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 41866U 26151.47331927 +.00000000 +00000-0 +00000-0 0 00009
2 41866 0.2986 85.7075 0000798 309.0840 279.9309 1.00271376 08
| Epoch (UTC): | 31 May 2026 11:21:34 |
| Eccentricity: | 0.0000798 |
| inclination: | 0.2986° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 85.7075° |
| argument of perigee: | 309.0840° |
| revolutions per day: | 1.00271376 |
| mean anomaly at epoch: | 279.9309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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