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 20805U 90083B 23028.37572090 .00000134 00000-0 12134-3 0 9995
2 20805 82.9391 337.8946 0032002 64.6264 47.8996 13.75998991625191
| Epoch (UTC): | 28 January 2023 09:01:02 |
| Eccentricity: | 0.0032002 |
| inclination: | 82.9391° |
| perigee height: | 954 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 337.8946° |
| argument of perigee: | 64.6264° |
| revolutions per day: | 13.75998991 |
| mean anomaly at epoch: | 47.8996° |
| orbit number at epoch: | 62519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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