Encyclopedia Astronautica
June 07


June 07 Chronology


1905 June 7 - .
1938 June 7 - .
  • Korolev arrested by Soviet secret police. - . Nation: USSR. Related Persons: Korolev.

1944 June 7 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P10. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 17557.
1949 June 7 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Corporal. Launch Vehicle: Corporal E. LV Configuration: Corporal E 4E. FAILURE: Failure.
  • 4E test - . Nation: USA. Agency: USA OR. Apogee: 0 km ( mi).

1951 June 7 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Vehicle: Lark. LV Configuration: Lark 238. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 0 km ( mi).

1954 June 7 - . Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: Honest John. LV Configuration: Honest John 206M.
  • Test mission - . Nation: USA. Apogee: 10 km (6 mi).

1955 June 7 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1882T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1956 June 7 - .
  • X-1E Flight 7 - . Crew: Walker, Joseph. Payload: X-1E flight 7. Nation: USA. Related Persons: Walker, Joseph. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1E. Summary: NACA flight 6. Mach 1.55 at 13725 m. Longitudinal and lateral trim changes in transonic region found annoying to pilot..

1956 June 7 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1E (A-1). LV Configuration: R-1E (A-1) 6.
  • Biological mission - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi). Summary: Payload, instruments, left and right animal containers all recovered. Smoke container functioned. Carried dogs..

1956 June 7 - . Launch Site: Wallops Island. LV Family: Nike. Launch Vehicle: Nike T40 T55 Nike.
  • Heat Transfer Re-entry Vehicle test - . Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).

1957 June 7 - .
  • X-1B Flight 18 - . Crew: McKay. Payload: X-1B flight 18. Nation: USA. Related Persons: McKay. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1B. Summary: NACA flight 8. Supersonic maneuvers to mach 1.5 at 18300 m to determine the dynamic and static stability and control characteristics..

1960 June 7 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25A. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1X-27. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 50 km (31 mi).

1961 June 7 - . LV Family: Little Joe II. Launch Vehicle: Little Joe II.
  • Preliminary study of Little Joe Senior - . Nation: USA. Program: Apollo. A preliminary study of a fin-stabilized solid-fuel rocket booster, the Little Joe Senior, was completed by members of STG. The booster would be capable of propelling a full-size Apollo reentry spacecraft to velocities sufficient to match critical portions of the Saturn trajectory. Additional Details: Preliminary study of Little Joe Senior.

1961 June 7 - . 00:40 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 2. LV Configuration: Skylark-2 SL26.
  • Test mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 184 km (114 mi).

1961 June 7 - . 11:20 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA5B. Launch Pad: LA5B?. LV Family: Black Knight. Launch Vehicle: Black Knight 201/C. LV Configuration: Black Knight-201/C BK.17. FAILURE: Failure.
  • Gaslight Re-entry Vehicle test - . Nation: UK. Agency: RAE. Apogee: 583 km (362 mi).

1961 June 7 - . 21:37 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF1. LV Family: Atlas. Launch Vehicle: Atlas E. LV Configuration: Atlas E 27E. FAILURE: Failure. Failed Stage: 1.
  • Research and development Category II test - . Nation: USA. Agency: USAF. Summary: First E launched at SMS 576 from OSTF-1, unsuccessful.

1962 June 7 - . LV Family: Saturn I; Saturn V.
  • von Braun recommends lunar orbit rendezvous mode for Apollo - . Nation: USA. Related Persons: von Braun. Program: Apollo. Spacecraft: Apollo CSM; Apollo Lunar Landing; CSM Recovery; CSM SPS. Wernher von Braun, Director, Marshall Space Flight Center, recommended to the NASA Office of Manned Space Flight that the lunar orbit rendezvous mode be adopted for the lunar landing mission. He also recommended the development of an unmanned, fully automatic, one-way Saturn C-5 logistics vehicle in support of the lunar expedition; the acceleration of the Saturn C-1B program; the development of high-energy propulsion systems as a backup for the service module and possibly the lunar excursion module; and further development of the F-1 and J-2 engines to increase thrust or specific impulse.

1962 June 7 - . 00:10 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.43GA.
  • Grenade, Inflating Sphere 4 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 120 km (70 mi).

1962 June 7 - . 00:56 GMT - . Launch Site: Wallops Island. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp NASA 03.21CA.
  • Sodium release Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 162 km (100 mi).

