Designation | 35682 / 09041B |
Launch date | 29 Jul 2009 |
Country of origin | United Arab Emirates |
Mission | Remote sensing |
Perigee/Apogee | 680 km (sun-synchronous) |
Inclination | |
Period | |
Launch vehicle | Dnepr #13 |
Prime contractor | SaTReC |
Platform | |
Mass at launch | 190 kg |
Dry mass | |
Dimension | |
Solar array | |
Stabilization | |
DC power | |
Design lifetime | 5 years |