$A$ satellite is to be placed in an equatorial geostationary orbit around the Earth for communication purposes. The height of such a satellite is $(M_{E} = 6 \times 10^{24} \,kg, R_{E} = 6400 \,km)$.

  • A
    $3.57 \times 10^8 \,m$
  • B
    $3.57 \times 10^7 \,m$
  • C
    $3.57 \times 10^5 \,m$
  • D
    $3.57 \times 10^6 \,m$

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