Calculating Satellite Orbital Radius from Period

In summary, the conversation discusses finding the orbital radius of a satellite based on its orbital period. The formula used is r = (t / (2pi)) ^ {2 / 3} * (G * M) ^ {1 / 3}, and after some confusion and calculation errors, the final answer is determined to be 6942704.95871195 meters.
  • #1
Format
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I need to find the orbital radius of a satilite, while only knowing its orbital period.


i tried..

a = 4π²r/T²
Fnet = Fg
a = Gm/r²

Gm/r² = 4π²r/T²
r = cuberoot(T²Gm/4π²)

didnt work out..
 
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  • #2
What??What are u saying by "didn't work out" ?Your formula is okay for a circular orbit...

Daniel.
 
  • #3
Hmm..i keep getting 3.19x10^7

but the answer is 6.95x10^6
 
  • #4
Try this:
From the period, find the speed (simple calculation). Then, use this formula to find the radius:

[tex]v=\sqrt{\frac{Gm_E}{r}}[/tex]
 
  • #5
hmm, in order to find the speed don't you need the radius?

like v = 2πr/T ?
 
  • #6
Format said:
Hmm..i keep getting 3.19x10^7

but the answer is 6.95x10^6

I see nothing wrong with your approach. Why don't you post the numbers given (actually just the value of T), so we can check the calculation ?
 
  • #7
Oh yeah. Just give me a second to think about this...
 
  • #8
i guess that would help lol..

A satilite has an orbital period of T = 5760 s. What is the average orbital radius of its orbit?
 
Last edited:
  • #9
Format said:
Hmm..i keep getting 3.19x10^7

but the answer is 6.95x10^6

Please post the initial text of the problem...

Daniel.
 
  • #10
I get 6.95 * 10^6 m.

You must have made a calculation error. Show us your working, and we'll show you what's wrong.
 
  • #11
Format said:
I need to find the orbital radius of a satilite, while only knowing its orbital period.


i tried..

a = 4π²r/T²
Fnet = Fg
a = Gm/r²

Gm/r² = 4π²r/T²
r = cuberoot(T²Gm/4π²)

didnt work out..
I did exactly that and got 6.95 x 10^6 m. Maybe you punched in the numbers wrong...
 
  • #12
well isn't this anoying..
k i put the cube root of..

( (5760²)(6.67x10^(-11)(5.98x10^24) ) / 4π²
 
  • #13
wait...i see a missing bracket, one sec lol

damn didnt make a difference...wut am i doing wrong?
 
Last edited:
  • #14
Without using the calculator i could show that the result is
[tex] 6\cdot 10^{6} <r<7\cdot 10^{6} [/tex]

:wink:

So how about pluggng in the numbers properly...

Daniel.
 
  • #15
Format said:
well isn't this anoying..
k i put the cube root of..

( (5760²)(6.67x10^(-11)(5.98x10^24) ) / 4π²
yeah, you're missing a bracket. :tongue2:
 
  • #16
ive done this like 10 times now and added the brackets...still gettin 3.2x10^7 lol
 
  • #17
OK, show me exactly what you typed into you calculator.
 
  • #19
Okay:U need to take 3-rd order root from:
[tex]\frac{(5.76)^{2}\cdot 1000^{2}\cdot 6.67\cdot 10^{-11}\cdot 5.98\cdot 10^{-24}}{4\pi^{2}} \simeq 300\cdot 10^{18} [/tex]

Daniel.
 
  • #20
ok i got it to work haha, thanks for the help guys
 
  • #21
[tex]r = (t / (2pi)) ^ {2 / 3} * (G * M) ^ {1 / 3}[/tex]
r = 6942704.95871195 meters
 

1. How do you calculate the orbital radius of a satellite from its period?

To calculate the orbital radius of a satellite from its period, you can use the following equation:

Orbital radius (r) = (Gravitational constant * Mass of central body) / (4π² * Period²)

2. What is the unit of measurement for the orbital radius?

The unit of measurement for the orbital radius is typically meters (m) or kilometers (km), depending on the size of the orbit.

3. Can the orbital radius change over time?

Yes, the orbital radius can change over time due to various factors such as atmospheric drag, gravitational pull from other celestial bodies, and propulsion from the satellite itself.

4. How accurate is the calculation of orbital radius from period?

The calculation of orbital radius from period is typically accurate as long as the satellite is in a stable orbit and there are no major external forces affecting its orbit. However, small variations or uncertainties in the mass of the central body or the gravitational constant can affect the accuracy of the calculation.

5. Can the orbital radius of a satellite be determined from its altitude?

Yes, the orbital radius of a satellite can be determined from its altitude using the equation: Orbital radius (r) = Altitude (h) + Radius of central body. However, this method assumes a circular orbit and may not be as accurate as using the period to calculate the orbital radius.

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