1.

A satellite can be in a geostationary orbit around earth at a distance r from the centre. If the angular velocity of earth about its axis doubles, a satellite can now be in a geostationary orbit around earth if its distance from the centre is

A. \[\frac{r}{2}\]
B. \[\frac{r}{2\sqrt{2}}\]
C. \[\frac{r}{{{\left( 4 \right)}^{1/3}}}\]
D. \[\frac{r}{{{\left( 2 \right)}^{1/3}}}\]
Answer» D. \[\frac{r}{{{\left( 2 \right)}^{1/3}}}\]


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