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 66564U 26145.40176231 +.00000000 +00000-0 +70334-3 0 00002
2 66564 43.0043 273.6807 0001238 266.3454 93.7256 15.27617309 03
| Epoch (UTC): | 25 May 2026 09:38:32 |
| Eccentricity: | 0.0001238 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.6807° |
| argument of perigee: | 266.3454° |
| revolutions per day: | 15.27617309 |
| mean anomaly at epoch: | 93.7256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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