STS-107 <br />1 27647U 03003A 03018.29469453 .00022218 20611-8 46633-4 0 53<br />2 27647 39.0167 218.2620 0012306 2.7745 129.0843 15.97706352 273<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Centered Inertial State Vector:<br /><br />Vector format = 7<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03018.29469452500<br /> 01/18/2003 07:04:21.606 UTC<br />ECI X: 5881.02487925676 km<br /> Y: -258.62834087729 km<br /> Z: 3113.11400718382 km<br /> Xdot: 2.03343639827535 km/s<br /> Ydot: 6.71834590631216 km/s<br /> Zdot: -3.2564179952151 km/s<br />ndot/2 (drag): 0.00022218151 rev/day^2<br />nddt/6: 2.06106E-09 rev/day^3<br />Bstar: 4.66328E-05 1/Earth Radii<br />Elset #: 5<br />Rev @ Epoch: 27.36627585360<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03018.29469453<br />Element set: 5<br />Inclination: 39.0167 deg<br />RA of node: 218.2620 deg<br />Eccentricity: 0.0012306<br />Arg of perigee: 2.7745 deg<br />Mean anomaly: 129.0843 deg<br />Mean motion: 15.97706352 rev/day<br />Decay rate: 2.22182e-04 rev/day^2<br />Epoch rev: 27<br />Checksum: 283<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

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

STS-107 <br />1 27647U 03003A 03019.42023049 .00022586 21294-8 46753-4 0 99<br />2 27647 39.0177 210.7560 0012079 10.9170 124.9129 15.97957824 457<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Centered Inertial State Vector:<br /><br />Vector format = 7<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03019.42023048600<br /> 01/19/2003 10:05:07.913 UTC<br />ECI X: 5954.08619127898 km<br /> Y: -639.88207134047 km<br /> Z: 2910.61197849018 km<br /> Xdot: 2.42047708740903 km/s<br /> Ydot: 6.46365630641237 km/s<br /> Zdot: -3.5004749996821 km/s<br />ndot/2 (drag): 0.00022585549 rev/day^2<br />nddt/6: 2.12945E-09 rev/day^3<br />Bstar: 4.67529E-05 1/Earth Radii<br />Elset #: 9<br />Rev @ Epoch: 45.37730662280<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03019.42023049<br />Element set: 9<br />Inclination: 39.0177 deg<br />RA of node: 210.7560 deg<br />Eccentricity: 0.0012079<br />Arg of perigee: 10.9170 deg<br />Mean anomaly: 124.9129 deg<br />Mean motion: 15.97957824 rev/day<br />Decay rate: 2.25855e-04 rev/day^2<br />Epoch rev: 45<br />Checksum: 294<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 03020.33348184 .00023157 22380-8 46944-4 0 129<br />2 27647 39.0180 204.6631 0011388 21.7988 336.3744 15.98344336 609<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Centered Inertial State Vector:<br /><br />Vector format = 7<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03020.33348184000<br /> 01/20/2003 08:00:12.830 UTC<br />ECI X: -6113.3098596272 km<br /> Y: -2612.5101103699 km<br /> Z: -143.13900735814 km<br /> Xdot: 2.27778779901154 km/s<br /> Ydot: -5.5746888654122 km/s<br /> Zdot: 4.87894099369440 km/s<br />ndot/2 (drag): 0.00023156678 rev/day^2<br />nddt/6: 2.23797E-09 rev/day^3<br />Bstar: 4.69438E-05 1/Earth Radii<br />Elset #: 12<br />Rev @ Epoch: 60.99492583940<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03020.33348184<br />Element set: 12<br />Inclination: 39.0180 deg<br />RA of node: 204.6631 deg<br />Eccentricity: 0.0011388<br />Arg of perigee: 21.7988 deg<br />Mean anomaly: 336.3744 deg<br />Mean motion: 15.98344336 rev/day<br />Decay rate: 2.31567e-04 rev/day^2<br />Epoch rev: 60<br />Checksum: 289<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 03020.87799617 .00023590 23222-8 47345-4 0 133<br />2 27647 39.0161 201.0276 0010715 28.8712 227.3389 15.98536365 687<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Centered Inertial State Vector:<br /><br />Vector format = 7<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03020.87799616900<br /> 01/20/2003 21:04:18.869 UTC<br />ECI X: -314.31149697887 km<br /> Y: 5266.46848772419 km<br /> Z: -4071.3380167036 km<br /> Xdot: -7.5200958948634 km/s<br /> Ydot: -1.3546129544756 km/s<br /> Zdot: -1.1627149958496 km/s<br />ndot/2 (drag): 0.00023590056 rev/day^2<br />nddt/6: 2.32224E-09 rev/day^3<br />Bstar: 4.73450E-05 1/Earth Radii<br />Elset #: 13<br />Rev @ Epoch: 68.71169428567<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03020.87799617<br />Element set: 13<br />Inclination: 39.0161 deg<br />RA of node: 201.0276 deg<br />Eccentricity: 0.0010715<br />Arg of perigee: 28.8712 deg<br />Mean anomaly: 227.3389 deg<br />Mean motion: 15.98536365 rev/day<br />Decay rate: 2.35901e-04 rev/day^2<br />Epoch rev: 68<br />Checksum: 304<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 03021.83598380 .00024165 24362-8 47459-4 0 157<br />2 27647 39.0157 194.6347 0010784 36.8987 341.3893 15.98916153 849<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Fixed Greenwich State Vector:<br /><br />Vector format = 117<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03021.83598379600<br /> 01/21/2003 20:03:48.999 UTC<br />EFG E: -17976847.000000 ft<br /> F: 11576762.0000000 ft<br /> G: 4279610.00000000 ft<br /> Edot: -7480.5500000000 ft/s<br /> Fdot: -17294.950000000 ft/s<br /> Gdot: 15215.1000000000 ft/s<br />ndot/2 (drag): 0.00024164906 rev/day^2<br />nddt/6: 2.43622E-09 rev/day^3<br />Bstar: 4.74594E-05 1/Earth Radii<br />Elset #: 15<br />Rev @ Epoch: 84.05079955901<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03021.83598380<br />Element set: 15<br />Inclination: 39.0157 deg<br />RA of node: 194.6347 deg<br />Eccentricity: 0.0010784<br />Arg of perigee: 36.8987 deg<br />Mean anomaly: 341.3893 deg<br />Mean motion: 15.98916153 rev/day<br />Decay rate: 2.41649e-04 rev/day^2<br />Epoch rev: 84<br />Checksum: 335<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 3022.16963889 .00024502 25043-8 47460-4 0 169<br />2 27647 39.0170 192.4039 0010912 38.1446 103.8178 15.99156000 896<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Fixed Greenwich State Vector:<br /><br />Vector format = 117<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 3022.16963888900<br /> 01/22/2003 04:04:16.800 UTC<br />EFG E: -18808028.000000 ft<br /> F: 7183104.00000000 ft<br /> G: 8428317.00000000 ft<br /> Edot: -12091.620000000 ft/s<br /> Fdot: -16716.580000000 ft/s<br /> Gdot: -12617.090000000 ft/s<br />ndot/2 (drag): 0.00024501906 rev/day^2<br />nddt/6: 2.50427E-09 rev/day^3<br />Bstar: 4.74599E-05 1/Earth Radii<br />Elset #: 16<br />Rev @ Epoch: 89.39434165831<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 3022.16963889<br />Element set: 16<br />Inclination: 39.0170 deg<br />RA of node: 192.4039 deg<br />Eccentricity: 0.0010912<br />Arg of perigee: 38.1446 deg<br />Mean anomaly: 103.8178 deg<br />Mean motion: 15.99156000 rev/day<br />Decay rate: 2.45019e-04 rev/day^2<br />Epoch