Physics, asked by vishnupriya2510, 11 months ago

can you calculate the orbital velocity of satelliteborbiting at an altitude of 500 km.Data: G=6.673 × 10 power of -11 SI units, M =5.972× 10 power of 24 kg ,R = 6371000 m, h= 500000 m.Please solve with steps.

Answers

Answered by alisalimali78666

0

Explanation:

use the formula v=sqrt(GM/r)

where sqrt stands for squareroot M is mass of earth and r is the distance from centre of earth

now put the values carefully and get the ans as v=7615.71m/s

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