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 66055U 26145.43528263 +.00000000 +00000-0 +18626-3 0 00002
2 66055 97.4268 214.0374 0013514 233.9882 126.0103 15.23907475 06
| Epoch (UTC): | 25 May 2026 10:26:48 |
| Eccentricity: | 0.0013514 |
| inclination: | 97.4268° |
| perigee height: | 485 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 214.0374° |
| argument of perigee: | 233.9882° |
| revolutions per day: | 15.23907475 |
| mean anomaly at epoch: | 126.0103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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