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 56259U 22151ACB 24357.44712872 .00006501 00000-0 34423-2 0 9994
2 56259 98.8150 355.0345 0052912 77.0196 283.6878 14.13285059 96447
| Epoch (UTC): | 22 December 2024 10:43:51 |
| Eccentricity: | 0.0052912 |
| inclination: | 98.8150° |
| perigee height: | 810 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 355.0345° |
| argument of perigee: | 77.0196° |
| revolutions per day: | 14.13285059 |
| mean anomaly at epoch: | 283.6878° |
| orbit number at epoch: | 9644 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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