Encyclopedia Astronautica
June 10


June 10 Chronology


1909 June 10 - .
  • Birth of Ludwig Roth - . Nation: Germany; USA. Summary: German engineer in WW2, member of the Rocket Team in the United States thereafter..

1929 June 10 - .
1944 June 10 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-158.
  • V-2 4158 - . Nation: Germany. Summary: Burnout at T+68seconds. Flight duration 264 seconds..

1953 June 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. Launch Pad: LC3/4?. LV Family: Bomarc. Launch Vehicle: Bomarc. LV Configuration: Bomarc 623-1. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 20 km (12 mi).

1954 June 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-12489.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1955 June 10 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 2246T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1957 June 10 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar SP-2. LV Family: R-2. Launch Vehicle: R-2A.
  • NIIP-A target - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1958 June 10 - .
  • X-1E Flight 20 - . Crew: Walker, Joseph. Payload: X-1E flight 20. Nation: USA. Related Persons: Walker, Joseph. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1E. Summary: NACA flight 19. Flight aborted after only 1 cylinder of engine fired. Plane damaged on landing..

1959 June 10 - . 16:40 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 AA3.280C.
  • Ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 225 km (139 mi).

1960 June 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-54-125.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1961 June 10 - . Launch Vehicle: Saturn C-2.
  • Lundin Committee recommended earth orbit rendezvous mode - . Nation: USA. Related Persons: Seamans. Program: Apollo. Spacecraft: Apollo Lunar Landing. 'The Lundin Committee completed its study of various vehicle systems for the manned lunar landing mission, as requested on May 25 by NASA associate Administrator Robert C. Seamans, Jr. The Committee had considered alternative methods of rendezvous: earth orbit, lunar orbit, a combination of earth and lunar orbit, and lunar surface. Launch vehicles studied were the Saturn C-2 and C-3. Conclusion was that 43,000 kg stage (85% fuel) was needed for a lunar landing mission. The concept of a low- altitude earth orbit rendezvous using two or three C-3's was clearly preferred by the Committee. Reasons for this preference were the small number of launches and orbital operations required and the fact that the Saturn C- 3 was considered to be an efficient launch vehicle of great utility and future growth.

1961 June 10 - . LV Family: Nova. Launch Vehicle: Nova A.
  • Preparation for NOVA rocket motor tests. - . Nation: USA. Summary: National Bureau of Standards broke ground for new research facility at Gaithersburg, Md., which will include a mega-pound deadweight testing machine to provide measurement standards for multimillion rocket thrust requirements..

1961 June 10 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique AGI31.
  • Aeronomy mission - . Nation: France. Agency: CRS. Apogee: 100 km (60 mi).

1963 June 10 - .
  • Vostok 5 scrubbed due to solar flares. - . Nation: USSR. Related Persons: Keldysh; Korolev. Flight: Vostok 5; Vostok 6. Spacecraft: Vostok. The launch of Vostok 5 is set for 11 June. Final training and consultations are under way. Korolev is not happy with the condition of the spacecraft. At 22:30 in the evening the launch is scrubbed when Keldysh calls from Moscow and advises excessive solar flare activity is expected. Keldysh will review the data tomorrow and advise if it really poses a danger to the cosmonauts.

1964 June 10 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • Contract with Martin for 15 Gemini launch vehicles (GLV) converted. - . Nation: USA. Air Force Space Systems Division's cost-plus-fixed-fee contract with Martin for 15 Gemini launch vehicles (GLV) and associated aerospace ground equipment was replaced by a cost-plus-incentive-fee contract. Contract negotiations had been conducted between March 15 and April 30, 1964. The final contract contained cost, performance, and schedule incentives. Target cost was $111 million and target fee was $8.88 million. The maximum fee possible under the contract was $16.65 million as against a minimum of $3.33 million. The period of performance under the contract was July 1, 1963, through December 31, 1967, and covered the delivery of 14 GLVs (one GLV had already been delivered) and associated equipment and services, including checkout and launch.

