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 25160U 98007D 24357.86038608 .00000367 00000-0 21924-3 0 9995
2 25160 108.0059 319.6693 0063033 336.6034 79.6839 14.22207599393543
| Epoch (UTC): | 22 December 2024 20:38:57 |
| Eccentricity: | 0.0063033 |
| inclination: | 108.0059° |
| perigee height: | 772 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 319.6693° |
| argument of perigee: | 336.6034° |
| revolutions per day: | 14.22207599 |
| mean anomaly at epoch: | 79.6839° |
| orbit number at epoch: | 39354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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