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 31920U 99025CLX 24357.85004075 .00078411 00000-0 18266-2 0 9996
2 31920 98.7693 311.6284 0067364 149.1614 211.3612 15.39588081947763
| Epoch (UTC): | 22 December 2024 20:24:03 |
| Eccentricity: | 0.0067364 |
| inclination: | 98.7693° |
| perigee height: | 401 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 311.6284° |
| argument of perigee: | 149.1614° |
| revolutions per day: | 15.39588081 |
| mean anomaly at epoch: | 211.3612° |
| orbit number at epoch: | 94776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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