An artificial satellite is revolving round the earth at a height of 30 km above the surface of the earth. Find its orbital velocity.(R = 6370 km , g = 9.8 m/s2
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Answer:
11200m/s or 11.2 km/s
Explanation:
h=30 km= 30000m
R= h+r
=30000+6370000
= 6400000m
V= √2gR
=√2×9.8×6400000
=√125440000
=11200m/s
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