Communications satellites are placed in a circular orbit where they stay directly over a fixed point on the equator as the earth rotates. These are called geosynchronous orbits. The altitude of a geosynchronous orbit is 3.58 x 107 m ( 22,000 miles). Correct ▼ Part B ▼ Find the value of g at this altitude. Express your answer with the appropriate units. ►View Available Hint(s) HÅ 9= 0.2242 Submit Previous Answers Part C W = 0 What is the weight of a 2000 kg satellite in a geosynchronous orbit? Express your answer with the appropriate units. View Available Hint(s) O m sec² HÅ 6.0 p ? g w ?

College Physics
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**Educational Content on Geosynchronous Orbits**

**Introduction to Geosynchronous Orbits:**

Communications satellites are strategically placed in a circular orbit that allows them to maintain a fixed position relative to a point on the Earth's equator. This type of orbit is known as a geosynchronous orbit, allowing the satellite to stay synchronized with the Earth's rotation. The typical altitude for such an orbit is approximately \(3.58 \times 10^7 \, \text{m}\) (or about 22,000 miles).

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**Part B: Calculating Gravitational Acceleration (\(g\)) at Geosynchronous Orbit Altitude**

- **Task:** Find the value of \(g\) (gravitational acceleration) at the altitude of a geosynchronous orbit.
- **Provided Calculation:** The value of \(g\) is calculated as \(0.2242 \, \text{m/s}^2\).
- **Instructions:** Express your answer using the appropriate units.

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**Part C: Determining the Weight of a Satellite in Geosynchronous Orbit**

- **Problem Statement:** Calculate the weight of a 2000 kg satellite located in a geosynchronous orbit.
- **Task:** Express the answer with the appropriate units for weight.

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This educational content is designed to inform and guide learners on the concepts and calculations related to the behavior and positioning of satellites within geosynchronous orbits.
Transcribed Image Text:**Educational Content on Geosynchronous Orbits** **Introduction to Geosynchronous Orbits:** Communications satellites are strategically placed in a circular orbit that allows them to maintain a fixed position relative to a point on the Earth's equator. This type of orbit is known as a geosynchronous orbit, allowing the satellite to stay synchronized with the Earth's rotation. The typical altitude for such an orbit is approximately \(3.58 \times 10^7 \, \text{m}\) (or about 22,000 miles). --- **Part B: Calculating Gravitational Acceleration (\(g\)) at Geosynchronous Orbit Altitude** - **Task:** Find the value of \(g\) (gravitational acceleration) at the altitude of a geosynchronous orbit. - **Provided Calculation:** The value of \(g\) is calculated as \(0.2242 \, \text{m/s}^2\). - **Instructions:** Express your answer using the appropriate units. --- **Part C: Determining the Weight of a Satellite in Geosynchronous Orbit** - **Problem Statement:** Calculate the weight of a 2000 kg satellite located in a geosynchronous orbit. - **Task:** Express the answer with the appropriate units for weight. --- This educational content is designed to inform and guide learners on the concepts and calculations related to the behavior and positioning of satellites within geosynchronous orbits.
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