Gsat 16
General
| Designation | 40332 / 14078A |
| Launch date | 6 Dec 2014 |
| Country of origin | India |
| Mission | Telecommunications |
| Geostationary orbit | 55°E |
| Launch vehicle | Ariane VA221 |
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Technical data
Lyngsat transponder loading
Specifications
| Prime contractor | ISRO |
| Platform | I-3K |
| Mass at launch | 3180 kg |
| Dry mass | |
| Dimension | 3.1x1.7x2.0m |
| Solar array | 15.4m span |
| Stabilization | 3 axis |
| DC power | EOL: 5600 W |
| Design lifetime | 15 years |
C-band
| Main transponders | 24+12 (extended) |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage | India and part of Indian Ocean including Sri Lanka and Andaman and Nicobar |
| EIRP max | 37 dBW |
| G/T max | -4 dB/K |
| Polarization |
Ku-band
| Main transponders | 12 |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage | India mainland and Andaman and Nicobar |
| EIRP max | |
| G/T max | |
| Polarization |
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V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly