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Explanation of Length of Year for Objects in Gravitational Orbit - Succeed in Understanding Physics. Also refer to Earth, Sun, Moon, Jupiter, planets, attraction, centrifugal force, universal gravitational constant, elliptical orbit, physical science, Ron Kurtus, School for Champions. Copyright © Restrictions

Length of Year for Objects in Gravitational Orbit

by Ron Kurtus (revised 8 July 2010)

You can derive the equation for the time it takes an object in a gravitational orbit to make one revolution, provided you know its orbital velocity, its distance to the center of the much larger object about which it is in orbit, as well as the mass of the larger object.

The time it takes the Earth to make one revolution around the Sun is called a year, so it is convenient to state the orbital period in terms of Earth years or even Earth days.

To simplify the calculations, the equation for the orbital period assumes that the orbit is circular. The equation can be verified by considering the period of the Moon around the Earth and how long it takes the Earth, as well as the planet Jupiter, to go around the Sun.

Questions you may have include:

This lesson will answer those questions. There is a mini-quiz near the end of the lesson.

Useful tools: Metric-English Conversion | Scientific Calculator.

Velocity to be in a circular orbit

The velocity of an object in circular orbit is a function of the mass of the larger object and the distance between their centers. The equation for the orbital velocity is derived by equating the Universal Gravitational Equation with the centrifugal inertial force of the object.

(See Circular Gravitational Orbits for more information.)

The equation for the velocity of a circular orbit is:

v = √(GM/R)

where

Note that the mass of the object in orbit is not a factor in this equation.

Deriving equation for one revolution

Knowing the required velocity to be in a circular orbit allows you to determine the time it takes to make one revolution around the larger object. The distance traveled in one revolution is the circumference of the circle of radius R:

C = 2πR

where

Note: Circumference is in meters since G is in meters.

Since distance equals velocity times time:

C = vT

where

Substitute in C and solve for T:

vT = 2πR

T = 2πR/v

Substitute v = √(GM/R):

T = 2πR/√(GM/R)

T = 2π√(R2)/√(GM/R)

Multiply by √(R3/GM)/√(R3/GM) = 1 to facilitate calculations:

T = 2π√(R3/GM)

Verify units

Verify the equation is correct for the units used:

T s = 2π√[(R3 m3)/(G m3/kg-s2)(M kg)]

s = √(s2)

s = s

Convert from seconds

You usually calculate the orbit in Earth days or years, so you need to convert seconds to a different unit of measurement.

Equation for number of days

Thus, 1 day = (24 hours)*(60 minutes)*(60 seconds) = 86400 seconds. Divide by the number of seconds per day to get the orbit equation for days:

D = 2π√(R3/GM)/86400

Since 2π = 6.28, you get:

D = (7.27*10−5)√(R3/GM) Earth days

Equation for number of years

Also, 1 year = (365 days)*(86400 seconds) = 31,536,000 seconds. That can be simplified to 3.15*107 s/yr.

Y = [2π√(R3/GM)]/3.15*107

Y = 2*10−7√(R3/GM) Earth years

Examples

You can calculate the number of days it takes the Moon to rotate around the Earth and the number of years it takes the Earth and planet Jupiter to go around the Sun.

Note: Since the distance R and mass M are not exact, as well as the fact that the orbits are not exactly circular, but are slightly elliptical, the time to complete an orbit is not exact. However, the calculations do come out fairly close to what is experienced.

Moon orbits the Earth

The average distance from the center of the Earth to the center of the Moon is 384,403 kilometers or R = 3.84*108 m.

R3 = 56.62*1024 m3

The mass of the Earth is M = 5.9736*1024 kg.

GM = (6.67*10−11)(5.97*1024) = 39.8*1013 m3/s2

R3/GM = 56.62*1024/39.8*1013 = 1.423*1011 s2

Make the exponent even to facilitate taking square root:

R3/GM = 14.23*1010 s2

√(R3/GM) = 3.77*105 s

Substitute into D = (7.27*10−5)√(R3/GM)

D = (7.27*10−5)(3.77*105) days = 27.4 days

That is close to the average of 28 days for the Moon to orbit the Earth.

Earth orbits the Sun

Let's test these equations by checking the time it takes the Earth to rotate around the Sun.

The average distance from the center of the Sun to the center of the Earth is
R = 1.496*1011 m.

R3 = 3.348*1033 m3

The mass of the Sun is M = 1.989*1030 kg. Thus:

GM = (6.67*10−11)(1.9891*1030) = 13.27*1019 m3/s2

R3/GM = 3.348*1033/13.27*1019 = 0.2522*1014 s2

Increase number to facilitate taking square root:

R3/GM = 25.22*1012 s2

√(R3/GM) = 5.02*106 s

Substitute into D = (7.27*10−5)√(R3/GM):

D = (7.27*10−5)(5.02*106) days = 364.95 days

Substitute into Y = 2*10−7√(R3/GM):

Y = (2*10−7)(5.02*106) years

Y = 1.004 years

It takes one year for the Earth to orbit the Sun.

Earth and Jupiter orbit Sun

Earth and Jupiter orbit Sun

Jupiter orbits the Sun

The average distance of the planet Jupiter from the Sun is R = 7.786*1011 m. Thus:

R3 = 472*1033 m3

The mass of the Sun is M = 1.989*1030 kg. Thus:

GM = (6.67*10−11)(1.9891*1030) = 13.27*1019 m3/s2

R3/GM = 472*1033/13.27*1019 = 35.57*1014 s2

√(R3/GM) = 5.96*107 s

Substitute into Y = 2*10−7√(R3/GM):

Y = (2*10−7)(5.96*107) years

Y = 11.9 years

This corresponds to the measured time it takes Jupiter to orbit the Sun.

Summary

If you know the velocity of an object in orbit and its distance to the center of the much larger object, as well as the mass of the larger object, you can calculate how long it takes to make one revolution in Earth days or Earth years. The equation can be verified by considering the period of the Moon around the Earth and how long it takes the Earth and Jupiter to go around the Sun.

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Websites

Acceleration due to Gravity Calculations - from Western Washington University

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Mini-quiz to check your understanding

1. If many orbits are elliptical, why is the circular orbit equation used?

The velocity for an ellipse is 2/3 the velocity of a circle

Values are easier to calculate and are close enough for most purposes

No one is really sure why scientists continue to use the circular equation

2. Why is the orbital period converted into Earth years?

It is because orbits are not true circles

It depends on what planet you are talking about

It is a convenient way to relate to the time it takes to orbit

3. What would the Earth's orbital period be if it was 4 times as far from the Sun than it is now?

The orbital period would be the same

The orbital period would be 8 years (2*2*2)

The orbital period would be 64 years (4*4*4)

If you got all three correct, you are on your way to becoming a Champion in Physics. If you had problems, you had better look over the material again.


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