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 59530U 26145.57466013 +.00000000 +00000-0 -80228-4 0 00000
2 59530 43.0002 243.8533 0001611 270.7388 89.3279 15.27569580 01
| Epoch (UTC): | 25 May 2026 13:47:30 |
| Eccentricity: | 0.0001611 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.8533° |
| argument of perigee: | 270.7388° |
| revolutions per day: | 15.27569580 |
| mean anomaly at epoch: | 89.3279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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