rev: 89<br />Checksum: 295<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 03022.29381597 .00024654 25355-8 47604-4 0 178<br />2 27647 39.0183 191.5691 0010770 39.8453 98.0968 15.99214708 917<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Centered Inertial State Vector:<br /><br />Vector format = 7<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03022.29381597200<br /> 01/22/2003 07:03:05.699 UTC<br />ECI X: 5543.78675556001 km<br /> Y: -2387.4311533600 km<br /> Z: 2794.09101635088 km<br /> Xdot: 4.17843495542959 km/s<br /> Ydot: 5.42002000961440 km/s<br /> Zdot: -3.6263659984471 km/s<br />ndot/2 (drag): 0.00024654492 rev/day^2<br />nddt/6: 2.53546E-09 rev/day^3<br />Bstar: 4.76040E-05 1/Earth Radii<br />Elset #: 17<br />Rev @ Epoch: 91.38317396396<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03022.29381597<br />Element set: 17<br />Inclination: 39.0183 deg<br />RA of node: 191.5691 deg<br />Eccentricity: 0.0010770<br />Arg of perigee: 39.8453 deg<br />Mean anomaly: 98.0968 deg<br />Mean motion: 15.99214708 rev/day<br />Decay rate: 2.46545e-04 rev/day^2<br />Epoch rev: 91<br />Checksum: 326<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 03022.83333796 .00024671 25387-8 47500-4 0 186<br />2 27647 39.0174 187.9693 0010873 46.0948 322.7398 15.99262090 1003<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Fixed Greenwich State Vector:<br /><br />Vector format = 117<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03022.83333796300<br /> 01/22/2003 20:00:00.400 UTC<br />EFG E: -14800184.000000 ft<br /> F: 15884052.0000000 ft<br /> G: 2071106.00000000 ft<br /> Edot: -12305.379999999 ft/s<br /> Fdot: -13579.319999999 ft/s<br /> Gdot: 15830.8400000000 ft/s<br />ndot/2 (drag): 0.00024670719 rev/day^2<br />nddt/6: 2.53872E-09 rev/day^3<br />Bstar: 4.75002E-05 1/Earth Radii<br />Elset #: 18<br />Rev @ Epoch: 100.02454020664<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03022.83333796<br />Element set: 18<br />Inclination: 39.0174 deg<br />RA of node: 187.9693 deg<br />Eccentricity: 0.0010873<br />Arg of perigee: 46.0948 deg<br />Mean anomaly: 322.7398 deg<br />Mean motion: 15.99262090 rev/day<br />Decay rate: 2.46707e-04 rev/day^2<br />Epoch rev: 100<br />Checksum: 321<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 03023.33409610 .00024966 25996-8 47651-4 0 204<br />2 27647 39.0190 184.6170 0010342 47.9953 328.3602 15.99425990 1080<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Centered Inertial State Vector:<br /><br />Vector format = 7<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03023.33409610000<br /> 01/23/2003 08:01:05.903 UTC<br />ECI X: -6244.9275530124 km<br /> Y: -1951.5161268641 km<br /> Z: 1168.03801330186 km<br /> Xdot: 2.63308736666883 km/s<br /> Ydot: -5.5857294001906 km/s<br /> Zdot: 4.68685599942255 km/s<br />ndot/2 (drag): 0.00024966202 rev/day^2<br />nddt/6: 2.59963E-09 rev/day^3<br />Bstar: 4.76515E-05 1/Earth Radii<br />Elset #: 20<br />Rev @ Epoch: 108.04543108067<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03023.33409610<br />Element set: 20<br />Inclination: 39.0190 deg<br />RA of node: 184.6170 deg<br />Eccentricity: 0.0010342<br />Arg of perigee: 47.9953 deg<br />Mean anomaly: 328.3602 deg<br />Mean motion: 15.99425990 rev/day<br />Decay rate: 2.49662e-04 rev/day^2<br />Epoch rev: 108<br />Checksum: 289<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

