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 24262.47101089 .00017788 00000-0 11886-2 0 9996
2 32791 97.7002 233.3395 0005346 27.3954 332.7554 15.07033887890632
| Epoch (UTC): | 18 September 2024 11:18:15 |
| Eccentricity: | 0.0005346 |
| inclination: | 97.7002° |
| perigee height: | 541 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 233.3395° |
| argument of perigee: | 27.3954° |
| revolutions per day: | 15.07033887 |
| mean anomaly at epoch: | 332.7554° |
| orbit number at epoch: | 89063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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