Below is the current State Vector and Keplerian Elements for <br />STS-107. The vector data comes from NASA; the Keplerian Elements <br />were computed from the vector. <br /><br /><br />This file may be read by VEC2TLE version 9648 to update your <br />Keplerian Elements text file.<br /><br /><br />Vector format = 117<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03019.16974189800<br /> 01/19/2003 04:04:25.699 UTC<br />EFG E: -19254705.000000 ft<br /> F: 2264583.00000000 ft<br /> G: 10064554.0000000 ft<br /> Edot: -8084.0600000000 ft/s<br /> Fdot: -20007.509999999 ft/s<br /> Gdot: -10870.659999999 ft/s<br />ndot/2 (drag): 0.00022464485 rev/day^2<br />nddt/6: 2.10682E-09 rev/day^3<br />Bstar: 4.67758E-05 1/Earth Radii<br />Elset #: 8<br />Rev @ Epoch: 41.36877035269<br /><br /><br />Launch Occurred: 2003-JAN-16 1539:00.075 UTC<br /><br /><br />The following Keplerian elements were computed by VEC2TLE from the<br />vector, using a 0.5 drag multiplier:<br /><br /><br />STS-107 <br />1 27647U 03003A 03019.16974190 .00022464 21068-8 46776-4 0 80<br />2 27647 39.0140 212.4286 0012147 9.7385 123.0182 15.97851869 418<br /><br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03019.16974190<br />Element set: 8<br />Inclination: 39.0140 deg<br />RA of node: 212.4286 deg<br />Eccentricity: 0.0012147<br />Arg of perigee: 9.7385 deg<br />Mean anomaly: 123.0182 deg<br />Mean motion: 15.97851869 rev/day<br />Decay rate: 2.24645e-04 rev/day^2<br />Epoch rev: 41<br />Checksum: 293<br /><br /><br />VEC2TLE may be downloaded from http://www.orbitessera.com<br /><br /><br />Ken Ernandes<br />n2wwd@amsat.org<br />http://www.orbitessera.com