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Nilanjan Bhowmick AIR 3, CSIR NET (Earth Science)
Nafis Ahmad posted an Question
April 08, 2020 • 18:12 pm
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30 points
30 points
- IIT JAM
- Physics (PH)
A satellite is in elliptical orbit about the earth (radius = 64000 km). at perigee it has an altitude o 1100 km and at the apogee its altitude is 4100 km. the m
A satellite is in elliptical orbit about the earth (radius = 64000 km). At perigee it has an altitude o 1100 km and at the apogee its altitude is 4100 km. The major axis of the orbit is at the distano (A) (C) 12. (B) (D) 18,000 km 10,400 kmn 5,200 km 11,600 km
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Ruby negi Best Answer
we have to include R(radius of earth) to calculate total apogee and perigee.
do we have to calculate eccentricity ...or directly adding A +P as mentioned in attachment is enough...???
yeah , you can do it by adding also, it's upto you, answer will always be same..
no need to calculate eccentricity