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 53496C 22099AH 24358.51159722 .00018781 00000+0 14655-2 0 3589
2 53496 97.6541 116.6366 0000984 279.4545 72.8930 15.01230198 17
| Epoch (UTC): | 23 December 2024 12:16:42 |
| Eccentricity: | 0.0000984 |
| inclination: | 97.6541° |
| perigee height: | 562 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 116.6366° |
| argument of perigee: | 279.4545° |
| revolutions per day: | 15.01230198 |
| mean anomaly at epoch: | 72.8930° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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