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 60754U 24140ED 24357.44910747 .00004541 00000-0 22088-2 0 9996
2 60754 88.9795 335.3145 0059881 151.5897 208.8579 14.17132981 17555
| Epoch (UTC): | 22 December 2024 10:46:42 |
| Eccentricity: | 0.0059881 |
| inclination: | 88.9795° |
| perigee height: | 792 km |
| apogee height: | 878 km |
| right ascension of ascending node: | 335.3145° |
| argument of perigee: | 151.5897° |
| revolutions per day: | 14.17132981 |
| mean anomaly at epoch: | 208.8579° |
| orbit number at epoch: | 1755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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