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 15593U 85020B 23331.76564096 .00000952 00000-0 10815-3 0 9997
2 15593 82.5393 218.6349 0011410 172.2839 187.8555 14.85229477 72509
| Epoch (UTC): | 27 November 2023 18:22:31 |
| Eccentricity: | 0.0011410 |
| inclination: | 82.5393° |
| perigee height: | 605 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 218.6349° |
| argument of perigee: | 172.2839° |
| revolutions per day: | 14.85229477 |
| mean anomaly at epoch: | 187.8555° |
| orbit number at epoch: | 7250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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