1964 June 10 - . 05:30 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. LV Family: Diamant. Launch Vehicle: Rubis. LV Configuration: Rubis R1.
  • A-1 capsule test - . Nation: France. Agency: ONERA. Apogee: 1,800 km (1,100 mi).

1964 June 10 - . 10:48 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92. LV Configuration: Vostok 8A92 R15001-02.
  • Cosmos 32 - . Payload: Zenit-2 11F61 s/n 18. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: Korolev. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Duration: 8.00 days. Decay Date: 1964-06-18 . USAF Sat Cat: 807 . COSPAR: 1964-029A. Apogee: 322 km (200 mi). Perigee: 205 km (127 mi). Inclination: 51.3000 deg. Period: 89.80 min. Summary: Area survey photo reconnaissance satellite..

1964 June 10 - . 12:44 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.67NP.
  • Paraglider Technology / meteoroid mission - . Nation: USA. Agency: NASA. Apogee: 155 km (96 mi).

1964 June 10 - . 15:10 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.155GE.
  • B Field 1 Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 146 km (90 mi).

1965 June 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 669. FAILURE: Failure.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 10 km (6 mi).

1965 June 10 - . 12:26 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 302D.
  • NTMP RMV-303 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 June 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1261.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1966 June 10 - . Launch Site: Baikonur. Launch Complex: Baikonur PU32. LV Family: Tsiklon. Launch Vehicle: R-36 8K67.
  • SLI K Operational test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1966 June 10 - . Launch Site: Green River. Launch Complex: Green River Pad 2. LV Family: Athena RTV. Launch Vehicle: Athena RTV. LV Configuration: Athena D023.
  • USAF D023 re-entry vehicle test flight - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1966 June 10 - . 04:15 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA3A. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S147C.
  • OV3-04 - . Mass: 79 kg (174 lb). Nation: USA. Agency: USAF OAR. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV3. USAF Sat Cat: 2201 . COSPAR: 1966-052A. Apogee: 4,704 km (2,922 mi). Perigee: 643 km (399 mi). Inclination: 40.9000 deg. Period: 142.90 min. Summary: Radiation measurements. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1966 June 10 - . 11:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 96D.
  • NTMP KX-42 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 June 10 - . 16:09 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 645. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-421.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 June 10 - . 00:25 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.222GE.
  • SPICE (p / n) Plasma mission - . Nation: USA. Agency: NASA. Apogee: 149 km (92 mi).

1968 June 10 - . 15:49 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 5A. LV Configuration: Black Brant VA CRL AH17.751D. FAILURE: Failure.
  • D region protons Ionosphere mission - . Nation: USA. Agency: AFCRL. Apogee: 112 km (69 mi).

1968 June 10 - . 16:05 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.223GE.
  • SPICE Plasma mission - . Nation: USA. Agency: NASA. Apogee: 150 km (90 mi).

1968 June 10 - . 17:15 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.335UA.
  • Meteoroids Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 152 km (94 mi).

1969 June 10 - . LV Family: N1. Launch Vehicle: N1.
  • Revised Soviet lunar plans - . Nation: USSR. Program: Lunar L3; Lunar L1; Luna. Spacecraft: Luna Ye-8-5; Luna Ye-8; Soyuz 7K-L1; Soyuz 7K-LOK; LK. The VPK Military-Industrial Commission issues a decree on the schedule for the rest of 1969. There are to be five launches of Ye-8-5 lunar soil return robots, on 14 June, 13 and 28 July, 25 August, and 25 September. There are to be two launches of Ye-8 Lunokhod robot rovers on 22 October and 21 November. Further manned L1 flights are cancelled. There are no plans made for the L3 since the N1 is not ready.

1969 June 10 - . Launch Site: Vandenberg. LV Family: Titan. Launch Vehicle: Titan 3C.
  • MOL Program cancelled - . Nation: USA. Class: Manned. Type: Manned space station. Spacecraft: MOL. Department of Defense announced cancellation of the planned Manned Orbiting Laboratory (MOL) program from Space Launch Complex 6 at Vandenberg AFB. The cancellation was expected to save $ 1.5 billion of the projected total $ 3.0 billion program costs. The SLC-6 launch facility at Vandenberg, 90% complete, would be finished and mothballed. MOL reconnaisance systems useful on unmanned satellites would be completed for a total cost of $ 225 million. Ten thousand aerospace workers were laid off as a result of the cancellation.

