[STSTLE LIST]2010-08-01T00:59:30Z[STSTLE LIST] List Ownerlist.admin@aus-city.comhttp://www.aus-city.com/cgi-bin/dada/mail.cgiPro Dada 4.1.0 Stable 06/09/10[STSTLE LIST] Current STS TLEs @ 12:30 UTCtag:www.aus-city.com,2010-05-26:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100526224502%2F2010-05-26T22:45:02Z2010-05-26T22:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.242 11.4 -0.1 17.6
010/21:03:13.287 6.6 -0.0 194.0
000/00:00:12.574 11.6 -17.6 181.9
</pre>
<p> Coasting Arc #1 (Orbit 164)
</p><hr/>
<p> Vector Time (GMT): 2010/145/01:58:36.000
Vector Time (MET): 010/07:38:27.045
Weight (LBS) : 220514.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538637.26 A = 6725164.58 meter
Y = 4013380.82 meter E = .0015595
Z = 4076887.02 I = 51.57439
XDOT = -6442.461626 Wp = 30.11727
YDOT = -1786.561459 meter/sec RA = 348.59334 deg
ZDOT = -3813.611174 TA = 99.20289
MA = 99.02646
Ha = 192.466 n.mi
Hp = 183.276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11609702.31 X = -3603057.76
Y = 13167259.91 feet Y = 3973449.07 meter
Z = 13375613.59 Z = 4059539.92
XDOT = -21136.685124 XDOT = -6403.478973
YDOT = -5861.422108 feet/sec YDOT = -1858.386559 meter/sec
ZDOT = -12511.847685 ZDOT = -3844.814726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13454883.78 X = -4101048.57
Y = -11356575.88 feet Y = -3461484.33 meter
Z = 13306511.45 Z = 4055824.69
XDOT = 4506.902540 XDOT = 1373.703894
YDOT = -20220.931789 feet/sec YDOT = -6163.340009 meter/sec
ZDOT = -12636.113014 ZDOT = -3851.487247
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.12301315 .00020000 00000-0 20000-3 0 9000
2 36572 51.6440 348.9210 0011304 347.3969 12.6910 15.73955012 1651
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.12301315 = yrday.fracday
Element set: 900
Inclination: 51.6440 deg
RA of node: 348.9210 deg
Eccentricity: .0011304
Arg of perigee: 347.3969 deg
Mean anomaly: 12.6910 deg
</pre>
<p> Mean motion: 15.73955012 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 165
Checksum: 252
</pre>
<p> Coasting Arc #2 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.529
Vector Time (MET): 010/21:03:19.574
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284247.40 A = 6723350.68 meter
Y = 2584512.06 meter E = .0013265
Z = 4482276.08 I = 51.55234
XDOT = -5742.180619 Wp = 9.07042
YDOT = 4049.389236 meter/sec RA = 345.76447 deg
ZDOT = 3165.196910 TA = 49.35717
MA = 49.24191
Ha = 194.030 n.mi
Hp = 181.883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055929.81 X = 4233254.00
Y = 8479370.28 feet Y = 2632135.44 meter
Z = 14705630.17 Z = 4502965.78
XDOT = -18839.175258 XDOT = -5802.411091
YDOT = 13285.397757 feet/sec YDOT = 3984.839627 meter/sec
ZDOT = 10384.504298 ZDOT = 3137.155016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2291735.14 X = 698520.87
Y = -16179830.67 feet Y = -4931612.39 meter
Z = 14788017.83 Z = 4507387.83
XDOT = 18476.611363 XDOT = 5631.671144
YDOT = 11971.546591 feet/sec YDOT = 3648.927401 meter/sec
ZDOT = 10272.807379 ZDOT = 3131.151689
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69444688 .00020000 00000-0 20000-3 0 9014
2 36572 51.6440 345.9822 0017583 340.6204 19.4289 15.73989642 1740
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69444688 = yrday.fracday
Element set: 901
Inclination: 51.6440 deg
RA of node: 345.9822 deg
Eccentricity: .0017583
Arg of perigee: 340.6204 deg
Mean anomaly: 19.4289 deg
</pre>
<p> Mean motion: 15.73989642 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 315
