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 40114U 14047F 24357.47667593 .00000279 00000-0 44568-3 0 9992
2 40114 63.3860 0.5181 0343373 12.4805 348.4460 13.44219982509080
| Epoch (UTC): | 22 December 2024 11:26:24 |
| Eccentricity: | 0.0343373 |
| inclination: | 63.3860° |
| perigee height: | 837 km |
| apogee height: | 1350 km |
| right ascension of ascending node: | 0.5181° |
| argument of perigee: | 12.4805° |
| revolutions per day: | 13.44219982 |
| mean anomaly at epoch: | 348.4460° |
| orbit number at epoch: | 50908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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