French agency. Starsem SA, Paris, France.
Location: Paris.
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Starsem Chronology
2000 February 8 - .
23:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511U.
LV Configuration: Soyuz 11A511U A15000-079 / Ikar ST07.
- Dummy satellite - .
Nation: Russia. Agency: Starsem. Manufacturer: Lavochkin. Class: Technology. Type: Navigation technology satellite. USAF Sat Cat: 26086 . COSPAR: 2000-009A. Apogee: 613 km (381 mi). Perigee: 580 km (361 mi). Inclination: 64.8545 deg. Period: 96.53 min. Summary: .
2000 March 20 - .
18:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz 11A511U.
LV Configuration: Soyuz 11A511U/Fregat - ST08.
- Dumsat - .
Mass: 2,382 kg (5,251 lb). Nation: Europe. Agency: Starsem. Manufacturer: Toulouse. Class: Technology. Type: Navigation technology satellite. USAF Sat Cat: 26106 . COSPAR: 2000-015A. Apogee: 17,687 km (10,990 mi). Perigee: 332 km (206 mi). Inclination: 64.7000 deg. Period: 316.60 min. Summary: Cluster 2 Composite Mock-Up validation flight. Mass model of a pair of Cluster II scientific satellites built by Aerospatiale Matra. Second test launch of the Soyuz-Fregat launch vehicle..
2003 December 27 - .
21:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz FG.
LV Configuration: Soyuz-FG/Fregat D15000-008 084/ST12.
- Amos-2 - .
Nation: Israel. Agency: Starsem. Program: Amos. Class: Communications. Type: Military communications satellite. Spacecraft: Amos. USAF Sat Cat: 28132 . COSPAR: 2003-059A. Apogee: 35,795 km (22,241 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0600 deg. Period: 1,436.14 min. Summary: Intermediate orbit shown. Fregat stage later placed Amos-2 in geostationary orbit. As of 2007 Mar 9 located at 4.00W drifting at 0.003W degrees per day..
2007 December 14 - .
13:17 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz FG.
LV Configuration: Soyuz-FG/Fregat Ts15000-025.
- Radarsat-2 - .
Mass: 2,200 kg (4,800 lb). Nation: Canada. Agency: Starsem. Class: Surveillance. Type: Civilian surveillance radar satellite. Spacecraft: Radarsat. USAF Sat Cat: 32382 . COSPAR: 2007-061A. Apogee: 793 km (492 mi). Perigee: 791 km (491 mi). Inclination: 98.6000 deg. Period: 100.70 min. Follow-on to Canadian Radarsat-1 launched in 1995. Designed to provide C-band synthetic aperture radar mapping with resolution of 3 m to Canadian government users. Compared to the earlier model had greater resolution, vastly increased on-board data storage capacity, and capability to scan left or right of ground track. Planned lifetime of seven years.
2008 April 26 - .
22:16 GMT - .
Launch Site:
Baikonur.
LV Family:
R-7.
Launch Vehicle:
Soyuz FG.
LV Configuration: Soyuz-FG/Fregat.
- GIOVE B - .
Mass: 530 kg (1,160 lb). Nation: Europe. Agency: Starsem. Class: Navigation. Type: Navigation satellite. Spacecraft: Galileo Navsat. USAF Sat Cat: 32781 . COSPAR: 2008-020A. Apogee: 23,244 km (14,443 mi). Perigee: 23,104 km (14,356 mi). Inclination: 56.0000 deg. Period: 842.60 min. Second European Galileo navigation system test satellite. The booster placed the Giove/Fregat stack on a suborbital trajectory. The Fregat stage then burned to enter a a 170 km parking orbit. The stage burned at least twice more before releasing the satellite into its operational orbit.
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