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 56866U 26145.63286412 +.00000000 +00000-0 +28355-3 0 00000
2 56866 97.2910 209.7561 0012516 93.3542 266.9128 15.24642162 09
| Epoch (UTC): | 25 May 2026 15:11:19 |
| Eccentricity: | 0.0012516 |
| inclination: | 97.2910° |
| perigee height: | 483 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 209.7561° |
| argument of perigee: | 93.3542° |
| revolutions per day: | 15.24642162 |
| mean anomaly at epoch: | 266.9128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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