Answer:
7915.47m/s
Step-by-step explanation:
Parameters given:
Mass of satellite = 238kg
Earth's mean radius = 6370 km = 6370000 m
Orbital speed can be calculated using:
v = (GM/R)^½
where
G = gravitational constant
M = mass of earth
R = radius of earth
v = [(6.67408 * 10^(-11) * 5.98 * 10^24)/6370000]^½
v = 7915.47 m/s