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Spacecraft design
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Lockheed Martin A2100
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Orbital location
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103o W.L.
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| Launch Date / Vehicle |
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8 Sept. 96 / Atlas IIA |
| Design Life |
|
15 years |
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| C-band payload |
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24 x 36 MHz |
| Amp type |
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SSPA, 12 to 18 watt adjustable |
| Amp Redundancy |
|
16 for 12 |
| Receiver redundancy |
|
4 for 2 |
| Coverage |
|
50 State, Mexico, Caribbean, Canada |
| Beacon |
|
3700.5 MHz (V) 4199.5 MHz (H) |
|
|
Typical C-band footprint and frequency plan |
|
| Ku-band payload |
|
24 x 36 MHz |
| Amp type |
|
TWTA, 60 watt |
| Amp Redundancy |
|
18 for 12 |
| Receiver redundancy |
|
4 for 2 |
| Coverage |
|
50 State, Southern Canada, Northern Mexico |
| Polarization Offset |
|
26.0o CCW (viewed from the earth) |
| Beacon |
|
12198 MHz |
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Typical Ku-band footprint and frequency plan
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PDF of AMC-1 specifications and footprints |