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 25560U 98071A 24357.84291197 .00004883 00000-0 36320-3 0 9995
2 25560 69.8961 177.8062 0006782 339.9739 20.1154 15.03614586415716
| Epoch (UTC): | 22 December 2024 20:13:47 |
| Eccentricity: | 0.0006782 |
| inclination: | 69.8961° |
| perigee height: | 551 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 177.8062° |
| argument of perigee: | 339.9739° |
| revolutions per day: | 15.03614586 |
| mean anomaly at epoch: | 20.1154° |
| orbit number at epoch: | 41571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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