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 25114.68815329 .00011588 00000-0 37675-3 0 9999
2 53807 53.2318 190.0071 0006945 335.3869 24.6801 15.32354899145916
| Epoch (UTC): | 24 April 2025 16:30:56 |
| Eccentricity: | 0.0006945 |
| inclination: | 53.2318° |
| perigee height: | 464 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 190.0071° |
| argument of perigee: | 335.3869° |
| revolutions per day: | 15.32354899 |
| mean anomaly at epoch: | 24.6801° |
| orbit number at epoch: | 14591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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