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 26106.89709382 +.00000000 +00000-0 +25640-4 0 00009
2 12786 82.4889 164.4630 0017710 41.3031 318.9522 14.87179742 07
| Epoch (UTC): | 16 April 2026 21:31:48 |
| Eccentricity: | 0.0017710 |
| inclination: | 82.4889° |
| perigee height: | 594 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 164.4630° |
| argument of perigee: | 41.3031° |
| revolutions per day: | 14.87179742 |
| mean anomaly at epoch: | 318.9522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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