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 24794U 97020C 13140.29400156 .00000412 00000-0 14004-3 0 1553
2 24794 086.3995 221.1411 0002394 117.1548 242.9892 14.34220446839797
| Epoch (UTC): | 20 May 2013 07:03:21 |
| Eccentricity: | 0.0002394 |
| inclination: | 86.3995° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 221.1411° |
| argument of perigee: | 117.1548° |
| revolutions per day: | 14.34220446 |
| mean anomaly at epoch: | 242.9892° |
| orbit number at epoch: | 83979 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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