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 = Rₑ = 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 = √GMₑRₑ+h
by putting the values we have
Vₒ = √6.67x10⁻¹¹Nm²kg⁻²x6x10²⁴kg6.4x10⁶m+0.85x10⁶m
Vₒ = √6.67 x6 x10⁻¹¹⁺²⁴7.25x10⁶ m s⁻¹
Vₒ = √6.67 x6 x10⁻¹¹⁺²⁴⁻⁶ 7.25m s⁻¹
Vₒ = √5.52x10⁷m s⁻¹
Vₒ = √552x10⁶m 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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