1970 June 10 - .
  • Soyuz 9 Day 10 - . Nation: USSR. Related Persons: Nikolayev; Sevastyanov; Gorbatko. Program: Soyuz. Flight: Soyuz 9. Summary: This is the first day 'off' for the Soyuz 9 crew on their long duration flight. No experiments are scheduled and radio communications will be minimised. The crew plays chess via radio with Gorbatko..

1970 June 10 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 346 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 7.00 days. Decay Date: 1970-06-17 . USAF Sat Cat: 4409 . COSPAR: 1970-042A. Apogee: 351 km (218 mi). Perigee: 206 km (128 mi). Inclination: 51.8000 deg. Period: 90.00 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1971 June 10 - .
  • Soyuz 11 Day 5 - . Nation: USSR. Related Persons: Dobrovolsky; Patsayev; Volkov. Program: Salyut. Flight: Soyuz 11. All normal aboard Salyut 1. It is established that Soyuz 11 has enough propellant remaining for 57 hours of autonomous flight, including orientation and retrofire. It is decided to ask the crew to conduct a couple of experiments with the 'globus' instrument on the station to determine the accuracy of its landing point prediction.

1971 June 10 - .
  • Death of Aleksei Mikhailovich Isayev - . Nation: Russia. Related Persons: Isayev. Summary: Soviet Chief Designer at OKB-2, 1947-1971. Developed storable rocket engines for missiles, supplying innovative engines for Scuds, SLBM's. Leading designer of restartable space engines for satellites, manned spacecraft, and space stations..

1971 June 10 - . 23:10 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.11UA.
  • JHU Airglow 11 / S169 Aeronomy / test - . Nation: USA. Agency: NASA. Apogee: 328 km (203 mi).

1972 June 10 - . 04:30 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.415UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 164 km (101 mi).

1973 June 10 - . 10:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 572 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4M. Duration: 13.00 days. Decay Date: 1973-06-23 . USAF Sat Cat: 6684 . COSPAR: 1973-038A. Apogee: 281 km (174 mi). Perigee: 206 km (128 mi). Inclination: 51.7000 deg. Period: 89.30 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1973 June 10 - . 14:13 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta 1913. LV Configuration: Delta 1913 581/D95.
  • Explorer 49 - . Payload: RAE B. Mass: 328 kg (723 lb). Nation: USA. Agency: NASA Greenbelt. Program: Explorer. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: RAE. USAF Sat Cat: 6686 . COSPAR: 1973-039A. Summary: Radio Astronomy Explorer; measured galactic, stellar radio noise. Lunar Orbit (Selenocentric). Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..

1973 June 10 - . 17:20 GMT - . Launch Site: Syowa Base. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210JA-13.
  • Auroral mission - . Nation: Japan. Agency: NIPR. Apogee: 123 km (76 mi).

1974 June 10 - . 16:19 GMT - . Launch Site: Thule AFB. Launch Vehicle: Rocketsonde.
  • Starute, AN/DMQ-9- - . Nation: USA. Agency: MRN. Apogee: 60 km (37 mi).

1975 June 10 - . 10:15 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL A03.103-1.
  • Density / Laser Backscatter Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 158 km (98 mi).

1975 June 10 - . 13:18 GMT - . Launch Site: Andoya. LV Family: Cajun. Launch Vehicle: Nike Cajun.
  • Ferdinand 42 Auroral mission - . Nation: Norway. Agency: NTNF. Apogee: 100 km (60 mi).

