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 25544U 98067A 24257.43740581 .00029683 00000-0 54381-3 0 9994
2 25544 51.6389 238.2218 0007302 348.1172 146.9367 15.49035216472238
| Epoch (UTC): | 13 September 2024 10:29:51 |
| Eccentricity: | 0.0007302 |
| inclination: | 51.6389° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 238.2218° |
| argument of perigee: | 348.1172° |
| revolutions per day: | 15.49035216 |
| mean anomaly at epoch: | 146.9367° |
| orbit number at epoch: | 47223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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