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 29796U 99025CN 24357.69366021 .00002298 00000-0 12838-2 0 9997
2 29796 98.9034 47.0217 0054384 191.2388 293.7256 14.11062940920514
| Epoch (UTC): | 22 December 2024 16:38:52 |
| Eccentricity: | 0.0054384 |
| inclination: | 98.9034° |
| perigee height: | 816 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 47.0217° |
| argument of perigee: | 191.2388° |
| revolutions per day: | 14.11062940 |
| mean anomaly at epoch: | 293.7256° |
| orbit number at epoch: | 92051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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