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 66809U 26144.98727611 +.00000000 +00000-0 +53711-3 0 00000
2 66809 43.0017 43.8346 0001371 257.8308 102.2391 15.27592520 05
| Epoch (UTC): | 24 May 2026 23:41:40 |
| Eccentricity: | 0.0001371 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 43.8346° |
| argument of perigee: | 257.8308° |
| revolutions per day: | 15.27592520 |
| mean anomaly at epoch: | 102.2391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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