Encyclopedia Astronautica
September 07


September 07 Chronology


1914 September 7 - .
  • Birth of James A Van Allen - . Nation: USA. Summary: American astrophysicist; his experiment carried aboard the first American satellite established the existence of radiation belts that encircled the Earth; also very active in sounding rocket experiments..

1939 September 7 - .
  • Birth of Stanley David Griggs - . Nation: USA. Summary: American test pilot mission specialist astronaut. Flew on STS-51-D..

1944 September 7 - . Launch Site: V-2 Battery 444. LV Family: V-2. Launch Vehicle: V-2.
  • V-2 Battery 444 moves to a point near Houffalize, Belgium. - . Nation: Germany. Agency: Wehrmacht.

1956 September 7 - .
  • X-1B Flight 13 - . Crew: McKay. Payload: X-1B flight 13. Nation: USA. Related Persons: McKay. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1B. Summary: NACA flight 3. Speed run to 17080 m and mach 1.8. Limited heating data gathered..

1956 September 7 - .
  • X-2 Flight 16 - . Crew: Kincheloe. Payload: X-2 # 1 flight 16. Nation: USA. Related Persons: Kincheloe. Class: Manned. Type: Manned rocketplane. Spacecraft: X-2 . Summary: 12th powered flight. Capt. Iven C. Kincheloe (USAF) set new unofficial altitude record for manned flight at Edwards AFB, Calif., piloting a Bell X-2 rocket-powered aircraft to a height of 38,491 m, top speed Mach 1.7..

1957 September 7 - . 11:39 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: R-7. LV Configuration: R-7 No. 9.
  • M1-10 (I-4) test - . Nation: USSR. Agency: MVS. Apogee: 1,350 km (830 mi). Summary: Second successful ICBM flight..

1958 September 7 - . 10:33 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA5A. LV Family: Black Knight. Launch Vehicle: Black Knight 201. LV Configuration: Black Knight-201 BK.01.
  • Research and development test - . Nation: UK. Agency: RAE. Apogee: 225 km (139 mi). Summary: Black Knight missile of the United Kingdom was launched from the Australian range at Woomera to an altitude of over 300 miles..

1959 September 7 - . 12:45 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Agency: AN. Apogee: 85 km (52 mi).

1960 September 7 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-56-1929.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1961 September 7 - . LV Family: Saturn C-3; Saturn V.
  • Selection of Saturn first stage assembly plant - . Nation: USA. Program: Apollo. Class: Manned. Type: Manned space station. NASA announced that the government-owned Michoud Ordnance Plant near New Orleans, La., would be the site for fabrication and assembly of the Saturn C-3 first stage as well as larger vehicles. Finalists were two government-owned plants in St. Louis and New Orleans. The height of the factory roof at Michoud meant that an 8 x F-1 engined vehicle could not be built; 4 or 5 engines would have to be the maximum.

1961 September 7 - . 01:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I AJ-17.
  • Mk 4 re-entry vehicle test - . Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). Summary: USAF Titan successfully launched from Atlantic Missile Range, making 6,100-mile flight..

1961 September 7 - . 18:17 GMT - . Launch Site: Salto di Quirra. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp ISRC-RS-06.
  • Aeronomy mission - . Nation: Italy. Agency: CRS. Apogee: 200 km (120 mi).

1962 September 7 - .
  • Apollo boilerplate model BP-1 accepted by NASA - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Block I. Apollo command module boilerplate model BP-1 was accepted by NASA and delivered to the NAA Engineering Development Laboratory for land and water impact tests. On September 25, BP-1 was drop-tested with good results. Earth-impact attenuation and crew shock absorption data were obtained.

1963 September 7 - .
1966 September 7 - .
  • Laboratories for receiving Apollo lunar materials discussed - . Nation: USA. Program: Apollo. In response to a query from NASA Deputy Administrator Robert C. Seamans, Jr., Associate Administrator for Space Science and Applications Homer E. Newell said that no laboratories had been selected for receiving lunar materials but proposals had been solicited and were in process of review. Newell said the lunar samples fell under the planetary and planetary biology disciplines primarily. The Planetary Biology Subcommittee of the Space Science Steering Committee had four working groups evaluating the proposals geophysics, geochemistry, geology, and Lunar Receiving Laboratory (LRL). The working groups were expected to complete their evaluations in September and, following review by the program office, recommendations would be prepared for the Space Science Steering Committee. Following appropriate review by that Committee, Newell would select the Principal Investigators for approved experiments.

