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

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Homework Help Overview

The problem involves determining the altitude of satellites orbiting the Earth based on observational data regarding their positions over time. The context includes the effects of Earth's rotation on satellite observations and the application of gravitational equations.

Discussion Character

  • Exploratory, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants discuss how to account for Earth's rotation when calculating the satellite's orbital radius. There are attempts to use gravitational equations and observational data to derive the altitude of the satellites.

Discussion Status

Some participants have provided suggestions for visualizing the problem, such as drawing diagrams to clarify the relationship between the Earth's rotation and the satellite's movement. There is acknowledgment of a miscalculation regarding the radius of the Earth that affects the final altitude determination.

Contextual Notes

Participants are working under the constraints of a homework assignment, which may impose specific methods or approaches to solving the problem. There is an emphasis on understanding the relationship between the satellite's orbital period and the Earth's rotation.

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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