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 57525U 26145.08718390 +.00000000 +00000-0 +21102-4 0 00001
2 57525 43.0015 290.2907 0001191 300.1879 59.8855 15.27582341 06
| Epoch (UTC): | 25 May 2026 02:05:32 |
| Eccentricity: | 0.0001191 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 290.2907° |
| argument of perigee: | 300.1879° |
| revolutions per day: | 15.27582341 |
| mean anomaly at epoch: | 59.8855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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