The ratio of PE : KE : TE of an orbiting satellite is [ ]
a) 1 : 2 : 1 b) –2 : 1 : 1 c) –2 : –1 : 1 d) –2 : 1 : –1
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Answer:
d)
Explanation:
total energy is the negative of kinetic energy and double negative of kinetic energy is potential energy
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