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 54572U 22151LY 24280.99407229 .00074091 00000-0 14396-1 0 9997
2 54572 98.6756 311.9574 0093448 25.0534 335.5157 14.59970971 99664
| Epoch (UTC): | 06 October 2024 23:51:27 |
| Eccentricity: | 0.0093448 |
| inclination: | 98.6756° |
| perigee height: | 627 km |
| apogee height: | 759 km |
| right ascension of ascending node: | 311.9574° |
| argument of perigee: | 25.0534° |
| revolutions per day: | 14.59970971 |
| mean anomaly at epoch: | 335.5157° |
| orbit number at epoch: | 9966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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