View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 28931U 06002A 13138.54161676 .00001030 00000-0 22218-3 0 1458
2 28931 098.0323 204.3881 0001277 044.7742 315.3567 14.60390256389715
| Epoch (UTC): | 18 May 2013 12:59:55 |
| Eccentricity: | 0.0001277 |
| inclination: | 98.0323° |
| perigee height: | 691 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 204.3881° |
| argument of perigee: | 44.7742° |
| revolutions per day: | 14.60390256 |
| mean anomaly at epoch: | 315.3567° |
| orbit number at epoch: | 38971 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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