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.
| 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 | |
