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 56422U 26145.61622506 +.00000000 +00000-0 +18219-4 0 00003
2 56422 43.0045 105.1949 0001686 276.4122 83.6537 15.27575900 04
| Epoch (UTC): | 25 May 2026 14:47:21 |
| Eccentricity: | 0.0001686 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 105.1949° |
| argument of perigee: | 276.4122° |
| revolutions per day: | 15.27575900 |
| mean anomaly at epoch: | 83.6537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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