An 8000 kg satellite is launched from the surface of the Earth and injected into a circular orbit at an altitude of 100 km above the surface of the Earth. The gravitational potential energy of the satellite in the circular orbit is (G = 6.67 × 10-11 N-m²/kg², MẸ = 5.97 × 1024 kg, Rɛ = 6.37 x 106 m) %3D Multiple Choice -5.01 x 1011 J. -4.92 x 1011 J. -4.75 x 1 101 J. -4.02 x 1011 J. -3.85 x 1011 J.
An 8000 kg satellite is launched from the surface of the Earth and injected into a circular orbit at an altitude of 100 km above the surface of the Earth. The gravitational potential energy of the satellite in the circular orbit is (G = 6.67 × 10-11 N-m²/kg², MẸ = 5.97 × 1024 kg, Rɛ = 6.37 x 106 m) %3D Multiple Choice -5.01 x 1011 J. -4.92 x 1011 J. -4.75 x 1 101 J. -4.02 x 1011 J. -3.85 x 1011 J.
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