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 25196.94967040 .00000318 00000-0 33231-4 0 9998
2 15593 82.5364 19.3348 0011450 14.2743 345.8795 14.86494224161039
| Epoch (UTC): | 15 July 2025 22:47:31 |
| Eccentricity: | 0.0011450 |
| inclination: | 82.5364° |
| perigee height: | 601 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 19.3348° |
| argument of perigee: | 14.2743° |
| revolutions per day: | 14.86494224 |
| mean anomaly at epoch: | 345.8795° |
| orbit number at epoch: | 16103 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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