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 58262U 23174G 24357.73611204 .00016285 00000-0 49137-3 0 9994
2 58262 97.4388 71.9533 0008399 286.5579 73.4741 15.34328392 62478
| Epoch (UTC): | 22 December 2024 17:40:00 |
| Eccentricity: | 0.0008399 |
| inclination: | 97.4388° |
| perigee height: | 457 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 71.9533° |
| argument of perigee: | 286.5579° |
| revolutions per day: | 15.34328392 |
| mean anomaly at epoch: | 73.4741° |
| orbit number at epoch: | 6247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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