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 23159.42311087 .00010975 00000-0 38948-3 0 9999
2 17566 82.5017 279.4522 0004186 142.7328 217.4203 15.28918473985220
| Epoch (UTC): | 08 June 2023 10:09:16 |
| Eccentricity: | 0.0004186 |
| inclination: | 82.5017° |
| perigee height: | 476 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 279.4522° |
| argument of perigee: | 142.7328° |
| revolutions per day: | 15.28918473 |
| mean anomaly at epoch: | 217.4203° |
| orbit number at epoch: | 98522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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