Question

Obtain the formula for orbital velocity and energy of an orbiting satellite.​

Answer 1

Explanation:

a c = v orbit 2 r orbit 1.9 × 10 −13 m/s 2 = v orbit 2 ( 1.25 × 10 6 ) ( 9.5 × 10 15 m ) . a c = v orbit 2 r orbit 1.9 × 10 −13 m/s 2 = v orbit 2 ( 1.25 × 10 6 ) ( 9.5 × 10 15 m ) . Solving for the orbit velocity, we have v orbit = 47 km/s v orbit = 47 km/s .

Answer 2

Answer:

hope you understand

Explanation:

orbital speed can be found using v = SQRT(G*M/R). The R value (radius of orbit) is the earth's radius plus the height above the earth - in this case, 6.77 x 106 m.