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 13141.27075896 .00000393 00000-0 13317-3 0 1566
2 24794 086.3994 220.7334 0002412 117.0878 243.0564 14.34221049839935
| Epoch (UTC): | 21 May 2013 06:29:53 |
| Eccentricity: | 0.0002412 |
| inclination: | 86.3994° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 220.7334° |
| argument of perigee: | 117.0878° |
| revolutions per day: | 14.34221049 |
| mean anomaly at epoch: | 243.0564° |
| orbit number at epoch: | 83993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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