    Funding for the analyses could be determined only after selections had been made, but budget estimates for that purpose had been made for $2 million in FY 1968 and $6 million in FY 1969, exclusive of laboratory upgrading and funding of the LRL. As a part of the continuing research effort, 33 laboratories had received support during 1966 for upgrading their ability to handle and examine lunar material. Newell added that 125 proposals for handling lunar material had been received and were under review.


1967 September 7 - .
  • LM-1 (Apollo 5) continued to have serious schedule difficulties - . Nation: USA. Program: Apollo. Spacecraft: Apollo LM. LM-1 (Apollo 5) continued to have serious schedule difficulties. However, all known problems were resolved with the exception of the propulsion system leaks. Leak checks of the ascent stage indicated excessive leaking in the incline oxidizer orifice flange. The spacecraft was approximately 39 days behind the July 18, LM-1 KSC Operations Flow Plan.

1967 September 7 - . 05:00 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.176.
  • Density Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 101 km (62 mi).

1967 September 7 - . 20:34 GMT - . Launch Site: Arecibo. Launch Complex: Arecibo VB. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.308UI.
  • Lower ionosphere Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1967 September 7 - . 20:34 GMT - . Launch Site: Tonopah. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-88.
  • LRL BOX-8a X-ray astronomy mission - . Nation: USA. Agency: Sandia. Apogee: 187 km (116 mi).

1967 September 7 - . 22:04 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta G. LV Configuration: Thor Delta G 475/D51.
  • Biosatellite 2 - . Payload: Biosat 2. Mass: 507 kg (1,117 lb). Nation: USA. Agency: NASA Ames. Class: Biology. Type: Biology satellite. Spacecraft: Biosatellite. Decay Date: 1967-09-15 . USAF Sat Cat: 2935 . COSPAR: 1967-083A. Apogee: 318 km (197 mi). Perigee: 297 km (184 mi). Inclination: 33.5000 deg. Period: 90.70 min. Biological capsule recovered. The scientific payload, consisting of 13 select biology and radiation experiments, was exposed to microgravity during 45 hours of Earth-orbital flight. Experimental biology packages on the spacecraft contained a variety of specimens, including insects, frog eggs, microorganisms and plants. The planned three-day mission was recalled early because of the threat of a tropical storm in the recovery area, and because of a communication problem between the spacecraft and the tracking systems. The primary objective of the Biosatellite II mission was to determine if organisms were more, or less, sensitive to ionizing radiation in microgravity than on Earth. To study this question, an artificial source of radiation was supplied to a group of experiments mounted in the forward part of the spacecraft.

1968 September 7 - . 17:00 GMT - . Launch Site: Sea-launched. Launch Pad: M9132. Launch Platform: SHIP-SOV. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Agency: GMS. Apogee: 80 km (49 mi).

1969 September 7 - . 02:00 GMT - . Launch Site: Kagoshima. LV Family: MT-135. Launch Vehicle: MT-135P. LV Configuration: MT-135P MT-135-P -002.
  • Aeronomy mission - . Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi).

1970 September 7 - . 20:15 GMT - . Launch Site: Leba. LV Family: Meteor. Launch Vehicle: Meteor-3.
  • Aeronomy mission - . Nation: Poland. Agency: PIHM. Apogee: 62 km (38 mi).

1971 September 7 - . 01:15 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M Yu149-42.
  • Cosmos 436 - . Mass: 875 kg (1,929 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-O. Decay Date: 1980-01-04 . USAF Sat Cat: 5461 . COSPAR: 1971-074A. Apogee: 543 km (337 mi). Perigee: 510 km (310 mi). Inclination: 74.0000 deg. Period: 95.10 min. Summary: Possible ELINT satellite..

1971 September 7 - . 23:57 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.493CA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 176 km (109 mi).

1972 September 7 - . 22:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1973 September 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-44 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 September 7 - . 01:40 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima T. LV Family: S. Launch Vehicle: JCR. LV Configuration: JCR-9.
  • Test mission - . Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).

