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 63575U 26145.55115546 +.00000000 +00000-0 -43786-3 0 00001
2 63575 43.0006 247.7799 0001926 280.3514 79.7120 15.27568104 02
| Epoch (UTC): | 25 May 2026 13:13:39 |
| Eccentricity: | 0.0001926 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.7799° |
| argument of perigee: | 280.3514° |
| revolutions per day: | 15.27568104 |
| mean anomaly at epoch: | 79.7120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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