Keeping it simple

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Understanding the test site locations and how the sun season will effect test results.  Testing inside the prime meridian zones will result in higher sun angles this is because the orienting station (OS ) is now closer to the sun.  Testing outside the prime meridian zone will result in lower sun angles this is due to the OS being farther from the sun.  The Operation Resolute Time test site was located 765 miles north of the northern prime meridian the Tropic of Cancer.  Test results should have yielded far lower direct sun  angles if the earth was a globe or sphere.  This however was not the case, the exact opposite happened with direct sun angle readings exceeding 50 degrees. In other  words the sun is to high in the sky at 0900 and 1500 hours, meaning the geometric surface of earth is flat.  The other major effect on testing is the sun season.  The most difficult test time for the globe model to pass is late Spring and Summer sun seasons.  Again this is because the sun location is closer to the OS at this time.   This was evident during testing in Operation Resolute Time 2020, as the globe model failed 70% of tests.  Tests conducted in late Spring and Summer demonstrated geometric failure in the globe model during these sun seasons.

Setting the geometric edge (correct earth to sun alignment) is essential first step in determining earths true geometric shape.  Understanding the sector balance within the test zone is key.  This means readings prior to 3 hours or just after three hours will be out of balance when applied to the 45 degree sector.  Example would be an easterly reading time of  08:30 hours from sun survey time of 12:00 hours exceeds the 45 degree sector by 30 minutes.  Or if the reading was taken at 15:30 hours, 30 minutes past the 3 hour mark for westerly reading time. if the sun survey point was emplaced at 12:00 hours.  These are shown in the diagram above with the red arrows.  It's the step the heliocentric globe model left out (setting the geometric edge).  This step is key figuring the correct geometric alignment of earth to the sun.  The alignment angle  of earth to sun must be measured from the OS once the sun survey point is emplaced.  The OS can be anywhere along the magnetic line either inside or outside the prime meridian zone.  The OS does not have to be a vertical 90 degree, it can be anywhere along the north - south magnetic line.  Remember at 24 hours the sun will return back near the sun survey point mark.  Use of a compass and Marx Device fulfills this important requirement.  The maximum sun angle measurement for the globe model to be valid is 45 degree from the established sun survey point at the designated balanced times (easterly-westerly).  This is known as the line of parallel.

The first sun survey point method was emplaced by using tripods and a string line between them.  A compass was used to orient the string line on magnetic north.  The Marx Device was soon developed after this method which improved accuracy and timing of the sun survey point.  The Marx Device is named after Latvian Special Operations Force (LATSOF) soldier 1st Sergeant Marx who helped me build the very first device.

The sun as it nears the 90 degree center line of magnetic from ground up skyward perspective.  The sun was south of the observer in this picture.   This experiment was to view the sun and its movement as it crosses the 90 degree set line (north-south line of magnetic), from the observer on ground.  This is the view of proper earth to sun alignment along the line of magnetic (what it actually looks like) from the observer OS (orienting station) sun survey point.  Timing is the primary essential element as well within this process, that being three hour time mark after and prior to sun survey time.  This is because three hours equates to 45 degrees.  The sun will show up 24 hours the next day right on time at the marked location. within inches.

The actual Marx Device used during Operation Resolute Time 2020.  The first initial use of the Marx Device found the OS sun survey point off by approximately 22 minutes.  A single level vile is used to check the cross level of the device when emplaced.  The hole located in the center of the board is for marking and emplacing a stake or bottle cap which then becomes the sun survey point marker.  The sun survey point also designates the 45 degree sector at 3hours by the sun returning 24 hours later to the same marked survey point plus around 2".  The difference being the suns different path if you believe in the FE model or the earths different orbital rotation path, either way there is only 3hours. in each 45 degree sector.  The sun survey point verifies this. This is the accountability within this process.

Correct earth to sun alignment is essential in correctly measuring direct sun angle from the sun survey point.  The Marx Device in use, note the sun shadow line with the sun at 90 degree to the OS.  The Marx device is oriented north-south by use of a compass.  The sun was south approximately 765 miles of this OS position located in Kabul, Afghanistan.  Once correct earth to sun alignment is achieved this is whats called "setting the geometric edge".

Emplacing the Marx Device and timing as shown in the above picture.  Note once the sun is 90 degree to the magnetic line which cast (shadow line) from the string which is oriented magnetic north using a compass as the OS.  Once the sun survey point is established direct sun angle measurements can be taken.  This is what's called setting the geometric edge.  We must remember the sun whether you believe your on a globe or flat earth, the sun is 90 degree to a person,place, or thing every second of every minute of every day of every year.  This is the maximum forward angle to the sun on earth, meaning a perfect 90 vertical degree.   We can now create a 90 degree sheath along the line of magnetic from the sun survey point.  This line of magnetic travels as far as you can see the sun north-south,  once it is emplaced by the observer at the sun survey point.  This is the essential initial step for determining correct earth sun alignment. 

How to set in the sun survey point using the Marx device video link;

https://drive.google.com/file/d/1aJ-kzJTH0a7jvpD456t8FYGKia9S18sG/view?usp=drive_web

The very first Marx Device used in Operation Resolute Time 2020 from 7 February to 8 August 2020.  The Marx Device is used to emplace the sun survey point from which to measure direct sun angle from in determining earths true surface shape.  This is accomplished with the use of a compass which sets the sting line on the magnetic north-south line of orientation. This device is a manual alignment device for the observer to be aligned to the sun at a directional angle of 90 degrees to an exact point on earth along the line of magnetic at an exact time.  The Marx Device is used to set the geometric edge from which to accurately measure direct sun angles from.  Note the hole in the center of the board, this is to mark the sun survey point once the sun is 90 degree to the observer. This is shown by a shadow line that is created by the sun as it casts a shadow of the sting line on the board.   The Marx device was named after 1SG Marx of the Latvian Special Operations Forces (LATSOF) who helped me build the very first device in Kabul, Afghanistan.

Earth sun alignment and line of parallel are interlinked regardless of earths said axis or tilt.  This is because at the cumulative 90 degree mark line of parallel is reached.  The reason it is 90 degree is because the suns maximum forward angle when measured can only be 90 degree which is perfect vertical alignment with an observer in the prime meridian zone.  This also transfers to outside the prime meridian zone as well once a sun survey point is used (observer to sun alignment 90 degree).  In other words from one or two observers, the observer is now in line of parallel to the same observed object of reference once a measured surface reading to the sun is 45 degree.  The said observed object can only exceed its said given size at said distance based on line of parallel.  This is especially true in a SIMO observation, when the object is viewed from two observers at different locations at the same time.  This application can also be applied to STO process (single observer) as well.  This application and process is heavily used in Military Science for both near and extreme distances (indirect fire aiming references, weapons bore-sighting, indirect fire lay and safe procedures for lay and safe circles, SIMO observation, weapons live fire range safety box and sector range fans, fire control alignment test (FCAT)).  This is why setting the geometric edge is the critical first step in accurately determining earths true surface shape.