1974 September 7 - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.25DG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 250 km (150 mi).

1976 September 7 - . Launch Site: WTR Launch Area. Launch Platform: SSBN 609. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3T.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1976 September 7 - . Launch Site: WTR Launch Area. Launch Platform: SSBN 609. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3T.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1977 September 7 - .
  • Lower forward fuselage on dock, Palmdale, Columbia - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Columbia.

1978 September 7 - . 03:10 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 70 km (43 mi).

1979 September 7 - . 17:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC43. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 95 km (59 mi).

1981 September 7 - . 09:38 GMT - . Launch Site: Kagoshima. LV Family: S. Launch Vehicle: S-310. LV Configuration: S-310-11.
  • Submillimeter atmospheric spectra Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 193 km (119 mi).

1982 September 7 - . 20:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 88 km (54 mi).

1983 September 7 - . 13:24 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1496 - . Payload: Yantar-4K1 s/n 251. Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 42.00 days. Decay Date: 1983-10-19 . USAF Sat Cat: 14326 . COSPAR: 1983-093A. Apogee: 338 km (210 mi). Perigee: 167 km (103 mi). Inclination: 67.2000 deg. Period: 89.60 min. Summary: High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1983 September 7 - . 15:00 GMT - . Launch Site: White Sands. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.40UU.
  • CWAS 6 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1984 September 7 - . 19:13 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Cosmos 1596 - . Payload: Oko #37. Mass: 1,800 kg (3,900 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. USAF Sat Cat: 15267 . COSPAR: 1984-096A. Apogee: 35,908 km (22,312 mi). Perigee: 4,503 km (2,798 mi). Inclination: 67.8000 deg. Period: 718.90 min. Summary: Replaced Cosmos 1348. Covered Oko constellation plane 9 - 238 degree longitude of ascending node..

1985 September 7 - . 09:45 GMT - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Orion Sounding Rocket. LV Configuration: Orion NASA 30.26UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 85 km (52 mi).

1986 September 7 - . 07:48 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: USHAKOV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 60 km (37 mi).

1987 September 7 - . 23:50 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32. Launch Pad: LC32/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1875 - . Payload: Strela-3 no. 17. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 18334 . COSPAR: 1987-074A. Apogee: 1,408 km (874 mi). Perigee: 1,387 km (861 mi). Inclination: 82.6000 deg. Period: 113.70 min. Summary: Military store-dump communications satellite. Six satellites launched by a single carrier rocket..
  • Cosmos 1877 - . Payload: Strela-3 no. 19. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 18336 . COSPAR: 1987-074C. Apogee: 1,410 km (870 mi). Perigee: 1,407 km (874 mi). Inclination: 82.6000 deg. Period: 114.00 min.
  • Cosmos 1880 - . Payload: Strela-3 no. 22. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 18339 . COSPAR: 1987-074F. Apogee: 1,409 km (875 mi). Perigee: 1,393 km (865 mi). Inclination: 82.6000 deg. Period: 113.80 min.
  • Cosmos 1878 - . Payload: Strela-3 no. 20. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 18337 . COSPAR: 1987-074D. Apogee: 1,409 km (875 mi). Perigee: 1,403 km (871 mi). Inclination: 82.6000 deg. Period: 113.90 min.
  • Cosmos 1876 - . Payload: Strela-3 no. 18. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 18335 . COSPAR: 1987-074B. Apogee: 1,415 km (879 mi). Perigee: 1,409 km (875 mi). Inclination: 82.6000 deg. Period: 114.10 min.
  • Cosmos 1879 - . Payload: Strela-3 no. 21. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 18338 . COSPAR: 1987-074E. Apogee: 1,409 km (875 mi). Perigee: 1,397 km (868 mi). Inclination: 82.6000 deg. Period: 113.90 min.

