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 25162.80990416 .00004739 00000-0 15753-3 0 9990
2 53807 53.2325 325.9908 0008904 111.4194 248.7760 15.33086799153298
| Epoch (UTC): | 11 June 2025 19:26:15 |
| Eccentricity: | 0.0008904 |
| inclination: | 53.2325° |
| perigee height: | 460 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 325.9908° |
| argument of perigee: | 111.4194° |
| revolutions per day: | 15.33086799 |
| mean anomaly at epoch: | 248.7760° |
| orbit number at epoch: | 15329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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