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 25724U 99023A 13074.07874389 0.00000060 00000-0 74783-3 0 05
2 25724 28.2395 46.5224 2135416 1.5415 358.4580 9.37439698 03
| Epoch (UTC): | 15 March 2013 01:53:23 |
| Eccentricity: | 0.2135416 |
| inclination: | 28.2395° |
| perigee height: | 1094 km |
| apogee height: | 5152 km |
| right ascension of ascending node: | 46.5224° |
| argument of perigee: | 1.5415° |
| revolutions per day: | 9.37439698 |
| mean anomaly at epoch: | 358.4580° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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