1976 June 10 - . 00:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 2914. LV Configuration: Delta 2914 601/D124.
  • Marisat 2 - . Payload: Marisat 102. Mass: 362 kg (798 lb). Nation: USA. Agency: Comsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Marisat. Completed Operations Date: 1996-09-25 . USAF Sat Cat: 8882 . COSPAR: 1976-053A. Apogee: 37,604 km (23,365 mi). Perigee: 36,513 km (22,688 mi). Inclination: 14.9000 deg. Period: 1,501.60 min. Maritime communications. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Pacific Ocean at 176 deg E in 1976-1991 over the Pacific Ocean 178 deg W in 1991-1996 As of 5 September 2001 located at 158.48 deg W drifting at 15.761 deg W per day. As of 2007 Mar 10 located at 162.62W drifting at 15.745W degrees per day.

1976 June 10 - . 17:40 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 7 AC. LV Configuration: Skylark 7 AC SL1212.
  • XRCS X-ray astronomy mission - . Nation: UK. Agency: BAC. Apogee: 280 km (170 mi).

1977 June 10 - . 03:06 GMT - . Launch Site: El Arenosillo. LV Family: Black Brant. Launch Vehicle: Black Brant 5C. LV Configuration: Black Brant VC DLR H-BBV-84.
  • Heatpipe 2 Technology mission - . Nation: Germany. Agency: DFVLR. Apogee: 322 km (200 mi).

1977 June 10 - . 08:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 916 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MT. Duration: 11.00 days. Decay Date: 1977-06-21 . USAF Sat Cat: 10040 . COSPAR: 1977-046A. Apogee: 304 km (188 mi). Perigee: 255 km (158 mi). Inclination: 62.7000 deg. Period: 90.10 min. Summary: Military topography satellite; returned film capsule; also performed mapping, geodesy, earth resources; deployed capsule..

1978 June 10 - . 08:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1021 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MKM. Duration: 13.00 days. Decay Date: 1978-06-23 . USAF Sat Cat: 10939 . COSPAR: 1978-057A. Apogee: 313 km (194 mi). Perigee: 173 km (107 mi). Inclination: 65.0000 deg. Period: 89.40 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1978 June 10 - . 19:12 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 3C. LV Configuration: Titan IIIC 23C-15 (3C-33).
  • Chalet 1 - . Payload: Chalet 1 (Vortex 1) / OPS 9454. Mass: 820 kg (1,800 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Chalet. USAF Sat Cat: 10941 . COSPAR: 1978-058A. Apogee: 42,039 km (26,121 mi). Perigee: 29,929 km (18,596 mi). Inclination: 12.0000 deg. Period: 1,446.30 min. Summary: First launch of the heavier, mored advanced CHALET ELINT satellites. (the project was renamed VORTEX when the code name CHALET appeared in the New York Times)..

1979 June 10 - . 13:39 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 3C. LV Configuration: Titan IIIC 23C-13 (3C-31).
  • IMEWS 10 - . Payload: DSP MOS/PIM s/n 11 / OPS 7484. Mass: 1,170 kg (2,570 lb). Nation: USA. Agency: USAF. Class: Military. Type: Early warning satellite. Spacecraft: DSP. Completed Operations Date: 1984-06-01 . USAF Sat Cat: 11397 . COSPAR: 1979-053A. Apogee: 35,854 km (22,278 mi). Perigee: 35,712 km (22,190 mi). Inclination: 1.8000 deg. Period: 1,435.90 min. First Multi-Orbit Satellite / Performance Improvement ballistic missile launch detection satellite, remained in service for nearly six years. Positioned in geosynchronous orbit over the Pacific Ocean at 135 deg W in 1979-1982; 85 deg W in 1982-1984; 135 deg W in 1984; 125 deg W in 1985..

1980 June 10 - . 11:45 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.46AS.
  • Solar mission - . Nation: USA. Agency: NASA. Apogee: 298 km (185 mi).

1981 June 10 - . 01:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1982 June 10 - . 17:37 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/1. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1378 - . Payload: Tselina-D no. 36. Mass: 2,200 kg (4,800 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. USAF Sat Cat: 13271 . COSPAR: 1982-059A. Apogee: 618 km (384 mi). Perigee: 593 km (368 mi). Inclination: 82.5000 deg. Period: 96.80 min.

