The initial orbital data are distributed in the F1 format, which contains orbital elements as a the state vector (the spacecraft position and velocity vector) in the inertial frame (Standard reference of the Earths Equator and Equinox J2000).
This data set includes the following information:
INT | |
ITZ | |
01 | |
0001 | |
01 | |
00001 | |
030895 | |
011330887 | |
-001451.596 | |
-008276.384 | |
+000000.000 | |
+3.35109584 | |
-4.23559072 | |
+7.86668273 |
The F1 format for this data looks as follows:
INT/ITZ/01/0001/01/00001/
030895/011330887/
-001451.596/-008276.384/+000000.000/
+3.35109584/-4.23559072/+7.86668273/
5873/ZZ
The last line contains the checksum and the end of data symbol ZZ.