Question:
The energy required to take a satellite to a height ‘h’ above Earth surface (radius of earth 6.4×10³ km) is E1 and kinetic energy required for the satellite to be in a circular orbit at this height is E2. The value of h for which E1 and E2 are equal is
Options :
Answer :
(c) 3.2 x 103 km
Answer Steps :
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