1962 June 7 - . 14:45 GMT - . Launch Site: Sonmiani. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun Rehbar 1.
  • Sodium release Aeronomy mission - . Nation: Pakistan. Agency: SUPARCO. Apogee: 126 km (78 mi).

1962 June 7 - . 18:21 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-1.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 June 7 - . 18:29 GMT - . Launch Site: Hidden Hills DZ. Launch Pad: 36.1 N x 116.0 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-29-50.
  • X-15A Local flow, M=5 test - . Nation: USA. Agency: NASA; USAF. Apogee: 31 km (19 mi). Summary: Maximum Speed - 5908 kph. Maximum Altitude - 31580 m..

1963 June 7 - . 19:00 GMT - . Launch Site: Cape Canaveral. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike Smoke 361.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 13 km (8 mi).

1964 June 7 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/4. LV Family: R-16. Launch Vehicle: R-16U.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1965 June 7 - .
  • Procurement of Apollo lunar surface experiments package authorized - . Nation: USA. Related Persons: Mueller. Program: Apollo. Spacecraft: Apollo ALSEP. George E. Mueller, Associate Administrator for Manned Space Flight, approved procurement of the lunar surface experiments package (LSEP). The package, to be deployed on the moon by each LEM crew that landed there, would transmit geophysical and other scientific data back to earth. NASA's Office of Space Science and Applications would make the final selection of experiments. Mueller emphasized that the LSEP must be ready in time for the first lunar landing mission. Management responsibility for the project was assigned to MSC's Experiments Program Office.

1965 June 7 - .
  • Rocket landing system for the Block II Apollo CM - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Block II. Summary: MSC directed NAA to make a "predesign" study of a rocket landing system for the Block II CM. (The Center had already studied the system's feasibility and had conducted full-scale drop tests.).

1965 June 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 810.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1965 June 7 - .
  • Landing of Gemini 4 - . Return Crew: McDivitt; White. Nation: USA. Related Persons: McDivitt; White. Program: Gemini. Flight: Gemini 4. Gemini 4 landed at 17:11 GMT in the Atlantic Ocean about 725 km east of Cape Kennedy - some 65 km from its nominal landing point due to failure of its guidance computer. The crew boarded a helicopter 34 minutes after landing and was transported to the prime recovery ship, the aircraft carrier Wasp. Spacecraft recovery was completed at 2:28 p.m., a little more than 100 hours after Gemini 4 had been launched. Gemini 4 was the first mission to be controlled from the mission control center in Houston. Additional Details: Landing of Gemini 4.

1966 June 7 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • Gemini launch vehicle 10 was removed from storage and erected at complex 19. - . Nation: USA. Flight: Gemini 10. Summary: Umbilicals were connected and power applied June 9. Subsystems Reverification Tests (SSRT) began immediately. SSRT ended June 16, and the Prespacecraft Mate Verification Combined Systems Test was conducted June 17..

1966 June 7 - . 02:48 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC12. LV Family: Atlas. Launch Vehicle: SLV-3 Agena B. LV Configuration: SLV-3 Agena B 5601 (AA16) / Agena B 6502.
  • OGO 3 - . Payload: OGO B. Mass: 634 kg (1,397 lb). Nation: USA. Agency: NASA Greenbelt. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OGO. Decay Date: 1981-09-15 . USAF Sat Cat: 2195 . COSPAR: 1966-049A. Apogee: 102,806 km (63,880 mi). Perigee: 19,519 km (12,128 mi). Inclination: 77.6000 deg. Period: 2,911.50 min. Orbiting Geophysical Observatory 3. All 21 experiments returned good data. At the time, this was the largest experimental complement ever put into orbit. There were 4 cosmic ray instruments (1 of which included a gamma-ray spectrometer), 4 plasma, 2 trapped radiation, 2 magnetic fields, 5 ionosphere, 3 radio/optical, and 1 micrometeoroid detectors. OGO 3 maintained 3-axis stabilization for 46 days. At that point, an attitude controller failed and the spacecraft was put into a spin on 23 July 1966. The spin period varied from 90-125 seconds. By June 1969, data acquisition was limited to 50% of the orbital path. Routine spacecraft operation was discontinued on December 1, 1969, after which only data from Heppner's experiment (Rubidium + Fluxgate magnetometer) was acquired. By March 1971 spacecraft perigee had increased to 16,400 km and the inclination had increased to 75.8 deg. All spacecraft support terminated on February 29, 1972.

