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 66423U 26145.47884859 +.00000000 +00000-0 +58879-3 0 00005
2 66423 43.0037 200.8276 0001559 276.2810 83.7864 15.27608372 08
| Epoch (UTC): | 25 May 2026 11:29:32 |
| Eccentricity: | 0.0001559 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.8276° |
| argument of perigee: | 276.2810° |
| revolutions per day: | 15.27608372 |
| mean anomaly at epoch: | 83.7864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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