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 59576U 26145.41453647 +.00000000 +00000-0 +80471-4 0 00001
2 59576 43.0046 295.9638 0001869 276.4882 83.5757 15.27576606 04
| Epoch (UTC): | 25 May 2026 09:56:55 |
| Eccentricity: | 0.0001869 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.9638° |
| argument of perigee: | 276.4882° |
| revolutions per day: | 15.27576606 |
| mean anomaly at epoch: | 83.5757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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