Time period of an object traveling in an elliptical orbit

In summary, @gneill has told you that you can calculate the time period of an ellipse by dividing the total area of the ellipse by the specific angular momentum.
  • #1
Saptarshi Sarkar
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Homework Statement
A body of mass 1kg is moving under a central force in an elliptic orbit with semi major axis 1000 m and semi minor axis 100 m. The orbital angular momentum of the body is 1000 kg m²/s. What is the time period of the motion?
Relevant Equations
Angular Momentum : mvr = constant
Equation of ellipse : ##\frac 1 r = \frac {1 + εCosθ} l## where r = distance from foci and l = length of latus rectum
I know that the angular momentum of the particle orbiting in an elliptical path is constant and due to which the particle speeds up near the foci when r is small.

But, I cannot figure out how to calculate the time period of rotation. I can do the same for an ellipse by taking mv²/r = central force, but not able to find the equation required for the ellipse.
 
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  • #2
Kepler's second law is the key. It is essentially a statement about angular momentum, and "specific angular momentum" in particular.

What's the total area of your ellipse?
 
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  • #3
gneill said:
Kepler's second law is the key. It is essentially a statement about angular momentum, and "specific angular momentum" in particular.

What's the total area of your ellipse?

##πab = π*1000*100 = 100000π##
 
  • #4
Saptarshi Sarkar said:
##πab = π*1000*100 = 100000π##
At this level you shouldn't just answer the direct question and wait for the next hint. You have to think about how knowing the area of the ellipse helps you solve the problem.

In fact, @gneill already gave you a further hint: Kepler's second law.

The posts that homework helpers give are designed to make you think.
 
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  • #5
PeroK said:
At this level you shouldn't just answer the direct question and wait for the next hint. You have to think about how knowing the area of the ellipse helps you solve the problem.

In fact, @gneill already gave you a further hint: Kepler's second law.

The posts that homework helpers give are designed to make you think.

Sorry about that. I think I found a way to calculate the time period with the help of @gneill and Keplar's second law.

I can divide the total area of the ellipse by the areal velocity ##\frac {r×b} 2## which is equal to ##\frac {mr×v} 2 = \frac L {2m}##. So, ##T = \frac {2\pi abm } L##
 
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  • #6
Well done!

The specific angular momentum, usually denoted by ##h##, and is the angular momentum per unit mass for an orbiting body, has units ##m^2/s##. That's area per second (or in general, unit area per unit time).

If you have the angular momentum, ##L##, for an orbiting object and you also know it's mass ##m##, then the specific angular momentum is ##h = \frac{L}{m}##. So what you've done in your calculation is divide the total area of the ellipse by the specific angular momentum, giving you the period of the orbit.
 
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  • #7
gneill said:
So what you've done in your calculation is divide the total area of the ellipse by the specific angular momentum, giving you the period of the orbit.

Shouldn't the areal velocity be half the specific angular momentum? Because when I calculated the area swept per unit time of an ellipse it came out to be ##\frac {r×v} 2## (area of triangle made up of vectors r and v)
 
  • #8
By your own derivation you found:

##T = \frac {2\pi abm } L ##

Which is:

##2\pi ab \cdot \frac{m}{L}## and since ##\frac{m}{L} = \frac{1}{h}## you end up with:

##T = \frac{2 \pi a b}{h}##
 
  • #9
gneill said:
By your own derivation you found:

##T = \frac {2\pi abm } L ##

Which is:

##2\pi ab \cdot \frac{m}{L}## and since ##\frac{m}{L} = \frac{1}{h}## you end up with:

##T = \frac{2 \pi a b}{h}##

Yes, but the ##2πab## is twice the area of the ellipse.

gneill said:
So what you've done in your calculation is divide the total area of the ellipse by the specific angular momentum, giving you the period of the orbit.

This says that ##T = \frac {πab} h##
 
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  • #10
You're right. You need to divide the area by h/2.
 
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  • #11
We have ##\frac{dA}{dt} = \frac{L}{2m} = \frac h 2##.

Basically, the angular momentum would be the area of a rectangle ##v_{\perp} \times r##, but the area of the ellipse being mapped out is only a triangle.

PS I see we are all in agreement in any case.
 
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1. What is the time period of an object traveling in an elliptical orbit?

The time period of an object traveling in an elliptical orbit is the amount of time it takes for the object to complete one full revolution around its parent body. This is also known as the orbital period or the sidereal period.

2. How is the time period of an object in an elliptical orbit determined?

The time period of an object in an elliptical orbit is determined by the semi-major axis of its orbit and the mass of its parent body. The semi-major axis is the longest radius of the elliptical orbit, and the mass of the parent body affects the strength of the gravitational force that keeps the object in orbit.

3. Does the shape of an object's orbit affect its time period?

Yes, the shape of an object's orbit does affect its time period. In an elliptical orbit, the object travels at different speeds at different points in its orbit. This means that the time it takes to complete one revolution will vary depending on its location in the orbit.

4. How does the distance between an object and its parent body affect the time period of its orbit?

The distance between an object and its parent body does not significantly affect the time period of its orbit. This is because the time period is primarily determined by the semi-major axis of the orbit, rather than the distance between the two bodies.

5. Can the time period of an object in an elliptical orbit be changed?

Yes, the time period of an object in an elliptical orbit can be changed. This can be done by altering the semi-major axis of the orbit or by changing the mass of the parent body. Changes in the gravitational force between the two bodies can also affect the time period of the orbit.

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