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 24797U 97020F 13137.85365274 .00000497 00000-0 10477-3 0 3808
2 24797 086.8987 178.9697 0227825 244.9743 173.0729 14.42536367842827
| Epoch (UTC): | 17 May 2013 20:29:15 |
| Eccentricity: | 0.0227825 |
| inclination: | 86.8987° |
| perigee height: | 588 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 178.9697° |
| argument of perigee: | 244.9743° |
| revolutions per day: | 14.42536367 |
| mean anomaly at epoch: | 173.0729° |
| orbit number at epoch: | 84282 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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