By definition ECEF coordinates should be a Cartesian system centered at the earth center of mass. So how can a satellite in Aerospace Blockset simulation (R2019) have coordinates that are smaller than the earth radius? (eg, -5.7*10^6, -1.7*10^6, 3.15*10^6.)
MATLAB: ECEF smaller than earth radius
Aerospace Blocksetecef"satellitesimulink
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