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 52157U 22033A 24358.20678538 .00005885 00000-0 80051-3 0 9994
2 52157 97.8838 76.7900 0004742 238.3577 121.7172 14.79132783147363
| Epoch (UTC): | 23 December 2024 04:57:46 |
| Eccentricity: | 0.0004742 |
| inclination: | 97.8838° |
| perigee height: | 629 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 76.7900° |
| argument of perigee: | 238.3577° |
| revolutions per day: | 14.79132783 |
| mean anomaly at epoch: | 121.7172° |
| orbit number at epoch: | 14736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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