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 56107U 26145.55701964 +.00000000 +00000-0 +26528-5 0 00005
2 56107 43.0061 87.7584 0001237 275.8693 84.2018 15.27577492 09
| Epoch (UTC): | 25 May 2026 13:22:06 |
| Eccentricity: | 0.0001237 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.7584° |
| argument of perigee: | 275.8693° |
| revolutions per day: | 15.27577492 |
| mean anomaly at epoch: | 84.2018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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