The near-surface orbital period T₀ = 2π√(R_E/g) ≈ 85 minutes. This value can also be expressed as T₀ = 2π√(R_E³/GM_E). What is the physical significance of this minimum period?
A.
Satellites must orbit for at least 85 minutes to stay in orbit
B.
No artificial satellite can have a time period less than about 85 minutes while orbiting Earth
C.
The geostationary satellite has a period of 85 minutes
The geostationary satellite has a time period of 24 hours and orbits at radius R_G from Earth's centre. A near-surface satellite has period T₀ ≈ 1.4 hours. The ratio R_G/R_E is approximately: