Designation | 39731 / 14024A |
Launch date | 30 Apr 2014 |
Country of origin | Kazahkstan |
Mission | Remote sensing |
Perigee/Apogee | 750 km, sun-synchronous |
Inclination | 98.5° |
Period | 100 min |
Launch vehicle | Vega VV03 |
Prime contractor | Airbus Defense and Space |
Platform | Leostar-500-XO |
Mass at launch | 830 kg |
Dry mass | |
Dimension | |
Solar array | |
Stabilization | |
DC power | |
Design lifetime | 7 years |