STS-107 TLEs and State Vector - AUS-CITY Message Forums

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

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

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

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

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

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

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

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

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

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

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

Below is the current State Vector and Keplerian Elements for STS-107. The vector data comes from NASA; the Keplerian Elements were computed from the vector. This file may be read by VEC2TLE version 9648 to update your Keplerian Elements text file. Vector format = 117 Satellite Name: STS-107 Catalog Number: 27647 03003A Epoch Date/Time: 03027.54506365700 01/27/2003 13:04:53.499 UTC EFG E: 20072159.0000000 ft F: 8167608.00000000 ft G: -2541572.0000000 ft Edot: -8566.9400000000 ft/s Fdot: 16263.7299999999 ft/s Gdot: -15732.889999999 ft/s ndot/2 (drag): 0.00027142134 rev/day2 nddt/6: 3.06970E-09 rev/day3 Bstar: 4.76211E-05 1/Earth Radii Elset #: 33 Rev @ Epoch: 176.52910976025 Launch Occurred: 2003-JAN-16 1539:00.075 UTC The following Keplerian elements were computed by VEC2TLE from the vector, using a 0.5 drag multiplier: STS-107 1 27647U 03003A 03027.54506366 .00027142 30697-8 47621-4 0 331 2 27647 39.0169 156.4371 0009379 98.9066 91.5730 16.00900984 1765 Satellite: STS-107 Catalog number: 27647 Epoch time: 03027.54506366 Element set: 33 Inclination: 39.0169 deg RA of node: 156.4371 deg Eccentricity: 0.0009379 Arg of perigee: 98.9066 deg Mean anomaly: 91.5730 deg Mean motion: 16.00900984 rev/day Decay rate: 2.71421e-04 rev/day2 Epoch rev: 176 Checksum: 309 VEC2TLE may be downloaded from http://www.orbitessera.com To receive automatic Space Shuttle orbital data updates by email, send a message to listproc@spacelink.nasa.gov, with the following contents: subscribe STSTLE [your first and last name] Use the same procedure to terminate an email subscription, substituting "unsubscribe" for "subscribe" in the message text. Ken Ernandes n2wwd@amsat.org http://www.orbitessera.com

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