The speed of the satellite in orbit is 3069 m/s
For the geosynchronous orbit, the gravitational force of attraction on the satellite, F equals the centripetal force on the satellite, F'
So, F = F'
GMm/R² = mv²/R where
So, making v subject of the formula, we have
v = √(GM/R)
So, substituting the values of the variables into the equation, we have
v = √(GM/R)
v = √(6.67 × 10⁻¹¹ Nm²/kg² × 5.972 × 10²⁴ kg/4.23 × 10⁷ m)
v = √(39.83324 × 10¹³ Nm²/kg/4.23 × 10⁷ m)
v = √(9.4168 × 10⁶ Nm/kg)
v = 3.069 × 10³ m/s
v = 3069 m/s
So, the speed of the satellite in orbit is 3069 m/s
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