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 41056U 00055P 24357.55262751 .00001610 00000-0 89762-3 0 9993
2 41056 98.5599 9.6970 0016584 222.6337 137.3549 14.12217370466997
| Epoch (UTC): | 22 December 2024 13:15:47 |
| Eccentricity: | 0.0016584 |
| inclination: | 98.5599° |
| perigee height: | 840 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 9.6970° |
| argument of perigee: | 222.6337° |
| revolutions per day: | 14.12217370 |
| mean anomaly at epoch: | 137.3549° |
| orbit number at epoch: | 46699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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