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 59331U 26145.36664804 +.00000000 +00000-0 +49786-4 0 00007
2 59331 43.0032 114.2296 0001284 289.0930 70.9782 15.27579280 05
| Epoch (UTC): | 25 May 2026 08:47:58 |
| Eccentricity: | 0.0001284 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.2296° |
| argument of perigee: | 289.0930° |
| revolutions per day: | 15.27579280 |
| mean anomaly at epoch: | 70.9782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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