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 58594U 26145.24700617 +.00000000 +00000-0 +60259-4 0 00005
2 58594 43.0040 96.1199 0001173 286.1326 73.9397 15.27584373 02
| Epoch (UTC): | 25 May 2026 05:55:41 |
| Eccentricity: | 0.0001173 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.1199° |
| argument of perigee: | 286.1326° |
| revolutions per day: | 15.27584373 |
| mean anomaly at epoch: | 73.9397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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