Embedded Files
EXAMPLE 15. THE INNERMOST LARGE SATELLITES – THEIR MOVEMENTS SYNCHRONIZED WITH THE EARTH DAY.
Jupiter and Saturn are The Two Naked-Eye-Visible Giant Planets. The INNERMOST LARGE Satellite of each of these planets has its movements synchronized with The Earth Day.
(A). During TWO Earth days, Jupiter’s INNERMOST LARGE Satellite (Io) revolves 1 revolution + a residual angle of 46.98 degrees.
(B). During TWO Earth days, Saturn’s INNERMOST LARGE Satellite (Mimas) revolves 2 revolutions + a residual angle of 43.99 degrees.
Sample calculation:- (A). 2 ÷ 1.769137786 = 1.13049 revolutions of Io, and (0.13049 x 360) = 46.98 degrees. That is 1 revolution + a residual angle of 46.98 degrees.
When you depict each of these two residual angles as a (single line) radius, the two radiuses look like this:-
The material on this web site is also available in the book Astronomy - The Dishonest Science, by Roger Elliott (available on Amazon).
The material on this web site is also available in the book Astronomy - The Dishonest Science, by Roger Elliott (available on Amazon).
Once again, it is glaringly, blindingly obvious that these residual angles are NOT randomly distributed, as they absolutely SHOULD be if Newtonian Physics alone governed the movements of celestial bodies. (The gravitational field of Earth is insufficiently strong to alter or affect the orbital periods of distant satellites.) Once again, these residual angles all (mysteriously) “hug” the octants. “Something else” (other than Newtonian Physics) is influencing and dictating the movements of these satellites
The statistical odds against both residual angles “hugging” the octants so closely is calculated in the following manner:- The largest “deviation” is 1.98 degrees (Mimas). In that case, the odds against chance occurrence are 1 chance in
1 ÷ [[(1.98 x 2 x 8) ÷ 360]2] = 129 (1 chance in 129).
To check the above, you will need the following numerical data:- Io orbital period = 1.769137786 Earth days, and Mimas orbital period = 0.942421813 Earth days.
To verify numerical data, go to Appendix 2. Section 12 for large satellites. (Note:- Numerical data verification is only available in the book.)
Page updated
Google Sites
Report abuse