1966 June 7 - . 16:57 GMT - . Launch Site: Wallops Island. Launch Vehicle: Wasp.
  • WASP slosh test Technology mission - . Nation: USA. Agency: NASA. Apogee: 238 km (147 mi).

1967 June 7 - . 13:20 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.272.
  • Meteor dust Meteorites mission - . Nation: USA. Agency: AFCRL. Apogee: 154 km (95 mi).

1968 June 7 - . 15:25 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure 1. LV Configuration: Centaure 1 CE-44.
  • ESRO C42 / 2 Meteorites mission - . Nation: Europe. Agency: ESRO. Apogee: 138 km (85 mi).

1969 June 7 - .
  • Borman to visit USSR - . Nation: USSR. Related Persons: Borman. Kamanin is advised that US astronaut Borman will arrive in Moscow in July, and he is to put together a program for him. Kamanin notes it has been difficult for the cosmonauts to appear in public - citizens pester them with unanswerable questions about the status of the Soviet moon landing program.

1970 June 7 - .
  • Soyuz 9 Day 7 - . Nation: USSR. Related Persons: Nikolayev; Sevastyanov; Tereshkova. Program: Soyuz. Flight: Soyuz 9. Soyuz 9's environmental control system is working well. Tereshkova and her daughter arrive at the command point at 14:40 after landing at the airfield at 12:00. The landing commission meets in the evening to consider contingency landings. It is reported that the crew is medically in better shape on Day 6 than Day 1, according to telemetry. In fact they are doing so well, extension of the flight to 20 days duration is discussed. Between 20:00 and 20:30 Tereshkova and her daughter communicate via radio and television with Nikolayev aboard Soyuz 9.

1970 June 7 - . 07:26 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C48/1.
  • ESRO C48 / 1 Solar ultraviolet mission - . Nation: Europe. Agency: ESRO. Apogee: 162 km (100 mi).

1971 June 7 - .
  • Soyuz 11 docks with Salyut 1. - . Nation: USSR. Related Persons: Dobrovolsky; Patsayev; Volkov. Program: Salyut. Flight: Soyuz 11. Spacecraft: Soyuz 7KT-OK; Salyut 1. A joint meeting of the Soyuz 11 State Commission and Soviet of Chief Designers takes place at Yevpaptoriya at 07:00. Aboard Soyuz 11, the Igla automatic rendezvous and docking system is switched on when the spacecrafft is 7 km from Salyut 1. There is no manual intervention in the process; Dobrovolsky simply makes reports to the ground of the rendezvous and docking system's progress. Docking itself takes place out of tracking range. There is considerable suspense in mission control during the 90-minute wait until reacquisition. Before leaving radio contact, telemetry showed a signal that the docking mechanism had depressurised, which would have prevented the cosmonauts from opening the hatch and entering the space station. But when the station comes back in view, it turns out that all went normally and the crew has already entered the station. Patsayev entered first, turned on the air regenerator, and replaced two failed fans. The crew report that the station atmosphere is unpleasant, with a strong burned smell. It will take 20 hours for all of the air in the station to cycle through the ECS scrubbers, so the crew is told to spend the first night aboard their Soyuz.

1971 June 7 - . 16:53 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 630. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-4.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1971 June 7 - . 19:35 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 4A. LV Configuration: Black Brant IVA CRL A16.108-1.
  • VLF Propagation Ionosphere VLF mission - . Nation: USA. Agency: AFCRL. Apogee: 800 km (490 mi).

1972 June 7 - . 11:23 GMT - . Launch Site: El Arenosillo. LV Family: Skua. Launch Vehicle: Skua 2. LV Configuration: Skua 2 MSC-7207.
  • Ionosphere mission - . Nation: UK. Agency: INTA. Apogee: 95 km (59 mi).

1973 June 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-22 Target mission - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1973 June 7 - . 15:15 GMT - .
  • EVA Skylab 2-2 - . Crew: Conrad; Kerwin. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.15 days. Nation: USA. Related Persons: Conrad; Kerwin. Program: Skylab. Class: Manned. Type: Manned space station. Flight: Skylab 2. Spacecraft: Skylab. Summary: Succeeded in release of jammed solar panel..

1974 June 7 - . 13:44 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC43. Launch Vehicle: Rocketsonde.
  • Met Sphere - . Nation: USA. Agency: MRN. Apogee: 95 km (59 mi).

