When a satellite is moved from one stable circular orbit to another higher stable circular orbit, the physical quantity that increases is

$\text{L}=\sqrt{{\text{GMm}}^2\left(\text{R}+\text{h}\right)}$

$\text{L}\propto \sqrt{\text{R}+\text{h}}$

If satellite moved from lower orbit to higher orbit Angular momentum is increased. But angular velocity, KE and linear orbital speed decreases