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Oribital elements from ECI to ECEF

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VAHA
VAHA 2024-5-9
回答： ScottB 2024-5-9
Hello,
I have 6 orbital elements in ECI frame, but I need them to be in Earth fixed (ECEF).
Is there any MATLAB function available to get position, velocity vectors from 6 orbital elements and connvert them to ECEF position and velocity vectors?
Thanks in advance

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ScottB
ScottB 2024-5-9

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