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 is defined by the following mean orbital elements,
1 12786U 26017.13854133 +.00000000 +00000-0 +38808-4 0 00002
2 12786 82.4860 249.3834 0016290 339.3823 20.6735 14.87072557 05
| Epoch (UTC): | 17 January 2026 03:19:29 |
| Eccentricity: | 0.0016290 |
| inclination: | 82.4860° |
| perigee height: | 596 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 249.3834° |
| argument of perigee: | 339.3823° |
| revolutions per day: | 14.87072557 |
| mean anomaly at epoch: | 20.6735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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