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1670 -

  • Nova 1670 Vulpeculae Nation: France.

1945 -
  • Von Braun team to be brought to the US. Nation: USA.

    U.S. Secretary of State Cordell Hull approved the transfer of von Braun's German rocket specialists to the United States. This transfer was known as Operation Paperclip.

1951 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-1. Model: R-1. LV Configuration: R-1 IIIB-3.
  • Operational test Nation: USSR. Agency: NII-88. Apogee: 100 km (60 mi).

1956 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun.
  • First Cajun research rocket. Nation: USA.

    First Cajun research rocket successfully launched at NACA Wallops Island, Va.

1956 - Launch Vehicle: R-2, R-5.
  • Sounding rocket variants of R-2 and R-5 authorised. Nation: USSR.

    Decree 'MOP On production of the R-5A and R-2A scientific missiles at Plant No. 586' was issued.

1957 -
  • Two NACA groups focused their efforts on the problems involved in manned space flight. Nation: USA. Spacecraft: Dynasoar.

    One group concerned themselves with performance of aircraft at high speeds and altitudes and with rocket research; the other group, with problems associated with hypersonic flight and reentry.

1957 -
  • Robo evaluation committee. Nation: USA. Spacecraft: Dynasoar, Robo.

    A committee, with representation from ARDC headquarters, the Wright Air Development Center, the Cambridge Air Force Research Center, and the Air Materiel Command, was formed to evaluate contractor studies on Robo.

1957 - Launch Site: Cape Canaveral. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Snark. LV Configuration: Snark N-69E N-3321. FAILURE: Failure.
  • Test mission Nation: USA. Agency: USAF. Apogee: 0 km ( mi).

1959 - Launch Vehicle: DF-2, K-13, Kosmos 2, P-15.
  • Decision to withhold R-12 and nuclear warhead drawing package from China over Sidewinder affair Nation: China. Spacecraft: Project 581.

    The Soviet Central Committee advises China it will not provide prototype or drawings of atomic bombs as agreed previously. Khrushchev promised China that he would provide the drawing package for the R-12 IRBM as soon as testing was completed. However then came the affair of the Sidewinder. At the end of 1958 or early 1959 a complete missile fell into the hands of the Chinese. They promised to provide it to the Russians, but then dragged their feet. They were finally told in February 1959 that unless they provided the Sidewinder, they would not be given the R-12 package. The missile was finally delivered but it was found that the key crystal in the infrared homing sensor was missing. The Chinese had also been caught disassembling a P-15 cruise missile at a training facility in China. It had taken the Russian trainers two days to get it reassembled correctly. Therefore on June 20 1959 the decision was taken not to transfer the R-12 or the promised nuclear warhead design to China.

    The Soviets created a new design bureau to copy the Sidewinder. Fabrication of the crystal for the infrared sensor was the main obstacle. The initial production batches had a 99% rejection rate. A state commission was set up to get to the bottom of the problem, but couldn’t find a solution. The main problem seemed to be low-quality ore provided by the mines.

1961 - 23:54 GMT - Launch Site: Vandenberg. Launch Complex: SLC10E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 276.
  • Combat training launch Nation: USA. Agency: RAF. Apogee: 520 km (320 mi).

1962 - 05:20 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5C. LV Configuration: Skylark-5C SL45.
  • Solar X-rays / La / Gren. / FS Aeronomy / solar x-ray mission Nation: Australia. Agency: WRE/RAE. Apogee: 227 km (141 mi).

1962 - 08:46 GMT - Launch Site: Johnston Island. Launch Complex: LE1. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2E. LV Configuration: Thor DSV-2E 193. FAILURE: Failure.
  • STARFISH Nuclear test Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1962 - 13:29 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.26NP.
  • LeRC LH2 test Technology test Nation: USA. Agency: NASA. Apogee: 158 km (98 mi).

1963 -
  • Gemini sled test No. 2 at China Lake. Nation: USA. Program: Gemini. Spacecraft: Gemini.

