|
Welcome to Discourse
|
|
0
|
1805
|
August 6, 2018
|
|
Libration Family Orbit Access
|
|
1
|
34
|
March 13, 2025
|
|
Error when building Orekit using Maven DefaultDataContextPlugin
|
|
4
|
16
|
March 13, 2025
|
|
TLE data as input using ApsideDetector's implementation method
|
|
2
|
29
|
March 7, 2025
|
|
The mean semi-major axis is used to calculate the satellite altitude problem
|
|
3
|
54
|
March 6, 2025
|
|
TLE orbital propagation
|
|
4
|
64
|
March 5, 2025
|
|
CR3BP Frame Transformation - JavaError ("Cannot Normalize a Zero Norm Vector")
|
|
1
|
29
|
March 4, 2025
|
|
Is it okay to repost the job ad (revised)?
|
|
0
|
57
|
February 26, 2025
|
|
Estimating the parameter of onboard electric thruster in analytical and semi-analytical algorithm?
|
|
2
|
32
|
February 21, 2025
|
|
Orbit Determination with N-body attraction
|
|
5
|
502
|
February 10, 2025
|
|
Issue with IGRF model
|
|
14
|
62
|
February 8, 2025
|
|
Bug in OD with multiple CD estimation?
|
|
8
|
62
|
February 4, 2025
|
|
When using Orekit for orbit prediction with an atmospheric drag model, the predicted orbit 10 days out shows a 6-second difference compared to STK
|
|
25
|
334
|
January 28, 2025
|
|
Issues when trying to use FootprintOverlapDetector
|
|
1
|
28
|
January 28, 2025
|
|
CssiSpaceWeatherData class Issue in python
|
|
2
|
48
|
January 20, 2025
|
|
Time-dependent gravity coefficients
|
|
2
|
32
|
January 15, 2025
|
|
DSST Shadow Function Clarification
|
|
6
|
80
|
January 9, 2025
|
|
Phase Angle calculation between two stars
|
|
3
|
56
|
January 7, 2025
|
|
How to correctly set up force models?
|
|
2
|
67
|
January 6, 2025
|
|
Using XYZ position and speed information from the satellite navigation GPS data as input (in WGS84 coordinate system), orbit correction or forecast orbit for ground station tracking
|
|
9
|
133
|
January 3, 2025
|
|
Happy Holidays to the community!
|
|
3
|
43
|
January 1, 2025
|
|
Kalman filtering, TDM fabrication
|
|
3
|
49
|
December 28, 2024
|
|
ApsideDetector detects the perigee apogee time and the corresponding orbital altitude
|
|
1
|
19
|
December 25, 2024
|
|
There is an error in the code when adding some mechanical models to the dispersion model for the propagation of signals along the transmission line
|
|
1
|
28
|
December 23, 2024
|
|
Finding Sat roll angle to topocentric frame
|
|
2
|
476
|
December 23, 2024
|
|
Multiple ImpulseManeuvers
|
|
2
|
48
|
December 20, 2024
|
|
Is it a bug in the estimation/performance in the Orekit tutorial?
|
|
7
|
65
|
December 9, 2024
|
|
Modifiers and parameter drivers in multiplexed measurements
|
|
2
|
43
|
December 6, 2024
|
|
Keplerian Orbital Elements Convert to TLE Format
|
|
5
|
93
|
December 2, 2024
|
|
SGP4 vs. Keplerian vs. Numerical Propagator
|
|
1
|
122
|
November 29, 2024
|