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 25040U 97069B 13140.46560387 .00000301 00000-0 10056-3 0 3229
2 25040 086.3955 284.1436 0002456 112.5534 279.7296 14.34219124812931
| Epoch (UTC): | 20 May 2013 11:10:28 |
| Eccentricity: | 0.0002456 |
| inclination: | 86.3955° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 284.1436° |
| argument of perigee: | 112.5534° |
| revolutions per day: | 14.34219124 |
| mean anomaly at epoch: | 279.7296° |
| orbit number at epoch: | 81293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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