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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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