SUMMARY
This discussion focuses on calculating each planet's angle from its argument of perihelion, specifically seeking a chart that illustrates this angle over time on Earth. The user distinguishes between needing a chart and an ephemeris, emphasizing the requirement for the angle along the elliptical path, known as the true anomaly. The discussion references the JPL (Jet Propulsion Laboratory) charts, which provide the Longitude of the Ascending Node (LAN) and the Longitude of the Perihelion (LP). The formula for calculating the Argument of Perihelion (PA) is established as PA = LP - LAN.
PREREQUISITES
- Understanding of celestial mechanics and orbital elements
- Familiarity with the concepts of Longitude of the Ascending Node (LAN) and Longitude of the Perihelion (LP)
- Basic knowledge of 3D geometry and angles in astronomy
- Experience with astronomical data sources, particularly JPL resources
NEXT STEPS
- Research how to derive true anomaly from orbital elements
- Explore advanced celestial mechanics textbooks for deeper insights
- Learn to use JPL's SPICE toolkit for planetary position calculations
- Investigate software tools for visualizing planetary orbits and angles
USEFUL FOR
Astronomers, astrophysicists, and students studying celestial mechanics who need to calculate and visualize planetary angles and orbits.