Grade 12 Physics: Satellite Question | Distance & Speed

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In summary, satellites maintain their distance from the Earth by orbiting at a specific altitude and speed, known as a geostationary orbit. The speed of a satellite in orbit is affected by various factors, including its mass, the mass of the object it is orbiting, and the distance between them. The distance of a satellite from the Earth can be calculated using a formula that takes into account the gravitational force between the satellite and the Earth. There are two types of orbits, geostationary and polar, which are used for different purposes. The speed of a satellite also affects its orbit, as it can change the orbital radius and shape.
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AngularVelocity
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Hello I am in Grade 12 Physics and I would like some help on this problem as soon as possible. Thanks.

A satellite travels directly above the equator, in the same direction as the Earth's spin, and completes two orbits of the Earth in one day. Determine the distance above the Earth's surface, and the speed, of the satellite.
 
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Welcome to the forum. We ask that you at least try to post some ideas about solution to the problem. Do you know equation for uniform circular motion that relates velocity and distance?
 
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Hello, thank you for reaching out for help with this physics problem. To determine the distance above the Earth's surface and the speed of the satellite, we need to use some key equations and principles from physics.

First, let's define some variables. Let's call the distance above the Earth's surface "h" and the speed of the satellite "v". We also know that the satellite completes two orbits in one day, which means it travels a distance equal to the circumference of the Earth twice in one day.

Using the equation for circumference, we can say that:

2πr = 2h

Where r is the radius of the Earth. We can rearrange this equation to solve for h:

h = πr

Next, we can use the equation for the speed of an object in circular motion:

v = 2πr/T

Where T is the time it takes to complete one orbit. Since the satellite completes two orbits in one day, T is equal to 12 hours or 43200 seconds. Substituting this into the equation, we get:

v = 2πr/43200

Now, we can substitute our value for h (πr) into this equation:

v = 2(πr)/43200

Simplifying, we get:

v = πr/21600

We can also use the equation for the distance an object travels in circular motion:

d = vt

Where d is the distance, v is the speed, and t is the time. In this case, the distance is equal to the circumference of the Earth, which we know is 2πr. Substituting this into the equation, we get:

2πr = v(43200)

Simplifying, we get:

r = v(43200)/2π

Now, we can substitute this value for r into our equation for h:

h = π(v(43200)/2π)

Simplifying, we get:

h = 21600v

Therefore, we have two equations that relate h and v:

h = πr

h = 21600v

We can solve for h in the second equation and substitute it into the first equation to get:

πr = 21600v

πr = 21600(πr)

Simplifying, we get:

r = 21600v

Now, we can substitute this value for r into our equation for v:

 

1. How do satellites maintain their distance from the Earth?

Satellites maintain their distance from the Earth by orbiting at a specific altitude and speed. This is known as a geostationary orbit, where the satellite's orbital period matches the Earth's rotation, allowing it to remain in the same position relative to the Earth's surface.

2. What factors affect the speed of a satellite in orbit?

The speed of a satellite in orbit is affected by several factors, including the mass of the satellite, the mass of the object it is orbiting, and the distance between them. The speed also depends on the altitude of the satellite, as well as the gravitational force acting on it.

3. How is the distance of a satellite from the Earth calculated?

The distance of a satellite from the Earth can be calculated using the formula d = √(GM/r), where G is the gravitational constant, M is the mass of the Earth, and r is the distance between the satellite and the center of the Earth. This formula takes into account the gravitational force between the satellite and the Earth.

4. What is the difference between a geostationary and a polar orbit?

A geostationary orbit is one where the satellite remains in the same position relative to the Earth's surface, while a polar orbit is one where the satellite passes over the Earth's poles. A geostationary orbit is used for communication and weather satellites, while a polar orbit is used for remote sensing and mapping satellites.

5. How does the speed of a satellite affect its orbit?

The speed of a satellite affects its orbit in several ways. A higher speed will result in a larger orbital radius, while a lower speed will cause the satellite to orbit closer to the Earth. Additionally, a change in speed can also change the shape of the orbit, for example, increasing the speed can cause the orbit to become more elliptical.

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