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 58744U 26145.32296861 +.00000000 +00000-0 +13711-3 0 00002
2 58744 43.0032 1.5262 0002004 288.1778 71.8855 15.27584592 07
| Epoch (UTC): | 25 May 2026 07:45:04 |
| Eccentricity: | 0.0002004 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 1.5262° |
| argument of perigee: | 288.1778° |
| revolutions per day: | 15.27584592 |
| mean anomaly at epoch: | 71.8855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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