STS-107 <br />1 27647U 03003A 03024.33405497 .00025708 27557-8 47963-4 0 244<br />2 27647 39.0194 177.9303 0010288 57.1253 326.3680 15.99823116 1246<br /><br />Launch time for STS-107: 16 JAN 03 @ 15:39:00.075 UTC<br /><br />Earth-Centered Inertial State Vector:<br /><br />Vector format = 7<br />Satellite Name: STS-107<br />Catalog Number: 27647 03003A <br />Epoch Date/Time: 03024.33405496500<br /> 01/24/2003 08:01:02.348 UTC<br />ECI X: -6170.1043858994 km<br /> Y: -1825.5262335988 km<br /> Z: 1657.67901736232 km<br /> Xdot: 2.88182096578813 km/s<br /> Ydot: -5.6330646986309 km/s<br /> Zdot: 4.48075300524889 km/s<br />ndot/2 (drag): 0.00025707855 rev/day^2<br />nddt/6: 2.75570E-09 rev/day^3<br />Bstar: 4.79632E-05 1/Earth Radii<br />Elset #: 24<br />Rev @ Epoch: 124.06525842752<br /><br /><br />Keplerian Elements (Amsat format):<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03024.33405497<br />Element set: 24<br />Inclination: 39.0194 deg<br />RA of node: 177.9303 deg<br />Eccentricity: 0.0010288<br />Arg of perigee: 57.1253 deg<br />Mean anomaly: 326.3680 deg<br />Mean motion: 15.99823116 rev/day<br />Decay rate: 2.57079e-04 rev/day^2<br />Epoch rev: 124<br />Checksum: 300<br /><br />Drag Factor is 0.5<br /><br />SPACE SHUTTLE ORBITAL DATA:<br /><br />These 2-line elements have been generated using Ken Ernandes' program<br />VEC2TLE using real time state vector data supplied by DOD C-Band<br />Radar Network courtesy Dave Simonson. Note that the epoch of the<br />2-line elements is the same as the state vector time.<br /><br />Occasionally these elements are derived from the Goddard Space Flight<br />Center (GSFC) NASA Orbital Information Group (OIG), using Curtis<br />Haases' program VEC2VIF that formats the OIG vectors for use by<br />VEC2TLE.<br /><br />The source of the data can be confirmed by the data format of the<br />vector ;<br />EFG, ft, ft/s = DOD C-Band Radar Network<br />ECI, km, km/s = NASA OIG RAID RBBS<br /><br />Drag and B-Star parameters are internally calculated by VEC2TLE<br />using the drag factor. Rev numbers use NASA orbit numbering<br />convention.<br /><br /> David Cottle

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: 03027.54506365700<br /> 01/27/2003 13:04:53.499 UTC<br />EFG E: 20072159.0000000 ft<br /> F: 8167608.00000000 ft<br /> G: -2541572.0000000 ft<br /> Edot: -8566.9400000000 ft/s<br /> Fdot: 16263.7299999999 ft/s<br /> Gdot: -15732.889999999 ft/s<br />ndot/2 (drag): 0.00027142134 rev/day2<br />nddt/6: 3.06970E-09 rev/day3<br />Bstar: 4.76211E-05 1/Earth Radii<br />Elset #: 33<br />Rev @ Epoch: 176.52910976025<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 03027.54506366 .00027142 30697-8 47621-4 0 331<br />2 27647 39.0169 156.4371 0009379 98.9066 91.5730 16.00900984 1765<br /><br />Satellite: STS-107 <br />Catalog number: 27647<br />Epoch time: 03027.54506366<br />Element set: 33<br />Inclination: 39.0169 deg<br />RA of node: 156.4371 deg<br />Eccentricity: 0.0009379<br />Arg of perigee: 98.9066 deg<br />Mean anomaly: 91.5730 deg<br />Mean motion: 16.00900984 rev/day<br />Decay rate: 2.71421e-04 rev/day2<br />Epoch rev: 176<br />Checksum: 309<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

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