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 24255.00533853 .00017537 00000-0 64295-3 0 9997
2 53807 53.2353 157.6687 0007886 11.8688 348.2497 15.28068793111343
| Epoch (UTC): | 11 September 2024 00:07:41 |
| Eccentricity: | 0.0007886 |
| inclination: | 53.2353° |
| perigee height: | 476 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 157.6687° |
| argument of perigee: | 11.8688° |
| revolutions per day: | 15.28068793 |
| mean anomaly at epoch: | 348.2497° |
| orbit number at epoch: | 11134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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