a) R3=GT24π2MR^3=\frac{GT^2}{4\pi^2}MR3=4π2GT2M
(48⋅106)3=(6.67⋅10−11)(7⋅3600)24π2M(48\cdot10^{6})^3=\frac{(6.67\cdot10^{-11})(7\cdot3600)^2}{4\pi^2}M(48⋅106)3=4π2(6.67⋅10−11)(7⋅3600)2M
M=1.03⋅1026kgM=1.03\cdot10^{26}kgM=1.03⋅1026kg
b) The observed planet is Neptune.
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