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 24796U 97020E 13170.24838672 .00000162 00000-0 50677-4 0 4250
2 24796 086.3962 208.3090 0002346 110.7461 006.0151 14.34379619844108
| Epoch (UTC): | 19 June 2013 05:57:40 |
| Eccentricity: | 0.0002346 |
| inclination: | 86.3962° |
| perigee height: | 775 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 208.3090° |
| argument of perigee: | 110.7461° |
| revolutions per day: | 14.34379619 |
| mean anomaly at epoch: | 6.0151° |
| orbit number at epoch: | 84410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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