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 is defined by the following mean orbital elements,
1 25017U 97064A 11297.46889870 0.00000000 00000-0 00000-0 0 04
2 25017 56.9997 314.9237 0005000 211.7296 148.2704 14.71646799 04
| Epoch (UTC): | 24 October 2011 11:15:12 |
| Eccentricity: | 0.0005000 |
| inclination: | 56.9997° |
| perigee height: | 652 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 314.9237° |
| argument of perigee: | 211.7296° |
| revolutions per day: | 14.71646799 |
| mean anomaly at epoch: | 148.2704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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