Designation | 29079 / 06014A |
Launch date | 25 Apr 2006 |
Country of origin | Israel |
Mission | Remote sensing |
Perigee/Apogee | 500 km, sun-synchronous |
Inclination | 97.33° |
Period | 95 min |
Launch vehicle | Start #7 |
Prime contractor | IAI |
Platform | |
Mass at launch | 290 kg |
Mass in orbit | |
Dimension | |
Solar array | |
Stabilization | |
DC power | 800 W |
Design lifetime | 10 years |