Encyclopedia Astronautica
September 04


September 04 Chronology


1927 September 4 - .
1944 September 4 - . LV Family: V-2. Launch Vehicle: V-2.
  • First production V-2 delivered. - . Nation: Germany. 350 missiles were delivered in September, 500 in October, and 600 to 900 per month thereafter. There were many early failures of these production missiles - they had not been built for long-term storage. The solution was to use express trains to take the missiles from the factory to the launch areas and fire them within three days of leaving the production line.

1947 September 4 - .
  • XS-1 Flight 42 - . Crew: Yeager. Payload: XS-1 # 1 flight 24. Nation: USA. Related Persons: Yeager. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF flight 2. About mach 0.89. Telemeter failure required repeat of this flight..

1952 September 4 - . 09:17 GMT - . Launch Site: Arctic Ocean. Launch Pad: 77.2 N x 70.2 W. Launch Platform: WYG-279. LV Family: Rockoon. Launch Vehicle: Deacon Rockoon.
  • SUI 7 Chemical release mission - . Nation: USA. Agency: SUI. Apogee: 60 km (37 mi). Summary: Launched at Arctic Ocean Launch Site 1 Launch Point 7 - - Latitude: 77.18 N - Longitude: 70.22 W..

1953 September 4 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. Launch Pad: LC3/4?. LV Family: Bomarc. Launch Vehicle: Bomarc. LV Configuration: Bomarc 623-3. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 20 km (12 mi).

1958 September 4 - . 19:30 GMT - . Launch Site: Fort Churchill. LV Family: Loki. Launch Vehicle: Loki Dart. LV Configuration: Loki Dart II9.03F.
  • Chemical release / plasma mission - . Nation: USA. Agency: SUI. Apogee: 75 km (46 mi).

1959 September 4 - . Launch Site: Edwards. Launch Complex: Edwards RW04/22. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 2-A-2. FAILURE: Failure.
  • X-15A aborted launch. - . Nation: USA. Agency: NASA; USAF. Apogee: 14 km (8 mi).

1961 September 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/4. LV Family: R-16. Launch Vehicle: R-16. LV Configuration: R-16 23L.
  • Test mission - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1962 September 4 - .
  • Nine industry proposals for the Apollo lunar excursion module received - . Nation: USA. Program: Apollo. Spacecraft: Apollo LM; LM Source Selection. Nine industry proposals for the lunar excursion module were received from The Boeing Company, Douglas Aircraft Company, General Dynamics Corporation, Grumman Aircraft Engineering Corporation, Ling-Temco-Vought, Inc., Lockheed Aircraft Corporation, Martin-Marietta Corporation, Northrop Corporation, and Republic Aviation Corporation. NASA evaluation began the next day. Additional Details: Nine industry proposals for the Apollo lunar excursion module received.

1963 September 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 602. LV Family: Polaris. Launch Vehicle: Polaris A1.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1963 September 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 602. LV Family: Polaris. Launch Vehicle: Polaris A1.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1963 September 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 602. LV Family: Polaris. Launch Vehicle: Polaris A1.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1963 September 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 602. LV Family: Polaris. Launch Vehicle: Polaris A1.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1963 September 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 602. LV Family: Polaris. Launch Vehicle: Polaris A1.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1963 September 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 602. LV Family: Polaris. Launch Vehicle: Polaris A1.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1963 September 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/3. LV Family: R-16. Launch Vehicle: R-16U.
  • T - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1963 September 4 - . 13:11 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.91GE.
  • CR nuclei Cosmic rays mission - . Nation: USA. Agency: NASA. Apogee: 228 km (141 mi).

1964 September 4 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • Air Force Space Systems Division (SSD), supported by launch vehicle contractors, recommended that Gemini launch vehicle (GLV) 2 be flown as scheduled. - . Nation: USA. Manned Spacecraft Center had proposed dropping GLV-2 from the Gemini program because of possible ill effects resulting from the electromagnetic incident of August 17 and from Hurricane Cleo. GLV-3 would then be substituted for the second Gemini mission, and the program would be shortened by one flight. After reviewing the incidents, their effects, corrective action, and retesting, SSD, Martin, Aerospace, and Aerojet-General all felt GLV-2 should fly, and NASA accepted their recommendation.

1964 September 4 - . 01:20 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 5C. LV Configuration: Skylark-5C SL87A. FAILURE: Failure.
  • Test mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 182 km (113 mi).

1965 September 4 - . Launch Site: Baikonur. LV Family: R-7. Launch Vehicle: Molniya 8K78. LV Configuration: Molniya 8K78 s/n U103-27.
  • E-6 Launch Postponement - . Payload: E-6. Nation: USSR. Program: Luna. Class: Moon. Type: Lunar probe. Spacecraft: Luna E-6. Summary: The launch was delayed due to malfunction of the RKS system of the Stages 1/2's control system during pre-launch service..

