Solution. Find semi-major axis a
a=2ra+rp=26.1×1011+6.1×1011=6.1×1011m
where ra is aphelion distance; rp is perihelion distance.
Find the orbital period T of a comet
T2a3=4π2G(M+m) where M=2.0 × 10^30kg is the mass of the sun; m is a comet mass; (M>>m). Therefore
T=GM2πa3=6.67×10−11×2×10302π(6.1×1011)3=2.59×108s≈8.22years Average orbit speed
v=T2πa=2.59×1082π×6.1×1011≈14/55skm
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