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author | Emile <hanemile@protonmail.com> | 2019-09-27 20:41:33 +0200 |
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committer | Emile <hanemile@protonmail.com> | 2019-09-27 20:41:33 +0200 |
commit | 48dec4828b554582521baba3597f2c0c9532774d (patch) | |
tree | 7bbf12b25ba26cc378b6f74e580b5bb9f1a64f75 /README.md | |
parent | 964794bd9876e0ef0cde7995e6c1c763aa20c2b9 (diff) |
keppler orbital elements to cartesian state vectors
Diffstat (limited to 'README.md')
-rw-r--r-- | README.md | 4 |
1 files changed, 4 insertions, 0 deletions
diff --git a/README.md b/README.md index d8445d6..7f82c95 100644 --- a/README.md +++ b/README.md @@ -44,3 +44,7 @@ dump a specific TLE The TLE is searched by printing the first tle matching the given name. So by searching for `SIRIUSSAT` from the `stations` category, the TLE of the first match (`SIRIUSSAT-1`) will be returned, not `SIRIUSSAT-2`. + +## Links + +Convert Keppler Orbital Elements to Cartesian State Vectors: https://downloads.rene-schwarz.com/download/M001-Keplerian_Orbit_Elements_to_Cartesian_State_Vectors.pdf |