</pre>
<p> Coasting Arc #3 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:07.947
Vector Time (MET): 011/21:03:58.992
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859413.54 A = 6729444.61 meter
Y = -3868065.22 meter E = .0020285
Z = -2558488.24 I = 51.54449
XDOT = 4924.838215 Wp = 357.82024
YDOT = 2708.111398 meter/sec RA = 340.57592 deg
ZDOT = 5278.178461 TA = 333.07664
MA = 333.18174
Ha = 194.365 n.mi
Hp = 181.674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15942957.80 X = 4914734.67
Y = -12690502.71 feet Y = -3813414.70 meter
Z = -8393990.30 Z = -2534746.93
XDOT = 16157.605692 XDOT = 4868.548693
YDOT = 8884.879914 feet/sec YDOT = 2762.868410 meter/sec
ZDOT = 17316.858469 ZDOT = 5301.967411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18155278.61 X = -5533728.92
Y = -9337630.91 feet Y = -2846109.90 meter
Z = -8299418.23 Z = -2529662.68
XDOT = 794.954864 XDOT = 242.302243
YDOT = -16966.568591 feet/sec YDOT = -5171.410107 meter/sec
ZDOT = 17411.586358 ZDOT = 5307.051522
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64680877 .00020000 00000-0 20000-3 0 9023
2 36572 51.6450 341.0926 0017579 344.6561 15.4067 15.73979475 1897
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64680877 = yrday.fracday
Element set: 902
Inclination: 51.6450 deg
RA of node: 341.0926 deg
Eccentricity: .0017579
Arg of perigee: 344.6561 deg
Mean anomaly: 15.4067 deg
</pre>
<p> Mean motion: 15.73979475 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 321
</pre>
<p> Coasting Arc #4 (Orbit 204)
</p><hr/>
<p> Vector Time (GMT): 2010/147/15:25:10.509
Vector Time (MET): 012/21:05:01.554
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150549.74 A = 6722138.59 meter
Y = -2288073.62 meter E = .0022289
Z = -4781846.83 I = 51.49224
XDOT = 5521.837894 Wp = 19.75566
YDOT = -4720.940980 meter/sec RA = 335.47069 deg
ZDOT = -2516.702975 TA = 225.42535
MA = 225.60750
Ha = 194.445 n.mi
Hp = 181.261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13617289.19 X = -4101425.91
Y = -7506803.22 feet Y = -2334212.12 meter
Z = -15688473.87 Z = -4801891.56
XDOT = 18116.266056 XDOT = 5586.443784
YDOT = -15488.651510 feet/sec YDOT = -4658.830874 meter/sec
ZDOT = -8256.899524 ZDOT = -2489.721283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927861.25 X = -282812.11
Y = 15440560.24 feet Y = 4706282.76 meter
Z = -15768292.38 Z = -4806175.52
XDOT = -20690.334280 XDOT = -6306.413889
YDOT = -9623.103333 feet/sec YDOT = -2933.121896 meter/sec
ZDOT = -8149.412873 ZDOT = -2483.941044
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10147.66264701 .00020000 00000-0 20000-3 0 9031
2 36572 51.6450 335.8768 0017669 348.4819 11.5937 15.74010473 2057
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10147.66264701 = yrday.fracday
Element set: 903
Inclination: 51.6450 deg
RA of node: 335.8768 deg
Eccentricity: .0017669
Arg of perigee: 348.4819 deg
Mean anomaly: 11.5937 deg
</pre>
<p> Mean motion: 15.74010473 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 205
Checksum: 299</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
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[STSTLE LIST] Current STS TLEs @ 06:30 UTCtag:www.aus-city.com,2010-05-26:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100526164502%2F2010-05-26T16:45:02Z2010-05-26T16:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.242 11.4 -0.1 17.6
010/21:03:13.287 6.6 -0.0 194.0
000/00:00:12.574 11.6 -17.6 181.9
