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 55786U 26145.66668980 +.00000000 +00000-0 -91583-3 0 00001
2 55786 70.0019 10.4509 0002966 266.7998 129.0976 14.98346652 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0002966 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.4509° |
| argument of perigee: | 266.7998° |
| revolutions per day: | 14.98346652 |
| mean anomaly at epoch: | 129.0976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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