First Spacecraft successfully orbited onboard the second
developmental flight of PSLV.
Mission completed during 1997 after serving for 3 years.
Mission
Operational Remote Sensing
Weight
804 kg
onboard power
510 Watts
Communication
S-band, X-band
Stabilization
Three axis body stabilized with 4 Reaction Wheels,
Magnetic torquers
RCS
4 tanks containing Monopropellant Hydrazine
based with sixteen 1 N thrusters and one 11 N
thruster
Payload
Two solid state Push Broom Cameras operating in
four spectral bands in the visible and near-IR range
using CCD arrays: LlSS-2A & LlSS-2B
(Resolution: 32.74 metre)
