Question

Find the orbital velocity of a satellite orbiting 1800km above sea level in meters per second?
tchrwill
Te orbital velocity can be calculated from Vc = sqrt(µ/R) where µ = the gravitational constant of the earth and R = the radius of the orbit.

µ = 3.986365x10^14met.^3/sec.^2 and R = 6378 + 1800 km.