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 66814U 26145.39615354 +.00000000 +00000-0 +79137-3 0 00002
2 66814 42.9979 40.8760 0001199 334.4245 25.6547 15.27601012 01
| Epoch (UTC): | 25 May 2026 09:30:27 |
| Eccentricity: | 0.0001199 |
| inclination: | 42.9979° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.8760° |
| argument of perigee: | 334.4245° |
| revolutions per day: | 15.27601012 |
| mean anomaly at epoch: | 25.6547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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