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 43582U 26144.34445301 +.00000000 +00000-0 +00000-0 0 00006
2 43582 54.0836 183.1035 0004845 12.8500 347.2289 1.86227529 05
| Epoch (UTC): | 24 May 2026 08:16:00 |
| Eccentricity: | 0.0004845 |
| inclination: | 54.0836° |
| perigee height: | 21515 km |
| apogee height: | 21542 km |
| right ascension of ascending node: | 183.1035° |
| argument of perigee: | 12.8500° |
| revolutions per day: | 1.86227529 |
| mean anomaly at epoch: | 347.2289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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