacked Germany's Peenemünde Rocket Research Center, causing heavy damage and delaying V-weapon program by months.

    With the V-2 development program already in crisis, the Allies launch a massive bombing raid against Peenemuende. On that evening test pilot Hanna Reitsch was visiting the launch site. At 23:30 the air raid siren sounded. 600 British bombers drop 1500 tonnes of ordnance on the launch centre. However many bombs fell in the ocean around the peninsula, or buried themselves harmlessly in sand dunes. The resident area was hardest hit, while the Luftwaffe station at Peenemuende West was not touched. 47 British bombers were shot down - they were told before the raid that this was the most important mission of the war, and that their commanders would accept a 50% loss rate. 735 people were killed in the raid on the ground, including 178 of the 4000 inhabitants of the residential area. A large number of the foreign slave workers in the Trassenheide concentration camp barracks were also killed.

    After the tremendous raid the rocket team wander around the devastated facility, half-clothed, the buildings bathed in a weird light and everything covered in fine sand, as if flour was dropped over everything. Thiel and Walther - the two leading rocket engineers in Germany - were killed in the raid, and virtually all major facilities were damaged. The saving grace was that the soft sand of Peenemuende attenuated the blast of many bombs. Nine bombs hit the main assembly hall, but while there was splinter damage to some of the machine tools, there was no decisive hit that would prevent production from continuing. It was estimated that operations could resume in 4 to 6 weeks.

    The raid was not unexpected. The high altitude contrails of the V-2 test launches were called 'frozen lightning' and could be seen from Sweden on clear days. The location and purpose of Peenemuende appeared in a crossword puzzle in a illustrated magazine published in central Germany in early 1943. British reconnaissance flights to locate the launch facilities had been recognised for what they were.

    This raid, together with the bombing of V-2 production lines at the Zeppelinwerke in Friedrichshafen and the Raxwerke in Wiener Neustadt convinced Saur to reduce the V-2 production rate goal to 900 per month.

1950 - 15:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee RTV-N-10. LV Configuration: Aerobee RTV-N-10 A18.
  • Mass spectrometer Aeronomy mission Nation: USA. Agency: APL. Apogee: 101 km (62 mi).

    Composition research. Launched at 0845 local time. Reached 101.4 km.

1958 - Launch Site: China Lake. Launch Complex: G-2. Launch Pad: -. Launch Vehicle: Project Pilot. LV Configuration: Project Pilot-1. FAILURE: Failure.
  • Test mission Nation: USA. Agency: USN. Apogee: 0 km ( mi).

1958 - 12:18 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Able I. LV Configuration: Thor Able I 127. FAILURE: Thor exploded after 77 sec.
  • Pioneer (1) Nation: USA. Program: Pioneer. Payload: Pioneer / Able 1. Mass: 38 kg (83 lb). Class: Planetary. Type: Lunar. Spacecraft: Pioneer 0-1-2. Agency: U.S. Air Force. Apogee: 16 km (9 mi). COSPAR: F580817B. Decay Date: 1958-08-17.

    First US lunar attempt. The first US Air Force lunar probe, using a Thor-Able booster. An explosion ripped it apart 77 seconds after launch.

1959 - 09:18 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.13CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 236 km (146 mi).

    NIKE-ASP sounding rocket provided geophysical information on wind activity between 80 and 300 km high was launched successfully from NASA Wallops Station.

1960 - Launch Site: Aberporth. Launch Complex: -. Launch Pad: -. Launch Vehicle: Jaguar. Model: Jaguar 1. LV Configuration: Jaguar 1 G1.
  • Test mission Nation: UK. Agency: RAE. Apogee: 20 km (12 mi).

1960 - 10:42 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AA6.427.
  • Firefly SUSAN Aeronomy mission Nation: USA. Agency: USAF. Apogee: 114 km (70 mi).

1961 - 14:29 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18A. Launch Pad: LC18A. Launch Vehicle: Scout. Model: Blue Scout Jr. LV Configuration: Blue Scout Jr O-1.
  • HETS Magnetosphere mission Nation: USA. Class: Earth. Type: Magnetosphere. Agency: USAF. Apogee: 225,000 km (139,000 mi).