    Sled test No. 2, the first dynamic dual-ejection test of the Gemini escape system, was run at China Lake. Both seats ejected and all systems functioned properly. The test was scheduled to be rerun, however, because the sled failed to attain high enough velocity. The purpose of sled tests in the ejection seat development program was to simulate various high-altitude abort situations. Sled test No. 3 was successfully run on August 9. Further tests were delayed while the ejection system was being redesigned. A modified egress kit was tested in two dummy drops on December 12, with no problems indicated. Gemini Project Office directed McDonnell to proceed with plans for the next sled test. Developmental sled testing on the escape system, incorporating the redesigned egress kit and a soft survival pack, resumed on January 16, 1964, with test No. 4; all systems functioned normally. Test No. 5, the planned repetition of test No. 2, brought developmental sled testing to an end on February 7.

1963 -
  • Vostok 5/6 cosmonaut debriefing Nation: USSR. Spacecraft: Vostok. Flight: Vostok 6, Vostok 5.

    Korolev, Tyulin, and Rudenko left Tyuratam aboard an An-12, followed by 60 others (cosmonauts, officers, engineers) aboard an An-10. General Goreglyad requests that 'extraneous' staff remain in Kuibyshev, while the rest will proceed on to Moscow with Bykovskiy and Tereshkova. The aircraft arrive at 11:30 in Kuibyshev, then go to the debriefing building on the Volga river. There the debriefing of the two cosmonauts began at 13:00. After the debriefings, in the evening, Korolev took the cosmonauts for a trip on the Volga. Kamanin was infuriated - partying would ruin the post-flight medical tracking.

1963 - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-22.
  • Thread Needle Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

    Research and development launch. Mk 6 re-entry vehicle.

1963 - 03:00 GMT - Launch Site: Kwajalein. Launch Complex: RN. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun Falling Sphere 4.
  • Aeronomy mission Nation: USA. Agency: USN. Apogee: 180 km (110 mi).

1963 - 05:20 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL46.
  • LangP / Te / La / SpE / XR Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 227 km (141 mi).

1963 - 14:25 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.61AS.
  • NRL Coronagraph test Nation: USA. Agency: NASA. Apogee: 195 km (121 mi).

1966 -
  • President De Gaulle of France visited Baikonur Cosmodrome Nation: USSR.

    De Gaulle was shown a Vostok launch vehicle, scientific satellites, a Zenit-2 reconnaissance satellite, and viewed launches of an R-16 ICBM and Vostok space launcher. This was the first view by westerners of these systems. All such visits entailed a major effort by staff to fix up the cosmodrome, prepare illustrated materials, clean and paint all facilities, and so on.

1966 - Launch Vehicle: Titan. Model: Titan 2.
  • Gemini launch vehicle 10 and spacecraft No. 10 were electrically mated at complex 19. Nation: USA. Flight: Gemini 10.

    The Electrical Interface Integrated Validation and Joint Guidance and Control Test was conducted June 20-21. Following a data review, the Joint Combined Systems Test was run June 23.

1966 - 19:39 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C S08/1.
  • ESRO S08 / 1 (SK7) Aeronomy / solar ultraviolet mission Nation: Europe. Agency: ESRO. Apogee: 220 km (130 mi).

1967 - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. FAILURE: Failure.
  • Zenit-4 Nation: USSR. Spacecraft: Zenit-4. Agency: RVSN. COSPAR: F670620A.

    High resolution photo reconnaissance mission.

1967 - 16:19 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B. LV Configuration: Titan IIIB 3B-8.
  • OPS 4282 Nation: USA. Payload: KH-8 no. 06 / Agena D. Mass: 3,000 kg (6,600 lb). Class: Surveillance. Type: Military. Spacecraft: KH-8. Agency: NRO/USAF. Perigee: 127 km (78 mi). Apogee: 325 km (201 mi). Inclination: 111.40 deg. Period: 89.00 min. COSPAR: 1967-064A. USAF Sat Cat: 2858. Decay Date: 1967-06-30.

    KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

1968 - 21:46 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thorad SLV-2G Agena D. LV Configuration: Thorad SLV-2G Agena D 517 / Agena D 1645.
  • KH-4A 1047 Nation: USA. Payload: KH-4A s/n 1047 / Agena D 1645. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 183 km (113 mi). Apogee: 402 km (249 mi). Inclination: 85.00 deg. Period: 90.30 min. COSPAR: 1968-052A. USAF Sat Cat: 3296. Decay Date: 1968-07-16.

    KH-4A. Out-of-focus imagery is present on both main camera records.

