Someone help !

T Satellite Moon (space shuttle) 2/4 - Orbital Radius (r satellite) = Rs Rearth R. Orbital Radius (r moon) = Rmoon Rmoon Earth c) What velocity (V) is required to for this Satellite with a mass of 2,030 kg orbit to stay at an orbital radius of 2.66 x 10^5 m? Remember: Mass of Earth (M) = 5.97 x 10*24 kg V GM Gravitational Constant (G) = 6.67 x 10*-11 m 3/kg*s-2 Velocity( V) = m/s Note for parts (c) and (d): Type your answers in scientific notation, similar to the values provided above