In the diagram shown for both STO and SIMO from the established OS sun survey point  the sun is center mass to the observer.   Note the exceeded line of parallel or at measured direct sun angle of 46 degree or more, the observer is no longer on the sun or line of survey (sun target line).  This action now distinguishes earths true surface shape as flat.  The sun survey point is established  along the line of magnet when the sun is 90 degree to the observer.   Observation time will be three hour prior to and after sun survey time.  Example: for sun survey time of 12:00 hours the first observation time would be 15:00 hours(3pm) a westerly reading time, the next observer time would be the following day at 09:00 am easterly reading time.

When verifying an objects said size at said distance a range fan is utilized to compute accuracy of this information.  For one degree past line of parallel using either STO or SIMO (minimal degree example) which is a direct measured angle of 46 degree using the heliocentric model you now have exceeded that models tolerance by over 1,638,664 miles.  If we subtract the suns actual size or half sun of 482,685 miles again the heliocentric model is still exceeded by 1,155,979 miles.  Remember as the observer the sun is center mass to the observer.  This now puts the observer off line of survey or sun target line (line of survey) when using the heliocentric globe model.  Unlike the flat earth model which has full 90 degree measurable direct sun angle which puts the flat earth model well within tolerance.

The OS can be anywhere in the world.  From the OS we use a compass to determine the line of magnetic from that position.  Line of magnetic is the magnetic north-south line and is read by using a compass at the sun survey point.  This means inside or outside the zones of prime meridian (Tropic of Cancer-North, Equator-Central, Tropic of Capricorn-South).  Once established the OS which is emplaced on the sun survey point when the sun is 90 degree to the observer  (example 12:00 hours) can be utilized for solar observation to measure direct sun angle readings. The measured direct sun angle reading of 46 degree or more distinguishes earths true surface shape as flat at; observation times of 09:00 easterly and 15:00 or 3pm westerly reading times.  This is 1 degree beyond line of parallel which exceeds the heliocentric globe models sun size at distances of between 91 to 94 million miles.  Flat earth keeping it simple.

Identifying the OS test equipment required to conduct direct sun angle measurements. This is used for testing the 45 degree sector.  

1.The OS platform is a white dry erase board. 2.The digital protractor runs on 9volt battery 0-225 degree with .5 degree accuracy. The protractor also has a level bubble. 

3.Tape measure for measuring OS platform height. 

4.Sun shield for eye protecting when viewing the sun (should be used with sun glasses as well). 5.Marker pen for writing on dry erase board the test results. 

6.Plum-bob and line for positioning the OS over the sun survey point. 

7.Tri-level used for leveling the OS platform. 8.Survey marking stake (coin, bottle cap can be used). Mark the sun survey point. 

9.Single level vile, used to check cross-level of the Marx device. 

10.Compass to orient the Marx device on line of magnetic and measure sun azimuth.  

11.Tripod used to hold the OS platform elevated. 12.Stabilizer board 18” x 18” piece of plywood used to shift the OS (optional not shown). 

13.The Marx device. Used for setting in the sun survey point. 

Total equipment cost is right at $175.00 to $200.00 USD. One of the reasons I developed this process was to keep the experiment relatively inexpensive, available to anyone, cost was a factor in the process. Keep it simple yet very effective and accurate.   

Identifying the OS test equipment required to conduct direct sun angle measurements.  Testing the 45 degree sector.  Total equipment cost is right at $175.00 to $200.00 USD.  One of the reasons I developed this process was to keep the experiment relatively inexpensive, available to anyone, cost was a factor in the process.  Keep it simple yet very effective and accurate.  Orienting station equipment is described in in the video link provided;

https://drive.google.com/file/d/1Q2_mwHs8EgzBG-iA4h8dDZUJugbVkAZX/view?usp=drive_web

Use of the digital protractor was selected for its ease of use, ability to  measure angles at very low height to the earths surface all while maintaining high degree of accuracy in measurement.  It's as easy as level, point at your object, click on the reading (instrument display) and that's it.  When verified against a manual protractor there was no difference in angle measured.  This model has a +- of half a degree accuracy.   It measures angles from 0-225 degrees.  Priced right at $35.00 USD.

Using the digital protractor we must ensure it's accuracy, one way to do this is check an angle that is drawn out using a manual protractor on a white board.  Once this is accomplished take the digital protractor and align it on the angle drawn.  In the test we used an angle of 45 degree which when we tested it with the digital protract there was no difference in angle reading.  We have now verified the digital protractors accuracy.  This test should be done prior to any STO or SIMO tests measuring sun angle to ensure accuracy of readings.

The sun survey positioning is critical in the process of ensuring the geometric edge is set from which to take direct sun angle readings to and from.  This is obtaining correct earth to sun alignment.  The observer must understand the sun season and his/her location inside or outside the prime meridian zone and latitude.  This will tell where the sun position to the observer will be in the daytime sky.  Another important fact and that is the farther you are away from the prime meridian the lower the observer sun angle at the OS will be, this must be understood, and the effect it will have when testing both models.  It is also important to understand that in a 24 hour period the sun will be right back near the sun survey point usually within 6-12 inches.  This difference is based on movement of the sun to and from the prime meridian.  Direct sun angle readings were also taken over a long period than one day from the sun survey point to make note in the angle reading versus a 24 hour period..  The most important factor being the sun at 90 degree to the observer at the OS to set in the sun survey point using a compass and the Marx device  The easiest example of this would be to imagine standing in the threshold of a doorway, where the walls are 90 degree as you stand in the doorway, (left, right and vertical). 

The 

Marx Sun Survey Positioning Device is instrumental for emplacement of a sun survey point at the OS.    Using a simple piece of plywood approximately 6" wide and 24" in length with a hole cut in the center and two fasteners or nails centered on each end to support a string.  The string is used to reflect a shadow line on the board from the sun as it moves across the sky.  The Marx device is oriented north-south magnetic by using a compass.  Simply orient the center string line along magnetic north using a compass. Example of this would be at (12:00 hours) at the OS sun survey point or once the sun is 90 degree to the observer, meaning the shadow line will be center-lined on the Marx Device.  A stake or bottle cap can be used to mark the new survey point.  This is the reason for the hole in the center of the board.  Again remember the Marx device is oriented north-south by magnetic compass at the OS location.  A cross-level vile is used to ensure the device is level as to not introduce angle error   A tri-level may also be used to level the device on the ground.  The sun survey point is emplaced at 12:00 hours.    The survey point can be emplaced daily or as sun illumination permits.  Survey points were used daily and over 3-4 day length to see the effect on measured sun angles.