</pre>
<p> Coasting Arc #1 (Orbit 164)
</p><hr/>
<p> Vector Time (GMT): 2010/145/01:58:36.000
Vector Time (MET): 010/07:38:27.045
Weight (LBS) : 220514.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538637.26 A = 6725164.58 meter
Y = 4013380.82 meter E = .0015595
Z = 4076887.02 I = 51.57439
XDOT = -6442.461626 Wp = 30.11727
YDOT = -1786.561459 meter/sec RA = 348.59334 deg
ZDOT = -3813.611174 TA = 99.20289
MA = 99.02646
Ha = 192.466 n.mi
Hp = 183.276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11609702.31 X = -3603057.76
Y = 13167259.91 feet Y = 3973449.07 meter
Z = 13375613.59 Z = 4059539.92
XDOT = -21136.685124 XDOT = -6403.478973
YDOT = -5861.422108 feet/sec YDOT = -1858.386559 meter/sec
ZDOT = -12511.847685 ZDOT = -3844.814726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13454883.78 X = -4101048.57
Y = -11356575.88 feet Y = -3461484.33 meter
Z = 13306511.45 Z = 4055824.69
XDOT = 4506.902540 XDOT = 1373.703894
YDOT = -20220.931789 feet/sec YDOT = -6163.340009 meter/sec
ZDOT = -12636.113014 ZDOT = -3851.487247
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.12301315 .00020000 00000-0 20000-3 0 9000
2 36572 51.6440 348.9210 0011304 347.3969 12.6910 15.73955012 1651
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.12301315 = yrday.fracday
Element set: 900
Inclination: 51.6440 deg
RA of node: 348.9210 deg
Eccentricity: .0011304
Arg of perigee: 347.3969 deg
Mean anomaly: 12.6910 deg
</pre>
<p> Mean motion: 15.73955012 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 165
Checksum: 252
</pre>
<p> Coasting Arc #2 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.529
Vector Time (MET): 010/21:03:19.574
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284247.40 A = 6723350.68 meter
Y = 2584512.06 meter E = .0013265
Z = 4482276.08 I = 51.55234
XDOT = -5742.180619 Wp = 9.07042
YDOT = 4049.389236 meter/sec RA = 345.76447 deg
ZDOT = 3165.196910 TA = 49.35717
MA = 49.24191
Ha = 194.030 n.mi
Hp = 181.883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055929.81 X = 4233254.00
Y = 8479370.28 feet Y = 2632135.44 meter
Z = 14705630.17 Z = 4502965.78
XDOT = -18839.175258 XDOT = -5802.411091
YDOT = 13285.397757 feet/sec YDOT = 3984.839627 meter/sec
ZDOT = 10384.504298 ZDOT = 3137.155016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2291735.14 X = 698520.87
Y = -16179830.67 feet Y = -4931612.39 meter
Z = 14788017.83 Z = 4507387.83
XDOT = 18476.611363 XDOT = 5631.671144
YDOT = 11971.546591 feet/sec YDOT = 3648.927401 meter/sec
ZDOT = 10272.807379 ZDOT = 3131.151689
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69444688 .00020000 00000-0 20000-3 0 9014
2 36572 51.6440 345.9822 0017583 340.6204 19.4289 15.73989642 1740
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69444688 = yrday.fracday
Element set: 901
Inclination: 51.6440 deg
RA of node: 345.9822 deg
Eccentricity: .0017583
Arg of perigee: 340.6204 deg
Mean anomaly: 19.4289 deg
</pre>
<p> Mean motion: 15.73989642 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 315
</pre>
<p> Coasting Arc #3 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:07.947
Vector Time (MET): 011/21:03:58.992
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859413.54 A = 6729444.61 meter
Y = -3868065.22 meter E = .0020285
Z = -2558488.24 I = 51.54449
XDOT = 4924.838215 Wp = 357.82024
YDOT = 2708.111398 meter/sec RA = 340.57592 deg
ZDOT = 5278.178461 TA = 333.07664
MA = 333.18174
Ha = 194.365 n.mi
