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 64611U 26145.23253920 +.00000000 +00000-0 +45838-3 0 00006
2 64611 53.1587 339.7209 0000980 92.8894 267.2219 15.30200128 00
| Epoch (UTC): | 25 May 2026 05:34:51 |
| Eccentricity: | 0.0000980 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.7209° |
| argument of perigee: | 92.8894° |
| revolutions per day: | 15.30200128 |
| mean anomaly at epoch: | 267.2219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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