Specifications
| Prime contractor | Ball Aerospace/TRW/Raytheon |
| Operator | US Department of Energy/Office of Nonproliferation and National Security |
| Mass at launch | 587 kg |
| Mass in orbit | |
| Basic shape | Box + 4 panels |
| Dimension | |
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Solar
array
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Stabilization
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| DC power | 575 W |
| Design lifetime | 3 yrs |
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End of live:
| End of Operation: | Feb 2011 |
| Cause: | |
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