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 22825U 93061C 13145.46779353 .00000136 00000-0 70164-4 0 3914
2 22825 098.6167 089.7342 0008165 003.5393 109.2597 14.29563416 25386
| Epoch (UTC): | 25 May 2013 11:13:37 |
| Eccentricity: | 0.0008165 |
| inclination: | 98.6167° |
| perigee height: | 787 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 89.7342° |
| argument of perigee: | 3.5393° |
| revolutions per day: | 14.29563416 |
| mean anomaly at epoch: | 109.2597° |
| orbit number at epoch: | 2538 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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