1983 June 10 - . 14:20 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1984 June 10 - . Launch Site: Kwajalein. Launch Vehicle: HOE. LV Configuration: HOE HOE 4.
  • HOE 4 ABM test - . Nation: USA. Agency: USAF AFSC. Apogee: 200 km (120 mi).

1984 June 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-13 (HOE) Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1985 June 10 - . 08:26 GMT - . Launch Site: ETR Launch Area. Launch Platform: UK S22. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3TK.
  • Chevaline demonstration and shakedown operations launch - . Nation: UK. Agency: RN. Apogee: 1,000 km (600 mi).

1986 June 10 - . 00:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 322-02.
  • Gorizont 12 - . Payload: Gorizont s/n 24L. Mass: 2,100 kg (4,600 lb). Nation: USSR. Agency: MOM. Class: Communications. Type: Civilian communications satellite. Spacecraft: Gorizont . Completed Operations Date: 1991-01-23 . USAF Sat Cat: 16769 . COSPAR: 1986-044A. Apogee: 35,794 km (22,241 mi). Perigee: 35,763 km (22,222 mi). Inclination: 10.1000 deg. Period: 1,435.70 min. Stationed at 345 deg E. Provision of telephone and telegraph radiocommunications and television broadcasting. Positioned in geosynchronous orbit at 14 deg W in 1986-1989; 40 deg E in 1989-1990 As of 28 August 2001 located at 84.75 deg E drifting at 0.265 deg W per day. As of 2007 Mar 10 located at 45.79E drifting at 0.142E degrees per day.

1987 June 10 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: SSBS. Launch Vehicle: SSBS S3. LV Configuration: SSBS S3 2608.
  • Operational test - . Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1988 June 10 - . 07:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: USHAKOV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 59 km (36 mi).

1989 June 10 - . 22:19 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 6925. LV Configuration: Delta 6925 D185.
  • USA 38 - . Payload: GPS 2-2 / GPS SVN 13. Mass: 1,665 kg (3,670 lb). Nation: USA. Agency: USAF. Manufacturer: Seal Beach. Program: Navstar. Class: Navigation. Type: Navigation satellite. Spacecraft: GPS Block 2 and 2A. USAF Sat Cat: 20061 . COSPAR: 1989-044A. Apogee: 20,514 km (12,746 mi). Perigee: 19,849 km (12,333 mi). Inclination: 54.8000 deg. Period: 718.00 min. Summary: Global Positioning System. Placed in Plane B Slot 3..

1992 June 10 - .
  • Spacewedge 2 first flight - . Nation: USA. Spacecraft: X-38. A second vehicle to test autonomous parasail spacecraft recovery was fabricated with the same external geometry and weight as Wedge 1. It was dropped from a Cessna U-206 and a Rans S-12 ultralight. A total of 36 flight tests were made, the last taking place on February 12, 1993. These flights verified the manual control and autonomous landing systems of the vehicle. Phase II of the program ran from March 1993 to March 1995, and encompassed 45 flights.

1992 June 10 - . 00:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas IIA. LV Configuration: Atlas IIA AC-105 / Centaur II 8105.
  • Intelsat K - . Mass: 2,928 kg (6,455 lb). Nation: International. Agency: Intelsat. Manufacturer: Lockheed. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 5000. USAF Sat Cat: 21989 . COSPAR: 1992-032A. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Stationed at 21.5 deg W. Intelsat K is a single spacecraft purchased to meet critical requirements for Ku-band capacity over the Atlantic region, driven primarily by international broadcasters. The satellite was purchased from GE Americom while under construction (as Satcom K4) and required extensive payload modifications. Spacecraft: Based on GE 5000 series bus.3-axis stabilised using magnetotorquers. Hydrazine propulsion system. Two large solar panels with 1-axis articulation provide 4800 W BOL.4 50 Ahr NiH batteries. Payload: 16 Ku-band transponders which can be configured into 32 high quality television channels. Permits access from ground antennas 1.2 meters dia. and smaller. Launch vehicle put payload into geosynchronous transfer orbit with GCS trajectory option. Positioned in geosynchronous orbit at 21 deg W in 1992-1999 As of 6 September 2001 located at 21.54 deg W drifting at 0.011 deg W per day. As of 2007 Mar 10 located at 160.51W drifting at 11.137W degrees per day.

