innermost-sats

EXAMPLE 4. THE INNERMOST SATELLITES – THEIR MOVEMENTS SYNCHRONIZED WITH THE EARTH DAY.

The “Superior” Planets (ie:- orbiting outside Earth’s orbit) are:- Mars, Jupiter, Saturn, Uranus, and Neptune. (We will treat Pluto as a Trans-Neptunian Object, rather than a planet, in this example.) Here is a list of The INNERMOST Satellites for each of these five planets, together with the orbital periods (expressed in Earth days) of these satellites:- Mars’ INNERMOST Satellite is Phobos (0.3189), and Jupiter’s INNERMOST Satellite is Metis (0.294780), and Saturn’s INNERMOST Satellite is Pan (0.5750), and Uranus’ INNERMOST Satellite is Cordelia (0.3350331), and Neptune’s INNERMOST Satellite is Naiad (0.294396).  

 To verify the above numerical data, scroll to the bottom of this page.

During One Earth day (24 hours):-

(A). Phobos revolves (1 ÷ 0.3189) = 3.1358 revolutions, ie:- 3 complete revolutions plus A RESIDUAL ANGLE of (0.1358 x 360) = 48.9 degrees. 

(B). Metis revolves (1 ÷ 0.294780) = 3.3924 revolutions, ie:- 3 complete revolutions plus A RESIDUAL ANGLE of (0.3924 x 360) = 141.2 degrees. 

(C). Pan revolves (1 ÷ 0.5750) = 1.7391 revolutions, ie:- 1 complete revolution plus A RESIDUAL ANGLE of (0.7391 x 360) = 266.1 degrees. 

(D). Cordelia revolves (1 ÷ 0.3350331) = 2.9848 revolutions, ie:- 2 complete revolutions plus A RESIDUAL ANGLE of (0.9848 x 360) = 354.5 degrees. 

(E). Naiad revolves (1 ÷ 0.294396) = 3.3968 revolutions, ie:- 3 complete revolutions plus A RESIDUAL ANGLE of (0.3968 x 360) = 142.8 degrees. 

We now have five RESIDUAL ANGLES, which are as follows:- 

(A). 48.9 degrees. 

(B). 141.2 degrees. 

(C). 266.1 degrees. 

(D. 354.5 degrees. 

(E). 142.8 degrees. 

When you depict each of these five RESIDUAL ANGLES as a (single line) radius, the five radiuses SHOULD look something like this:-

In fact, they look like this:-

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 the orbital periods of all these separate 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 all five residual angles “hugging” the octants so closely is calculated in the following manner:- The largest “deviation” is 7.8 degrees (Naiad). In that case, the odds against chance occurrence are 1 chance in

1 ÷ [[(7.8 x 2 x 8) ÷ 360]5] = 199 (1 chance in 199). In fact, the odds are longer than this, because many of the residual angles are closer to an octant than 7.8 degrees.

NUMERICAL DATA VERIFICATION. 

The “Superior” Planets (ie:- orbiting outside Earth’s orbit) are:- Mars, Jupiter, Saturn, Uranus, and Neptune. To verify this, click on the following link:-

www.solarsystemtimeperiods.com/planet-orbital

(We will treat Pluto as a Trans-Neptunian Object, rather than a planet, in this example.) Here is a list of The INNERMOST Satellites for each of these five planets, together with the orbital periods (expressed in Earth days) of these satellites:- Mars’ INNERMOST Satellite is Phobos (0.3189)To verify this, click on the following link:-

www.solarsystemtimeperiods.com/planet-orbital

Jupiter’s INNERMOST Satellite is Metis (0.294780). To verify this, click on this link:- 

www.solarsystemtimeperiods.com/jup-inner

Saturn’s INNERMOST Satellite is Pan (0.5750). To verify this, click on this link:-

www.solarsystemtimeperiods.com/saturn-sats

Uranus’ INNERMOST Satellite is Cordelia (0.3350331). To verify this, click on this link:-

www.solarsystemtimeperiods.com/uranus-innermost

 and Neptune’s INNERMOST Satellite is Naiad (0.294396). To verify this, click on this link:-

www.solarsystemtimeperiods.com/neptune-sats  

To see further similar examples (FULL Demonstrations) of THE OCTANTS RULE, and synchronization of the movements of Solar System bodies, go back to the "full-demonstrations" page by clicking on the following link:

full-demonstrations