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+ <meta name="description" content="At what speed should a satellite fly in order to move in a circle while "falling" to the Earth with acceleration g? Assume the orbit radius R = 6400 km and g = 10 \frac{m}{s^2}.">
+ <meta name="author" content="Aliaksandr Melnichenka">
+ <meta name="date" content="2023-10" scheme="YYYY-MM">
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+ <header style="text-align:center;">
+ <h2>Solutions of Savchenko Problems in Physics</h2>
+ <p class="author">
+ Aliaksandr Melnichenka <br/>
+ October 2023
+ </p>
+ </header>
+
+ <h3 id="back-link"><a href="../../#1.3">$\leftarrow$Back</a></h3>
+
+ <h3> Statement </h3>
+ <p>
+ $1.3.21.$ At what speed should a satellite fly in order to move in a circle while "falling" to the Earth with acceleration $g$? Assume the orbit radius $R = 6400$ km and $g = 10$ $\frac{m}{s^2}$.
+ </p>
+
+ <h3>Solution</h3>
+ <p>
+ <p>
+Equilibrium condition: centrifugal force compensates for gravitational force
+</p>
+<p class="exp">
+$$ mg = \frac{mv^2}{R} $$
+</p>
+<p>
+Where, the desired speed
+</p>
+<p class="exp">
+$$v = \sqrt{gR}=8\text{ km/s}$$
+</p>
+ </p>
+
+ <h4>Answer</h4>
+ <p>
+ $$v = \sqrt{gR}=8\text{ km/s}$$
+ </p>
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