1995 June 10 - .
  • Spektr module docks with Mir - . Nation: Russia. Flight: Mir EO-18. Spacecraft: Kristall. After that it was moved several times by the small manipulator arm on Mir to accommodate the addition of the Spektr module to the station and to allow rendezvous with the US Shuttle at Kristall's main docking port. The module was transferred to its final location at the Mir transfer compartment's starboard radial port on July 17, 1995.

1995 June 10 - . 00:24 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 42P. LV Configuration: Ariane 42P-3 V74.
  • DBS 3 - . Mass: 2,934 kg (6,468 lb). Nation: USA. Agency: DirecTV. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 601. USAF Sat Cat: 23598 . COSPAR: 1995-029A. Apogee: 35,789 km (22,238 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Commercial TV. Stationed at 101.0 deg W. Positioned in geosynchronous orbit at 101 deg W in 1995-1999 As of 5 September 2001 located at 100.90 deg W drifting at 0.012 deg W per day. As of 2007 Mar 10 located at 82.00W drifting at 0.004W degrees per day..

1996 June 10 - . Launch Site: Wallops Island. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A NASA 12.48WT. FAILURE: Failure.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).

1997 June 10 - . 12:01 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. LV Family: CZ. Launch Vehicle: CZ-3. LV Configuration: Chang Zheng 3 CZ3-12 (45).
  • FY-2A - . Payload: Fengyun 2A. Nation: China. Agency: CASC. Manufacturer: SARTI. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. USAF Sat Cat: 24834 . COSPAR: 1997-029A. Apogee: 35,784 km (22,235 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.8000 deg. Period: 1,436.10 min. Geosynchronous weather satellite; also known as FY-2B. Operated in geosynchronous orbit at 105 deg E in 1997-2000; 85 deg E in 2000.. The FY-2A stopped transmission in April 1998 but was put back into partial operation in December 1998. Its imager then failed completely on 30 September 1998 and it was retired in April 2000. As of 4 September 2001 located at 83.55 deg E drifting at 0.074 deg W per day. As of 2007 Mar 11 located at 58.96E drifting at 0.025W degrees per day.

1998 June 10 - . 00:35 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 7925-9.5. LV Configuration: Delta 7925-9.5 D258.
  • Thor 3 - . Nation: Norway. Agency: Telenor. Manufacturer: El Segundo. Program: Thor Comsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. USAF Sat Cat: 25358 . COSPAR: 1998-035A. Apogee: 35,798 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. The spacecraft was delivered to its final orbit in a complex series of five engine burns by three rocket stages. The Delta's second stage demonstrated its restart capability in 4 burns: Burn 1 placed the rocket and payload into a low circular orbit; Burn 2 raised the apogee to 1400 km; Burn 3 circularised the orbit at 1400 km. The second stage then separated, and Burn 4 lowered the spent stage's perigee to a low altitude to ensure the stage would decay quickly and not add to the space junk already on orbit. Stage 3 burned once to place the payload and its kick motor into a high 1400 km perigee geosynchronous transfer orbit. The Stage 4 Star 30 apogee kick motor circularised the spacecraft's orbit at geostationary altitude. Geostationary at 0.8 degrees W. Positioned in geosynchronous orbit at 1 deg W in 1998-1999 As of 4 September 2001 located at 0.83 deg W drifting at 0.000 deg E per day. As of 2007 Mar 9 located at 0.85W drifting at 0.002W degrees per day.

1999 June 10 - . 11:07 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC94. Launch Pad: FIX. Launch Vehicle: Hera. LV Configuration: Hera 15.
  • BRV/THAAD Target 6 Target mission - . Nation: USA. Agency: USA. Apogee: 314 km (195 mi).