For ease of use with a tripod, mounting a small piece of wood on the OS platform underside is required.  This will allow for the tripod to attach to the OS platform securely.  I used a strip of wood three screws and adhesive for this.   The strip of wood is approximately 1.5 inches wide by 13 inches in length.  For ease of use I marked where the tripod grips to the wood base.  Of important note I also used duct tape to keep the digital protractor to the OS platform for ease of use and to stabilize it during periods of high wind.  I used a whiteboard for the OS base, this can also be used to record data easily.

The orienting station (OS) setup; 

Step 1 Orient the stabilizer board towards the sun (marking the board to match the survey point helps).

Step 2 Attach the tripod to the OS platform and orient the center-line of the OS platform towards the sun.

Step 3 Emplace the digital protractor on the tripod (use of duct tape to attach the digital protractor to the OS platform maybe used).

Step 4 Set the OS platform height to half meter.  Level and position the OS platform over the OS sun survey point.  Use tri-level to level OS platform.  This may require shifting of the tripod as well to position the radial arm over the OS survey point.  Use of a stabilizer board helps facilitate this process much easier.  Use a plum-bob to check position of the digital protractor over the sun survey point.   Try to be within 1/2 inch of of center of the survey marker.

Step 5 check digital protractor level ensure level bubble is center.  Adjust as required.

Step 6 Sight in on the sun first check, then check OS level, plum position and sun position.  Use sun shield and eye protection when viewing the sun.

Step 7 Track sun movement 2 minute window.  Recheck OS platform position is level and plumb, adjust as needed.  Turn power ON the digital protractor.

Step 8 Measure sun at required time for easterly 0900 hours, westerly 1500 hours.  Or 3 hours from sun survey point time.  The sun survey point may not always be 12:00 hours it is based on observer location to the sun, one the sun is at 90 degree to the observer.  Sight in center mass of sun with digital protractor radial arm.  Record the measured angle shown in the digital protractor window.  Use of a whiteboard for the OS platform facilitates the recording process easily.

Step 9 Final data recordings. Measure azimuth to the sun from the OS using a compass.  Do this by simply standing approximately 10 feet back aiming compass down along the digital protractor arm which was pointed at the sun, record the azimuth for record.  Record OS elevation and GPS grid location for record.

The orienting station (OS) setup is very simple, but there are important steps one must know how to perform each correctly,  and why.  Setup can be accomplished in about 5-10 minutes for a beginner and about 3 minutes once you learn the process.  You will note duct tape was used to help stabilize the digital protractor, this helps against higher wind or windy test conditions to stabilize the device on the platform.

Corey conducting a STO easterly reading time at 0900 in Kabul Afghanistan.  Use of a sun shield and sun glasses for eye protection during solar observation.  These tests were conducted in a war zone, 765 miles north of the prime meridian Tropic of Cancer.  This reading was 50.1 degree, which exceeds the allowed tolerance for the globe model by 5.1 degree, this gives a total composite sum angle of 95.1 degree.  For the flat earth model the 50.1 degree is well within the flat earth models tolerance with a total composite sum angle of 50.1 degree

Understanding the effects of elevation on test readings.  The higher in elevation the test site is located the lower the measured sun angle will be as a result.  If we look at the examples shown the highest sun angle readings show be at sea level.  Now one thing that must be considered is if the sun dips towards earth this could effect the reading at lower elevation.  Further testing of the sun will determine if this is true or not.  However, these examples given provide a clear example of the effect of elevation has on measured angles.

1. Video on OS equipment identification and required for orienting station setup.  https://drive.google.com/file/d/1Q2_mwHs8EgzBG-iA4h8dDZUJugbVkAZX/view?usp=drive_web

2. Setup of the sun survey point and how it works using the Marx device.

https://drive.google.com/file/d/1aJ-kzJTH0a7jvpD456t8FYGKia9S18sG/view?usp=drive_web

3. https://flatearthstuff.com/proving-the-sun-rotates-over-a-flat-earth-by-corey-kell/

1. https://youtu.be/W01JgbG99B0 (Info Wars introductory on Flat Earth).

2. https://youtu.be/4SlRsbQ3nfM (Flat Earth Clues) Mark Sargent

3. https://youtu.be/1FoTOp5MdtY (The Greatest Lie on Earth Proof Our World is not moving) Edward Hendrie

4. https://youtu.be/_9UjQTp-EC0  (Interview with Corey on Strange World #279)

5. https://youtu.be/aQ7_9eIAlT4 Flat Earth Documentary 2020 Part II by ODDTV.

6. Force of Gravity how it works.

https://youtu.be/Eic4xivGP7E

7. Double Slit Experiment

https://youtu.be/Q1YqgPAtzho

The first step in setting up the OS is emplacing the stabilizer board facing the direction of the sun at the sun survey point.  You can use a compass to check the azimuth of the oncoming sun.  Mark the stabilizer board where the sun survey point is for ease of reference.  The sun survey point in these photos is a blue bottle cap.

Having the tripod and OS platform (whiteboard) already connected and the digital protractor mounted on the platform can help with ease of use.  Additionally the platform base height can be pre-adjusted to half meter.  A strip of wood mounted to the underside of the OS platform helps attach the tripod tot he OS platform.  Level the OS platform using tri-level and the digital protract level.

Set OS platform height to half meter from the ground.  Remember ideally you want to be closest to earths surface as possible, a half meter is really the closest without digging into the ground.  Use a tape measure to set and check this height.

Step 4 Check plumb of OS station using a plumb-bob.  The plum-bob should be set at the digital protractor radial arm.  You want this section of the digital protractor over the sun survey marker.

Step 5 Record GPS location of OS and elevation for record.  Remember elevation does have an effect on the test results.  Higher test elevation means lower sun angle, and lower test elevation means higher sun angle.  Ideally we want to be at sea level to be at the closest geometric form of the earth.  However this is not always possible, so we must understand the effect of elevation.

OS setup is complete.  You want to make sure the OS station is oriented at the incoming (easterly) or outgoing (westerly) sun.  If any movement of the orienting station is required always check that the OS is over the sun survey point or within 1".  Also check the level of the OS platform.  Sun observation reading times will be 3 hours after sun survey time (westerly) and 3 hours prior to sun survey time (easterly). 

