an artificial satellite is moving in a cirucular orbit of radius 42250 km . calculate its speed if it takes 24 hours to revolve around the earth
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0
r=42250km
distance covered in 1 revolution,
d=2pie r. (circumference of orbit)
2×22/7×42250=265571.43
time taken in 1 revolution,t= 24h
speed of satellite= distance/ time
265571.43/24=11065.48km/h
distance covered in 1 revolution,
d=2pie r. (circumference of orbit)
2×22/7×42250=265571.43
time taken in 1 revolution,t= 24h
speed of satellite= distance/ time
265571.43/24=11065.48km/h
Answered by
0
Hey there!
Given,
Radius (r) = 42250 km
Time (t) = 24 hours
Distance will equal to perimeter of the orbit
= 2πr
= 2π * 42250
Speed of artificial satelite
= 2π * 42250/24
= 11059 km/h
Hope It Helps You!
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