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 56811U 26145.60721751 +.00000000 +00000-0 +51483-3 0 00005
2 56811 69.9858 76.9329 0014344 239.8162 120.1647 16.36776173 09
| Epoch (UTC): | 25 May 2026 14:34:23 |
| Eccentricity: | 0.0014344 |
| inclination: | 69.9858° |
| perigee height: | 165 km |
| apogee height: | 184 km |
| right ascension of ascending node: | 76.9329° |
| argument of perigee: | 239.8162° |
| revolutions per day: | 16.36776173 |
| mean anomaly at epoch: | 120.1647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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