Once the OS setup is complete.  You are now ready to perform the observation.   Remember to always use eye protection and a sun shield when viewing the sun.  

The two major prime meridian zones as shown for both the globe and flat earth models.  Effects of each respective are is described.  Inside the prime meridian zone the sun angles will be higher this is due to the observer being closer to the sun inside the prime meridian zone.  Outside the prime meridian zone the observer measured sun angles will be lower, this is due to farther distances of the sun from the observer.  The significance of these elements of distance is a major key factor of understanding "distance" and its effects on both models and their validity.  The globe model having the most difficult testing inside the prime meridian zone in staying under the line of parallel at 45 degrees or less.  This results in a major issue for the globe model due to the fact it has failed major testing outside the prime meridian zone in Operation Resolute Time 2020.

The suns operating range is within the lines of meridian for the flat earth model.  The flat earth model with the lines of meridian along with the antarctic ring and north pole as shown.  The suns depicted in this diagram are examples to show the suns actual operating range within these three rings of prime meridian.  With the surface angle of 0 degree the flat earth model has no issues in meeting the validation testing,  this is because this model has a full 90 degree measurable angle to work with.  The earth sun alignment within this model meets the validation process for orbital mechanics as well, unlike the globe model which fails in both processes when tested.  The importance of setting the geometric edge using the sun is paramount in the setting up process for testing to determine earths true surface shape.  It is the major *first* step the Heliocentric globe model failed to utilize, hence that models failure geometrically.

In understanding the OS locations we must be aware of the effects of distance within and outside the prime meridian zones.  A key factor is that the sun within the prime meridian zone is vertical 90 degrees to a person place or thing every second of every minute of every hour of every day of every year on earth.  The sun within the prime meridian zone is much closer in distance, as a result we can expect  higher measured sun angles.  This means we can triangulate the sun to determine its actual distance from either STO or SIMO observations.  Also measured sun angles will be higher within the prime meridian zone based on the suns operating range within the prime meridian zones (north-Tropic of Cancer, central-Equator, and south-Tropic of Capricorn).  The sun may also be a lateral 90 degrees to the OS within the prime meridian zone as well, when this occurs measured sun angles that are a lateral 90 degrees will be lower.

For OS locations outside the prime meridian zones such as in Operation Resolute Time 2020 measured sun angles will be lower based on distance of the suns primary operating ranges within the prime meridian zones.  This is because we are farther from the sun when outside the prime meridian zone.  Understanding the lateral 90 degree sheath becomes more important.  In other words its like walking through a door threshold where you have all supports and walls 90 degree to you.  Hence the importance of the Marx Device used to emplace the sun survey position.  The suns distance can also be calculated through timing and distance and triangulation using both methods (STO or SIMO).  Of note also the elevation shown here was just under 6000' feet above sea level.  These tests were conducted at high altitude which gave the globe model another major advantage which means lower sun angles at these high altitudes.  This however did not occur, measured sun angles were over 50 degree during Operation Resolute Time.  

Of importance when we make measurements and check measured angles, we must understand the effects distance has on those angles.  As the diagram shows if distance is increased when viewing an elevated object the measured angle to that object will decrease.  The closer we are to an elevated object the higher measured angle to that object will be.  Note the use of the guide angle at 90 degree to the sun in the diagram.  A protractor is used to demonstrate this effect and  to show the measured angles to the object of reference the sun.  This is also true when we view the sun at distances from the prime meridian areas, as the distance from the prime meridian zone increases the direct sun angle decreases.  Measured sun angles within the prime meridian band would increase as the observer is closer to the sun.

Using the M2A2 aiming circle the orienting station (OS) can utilize both the sun or stars to emplace survey in orienting the gun-line on direction of fire.  This method of lay or survey is used by airborne artillery units.  Extensive use of celestial survey techniques and triangulation in applied geometry.  Through this extensive use in the field of military science we can exclude atmospheric lensing at higher elevations or 15 degree above the horizon.  This is because this procedure is a celestial survey and is bumped or checked via another method of survey lay using grid magnetic which is less tan 1/3 of a degree 99% of the time.

 Aiming circle and Safe circle are the same type of device.  As shown the increments are in mils, there are 6400 mils in a complete circle.  You will note some numbers are in red, this is used for when the aiming circle and safe circle bump or verify lay of survey.  The mil number on the outer ring are read in.  Meaning read from outside in.  In this example shown the circles are bumped at 1600 mils as shown by the red arrows.  On the actual circles the mils are in 100 mil increments and a micrometer knob which reads in one mil increments 0-99 mils.  This completes readings in mills up to a complete 6400 mil circle.  When verifying lay of circle, or as known as (BUMPING Circles) where each circle operators turn an angle on each other, circle operators rule of thumb when verifying lay is if you see RED you read RED.  Methods of lay (survey) using the M2A2 aiming circle are; grid magnetic, orienting angle (OA), celestial survey, star shot, sun shot, Polaris-Kochab, and SIMO-survey transfer.

Understanding the use of Military Sciences methods of survey and lay and the effects of refraction and lensing at higher angles that can be excluded (15 degree above the horizon).  This is based on military sciences actions and validation processes in methods of lay/survey using the sun and stars.  In using different methods of lay the lay circle and safe circle validate the survey when they *bump* or turn an angle on each other to check the lay of each instrument.  The difference in reading must be 10 mils or less.  There are 17.8 mils in one degree.  Most often or 99% of the time the difference will be only  1-2 mils.  This is why and how we can exclude atmospheric lensing and refraction at angles above 10-15 degrees above the horizon.  The M2A2 Aiming Circle as shown.  The accountability process within military science is paramount to its principles and high standard.

Hasty Astro method of lay or emplacing survey is both very accurate and can be done in relatively short period of time.  This method of lay uses both sun in the day time or stars such as Polaris at night time.  You will note these are extreme distances when using the sun and stars for this method of lay.  Lensing and refraction are excluding at these extreme distance because  of the second M2A2 aiming circle called the safe circle verifies the survey data using an alternate method of lay typically magnetic.   Both circles must be within 10 mils of each other, they typically are within 1-2 mils 99.9% of the time.  There are 17.8 mils in one degree.

The real world military science applications applied directly into STO and SIMO.  The transition is exact with application and process providing solid principle and fundamentals to both STO and SIMO applications.  You will note the triangulation in this application, also the 45 degree sector test box.  Can you pick out the hallway walls, floor as they all come together?  Remember seeing it somewhere else,

perhaps in visual perspective?

