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 56641U 22151AFR 24284.41905498 .00025053 00000-0 37486-2 0 9998
2 56641 98.7143 335.1042 0166134 318.0345 40.8223 14.65694672 83166
| Epoch (UTC): | 10 October 2024 10:03:26 |
| Eccentricity: | 0.0166134 |
| inclination: | 98.7143° |
| perigee height: | 557 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 335.1042° |
| argument of perigee: | 318.0345° |
| revolutions per day: | 14.65694672 |
| mean anomaly at epoch: | 40.8223° |
| orbit number at epoch: | 8316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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