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 />This file may be read by VEC2TLE version 9648 to update your <br />Keplerian Elements text file.<br /><br />Vector format = 117<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03029.54489699100<br /> 01/29/2003 13:04:39.100 UTC<br />EFG E: 18240824.0000000 ft<br /> F: 9119790.00000000 ft<br /> G: -7766690.0000000 ft<br /> Edot: -13244.030000000 ft/s<br /> Fdot: 15323.9200000000 ft/s<br /> Gdot: -13206.879999999 ft/s<br />ndot/2 (drag): 0.00027557955 rev/day2<br />nddt/6: 3.16401E-09 rev/day3<br />Bstar: 4.76940E-05 1/Earth Radii<br />Elset #: 38<br />Rev @ Epoch: 207.59517721922<br /><br />Launch Occurred: 2003-JAN-16 1539:00.075 UTC<br /><br />The following Keplerian elements were computed by VEC2TLE from the<br />vector, using a 0.5 drag multiplier:<br /><br />STS-107 <br />1 27647U 03003A 03029.54489699 .00027558 31640-8 47694-4 0 387<br />2 27647 39.0187 143.0425 0009436 119.6228 94.6414 16.01133712 2078<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03029.54489699<br />Element set: 38<br />Inclination: 39.0187 deg<br />RA of node: 143.0425 deg<br />Eccentricity: 0.0009436<br />Arg of perigee: 119.6228 deg<br />Mean anomaly: 94.6414 deg<br />Mean motion: 16.01133712 rev/day<br />Decay rate: 2.75580e-04 rev/day2<br />Epoch rev: 207<br />Checksum: 308<br /><br />VEC2TLE may be downloaded from http://www.orbitessera.com<br /><br />To receive automatic Space Shuttle orbital data updates by email, send <br />a message to listproc@spacelink.nasa.gov, with the following contents:<br /><br />subscribe STSTLE [your first and last name]<br /><br />Use the same procedure to terminate an email subscription, <br />substituting "unsubscribe" for "subscribe" in the message text.<br /><br />Ken Ernandes<br />n2wwd@amsat.org<br />http://www.orbitessera.com