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Physics Question 47 – JEE-MAIN 2025

A satellite of mass 1000 kg is launched to revolve around the earth in an orbit at a height of 270 km from the earth's surface. Kinetic energy of the satellite in this orbit is _______ ×1010 J. (Mass of earth =6×1024 kg, Radius of earth =6.4×106 m, Gravitational constant =6.67×1011 Nm2kg2)

For a satellite in a stable circular orbit, the gravitational force provides the necessary centripetal force.

Step 1: Calculate the orbital radius✦ Active

The orbital radius r is the sum of the Earth's radius Re and the height h of the satellite from the surface. Convert all values to meters.

Re=6.4×106 m h=270 km=270×103 m=0.27×106 m r=Re+h=6.4×106 m+0.27×106 m=6.67×106 m
Step 2: Determine the kinetic energy formula for a satellite in orbit○ Expand

For a satellite in a stable circular orbit, the gravitational force provides the centripetal force. Equating the gravitational force Fg=GMemr2 and the centripetal force Fc=mv2r allows us to find the orbital velocity squared v2. The kinetic energy is K.E.=12mv2.

GMemr2=mv2rv2=GMer K.E.=12mv2=12m(GMer)=GMem2r
Step 3: Substitute values and calculate the kinetic energy○ Expand

Substitute the given values for G, Me, m, and the calculated r into the kinetic energy formula.

K.E.=(6.67×1011 Nm2kg2)×(6×1024 kg)×(1000 kg)2×(6.67×106 m) K.E.=6×10(11+24+3)2×106=6×10162×106=3×1010 J

The kinetic energy is 3×1010 J. Therefore, the value to be filled in the blank is 3.

💡 Teacher's Secret Hint

Pay attention to unit conversions and scientific notation for accurate calculation.

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