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 56805U 26145.39022016 +.00000000 +00000-0 +52830-4 0 00000
2 56805 69.9988 131.0206 0003731 264.8559 95.2175 14.98332799 05
| Epoch (UTC): | 25 May 2026 09:21:55 |
| Eccentricity: | 0.0003731 |
| inclination: | 69.9988° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.0206° |
| argument of perigee: | 264.8559° |
| revolutions per day: | 14.98332799 |
| mean anomaly at epoch: | 95.2175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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