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 56375U 26145.33444093 +.00000000 +00000-0 +48771-4 0 00008
2 56375 43.0045 124.8652 0001743 286.9442 73.1219 15.27579663 06
| Epoch (UTC): | 25 May 2026 08:01:35 |
| Eccentricity: | 0.0001743 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.8652° |
| argument of perigee: | 286.9442° |
| revolutions per day: | 15.27579663 |
| mean anomaly at epoch: | 73.1219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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