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 59159U 26145.41370227 +.00000000 +00000-0 +35619-4 0 00004
2 59159 43.0043 33.3786 0001013 247.2961 112.7784 15.27582007 08
| Epoch (UTC): | 25 May 2026 09:55:43 |
| Eccentricity: | 0.0001013 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.3786° |
| argument of perigee: | 247.2961° |
| revolutions per day: | 15.27582007 |
| mean anomaly at epoch: | 112.7784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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