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 40500U 95015CP 24279.07535940 .00074818 00000-0 21612-1 0 9997
2 40500 98.7952 320.9941 0018647 251.6882 108.2279 14.43997724495420
| Epoch (UTC): | 05 October 2024 01:48:31 |
| Eccentricity: | 0.0018647 |
| inclination: | 98.7952° |
| perigee height: | 732 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 320.9941° |
| argument of perigee: | 251.6882° |
| revolutions per day: | 14.43997724 |
| mean anomaly at epoch: | 108.2279° |
| orbit number at epoch: | 49542 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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