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 41256U 00055FG 24355.39078152 .00015747 00000-0 47790-2 0 9995
2 41256 99.1012 209.4548 0019830 337.7627 22.2699 14.42143339465357
| Epoch (UTC): | 20 December 2024 09:22:43 |
| Eccentricity: | 0.0019830 |
| inclination: | 99.1012° |
| perigee height: | 737 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 209.4548° |
| argument of perigee: | 337.7627° |
| revolutions per day: | 14.42143339 |
| mean anomaly at epoch: | 22.2699° |
| orbit number at epoch: | 46535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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