Hp = 181.674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15942957.80 X = 4914734.67
Y = -12690502.71 feet Y = -3813414.70 meter
Z = -8393990.30 Z = -2534746.93
XDOT = 16157.605692 XDOT = 4868.548693
YDOT = 8884.879914 feet/sec YDOT = 2762.868410 meter/sec
ZDOT = 17316.858469 ZDOT = 5301.967411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18155278.61 X = -5533728.92
Y = -9337630.91 feet Y = -2846109.90 meter
Z = -8299418.23 Z = -2529662.68
XDOT = 794.954864 XDOT = 242.302243
YDOT = -16966.568591 feet/sec YDOT = -5171.410107 meter/sec
ZDOT = 17411.586358 ZDOT = 5307.051522
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64680877 .00020000 00000-0 20000-3 0 9023
2 36572 51.6450 341.0926 0017579 344.6561 15.4067 15.73979475 1897
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64680877 = yrday.fracday
Element set: 902
Inclination: 51.6450 deg
RA of node: 341.0926 deg
Eccentricity: .0017579
Arg of perigee: 344.6561 deg
Mean anomaly: 15.4067 deg
</pre>
<p> Mean motion: 15.73979475 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 321
</pre>
<p> Coasting Arc #4 (Orbit 204)
</p><hr/>
<p> Vector Time (GMT): 2010/147/15:25:10.509
Vector Time (MET): 012/21:05:01.554
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150549.74 A = 6722138.59 meter
Y = -2288073.62 meter E = .0022289
Z = -4781846.83 I = 51.49224
XDOT = 5521.837894 Wp = 19.75566
YDOT = -4720.940980 meter/sec RA = 335.47069 deg
ZDOT = -2516.702975 TA = 225.42535
MA = 225.60750
Ha = 194.445 n.mi
Hp = 181.261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13617289.19 X = -4101425.91
Y = -7506803.22 feet Y = -2334212.12 meter
Z = -15688473.87 Z = -4801891.56
XDOT = 18116.266056 XDOT = 5586.443784
YDOT = -15488.651510 feet/sec YDOT = -4658.830874 meter/sec
ZDOT = -8256.899524 ZDOT = -2489.721283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927861.25 X = -282812.11
Y = 15440560.24 feet Y = 4706282.76 meter
Z = -15768292.38 Z = -4806175.52
XDOT = -20690.334280 XDOT = -6306.413889
YDOT = -9623.103333 feet/sec YDOT = -2933.121896 meter/sec
ZDOT = -8149.412873 ZDOT = -2483.941044
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10147.66264701 .00020000 00000-0 20000-3 0 9031
2 36572 51.6450 335.8768 0017669 348.4819 11.5937 15.74010473 2057
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10147.66264701 = yrday.fracday
Element set: 903
Inclination: 51.6450 deg
RA of node: 335.8768 deg
Eccentricity: .0017669
Arg of perigee: 348.4819 deg
Mean anomaly: 11.5937 deg
</pre>
<p> Mean motion: 15.74010473 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 205
Checksum: 299</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
<p>The following information is a reminder of your current mailing
list subscription:
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[STSTLE LIST] Current STS TLEs @ 00:30 UTCtag:www.aus-city.com,2010-05-26:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100526104502%2F2010-05-26T10:45:02Z2010-05-26T10:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.242 11.4 -0.1 17.6
010/21:03:13.287 6.6 -0.0 194.0
000/00:00:12.574 11.6 -17.6 181.9
</pre>
<p> Coasting Arc #1 (Orbit 164)
</p><hr/>
<p> Vector Time (GMT): 2010/145/01:58:36.000
Vector Time (MET): 010/07:38:27.045
Weight (LBS) : 220514.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538637.26 A = 6725164.58 meter
Y = 4013380.82 meter E = .0015595
Z = 4076887.02 I = 51.57439
XDOT = -6442.461626 Wp = 30.11727
YDOT = -1786.561459 meter/sec RA = 348.59334 deg
