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 17642U 81053LM 24357.87710888 .00007671 00000-0 25688-2 0 9997
2 17642 82.8639 203.2913 0036666 350.4333 9.6155 14.36866249 58879
| Epoch (UTC): | 22 December 2024 21:03:02 |
| Eccentricity: | 0.0036666 |
| inclination: | 82.8639° |
| perigee height: | 742 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 203.2913° |
| argument of perigee: | 350.4333° |
| revolutions per day: | 14.36866249 |
| mean anomaly at epoch: | 9.6155° |
| orbit number at epoch: | 5887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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