|
Startdatum |
29.12.2003 |
B 1 |
10.981 GHz hor. |
D 5 |
11.606 GHz ver. |
|
Startrakete |
Proton Flug 302 |
B 2 |
10.981 GHz ver. |
D 6 |
11.606 GHz hor. |
|
Satellit |
NPO PM / Express-727M |
B 3 |
11.044 GHz hor. |
D 7 |
11.669 GHz ver. |
|
Energieleistung |
6000 W |
B 4 |
11.044 GHz ver. |
D 8 |
11.669 GHz hor. |
|
Lebensdauer |
12 Jahre |
B 5 |
11.106 GHz hor. |
A 1 |
12.531 GHz ver. |
|
Transponder |
24 Ku-Bandtransponder +
8Backup-Transponder |
B 6 |
11.106 GHz ver. |
A 2 |
12.531 GHz hor. |
|
Leistung |
jeweils 103,5 W |
B 7 |
11.169 GHz hor. |
A 3 |
12.594 GHz ver. |
|
Bandbreite |
32*54 MHz |
B 8 |
11.169 GHz ver. |
A 4 |
12.594 GHz hor. |
| EIRP |
fixed Beam Europa 50
dBW |
D 1 |
11.481 GHz ver. |
A 5 |
12.656 GHz ver. |
|
Wide-Beam Südafrika
483dBW |
D 2 |
11.481 GHz hor. |
A 6 |
12.656 GHz hor. |
|
Steerable Beam 1 52 dBW |
D 3 |
11.544 GHz ver. |
A 7 |
12.719 GHz ver. |
|
Steerable Beam 2 50 dBW |
D 4 |
11.544 GHz hor. |
A 8 |
12.719 GHz hor. |
| Eutelsat hatte Anfang
2004zwölf Transponder des Orbiters auf Lebenszeit
angemietet. |
Testbilder und Feedhunting
