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 56925U 26145.55805307 +.00000000 +00000-0 +17117-4 0 00002
2 56925 43.0050 356.6097 0001158 267.7675 92.3044 15.27577469 07
| Epoch (UTC): | 25 May 2026 13:23:35 |
| Eccentricity: | 0.0001158 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.6097° |
| argument of perigee: | 267.7675° |
| revolutions per day: | 15.27577469 |
| mean anomaly at epoch: | 92.3044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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