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 53807U 22111AL 24285.54101053 .00031489 00000-0 11076-2 0 9992
2 53807 53.2355 16.4464 0008966 87.5543 272.6485 15.29069014116014
| Epoch (UTC): | 11 October 2024 12:59:03 |
| Eccentricity: | 0.0008966 |
| inclination: | 53.2355° |
| perigee height: | 472 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 16.4464° |
| argument of perigee: | 87.5543° |
| revolutions per day: | 15.29069014 |
| mean anomaly at epoch: | 272.6485° |
| orbit number at epoch: | 11601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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