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 54024U 22127B 23340.52556642 .00003079 00000-0 39062-3 0 9998
2 54024 98.2881 354.9493 0134417 109.0817 252.5003 14.76277395 62585
| Epoch (UTC): | 06 December 2023 12:36:48 |
| Eccentricity: | 0.0134417 |
| inclination: | 98.2881° |
| perigee height: | 547 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 354.9493° |
| argument of perigee: | 109.0817° |
| revolutions per day: | 14.76277395 |
| mean anomaly at epoch: | 252.5003° |
| orbit number at epoch: | 6258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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