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Spacecraft design
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Lockheed Martin A2100AX
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Orbital location
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105o W.L.
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| Launch Date / Vehicle |
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15 October 2004; Proton M/Breeze M |
| Design Life |
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15 years
|
| Ku-band payload |
|
24 x 36 MHz |
| Amp type |
|
Linearized TWTA; 140 watts |
| Amp Redundancy |
|
two groups of 18 for 12 |
| Receiver redundancy |
|
4 for 2 |
| Coverage |
|
CONUS, Alaska, Hawaii |
| Beacon |
|
11702.0 MHz (H) 12198.0 MHz (V)
|
| Ka-band payload |
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12 spot beams @ 125MHz (3 x 39 MHz subchannels) |
| Amp type |
|
LTWTA, 75 watts |
| Amp Redundancy |
|
two groups of 9 for 6 |
| Receiver Redundancy |
|
two groups of 2 for 1 two groups of 7 for 5 |
| Coverage |
|
CONUS, Alaska, Hawaii |
| Beacon |
|
18582.0 MHz (RHCP) |
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