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 63456U 26144.72761898 +.00000000 +00000-0 +59533-3 0 00000
2 63456 53.1597 146.6281 0001302 80.6312 279.4841 15.42177499 04
| Epoch (UTC): | 24 May 2026 17:27:46 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1597° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 146.6281° |
| argument of perigee: | 80.6312° |
| revolutions per day: | 15.42177499 |
| mean anomaly at epoch: | 279.4841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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