Physics, asked by adityahypertext1234, 10 months ago

A remote sensing satellite is moving around the earth in an orbit whose altitude from the surface of earth is 800km calculate orbital velocity and orbital period of the satellite​


Answers

Answered by harsharora111
0

Answer:

Use formula

orbital velocity = √GM/r

r= distance from centre

in question distance for surface is Given

Then r= Re + 800(given)

Re = Radius of Earth

Calculation karo answer aa yega

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