here,
a)
the period of satellite , T = 7.1 yrs = 7.1 * 3600 * 365 * 24 s
let the radius of orbit be r1
the circumference of orbit = 2*pi*r1 = T * v1
2*pi*r1 = 7.1 * 3600 * 365 * 24 * 45.8 * 10^3
solving for r1
r1 = 1.62 * 10^13 m
let the mass of the star be M
the time period , T = 2*pi* sqrt(r1^3 /(G * M))
7.1 * 3600 = 2*pi*sqrt((1.62 * 10^13)^3 /(6.67 * 10^-11 * M) )
solving for M
M = 3.85 * 10^42 kg
the mass of star is 3.85 * 10^42 kg
b)
P2 /P1 = (r2 /r1)^3/2
P2 /P1 = ( (v2 * P2) /(v1 * P1))^3/2
(P2/P1)-1/2 = ( v2 /v1)^3/2
(P1/P2) = ( v2 /v1)^3
7.1 /P2 = (59.8 / 45.8)
P2 = 5.44 yrs
the new period is 5.44 yrs