Designation | 27434 / 02025A |
Launch date | 28 May 2002 |
Country of origin | Israel |
Mission | Military: reconnaissance |
Perigee/Apogee | 480 km? |
Inclination | 143.5° |
Period | |
Launch vehicle | Shavit #6 |
Launch site | Palmahim |
Decay | 21 Feb 2024 |
Prime contractor | IAI |
Platform | |
Mass at launch | 300 kg |
Mass in orbit | |
Dimension | 2.3 m x 1.2 m diameter |
Solar array | |
Stabilization | |
DC power | |
Design lifetime | 4 years |