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This page contains the earlier versions of TLE2ECL.
Beta 1:
The first release.
Download it here (13 kb)
Beta 2:
Second release with some bug fixes:
- Converted Semi-major axis was 3 kilometers too high.
- Converted MJD was 1 day too high.
Download it here (13 kb)
Beta 3 release 1:
The third release.
Additional features:
- The user can specify the file which the TLE data is.
- The user can choose the satellite elements in the TLE file (if there is more than one).
- The way of opening a satellite from the default TLE2ECL.txt file is also included.
- Multiple satellite choice. Now you can specify a file which has more than one satellite TLE data and choose among the
satellites in the file.
Known bugs:
- The ecliptical mean anomaly and the ecliptical argument of perigee aren't very accurate. This is OK
if you don't want to simulate the real ISS position, for example, or use ORBITER for satellite tracking purposes.
This bug will, hopefully, be fixed in one of the next releases.
- If the data is not in the correct format specified in the readme file, then the results will be erroneous.
Download here (20 kb)