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 56426U 26145.29978778 +.00000000 +00000-0 -43733-5 0 00007
2 56426 43.0033 107.1055 0001133 255.4824 104.5901 15.26738778 09
| Epoch (UTC): | 25 May 2026 07:11:41 |
| Eccentricity: | 0.0001133 |
| inclination: | 43.0033° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 107.1055° |
| argument of perigee: | 255.4824° |
| revolutions per day: | 15.26738778 |
| mean anomaly at epoch: | 104.5901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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