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 66579U 26145.40693583 +.00000000 +00000-0 +40047-3 0 00000
2 66579 43.0022 273.7196 0000623 284.0252 76.0530 15.27557276 03
| Epoch (UTC): | 25 May 2026 09:45:59 |
| Eccentricity: | 0.0000623 |
| inclination: | 43.0022° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.7196° |
| argument of perigee: | 284.0252° |
| revolutions per day: | 15.27557276 |
| mean anomaly at epoch: | 76.0530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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