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 47563U 26144.91333111 +.00000000 +00000-0 +79017-3 0 00004
2 47563 53.0409 339.3879 0002349 282.8647 77.2111 15.78667296 01
| Epoch (UTC): | 24 May 2026 21:55:11 |
| Eccentricity: | 0.0002349 |
| inclination: | 53.0409° |
| perigee height: | 333 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 339.3879° |
| argument of perigee: | 282.8647° |
| revolutions per day: | 15.78667296 |
| mean anomaly at epoch: | 77.2111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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