The real world military science applications applied directly relate from Military sciences real world applications.  Included are uses of applied geometry for this application.  There is both a manual and computerized version for determining weapons sector range fans. The computerized version is called ArGIS. Calculating and determining safety is an exact science, and there is no room for error in these applications, because lives depend on its safe practice every day.  Also very important are the lines of parallel or the left and right limits, lines of intersect, they are very definitive in this application of military science.  This is why military science may mention heliocentric science in some of its manuals but never apply it in its real world applications.  Now see if you can pick out the visual perspective items in this and the next diagram where STO and SIMO applications were developed from.  

The real world military science applications applied directly into STO and SIMO.  Note the key in this diagram showing STO and SIMO.  The transition is exact with application and process providing solid principle and fundamentals to both STO and SIMO applications.  The applications in Range Sector Fans and HASTY Astro applications both demonstrate near and extreme distances of visual perspective, which lensing and refraction can be excluded at over 15 degree above the horizon.

The real world military science applications are present in many things we should recognize if we just take the time to understand them.  This is true with visual perspective, military science real world applications verify this as accurate.  You will note the hallway, walls, and lines of parallel.

Can you pick out the lines of parallel lines of intersect, and visual perspective in the military science applications shown?

The lines of visual perspective, left and right limits, lines of parallel and intersect all combine within visual perspective and are interlinked within the field of military science real world applications shown.  The evidence is overwhelming once we learn how to identify it and know where to look.  

Visual effects at lower elevations up to 10-15 degree above the horizon has an effect on optics and our vision.  Conditions that effect this are weather, temperature, pollution, water in our atmosphere, and air density.  Understanding these effects and how it can limit, lens, and effect our vision especially at long distances.  Military Science identifies this and addresses it accordingly; for artillery units using distant aiming points are not to exceed 1500 meters or just under one mile in distance, when looking out at lower elevations of below 15 degree.  However at higher angles for lay and safe circle procedures the skies the limit, if you can see it you can use it, meaning celestial bodies such as the sun and stars.  Military Science also addresses refraction and lensing at higher angles.  Meaning once the lay circle and safe circle BUMP or turn an angle on each other using alternate method of lay (survey) they must be within 10mils of each other.  There are 17.8 mils in 1 degree.  By doing this act on a regular basis Military Science has proven refraction and lensing at higher angles does NOT exist or is extremely minimal under 1 degree.    Again this is because Military Science has a high degree of accountability because lives depend on it every day.

The list of military manuals as references for this information are;

1. The U.S. Army, Tactics, Techniques, and Procedures for Corps Artillery, Divisional Artillery, and Brigade Artillery, Artillery Training Planner, ATP 3-09.24, dated 21 November 2012.

2. The U.S. Army Training Circular (TC), Field Artillery Manual Cannon Gunnery, TC 3-09.81, dated April 13, 2016.

3. U.S. Army, Artillery Survey Operations, Field Manual Tactics, Techniques, and Procedures for Field Artillery Survey Operations, FM 6-2, dated 23 September 1993.

4. U.S. Army Field Artillery Cannon Battery Operations Field Manual, FM 6-50, dated 23 December 1996.

5. U.S. Army Artillery Training Planner, The Field Artillery Cannon Battery, ATP 3-09.50 manual dated May 2016.

6. U.S. Army Map Reading, Field Manual, FM 3-25.26 dated January 2005.

7.  U.S. Army Developmental Test Command Test Operations Procedure, Test Operation Procedure 03-2-709, dated 19 November 2010.

8. The U.S. Army, Field Artillery School, Ft. Sill. Oklahoma, The Special Text ST 6-50-20 Executive Officer/Platoon Leader Handbook Cannon Artillery, dated 20 February 1998.

9. Department of the Army, DA-PAM 385-63 Range Safety, dated 10 April 2003.

10. Department of the Army Regulation, AR 385-63, Range Safety (MCO 3570.1C), dated 

30 January 2012.

11. The U.S. Army Field Manual FM 3-09.8 Field Artillery Gunnery, dated July 2006.

 The strategic and fundamental accuracy of military science is vital, lives depend on its safe use and practice every day, and because second place in military science can get you conquered.  

Military Science links

1. Setting up the M2Aiming Circle

https://youtu.be/yHjE3cCr94w

2. Declinating the M2 Aiming Circle

https://youtu.be/gl3L2JeIeuQ

3. Performing Hasty Traverse M2 Aiming Circle

https://youtu.be/3XraXwUHgxY

4. Performing HASTY ASTRO SUN /STAR SHOT using the M2 Aiming Circle

https://youtu.be/zdZg6NvtUD4

5. Magnetic Checks using M2 Aiming Circle verifying lay of survey using grid magnetic

https://youtu.be/LIhlaA9Zdms

The three angles of measurement we need to understand whether they be visual orientation, drawn, or otherwise, these are;    

The measured angle, this can be visual as in survey, mechanical as in engineering, or manual as in a rocking chair.  It’s exact angle is determined using protractors a instrument of measurement to measure exact angles which are in degrees.

Lines of Parallel where two lines one of which a guide angle (visual or otherwise) run side by side maintaining equal distance between. Example of this would be two 90 degree angles running side by side. They neither intersect or increase in separation. 

The guide angle the most important angle to an observable object (elevated of otherwise) generally this angle is at 90 degree and is key in performing triangulation to determine measured angle and distance of the object. It is the primary angle to an object that maybe measured from other angles to it as the primary.   

Time zones can be easily explained in the flat earth model as sun illumination time.  As the sun moves across the earth it not only illuminates the surface of the earth but it heats it as well.  Time zones are merely sun angle time, from full illumination time to no illumination time.  Then broken down by sun movement based on distance coverage or right at 15 degrees an hour.

Flat earth keeping it simple.  Another important factor to consider is that on the flat earth model the sun is only about 50-60 miles in diameter, very small, and if we were to look at it on the flat earth map it would be the size of a pin head, very small.  The sun is shown larger in these diagrams merely for ease of reference.

The 45 degree sector range fan information for 1 degree past line of parallel or OS line of survey.  Even at 1 degree or a direct sun angle reading  of 46 degree at the OS is significant because it now exceeds the globe models tolerance.  You are now off sun target line or line of survey 1,638,664 miles which exceeds the suns width at distance for the heliocentric globe model..  Providing solid evidence of flat earth using the sun, military science, and geometry.  This is the reason Copernicus was afraid to release his model because the earth sun alignment in the Heliocentric model does not align.  And if your alignment is wrong the entire model is wrong.  It's not just a matter of fixing the numbers, your alignment is either on or off, this just shows by how much.

