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 25544U 98067A 24286.17692722 .00031145 00000-0 55599-3 0 9998
2 25544 51.6377 95.9360 0009253 61.6494 298.5427 15.49732338476696
| Epoch (UTC): | 12 October 2024 04:14:46 |
| Eccentricity: | 0.0009253 |
| inclination: | 51.6377° |
| perigee height: | 411 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 95.9360° |
| argument of perigee: | 61.6494° |
| revolutions per day: | 15.49732338 |
| mean anomaly at epoch: | 298.5427° |
| orbit number at epoch: | 47669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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