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 56810U 26145.41130829 +.00000000 +00000-0 -30748-5 0 00007
2 56810 69.9984 150.9623 0003729 266.8515 93.2217 14.98330400 03
| Epoch (UTC): | 25 May 2026 09:52:17 |
| Eccentricity: | 0.0003729 |
| inclination: | 69.9984° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 150.9623° |
| argument of perigee: | 266.8515° |
| revolutions per day: | 14.98330400 |
| mean anomaly at epoch: | 93.2217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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