A-P,
B-P,
C-S
Explanation:
(A) Time period is independent of mass of satellite as
T = 2π(r3 / gR2)1/2
(B) Orbital velocity of satellite is independent of mass of satellite (P) as
V = √(GM / r) where M is mass of planet
(C) Mechanical energy of satellite = [(– GMm) / (2R)]
hence A → P
B → P
C → S