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 57645U 26145.56142294 +.00000000 +00000-0 +15315-3 0 00009
2 57645 43.0073 236.2672 0001928 273.0464 87.0168 15.27564001 01
| Epoch (UTC): | 25 May 2026 13:28:26 |
| Eccentricity: | 0.0001928 |
| inclination: | 43.0073° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.2672° |
| argument of perigee: | 273.0464° |
| revolutions per day: | 15.27564001 |
| mean anomaly at epoch: | 87.0168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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