1988 September 7 - . 11:41 GMT - . Launch Site: Thumba. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1988 September 7 - .
  • Landing of Soyuz TM-5 - . Return Crew: Lyakhov; Mohmand. Nation: USSR. Related Persons: Lyakhov; Mohmand. Program: Mir. Flight: Mir EP-3; Mir LD-2; Mir EO-3. Undocked 22:55 GMT 5 September. Jettisoned Orbital Module 23:35 GMT 5 September. Planned landing 02:15 September 6 1988 failed due to confusion of infrared horizon sensors. Repeat retrofire attempt one orbit later resulted in a partial burn only. The crew had to spend a tense 24 hours in the cramped Descent Module (the Orbital Module having already been jettisoned before the retrofire burn) before making last chance deorbit. Finally Lyakhov and Afghani cosmonaut Mohmand (Soyuz TM-6) returned safely to Earth and landed September 7, 1988 00:50 GMT, 160 km SE Dzhezkazgan.

1990 September 7 - . 11:59 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Resurs F-09 - . Payload: Resurs-F1 14F43 s/n 51. Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs F1-14F43. Duration: 14.00 days. Decay Date: 1990-09-21 . USAF Sat Cat: 20794 . COSPAR: 1990-082A. Apogee: 238 km (147 mi). Perigee: 177 km (109 mi). Inclination: 82.5000 deg. Period: 88.70 min. Summary: Carried German microgravity experiment. Investigation of the natural resources of the Earth in the interests of various branches of the national economy of the USSR; solution of problems relating to ecology and international cooperation. .

1991 September 7 - .
  • Death of Chandler Cole 'Chan' Ross - . Nation: USA. Related Persons: Ross, Chan. Summary: American engineer. Director of numerous advanced projects at Aerojet (including Aerotojet, Aerorocket, NERVA)..

1992 September 7 - . 11:47 GMT - .
  • EVA Mir EO-12-2 - . Crew: Solovyov; Avdeyev. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.21 days. Nation: Russia. Related Persons: Solovyov; Avdeyev. Program: Mir. Class: Manned. Type: Manned space station. Flight: Mir EO-12. Spacecraft: Mir. Summary: Continued installation of VDU thruster pod on Sofora tower..

1993 September 7 - .
1993 September 7 - . 13:25 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Cosmos 2262 - . Payload: Orlets-1 no. 5. Mass: 6,500 kg (14,300 lb). Nation: Russia. Agency: MOM. Program: Orlets. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Orlets-1. Duration: 102.00 days. Decay Date: 1993-12-18 . USAF Sat Cat: 22789 . COSPAR: 1993-057A. Apogee: 261 km (162 mi). Perigee: 182 km (113 mi). Inclination: 64.9000 deg. Period: 88.90 min. Summary: Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited. First launch that demonstrated doubled operational life..

1994 September 7 - . 14:41 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper 16PA.
  • Operational test - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,000 km (600 mi).

1995 September 7 - . 15:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-69.
  • STS-69 - . Call Sign: Endeavour. Crew: Cockrell; Gernhardt; Newman; Voss; Walker, Dave. Payload: Endeavour F09 / Spartan / WSF. Mass: 11,499 kg (25,350 lb). Nation: USA. Related Persons: Cockrell; Gernhardt; Newman; Voss; Walker, Dave. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-69. Spacecraft: Endeavour. Duration: 10.85 days. Decay Date: 1995-09-18 . USAF Sat Cat: 23667 . COSPAR: 1995-048A. Apogee: 321 km (199 mi). Perigee: 321 km (199 mi). Inclination: 28.4500 deg. Period: 91.40 min. Deployed and retrieved Spartan 201, WSF 2. Payloads: Wake Shield Facility (WSF) 2; Shuttle Pointed Autonomous Research Tool for As-tronomy (SPARTAN) 201; International Extreme Ultraviolet Hitchhiker (IEH)1; Inter-Mars Tissue Equivalent Proportional Counter (ITEPC); Extravehicular Activity Development Flight Test (EDFT) 2; Capillary Pumped Loop (CAPL) 2/ getaway special (GAS) bridge assembly with five GAS payloads; Auroral Photography Experiment (APE) B; Biological Research in Canisters (BRIC); Commercial Generic Bioprocessing Apparatus (CGBA), Configuration A; Electrolysis Perfor-mance Improvement Concept Study (EPICS); Space Tissue Loss (STL)/National Institutes of Health (NIH) Cells (C); Commercial Middeck Instrumentation Technology Associates Experiment (CMIX).
  • IEH-1 - . Payload: IEH-1/HH-M. Nation: USA. Agency: NASA. Program: STS. Decay Date: 1995-09-18 . USAF Sat Cat: 23667 . COSPAR: 1995-048xx. Apogee: 345 km (214 mi). Perigee: 339 km (210 mi). Inclination: 28.5000 deg. Period: 91.40 min.
  • GBA-8/CAPL - . Nation: USA. Agency: NASA. Program: STS. Decay Date: 1995-09-18 . USAF Sat Cat: 23667 . COSPAR: 1995-048xx. Apogee: 345 km (214 mi). Perigee: 339 km (210 mi). Inclination: 28.5000 deg. Period: 91.40 min.
  • Spartan 201 - . Nation: USA. Agency: NASA Greenbelt. Program: STS. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Spartan. Decay Date: 1995-09-18 . USAF Sat Cat: 23668 . COSPAR: 1995-048B. Apogee: 376 km (233 mi). Perigee: 368 km (228 mi). Inclination: 28.5000 deg. Period: 92.00 min. Summary: Released by STS-69 9/8/95; retrieved 9/10/95; examined solar corona..
  • WSF 2 - . Payload: Wake Shield Facility. Mass: 1,935 kg (4,265 lb). Nation: USA. Agency: SII. Class: Materials. Type: Materials science satellite. Spacecraft: WSF. Decay Date: 1995-09-18 . USAF Sat Cat: 23669 . COSPAR: 1995-048C. Apogee: 405 km (251 mi). Perigee: 397 km (246 mi). Inclination: 28.5000 deg. Period: 92.60 min. Summary: Wake Shield Facility; released by STS-69 9/11/95; retrieved 9/14/95; semiconductor materials research. Retrieved by Endeavour Sep 14 .

