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 56909U 26144.99784657 +.00000000 +00000-0 +32086-4 0 00007
2 56909 43.0071 0.1506 0001872 254.5595 105.5050 15.27577828 09
| Epoch (UTC): | 24 May 2026 23:56:53 |
| Eccentricity: | 0.0001872 |
| inclination: | 43.0071° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 0.1506° |
| argument of perigee: | 254.5595° |
| revolutions per day: | 15.27577828 |
| mean anomaly at epoch: | 105.5050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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