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 20885U 90081AV 23342.72482095 .00000159 00000-0 15861-3 0 9991
2 20885 98.8320 0.4737 0066504 328.6078 97.6652 13.90550163682050
| Epoch (UTC): | 08 December 2023 17:23:44 |
| Eccentricity: | 0.0066504 |
| inclination: | 98.8320° |
| perigee height: | 878 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 0.4737° |
| argument of perigee: | 328.6078° |
| revolutions per day: | 13.90550163 |
| mean anomaly at epoch: | 97.6652° |
| orbit number at epoch: | 68205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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