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 59588U 24077B 24280.19234058 .00006147 00000-0 69524-2 0 9999
2 59588 97.4396 322.6803 0051374 184.7134 175.3541 13.70097128 22588
| Epoch (UTC): | 06 October 2024 04:36:58 |
| Eccentricity: | 0.0051374 |
| inclination: | 97.4396° |
| perigee height: | 961 km |
| apogee height: | 1037 km |
| right ascension of ascending node: | 322.6803° |
| argument of perigee: | 184.7134° |
| revolutions per day: | 13.70097128 |
| mean anomaly at epoch: | 175.3541° |
| orbit number at epoch: | 2258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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