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 55041U 23001AJ 24280.83934448 .00037815 00000-0 13906-2 0 9995
2 55041 97.4112 339.1898 0011415 138.2874 221.9237 15.27725680 97620
| Epoch (UTC): | 06 October 2024 20:08:39 |
| Eccentricity: | 0.0011415 |
| inclination: | 97.4112° |
| perigee height: | 475 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 339.1898° |
| argument of perigee: | 138.2874° |
| revolutions per day: | 15.27725680 |
| mean anomaly at epoch: | 221.9237° |
| orbit number at epoch: | 9762 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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