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 24260.13915961 -.00118014 00000-0 -21510-2 0 9997
2 25544 51.6391 224.8557 0006897 357.6020 94.5423 15.49172500472658
| Epoch (UTC): | 16 September 2024 03:20:23 |
| Eccentricity: | 0.0006897 |
| inclination: | 51.6391° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 224.8557° |
| argument of perigee: | 357.6020° |
| revolutions per day: | 15.49172500 |
| mean anomaly at epoch: | 94.5423° |
| orbit number at epoch: | 47265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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