Designation | n/a |
Launch date | destroyed on launch pad on 1 Sep 2016 |
Country of origin | Israel |
Mission | Telecommunications |
Geostationary orbit | 4°W |
Launch vehicle | Falcon 9 |
Launch site | Cape Canaveral |
Prime contractor | IAI |
Platform | Amos-4000 |
Mass at launch | 5400 kg |
Dry mass | |
Dimension | |
Solar array | (ATK built) |
Stabilization | |
DC power | 10 kW |
Design lifetime | 16 years |
Main transponders | 39 |
Backup transponders | |
Power | |
Bandwidth | |
Coverage |
3
beams: Middle-East Central-East Europe Pan-Europe |
EIRP max | |
G/T max | |
Polarization |
Main transponders | 24 |
Backup transponders | |
Power | |
Bandwidth | |
Coverage | Sub-Sahara Africa and part of Europe |
EIRP max | |
Polarization | |
Frequencies |
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