MIMOSA
1. Launching State
- The Czech Republic together with the Russian Federation
2. An appropriate designator of the space object or its registration number
- MIMOSA, 2003 – 031B
3. Date and territory or location of launch
- June 30, 2003, The Russian Federation
4. Basic orbit parameters:
a) Nodal period
- 96.31 min
b) Inclination
- 96.82 degrees
c) Apogee
- 848 km
d) Perigee
- 319 km
5. General function of space object:
- The MIMOSA spacecraft is designed for the very precise measurement of atmospheric drag and other forces of non-gravitational origin.