Question
Question: How is orbital period calculated if perihelion and aphelion are known? For example, the orbit of a s...
How is orbital period calculated if perihelion and aphelion are known? For example, the orbit of a spacecraft about the sun has a perihelion distance of 0.5AU and aphelion of 3.5AU. What is its orbital period?
Solution
You could find the orbital period from by using kepler’s third law. You may not find the perihelion and aphelion in the common expression but their sum is the semi major axis which would be the R in the formula. Since all we have is proportionality relation, we could find their ratio which would be a constant by substituting earth’s semi major axis and time period and then find the orbital period for the given spacecraft by substituting accordingly.
Formula used:
Kepler’s third law of planetary motion,
T2∝R3
Complete answer:
We could find the orbital period by using Kepler’s third law of planetary motion when the perihelion and aphelion are known.
According to Kepler’s third law,
T2∝R3
Where, R is the body’s average distance from the sun and T is the time period.
R3T2=C ………………………………….. (1)
Now let us find this constant C by substituting Earth’s orbital period and semi major axis.
C=(1AU)3(1Year)2=1AU3year2 ………………………………….. (2)
Now, for the spacecraft,
R=2perihelion+aphelion
⇒R=25AU+3.5AU=2AU ………………………………. (3)
Now from equation (1) we have,
T2=CR3
Substituting (2) and (3) we get,
T2=(1AU3Year2)(2AU)3
⇒T2=8years2
∴T=22years
Hence, we found the spacecraft’s orbital speed to be 2.83years.
Note:
Kepler’s third law is not limited to the sun and its planetary system. It could be applied to all orbiting bodies. However, the constant that we found would quite obviously be different and hence should be found accordingly. Also, AU stands for astronomical unit which is used as a unit for measuring greater distances.