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 66611U 26145.56241488 +.00000000 +00000-0 +70141-3 0 00005
2 66611 43.0017 341.9473 0001296 277.1947 82.8757 15.27592009 00
| Epoch (UTC): | 25 May 2026 13:29:52 |
| Eccentricity: | 0.0001296 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.9473° |
| argument of perigee: | 277.1947° |
| revolutions per day: | 15.27592009 |
| mean anomaly at epoch: | 82.8757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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