  • SRV 745 Nation: USA. Payload: SRV 1047-1. Mass: 60 kg (132 lb). Spacecraft: KH-4A. Agency: NRO/USAF. Perigee: 435 km (270 mi). Apogee: 514 km (319 mi). Inclination: 85.10 deg. Period: 94.10 min. COSPAR: 1968-052B. USAF Sat Cat: 3297. Decay Date: 1970-01-11.

    Radar monitoring.

  • OPS 5259 Nation: USA. Payload: EHH B12. Class: Sigint. Spacecraft: SSF. Agency: USAF. COSPAR: 1968-052xx. USAF Sat Cat: 3297. Decay Date: 1970-01-11.

1969 -
  • Kamanin meets with Chief of Ministry of Defence General Staff Zakharov. Nation: USSR. Program: Lunar L3.

    Zakharov is violently opposed to the Ministry of Defence spending a single kopeck on the exploration of space. It all must be paid for by the Academy of Sciences or be consigned to the waste bin.

1969 - Launch Site: Vandenberg. Launch Complex: LF21. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2320.
  • ST Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena V119D.
  • USAF V119D re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1969 - 03:15 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 166 km (103 mi).

1969 - 05:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.269UG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 181 km (112 mi).

1970 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2338.
  • OT GT27M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 -
  • Soyuz 11 Day 15 Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 11.

    The Soyuz 11 crew completes their 1000th revolution of the earth. Gorbatko jokes that they are 'go for 2000' but the crew is not enthusiastic. Kamanin does not believe they have more than 10 or 11 days endurance left in them. Clear problems exist: the Penguin training suits do not adequately replace gravitational effects (they have suffered torn elastic bands); the measured lung capacity of the crews has declined from 300 on the first day of the flight to 200 now; use of the treadmill caused the whole station to vibrate alarmingly and was discontinued (the solar panels flapped, the propellants sloshed in the tanks, and the noise of the track couldn't be kept out of the rest areas). The weather is very poor in the prime recovery area for the last two days - 20-25 m/s wind - dangerous for landing.

1971 - 19:31 GMT - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B. LV Configuration: Scout B S144CR.
  • PAET re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 377 km (234 mi).

1971 - 22:45 GMT - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-12.
  • Operational Test M1-17 Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

    SSTTP M1-17 Target mission

1972 - 16:45 GMT - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • FOT GT107M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1973 - 06:16 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53724-116.
  • Cosmos 574 Nation: USSR. Mass: 550 kg (1,210 lb). Class: Navigation. Spacecraft: Tsiklon. Agency: MO SSSR. Perigee: 976 km (606 mi). Apogee: 1,010 km (620 mi). Inclination: 83.00 deg. Period: 105.00 min. COSPAR: 1973-042A. USAF Sat Cat: 6707.

    Military navigation satellite.

1974 - 05:11 GMT - Launch Site: Lancelin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sandhawk. Model: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia.
  • Eclipse Solar ultraviolet eclipse mission Nation: USA. Agency: Sandia. Apogee: 320 km (190 mi).

    Eclipse observations - Launched from Lancelin, Perth, W. Australia - Latitude: 31.01 S, Longitude:115.19 E.

1974 - 05:11 GMT - Launch Site: Lancelin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sandhawk. Model: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia.
  • Eclipse Solar ultraviolet eclipse mission Nation: USA. Agency: Sandia. Apogee: 320 km (190 mi).

    Eclipse observations - Launched from Lancelin, Perth, W. Australia - Latitude: 31.01 S, Longitude:115.19 E.

1974 - 08:15 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 160 km (90 mi).

1974 - 20:03 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 160 km (90 mi).

1975 - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 3.
  • OT GT31GM operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1975 - 06:54 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Cosmos 744 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 7. Mass: 2,500 kg (5,500 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MOM. Perigee: 367 km (228 mi). Apogee: 380 km (230 mi). Inclination: 81.20 deg. Period: 92.00 min. COSPAR: 1975-056A. USAF Sat Cat: 7968. Decay Date: 1991-10-12.

1978 - Launch Site: Biscarosse. Launch Complex: BLB. Launch Pad: -. Launch Vehicle: SSBS. Model: SSBS S3. LV Configuration: SSBS S3 V6.
  • Test mission Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1978 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.543UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 184 km (114 mi).