1998 September 7 - . 02:00 GMT - . Launch Site: Kagoshima. LV Family: MT-135. Launch Vehicle: MT-135. LV Configuration: MT-135-68.
  • Ozone Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 57 km (35 mi).

1999 September 7 - . 02:00 GMT - . Launch Site: Kagoshima. LV Family: MT-135. Launch Vehicle: MT-135. LV Configuration: MT-135-70.
  • Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 55 km (34 mi).

2000 September 7 - . 02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi).

2001 September 7 - . 19:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC8. LV Family: Minotaur. Launch Vehicle: Minotaur 1. LV Configuration: Minotaur 2.
  • Picosat 7/8 - . Nation: USA. Agency: USAF AFSPC. Class: Technology. Type: Navigation technology satellite. Spacecraft: Picosat. Decay Date: 2002-07-11 . USAF Sat Cat: 26929 . COSPAR: 2000-042C. Apogee: 286 km (177 mi). Perigee: 266 km (165 mi). Inclination: 97.8000 deg. Period: 90.00 min. Picosat 7/Picosat 8, were ejected from the Mightysat II.1 satellite on September 7 at 1939 UTC into a 511 x 539 km x 97.8 deg orbit. The 0.25 kg satellites were connected by a 30 m tether and were cataloged as a single object. Mightysat II.1 (Sindri) was launched in July 2000, and the deployment of the picosats was planned for a year after launch.

2004 September 7 - . 11:45 GMT - . Launch Site: Kwajalein. LV Family: Black Brant. Launch Vehicle: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.132GE.
  • EQUIS II Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 250 km (150 mi).

2004 September 7 - . 23:56 GMT - . Launch Site: Kwajalein. LV Family: Terrier. Launch Vehicle: Terrier Orion Improved. LV Configuration: Terrier Improved Orion NASA 41.048UE.
  • EQUIS II Ionosphere mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 130 km (80 mi).

2005 September 7 - .
  • Cassini, Titan Flyby, Successful - . Nation: USA. Spacecraft: Cassini.

2005 September 7 - . 08:53 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • GT-187GM-1 operational test launch - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi). Summary: Minuteman operational missile test. Delayed from February 9, March 23, 25 and 26. Initial missile replaced after contamination by rain on March 22. Failed to launch on April 27 and June 1. 2 dummy warheads..

2006 September 7 - .
  • Cassini, Titan Flyby - . Nation: USA. Spacecraft: Cassini.

2006 September 7 - . 15:50 GMT - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: TK-208. Launch Vehicle: Bulava. FAILURE: Failure.
  • Bulava SLBM test - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 mi).

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