$A$ satellite is launched into a circular orbit of radius $R$ around the Earth. $A$ second satellite is launched into an orbit of radius $1.03 R$. The time period of revolution of the second satellite is larger than the first one approximately by: (in $\%$)

  • A
    $3$
  • B
    $4.5$
  • C
    $9$
  • D
    $2.5$

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