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 24264.03049623 .00010782 00000-0 39745-3 0 9994
2 53807 53.2328 115.9478 0008522 37.4563 322.7031 15.28325450112724
| Epoch (UTC): | 20 September 2024 00:43:54 |
| Eccentricity: | 0.0008522 |
| inclination: | 53.2328° |
| perigee height: | 475 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 115.9478° |
| argument of perigee: | 37.4563° |
| revolutions per day: | 15.28325450 |
| mean anomaly at epoch: | 322.7031° |
| orbit number at epoch: | 11272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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