1999 June 10 - . 11:14 GMT - . Launch Site: White Sands. Launch Vehicle: THAAD. LV Configuration: THAAD FT-10.
  • ABM test - . Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

1999 June 10 - . 13:48 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. Launch Pad: SLC17B. LV Family: Delta. Launch Vehicle: Delta 7420-XC. LV Configuration: Delta 7420-10C D270.
  • Globalstar 52 - . Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25770 . COSPAR: 1999-031A. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.
  • Globalstar 49 - . Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25771 . COSPAR: 1999-031B. Apogee: 2,101 km (1,305 mi). Perigee: 2,099 km (1,304 mi). Inclination: 52.0000 deg. Period: 129.50 min.
  • Globalstar 47 - . Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25773 . COSPAR: 1999-031D. Apogee: 1,415 km (879 mi). Perigee: 1,412 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.
  • Globalstar 25 - . Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25772 . COSPAR: 1999-031C. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.

2002 June 10 - . 01:14 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M 407-01.
  • Ekspress A1R - . Payload: Ekspress A No. 4. Mass: 2,600 kg (5,700 lb). Nation: Russia. Agency: Svyaz. Manufacturer: Reshetnev. Class: Communications. Type: Civilian communications satellite. Spacecraft: Ekspress. USAF Sat Cat: 27441 . COSPAR: 2002-029A. Apogee: 35,792 km (22,240 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.2000 deg. Period: 1,436.00 min. Launch delayed from May 2002. The Ekspress A1R Russian domestic communications satellite was built by NPO PM and Alcatel for Kosmicheskiya Svyaz, the Russian satcom operator. The Proton's parking orbit was off-nominal but the 11S861-01 Blok DM-2M upper stage corrected for this and delivered the payload to the correct orbit. Parking orbit was about 180 x 185 km x 51.6 deg; transfer orbit after the first DM-2M burn was 328 x 36133 km x 47.4 deg; orbit at spacecraft separation was 36102 x 36171 km x 0.2 deg. Two SOZ ullage motors were left in the transfer orbit. As of 2007 Mar 10 located at 14.07W drifting at 0.008W degrees per day.

2003 June 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. Launch Pad: SLC17A. LV Family: Delta. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925-9.5 D298 / Star 48.
  • Spirit (Mars Exploration Rover A, MER-2) - . Payload: MER-A. Mass: 1,063 kg (2,343 lb). Nation: USA. Agency: NASA. Manufacturer: JPL. Class: Mars. Type: Mars probe. Spacecraft: MER. Decay Date: 2004-01-03 . USAF Sat Cat: 27827 . COSPAR: 2003-027A. Summary: Mars rover, placed in a 1.014 AU x 1.531 AU x 0.2 deg solar orbit. Anticipated landing on Mars on Launch delayed from May 30, June 6, 8 and 9. Payload included 530 kg Mars lander total mass, 170 kg Mars Rover mass...

2003 June 10 - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL.
  • Thuraya 2 - . Mass: 5,177 kg (11,413 lb). Nation: UAE. Agency: Thuraya. Manufacturer: El Segundo. Program: Thuraya. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 27825 . COSPAR: 2003-026A. Apogee: 35,806 km (22,248 mi). Perigee: 35,766 km (22,223 mi). Inclination: 5.0000 deg. Period: 1,436.10 min. Summary: The Boeing 'GEM' spacecraft was a modified BSS-702 with a 12 m wide antenna for L-band mobile communications. Launch delayed from January 20, then April 4. As of 2007 Mar 9 located at 43.94E drifting at 0.004E degrees per day..

2003 June 10 - . 06:31 GMT - . Launch Site: Wallops Island. LV Family: Terrier. Launch Vehicle: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.035UP.
  • DEBI (Bowshock) Technology mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 600 km (370 mi).

2004 June 10 - . 01:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2. LV Configuration: Zenit-2 1-95.
  • Cosmos 2406 - . Mass: 3,200 kg (7,000 lb). Nation: Russia. Agency: VKA. Manufacturer: Yuzhnoye. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-2. USAF Sat Cat: 28352 . COSPAR: 2004-021A. Apogee: 866 km (538 mi). Perigee: 846 km (525 mi). Inclination: 71.0000 deg. Period: 102.10 min. Summary: Delayed from February 17 and 18; March 17 and 31; April 6, 25 and 26..

