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Olá User.
Here's ur answer.
⭐As per question,radius of a circular orbit,r =42250 km =42250×1000 m.
and revolution period,T =24 h =24×60×60 s.
Therefore, speed of sattelite,v =2πr/T.
[NOTE:When 165982135 was divided by 54 the answer was 307343.--
So ,I converted it into km.]
HOPE IT HELPS!!
@Charlie16.
Here's ur answer.
⭐As per question,radius of a circular orbit,r =42250 km =42250×1000 m.
and revolution period,T =24 h =24×60×60 s.
Therefore, speed of sattelite,v =2πr/T.
[NOTE:When 165982135 was divided by 54 the answer was 307343.--
So ,I converted it into km.]
HOPE IT HELPS!!
@Charlie16.
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hargobind:
Thanks
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