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 54567U 22151LT 24358.21405969 .00000661 00000-0 40852-3 0 9991
2 54567 98.8346 355.6111 0056731 83.9789 276.7842 14.07941673108383
| Epoch (UTC): | 23 December 2024 05:08:14 |
| Eccentricity: | 0.0056731 |
| inclination: | 98.8346° |
| perigee height: | 825 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 355.6111° |
| argument of perigee: | 83.9789° |
| revolutions per day: | 14.07941673 |
| mean anomaly at epoch: | 276.7842° |
| orbit number at epoch: | 10838 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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