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 22566U 93016B 13143.12820217 .00000195 00000-0 12585-3 0 7925
2 22566 071.0093 305.8694 0012038 240.6188 119.3733 14.14781703 41076
| Epoch (UTC): | 23 May 2013 03:04:36 |
| Eccentricity: | 0.0012038 |
| inclination: | 71.0093° |
| perigee height: | 834 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 305.8694° |
| argument of perigee: | 240.6188° |
| revolutions per day: | 14.14781703 |
| mean anomaly at epoch: | 119.3733° |
| orbit number at epoch: | 4107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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