Launch data:
| Designation | 42901 / 17044B |
| Launch date | 02 Aug 2017 - 01:58 UT |
| Launch site | Ko, ELV |
| Launch vehicle | Vega |
| Mission | Earth observation |
| Earth orbit: | |
| Perigee / Apogee | 720 x 724 km |
| Eccentricity | |
| Inclination | 98.4° |
| Period | min |
VENμS |
Israel, France |
Int. spacecraft nº: |
Israel spacecraft nº: 26 |
Launch data:
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| Prime manufacturer | IAI, Rafael |
| Platform | TECSAR Bus |
| Operator | IAI, CNES |
| Mass at launch | 264 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | 2 deployable fixed solar arrays |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | 4.5 yrs |
| Ref.: #7(JR740), #14 - update: 16.01.18 | Home |