Space physics, is this correct?

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Homework Help Overview

The discussion revolves around a physics problem involving a satellite in orbit above Earth's equator, specifically focusing on determining the satellite's altitude and orbital period based on its speed of 7.45 km/s. The relevant equation for orbital speed is mentioned, and participants are exploring the calculations related to the satellite's radius and altitude.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss the calculation of the satellite's radius using the orbital speed and gravitational parameters. There is uncertainty about how to derive the altitude from the radius and whether the calculations are accurate. Some participants question the values used for Earth's radius and mass, and how rounding affects the results.

Discussion Status

Several participants are engaged in verifying calculations and discussing the implications of rounding on their results. There is acknowledgment of approximate correctness in the initial attempts, and some participants are refining their values based on feedback. No explicit consensus has been reached, but productive dialogue is ongoing.

Contextual Notes

Participants are working under the constraints of homework guidelines, which may limit the information they can use or the methods they can apply. There is a focus on ensuring accuracy in calculations and understanding the relationships between the variables involved.

x86
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Homework Statement


A satellite in orbit above Earths equator is traveling at an orbital speed of 7.45 km/s.

a) Determine the altitude of the satellite
b) Determine the satellites period


Homework Equations


v = sqrt(Gm/r)

The Attempt at a Solution


7.45 * 1000 = 7450 m/s

I plugged in the values to that equation and got a radius of 7.1 * 10^6 m.

Now, I'm not sure how to find the altitude, but shouldn't it be the value I found (7.1*10^6m) minus Earth's radius? This gives me the value of 700 km

For b, I'm not sure how to find the period, I tried T = 2pir / V where r was the radius I found and got 5988 seconds. Is this correct?
 
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x86 said:

Homework Statement


A satellite in orbit above Earths equator is traveling at an orbital speed of 7.45 km/s.

a) Determine the altitude of the satellite
b) Determine the satellites period


Homework Equations


v = sqrt(Gm/r)

The Attempt at a Solution


7.45 * 1000 = 7450 m/s

I plugged in the values to that equation and got a radius of 7.1 * 10^6 m.

Now, I'm not sure how to find the altitude, but shouldn't it be the value I found (7.1*10^6m) minus Earth's radius? This gives me the value of 700 km

For b, I'm not sure how to find the period, I tried T = 2pir / V where r was the radius I found and got 5988 seconds. Is this correct?

All of those are approximately correct. You are doing the right things. I get a distance closer to 800km. If you want a closer check you'll need to show all the numbers you are using.
 
Dick said:
All of those are approximately correct. You are doing the right things. I get a distance closer to 800km. If you want a closer check you'll need to show all the numbers you are using.

okay, thank you for your help. I am doing things this way:

a)
7450 = sqrt((6.67*10^-11 * 5.9*10^24/(r)

r = 700 km
 
EDIT: Didn't see this had already been solved; ignore this post.
 
x86 said:
okay, thank you for your help. I am doing things this way:

a)
7450 = sqrt((6.67*10^-11 * 5.9*10^24/(r)

r = 700 km

Nah, that doesn't give you r=700 km. That gives you the radius of the orbit. You have to subtract the radius of Earth to get anything close to 700 km. What did you get for that r, and then what did you use for the radius of earth? As I already said, I think you are doing everything correctly except for maybe rounding off and exact numbers. I really wouldn't worry about it.
 
Last edited:
Dick said:
Nah, that doesn't give you r=700 km. That gives you the radius of the orbit. You have to subtract the radius of Earth to get anything close to 700 km. What did you get for that r, and then what did you use for the radius of earth?

Ah yes, I was rounding the mass of the Earth too much. I get about 810 km now after using a different value of the mass. Thank you
 
x86 said:
Ah yes, I was rounding the mass of the Earth too much. I get about 810 km now after using a different value of the mass. Thank you

Right. You were doing everything correctly. You should pay attention to round-off etc. Very welcome.
 

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