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The eccentricity of the orbit of an Earth-orbiting spacecraft is 0.5. Its position at apoapsis in ECI is 13000000x -12000000y+5000000z. What is the orbit's eccentricity
The eccentricity of the orbit of an Earth-orbiting spacecraft is 0.5. Its position at apoapsis in ECI is 13000000x -12000000y+5000000z. What is the orbit's eccentricity vector
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