Eutelsat-2 F1 |
EUTELSAT |
Spacecraft n°: |
Eutelsat spacecraft n°: 6 |
Launch data:
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| Prime contractor | Aerospatiale |
| Platform | Spacebus-2000 |
| Operator | Eutelsat |
| Mass at launch | 1870 kg |
| Mass in orbit | 915 kg |
| Payload mass | 207.9 kg: transponders: 167.9 kg, antennas: 40 kg |
| Dimension | 2.8 x 2.2 x 2.5 m |
| Solar array | 2 deployable solar arrays, 22.4 m span |
| Stabilization | 3-axis |
| Equipment | 16 (+8) Ku-band transponders |
| DC power | BOL: 3000 W EOL: 2890 W |
| Payload power | 2090 W |
| G/T | -3.5 to +2.5 dB/K |
| Design lifetime | 10 years |
| Begin | End | Position |
| L: 30 Aug 1990 | Nov 1998 | 13°E |
| Dec 1998 | Jan 1999 | 36°E (replaces TDF 2) |
| Feb 1999 | 48°E (went inclined) |
|
Horizontal Uplink |
Horizontal Downlink | Transponder |
Vertical Downlink |
Vertical Uplink | Remarks |
| 10.971 | 20A | 14.271 | |||
| 14.286 | 25A | 10.986 | |||
| 11.005 | 20B | 14.305 | |||
| 14.316 | 25B | 11.016 | |||
| 14.349 | 26A | 11.049 | |||
| 11.055 | 21A | 14.355 | |||
| 14.380 | 26B | 11.080 | |||
| 11.095 | 21B | 14.395 | |||
| 14.433 | 27A | 11.133 | |||
| 11.146 | 22A | 14.446 | |||
| 14.463 | 27B | 11.163 | |||
| 11.181 | 22B | 14.481 | |||
| 11.554 | 32 | 14.104 | when 32 off | ||
| 14.125 | 37 | 11.575 | when 47 off | ||
| 11.595 | 33 | 14.145 | when 43 off | ||
| 14.166 | 38 | 11.616 | when 48 off | ||
| 11.638 | 34A | 14.188 | when 44 off | ||
| 14.208 | 39 | 11.658 | when 49 off | ||
| 11.675 | 34B | 14.225 | when 44 off | ||
| 12.521 | 40 | 14.021 | |||
| 14.042 | 45 | 12.542 | |||
| 12.563 | 41 | 14.062 | |||
| 14.083 | 46 | 12.583 | |||
| 12.604 | 42 | 14.104 | when 32 off | ||
| 14.125 | 47 | 12.625 | when 37 off | ||
| 12.645 | 43 | 14.145 | when 33 off | ||
| 14.166 | 48 | 12.666 | when 38 off | ||
| 12.688 | 44A | 14.188 | when 34 off | ||
| 14.208 | 49 | 12.708 | when 39 off | ||
| 12.728 | 44B | 14.228 | when 34 off |
| Ref.: #14, #15 - update: 19.11.11 | Home |