1962 -
  • Carl Sagan warned scientists of need for sterilization of lunar spacecraft Nation: USA. Program: Apollo.

    Carl Sagan, University of California astronomer, warned scientists at a lunar exploration conference, Blacksburg, Va., of the need for sterilization of lunar spacecraft and decontamination of Apollo crewmen, pointing out that Lunik II and Ranger IV probably had deposited terrestrial microorganisms on the moon. Even more serious, he said, was the possibility that lunar microorganisms might be brought to earth where they could multiply explosively.

1963 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1964 -
  • Apollo X spacecraft to be used in Earth orbit for extended duration biomedical and scientific flights. Nation: USA. Spacecraft: Apollo X.

    MSC's Spacecraft Integration Branch proposed an Apollo 'X' spacecraft to be used in Earth orbit for biomedical and scientific missions of extended duration. The spacecraft would consist of the lunar Apollo spacecraft and its systems, with minimum modifications consisting- of redundancies and spares. The concept provided for a first-phase mission which would consider the Apollo 'X' a two-man Earth-orbiting laboratory for a period of 14 to 45 days. The spacecraft would be boosted into a 370-km orbit by a Saturn IB launch vehicle. - Additional details.

1964 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 556.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1964 - 00:29 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.58DA.
  • K64-S-4 Air sampling Aeronomy mission Nation: USA. Agency: NASA. Apogee: 124 km (77 mi).

1964 - 00:49 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.141GA.
  • K64-G-4 Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 132 km (82 mi).

1964 - 12:55 GMT - Launch Site: Ascension. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.116GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 122 km (75 mi).

1965 - 00:05 GMT - Launch Site: Pameungpeuk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8. LV Configuration: Kappa 8 K-8(L).
  • SK-8-3 (Grenades) Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 100 km (60 mi).

1965 - 20:59 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 449 / Agena D SS-01B 1618.
  • KH-4A 1023 Nation: USA. Payload: KH-4A s/n 1023 / Agena D 1618. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 179 km (111 mi). Apogee: 399 km (247 mi). Inclination: 70.00 deg. Period: 90.30 min. COSPAR: 1965-067A. USAF Sat Cat: 1513. Decay Date: 1965-10-11.

    KH-4A. Program anomaly caused the fore camera to cease operation during revolutions 103-132.

1966 - 03:39 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB ALF-VB-08.
  • MPE Barium release Aeronomy / Barium release mission Nation: Germany. Agency: MPI. Apogee: 390 km (240 mi).

1966 - 15:20 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta E1. LV Configuration: Thor Delta E1 462/D40.
  • Pioneer 7 Nation: USA. Program: Pioneer. Payload: Pioneer B. Mass: 63 kg (138 lb). Class: Solar. Spacecraft: Pioneer 6-7-8-9-E. Agency: NASA ARC. Perigee: 246 km (152 mi). Apogee: 993 km (617 mi). Inclination: 33.00 deg. Period: 97.20 min. COSPAR: 1966-075A. USAF Sat Cat: 2398.

    Monitored solar wind, cosmic rays. SOLAR ORB. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).

1966 - 16:30 GMT - Launch Site: CELPA. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Boosted Dart. LV Configuration: Boosted Dart EXAMETNET 8.
  • Aeronomy mission Nation: USA. Agency: CONAE. Apogee: 194 km (120 mi).

1966 - 19:50 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.02GT-GI-GS.
  • Test / ionosphere-solar mission Nation: USA. Agency: NASA. Apogee: 358 km (222 mi).

1967 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 466.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1968 - Launch Vehicle: Saturn V.
  • Webb approves Apollo 8 lunar orbit mission for December - but no public announcement until after a successful Apollo 7 flight. Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Flight: Apollo 7, Apollo 8, Apollo 9.

