Determining the Argument of the Perihelion of the Earth: Which Value is Correct?

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In summary, the two values for the Argument of the Perihelion of the Earth are w=114.20783 @J2000 and w=282.9404*4.70935e-5*d. The first value is specific to a particular epoch and to that epoch only, while the second is a more general expression that represents the time variability as a linear function of time.
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Philosophaie
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I have seen conflicting values for the angle where the Argument of the Perihelion of the Earth or where the Winter Solstice(Dec 21) strikes. This is where the ellipse value of the True Anomaly is zero. The two values are: w=114.20783 @J2000 or w=282.9404*4.70935e-5*d where d is a formula encompassing the Julian Date. These values have different Longitude of the Ascending Node by that is just where all the planets are referenced at and does not change the Argument of the Perihelion. My question is: which is the correct Argument of the Perihelion of the Earth?
 
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Normally, orbital elements are given with respect to the ecliptic plane. Argument of perihelion is the amount of degrees that separates the longitude of perihelion from the longitude of the ascending node. But Earth's orbit by definition has no inclination since Earth's orbit defines the ecliptic. Therefore, it has no ascending node.

In reality, Earth does have a little bit of inclination since inclination is an oscillating orbital element, we can only define it at 0 for an instant in time, which was Jan 1, 2000. Although it has drifted a small amount since then, it is still effectively 0, meaning that the ascending node is weakly defined, and can rapidly change.

Winter solstice has nothing to do with perihelion. It's when Earth's tilt is directed away from the Sun from the Northern hemisphere.
 
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Philosophaie said:
I have seen conflicting values for the angle where the Argument of the Perihelion of the Earth or where the Winter Solstice(Dec 21) strikes.
The winter solstice does not occur at perihelion, and neither value is constant. The Earth's axial tilt changes largely because of lunisolar precession. The time between solstice and perihelion passage changes because of anomalistic precession.

Note that longitude of ascending node is not a particularly well-defined concept for the Earth's orbit, and hence neither is the argument of perihelion particularly well-defined. Astronomers prefer to use longitude of perihelion when describing the Earth's orbit.

This is where the ellipse value of the True Anomaly is zero. The two values are: w=114.20783 @J2000 or w=282.9404*4.70935e-5*d where d is a formula encompassing the Julian Date.
A couple preliminary questions: Where did you get these values? Are you sure you are interpreting them correctly? Regarding your values: One value is specific to a particular epoch and to that epoch only. The other is a more general expression that represents the time variability as a linear function of time. Both might well be correct; post your sources.
 

1. What is the Argument of the Perihelion?

The Argument of the Perihelion is a term used in astronomy to describe the angular distance between the ascending node (where an orbit crosses the plane of reference) and the point of closest approach to the sun (known as the perihelion) in an elliptical orbit.

2. How is the Argument of the Perihelion calculated?

The Argument of the Perihelion is calculated by taking the difference between the longitude of the ascending node and the longitude of the perihelion. This value is then expressed in degrees or radians.

3. What is the significance of the Argument of the Perihelion?

The Argument of the Perihelion is important because it helps to determine the shape and orientation of an orbit. It can also provide information about the gravitational forces acting on an object in orbit.

4. How does the Argument of the Perihelion change over time?

The Argument of the Perihelion can change over time due to various factors such as the gravitational influence of other objects in the solar system, the precession of the orbit, and the effects of relativity. It can also change in response to changes in the mass or shape of the object in orbit.

5. Can the Argument of the Perihelion be used to predict future orbits?

Yes, the Argument of the Perihelion can be used to predict future orbits of objects in our solar system. By tracking changes in this value, scientists can make predictions about the path an object will take in its future orbits around the sun.

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