Above the earth's surface at a height of

h =m

   = x 10⁶ m,

which is the same as a radius

r = x earth radius,

a_{gravity at radius r} = m/s²

= x g_{earth surface}  (9.8 m/s²)

At the specified orbit radius, the velocity required for orbit is

v_tangential =m/s=km/h=mi/h.

The period of the orbit is minutes = hours.