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 25504U 98060A 24357.85142175 .00000784 00000-0 16908-3 0 9999
2 25504 24.9934 169.6440 0016929 163.3447 333.4813 14.45100751381920
| Epoch (UTC): | 22 December 2024 20:26:02 |
| Eccentricity: | 0.0016929 |
| inclination: | 24.9934° |
| perigee height: | 729 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 169.6440° |
| argument of perigee: | 163.3447° |
| revolutions per day: | 14.45100751 |
| mean anomaly at epoch: | 333.4813° |
| orbit number at epoch: | 38192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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