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 31760U 99025CFK 24357.13700768 .00003125 00000-0 12479-2 0 9991
2 31760 99.2698 66.7978 0054579 140.9547 219.5592 14.28436177910528
| Epoch (UTC): | 22 December 2024 03:17:17 |
| Eccentricity: | 0.0054579 |
| inclination: | 99.2698° |
| perigee height: | 758 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 66.7978° |
| argument of perigee: | 140.9547° |
| revolutions per day: | 14.28436177 |
| mean anomaly at epoch: | 219.5592° |
| orbit number at epoch: | 91052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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