    Phillips and Hage visited MSC, bringing the news that Webb had given clear-cut authority to prepare for a December 6 launch, but that they could not proceed with clearance for lunar orbit until after the Apollo 7 flight, which would be an earth-orbital mission with basic objectives of proving the CSM and Saturn V systems. Phillips said that Webb had been "shocked and fairly negative" when he talked to him about the plan on August 15. Subsequently, Paine and Phillips sent Webb a lengthy discourse on why the mission should be changed, and it was felt he would change his mind with a successful Apollo 7 mission.

1969 - Launch Site: Kagoshima. Launch Complex: M. Launch Pad: -. Launch Vehicle: Mu. Model: Mu-3D. LV Configuration: Mu-3D M-3D-1.
  • Test mission Nation: Japan. Agency: ISAS. Apogee: 160 km (90 mi).

1970 - 05:38 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Venera 7 Nation: USSR. Program: Venera. Payload: 3V (V-70) s/n 630. Mass: 1,180 kg (2,600 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 3V (V-70). Agency: MOM. COSPAR: 1970-060A. USAF Sat Cat: 4489. Decay Date: 1970-12-15.

    Venera 7 was launched from an earth parking orbit towards Venus to study the Venusian atmosphere and other phenomena of the planet. Venera 7 entered the atmosphere of Venus on December 15, 1970, and a landing capsule was jettisoned. After aerodynamic braking, a parachute system was deployed. The capsule antenna was extended, and signals were returned for 35 min. Another 23 min of very weak signals were received after the spacecraft landed on Venus. The capsule was the first man-made object to return data after landing on another planet.

1970 - 16:16 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3P-2.
  • PEM-2 operational test launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1972 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Sprint. LV Configuration: Sprint ABM FLA-70. FAILURE: Failure.
  • Safeguard M2-42 Interceptor mission Nation: USA. Agency: USA. Apogee: 0 km ( mi).

1972 - 10:02 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure ISRO 5.16.
  • ISRO 5.16 Ionosphere mission Nation: India. Agency: ISRO. Apogee: 151 km (93 mi).

1973 -
  • X-24 Flight 30 Nation: USA. Payload: X-24B flight 2. Class: Manned. Type: Spaceplane. Spacecraft: X-24B. Crew: Manke.

    Maximum Speed - 722 kph. Maximum Altitude - 13720 m. Flight Time - 267 sec.

1973 - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67PM.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 - 04:49 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 2A. LV Configuration: Thor Burner 2A 291.
  • DMSP-Block-5B F4 Nation: USA. Program: DMSP. Payload: DMSP 7529. Mass: 195 kg (429 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 5B. Agency: USAF. Perigee: 779 km (484 mi). Apogee: 819 km (508 mi). Inclination: 98.90 deg. Period: 100.90 min. COSPAR: 1973-054A. USAF Sat Cat: 6787.

    Defense Meteorological Satellite Program.

1974 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • FOT GT45GM Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1974 - 05:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Ute Tomahawk. LV Configuration: Ute Tomahawk CRL A09.214-2.
  • Vehicle Potential test Nation: USA. Agency: USAF CRL. Apogee: 161 km (100 mi).

1975 - 06:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Pad: -. Launch Vehicle: S. Model: TT-210. LV Configuration: TT-210 TT-210-1F.
  • Test mission Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi).

1976 - 10:15 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210-11.
  • Aeronomy / ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 112 km (69 mi).

1977 - 17:10 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.182GA. FAILURE: Failure.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 198 km (123 mi).

1978 - 20:02 GMT - Launch Site: Baikonur. Launch Complex: LC200/40. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM. LV Configuration: Proton-K/DM 297-02. FAILURE: Stage 1 - vehicle failed at launch.
  • Ekran s/n 15L Nation: USSR. Payload: Ekran s/n 15L. Mass: 1,970 kg (4,340 lb). Class: Communications. Spacecraft: Ekran. Agency: RVSN. COSPAR: F780817A.

1979 - 07:45 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1122 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 208 km (129 mi). Apogee: 227 km (141 mi). Inclination: 81.30 deg. Period: 88.90 min. COSPAR: 1979-075A. USAF Sat Cat: 11491. Duration: 13.00 days. Decay Date: 1979-08-30.

