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 59124U 24043AC 25341.25824261 .00008481 00000-0 32690-3 0 9993
2 59124 97.5367 110.3178 0010869 196.8298 163.2581 15.26531721 97687
| Epoch (UTC): | 07 December 2025 06:11:52 |
| Eccentricity: | 0.0010869 |
| inclination: | 97.5367° |
| perigee height: | 479 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 110.3178° |
| argument of perigee: | 196.8298° |
| revolutions per day: | 15.26531721 |
| mean anomaly at epoch: | 163.2581° |
| orbit number at epoch: | 9768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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