Решение до правки #6939 от , автор astrosander. Это не текущая версия.
For problem $2.6.37$
The Molniya-1 communications satellite has a perigee over the southern hemisphere of the Earth at an altitude of about 500 km, and an apogee at an altitude of about 40,000 km over the northern hemisphere. What is the ratio of the angular velocities of rotation of this satellite at perigee and apogee?

Solutions of Savchenko Problems in Physics

Aliaksandr Melnichenka
October 2023

    <h3 id="back-link"><a href="/#2.6">$\leftarrow$Back</a></h3>

    <h3> Statement </h3>
    <p>
        $2.6.37.$ The Molniya-1 communications satellite has a perigee over the southern hemisphere of the Earth at an altitude of about $500$ km, and an apogee at an altitude of about $40,000$ km over the northern hemisphere. What is the ratio of the angular velocities of rotation of this satellite at perigee and apogee?

For problem

    <h3>Solution</h3>
    <p>

Sattelite at apogee and perigee

Law of energy preservation

Conservation of angular momentum

From where velocity at closest position to the planet, at perigee

Let's substitute value of to :

From where, we could value of the velocity at farthest position to the planet, at apogee

Considering dependence from , we obtain

By definition of angular velocity


The desired relationship could be found by dividing one equation on another

Considering the radius of the Earth


After substituting into , we are getting

    </p>

    <h4>Answer</h4>
    <p>
        $$\frac{\omega_p}{\omega_a}\approx 45$$
    </p>

    <p style="text-align: right; font-style: italic; font-size: 14;">
      Almaskhan Arsen<br>
    </p>


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