ZDOT = -3813.611174 TA = 99.20289
MA = 99.02646
Ha = 192.466 n.mi
Hp = 183.276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11609702.31 X = -3603057.76
Y = 13167259.91 feet Y = 3973449.07 meter
Z = 13375613.59 Z = 4059539.92
XDOT = -21136.685124 XDOT = -6403.478973
YDOT = -5861.422108 feet/sec YDOT = -1858.386559 meter/sec
ZDOT = -12511.847685 ZDOT = -3844.814726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13454883.78 X = -4101048.57
Y = -11356575.88 feet Y = -3461484.33 meter
Z = 13306511.45 Z = 4055824.69
XDOT = 4506.902540 XDOT = 1373.703894
YDOT = -20220.931789 feet/sec YDOT = -6163.340009 meter/sec
ZDOT = -12636.113014 ZDOT = -3851.487247
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.12301315 .00020000 00000-0 20000-3 0 9000
2 36572 51.6440 348.9210 0011304 347.3969 12.6910 15.73955012 1651
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.12301315 = yrday.fracday
Element set: 900
Inclination: 51.6440 deg
RA of node: 348.9210 deg
Eccentricity: .0011304
Arg of perigee: 347.3969 deg
Mean anomaly: 12.6910 deg
</pre>
<p> Mean motion: 15.73955012 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 165
Checksum: 252
</pre>
<p> Coasting Arc #2 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.529
Vector Time (MET): 010/21:03:19.574
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284247.40 A = 6723350.68 meter
Y = 2584512.06 meter E = .0013265
Z = 4482276.08 I = 51.55234
XDOT = -5742.180619 Wp = 9.07042
YDOT = 4049.389236 meter/sec RA = 345.76447 deg
ZDOT = 3165.196910 TA = 49.35717
MA = 49.24191
Ha = 194.030 n.mi
Hp = 181.883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055929.81 X = 4233254.00
Y = 8479370.28 feet Y = 2632135.44 meter
Z = 14705630.17 Z = 4502965.78
XDOT = -18839.175258 XDOT = -5802.411091
YDOT = 13285.397757 feet/sec YDOT = 3984.839627 meter/sec
ZDOT = 10384.504298 ZDOT = 3137.155016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2291735.14 X = 698520.87
Y = -16179830.67 feet Y = -4931612.39 meter
Z = 14788017.83 Z = 4507387.83
XDOT = 18476.611363 XDOT = 5631.671144
YDOT = 11971.546591 feet/sec YDOT = 3648.927401 meter/sec
ZDOT = 10272.807379 ZDOT = 3131.151689
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69444688 .00020000 00000-0 20000-3 0 9014
2 36572 51.6440 345.9822 0017583 340.6204 19.4289 15.73989642 1740
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69444688 = yrday.fracday
Element set: 901
Inclination: 51.6440 deg
RA of node: 345.9822 deg
Eccentricity: .0017583
Arg of perigee: 340.6204 deg
Mean anomaly: 19.4289 deg
</pre>
<p> Mean motion: 15.73989642 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 315
</pre>
<p> Coasting Arc #3 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:07.947
Vector Time (MET): 011/21:03:58.992
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859413.54 A = 6729444.61 meter
Y = -3868065.22 meter E = .0020285
Z = -2558488.24 I = 51.54449
XDOT = 4924.838215 Wp = 357.82024
YDOT = 2708.111398 meter/sec RA = 340.57592 deg
ZDOT = 5278.178461 TA = 333.07664
MA = 333.18174
Ha = 194.365 n.mi
Hp = 181.674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15942957.80 X = 4914734.67
Y = -12690502.71 feet Y = -3813414.70 meter
Z = -8393990.30 Z = -2534746.93
XDOT = 16157.605692 XDOT = 4868.548693
YDOT = 8884.879914 feet/sec YDOT = 2762.868410 meter/sec
ZDOT = 17316.858469 ZDOT = 5301.967411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18155278.61 X = -5533728.92