 The suns movement and path as we view moving across our daytime sky.  Our position on earth and the sun season will determine this from the observer.   You will note the sun clock shown in this diagram as well.  Knowing the sun clock position in relation to time is also key.

The flat earth sun clock model as shown, you will note the sun positions are to demonstrate the full range of the suns orbital rotation around the flat earth above it.  Both the sun and moon rotate around earth similar to a needle on phonograph record moving within the prime meridian bands.   The location of the sun in the prime meridian bands determines the sun season, fall, winter, spring, summer.  When the sun is in the Tropic of Capricorn it is winter in the United States, and summer in Australia.  Flat earth made simple.

The enclosed world flat earth model, not all flat earther's  believe in an enclosed system.  For some  the models vary.  This model depicts the entire operating system.  The sun shown here is a projected object which requires a power sources using the star field in the firmament above to provide the required power.  The moon would be a similar operating system as a projected object.  The tides and star field movement maybe interlinked and connected this is because the saltwater facilitates the power grid system just as fluid in a car battery does for that batteries cells.  The stars being made of a crystal quartz, not all are power generators some may only be projected objects within the system.  A canal system which is located around the entire flat earth under Antarctica would facilitate this process.  After all our entire atmosphere is electric, this also would facilitate gravity within the system being electric with elevation being a key factor.  This has already been demonstrated in  an experiment.

The projected sun whether right at the firmament or projected in farther as shown.  The primary light generating source would give off secondary lighting or back-lighting which when viewed by us humans would be extended hours of light in our daytime sky's in the southern hemisphere.  There may also be properties built into the firmament at lower elevations which help illuminate light.  There have also been reports of second sun sightings, this would be explained by a projection device the projects our sun within the enclosed world model, being the main light source.  This would only be seen at very limited locations and for very short periods of time.  Most likely in areas such as Thailand or Malaysia in the southern hemisphere.   Another time this maybe seen is during solar eclipses, exposure time again would be very limited this maybe due to the recessed light at the source or the projection device.

The enclosed world model maybe just one of many, with other civilization's only thousands of miles from our world.  The possibilities are endless.  The celestial night sky maybe a map to where we live, with the pole star being that enclosed worlds model identifier.  As above, so below.

Through the use of STO and SIMO we can remove the Heliocentric globe models long distance game piece off the board.  Meaning the sun, which is now proven to be between 3000 and 4000 miles from earth and not the 93 million miles the heliocentric model tells us.  The actual suns distance can be calculated thru triangulation from measured sun angles as valid evidence of this.  Use of the military science range fan gives us this evidence when we input the heliocentric model data and its shown to be out of tolerance and not by just a little, but by a great margin.  And its not just a matter of fudging the numbers to get it within tolerance.  It doesn't work like that, for each model tested, your either in alignment or out of alignment, this just tells you by how much.  The sun the object of reference is within or inside the triangle.  This effect removes heliocentrism long distance off the board which collapses this model which requires immense distances for its survival.  This now means the sky barrier above us caps out at between 4000- 8000 miles maximum, and what you see in the night sky is actually very close.

1. No experiment has ever proven earths movement.
2. Heliocentrism has never provided a validation test for determining earths true surface shape.
3. The globe model was released after Nicolas Copernicus death, his model was never validated.
4. The Azimuthal Equidistant map used by the USGS is a flat earth map with circumnavigation in all directions.  This map is used by the United Nations.
5. The suns movement within the prime meridian bands Tropic of Cancer, Equator, and Tropic of Capricorn determine the sun seasons.
6. Motion will always be detected especially with water as it seeks it's level.
7. The sky above is a celestial clock as determined centuries ago in the Ptolemaic system this includes sun, moon and stars.
8. Ancient cultures who all displayed a flat earth model; Sumerian, Egyptian, Norse, Mayan, Native American, Celtic, Hindu, Hebrew, Inca.
9.  No one has ever circumnavigated the continent of  Antarctica.

1. Does the sun survey point always need to be at 12:00 hours?  No this is based on the observer location.  The sun needs to be at 90 degree to the observer at the OS.  If that means time is 12:45 this then becomes the 3 hour mark.  Meaning observer times are now 09:45 easterly and 15:45 westerly reading times.  Sun clock time is sun position time to the observer at the OS.
2. When using the right triangle calculator what do I enter for the angle and distance?   The angle for A is the difference from point of parallel.  Meaning if the measured sun angle reading is 46 degree this is 1 degree beyond point of parallel which is 45 degree.  Enter 1 for angle (a).   Distances (b) vary based on the Heliocentric model may vary from 91-94 million miles, based on sun season. 
3. Why is it necessary to use a level vile on the Marx device?  To check cross-level of the device as to not enter another angle or error in the angle reading of the sun at the OS.
4. What facilitated my understanding of this process using the sun?  In reading some of this information it is with the understanding that most, even in our education systems are not exposed or taught this information.  This is not to belittle or make fun of the education system or educators.  What helped me in my journey was my intense exposure to applied geometry within the field of military science.  Artillery specifically is 90% applied geometry in application and principle, this includes survey (celestial) procedures and types of survey, gun-line safety, call for fire, fire direction center processes, and line of parallel in aiming references, and weapons bore-sighting.
5. What's outside the flat earth?  Good question, and depending on who you talk to within the FE community you will get different answers.  Answers vary from land and water to an un-limted plain among some of the most common answers.  But really this is an unknown.
6. How did you get into flat earth?  In my research on giants, flat earth was recommended to me.  I had to laugh when I first saw it, thinking people really believe the earth is flat.  After I started researching flat earth it then became more believable.  From there I started doing my own experiments.   I had to develop  processes and applications from what I knew in military science, and geometry the answer was there.   Once these were completed flat earth became reality.  Experimentation and doing them correctly is key.
7. Do you believe there is space or outer space? Not in the sense as described in the globe heliocentric model.  This area is merely a barrier area from which we cannot pass.  It is also very close, and is the area between earth and the next realm or heaven.

