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 25166.78650605 .00005239 00000-0 17260-3 0 9995
2 53807 53.2335 307.4696 0008656 121.5072 238.6777 15.33148503153905
| Epoch (UTC): | 15 June 2025 18:52:34 |
| Eccentricity: | 0.0008656 |
| inclination: | 53.2335° |
| perigee height: | 460 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 307.4696° |
| argument of perigee: | 121.5072° |
| revolutions per day: | 15.33148503 |
| mean anomaly at epoch: | 238.6777° |
| orbit number at epoch: | 15390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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