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 20963U 90097B 18244.64449516 0.00000000 00000-0 00000-0 0 06
2 20963 16.5470 359.4689 0014013 222.2525 137.6515 0.98582466 04
| Epoch (UTC): | 01 September 2018 15:28:04 |
| Eccentricity: | 0.0014013 |
| inclination: | 16.5470° |
| perigee height: | 36207 km |
| apogee height: | 36326 km |
| right ascension of ascending node: | 359.4689° |
| argument of perigee: | 222.2525° |
| revolutions per day: | 0.98582466 |
| mean anomaly at epoch: | 137.6515° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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