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 59932U 26145.46774029 +.00000000 +00000-0 -15343-2 0 00007
2 59932 42.9983 259.0374 0001477 287.0526 73.0164 15.27566012 00
| Epoch (UTC): | 25 May 2026 11:13:32 |
| Eccentricity: | 0.0001477 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.0374° |
| argument of perigee: | 287.0526° |
| revolutions per day: | 15.27566012 |
| mean anomaly at epoch: | 73.0164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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