Calculating Satellite Orbital Radius from Period

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SUMMARY

The discussion focuses on calculating the orbital radius of a satellite given its orbital period using the formula r = cuberoot(T²Gm/4π²). The participants clarify that the orbital period T is 5760 seconds, and the gravitational constant G is 6.67 x 10^(-11) m³/kg/s², with Earth's mass m_E being 5.98 x 10^24 kg. The correct calculation yields an orbital radius of approximately 6.95 x 10^6 meters, highlighting the importance of accurate input and proper bracket usage in calculations.

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

Daniel.
 
Hmm..i keep getting 3.19x10^7

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

v=\sqrt{\frac{Gm_E}{r}}
 
hmm, in order to find the speed don't you need the radius?

like v = 2πr/T ?
 
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 ?
 
Oh yeah. Just give me a second to think about this...
 
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:
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
6\cdot 10^{6} <r<7\cdot 10^{6}

: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. :-p
 
  • #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:
\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}

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

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