1.  How did you select the name for Operation Resolute Time?   Operation was input because testing was done over a six month period from 7 February to 8 August 2020.  It was one of the most extensive tests conducted in recorded history with regards to the earths true surface shape using the sun.  Resolute because the process and applications of military science are definitive and absolute, not only in the OS setup but applied geometry as well.  The "Time" portion was for timing of the object of reference used (the sun).  You cannot escape timing, or the actual movement of the sun, you can set your watch by it.  Timing is a critical element especially when using the sun survey point.  The sun will show up right near (inches) the sun survey point 24 hours later, the next day.  Again this process and application is definitive.   Hence the proper name given "Operation Resolute Time".
2. Vision or eyesight questions often are asked with regards to earths true surface shape.  Example; If the earth were flat;  Why can't I see England or France from the east-coast of the United States?  Vision is one of the weakest parts of our human anatomy.  Most people have their vision checked annually, part of this eye check is reading letters or figures off a chart at distance.  We can also conduct a vision test of our own with regards to distance and vision acuity.  Take a beverage can and hold it in your hand, you will note the label or brand name then on another part of the can there are ingredients listed in more fine print. With the ingredients facing you extend the can out at arms length and see if you can read the fine print at arms length.  Many may find they cannot see or read the letters even at a small distance of arms length.  You can also take the can with the brand name written in large print and place it out at a distance of 25 feet, 50 feet, and then 100, make note of if you can read the letters, or even when the letters themself disappear as distance is increased.  Now go back to that original question of why can't I see England or France from the east coast of the United States.   Our vision is fair at best, but still one of the weakest parts of the human anatomy.  Our eyes are not designed to see great distances regardless of earths shape.  Other factors affect our vision at lower degrees at the horizon meaning at 10-15 degree (lower elevations).   They include; pollution, weather, temperature, and moisture /water all within our atmosphere, air is thicker at lower elevations.  Another example is; If your unsure, try looking underwater at distances, even on really clear rivers or lakes, you cannot see very far 20-25 feet,  vision may go 50-100 at the greatest distance.  Even sunlight is blocked out in water at very short distances.

Our human body is a a configuration of a tripod and protractor if we break it down into simpler more defined ability.  The human head is a built in protractor, it physically moves in the direction and angle we want to see an object  The human body is the tripod.  It physically stands on the surface of the earth in the desired direction and supports the protractor.  The movement of our head or protractor is the recorded upper motion we physically view an object.  This is also the check angle of measurement.  The position of our body or tripod whether on a flat or curved surface is the recorded lower non-motion we physically stand on.  Any angle our body or the tripod is physically on must be added or accounted for along with the upper recorded motion (our head-protractor) for accuracy.  

This diagram description details the human head or protractor as the recorded upper motion.  This is because our head adjusts on the body or tripod to view an object we want to see.   This angle must be recorded as part of the total composite angle along with the tripod or our human body.

The human body or tripod is the recorded lower non-motion we are physically on.  This angle is part of the total composite angle along with the recorded upper motion or protractor as shown in this diagram.

In question number one can you figure out the correct total composite sum angle?

The answer to question number one, is 55 degree angle.  This is computed by adding the recorded upper motion angle of 35 degree and recorded lower non-motion of 20 degree.  The correct answer is A , 55 degree.

The lines of parallel are not something that's mentioned often in our institutions of learning as lines of parallel.  They do however have common names we can identify easily, they are  definitive and absolute.  They can be increments of measurement just as the lines on a ruler or on a measuring cup, or the left and right  frame of a doorway.  Understanding lines of parallel and you'll walk through the open doorway, make the right measurement whether building or baking.

In more simple terms lines of parallel are like windows as shown in the example.  When the said curved is applied for the globe model as in Operation Resolute Time 2020 this pushes the sun out of the window or lines of parallel 70% of the time it was tested.  Unlike the flat earth model which has no issue in complying with the window or lines of parallel.  We must remember the guide angle which is set at 90 degree by the sun survey point pins the observer(s) to 90 degree total.  This can only be exceeded if the objects said size at distance falls within the allowable tolerance.  Example of this would be 90.3 for the heliocentric models sun at size and distance of 93,867,000 miles.  At one degree past line of parallel is 1,638,664 miles, the sun (965,370 miles in size) half sun at (482,685 miles in size) miles wide, this far exceeds the suns actual size.  Remember we are measuring sun angle from center mass of the sun on line of sun survey at the OS.  The globe model still failed by a great margin even when allowed this additional tolerance.  The high sun works against the heliocentric model.  You will note the recorded upper motion which is the actual physical measure angle from earths surface is added with the observer angle to the object of reference the sun or what is called the recorded lower non-motion.   When added together this composite sum angle must be within 90 degree or the allowed tolerance for that model at size and distance.  This then transitions to each models orbital mechanics which is earth to sun alignment, and why it is soo very important.  If your alignment is off as shown in the heliocentric globe model your entire model is invalid.

In the check on learning question, will use lines of parallel in an everyday use

which for many people may not realize its very common use.   This is to demonstrate lines of parallel every day use in our lives as a common occurrence, to which they are both definitive and absolute. 

The answer to question one example on lines of parallel using a doorway.    The doorway has definitive size measurements both horizontal and vertical.  The measurements given  for the doorway opening is 39" wide by 81" in length.    In the selections given choice A exceeds the line of parallel (Height) by 3", and choice C exceeds the line of parallel (width) by 3".  The correct answer is B, which falls in the correct doorway width of 39" and height of 81".  This is the first example of lines of parallel we use in our everyday lives, but may not recognize.

In this check on learning question, select the right amount of flour Jenny needs to put into the measuring cup using the recipe amount given.  Review the information and diagram information and select the correct answer.

The answer to question #2 measuring cup.  Jenny is required to add 3 cups of flour per the recipe.  The correct answer is B.  Choice A is 4 cups which is to much flour, and selection C and D are 1 and 2 cups which is not enough flour per the recipe given.  Selection B (3 cups) is within the lines of parallel per the recipe (limit).  This is just another common everyday example with regards to lines of parallel we use.

Sometime exceeding lines of parallel such as a train on the railroad tracks can have disastrous effects.  The railroad tracks being lines of parallel in engineering.  A derailed train is an example of exceeding the lines of parallel in real world application in engineering.

You unknowingly for many are the expert in line of parallel.  Performing it on average 50+ times daily.  Examples such as pressing keys on touch pads to keyboards on computers, phones, or remote controls.  Other examples range from eating (putting food in your mouth) to driving a car, walking along a sidewalk to sitting in a chair are all examples of line of parallel.  It is in our everyday life.

In this example given using SIMO, we can see now how the lines of parallel are formed from two OS stations at distance in testing the globe models 45 degree sector.  The first OS is the master station and sets the guide angle in at 90 degree.  This now pins BOTH observers to that 90 degree mark.  Or in more simpler terms line of parallel is now 90 degree for total sum composite angle from both stations (master and flank).  We must remember the master station observer has set the edge at 90 degree while flank station observer is looking (measuring direct angle) center mass to the object of reference the sun.  The sum composite can only be exceeded by the object of reference known size at distance.  A sector range fan is used to determine accurate size at distance.  In this example given the line of parallel is exceeded for the globe model by 10 degree.  The measured angle to the sun was 55 degree, when added with the said curve this totals 100 degree (surface angle of 45 degree).  The globe model now has failed the 45 degree sector test by 10 degrees.  The extended scale was put in to give a better view of what actually occurs from the flank observer.  This now pulls that observer (flank station) off by 10 degrees.

