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 09510U 76108B 25346.82879677 .00000102 00000-0 86224-4 0 9990
2 09510 82.9373 236.1881 0026837 134.4550 225.8809 13.77862404468392
| Epoch (UTC): | 12 December 2025 19:53:28 |
| Eccentricity: | 0.0026837 |
| inclination: | 82.9373° |
| perigee height: | 952 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 236.1881° |
| argument of perigee: | 134.4550° |
| revolutions per day: | 13.77862404 |
| mean anomaly at epoch: | 225.8809° |
| orbit number at epoch: | 46839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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