31:T8d5,

R_T = 6{,}38 \cdot 10^6\,\text{m}

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M_T = 5{,}97 \cdot 10^{24}\,\text{kg}

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m = 200\\,\\text{kg}

"}}],["$","$1","2",{"children":" describe una órbita circular geoestacionaria alrededor de la Tierra. Determina la velocidad orbital del satélite y el módulo de su momento angular respecto del centro de la Tierra."}]]}],["$","span",null,{"className":"float-right ml-3 sm:hidden","children":["$","span",null,{"className":"whitespace-nowrap text-[13px] leading-none text-muted-foreground","children":"1 pt"}]}]]}],null]}],["$","span",null,{"className":"hidden text-right tabular-nums sm:block pt-0.5 text-sm font-medium text-foreground/70","children":"1 pt"}]],null]}]]}]]}]]}]