Scott D. answered 10/29/20
Knowledgeable Astronomy Tutor with 3 Years Teaching Experience
We can start with an equation relating period of an elliptical orbit to its semi-major axis:
Period (T)2 = 4π2(semi-major axis (a))3 / gravitational constant (G)(mass of the sun (M) + mass of the comet (m))
m is so much smaller than M that we can ignore it
(74 yr * 365 d/yr * 24 h/d * 3600 s/h)2 = 4π2a3 / (6.67 x 10-11)(2 x 1030)
a = 2.64 x 1012 m * 1 astronomical unit (AU)/ 1.5 x 1011 m = 17.6 AU
In an ellipse, perihelion distance = a - a(eccentricity) = 17.6 -17.6(0.94) = 1.06 AU