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 59186U 26145.56453326 +.00000000 +00000-0 +29949-5 0 00002
2 59186 43.0039 356.9698 0000911 286.2496 73.8256 15.27581593 01
| Epoch (UTC): | 25 May 2026 13:32:55 |
| Eccentricity: | 0.0000911 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.9698° |
| argument of perigee: | 286.2496° |
| revolutions per day: | 15.27581593 |
| mean anomaly at epoch: | 73.8256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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