T is the period of the orbit around the Sun in earth years.
a is the semimajor axis in astronomical units, AU
The standard form of Kepler's third law:
T2 = a3
Solution for unknown T
T = a(3/2)
Solution for unknown a
a = T(2/3)
T is the period of the orbit around the Sun in earth years.
a is the semimajor axis in astronomical units, AU
The standard form of Kepler's third law:
T2 = a3
Solution for unknown T
T = a(3/2)
Solution for unknown a
a = T(2/3)
