Name:INSAT-2C
LaunchDate:07.12.1995
Power of four C-band transponders increased to improve communication facilities in remote areas like Northeast and Andaman & Nicobar Islands. Coverage of two other C-band transponders is enlarged to include parts of southeast Asia, Central Asia and West Asia | ||
| Mission | Communication |
| Weight | 2106kg with propellants 946 kg dry weight |
| Onboard power | 1320 Watts |
| Communication | C extended C, S and Ku bands |
| Stabilization | Three axis stabilized with two Momen'tum Wheels & one Reaction Wheel,Magnetic torquers |
| Propulsion | Integrated bipropellan stystem ( MMH and N24) With sixteen 22N thrusters and 440N LAM. 0 |
| Payload | Transponders: 16C-band / extended C-band transponders (forFSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders |
| Launch date | December 7, 1995 |
| Launch site | French Guyana |
| Launch vehicle | Ariane4 |
| Orbit | Geostationary 93.5 deg E |
| Inclination | 0 deg. |
| Mission life | Seven years(nominal) |
| Orbit life | Very Long |
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