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 26106.21641779 +.00000000 +00000-0 +00000-0 0 00000
2 41866 0.1855 84.9208 0001665 245.5384 207.1254 1.00271343 08
| Epoch (UTC): | 16 April 2026 05:11:38 |
| Eccentricity: | 0.0001665 |
| inclination: | 0.1855° |
| perigee height: | 35780 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 84.9208° |
| argument of perigee: | 245.5384° |
| revolutions per day: | 1.00271343 |
| mean anomaly at epoch: | 207.1254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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