Scenario Is it possible to use equatorial fixed reference system for RPOS and RVEL when creating a scenario file?

[supersonic71]

I'm trying to write a script to convert a list of TLEs to Orbiter's Scenario format.

For example - convert this https://celestrak.org/NORAD/elements/gp.php?GROUP=starlink&FORMAT=tle
to something like

STARLINK-24:starlink\starlink_odd
  STATUS Orbiting Earth
  RPOS A B C
  RVEL E F G
END
STARLINK-61:starlink\starlink_odd
  STATUS Orbiting Earth
  RPOS H I J
  RVEL K L M
END
...
...
...

Scenario Editor TLE

Modified version of Scenario Editor with NORAD TLE (Two-Line Element Sets) import support.Used NORAD SGP4/SDP4 orbital model for calculation state/speed vectors of earth-orbiting objects.C++ Source code for the SGP4/SDP4 algorithms was developed...

www.orbiter-forum.com

Used code from above addon to convert TLE to equatorial-fixed reference system.
But looks like Orbiter .scn file expects RPOS and RVEL in Elliptical reference, correct?
Is it possible to make orbiter accept equatorial-fixed values in its .scn?

 

[supersonic71]

Found an old thread : https://www.orbiter-forum.com/threads/orbiter-and-tle-data.36522/
There's a tool by Ajaja called eq_to_ecl which converts TLE to ELEMENTS
I think I'll just use that instead of RPOS/RVEL
Thanks @Marijn !