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 24968U 97056D 13139.34260534 .00000448 00000-0 15272-3 0 3316
2 24968 086.3996 221.5203 0002316 109.5295 250.6151 14.34220158818995
| Epoch (UTC): | 19 May 2013 08:13:21 |
| Eccentricity: | 0.0002316 |
| inclination: | 86.3996° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 221.5203° |
| argument of perigee: | 109.5295° |
| revolutions per day: | 14.34220158 |
| mean anomaly at epoch: | 250.6151° |
| orbit number at epoch: | 81899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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