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 22784U 93055C 13142.14086222 -.00000000 00000-0 -13527-4 0 2167
2 22784 082.5488 125.6367 0020703 287.8990 122.1628 13.83368786995924
| Epoch (UTC): | 22 May 2013 03:22:50 |
| Eccentricity: | 0.0020703 |
| inclination: | 82.5488° |
| perigee height: | 937 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 125.6367° |
| argument of perigee: | 287.8990° |
| revolutions per day: | 13.83368786 |
| mean anomaly at epoch: | 122.1628° |
| orbit number at epoch: | 99592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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