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 12786U 81082B 25194.92738742 .00000286 00000-0 29327-4 0 9999
2 12786 82.4866 66.4941 0015599 231.3880 128.5941 14.86827077351384
| Epoch (UTC): | 13 July 2025 22:15:26 |
| Eccentricity: | 0.0015599 |
| inclination: | 82.4866° |
| perigee height: | 597 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 66.4941° |
| argument of perigee: | 231.3880° |
| revolutions per day: | 14.86827077 |
| mean anomaly at epoch: | 128.5941° |
| orbit number at epoch: | 35138 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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