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 65424U 26145.26610319 +.00000000 +00000-0 +64009-3 0 00002
2 65424 53.1574 236.2883 0002348 94.9214 265.2056 15.31727043 05
| Epoch (UTC): | 25 May 2026 06:23:11 |
| Eccentricity: | 0.0002348 |
| inclination: | 53.1574° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 236.2883° |
| argument of perigee: | 94.9214° |
| revolutions per day: | 15.31727043 |
| mean anomaly at epoch: | 265.2056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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