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 64066U 26145.28052458 +.00000000 +00000-0 +14399-2 0 00005
2 64066 43.0000 356.5853 0000946 299.0447 61.0326 15.70883221 05
| Epoch (UTC): | 25 May 2026 06:43:57 |
| Eccentricity: | 0.0000946 |
| inclination: | 43.0000° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 356.5853° |
| argument of perigee: | 299.0447° |
| revolutions per day: | 15.70883221 |
| mean anomaly at epoch: | 61.0326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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