2005 June 10 - .
  • International Space Station Status Report #05-29 - . Nation: USA. Related Persons: Krikalyov; Phillips. Program: ISS. Flight: ISS EO-11. Aboard the International Space Station this week, the eleventh Expedition crew spent the latter part of its second month in space preparing for the arrival of new cargo as its commander quietly slipped into second place on the all-time human space endurance list. Additional Details: International Space Station Status Report #05-29.

2007 June 10 - . 23:40 GMT - . Launch Site: Palmachim. LV Family: Shavit. Launch Vehicle: Shavit 1. LV Configuration: Shaviyt 1 7.
  • Ofeq-7 - . Mass: 300 kg (660 lb). Nation: Israel. Agency: Tsahal. Manufacturer: IAI. Program: Offeq. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Ofeq 5. USAF Sat Cat: 31601 . COSPAR: 2007-025A. Apogee: 576 km (357 mi). Perigee: 340 km (210 mi). Inclination: 141.8000 deg. Period: 93.80 min. Summary: Israeli optical reconnaisance satellite, evidently using an improved version of the Shavit booster and probably heavier and more capable than its predecessors..

2008 June 10 - .
  • STS-124 MCC Status Report #20 - . Nation: USA. Program: ISS. Flight: STS-124. Summary: The crew of Discovery has begun its last day of joint operations with the International Space Station.. Additional Details: STS-124 MCC Status Report #20.

2009 June 10 - .
  • EVA ISS EO-20-2 - . Crew: Padalka; Barratt. EVA Type: Extravehicular activity. EVA Duration: 0.0083 days. Nation: USA. Program: ISS. Flight: ISS EO-20; ISS EO-19. Internal spacewalk in a depressurized Zvezda module to reconfigure it. The spacesuited crew entered the forward transfer comparment of Zvezda and closed the hatches to Zarya and to the aft compartments of Zvezda. The transfer compartment was then depressurized at 06:22 GMT. Then a flat cover on the zenith hatch was removed and stowed on top of the Pirs hatch, leaving the port open to space. The no-longer-required docking cone on the port leading to Zarya was removed installed on the zenith port, preparing it for arrival of the new MIM-2 research/docking module later in the year. The transfer compartment was repressurized at 07:11 GMT.

2010 June 10 - . 18:01 GMT - . Launch Site: Goheung. LV Family: KSLV. Launch Vehicle: KSLV-I. LV Configuration: Naro-1. FAILURE: First stage failure..
  • STSAT-2B - . Mass: 99 kg (218 lb). Nation: Korea South. Agency: KARI. Class: Technology. Type: Technology satellite. Spacecraft: STSAT. Summary: Science and Technology Satellite with Lyman-alpha imaging solar telescope and laser altimeter..

2011 June 10 - . 11:16 GMT - . Launch Site: Wallops Island. LV Family: Terrier. Launch Vehicle: Terrier Orion.
  • NASA 41.096GT - . Nation: USA. Summary: Technology mission. Carried high data rate X-band telemetry system and an 0.4-meter SMART microsatellite bus..

2011 June 10 - . 14:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Delta 7320-10.
  • SAC-D/Aquarius - . Nation: Argentina. Program: SAC. Class: Earth. Type: Weather satellite. Spacecraft: SAC-D. COSPAR: 2011-024A. Apogee: 655 km (406 mi). Perigee: 653 km (405 mi). Inclination: 98.0000 deg. Period: 97.80 min. Argentinian 'Satelite de Aplicaciones Cientificas-D' satellite. Carried NASA Aquarius L-band radiometer/scatterometer map sea salinity; a Ka-band microwave radiometer; a an infrared scanner to measure sea surface temperature; a high sensitivity camera to study light sources at night; and an Italian experiment which measured atmospheric deflection of GPS signals to determine air temperature and humidity.

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