PHYSICS · Single correct · A Level · Physics · Fields and their consequences · Fields and their consequences
Problem
Calculate the orbital speed (in kms−1, correct to one decimal place) of a satellite circling the Earth at an altitude of 400km above the surface. (Take G=6.67×10−11Nm2kg−2, M⊕=6.0×1024kg, and R⊕=6.4×106m.)
(a) 10.9
(b) 5.9
(c) 7.7
(d) 8.1