| Mission type | Communication |
|---|---|
| Operator | ISRO |
| COSPAR ID | 2014-001A |
| SATCAT no. | 39498 |
| Mission duration | Planned: 12 years Elapsed: 10 years, 10 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[1] |
| 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)[2] |
| Apogee altitude | 35,809 kilometres (22,251 mi)[2] |
| Inclination | 0.11 degrees[2] |
| Period | 1436.12 minutes[2] |
| Epoch | 22 January 2015, 20:39:21 UTC[2] |
| 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[3] by a Geosynchronous Satellite Launch Vehicle Mk.II, which incorporated an Indian-built cryogenic engine on the third stage.
- ^ Subramanian, T. S. (22 December 2013). "GSLV-D5 to lift off on 5 January". The Hindu. India. Retrieved 24 December 2013.
- ^ a b c d e "GSAT-14 Satellite details 2014-001A NORAD 39498". N2YO. 22 January 2015. Retrieved 25 January 2015.
- ^ "ISRO successfully launches indigenous cryogenic engine-powered GSLV-D5". The Times of India. 5 January 2014. Retrieved 7 February 2014.