I'm looking for pointers to good example code/descriptions of algorithms for handling TLEs and converting between multiple epochs and orbit propagation models. The aim is to improve the existing TLE-handling Tcl code in SaVi (http://savi.sourceforge.net/), which is really only good for satellites whose TLEs use the same epoch right now. SaVi has reasonably fair visualisation display capabilities (for a free package), but it's all a bit abstract and idealised, and not yet useful for the kind of real-time simulation needed for tracking or observation. thanks, L. <http://www.ee.surrey.ac.uk/Personal/L.Wood/><L.Wood@surrey.ac.uk> ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www.satellite.eu.org/seesat/seesatindex.html
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