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 62426U 26145.55592274 +.00000000 +00000-0 +51302-3 0 00004
2 62426 42.9987 240.4626 0000623 256.8929 103.1853 15.27593910 00
| Epoch (UTC): | 25 May 2026 13:20:31 |
| Eccentricity: | 0.0000623 |
| inclination: | 42.9987° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 240.4626° |
| argument of perigee: | 256.8929° |
| revolutions per day: | 15.27593910 |
| mean anomaly at epoch: | 103.1853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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