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