What is the Height of the International Space Station Above the Earth's Surface?

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SUMMARY

The height of the International Space Station (ISS) above the Earth's surface is approximately 1196 kilometers, calculated using the formula h = [(T^2)*g / 4*pi*pi] - Re, where T is the orbital period and Re is the Earth's radius. The ISS completes 15.65 revolutions daily, equating to an orbital period of 5520.77 seconds. However, the calculation must account for the variation in gravitational acceleration at such altitudes, necessitating the use of the formula g = G(M_Earth / r^2) instead of the standard 9.8 m/s². This adjustment is crucial for accurate height determination.

PREREQUISITES
  • Understanding of circular motion and centripetal force
  • Familiarity with gravitational equations, specifically g = G(M_Earth / r^2)
  • Knowledge of orbital mechanics, including Kepler's laws
  • Basic proficiency in algebra and unit conversion
NEXT STEPS
  • Research gravitational variations at different altitudes using g = G(M_Earth / r^2)
  • Study Kepler's laws of planetary motion for further insights into orbital mechanics
  • Explore the implications of centripetal acceleration in satellite motion
  • Learn about the calculation of orbital periods and their relation to satellite heights
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Aerospace engineers, physics students, and anyone interested in satellite dynamics and orbital mechanics will benefit from this discussion.

Chan M

Homework Statement


The International Space Station, launched in 1998, makes 15.65 revolutions around the Earth each day in a circular orbit. Find the height of the space station (in kilometers) above the earth’s surface.

Homework Equations


T = (2*pi*r) / v
r - radius, distance between center of Earth and the station
r = Re + h
Re - radius of earth
h = height above ground
Find h

The Attempt at a Solution


So there is only one force acting on the station, which is gravity. Acceleration due to gravity is also centripetal acceleration. Gravity is the centripetal force.

15.65 revolution each day is one revolution every 5520.77 seconds

Fg = m*Ac
mg = m * (v^2 / r)
g = v^2 / r
g = [ (2*pi*r) / T ]^2 / r
g = 4*pi*pi*r / T^2
h = [(T^2)*g / 4*pi*pi ] - Re
h = [(5520.77^2)*9.8 / 4*pi*pi ] - (6.37 * 10^6)
h =
upload_2017-10-2_21-38-59.png
(this is what I put in the calculator)
h = 1195987.99 meters
h = 1196 km

This is not the correct answer, I know the correct answer, I just don't know how to get it or what I'm doing wrong. Thanks!
 

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Gravity is weaker that high up so ##g=9.8##m/s won't work. You need
$$g=G\frac{M_{Earth}}{r^{2}}$$
 
can one use Kepler's 3rd law?
 

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