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 59567U 26145.66628564 +.00000000 +00000-0 +45370-4 0 00009
2 59567 43.0032 290.9604 0001804 270.5937 89.4707 15.27580702 04
| Epoch (UTC): | 25 May 2026 15:59:27 |
| Eccentricity: | 0.0001804 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 290.9604° |
| argument of perigee: | 270.5937° |
| revolutions per day: | 15.27580702 |
| mean anomaly at epoch: | 89.4707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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