Welcome to Discourse [Uncategorized] (1)
Frame Conversion ( True of Date to True of Epoch) [Orekit usage] (13)
Asteroid propagation not matching MPC results [Orekit usage] (5)
Converting from TEME to EME2000 Frame [Orekit usage] (5)
Parameters in State and STM [Orekit usage] (3)
Implementing a state transition matrix (STM) in python [Orekit usage] (5)
Geodetic to geocentric coordinates - strange behaviour [Orekit usage] (3)
Problem with Numerical Propagator Tolerances [Orekit usage] (3)
Advice on dihedral FoV construction [Orekit usage] (4)
Orekit Python Wrapper for python 3.7 released [Orekit usage] (1)
How to show unresolved issues? [Site Feedback] (3)
Impulse Maneuvers when initial state not at the start of propagation [Orekit usage] (4)
Adding constant thrust maneuvers to DSST propagator [Orekit usage] (7)
Orbit propagation - modified initial orbit? [Orekit usage] (9)
Advice on setting up an orbit propagation loop [Orekit usage] (3)
clearFactories() method from test class Utils [Orekit usage] (6)
Is there anyway I can find the short routing from one satellite to another at certain time [Orekit usage] (2)
RA-Dec to AzEl conversion [Orekit usage] (2)
Migration to Gitlab [Orekit development] (7)
Combine Old and New WMM Files [Orekit usage] (2)
OreKit for embedding into hardware [Orekit usage] (3)
Receive all posts via email? [Site Feedback] (6)
How to determine satellites with the same orbit from TLE file [Orekit usage] (4)
DSST propagator initialization [Orekit usage] (2)
Endless loop while creating mean orbit? [Orekit development] (5)
Setting up uncertainties in force models for field propagation [Orekit usage] (3)
Get distance between two satellites [Orekit usage] (6)
Using Jenkins multibranch pipeline for continuous integration [Orekit development] (10)
Project Persephone - revival and improvement of SpriteOrbits [Orekit usage] (5)
SP3 Parser Crash [Orekit usage] (10)