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 29517U 06048B 13145.43586448 .00062225 19900-6 12331-2 0 8328
2 29517 028.4543 260.4073 5662976 031.5510 007.7965 04.65783065 80590
| Epoch (UTC): | 25 May 2013 10:27:38 |
| Eccentricity: | 0.5662976 |
| inclination: | 28.4543° |
| perigee height: | 190 km |
| apogee height: | 17344 km |
| right ascension of ascending node: | 260.4073° |
| argument of perigee: | 31.5510° |
| revolutions per day: | 4.65783065 |
| mean anomaly at epoch: | 7.7965° |
| orbit number at epoch: | 8059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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