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 15598U 85022B 25318.84422965 .00000080 00000-0 65575-4 0 9994
2 15598 82.9376 342.9626 0022810 152.1464 21.2872 13.76815874 42988
| Epoch (UTC): | 14 November 2025 20:15:41 |
| Eccentricity: | 0.0022810 |
| inclination: | 82.9376° |
| perigee height: | 958 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 342.9626° |
| argument of perigee: | 152.1464° |
| revolutions per day: | 13.76815874 |
| mean anomaly at epoch: | 21.2872° |
| orbit number at epoch: | 4298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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