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 58686U 26145.32420370 +.00000000 +00000-0 -16806-4 0 00001
2 58686 43.0059 12.5898 0000799 295.9373 64.1397 15.27576074 06
| Epoch (UTC): | 25 May 2026 07:46:51 |
| Eccentricity: | 0.0000799 |
| inclination: | 43.0059° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.5898° |
| argument of perigee: | 295.9373° |
| revolutions per day: | 15.27576074 |
| mean anomaly at epoch: | 64.1397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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