A polar satellite is launched at 850 km above Earth. Find its orbital speed. Ans. (7431 ms⁻¹)


Given:  

Height of the Satellite  = h =  850 Km = = 0.85 x 10³x 10³ m = 0.85 x 10⁶ m 

∴ Mass of the Earth = Mₑ = 6 x 10²⁴ kg
∴ Radius of the Earth = R = 6.4 x 10⁶ m
∴ Gravitational Constant = G = 6.67 x 10⁻¹¹ N m² kg⁻²



To Find:

Orbital speed of Satellite = Vₒ = ? meters



Solution:   

We have the formula for the orbital speed of the Satellite

Vₒ GMR+h

by putting the values we have

Vₒ 6.6710¹¹Nm²kg²610²kg6.410m+0.8510m

Vₒ 6.67 6 10¹¹²7.2510 m s⁻¹

Vₒ 6.67 6 10¹¹² 7.25m s⁻¹

Vₒ 5.5210m s⁻¹

Vₒ 55210m s⁻¹

Vₒ = 0.742967x 10³ m s⁻¹

or

Vₒ 7429.67 m s⁻¹

or

Vₒ 7430 m s⁻¹

Thus the orbital speed polar satellite will be 7430 ms⁻¹ when launched at 850 km above Earth. 

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