An engineer wants a satellite to orbit the earth with a period of 28 hours. Hint: You need to find an equation for r in terms of givens (T, M and G only). Start by setting your two equations for acceleration equal. Then rearrange the orbital period equation to solve for T and substitue. Finally, solve for r and plug in! You may enter answers in scientific notation as shown: 1.23 x 105 - 1.23e5 At what orbital radius must the satellite orbit? m How far is this above the earth's surface? m At what speed does the satellite need to orbit? m/s 8 earth data mass: 5.97 x 1024kg radius: 6.37 x 106m

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**Title: Calculating the Orbital Requirements for a Satellite with a 28-Hour Period**

**Objective:** Determine the orbital radius and speed for a satellite to orbit the Earth with a period of 28 hours.

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**Instructions:**

An engineer aims to position a satellite in orbit around Earth with a specified orbital period of 28 hours. To achieve this, you'll need to derive the equation for the orbital radius \( r \) using the given values (orbital period \( T \), Earth's mass \( M \), and gravitational constant \( G \)). Follow these steps:

1. Set the equations for gravitational and centripetal acceleration equal.
2. Rearrange the orbital period equation to solve for \( T \), and substitute the values.
3. Calculate the orbital radius \( r \) and plug in your values.

*Note:* You may enter answers in scientific notation (e.g., \( 1.23 \times 10^5 \) as 1.23e5).

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**Questions:**

1. **At what orbital radius must the satellite orbit?**  
   Enter your answer: [______] m

2. **How far is this above the Earth's surface?**  
   Enter your answer: [______] m

3. **At what speed does the satellite need to orbit?**  
   Enter your answer: [______] m/s

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**Diagram Explanation:**

The diagram illustrates a satellite in orbit around Earth. It highlights the following:

- The satellite’s orbit is depicted as a gray dashed circle.
- The line labeled \( r \) represents the orbital radius from the center of the Earth to the satellite.
- **Earth data:**  
  - Mass: \( 5.97 \times 10^{24} \) kg  
  - Radius: \( 6.37 \times 10^6 \) m

Using the values provided, calculate the necessary orbital parameters to maintain a 28-hour orbit.
Transcribed Image Text:**Title: Calculating the Orbital Requirements for a Satellite with a 28-Hour Period** **Objective:** Determine the orbital radius and speed for a satellite to orbit the Earth with a period of 28 hours. --- **Instructions:** An engineer aims to position a satellite in orbit around Earth with a specified orbital period of 28 hours. To achieve this, you'll need to derive the equation for the orbital radius \( r \) using the given values (orbital period \( T \), Earth's mass \( M \), and gravitational constant \( G \)). Follow these steps: 1. Set the equations for gravitational and centripetal acceleration equal. 2. Rearrange the orbital period equation to solve for \( T \), and substitute the values. 3. Calculate the orbital radius \( r \) and plug in your values. *Note:* You may enter answers in scientific notation (e.g., \( 1.23 \times 10^5 \) as 1.23e5). --- **Questions:** 1. **At what orbital radius must the satellite orbit?** Enter your answer: [______] m 2. **How far is this above the Earth's surface?** Enter your answer: [______] m 3. **At what speed does the satellite need to orbit?** Enter your answer: [______] m/s --- **Diagram Explanation:** The diagram illustrates a satellite in orbit around Earth. It highlights the following: - The satellite’s orbit is depicted as a gray dashed circle. - The line labeled \( r \) represents the orbital radius from the center of the Earth to the satellite. - **Earth data:** - Mass: \( 5.97 \times 10^{24} \) kg - Radius: \( 6.37 \times 10^6 \) m Using the values provided, calculate the necessary orbital parameters to maintain a 28-hour orbit.
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