Duende has an elliptical orbit about the Sun, with a perihelion distance of 0.829 AU and aphelion distance of 0.992 AU. What is the period of its orbit (in years)?
From Kepler's third law:
T^2 = (4*pi^2/GM)*a^3
Given that
T = time period of Duende's orbit = ?
M = mass of Sun = 2.0*10^30 kg
G = 6.67*10^-11
a = orbital radius of Duende = (perihelion distance + aphelion distance)/2 = (0.829 AU + 0.992 AU)/2 = 0.9105 AU
Since 1 AU = 1.496*10^11 m, So
a = 0.9105*1.496*10^11 m
So, Using above values:
T = sqrt (4*pi^2*a^3/(G*M))
T = sqrt (4*pi^2*(0.9105*1.496*10^11)^3/(6.67*10^-11*2.0*10^30))
T = 27347603.148 sec
Since 1 yr = 3.154*10^7 sec
So,
T = 27347603.148/(3.154*10^7) yr
T = 0.867 yrs = time period of Duende's orbit
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