Prove that the time taken by the Earth to travel over half of its orbit, which is separated by the minor axis and is remote from the Sun, when the Sun is at the focus of the elliptic orbit, is two days more than half of the year. The eccentricity of the orbit is taken as 601.
Technique
Use Kepler’s second law (constant areal velocity): the time over an arc equals the area swept by the radius vector from the focus divided by the constant areal velocity Tπab.
Solution
Place the ellipse a2x2+b2y2=1 with centre at the origin and the Sun at the focus S=(ae,0). The minor axis is the line x=0; its endpoints are L=(0,b) and L′=(0,−b). The minor axis cuts the orbit into two halves:
the half x>0, near the Sun;
the half x<0, remote from the Sun (this is the half in question).
By Kepler’s second law the radius vector from S sweeps area at the constant rate
dtdA=Ttotal area=Tπab,
where T is the orbital period (one year).
Area swept over the remote half. As the Earth moves along the far arc from L=(0,b) to L′=(0,−b), the area swept out by SL,SL′ is the region bounded by the far arc and the two radii SL,SL′. This equals
Aremote=area of the half-ellipse x<021πab+triangle with base LL′(△SLL′),
because the focus S lies on the near side (x>0), so the triangle SLL′ must be added to the half-ellipse area to obtain the focal sector.
The triangle SLL′ has base LL′=2b along the y-axis and height ae (the x-distance of S from the minor axis), so
△SLL′=21(2b)(ae)=abe.
Hence
Aremote=2πab+abe.
Time for the remote half.tremote=πab/TAremote=T(21+πe)=2T+πTe.
So the remote half takes longer than half the year by
Δt=tremote−2T=πTe.
Numerical value. With e=601 and T=365.25 days,
Δt=π365.25⋅601=60π365.25≈1.938 days≈2 days.
(With T=365 days, Δt≈1.936 days; in either case “two days more than half a year,” as required.)
Answer
tremote=2T+πTe,Δt=πTe=60π365.25≈1.94≈2days.
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