ECS 2 --> Eutelsat 1F2 |
ESA / EUTELSAT |
Spacecraft n°: |
EUTELSAT spacecraft n°: 2 |
Launch data:
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| Prime contractor | British Aerospace |
| Platform | ECS-Bus |
| Operator | ESA / Eutelsat |
| Mass at launch | 1175 kg |
| Mass (in geostationary orbit) | 700 kg |
| Dimensions: | |
| Height: | 2.4 m |
| Diameter: | 2.2 m |
| Overall width (with solar arrays extended): | 13.8 m |
| Solar array | 2 deployable solar arrays, span 13.8 m |
| Equipment | 12 (+2) Ku-band transponders |
| Stabilization | three-axis |
| Propulsion | Mage-2 |
| Electrical power: | |
| At beginning of live: | 1 000 W |
| At end of live: | 800 W |
| Design lifetime | 7 y |
| Begin | End | Position |
| L: 4 Aug 1984 | Sep 1990 | 7°E |
| late-1990 | Feb 1992 | 4°E |
| late-1992 | late-1992 | 2°E |
| Jun 1993 | Dec 1993 | 1°E |
| Out of service | December 1993 |
| Cause |
End
of life, moved to the junk orbit Broadcast 634,969 hours |
![]() Launch cancel Kourou |
![]() Headquarter cancel Paris. Credit: #411 |
| Ref.: #14, #66, #411 - update: 17.11.19 | Home |