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Vandenberg SLC6
Part of Vandenberg
Delta IV, Athena launch complex. Space Launch Complex
First Launch: 1995-08-15. Last Launch: 2013-08-28. Number: 9 . Longitude: -120.63 deg. Latitude: 34.58 deg.
Country:
USA.
Spacecraft:
EIS,
Topaz,
GemStar,
Lewis satellite,
Ikonos,
DMSP Block 5D-3,
Jumpseat-2.
Launch Vehicles:
Raven,
Athena-1,
LLV-1,
LMLV-1,
Athena-2,
Delta 4M+(4,2),
Delta 4M,
Delta 4H,
Delta 4M+(5,2).
Launch Sites:
Vandenberg.
1995 August 15 - .
22:30 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Athena.
Launch Vehicle:
Athena-1.
FAILURE: Destroyed by range safety 160 sec into flight after failure of thrust vector control system..
Failed Stage: 2.
- GemStar 1 (VitaSat) - .
Payload: Gemstar DSS-1. Mass: 113 kg (249 lb). Nation: USA.
Agency: LMSC.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: GemStar.
Decay Date: 1995-08-15 . Global Electronic Messaging Satellite..
1997 August 23 - .
06:51 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Athena.
Launch Vehicle:
Athena-1.
- Lewis - .
Payload: SSTI/Lewis. Nation: USA.
Agency: NASA,
TRW.
Manufacturer: Chantilly.
Class: Earth.
Type: Earth resources satellite. Spacecraft Bus: T200.
Spacecraft: Lewis satellite.
Decay Date: 1997-09-28 . USAF Sat Cat: 24909 . COSPAR: 1997-044A. Apogee: 134 km (83 mi). Perigee: 124 km (77 mi). Inclination: 97.50 deg. Period: 87.10 min. Reentered Sep 28.
1999 April 27 - .
18:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Athena.
Launch Vehicle:
Athena-2.
FAILURE: Payload shroud failed to separate four minutes after launch..
Failed Stage: S.
1999 September 24 - .
18:21 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Athena.
Launch Vehicle:
Athena-2.
- Ikonos - .
Mass: 726 kg (1,600 lb). Nation: USA.
Agency: SpaceIm.
Manufacturer: Lockheed.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: LM-900.
Spacecraft: Ikonos.
USAF Sat Cat: 25919 . COSPAR: 1999-051A. Apogee: 679 km (421 mi). Perigee: 678 km (421 mi). Inclination: 98.10 deg. Period: 98.30 min. Commercial / civilian high resolution (1 metre resolution) photograhic satellite..
2006 June 25 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(4,2).
- USA 184 - .
Payload: Raven 4 / NROL-22. Mass: 4,500 kg (9,900 lb). Nation: USA.
Agency: NRO.
Class: Surveillance.
Type: ELINT. Spacecraft: Raven satellite.
USAF Sat Cat: 29249 . COSPAR: 2006-027A. Apogee: 39,000 km (24,000 mi). Perigee: 1,100 km (600 mi). Inclination: 63.60 deg. Period: 720.00 min.
Secret payload for the National Reconnaissance Office. The intended orbit was thought to be a "Molniya" elliptical 12-hour orbit with an inclination of 63 degrees. American data relay and signals intelligence satellites have used this orbit in the past, notably the Jumpseat series of 1971-1983. A secondary payload was later confirmed to be the first SBIRS-HEO (Space-based Infrared System) sensor. SBIRS was the successor to the DSP (Defence Support Program), which provided early warning of missile launches. Also carried the NASA/Los Alamos TWINS-A magnetospheric research payload
2006 November 4 - .
13:53 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M.
- DMSP-Block-5D3-F17 - .
Mass: 1,154 kg (2,544 lb). Nation: USA.
Agency: USAF.
Program: DMSP.
Class: Earth.
Type: Weather satellite. Spacecraft Bus: TIROS N.
Spacecraft: DMSP Block 5D-3.
USAF Sat Cat: 29522 . COSPAR: 2006-050A. Apogee: 855 km (531 mi). Perigee: 841 km (522 mi). Inclination: 98.80 deg. Period: 101.90 min.
Defense Meteorological Satellite Program satellite with the Operational Linescan System camera, a microwave imager-sounder, ultraviolet spectrometers, particle detectors, a magnetometer, and a laser threat warning sensor. Reportedly went for a time into safe mode due to software problems after launch. The booster upper stage was conducted a maneuver to deorbit itself after placing the satellite in orbit. After the burn an explosion evidently occurred aboard the stage - dozens of objects were tracked in various orbits with perigees down to 670 km and apogees up to 851 km.
2011 January 20 - .
21:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 224 - .
Payload: EIS-6 / NROL-49. Mass: 17,000 kg (37,000 lb). Nation: USA.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 37348 . COSPAR: 2011-002A. National Reconnaissance Office satellite placed into 252 km x 1023 km x 97.9 deg polar orbit, consistent with reports that it is was an Improved CRYSTAL type (KH-11 derivative) imaging reconnaissance satellite..
2012 April 3 - .
23:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(5,2).
- USA 234 - .
Payload: NROL-25. Nation: USA.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Topaz.
USAF Sat Cat: 38109 . COSPAR: 2012-014A. Second FIA Radarsat mission, following NROL-41 / USA-25 / 2010-46A..
2013 August 28 - .
18:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 245 - .
Payload: EIS- 7 / NROL-65. Mass: 15,000 kg (33,000 lb). Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: EIS.
USAF Sat Cat: 39232 . COSPAR: 2013-043A. Apogee: 1,002 km (622 mi). Perigee: 259 km (160 mi). Inclination: 97.90 deg. Secret payload for the National Reconnaissance Office; thought to be an imaging spy satellite of the EIS/Enhanced CRYSTAL type..
2016 February 10 - .
11:40 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(5,2).
- USA 267 - .
Payload: TOPAZ 4?. Nation: USA.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Topaz.
USAF Sat Cat: 41334 . COSPAR: 2016-010A. Apogee: 1,085 km (674 mi). Perigee: 1,078 km (669 mi). Inclination: 123.00 deg. Satellite for the US National Reconnaissance Office. The launch was designated NRO L-45. The USA 267 payload was observed in a 1078 x 1085 km orbit with a retrograde 123 degree inclination, characteristic of the TOPAZ radar imaging satellites..
2018 January 12 - .
22:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4M+(5,2).
2019 January 19 - .
19:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC6.
LV Family:
Delta IV.
Launch Vehicle:
Delta 4H.
- USA 290 - .
Nation: USA.
Type: Imaging 0. Spacecraft: Improved Crystal.
USAF Sat Cat: 43941 . COSPAR: 2019-004A.
See KH-11 17 (Crystal 17, USA 290, NROL 71) ?. National Reconnaissance Office satellite believed to be the first of a new series of imaging spy satellites, probably derived from the Improved CRYSTAL design
that in turn descended from the 1970s KENNEN spacecraft which carried the KH-11
camera system.
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