Operation Resolute time 2020 conducted from 7 February to 8 August 2020 in Kabul, Afghanistan.  With 81 experiments conducted, measured direct sun angles at an elevation of 5,963' above sea level.  Test and experiment results were applied to both the globe and flat earth model.  Of significance 70% or 57 of a total of 81 test results exceeded the globe models parameter.  This result was catastrophic geometric failure for the globe model.  This is because the globe model was given significant advantages of both distance from the northern most prime meridian the Tropic of Cancer at 765 miles, and tests conducted at high elevation just under 6000' above sea level.  Both of these factors should have resulted in significantly lower sun angle readings if the globe model is to be valid.

Operation Resolute Time Data from 7 February to 11 April 2020.  Sun season late Winter to early Spring.  Data includes; Date and Time of Observation,Direct Sun Angle Reading from the OS (Easterly and Westerly), Azimuth of the sun from the OS, Elevation at the OS, Sun at the OS, and Remarks.

Operation Resolute Time Data from 16 April to 12 May 2020.  Readings indicated in the green boxes indicated measured surface angle to the sun exceeding 45.5 degree or geometric failure for the globe model.  Sun season Spring, early and late.

Operation Resolute Time Data from 13 May to 7 June 2020.  Readings indicated in the green boxes indicated measured surface angle to the sun exceeding 45.5 degree or geometric failure for the globe model.  Sun season late Spring to early Summer.

Operation Resolute Time Data from 8 to 21 June 2020.  Readings indicated in the green boxes indicated measured surface angle to the sun exceeding 45.5 degree or geometric failure for the globe model.  Sun season, Summer.

Operation Resolute Time Data from 28 June to 11 July 2020.  Readings indicated in the green boxes indicated measured surface angle to the sun exceeding 45.5 degree or geometric failure for the globe model.  Sun season, Summer.  Yellow boxed information note multiple observers taking readings.

Operation Resolute Time Data from 12 July to 3 August 2020.  Readings indicated in the green boxes indicated measured surface angle to the sun exceeding 45.5 degree or geometric failure for the globe model.  Sun season, Summer.

Operation Resolute Time Data from 7 to 8 August 2020.  Readings indicated in the green boxes indicated measured surface angle to the sun exceeding 45.5 degree or geometric failure for the globe model.  The final reading taken on 7 August 2020.  Sun season, Summer.

Operation Resolute Time 2020 was one of the most extensive tests  over 6 month period ever conducted in determination of earths true geometric shape.  The globe model failed to meet the test requirement standard 70% of all testing, while the flat earth model passed all 100% of testing.  Testing of the 45 degree sector whether you believe in the globe or flat earth model was set in place using the sun, geometry and military science applications.  Results of tests conducted provide solid evidence of earths true geometric surface shape as being flat.  Further testing should be conducted inside the prime meridian zones and the southern outside zone.

Operation Resolute Time 2020 testing zone was 765 miles north of the northern most prime meridian the Tropic of Cancer at an elevation of 5,963' above sea level.  When applied the test result readings to both the globe and flat earth models, the globe model suffered geometric failure 70% (57 of 81 tests) of all tests, while the flat earth model passed all 100% of tests.  The globe model failed to take major advantages of distance from the prime meridian and elevation when tested.

Understanding OS position and its relation to the sun and its path of movement both inside and outside the prime meridian zone.  You will note for angle readings which are off of the direct east west line, the farther the sun is the lower measured sun angles are as shown in this diagram.  Of importance is also the drift to the southwest which is an indicator and evidence of the orbital movement of the sun as it moves within the lines of meridian above the flat earth.

Earth sun alignment is paramount for any model we are to view and evaluate as real.  Measuring direct sun angles from the earths surface will give the details of just how far off the heliocentric model is when we look at earth to sun alignment.  When applied data from Operation Resolute Time 2020 shows just how far the heliocentric model is off.  It's not just a matter of recalculating to try and correct the heliocentric model, it doesn't work like that.  Its a matter of direct sun angle reading (alignment of the earth and sun) that show just how far off the heliocentric model really is.   The heliocentric globe model requires a low sun in the 45 degree sector for it's orbital mechanics to work.  However the high measured sun angles (46 degree and more) in the 45 degree sector test provide solid evidence of orbital failure for the heliocentric globe model.  In other words the sun is to high in the sky for that models orbital mechanics to work.  While the flat earth orbital mechanics easily meets the requirement with the high sun.  

The orbital mechanics RED zones as shown which exceed the heliocentric model orbital mechanics, or in better terms areas of major geometric failure.  Distances this model is off range from between 8 to over 10 million miles off earth sun alignment.   What does this mean?  In using the object of reference the sun, this means this orbit of the earth does not exist as shown in areas of red.  This is why one must use the sun as your first step in determining your model, because if the alignment is off here it transitions to everything else within the heliocentric said model.  This is the main reason I conducted testing of earth sun alignment to validate if the heliocentric model was correct, extensive tests conducted in Operation Resolute Time 2020  tell us that the heliocentric globe model is very flawed geometrically and does not meet the standard.

When tested in Operation Resolute Time 2020 and now in Operation North American Sun 21 the Geocentric Flat Earth model when tested meets earth to sun correct measured angular measurements (alignment) which is required to support the models orbital mechanics above the flat earth.  All measured angles meeting the tested requirements in the 45 degree sector validation test with results at 100% pass rate.  This is because the OS station is at 0 degree and all measured sun angles are 90 degree and below, giving the composite sum angle totals well within tolerance for this model.  These results mean the high sun in the summer sun season supports the flat earth models orbital mechanics rotation above the surface of the earth.  The three suns in the diagram show the suns operating range within the three prime meridian bands (North-Tropic of Cancer, Center-Equator, South-Tropic of Capricorn).

The earth sun alignment effects and how to determine alignment based on actual measured direct sun angles.  Of note is the numbers exceeding point or line of parallel.  Using right triangle calculator these numbers can be inputted to determine if the heliocentric model information we are given is accurate with what we see in nature our reality.

The step process when using distant aiming references which must take into consideration the object of reference said size and distance.  Use of the sun survey point is essential in measurements and earth to sun alignment.  This step must be accomplished prior to taking measurements.  In other words the geometric edge must be set at the observer OS for geometric accuracy.