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 54506U 22151JJ 24358.01887586 .00005465 00000-0 25484-2 0 9991
2 54506 98.9217 13.9359 0104463 332.6858 26.8847 14.17994159108869
| Epoch (UTC): | 23 December 2024 00:27:10 |
| Eccentricity: | 0.0104463 |
| inclination: | 98.9217° |
| perigee height: | 757 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 13.9359° |
| argument of perigee: | 332.6858° |
| revolutions per day: | 14.17994159 |
| mean anomaly at epoch: | 26.8847° |
| orbit number at epoch: | 10886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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