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 41665U 00055PE 24279.74014968 .00005264 00000-0 31104-2 0 9993
2 41665 98.6275 283.1902 0041797 151.2721 209.0764 14.07703166433961
| Epoch (UTC): | 05 October 2024 17:45:48 |
| Eccentricity: | 0.0041797 |
| inclination: | 98.6275° |
| perigee height: | 837 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 283.1902° |
| argument of perigee: | 151.2721° |
| revolutions per day: | 14.07703166 |
| mean anomaly at epoch: | 209.0764° |
| orbit number at epoch: | 43396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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