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 15595U 85021A 25118.44067394 .00000574 00000-0 22656-3 0 9995
2 15595 108.0585 298.2638 0001366 269.1943 90.9043 14.39647699103379
| Epoch (UTC): | 28 April 2025 10:34:34 |
| Eccentricity: | 0.0001366 |
| inclination: | 108.0585° |
| perigee height: | 758 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 298.2638° |
| argument of perigee: | 269.1943° |
| revolutions per day: | 14.39647699 |
| mean anomaly at epoch: | 90.9043° |
| orbit number at epoch: | 10337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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