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 59565U 26145.47607125 +.00000000 +00000-0 +10045-3 0 00006
2 59565 43.0033 295.5869 0002063 275.1916 84.8700 15.27569752 07
| Epoch (UTC): | 25 May 2026 11:25:32 |
| Eccentricity: | 0.0002063 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.5869° |
| argument of perigee: | 275.1916° |
| revolutions per day: | 15.27569752 |
| mean anomaly at epoch: | 84.8700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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