GSAT-14
| Mission type | Communication |
|---|---|
| Operator | ISRO |
| COSPAR ID | 2014-001A |
| SATCAT no. | 39498 |
| Mission duration | Planned: 12 years Elapsed: 11 years, 5 months, 12 days |
| Spacecraft properties | |
| Bus | I-2K |
| Manufacturer | ISRO Satellite Centre Space Applications Centre |
| Launch mass | 1,982 kilograms (4,370 lb) |
| Dry mass | 851 kilograms (1,876 lb) |
| Power | 2,600 watts |
| Start of mission | |
| Launch date | 5 January 2014, 10:48 UTC |
| Rocket | GSLV Mk.II D5 |
| Launch site | Satish Dhawan SLP |
| Contractor | ISRO |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Geostationary |
| Longitude | 74° East |
| Perigee altitude | 35,776 kilometres (22,230 mi) |
| Apogee altitude | 35,809 kilometres (22,251 mi) |
| Inclination | 0.11 degrees |
| Period | 1436.12 minutes |
| Epoch | 22 January 2015, 20:39:21 UTC |
| Transponders | |
| Band | 6 Ku band 6 ext. C band 2 Ka band |
| Coverage area | India |
GSAT-14 is an Indian communications satellite launched in January 2014. It replaced the GSAT-3 satellite, which was launched in 2004. GSAT-14 was launched by a Geosynchronous Satellite Launch Vehicle Mk.II, which incorporated an Indian-built cryogenic engine on the third stage.