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 22782U 93055A 13139.12246516 .00000026 00000-0 10675-4 0 7424
2 22782 082.5478 125.9828 0020987 291.3974 114.3686 13.83704787995621
| Epoch (UTC): | 19 May 2013 02:56:20 |
| Eccentricity: | 0.0020987 |
| inclination: | 82.5478° |
| perigee height: | 935 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 125.9828° |
| argument of perigee: | 291.3974° |
| revolutions per day: | 13.83704787 |
| mean anomaly at epoch: | 114.3686° |
| orbit number at epoch: | 99562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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