A planet revolves about the sun in elliptical orbit. The areal velocity $$\left( {\frac{{dA}}{{dt}}} \right)$$ of the planet is $$4.0 \times {10^{16}}\,{m^2}/s.$$ The least distance between planet and the sun is $$2 \times {10^{12}}m.$$ Then the maximum speed of the planet in $$km/s$$ is
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-