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 24340.38582964 .00021382 00000-0 12819-2 0 9990
2 32791 97.7110 311.5713 0007703 85.1201 275.0908 15.10961204902308
| Epoch (UTC): | 05 December 2024 09:15:35 |
| Eccentricity: | 0.0007703 |
| inclination: | 97.7110° |
| perigee height: | 528 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 311.5713° |
| argument of perigee: | 85.1201° |
| revolutions per day: | 15.10961204 |
| mean anomaly at epoch: | 275.0908° |
| orbit number at epoch: | 90230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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