Relative to a nonrotating frame of reference with origin at the center of the earth, a 1000 kg satellites initial position vector is r(0) 8000i 6000k (km) and its initial velocity vector is v(0) 7j (kms) Use Algorithm the RKF4(5) method to solve for the path of the spacecraft over the next four hours Determine its minimum and maximum distance from the earths surface during that time

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