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 20624U 90046A 13144.40667862 .00000149 00000-0 10320-3 0 6546
2 20624 071.0406 081.8366 0013652 137.2758 353.4746 14.13991159187298
| Epoch (UTC): | 24 May 2013 09:45:37 |
| Eccentricity: | 0.0013652 |
| inclination: | 71.0406° |
| perigee height: | 836 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 81.8366° |
| argument of perigee: | 137.2758° |
| revolutions per day: | 14.13991159 |
| mean anomaly at epoch: | 353.4746° |
| orbit number at epoch: | 18729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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