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 41922U 17003F 24283.64201126 .00001054 00000-0 36927-3 0 9990
2 41922 86.4013 345.6931 0001683 96.2431 263.8956 14.34221324405044
| Epoch (UTC): | 09 October 2024 15:24:29 |
| Eccentricity: | 0.0001683 |
| inclination: | 86.4013° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 345.6931° |
| argument of perigee: | 96.2431° |
| revolutions per day: | 14.34221324 |
| mean anomaly at epoch: | 263.8956° |
| orbit number at epoch: | 40504 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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