Oribital elements from ECI to ECEF
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 advanceHello,
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 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 matlab MATLAB Answers — New Questions