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Hitung laju linear ,v satelit C . Apabila jejari orbit ,r satelit C adalah 7050 km

To calculate the linear velocity (\(v\)) of satellite C, we can use the formula for orbital velocity derived from Newton's law of gravitation:

\[
v = \sqrt{\frac{GM}{r}}
\]

Where:
- \( G = 6.67 \times 10^{-11} \, \text{Nm}^2/\text{kg}^2 \) (gravitational constant),
- \( M = 5.97 \times 10^{24} \, \text{kg} \) (mass of the Earth),
- \( r = 7050 \, \text{km} = 7.05 \times 10^6 \, \text{m} \) (radius of the satellite's orbit from Earth's center).

Let's plug in the values and calculate the velocity.The linear velocity (\(v\)) of satellite C is approximately \(7515.46 \, \text{m/s}\).

Would you like more details or have any questions? Here are five related questions to explore further:

1. How does changing the altitude of the satellite affect its orbital speed?
2. What is the difference between linear velocity and angular velocity for a satellite?
3. How do gravitational forces influence the satellite's orbit?
4. Can this formula be used for satellites orbiting other planets?
5. How would the satellite's velocity change if Earth's mass were different?

**Tip:** The higher a satellite orbits, the slower its orbital speed becomes due to the increased distance from Earth's center.

Hitung laju linear, v satelit C. Apabila jejari orbit, r satelit C adalah 7050 km.

Learn how to calculate the linear velocity of a satellite orbiting the Earth at a height of 7050 km. This problem covers key concepts in orbital mechanics, including gravitational force, and the formula for orbital velocity using Newton's Law of Gravitation.

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