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 31503U 99025BWS 24352.21282720 .00004389 00000-0 20473-2 0 9999
2 31503 100.1144 160.1775 0050649 101.9723 258.7133 14.20356579591241
| Epoch (UTC): | 17 December 2024 05:06:28 |
| Eccentricity: | 0.0050649 |
| inclination: | 100.1144° |
| perigee height: | 787 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 160.1775° |
| argument of perigee: | 101.9723° |
| revolutions per day: | 14.20356579 |
| mean anomaly at epoch: | 258.7133° |
| orbit number at epoch: | 59124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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