Kinetic energy of the satellite, $K = \frac{GMm}{2r}$
Potential energy of the satellite, $U = -\frac{GMm}{r}$
Total energy of the satellite, $E = -\frac{GMm}{2r}$
In figure,
Variation of $K$ with $r$ is shown by curve $A$.
Variation of $U$ with $r$ is shown by curve $B$.
Variation of $E$ with $r$ is shown by curve $C$.