How Do Satellites Stay in Orbit with Centripetal and Gravitational Forces?

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Discussion Overview

The discussion revolves around the mechanics of satellite orbits, specifically the roles of centripetal and gravitational forces, and the concept of centrifugal force. Participants explore the equilibrium state of satellites in orbit, the nature of forces acting on them, and the distinctions between inertial and non-inertial frames of reference.

Discussion Character

  • Technical explanation
  • Conceptual clarification
  • Debate/contested

Main Points Raised

  • Some participants express confusion about how satellites remain in orbit, questioning the equilibrium state involving centripetal and gravitational forces.
  • One participant clarifies that centrifugal force is a pseudo force arising from non-inertial frames of reference, while centripetal force acts towards the center.
  • Another participant emphasizes that satellites are not in equilibrium but are accelerating centripetally, with gravity providing the necessary centripetal force.
  • Several participants discuss the differences between inertial and non-inertial frames of reference, noting that inertial frames comply with Newton's laws, while non-inertial frames introduce pseudo forces.
  • A participant explains that kinematics requires a net inward force for circular motion, and dynamics must provide the source of this force, leading to discussions about the nature of orbits beyond circular paths.
  • There is mention of the limitations of using centripetal force to explain orbits, as it only applies to circular orbits, and deviations lead to elliptical or other types of orbits.

Areas of Agreement / Disagreement

Participants express varying degrees of confusion and differing interpretations regarding the nature of forces in satellite motion. There is no consensus on the role of centrifugal force or the implications of different frames of reference.

Contextual Notes

Participants highlight the complexity of orbital mechanics, noting that assumptions about circular orbits may not hold in all cases, and the discussion reflects a range of understandings about the forces at play.

Elmorshedy
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I'm really confused I have learned at school that the satellite remains in it's orbit because it's in an equilibrium state due to Centripetal force and the gravitational force but how?
Doesn't the centripetal force and the the gravitational force both of them act toward the the earth?
And what is the role of the centrifugal force?
 
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Centrifugal force acts away the center(frugal meaning to flee) while centripetal force acts towards the center(petel means to seek).

Centrifugal force is simply a pseudo force due to use of non inertial frame of reference
 
Elmorshedy said:
I'm really confused I have learned at school that the satellite remains in it's orbit because it's in an equilibrium state due to Centripetal force and the gravitational force but how?
A satellite in orbit is accelerating centripetally--towards the center of the earth--and thus requires a centripetal force. Gravity provides that force. (A satellite is not in equilibrium--it's accelerating.)
 
whats the difference between an inertial and non inertial frame of reference?>
 
Tricks67 said:
whats the difference between an inertial and non inertial frame of reference?>

An inertial frame of reference complies with Newton's laws of motion. This is the case for a non rotating system where the satellite orbits earth. The gravitational force between satellite and Earth is consistent with all three laws. In a rotating frame of reference the first two laws would be violated because the satellite is at rest even though the gravitational force is acting on it. If you assume the first two laws to be fulfilled you will get pseudo forces (e.g. centrifugal force) violating the third law.
 
Elmorshedy said:
I'm really confused I have learned at school that the satellite remains in it's orbit because it's in an equilibrium state due to Centripetal force and the gravitational force but how?
Doesn't the centripetal force and the the gravitational force both of them act toward the the earth?

For now, I'll consider just circular orbits. Kinematics tells us there must be some net force acting on the satellite that is directed radially inward: A centripetal force. Kinematics doesn't say anything about the source of the centripetal force that causes uniform circular motion. A rock tied to a string that is swung around in a circle, a train running on a circular track, a satellite in circular orbit: As far as kinematics is concerned, these are all uniform circular motion.

It is dynamics that explains the source of the force that causes the uniform circular motion. From kinematics, we can derive the magnitude of the centripetal force. The dynamical considerations must necessarily yield the exact same force. So in a sense, this is a "balance" -- but not in the context of Newton's third law. In the case of the orbiting satellite, kinematics says the centripetal force is mv^2/r while Newton's law of gravitation says the gravitational force is GMm/r^2. Equating these requires that v^2=GM/r. What if the dynamics say the force is something else? For example, what if the satellite is moving at some velocity other than the circular orbit velocity?

The answer is simple: You don't get a circular orbit. The satellite instead follows an ellipse, or a parabola, or a hyperbola. Explaining orbits in terms of centripetal force only works in the case of circular orbits. Circular orbits are nice fictions that make the behavior a bit easier to understand. In nature, there is no such thing as a perfectly circular orbit. Deviate one iota from the circular orbit conditions and you no longer have a circular orbit. You still do have an orbit, however. It's just not circular.
And what is the role of the centrifugal force?
In terms of looking at things from the perspective of an inertial frame of reference, there is no such role. There is no centrifugal force in an inertial frame.
 

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