Physics, asked by ruhul1597, 6 months ago

Pre-Medical : Physics
AIMS 2018
30.
A satellite of mass 2000 kg is revolving in elliptical
path around earth. If mean altitude at perigee and
apogee are 1600 km and 5600 km respectively,
then the energy required to send the satellite in
this orbit will be (Radius of earth is 6400 km)
(1) 7.2 x 1010 J
(2) 7.8 x 1010 J
(3) 8.5 x 1010 J
(4) 5.6 x 1010 j​

Answers

Answered by apruparabha
0

Answer:

2

Explanation:

2

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