    Zenit-2M area survey photo reconnaissance satellite used for earth resources studies as part of 'Gektor-Priroda' project. Nauka subsatellite 31KS jettisoned into independent orbit in the course of the mission. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation.

  • Cosmos 1122 Nauka Nation: USSR. Class: Earth. Type: Magnetosphere. Spacecraft: Nauka. Agency: RVSN. COSPAR: 1979-075xx.

1979 - 21:15 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee F. LV Configuration: Astrobee F NASA 25.11AS.
  • Solar mission Nation: USA. Agency: NASA. Apogee: 225 km (139 mi).

1983 - 12:08 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. LV Configuration: Soyuz 11A511U Ts15000-302.
  • Progress 17 Nation: USSR. Program: Salyut 7. Payload: Progress s/n 119. Mass: 7,020 kg (15,470 lb). Class: Manned. Type: Logistics. Spacecraft: Progress. Agency: MOM. Perigee: 189 km (117 mi). Apogee: 242 km (150 mi). Inclination: 51.60 deg. Period: 88.80 min. COSPAR: 1983-085A. USAF Sat Cat: 14283. Duration: 31.48 days. Completed Operations Date: 1983-09-17 23:42:37 PM. Decay Date: 1983-09-17 23:42:37 PM. Flight: Salyut 7 EO-2.

    Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 19 Aug 1983 13:47:00 GMT. Undocked on 17 Sep 1983 11:44:00 GMT. Destroyed in reentry on 17 Sep 1983 23:43:00 GMT. Total free-flight time 2.57 days. Total docked time 28.91 days.

1989 -
  • Japanese Commercial Cosmonaut Training Group selected. Nation: Japan.

    Japanese journalists trained for a commercial flight to the Mir space station.

1990 - 10:00 GMT - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-36M. Model: R-36M2 15A18M.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1993 - 18:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.105GS.
  • SERTS-93 (05) Solar mission Nation: USA. Agency: NASA. Apogee: 312 km (193 mi).

1996 - 01:53 GMT - Launch Site: Tanegashima. Launch Complex: Y. Launch Pad: -. Launch Vehicle: H-2. Model: H-II. LV Configuration: H-II H-II-4F.
  • ADEOS Nation: Japan. Class: Earth. Type: Atmosphere. Spacecraft: ADEOS. Agency: NASDA. Perigee: 799 km (496 mi). Apogee: 800 km (490 mi). Inclination: 98.60 deg. Period: 100.90 min. COSPAR: 1996-046A. USAF Sat Cat: 24277.

  • JAS-2 Nation: Japan. Class: Communications. Spacecraft: Fuji. Agency: JARL. Perigee: 801 km (497 mi). Apogee: 1,323 km (822 mi). Inclination: 98.60 deg. Period: 106.50 min. COSPAR: 1996-046B. USAF Sat Cat: 24278.

    Japanese amateur radio satellite.

1996 - 13:18 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Soyuz TM-24 Nation: Russia. Program: Mir. Payload: Soyuz TM 11F732 s/n 73. Mass: 7,150 kg (15,760 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TM. Agency: RKA. Perigee: 378 km (234 mi). Apogee: 394 km (244 mi). Inclination: 51.70 deg. Period: 92.30 min. COSPAR: 1996-047A. USAF Sat Cat: 24280. Duration: 196.73 days. Decay Date: 1997-03-02. Crew: Andre-Deshays, Kaleri, Korzun. Flight: Mir EO-22, Mir Cassiopee, Mir NASA-1, Mir EO-21.

    Mir Expedition EO-22. Valeriy Korzun and Aleksandr Kaleri of the Russian Space Agency (RKA) Claudie Andre-Deshays of the French space agency CNES. This launch was the first of the Soyuz-U booster with a crew aboard following two launch failures of on unmanned flights. Soyuz docked with Mir's front port at 14:50:21 GMT on August 19; Mir was in a 375 x 390 km x 51.6 deg orbit.