1967 September 4 - . Launch Site: Baikonur. Launch Complex: Baikonur PU31. Launch Pad: PU31?. LV Family: Tsiklon. Launch Vehicle: R-36 8K67.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1968 September 4 - .
  • Von Braun performed a full-pressure suit test in the Neutral Buoyancy Tank. - . Nation: USA. Spacecraft: Orbital Workshop. MSFC Director Wernher von Braun performed a full-pressure suit test in the Saturn I Workshop immersed in the Neutral Buoyancy Tank. He reported that the upgraded seals used in the aft dome penetration sealing study were 'very good,' but recommended additional handholds and tether points.

1968 September 4 - . 01:04 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.913-1.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 227 km (141 mi).

1968 September 4 - . 01:29 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.913-2.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 232 km (144 mi).

1968 September 4 - . 14:50 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.130UA.
  • Structure Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 124 km (77 mi).

1969 September 4 - .
  • The critical design review on the ATM charger battery regulator module was held with satisfactory results. - . Nation: USA. Spacecraft: Apollo ATM. Summary: Numerous tests on the module components were conducted. An engineering prototype was undergoing thermal cycle, charge, and discharge test..

1970 September 4 - .
  • Death of James Martin Taylor at Palmdale, California. Crash of T-38 trainer. - . Nation: USA. Related Persons: Taylor. Summary: American test pilot astronaut, 1965-1969..

1971 September 4 - . 13:52 GMT - . Launch Site: Resolute Bay. LV Family: Black Brant. Launch Vehicle: Black Brant 3B. LV Configuration: Black Brant IIIB NASA 22.01UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 150 km (90 mi).

1973 September 4 - . 16:45 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.13DS-NP.
  • Solar Ultraviolet/Solar X-ray mission - . Nation: USA. Agency: NASA. Apogee: 235 km (146 mi).

1974 September 4 - . 10:24 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Aerobee. Launch Vehicle: Aerobee 200. LV Configuration: Aerobee 200 CRL A05.391-1.
  • HISTAR 8 Infrared astronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 193 km (119 mi).

1975 September 4 - . 16:35 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Plasma mission - . Nation: USSR. Apogee: 170 km (100 mi).

1976 September 4 - . 03:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: USHAKOV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 62 km (38 mi).

1978 September 4 - . 18:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1979 September 4 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle SSME Failure - . Nation: USA. Summary: In a test run, a liquid oxygen turbopump fails 9.7 seconds into the burn..

1979 September 4 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: DF-5.
  • - . Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Summary: Other sources say launch was from Taiyuan..

1980 September 4 - . 12:45 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-71.
  • Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 308 km (191 mi).

1981 September 4 - . 08:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1303 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-6U. Duration: 14.00 days. Decay Date: 1981-09-18 . USAF Sat Cat: 12801 . COSPAR: 1981-086A. Apogee: 363 km (225 mi). Perigee: 208 km (129 mi). Inclination: 70.4000 deg. Period: 90.20 min. Summary: Photo surveillance; returned film capsule..

1981 September 4 - . 11:06 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 1304 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Tsikada. USAF Sat Cat: 12803 . COSPAR: 1981-087A. Apogee: 972 km (603 mi). Perigee: 906 km (562 mi). Inclination: 82.9000 deg. Period: 103.80 min. Summary: Civilian naval navigation satellite; replaced Cosmos 926..

1982 September 4 - . 17:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 1405 - . Mass: 3,000 kg (6,600 lb). Nation: USSR. Agency: MO. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-P. Decay Date: 1984-01-31 . USAF Sat Cat: 13508 . COSPAR: 1982-088A. Apogee: 443 km (275 mi). Perigee: 425 km (264 mi). Inclination: 65.0000 deg. Period: 93.30 min. Summary: Ocean monitoring..

1983 September 4 - . Launch Site: Plesetsk. LV Family: RT-23. Launch Vehicle: RT-23U 15Zh60.
  • Test mission - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1984 September 4 - . 10:20 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1592 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 14.00 days. Decay Date: 1984-09-18 . USAF Sat Cat: 15257 . COSPAR: 1984-094A. Apogee: 352 km (218 mi). Perigee: 193 km (119 mi). Inclination: 72.9000 deg. Period: 90.00 min. Summary: Military cartographic satellite; returned film capsule; maneuverable..

