Mysterious Sedna
How did Sedna get into the strange orbit?
It should be impossible.
http://science.nasa.gov/science-news/science-at-nasa/2004/16mar_sedna/
The answer is again due to RR. To understand what happens in Sednas orbit we must first understand what went wrong in Mercury's orbit.
Albert Einstein is belived to have solved the Mercury Perihelion Precession Anomaly.
But when the ruler is "stretching" proportional with time this is not the case. Hence the cause of this anomaly must be reconsidered.
According to the theory I represent distances are stretching proportional with time dilation.
Hence also the cause of Mercury's perihelion Precession anomaly must be found a completely different place.
The table above shows how arc second of Mercury's orbit can be converted to meter.
When we (on the one hand) compare the RR that shows 14603 m per half orbit (
29206 m per orbit), with (on the other hand) the
known magnitude value of the Mercury's orbit (
19399 m), we can off course see that these values not are matching.
This indicate that the RR influence must be weaker as calculated above.
Which indicate that the magnitude of RR only is 100% when moving directly towards the RR direction.
Experiences and better understanding the nature of RR will guaranteed eliminate such "gap" in the future.
Furthermore the calculation shown here don't take everything into consideration, for example not that deceleration due to moving towards RR, - immediately is turned into acceleration , when approaching the orbiting object.
The calculations above only shows the decelerating, not the consequence of that.
This mean Sedna's Perihelion Precession Period (caused only due to RR) is increasing ('about') 16,000,000 km per 6,030 year.
Sedna's aphelion is today approximately 1,34 * 10
14 meter further away from the Sun as its perihelion is.
To reach that distant distance due to the influence of RR can be calculated to 1,34 * 10
14 / 1,6 * 10
10 m = 8375 periods.
Because each period takes 6030 years, the total time to have created the strange orbit can be calculated to 50 million years.
The orbit circumference is about 4,9 * 10
14 m .
The perturbation influence of he orbit is insignificant, - which mean that almost only RR is responsible.
We can therefore also calculate how many period a complete perihelion precession period must take. 4,9 * 10
14 m / 1,6 * 10
10 m = 30625 period of 6030 years.
A perihelion precession period therefore takes about 184,6 billion years.
This is off course also only a estimated calculation.
There are several other influences that must be taken into consideration as well.
At least we have here one more significant factor that shows that we have a lot more to learn.
100 years ago we did only knew one orbit anomaly, this was the anomaly of Mercury. But since the list have been growing.....
This theory solves
all these mysteries in one go.
- The Flyby Anomalies.
- The cause of the Pioneer Anomalies.
- That stars continue to be dragged into the galaxies’ black holes. *) note1
- The long term (known) weak eccentricity anomaly of the moon. *) note2
- That Spiral galaxies can last much longer than the expected 1 billion years .
- The Milankovitch cycle problem of 100,000 years, and all other ice age cycle mysteries. *) note3
- Stars in a dwarf galaxy swarm like bees in a beehive instead of moving in nice, circular orbits like a spiral galaxy *)note4
- It predicts a periodical short term, relatively large perigee / apogee anomaly of the Moon’s orbit, still not discovered.
- It solves the Sedna orbit Anomaly.
*) note1
http://translate.google.dk/translat...r.dk/Videnskab/Videnskab/2006/06/27105328.htm
*) note2
http://arxiv.org/PS_cache/arxiv/pdf/1102/1102.0212v3.pdf
*) note3
http://en.wikipedia.org/wiki/Milankovitch_cycles
*) note4
http://esciencenews.com/articles/2011/10/17/dark.matter.mystery.deepens
*) note4
http://science.nasa.gov/science-news/science-at-nasa/2004/16mar_sedna/