Computing...

Input interpretation:

circular orbit velocity


Equation:

v_c = sqrt((G m)\/r) |  \nv_c | circular velocity\nm | mass of orbit center\nr | orbital radius\nG | Newtonian gravitational constant (~~ 6.674×10^-11 m^3\/(kg s^2))


Input values:

mass of orbit center | 5.98×10^24 kg  (kilograms)\norbital radius | 384000 km  (kilometers)


Result:

circular velocity | 1.019 km\/s  (kilometers per second)\n= 2281 mph  (miles per hour)\n= 3670 km\/h  (kilometers per hour)

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