Compare the linear velocity, angular velocity, centripetal force and centripetal acceleration of objects on the earth's equator, near earth satellites and geostationary satellites

Compare the linear velocity, angular velocity, centripetal force and centripetal acceleration of objects on the earth's equator, near earth satellites and geostationary satellites

Object 1 on the earth's equator and geostationary satellite 2
Linear velocity v = 2 π R / T, angular velocity W = 2 π / T, centripetal force F = M4 π ^ 2R / T ^ 2, centripetal acceleration a = 4 π ^ 2R / T ^ 2
The quantities of objects on the earth's equator are smaller than those of geostationary satellites
Near earth satellite 3. Geostationary satellite
GMm/r^2=mv^2/r v=(GM/r)^1/2 GMm/r^2=mω^2*r ω^2=GM/r^3 GMm/r^2=m4π^2r/T^2
T ^ 2 = GM / 4 π ^ 2R ^ 3 centripetal force F = GMM / R ^ 2 centripetal acceleration a = GM / R ^ 2
Conclusion T1 = T2 > T3 V3 > V2 > V1 ω 1 = ω 2F2 > F1 A3 > A2 > A1