1975 June 7 - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. LV Family: R-36M. Launch Vehicle: R-36M.
  • SLI? - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 June 7 - . 16:07 GMT - . Launch Site: Chilca. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.150GE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 259 km (160 mi).

1975 June 7 - . 16:25 GMT - . Launch Site: Chilca. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.541CA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 197 km (122 mi).

1976 June 7 - . 15:34 GMT - . Launch Site: Thule AFB. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1977 June 7 - .
  • Complete integrated checkout of Enterprise - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Complete integrated checkout and hot-fire ground test, Edwards, Enterprise (OV-101).

1978 June 7 - . 22:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53716-321.
  • Cosmos 1013 - . Payload: Strela-1M no. 145. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10930 . COSPAR: 1978-056A. Apogee: 1,554 km (965 mi). Perigee: 1,478 km (918 mi). Inclination: 74.0000 deg. Period: 116.30 min. Summary: Eight satellites launched by a single carrier rocket..
  • Cosmos 1014 - . Payload: Strela-1M no. 146. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10931 . COSPAR: 1978-056B. Apogee: 1,531 km (951 mi). Perigee: 1,479 km (919 mi). Inclination: 74.0000 deg. Period: 116.10 min.
  • Cosmos 1015 - . Payload: Strela-1M no. 147. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10932 . COSPAR: 1978-056C. Apogee: 1,516 km (941 mi). Perigee: 1,474 km (915 mi). Inclination: 74.0000 deg. Period: 115.90 min.
  • Cosmos 1016 - . Payload: Strela-1M no. 148. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10933 . COSPAR: 1978-056D. Apogee: 1,498 km (930 mi). Perigee: 1,471 km (914 mi). Inclination: 74.0000 deg. Period: 115.60 min.
  • Cosmos 1017 - . Payload: Strela-1M no. 149. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10934 . COSPAR: 1978-056E. Apogee: 1,492 km (927 mi). Perigee: 1,458 km (905 mi). Inclination: 74.0000 deg. Period: 115.40 min.
  • Cosmos 1018 - . Payload: Strela-1M no. 150. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10935 . COSPAR: 1978-056F. Apogee: 1,488 km (924 mi). Perigee: 1,442 km (896 mi). Inclination: 74.0000 deg. Period: 115.20 min.
  • Cosmos 1019 - . Payload: Strela-1M no. 151. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10936 . COSPAR: 1978-056G. Apogee: 1,488 km (924 mi). Perigee: 1,424 km (884 mi). Inclination: 74.0000 deg. Period: 115.00 min.
  • Cosmos 1020 - . Payload: Strela-1M no. 152. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 10937 . COSPAR: 1978-056H. Apogee: 1,484 km (922 mi). Perigee: 1,408 km (874 mi). Inclination: 74.0000 deg. Period: 114.80 min.

1979 June 7 - . 10:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65055-109.
  • Bhaskara 1 - . Payload: SEO. Mass: 441 kg (972 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: Bhaskara. Decay Date: 1989-02-17 . USAF Sat Cat: 11392 . COSPAR: 1979-051A. Apogee: 399 km (247 mi). Perigee: 394 km (244 mi). Inclination: 50.7000 deg. Period: 92.50 min. Summary: Launched from a cosmodrome in the USSR. Experimental satellite for conducting earth resources survey over India. .

1980 June 7 - . 03:07 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 76 km (47 mi).

1981 June 7 - . Launch Site: Tawiwa. Launch Vehicle: Otrag. LV Configuration: 4 x 2.5 tonne thrust.
  • Otrag Flight 5 - . Nation: Germany. Agency: OTRAG. Summary: High acceleration test, 20 % propellant loading.

1982 June 7 - . 20:37 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 73 km (45 mi).

1983 June 7 - . 02:32 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K/D-1. LV Configuration: Proton-K/D-1 321-02.
  • Venera 16 - . Payload: 4V-2 s/n 861. Mass: 4,000 kg (8,800 lb). Nation: USSR. Agency: MOM. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft: Venera 4V-2. USAF Sat Cat: 14107 . COSPAR: 1983-054A. Venus radar mapper; entered Venus orbit 10/14/83. Venera 16 was part of a two spacecraft mission (along with Venera 15) designed to use side-looking radar mappers to study the surface properties of Venus. The two spacecraft were inserted into Venus orbit a day apart with their orbital planes shifted by an angle of approximately 4 degrees relative to one another. This made it possible to reimage an area if necessary. Each spacecraft was in a nearly polar orbit with a periapsis at 62 N latitude. Together, the two spacecraft imaged the area from the north pole down to about 30 degrees N latitude over the 8 months of mapping operations.

