Editing Science/Memorandum Series

{{UI Accordion
| '''M001: Keplerian Orbit Elements to Cartesian State Vectors'''
| 
This Memorandum contains an algorithm for converting a traditional set of {{sc|Kepler}}ian Orbit Elements (semi-major axis, eccentricity, argument of periapsis, longitude of ascending node, inclination, and mean anomaly) to cartesian state vectors (position and velocity vector).

'''Keywords:'''<br />
Kepler, Orbit, Elements, Cartesian, State, Vector, Rotation, Matrix
<hr />
'''Download:''' http://downloads.rene-schwarz.com/dc/category/19
| '''M002: Cartesian State Vectors to Keplerian Orbit Elements'''
|
This Memorandum contains an algorithm for converting cartesian state vectors (position and velocity vector) to a traditional set of {{sc|Kepler}}ian Orbit Elements (semi-major axis, eccentricity, argument of periapsis, longitude of ascending node, inclination, and mean anomaly).

'''Keywords:'''<br />
Kepler, Orbit, Elements, Cartesian, State, Vector
<hr />
'''Download:''' http://downloads.rene-schwarz.com/dc/category/20
}}