If height of a satellite from the surface of earth is increased, then its

For a satellite orbiting at height h from earth,
$\mathrm{P}.\mathrm{E}=-\frac{{\mathrm{GM}}_{\mathrm{c}}{\mathrm{m}}_{\mathrm{s}}}{\left({\mathrm{R}}_{\mathrm{c}}+\mathrm{h}\right)},\mathrm{K}.\mathrm{E}=\frac{{\mathrm{GM}}_{\mathrm{c}}{\mathrm{m}}_{\mathrm{s}}}{2\left({\mathrm{R}}_{\mathrm{c}}+\mathrm{h}\right)}\mathrm{\&}\mathrm{T}.\mathrm{E}=-\frac{{\mathrm{GM}}_{\mathrm{c}}{\mathrm{m}}_{\mathrm{s}}}{2\left({\mathrm{R}}_{\mathrm{e}}+\mathrm{h}\right)}$
If h is increased, P.E increases (becomes less negative) K.E decreases T.E increases (becomes less negative)