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 23083.87435874 .00001108 00000-0 12762-3 0 9991
2 15593 82.5343 90.8910 0009892 282.0695 77.9412 14.84861899 35711
| Epoch (UTC): | 24 March 2023 20:59:04 |
| Eccentricity: | 0.0009892 |
| inclination: | 82.5343° |
| perigee height: | 607 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 90.8910° |
| argument of perigee: | 282.0695° |
| revolutions per day: | 14.84861899 |
| mean anomaly at epoch: | 77.9412° |
| orbit number at epoch: | 3571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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