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 24906U 97043D 13138.48364823 .00000217 00000-0 70431-4 0 3845
2 24906 086.3966 158.4715 0002379 108.1147 041.3084 14.34213819824162
| Epoch (UTC): | 18 May 2013 11:36:27 |
| Eccentricity: | 0.0002379 |
| inclination: | 86.3966° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 158.4715° |
| argument of perigee: | 108.1147° |
| revolutions per day: | 14.34213819 |
| mean anomaly at epoch: | 41.3084° |
| orbit number at epoch: | 82416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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