Weight ∝ 1/distance2
Let W = the astronaut's weight 500 miles above the earth's surface and R = the Earth's radius = 4000 mi. We can set up a proportion:
W/227 = [1/(R+500)2]/[1/R2]
W/227 = R2/(R+500)2
W = 227*(4000)2/(4500)2
Solve for W.