1983 June 7 - . 07:50 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1468 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs F1-17F41. Duration: 14.00 days. Decay Date: 1983-06-21 . USAF Sat Cat: 14110 . COSPAR: 1983-055A. Apogee: 251 km (155 mi). Perigee: 211 km (131 mi). Inclination: 82.4000 deg. Period: 89.10 min. High resolution photo surveillance; film capsule; maneuverable; also performed earth resources tasks. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation.

1984 June 7 - . 00:16 GMT - . Launch Site: Wallops Island. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki PWN-11D.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 68 km (42 mi).

1985 June 7 - . 07:45 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1657 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs F1-17F41. Duration: 14.00 days. Decay Date: 1985-06-21 . USAF Sat Cat: 15806 . COSPAR: 1985-044A. Apogee: 282 km (175 mi). Perigee: 177 km (109 mi). Inclination: 82.3000 deg. Period: 89.10 min. Summary: High resolution photo surveillance; film capsule; maneuverable (?). Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..

1988 June 7 - . 14:03 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Soyuz TM-5 - . Call Sign: Rodnik (Spring - water spring). Crew: Aleksandrov, Aleksandr; Savinykh; Solovyov. Backup Crew: Lyakhov; Serebrov; Stoyanov. Payload: Soyuz TM 11F732 s/n 55. Mass: 7,000 kg (15,400 lb). Nation: USSR. Related Persons: Aleksandrov, Aleksandr; Savinykh; Solovyov; Lyakhov; Serebrov; Stoyanov. Agency: MOM. Program: Mir. Class: Manned. Type: Manned spacecraft. Flight: Mir EP-2; Mir EO-3. Spacecraft: Soyuz TM. Duration: 91.45 days. Decay Date: 1988-09-07 . USAF Sat Cat: 19204 . COSPAR: 1988-048A. Apogee: 216 km (134 mi). Perigee: 196 km (121 mi). Inclination: 51.6000 deg. Period: 88.60 min. Transported to the Mir orbital station a Soviet/Bulgarian crew comprising cosmonauts A Y Solovyev, V P Savinykh and A P Aleksandrov (Bulgaria) to conduct joint research and experiments with cosmonauts V G Titov and M K Manarov. Interim orbit 343 x 282 km. Maneuvered to Mir's 355 x 349 km orbit. Docked 15:57 GMT 9 June to Mir's aft port. Moved to forward port 18 June.

1989 June 7 - .
  • Death of Theo Vowe - . Nation: Germany; USA. Related Persons: Vowe. Summary: German-American engineer in WW2, member of the German rocket team, went to America after the first group. Died at Huntsville, Alabama..

1989 June 7 - . 05:12 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53711-225.
  • Cosmos 2026 - . Mass: 825 kg (1,818 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 20045 . COSPAR: 1989-042A. Apogee: 1,008 km (626 mi). Perigee: 951 km (590 mi). Inclination: 82.9000 deg. Period: 104.70 min. Summary: Military navigation satellite..

1991 June 7 - . 13:33 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 71 km (44 mi).

1992 June 7 - . 16:40 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 6920-X. LV Configuration: Delta 6920-10 D210.
  • EUVE - . Mass: 3,275 kg (7,220 lb). Nation: USA. Agency: NASA Greenbelt. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: EUVE. Decay Date: 2002-01-31 . USAF Sat Cat: 21987 . COSPAR: 1992-031A. Apogee: 524 km (325 mi). Perigee: 510 km (310 mi). Inclination: 28.4000 deg. Period: 95.00 min. Extreme Ultra-Violet Explorer; mapped galactic EUV sources. The Extreme Ultraviolet Explorer was switched off on February 2, 2001. NASA decided to terminate funding for the mission, even though the spacecraft was still operating well. The sky survey was completed in January 1993 and after that the EUVE was used by guest astronomers for observations of specific targets. The final observations were made on January 26, 2001. After end-of-life tests of the never-used backup high voltage supplies and checking the remaining battery capacity, EUVE was stabilized pointing away from the Sun and sent into safehold at 2359 GMT on January 31. The transmitters were commanded off on February 2.

