The total energy of a satellite in orbit is the sum of its kinetic energy and gravitational potential energy. The total energy \( E \) of the satellite is given by:
\[
E = K + U
\]
where:
- \( K \) is the kinetic energy of the satellite,
- \( U \) is the potential energy.
For a satellite at height \( h \), the total energy is negative and is related to the kinetic energy by:
\[
E = - \frac{K}{2}
\]
Thus, if the kinetic energy at height \( h \) is \( k \), then the total energy is:
\[
E = - \frac{k}{2} = -2k
\]
Therefore, the correct answer is \( -2k \).