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 59952U 26145.52624906 +.00000000 +00000-0 +44227-4 0 00008
2 59952 53.1589 232.5119 0001073 75.1520 284.9616 15.69736000 00
| Epoch (UTC): | 25 May 2026 12:37:47 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 232.5119° |
| argument of perigee: | 75.1520° |
| revolutions per day: | 15.69736000 |
| mean anomaly at epoch: | 284.9616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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