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 66850U 26040.31089512 +.00000000 +00000-0 +14191-2 0 00007
2 66850 42.9975 143.8883 0000762 262.2566 97.8199 15.27612843 04
| Epoch (UTC): | 09 February 2026 07:27:41 |
| Eccentricity: | 0.0000762 |
| inclination: | 42.9975° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 143.8883° |
| argument of perigee: | 262.2566° |
| revolutions per day: | 15.27612843 |
| mean anomaly at epoch: | 97.8199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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