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 66805U 26145.43984131 +.00000000 +00000-0 +83075-3 0 00005
2 66805 43.0045 41.2157 0001609 251.8661 108.2016 15.27586293 04
| Epoch (UTC): | 25 May 2026 10:33:22 |
| Eccentricity: | 0.0001609 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.2157° |
| argument of perigee: | 251.8661° |
| revolutions per day: | 15.27586293 |
| mean anomaly at epoch: | 108.2016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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