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 59191U 26144.91855368 +.00000000 +00000-0 -19832-4 0 00008
2 59191 43.0026 18.2604 0001322 247.9375 112.1336 15.27589993 03
| Epoch (UTC): | 24 May 2026 22:02:43 |
| Eccentricity: | 0.0001322 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 18.2604° |
| argument of perigee: | 247.9375° |
| revolutions per day: | 15.27589993 |
| mean anomaly at epoch: | 112.1336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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