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 20480U 90013C 16269.06843769 -.00000028 00000-0 17805-4 0 9990
2 20480 99.0218 86.3242 0539397 271.8256 207.4574 12.83412401247713
| Epoch (UTC): | 25 September 2016 01:38:33 |
| Eccentricity: | 0.0539397 |
| inclination: | 99.0218° |
| perigee height: | 912 km |
| apogee height: | 1743 km |
| right ascension of ascending node: | 86.3242° |
| argument of perigee: | 271.8256° |
| revolutions per day: | 12.83412401 |
| mean anomaly at epoch: | 207.4574° |
| orbit number at epoch: | 24771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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