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 28926U 05052C 13137.43238762 .00003140 00000-0 50877-3 0 8503
2 28926 049.5646 254.5048 5250322 295.5609 049.9485 05.21572975138370
| Epoch (UTC): | 17 May 2013 10:22:38 |
| Eccentricity: | 0.5250322 |
| inclination: | 49.5646° |
| perigee height: | 293 km |
| apogee height: | 15041 km |
| right ascension of ascending node: | 254.5048° |
| argument of perigee: | 295.5609° |
| revolutions per day: | 5.21572975 |
| mean anomaly at epoch: | 49.9485° |
| orbit number at epoch: | 13837 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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