Description

The Microsat is developed to observe dynamic processes in Earth’s ionosphere and run technology experiments in space to test onboard instruments and components of future spacecraft.

The Microsat is developed based on the MS-2 under the National Space Program of Ukraine.

Specifications

Mass:

Satellite, kg

Payload, kg

 

195

75

Altitude, km 668
Inclination, deg 98,1
Orbital period, minutes 98,03
Type 3-axis active
Sensors 3 axis magnetometer
Actuators Reactionwheels,
Magnetorquer
Attitude control accuracy, deg, not worse than: 5
Active life, years, not less than 3
Note: These specifications of satellite are preliminary