|Units or mass||9 kg|
|Status||not launched, expected in 2025|
|Organisation||College of Engineering, Pune|
|Entity||Academic / Education|
Custom nanosatelltie with solar sail to raise orbit and measure charged particles.
Solar sailing low earth orbit nanosatellite COEPSAT-2. It aims to demonstrate orbit raising from 700 km. to 1200 km. by using a solar sail. The scientific objective of this satellite is to measure energy of the charged particles in space. The proposed satellite is of dimensions 0.16 m X 0.16 m X 0.28 m and weighs around 9 kg
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|Keywords||De-orbit device, Solar sail|