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 24282.36033686 .00193946 00000-0 33124-2 0 9996
2 17566 82.4917 141.7036 0001675 111.9695 248.1734 15.50602665 60158
| Epoch (UTC): | 08 October 2024 08:38:53 |
| Eccentricity: | 0.0001675 |
| inclination: | 82.4917° |
| perigee height: | 414 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 141.7036° |
| argument of perigee: | 111.9695° |
| revolutions per day: | 15.50602665 |
| mean anomaly at epoch: | 248.1734° |
| orbit number at epoch: | 6015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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