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 32791U 08021J 24280.65936851 .00031073 00000-0 20217-2 0 9990
2 32791 97.7041 251.5484 0002305 322.5889 37.5178 15.07905291893378
| Epoch (UTC): | 06 October 2024 15:49:29 |
| Eccentricity: | 0.0002305 |
| inclination: | 97.7041° |
| perigee height: | 541 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 251.5484° |
| argument of perigee: | 322.5889° |
| revolutions per day: | 15.07905291 |
| mean anomaly at epoch: | 37.5178° |
| orbit number at epoch: | 89337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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