    On Feb 7 at 16:28:01 GMT the EO-22 crew and American astronaut Linenger undocked the Soyuz TM-24 ferry from the front docking port, flew it around to the far side of the complex and redocked at the rear Kvant port at 16:51:27 GMT. This cleared the forward port for the arrival of the EO-23 crew, who brought with them German astronaut Reinhold Ewald on Feb 12.

1999 - 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.

  • 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.

  • 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.

  • 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.

2000 - 23:16 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 44LP. LV Configuration: Ariane 44LP-3 V131.
  • Brasilsat B-4 Nation: Brazil. Program: Brasilsat. Mass: 1,757 kg (3,873 lb). Class: Communications. Spacecraft: HS 376W. Manufacturer: Hughes Space and Communications, El Segundo. Agency: Embratel. Perigee: 35,776 km (22,230 mi). Apogee: 35,799 km (22,244 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2000-046A. USAF Sat Cat: 26469.

    Brasilsat B4 was a C-band geosynchronous communications satellite, replacing the 15-year-old Brasilsat A2 for the Brazilian communications company Embratel. Positioned in geosynchronous orbit at 75 deg W in 2000. As of 2 September 2001 located at 92.03 deg W drifting at 0.011 deg W per day. As of 2007 Mar 9 located at 70.08W drifting at 0.020W degrees per day.

  • Nilesat 102 Nation: Egypt. Mass: 1,827 kg (4,027 lb). Class: Communications. Spacecraft: Eurostar 2000. Manufacturer: Astrium, Toulouse (former Matra). Agency: Nilesat. Perigee: 35,775 km (22,229 mi). Apogee: 35,797 km (22,243 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2000-046B. USAF Sat Cat: 26470.

    Geosynchronous communications satellite of the Egyptian company Nilesat SA. The satellite joined Nilesat 101 in providing Ku-band broadcast services. Stationed at 7 deg W. Positioned in geosynchronous orbit at 7 deg W in 2000. As of 2 September 2001 located at 6.98 deg W drifting at 0.002 deg W per day. As of 2007 Mar 9 located at 6.97W drifting at 0.004W degrees per day.

2000 - 23:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 403B. LV Configuration: Titan 403B 4B-28 / K-25.
  • USA 152 Nation: USA. Payload: Onyx F1. Mass: 14,500 kg (31,900 lb). Class: Surveillance. Type: Radarsat. Spacecraft: Lacrosse. Manufacturer: Lockheed Martin Astronautics, Denver. Agency: NRO. Perigee: 689 km (428 mi). Apogee: 695 km (432 mi). Inclination: 68.00 deg. Period: 98.53 min. COSPAR: 2000-047A. USAF Sat Cat: 26473.

    The National Reconnaissance Office satellite was reported to be an Onyx (formerly Lacrosse) radar imaging spacecraft built by Lockheed Martin. The Titan second stage reached a 572 x 675 km x 68.0 deg orbit and separated from the payload. Amateur observers reported the payload has made two small maneuvers and by Aug 23 was in a 681 x 695 km x 68.1 deg orbit.

2005 - 07:06 GMT - Launch Site: Barents Sea Launch Area. Launch Complex: -. Launch Pad: 69.5 N x 34.2 E. Launch Vehicle: R-29. Model: Sineva. LV Configuration: Sineva VMF RF.
  • RSM-54 test Nation: Russia. Agency: VMF RF. Apogee: 1,000 km (600 mi).


Born on this day in:
  • 1952 - Thomas (Tom) John Hennen.  American Payload Specialist Astronaut. Birth City: Albany. Birth State: Georgia. Birth Country: USA.
  • 1953 - Dr Robert Brent Thirsk.  Canadian Payload Specialist Astronaut. Birth City: New Westminister. Birth State: British Columbia. Birth Country: Canada.

Died on this day in:
  • 1943 - Walter Thiel.  German Rocket engineer.
  • 2000 - Robert R Gilruth.  American Manager.

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