Designation | 33506 / 09004A |
Launch date | 2 Feb 2009 |
Country of origin | Iran |
Mission | Technology |
Perigee/Apogee | 245/378 km |
Inclination | 55.6° |
Period | |
Launch vehicle | Safir #2 |
Launch site | Semnan |
Out of service | 19 Mar 2009 |
Cause | Normal EOL |
Decay | 24 April 2009 |
Prime contractor | |
Platform | |
Mass at launch | 25 or 27 kg |
Dry mass | |
Dimension | 0.4m cube |
Solar array | none |
Stabilization | none |
DC power | battery only |
Design lifetime | 3 months |