Launch Date
The satellite was launch onboard into second developmental site of ASLV. However did not reach the orbit.
Mission Experimental
Weight 150 kg
Onboard power 90 Watts
Communication S-band and VHF
Stabilization Three axis body stabilized (biased momentum) with a Momentum Wheel and Magnetic Torquer
Propulsion system Monopropellant (Hydrazine based)
Reaction Control System
Payload Gamma Ray Burst (GRB) payload and Mono Payload
Ocular Electro-Optic Stereo Scanner (MEOSS) built by DLR, Germany
Launch date July 13, 1988
Launch site SHAR Centre, Sriharikota, India
Launch vehicle Augmented Satellite Launch Vehicle (ASLV)
Orbit Not realised
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