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 36510U 10013C 25188.58560083 .00001640 00000-0 25343-3 0 9990
2 36510 92.0153 218.8627 0021591 146.8735 213.3842 14.73110852813729
| Epoch (UTC): | 07 July 2025 14:03:15 |
| Eccentricity: | 0.0021591 |
| inclination: | 92.0153° |
| perigee height: | 636 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 218.8627° |
| argument of perigee: | 146.8735° |
| revolutions per day: | 14.73110852 |
| mean anomaly at epoch: | 213.3842° |
| orbit number at epoch: | 81372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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