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 59190U 26145.06040705 +.00000000 +00000-0 +38469-4 0 00001
2 59190 43.0041 21.0393 0001171 267.8981 92.1736 15.27584885 08
| Epoch (UTC): | 25 May 2026 01:26:59 |
| Eccentricity: | 0.0001171 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.0393° |
| argument of perigee: | 267.8981° |
| revolutions per day: | 15.27584885 |
| mean anomaly at epoch: | 92.1736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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