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 56059U 26145.58378200 +.00000000 +00000-0 +82612-4 0 00002
2 56059 87.9252 248.4759 0001784 108.9505 251.1823 13.21825698 04
| Epoch (UTC): | 25 May 2026 14:00:38 |
| Eccentricity: | 0.0001784 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4759° |
| argument of perigee: | 108.9505° |
| revolutions per day: | 13.21825698 |
| mean anomaly at epoch: | 251.1823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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