Specifications
| Prime contractor
| TRW with KARI (Korea Aerospace Research Inst.) |
| Platform | T200B |
| Operator | KARI |
| Mass at launch | 465 kg |
| Mass in orbit | |
| Dimension | |
| Equipment | EOC, OSMI, SPS |
| Solar array | 2 deployable solar arrays |
| Stabilization | 3-axis |
| DC power | |
| Design lifetime | |
|
End of live:
| End of Operation: | 31 Jan 2008 |
| Cause: | controllers had lost contact with the satellite |
| Reentered date: | |
| Lifetime: | |
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