2024年1月26日 · Hello everyone, I am new to Orbital mechanics and have put together some code that other folks might find helpful. The code demonstrates the use of Orekit for satellite …

2023年11月9日 · Following the major release of v12.0, an updated version of the Orekit Python Wrapper is released. The v12.0 Orekit is a major release and contains lots of new features as …

2025年3月26日 · Orekit (and related projects) community support. Hi all! With the Orekit development team we would like to perform a survey of scientific publications (i.e., conference …

2023年11月8日 · Many thanks to you for taking charge of this release. I know it’s been hard work . And an even bigger thank you to all the contributors who keep this project alive by constantly …

2023年8月21日 · Hi all! With the Orekit development team we would like to perform a survey of scientific publications (i.e., conference papers, peer review papers, master thesis, PHD thesis, …

2024年4月5日 · Dear all, I am currently trying to measure the effects of higher order perturbations and drag on the nominal trajectory of a satellite over 3 days. The method I am using is: …

2025年1月28日 · Hey, folks! My 2-month orbit propagation (60s steps) runs in ~30min with gravity alone but jumps to 103min when adding atmospheric drag. Including other forces (SRP, third …

2023年10月8日 · Your Orekit code is good. But I maybe understood why you have differences. Please find below the description of STK’s J2Perturbation:

2022年3月7日 · Hi all, I am new to Orekit and trying to use it in Matlab. My goal is to create two orbits that are equal to within a few centimeters. One of the orbits will be the basis for a later …

2024年8月16日 · I believe I have discovered a synergistic bug when combining the kalman filter code with both a DynamicOutlierFilter and a dynamic process noise generator. The short …