What happens to the speed and time of a satellite orbiting closer to Earth?

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When a satellite moves to a lower orbit closer to Earth, its speed increases while the time taken for one complete orbit decreases. The gravitational force acting on the satellite increases as it approaches Earth, which affects its acceleration and angular velocity. The relationship between acceleration, angular velocity, and radius is described by the equations a = ω²r and a = (2π/T)²/r, indicating that as the radius decreases, the period of orbit also decreases. The discussion emphasizes that gravity acts as a force even when the satellite is not in contact with other objects, validating the application of F = ma in this context. Understanding these dynamics can be further clarified by comparing orbital velocities at varying altitudes.
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Homework Statement


A satellite orbiting the Earth moves to an orbit which is closer to the earth.
What happens to the speed and the time it takes for the one orbit of the Earth.

Homework Equations



It is circular motion so I will use [/B]
a=ω^2(r) a=(2π/T)^2/r

The Attempt at a Solution


If the r is decreasing, then the value of a is also decreasing this means that period will increase as it is inversely proportional.

Can someone help me out?
 
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Kajan thana said:
a=ω^2(r) a=(2π/T)^2/r
In the first equation, r is in the numerator on the right-hand side. But in the second equation you have moved r into the denominator. Did you mean to do that?
If the r is decreasing, then the value of a is also decreasing... .
Can you justify this statement?
 
TSny said:
In the first equation, r is in the numerator on the right-hand side. But in the second equation you have moved r into the denominator. Did you mean to do that?
Can you justify this statement?
a is proportional to r by the omega constant. If I increase a then r will also increase.
 
Is it correct to assume that ω is constant when you switch orbits?
 
yes, the omega will change also but I am still clueless.
 
It will help to consider where the acceleration is coming from. When the satellite is in a circular orbit, what force acts on the satellite?
 
Gravity is acting in between them two.
 
I don't know if I am on the right line.
 
Yes, the force acting on the satellite is the force of gravity. If the satellite is moved closer to the earth, does the force of gravity on the satellite increase or decrease?
 
  • #10
Increases, is ma is proportional to 1/r^2
 
  • #11
Kajan thana said:
Increases, is ma is proportional to 1/r^2
Yes. Good.
 
  • #12
how will I still find out if the period is increasing or decreasing?
 
  • #13
Look at your equation a = ω r. [EDIT: Meant to write a = ω2 r] If you switch to an orbit closer to the earth, what happens to r? What happens to a? What happens to ω?
 
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  • #14
yes but like what you said the r is not a constant.
 
  • #15
or is the R constant after it has moved closer.
 
  • #16
Using the formula a = ω2 r, you should be able to figure out if ω increases or decreases when the satellite is moved into an orbit closer to the earth.
Does the left side of the equation get larger or smaller?
 
  • #17
Left hand side get larger, I thought in order to look at proportionality something need to remain constant, isn't that the case?

And also I want make sure if we are allowed to relate MA with gravity because my teacher told me MA can be only used when it is contact with something else.
 
  • #18
Kajan thana said:
Left hand side get larger, I thought in order to look at proportionality something need to remain constant, isn't that the case?
In the equation a = ω2 r, all three quantities a, ω, and r change when moving to an orbit closer to the earth. Nevertheless, you can still use the equation to deduce what happens to ω.

And also I want make sure if we are allowed to relate MA with gravity because my teacher told me MA can be only used when it is contact with something else.
Gravity is an "action-at-a-distance" force. It can act on an object even when the object is not in contact with any other object. The satellite is a good example. When it is in orbit, it is not in contact with any other object. Yet, there is the force of gravity acting on the satellite.
F = ma will apply to this situation.
 
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  • #19
It makes sense.
Thanks for the help.
 
  • #20
If it helps then try thinking about the extremes
Try thinking about or solving the velocity required to orbit the Earth a meter above the surface and the velocity required to orbit the Earth far out like 1000 km away
Compare the two results and see what relationship they hold
 
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