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 20625U 90046B 13143.78778500 .00000273 00000-0 16680-3 0 4450
2 20625 071.0008 026.4073 0015104 211.0640 181.7824 14.14475903187780
| Epoch (UTC): | 23 May 2013 18:54:24 |
| Eccentricity: | 0.0015104 |
| inclination: | 71.0008° |
| perigee height: | 833 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 26.4073° |
| argument of perigee: | 211.0640° |
| revolutions per day: | 14.14475903 |
| mean anomaly at epoch: | 181.7824° |
| orbit number at epoch: | 18778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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