How would we establish a geo-stationary orbit of a OKBR satellite launched with public funding of th...

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How would we establish a geo-stationary orbit of a OKBR satellite launched with public funding of the members of the subreddit?

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So basically a geostationary orbit around the earth is about 35,789 kilometers above the earths equatorial line and following the general directions of our planets rotation. But in order to launch an OKBR satélite we need to use the geosynchronous equation of G = 0.667 x 10-10 Nm2/kg2, Me= 6×1024 kg and T=24 h × (3600 s/h) = 8.64 ×104 s. re−s=(0. 667×6×8.64240×10−10 24 2×4)13 km. Also what would the dimensions of our satellite be, as it can have a no larger than 3.5^2.4m of surface are with a reasonable amount of fuel.

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thegreatyee123

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Posted: 4 years ago
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External URL: reddit.com/r/okbuddyphd/...