1994 June 7 - . 07:20 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2281 - . Payload: Zenit-8 / Oblik no. 4. Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 22.00 days. Decay Date: 1994-07-29 . USAF Sat Cat: 23119 . COSPAR: 1994-032A. Apogee: 293 km (182 mi). Perigee: 236 km (146 mi). Inclination: 82.5000 deg. Period: 89.80 min. Military cartographic satellite; returned film capsule. Also photography of the earth's surface for the purpose of the natural resource mapping and area monitoring on behalf of various branches of the Russian economy and in the interests of international cooperation. Landed July 29.

1995 June 7 - .
  • Mir-Shuttle Docking Module delivered. - . Nation: Russia. Spacecraft: Mir-Shuttle Docking Module; Mir. Summary: Mir-Shuttle Docking Module flight article reached the Kennedy Space Center. It would be docked to the Mir station on November 14, 1995 at the Kristall module's axial docking port..

1996 June 7 - . 16:15 GMT - . Launch Site: White Sands. LV Family: DC-X. Launch Vehicle: DC-XA.
  • - . Nation: USA. Agency: NASA Huntsville. Apogee: 0 km ( mi). Summary: Maximum structural stresses with 50% full LOX tank. Reached altitude of 590 m during a 64 second flight..

2000 June 7 - . 13:19 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F29.
  • TSX 5 - . Payload: P95-2. Mass: 247 kg (544 lb). Nation: USA. Agency: USAF STP. Manufacturer: McLean. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: STEP. USAF Sat Cat: 26374 . COSPAR: 2000-030A. Apogee: 1,695 km (1,053 mi). Perigee: 412 km (256 mi). Inclination: 68.9379 deg. Period: 106.19 min. Military Technology satellite. Launch delayed from May 20 and June 6. Fifth STEP (Space Test Experiments Program) satellite. The satellite's main section was the STRV-2 experiment module, sponsored by the Ballistic Missile Defense Organization and the UK Ministry of Defense. This was to take infrared images of UK military aircraft at perigee, and then downlink data via laser. STRV-2 also carried vibration isolation and debris impact sensors. A secondary payload was the S97-1 CEASE (Compact Environmental Anomaly Sensor). This was an AFRL prototype sensor package to provide warning of spacecraft charging and radiation events.

2002 June 7 - . 08:24 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT179GM.
  • GT179GM Functional Dependency gate operational test launch - Test Flight, Guidance & Reentry Technologies - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi).

2006 June 7 - . 22:00 GMT - . Launch Site: Barking Sands. LV Family: Terrier. Launch Vehicle: Terrier Orion Improved. LV Configuration: Terrier Improved Orion NASA 41.071DR.
  • Target - . Nation: USA. Agency: NASA; NAWC. Apogee: 130 km (80 mi).

2007 June 7 - . 18:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2427 - . Mass: 6,700 kg (14,700 lb). Nation: Russia. Agency: VKS. Manufacturer: Kozlov. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 76.13 days. Decay Date: 2007-08-22 . USAF Sat Cat: 31595 . COSPAR: 2007-022A. Apogee: 339 km (210 mi). Perigee: 167 km (103 mi). Inclination: 67.1000 deg. Period: 89.80 min. Recoverable capsule military optical reconnaisance satellite. Orbit was raised on 11 June to 182 km x 354 km; decayed until 19 June, when it was lowered to 175 km x 325 km. On 28 June the orbit was raised to 183 km x 348 km; on 5 July to 169 km x 375 km. Landed at 21:00 GMT on 22 August after a 76-day mission.

2008 June 7 - .
  • STS-124 MCC Status Report #14 - . Nation: USA. Program: ISS. Flight: STS-124. Summary: The crew of Discovery began its eighth flight day this morning to the song “Taking Off.” It was performed by Godaigo and played for Mission Specialist Aki Hoshide. . Additional Details: STS-124 MCC Status Report #14 .

2011 June 7 - . 20:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG.
  • Soyuz TMA-02M - . Nation: Russia. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-28; ISS EO-27. Spacecraft: Soyuz TMA. USAF Sat Cat: 37633 . COSPAR: 2011-023A. Apogee: 403 km (250 mi). Perigee: 374 km (232 mi). Inclination: 51.6000 deg. Period: 92.30 min. Summary: Carried the EO-28 crew to the station. Docked with the ISS at the Rassvet on 9 June at 21:18 GMT..

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