| Orbit |
Geostationary
(55 deg East longitude) |
| Dry
Mass |
1181
kg |
| Lift-Off
Mass |
2750
kg |
| Size |
Cuboid
of dimensions 2.0 m x 1.77 m x 2.8 m with solar arrays on north
and south sides |
| Length
when fully deployed |
15.445
m (North-South) |
| Spacecraft
Propulsion and Control |
440
N Liquid Apogee Motor with MON-3 (Mixed Oxides of Nitrogen)
and MMH (Mono Methyl Hydrazine) for orbit raising.
3-axis body stabilised in orbit using sensors, momentum and
reaction wheels, magnetictorquers and eight 10 Newton &
eight 22 Newton Reaction Control Thrusters |
| Power |
Solar
array generating 2400 W. Two 70 Ah Nickel-Hydrogen batteries
to support full payload operation during eclipse period |
| Mission
life |
12
years |
