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 17566U 87024A 24284.55431338 .00051847 00000-0 89387-3 0 9991
2 17566 82.4916 139.4164 0001794 112.6020 247.5421 15.50828884 60491
| Epoch (UTC): | 10 October 2024 13:18:12 |
| Eccentricity: | 0.0001794 |
| inclination: | 82.4916° |
| perigee height: | 413 km |
| apogee height: | 415 km |
| right ascension of ascending node: | 139.4164° |
| argument of perigee: | 112.6020° |
| revolutions per day: | 15.50828884 |
| mean anomaly at epoch: | 247.5421° |
| orbit number at epoch: | 6049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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