Organization | Academy of Sciences of the Czech Republic |
---|---|
Contractor | Space Devices |
Mission Type | Astronomy |
Launch | June 30, 2003 on Rockot |
Launch site | Plesetsk Cosmodrome |
Mission duration | 18 months (calculated) |
Mass | 66 kg |
Webpage | www.asu.cas.cz/english/new/MIMOSA/ |
Orbital elements | |
Semi-major axis | 6948.57 km |
Eccentricity | 0.036 |
Inclination | 96.80° |
Orbital Period | 96.07 minutes |
Right ascension of the ascending node | 60° |
Argument of perigee | |
Instruments | |
Accelerometer | 3-axis micro-accelerometer for measuring non-gravitational forces, accurate to about 10−11 ms−2 |
MIMOSA (Micromeasurements of Satellite Acceleration) is a Czech scientific microsatellite. The satellite is nearly spherical with 28 sides and carries a microaccelerometer to monitor the atmospheric density profile by sensing the atmospheric drag on the approximated sphere. It has a fairly eccentric orbit, with an initial perigee of 320 km and apogee of 845 km.
MIMOSA is no longer in orbit. NORAD reported it burnt into the atmosphere on 11-Dec-2011.
MIMOSA was launched alongside other miniature satellites including MOST and several CubeSat-based satellites. Unfortunatelly the satellite never became fully functional due to the several technical problems on board.