Answer:
The ratio g : 
 = 3:1
 = 3:1
Step-by-step explanation:
Given that,
Height of the orbiting satellite from the ground, h = 484 km
 h = 484000 m
The gravitational force of Earth is proportional to acceleration at the location.
The acceleration at the surface is given by relation
 g = GM/R²
Similarly, acceleration at height, 
 = GM/(R+h)²
 = GM/(R+h)²
Therefore,
 g : 
 = (R+h)² : R²
 = (R+h)² : R²
where R is the radius of the Earth, R = 6400000 m
Substituting in the above equation
 g : 
 = (6400000 +484000)² : 6400000²
 = (6400000 +484000)² : 6400000²
 = 12.63 : 4.096
Approximating to the nearest real values
 = 3 : 1
Thus, the ratio of the Earth's gravitational force on the satellite when it is on ground to the gravitational force at an altitude 484 is g : 
 = 3:1
 = 3:1