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 41855U 16067H 24357.47957723 .00040965 00000-0 13795-2 0 9999
2 41855 98.0861 186.6113 0007698 133.1888 226.9995 15.30622123444396
| Epoch (UTC): | 22 December 2024 11:30:35 |
| Eccentricity: | 0.0007698 |
| inclination: | 98.0861° |
| perigee height: | 468 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 186.6113° |
| argument of perigee: | 133.1888° |
| revolutions per day: | 15.30622123 |
| mean anomaly at epoch: | 226.9995° |
| orbit number at epoch: | 44439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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