1984 September 4 - . 15:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 320-01.
  • Cosmos 1593 - . Payload: Glonass s/n 18L. Mass: 1,250 kg (2,750 lb). Nation: USSR. Agency: MOM. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass . USAF Sat Cat: 15259 . COSPAR: 1984-095A. Apogee: 19,170 km (11,910 mi). Perigee: 19,090 km (11,860 mi). Inclination: 65.9000 deg. Period: 675.70 min. Summary: Glonass. Testing components and apparatus from the space navigation system being set up to determine the position of Soviet civil aircraft and vessels in the Soviet merchant marine and fishing fleet. Three satellites launched by a single rocket. .
  • Cosmos 1594 - . Payload: Glonass s/n 19L. Mass: 1,250 kg (2,750 lb). Nation: USSR. Agency: MOM. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 15260 . COSPAR: 1984-095B. Apogee: 19,188 km (11,922 mi). Perigee: 19,145 km (11,896 mi). Inclination: 64.8000 deg. Period: 677.20 min. Summary: Glonass. Testing components and apparatus from the space navigation system being set up to determine the position of Soviet civil aircraft and vessels in the Soviet merchant marine and fishing fleet. Three satellites launched by a single rocket..
  • Cosmos 1595 - . Payload: Glonass Dummy. Mass: 1,250 kg (2,750 lb). Nation: USSR. Agency: MOM. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 15261 . COSPAR: 1984-095C. Apogee: 19,178 km (11,916 mi). Perigee: 19,079 km (11,855 mi). Inclination: 64.8000 deg. Period: 675.70 min. Summary: Glonass. Testing components and apparatus from the space navigation system being set up to determine the position of Soviet civil aircraft and vessels in the Soviet merchant marine and fishing fleet. Three satellites launched by a single rocket..

1985 September 4 - . 07:05 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65011-241.
  • Cosmos 1680 - . Mass: 700 kg (1,540 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-2M. USAF Sat Cat: 16011 . COSPAR: 1985-079A. Apogee: 798 km (495 mi). Perigee: 774 km (480 mi). Inclination: 74.1000 deg. Period: 100.60 min. Summary: Replaced Cosmos 1538..

1986 September 4 - . 17:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 68 km (42 mi).

1987 September 4 - . 20:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: KRENKEL'. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 60 km (37 mi).

1989 September 4 - . Launch Site: Barking Sands. LV Family: Terrier. Launch Vehicle: Terrier Malemute. LV Configuration: Terrier Malemute SDIO Starmate.
  • Target mission - . Nation: USA. Agency: SDIO. Apogee: 724 km (449 mi).

1989 September 4 - . 05:54 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 34D/Transtage. LV Configuration: Titan 34D/Transtage 34D-2 (05D-7).
  • USA 43 - . Payload: DSCS II F-16. Nation: USA. Agency: USAF. Program: DSCS. Class: Communications. Type: Military communications satellite. Spacecraft: DSCS III. USAF Sat Cat: 20202 . COSPAR: 1989-069A. Apogee: 35,799 km (22,244 mi). Perigee: 35,777 km (22,230 mi). Inclination: 6.1000 deg. Period: 1,436.10 min. Summary: Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit; at 57 deg E in 1995..
  • USA 44 - . Payload: DSCS III F-4. Nation: USA. Agency: USAF. Program: DSCS. Class: Communications. Type: Military communications satellite. Spacecraft: DSCS III. USAF Sat Cat: 20203 . COSPAR: 1989-069B. Apogee: 35,808 km (22,250 mi). Perigee: 35,771 km (22,227 mi). Inclination: 5.0000 deg. Period: 1,436.30 min. Summary: Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit; at 60 deg E in 1995..

1989 September 4 - . 16:15 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K. LV Family: S. Launch Vehicle: S-520. LV Configuration: S-520-10.
  • CIR Cosmic infrared Infrared astronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 288 km (178 mi).

1990 September 4 - . 19:04 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.72UL.
  • Extreme ultraviolet Spectrometer Aeronomy / solar extreme ultraviolet mission - . Nation: USA. Agency: NASA. Apogee: 326 km (202 mi).

1991 September 4 - . 05:50 GMT - . Launch Site: Barking Sands. LV Family: Super Chief. Launch Vehicle: Talos Castor. LV Configuration: Talos Castor ZEST-1.
  • Tungsten dust cloud Target/Release mission - . Nation: USA. Agency: Sandia. Apogee: 330 km (200 mi). Summary: Tungsten dust release for SDIO..

1992 September 4 - .
  • Mir News 145: 1st Solovyov/Avdeyev - . Nation: Russia. Program: Mir. Flight: Mir EO-12. This EVA started on 3.09.92 at 1330 UTC (opening hatch airlock Module-D) and ended at 1749 UTC. This EVA is the 1st one in a series to install the VDU (External Movements Control Motor) in the Sofora girder of Kvant-1. The cosmonauts achieved the goals of this EVA. They worked on the container in which the motor was delivered by the freighter Progress-M14. The cosmonauts will continue this work on 7.09.92. It had been expected that during this EVA the cosmonauts would haul down the Soviet flag still waving in the top of the Sofora girder. They only replaced the flag, but certainly will remove it during one of the next 3 or 4 EVA's.

