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 31633U 99025CAP 24354.84343570 .00001877 00000-0 11633-2 0 9992
2 31633 98.7364 16.1729 0068016 100.5238 260.3602 14.05189049520558
| Epoch (UTC): | 19 December 2024 20:14:32 |
| Eccentricity: | 0.0068016 |
| inclination: | 98.7364° |
| perigee height: | 826 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 16.1729° |
| argument of perigee: | 100.5238° |
| revolutions per day: | 14.05189049 |
| mean anomaly at epoch: | 260.3602° |
| orbit number at epoch: | 52055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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