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 65426U 26145.53874787 +.00000000 +00000-0 +62255-3 0 00006
2 65426 53.1567 235.1432 0002374 295.3520 64.7234 15.30192913 04
| Epoch (UTC): | 25 May 2026 12:55:47 |
| Eccentricity: | 0.0002374 |
| inclination: | 53.1567° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 235.1432° |
| argument of perigee: | 295.3520° |
| revolutions per day: | 15.30192913 |
| mean anomaly at epoch: | 64.7234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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