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 13144.54987562 .00000397 00000-0 13467-3 0 1606
2 24794 086.3990 219.3648 0002450 116.8816 243.2630 14.34217574840402
| Epoch (UTC): | 24 May 2013 13:11:49 |
| Eccentricity: | 0.0002450 |
| inclination: | 86.3990° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 219.3648° |
| argument of perigee: | 116.8816° |
| revolutions per day: | 14.34217574 |
| mean anomaly at epoch: | 243.2630° |
| orbit number at epoch: | 84040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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