Period of satellite in circular orbit

In summary, the period of a satellite in circular orbit 14120.3 km above the surface of a planet with a radius of 4190 km and an acceleration of gravity of 6.5 m/s^2 is 46084.2 seconds.
  • #1
bmoore509
66
0

Homework Statement



Given: G = 6.67259 × 10−11 Nm2/kg2
The acceleration of gravity on the surface
of a planet of radius R = 4190 km is 6.5 m/s2.
What is the period T of a satellite in circu-
lar orbit h = 14120.3 km above the surface?
Answer in units of s.

Homework Equations


a=G(m/r^2)
T = 2πR/V
V = sqrt(GM/R)
T = 2πR/sqrt(GM/R)

The Attempt at a Solution



My formulas might be incorrect but I really don't think they are. Yet I can't seem to get the right answer.

6.5 m/s2 = (6.67259 × 10−11 Nm2/kg2) (m/((4190000m+14120300m)^2))
m=3.265952291x1025

T = 2piR/sqrt(GM/R)

= 2*pi*(4190000+14120300)/ sqrt((6.67259 × 10−11 *3.265952291x1025)/(4190000m+14120300m)

=1054559091seconds

But that answer isn't right. Any help please?
 
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  • #2
The equations look correct, so I guess you made a calculation error in the last expression.

Note, that the period usually is written with the two R's combined into one, like
[tex]T = 2\pi\sqrt{\frac{R^3}{GM}}[/tex]
 
  • #3
bmoore509 said:
6.5 m/s2 = (6.67259 × 10−11 Nm2/kg2) (m/((4190000m+14120300m)^2))

6.5 m/s^2 is the acceleration at the surface of the planet, r=4190 km.

ehild
 
  • #4
I redid my work using the formula as you wrote it.

T = 2pi (sqrt((R^3)/GM))

R3= (4190000+14120300)3 = 6.138840926x1021

G*M = (6.6725x10-11)*(3.265952291x1025)=2.17923606x1015

sqrt ( R3/(G*M) = sqrt (6.138840926x1021/2.17923606x1015) = sqrt (281696.23) = 1678.382921

T=2pi(sqrt(r^3/GM)
= 2*pi*1678.382921 = 10545.59091

Which isn't the right answer. Can you tell me where I'm going wrong?
 
  • #5
Oh! Thank you! Let me rework this then.
 
  • #6
T = 2pi (sqrt((R^3)/GM))

R3= (4190000+14120300)3 = 6.138840926x1021

G*M = (6.67259x10-11)*(1.710200237x1024)=1.1411465x1014

sqrt ( R3/(G*M) = sqrt (6.138840926x1021/1.1411465x1014) = sqrt (53795379.7) = 7334.533366

T=2pi(sqrt(r^3/GM)
= 2*pi*7334.533366 = 46084.23228


Does that look correct?
 
  • #7
Yes, if you mean seconds. But use only 6 significant digits, and write out the units.

ehild
 
  • #8
ehild said:
6.5 m/s^2 is the acceleration at the surface of the planet, r=4190 km.

Ah, I missed that the height wrongly was "included" in the calculation of planet mass. My apologies to the original poster.
 

What is the definition of period of satellite in circular orbit?

The period of a satellite in circular orbit is the time it takes for the satellite to complete one full orbit around its parent body, such as a planet or moon.

How is the period of satellite in circular orbit calculated?

The period of a satellite in circular orbit can be calculated using the following formula: T = 2π√(r³/GM), where T is the period in seconds, r is the distance between the satellite and parent body in meters, G is the gravitational constant, and M is the mass of the parent body in kilograms.

What factors affect the period of satellite in circular orbit?

The period of a satellite in circular orbit is affected by the distance between the satellite and parent body, the mass of the parent body, and the gravitational constant. It is also affected by any external forces acting on the satellite, such as atmospheric drag or gravitational pull from other bodies.

How does the period of satellite in circular orbit relate to its speed?

The period of a satellite in circular orbit is directly related to its speed. As the speed of the satellite increases, the period decreases and vice versa. This is because a satellite with a higher speed will cover a larger distance in the same amount of time, resulting in a shorter period.

Why is the period of satellite in circular orbit important?

The period of a satellite in circular orbit is important because it determines the frequency and timing of its orbits. This information is crucial for satellite operators to plan and maintain the orbit of the satellite for various applications, such as communication, navigation, and scientific research.

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