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Create a matlab script that will convert position and velocity vectors into the 6 orbital elements. to test

your script you can use the example we did in class. (r=-6045i-3490j+2500k, v=-3.457i+6.618j+2.533k

results in a=8787.43 km, e = 0.171, i=153.249deg, ω=255.28 deg, ω=20.11 deg, ν=28.76 deg)

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Create a matlab script that will convert position and velocity vectors into the 6 orbital elements....
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