$$R$$ is the radius of the earth and $$\omega $$ is its angular velocity and $${g_p}$$ is the value of $$g$$ at the poles. The effective value of $$g$$ at the latitude $$\lambda = {60^ \circ }$$ will be equal to
If $$g$$ is the acceleration due to gravity on the earth’s surface, the gain in the potential energy of an object of mass $$m$$ raised from the surface of the earth to a height equal to the radius $$R$$ of the earth, is-
A geo-stationary satellite orbits around the earth in a circular orbit of radius $$36,000 \,km.$$ Then, the time period of a spy satellite orbiting a few hundred km above the earth's surface $$\left( {{R_{earth}} = 6400\,km} \right)$$ will approximately be-