Nirmal Singh.
Last Activity: 10 Years ago
if Radius R is the geostationary orbit then we know that v = 2*pie*R / T
and also we know v= sqrt (GM /R)
equating both equation
sqrt (GM/R) = 2 * pie* R /T
on squaring and calculating T^2 = [4*pie^2 / (GM)] * R1/3
R = [GMT2 / 4*pie2]1/3
putting all value we can calculate
G = 6.67x10^-11 Nm^2/kg^2
M = 5.936 x 10^24 Kg
T = 23 hr 56 min 4.0916 sec
R = 4.2 x 10^4 km
Thanks & Regards,
Nirmal Singh
Askiitians faculty