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 20855U 90081T 23331.93609807 .00000118 00000-0 92854-4 0 9994
2 20855 98.7372 321.0674 0022989 247.5431 165.6429 14.08851282708026
| Epoch (UTC): | 27 November 2023 22:27:58 |
| Eccentricity: | 0.0022989 |
| inclination: | 98.7372° |
| perigee height: | 846 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 321.0674° |
| argument of perigee: | 247.5431° |
| revolutions per day: | 14.08851282 |
| mean anomaly at epoch: | 165.6429° |
| orbit number at epoch: | 70802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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