Calculate the orbital period for the following orbits (assume around Venus):
a) ? = 8000??
b) ? = 0.05, ?? = 12000??
c) ? = 11645??,? = 0.0232, ? = 128°
By Kepler's 3rd law of planetary motion
The orbital period of two point masses orbiting each other in a circular or elliptical path is given by

where a is the semi-major axis of the orbiting ellipse (or radius of the circular orbit)
G the Universal gravitational constant
M is the mass of the more massive body in the system
As it is given in the question It is around venus mass of venus is given by


so
A)
given a=8000km


B)
As the symbols r, a, e are not specified I am taking
r- semi-latus rectum
a-semi-major axis
e-eccentricty
we have the relation connecting these three




so time period T

C)
equation of orbit is


given r=11645km=11645000m
e=0.0232
f=1280



Calculate the orbital period for the following orbits (assume around Venus): a) ? = 8000?? b)...
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