How far above the earth's surface is the satellite orbit?

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SUMMARY

The discussion focuses on calculating the altitude of a satellite's orbit based on its observed position over the Earth's equator. Using the formula T² = 4π²r³/GM, participants determined that the satellite's orbital radius is approximately 2.23 x 10⁷ meters. The key to solving the problem involved accounting for the Earth's rotation and subtracting the Earth's radius from the calculated orbital radius to find the altitude above the surface. The correct approach clarified the importance of visualizing the Earth's rotation during the calculation process.

PREREQUISITES
  • Understanding of gravitational constant (G = 6.67 x 10⁻¹¹ N(m/kg)²)
  • Familiarity with Earth's mass (M = 5.97 x 10²⁴ kg)
  • Knowledge of orbital mechanics and satellite motion
  • Ability to manipulate equations involving time and radius in physics
NEXT STEPS
  • Study the derivation of Kepler's laws of planetary motion
  • Learn about the effects of Earth's rotation on satellite orbits
  • Explore the concept of geostationary orbits and their calculations
  • Investigate the use of simulation tools for orbital mechanics
USEFUL FOR

Students studying physics, aerospace engineers, and anyone interested in satellite technology and orbital dynamics.

Julie323
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Homework Statement



A. Suppose you are at the Earth's equator and observe a satellite passing directly overhead and moving from west to east in the sky. Exactly 15.0 hours later, you again observe this satellite to be directly overhead. How far above the Earth's surface is the satellite's orbit?

B. You observe another satellite directly overhead and traveling east to west. This satellite is again overhead in 15.0 hours. How far is this satellite's orbit above the surface of the earth?



Homework Equations



T2=4π2r3/GM

The Attempt at a Solution


I was not sure how to account for the rotation of the earth, but I tried 15/(1+15/24)=9.23 hours, and then used that for T. I plugged in 6.67*10-11 for G and 5.97 *1024 for M. I solved for r giving me 2.23*107 meters.

Where did I go wrong? Thanks so much for any help!
 
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Suggest you draw a picture of the Earth and show the 15/24th turn the Earth makes. And the turn that the satellite makes going the other way round (for part a).

After you find how far round it goes in 15 hours, use a proportion to find its time to go a full orbit.
 
You got the radius of the orbit. The question is the distance of the satellite from the surface of Earth.

ehild
 
O right! I forgot to subtract the radius of the earth. I got both parts, thank you so much!
 

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