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 24261.93783046 .00013887 00000-0 50864-3 0 9998
2 53807 53.2347 125.6238 0008469 31.5081 328.6426 15.28285242112409
| Epoch (UTC): | 17 September 2024 22:30:28 |
| Eccentricity: | 0.0008469 |
| inclination: | 53.2347° |
| perigee height: | 475 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 125.6238° |
| argument of perigee: | 31.5081° |
| revolutions per day: | 15.28285242 |
| mean anomaly at epoch: | 328.6426° |
| orbit number at epoch: | 11240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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