Disprove... GO!
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1)
T^2=k{4∏^2 a^3 /(G(M+m)cos^2 i)}{(m/M)(r/R)+(M/m)(D/d)(2*(r/(∏ak)))^2 }
T=Rotation period of the large body (sec)
K=Moment of inertia factor of the large body.
M= Large body mass or parent Body mass (kg)
G=Gravitational constant.
R= Polar radius for the large body(meter)
D= Density for the large body(Kg/m3)
a=semimajor axis for the mass center of all satellites that orbit large body (meter)
=Distance between the large body center and the center of masses of all satellites that orbit this large body.
i=Orbit inclination degree for the mass center of all satellites that orbit large body (degrees)
m=Total mass of all satellites that orbit the large body (kg)
d= Mean density for the total satellites that orbit large body(Kg/m3)
r =Mean Polar radius of all satellites that orbit the large body (meter)
The Earth has one satellite (the Moon)
K=0.331
M=5.9736E+24 (kg)
R= 6.3568E+6(meter)
D= 5515(Kg/m3)
a=3.844E+8 (meter)
i=5.14 (degrees)
m=7.35E+22 (kg)
d= 3340(Kg/m3)
r =1735000 (meter)
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2)
http://en.wikipedia.org/wiki/Orbit_equation----
3)
http://mathforum.org/library/drmath/view/57576.html----
4)
Explain how a ship can sail in a straight path from the east asian shore and appear on the US West coast.
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5)If NASA has never sent a rocket into space (more technically orbit above the stratoshpere), than explain satellites. Look up the path of a satellite that is scheduled to pass over your home tonight, go outside, and watch it zip accurately by.
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I'll post more later.