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 32783U 08021A 24358.44074670 .00001807 00000-0 25259-3 0 9990
2 32783 97.8422 52.3787 0012564 70.9665 289.2906 14.78762281898973
| Epoch (UTC): | 23 December 2024 10:34:40 |
| Eccentricity: | 0.0012564 |
| inclination: | 97.8422° |
| perigee height: | 624 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 52.3787° |
| argument of perigee: | 70.9665° |
| revolutions per day: | 14.78762281 |
| mean anomaly at epoch: | 289.2906° |
| orbit number at epoch: | 89897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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