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 59533U 26145.01191079 +.00000000 +00000-0 +29653-4 0 00003
2 59533 43.0059 247.3861 0001888 270.5512 89.5124 15.27572463 07
| Epoch (UTC): | 25 May 2026 00:17:09 |
| Eccentricity: | 0.0001888 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.3861° |
| argument of perigee: | 270.5512° |
| revolutions per day: | 15.27572463 |
| mean anomaly at epoch: | 89.5124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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