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 55647U 26144.98802818 +.00000000 +00000-0 +70848-4 0 00002
2 55647 69.9996 351.9401 0002674 267.8117 92.2736 14.98331444 01
| Epoch (UTC): | 24 May 2026 23:42:45 |
| Eccentricity: | 0.0002674 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.9401° |
| argument of perigee: | 267.8117° |
| revolutions per day: | 14.98331444 |
| mean anomaly at epoch: | 92.2736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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