1983 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 34D.
  • First of seven Titan 34D launches Nation: USA.

    First of seven Titan 34D launches from the West Coast.

1983 - 18:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 34D. LV Configuration: Titan 34D 34D-5 (04D-3).
  • KH-9 no. 18 Nation: USA. Mass: 13,300 kg (29,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-9. Agency: NRO/CIA. Perigee: 159 km (98 mi). Apogee: 259 km (160 mi). Inclination: 96.50 deg. Period: 88.80 min. COSPAR: 1983-060A. USAF Sat Cat: 14137. Decay Date: 1984-03-21.

    KH-9 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • OPS 3899 Nation: USA. Payload: SSF-C No. 7. Mass: 60 kg (132 lb). Class: Sigint. Spacecraft: SSF. Agency: NRO/USAF. Perigee: 1,278 km (794 mi). Apogee: 1,296 km (805 mi). Inclination: 96.60 deg. Period: 111.31 min. COSPAR: 1983-060C. USAF Sat Cat: 14139.

    ABM monitoring; may or may not have existed!!!.

1986 - Launch Site: Baikonur. Launch Complex: Jubilee. Launch Pad: -. 1987 - 02:34 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 59E / Star-37S-ISS.
  • USA 26 Nation: USA. Program: DMSP. Payload: DMSP S-9/Star 37S S/N 15019. Mass: 750 kg (1,650 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 5D-2. Agency: USAF. Perigee: 828 km (514 mi). Apogee: 848 km (526 mi). Inclination: 98.80 deg. Period: 101.70 min. COSPAR: 1987-053A. USAF Sat Cat: 18123.

    Defense Meteorological Satellite Program.

1989 - 19:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.54US.
  • NCAR / CU-2 Solar ultraviolet mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).

1990 - 23:36 GMT - Launch Site: Baikonur. Launch Complex: LC200/40. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM. LV Configuration: Proton-K/DM 342-02.
  • Gorizont 20 Nation: USSR. Payload: Gorizont s/n 30L. Mass: 2,125 kg (4,684 lb). Class: Communications. Spacecraft: Gorizont . Agency: MOM. Perigee: 35,771 km (22,227 mi). Apogee: 35,801 km (22,245 mi). Inclination: 1.50 deg. Period: 1,436.10 min. COSPAR: 1990-054A. USAF Sat Cat: 20659. Completed Operations Date: 1999-02-01.

    Stationed at 90 deg E. Provision of telephone and telegraph communications and transmission of television programmes, continuation of work in the context of the 'Intercosmos' programme for the development of new frequency ranges and the creation of long-range systems of space c ommunications jointly with the Byelorussian SSR, GDR, Hungary and Czechoslovakia. Positioned in geosynchronous orbit at 90 deg E in 1990; 14 deg W in 1990-1995; 26 deg E in 1995-1998; 96 deg E in 1998-1999 As of 4 September 2001 located at 77.53 deg E drifting at 0.186 deg W per day. As of 2007 Mar 8 located at 83.10E drifting at 0.160E degrees per day.

1994 - 14:42 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: DC-X. Model: DC-X.
  • Nation: USA. Agency: MDAC. Apogee: 1.00 km (0.60 mi).

    First flight of second series after additional SDIO funding received. Full propellent load; radar altimeter in control loop. Reached altitude of 870 m during a 136 second flight.

1996 - 14:40 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.118NP.
  • DARTFire 1 Microgravity mission Nation: USA. Agency: NASA GSFC. Apogee: 300 km (180 mi).

1996 - 14:49 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39B. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-78.
  • STS-78 Nation: USA. Program: STS. Payload: Columbia F20 / EDO. Class: Manned. Type: Spaceplane. Spacecraft: Columbia. Agency: NASA JSC. Perigee: 246 km (152 mi). Apogee: 261 km (162 mi). Inclination: 39.00 deg. Period: 89.60 min. COSPAR: 1996-036A. USAF Sat Cat: 23931. Duration: 16.91 days. Decay Date: 1996-07-07. Crew: Brady, Favier, Helms, Henricks, Kregel, Linnehan, Thirsk. Flight: STS-78.

