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GSat 10 [ISRO]
GSAT-10 is a 3-axis body stabilized geostationary satellite based on ISROs I-3K (I-3000) bus to provide communication services/augment the existing services. It carries 12 Normal C-band, 6 Extended C-band, 12 Ku-band transponders along with GAGAN (GPS Aided Geo Augmented Navigation) payload. The lift-off mass of the satellite is 3400 kg and it generates 6.0 kW of Power. The satellite will be located at 83šE and will have a minimum operational life of 15 years.
The satellite was launched on board Ariane-5ECA in September 2012.
| Nation: | India |
|---|---|
| Type / Application: | Communication |
| Operator: | Insat |
| Contractors: | ISRO |
| Equipment: | 12 Normal C-band, 6 Extended C-band and 12 Ku-band transponders, GAGAN |
| Configuration: | I-3K (I-3000) Bus |
| Propulsion: | LAM |
| Power: | 2 deployable solar arrays, batteries |
| Lifetime: | 15 years |
| Mass: | 3435 kg |
| Orbit: | GEO |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| GSat 10 | 2012-051B | 28.09.2012 | Ko ELA-3 | Ariane-5ECA | with 2F |
Launch Sites:
- Ko = Centre Spatial Guyanais (CSG), Kourou, French Guiana, France
References:
- ISRO: GSAT-10
Further GSat missions:
- GSat 1 [I-2K]
- GSat 2 [I-2K]
- GSat 3 (EduSat) [I-2K]
- GSat 4 (HealthSat) [I-2K]
- GSat 5 [I-2K]
- GSat 5P [I-2K]
- GSat 6, 6A [I-2K]
- GSat 7 [I-2K]
- GSat 7A [I-2K]
- GSat 7R (CMS 03) [I-4K Bus]
- GSat 8 [I-3K]
- GSat 9 (South Asian Satellite) [I-2K]
- GSat 10 [I-3K]
- GSat 11 [I-6K]
- GSat 12, 12R (CMS 01) [I-1K]
- GSat 14 [I-2K]
- GSat 15 [I-3K]
- GSat 16 [I-3K]
- GSat 17 [I-3K]
- GSat 18 [I-3K]
- GSat 19 [I-3K]
- GSat 20 (GSat N2) [I-4K]
- GSat 22 [I-3K]
- GSat 23 [I-3K]
- GSat 24 (GSat N1, CMS 02) [I-3K]
- GSat 29 [I-3K]
- GSat 30 [I-3K]
- GSat 31 [I-2K]
- GSat 32 (GSat N3) [I-8K]
