Radius of Satellite Orbit - 2.1 Days Period

In summary, the conversation discusses finding the radius of a satellite's orbit around the sun, given its period of 2.1 days. The equations used include T=2pi*r/V and v2=GM/r, with the use of units and conversion also mentioned. The use of centripetal force and other equations are also suggested as alternative methods.
  • #1
talaroue
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Homework Statement


A satellite orbits the sun with a period of 2.1 day. What is the radius of its orbit?


Homework Equations



T=2pi*r/V

The Attempt at a Solution



If the time is given in days I have to convert to seconds right? Also how would I find velocity would I use V=square root (Gms/r)? For some reason gravity has got me confused
 
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  • #2
If the time is given in days I have to convert to seconds right?

That would be useful, as the units of G involve seconds.

Recognize that

v = 2πr/T

and m*v2/r = GMm/r2 or as you have written

v2 = GM/r

Combine with

v2 = (2πr/T)2 = GM/r
 
  • #3
so that actually gets rid of the actual speed of the object as far as usefulness in the equation.
 
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  • #4
Alternatively you could also use [itex]m \omega^2 r[/itex] as the centripetal force.
 
  • #5
That is an awesome way to check yourself since he wants the work done by using the gravity equations but just to double check myself I can use that! Thats a big help also thank you!
 
  • #6
talaroue said:
so that actually gets rid of the actual speed of the object as far as usefulness in the equation.

Well ... yes. They only ask you for the radius. Were you invested in wanting to find the speed?
 
  • #7
No, but I just didn't even think about using the equations that deal with velocity. So I was getting lost. Is there another way to go about this problem?
 
  • #8
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FAQ: Radius of Satellite Orbit - 2.1 Days Period

What is the radius of the satellite orbit with a 2.1 day period?

The radius of the satellite orbit with a 2.1 day period is approximately 22,236 kilometers.

How is the radius of a satellite orbit calculated?

The radius of a satellite orbit is calculated using the following formula: r = (G*M*T^2/4π^2)^(1/3), where r is the radius, G is the gravitational constant, M is the mass of the central body, and T is the orbital period in seconds.

Is the radius of a satellite orbit constant?

No, the radius of a satellite orbit is not constant. It can change depending on various factors such as the gravitational pull of other objects and atmospheric drag.

Can the radius of a satellite orbit change over time?

Yes, the radius of a satellite orbit can change over time due to various factors such as gravitational pull, atmospheric drag, and changes in the speed or direction of the satellite.

What is the significance of a 2.1 day period for a satellite orbit?

A 2.1 day period for a satellite orbit is significant because it is considered a short period orbit, which means the satellite completes one orbit around its central body in 2.1 days. This can have implications for the satellite's speed, altitude, and coverage area.

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