    Columbia carried Terence T Henricks, Kevin R Kregel, Susan J Helms, Richard M Linnehan, Charles E Brady, Jr, Jean-Jacques Favier, and Robert Brent Thirsk to orbit. Main payload was the Life and Microgravity Spacelab for conducting human biological and microgravity experiments. Columbia landed safely at Kennedy Space Center on July 7.

  • Spacelab LMS 1 Nation: USA. Program: Spacelab. Payload: Spacelab Long Module. Class: Manned. Type: Spacelab. Spacecraft: Spacelab. Agency: NASA JSC. Perigee: 246 km (152 mi). Apogee: 261 km (162 mi). Inclination: 39.00 deg. Period: 89.60 min. COSPAR: 1996-036xx. USAF Sat Cat: 23931. Decay Date: 1996-07-07.

  • EDO Nation: USA. Program: STS. Agency: NASA. COSPAR: 1996-036xx. USAF Sat Cat: 23931. Decay Date: 1996-07-07.

1996 - 18:45 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. FAILURE: Shroud broke up at T+50seconds.
  • Yantar-4K1 Nation: Russia. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-4K1. Agency: VKS. COSPAR: F960620A.

    High resolution photo reconnaissance mission.

1999 - 02:15 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2G. LV Configuration: Titan II SLV 23G-7 / M68B-75 / 63-7730.
  • QuikScat Nation: USA. Class: Earth. Type: Oceansat. Spacecraft: QuikScat. Manufacturer: Ball Aerospace, Boulder. Agency: NASA GSF. Perigee: 804 km (499 mi). Apogee: 806 km (500 mi). Inclination: 98.60 deg. COSPAR: 1999-034A. USAF Sat Cat: 25789.

    NASA's QuikScat carried the SeaWinds scatterometer for remote sensing of ocean winds. The Titan 2’s second stage shut down at 02:20 GMT and then coasted to apogee still attached to the QuikScat. The Titan second stage vernier thrusters ignited at apogee to raise perigee, leaving QuikScat in a 280 km x 813 km x 98.7 degree parking orbit. The QuikScat's own hydrazine propulsion system then fired to raise the perigee over a period of weeks.

2002 - 09:33 GMT - Launch Site: Plesetsk. Launch Complex: LC133/3. Launch Pad: -. Launch Vehicle: UR-100N. Model: Rokot. LV Configuration: Rokot 492882034.
  • Iridium SV97 Nation: USA. Program: Iridium. Mass: 690 kg (1,520 lb). Class: Communications. Spacecraft: LM 700. Manufacturer: LM-S/Motorola. Agency: Iridium. Perigee: 659 km (409 mi). Apogee: 669 km (415 mi). Inclination: 86.60 deg. Period: 98.00 min. COSPAR: 2002-031A. USAF Sat Cat: 27450.

    Launch delayed from June 6, 19. The two Iridium replacement mobile telephone satellites were owned by Iridium Satellite LLC, the successor to bankrupt Iridium LLC.

  • Iridium SV98 Nation: USA. Program: Iridium. Mass: 690 kg (1,520 lb). Class: Communications. Spacecraft: LM 700. Manufacturer: LM-S/Motorola. Agency: Iridium. Perigee: 658 km (408 mi). Apogee: 666 km (413 mi). Inclination: 86.60 deg. Period: 98.00 min. COSPAR: 2002-031B. USAF Sat Cat: 27451.


Born on this day in:
  • 1945 - James Frederick (Jim) Buchli.  American Mission Specialist Astronaut. Birth City: New Rockford. Birth State: North Dakota. Birth Country: USA.
  • 1948 - Gary Eugene Payton.  American Manned Spaceflight Engineer Astronaut. Birth City: Rock Island. Birth State: Illinois. Birth Country: USA.
  • 1953 - Brian J Duffy.  American Pilot Astronaut. Birth City: Boston. Birth State: Massachusetts. Birth Country: USA.
  • 1954 - Ilan Ramon.  Jewish Israeli Pilot Astronaut. Birth City: Tel Aviv. Birth Country: Israel.
  • 1955 - David Paul Staib Jr.  American Manned Spaceflight Engineer Astronaut. Birth City: Fort Campbell. Birth State: Kentucky. Birth Country: USA.

Died on this day in:
  • 2005 - Bernard A Schriever.  American Manager.

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