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<meta name="description" content="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?">
<meta property="og:title" content="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?">
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<meta property="og:description" content="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?">
<title>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?</title>
$2.6.37.$ 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?
<small>All rights belong to the authors. <br> Commercial use of materials - with the written permission of the authors. <br> alex@savchenkosolutions.com <br></small>
<meta name="keywords" content="Savchenko Problems in Physics, Savchenko solutions, physics problems, physics olympiad preparation, IPhO, Jaan Kalda">
<meta name="keywords" content="Savchenko Problems in Physics, Savchenko solutions, physics problems, physics olympiad preparation, IPhO, Jaan Kalda">
<meta name="description" content="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?">
<meta name="description" content="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?">
<meta property="og:title" content="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?">
<meta property="og:title" content="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?">
<meta property="og:image" content="img/logo.png">
<meta property="og:image" content="img/logo.png">
@@ -14,9 +14,9 @@
<meta property="og:description" content="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?">
<meta property="og:description" content="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?">
<title>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?</title>
<title>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?</title>
$2.6.37.$ 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?
$2.6.37.$ 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?
<small>All rights belong to the authors. <br> Commercial use of materials - with the written permission of the authors. <br> alex@savchenkosolutions.com <br></small>
<small>All rights belong to the authors. <br> Commercial use of materials - with the written permission of the authors. <br> alex@savchenkosolutions.com <br></small>