    During the EVA's OM Peter monitored the traffic from the Altair satellite. This traffic will be analysed later.

    Chris v.d. Berg, NL-9165/A-UK3202.


1995 September 4 - .
  • Mir News 270: Soyuz-TM22 launched from Baykonur. - . Nation: Russia. Program: Mir. Flight: Mir EO-20; Mir EO-19. This ship with on board the crew for the 20d Main Expedition to Mir and the Euromir'95 cosmonaut Thomas Reiter started flawlessly from Baykonur on 3.09.1995 at 0900 UTC (for the connoisseurs: 09.00.23.115). The Russians are the captain Yuriy Pavlovich Gidzenko, making his first spaceflight, Sergey Vasilyevich Avdeyev, making his 2d flight. The crew uses the call 'Uran', so for Gidzenko, Avdeyev and Reiter, respectively Uran-1, -2 and -3. The 1st day of the 2 days autonomous flight to Mir passed without any problems. Already during the 3d orbit at 120240 UTC Soyuz-TM22 came within our range. Gidzenko reported the successful check of the manual orientation control system. All went well. During the pass at 1332 UTC Gidzenko, sounding very fit, reported that the first 2 orbit corrections had been performed well. All systems worked without hitches and the health and mood of the crew were excellent.

    Planned linkup with Mir-station:

    If all continues to go according to plan the Soyuz-TM22 will dock at the forward docking port (P.Kh.O. -transition section), the -X axis on 5.09.95 at 1030 UTC. The last phase of the approach will take place within our range during Mir-orbit 54543 from 1018-1025 UTC. In this period we can expect radio traffic on the frequencies: 121.750 Mc (Soyuz-TM22) and 143.625 Mc (Mir). It is not possible to predict whether the old Altair on 17 dgs West will be used or not for this good old 'geo' did not show up since 26.08.95 0824 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202


1996 September 4 - . 09:01 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2.
  • Cosmos 2333 - . Payload: Tselina-2 no. 20. Nation: Russia. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-2. USAF Sat Cat: 24297 . COSPAR: 1996-051A. Apogee: 852 km (529 mi). Perigee: 849 km (527 mi). Inclination: 70.9000 deg. Period: 101.90 min. Summary: New heavy ELINT class..

1997 September 4 - . 12:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas IIAS. LV Configuration: Atlas IIAS AC-146.
  • GE 3 - . Nation: USA. Agency: GE Americom. Manufacturer: RCA. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 24936 . COSPAR: 1997-050A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Geosynchronous. Stationed over 87.1W Launch vehicle put payload into supersynchronous earth orbit with IFR/MRS trajectory option. Positioned in geosynchronous orbit at 87 deg W in 1997-1999 As of 3 September 2001 located at 87.12 deg W drifting at 0.002 deg W per day. As of 2007 Mar 11 located at 86.99W drifting at 0.010W degrees per day.

1999 September 4 - . 22:34 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 42P. LV Configuration: Ariane 42P-3 V120.
  • Koreasat 3 - . Payload: Mugunghwa 3. Nation: Korea South. Agency: KT. Manufacturer: Lockheed. Program: Koreasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 25894 . COSPAR: 1999-046A. Apogee: 35,792 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Geosynchronous communications satellite. Stationed at 112 deg E. Positioned in geosynchronous orbit at 112 deg E in 1999. As of 31 August 2001 located at 115.99 deg E drifting at 0.014 deg W per day. As of 2007 Mar 10 located at 116.12E drifting at 0.008W degrees per day.

2002 September 4 - . 10:00 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A.
  • RO-A-FS-05 Aeronomy mission - . Nation: Germany. Agency: DLR. Apogee: 75 km (46 mi).

2003 September 4 - .
2006 September 4 - . Launch Site: Taiyuan. LV Family: DF-31. Launch Vehicle: DF-31.
  • DF-31 test - . Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi).

2009 September 4 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral ETR. LV Family: Trident. Launch Vehicle: Trident D-5.
  • USN Mk 5? RV - . Mass: 1,000 kg (2,200 lb). Nation: USA. Agency: USN. Summary: Operational test.

2010 September 4 - . 16:14 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B.
  • Chinasat 6A - . Payload: Zhongxing 6A. Mass: 5,100 kg (11,200 lb). Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 37150 . COSPAR: 2010-042A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: C and Ku band communications transponders..

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