For a satellite to orbit around the earth, which of the following must be true ?
It must be above the equator at some time
Its period of rotation must be $> 2\pi \sqrt{R/g} $ where $R$ is radius of earth
Its height above the surface cannot exceed $36,000 \,km$
$(A)$ and $(B)$ both
If the earth stops rotating, the value of $‘g’$ at the equator will
The diameters of two planets are in the ratio $4 : 1$ and their mean densities in the ratio $1 : 2$. The acceleration due to gravity on the planets will be in ratio
The acceleration due to gravity at height $h$ above the earth if $h \ll R$ (radius of earth) is given by
If $M$ the mass of the earth and $R$ its radius, the ratio of the gravitational acceleration and the gravitational constant is
The height of the point vertically above the earth’s surface, at which acceleration due to gravity becomes $1\%$ of its value at the surface is (Radius of the earth $= R$)