Y = -9337630.91 feet Y = -2846109.90 meter
Z = -8299418.23 Z = -2529662.68
XDOT = 794.954864 XDOT = 242.302243
YDOT = -16966.568591 feet/sec YDOT = -5171.410107 meter/sec
ZDOT = 17411.586358 ZDOT = 5307.051522
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64680877 .00020000 00000-0 20000-3 0 9023
2 36572 51.6450 341.0926 0017579 344.6561 15.4067 15.73979475 1897
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64680877 = yrday.fracday
Element set: 902
Inclination: 51.6450 deg
RA of node: 341.0926 deg
Eccentricity: .0017579
Arg of perigee: 344.6561 deg
Mean anomaly: 15.4067 deg
</pre>
<p> Mean motion: 15.73979475 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 321
</pre>
<p> Coasting Arc #4 (Orbit 204)
</p><hr/>
<p> Vector Time (GMT): 2010/147/15:25:10.509
Vector Time (MET): 012/21:05:01.554
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150549.74 A = 6722138.59 meter
Y = -2288073.62 meter E = .0022289
Z = -4781846.83 I = 51.49224
XDOT = 5521.837894 Wp = 19.75566
YDOT = -4720.940980 meter/sec RA = 335.47069 deg
ZDOT = -2516.702975 TA = 225.42535
MA = 225.60750
Ha = 194.445 n.mi
Hp = 181.261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13617289.19 X = -4101425.91
Y = -7506803.22 feet Y = -2334212.12 meter
Z = -15688473.87 Z = -4801891.56
XDOT = 18116.266056 XDOT = 5586.443784
YDOT = -15488.651510 feet/sec YDOT = -4658.830874 meter/sec
ZDOT = -8256.899524 ZDOT = -2489.721283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927861.25 X = -282812.11
Y = 15440560.24 feet Y = 4706282.76 meter
Z = -15768292.38 Z = -4806175.52
XDOT = -20690.334280 XDOT = -6306.413889
YDOT = -9623.103333 feet/sec YDOT = -2933.121896 meter/sec
ZDOT = -8149.412873 ZDOT = -2483.941044
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10147.66264701 .00020000 00000-0 20000-3 0 9031
2 36572 51.6450 335.8768 0017669 348.4819 11.5937 15.74010473 2057
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10147.66264701 = yrday.fracday
Element set: 903
Inclination: 51.6450 deg
RA of node: 335.8768 deg
Eccentricity: .0017669
Arg of perigee: 348.4819 deg
Mean anomaly: 11.5937 deg
</pre>
<p> Mean motion: 15.74010473 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 205
Checksum: 299</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
<p>The following information is a reminder of your current mailing
list subscription:
</p><p>You are subscribed to the following list:
</p><p><strong>[STSTLE LIST]</strong>
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[STSTLE LIST] Current STS TLEs @ 18:30 UTCtag:www.aus-city.com,2010-05-26:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100526044502%2F2010-05-26T04:45:02Z2010-05-26T04:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.242 11.4 -0.1 17.6
010/21:03:13.287 6.6 -0.0 194.0
000/00:00:12.574 11.6 -17.6 181.9
</pre>
<p> Coasting Arc #1 (Orbit 164)
</p><hr/>
<p> Vector Time (GMT): 2010/145/01:58:36.000
Vector Time (MET): 010/07:38:27.045
Weight (LBS) : 220514.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538637.26 A = 6725164.58 meter
Y = 4013380.82 meter E = .0015595
Z = 4076887.02 I = 51.57439
XDOT = -6442.461626 Wp = 30.11727
YDOT = -1786.561459 meter/sec RA = 348.59334 deg
ZDOT = -3813.611174 TA = 99.20289
MA = 99.02646
Ha = 192.466 n.mi
Hp = 183.276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11609702.31 X = -3603057.76
Y = 13167259.91 feet Y = 3973449.07 meter
Z = 13375613.59 Z = 4059539.92
XDOT = -21136.685124 XDOT = -6403.478973
YDOT = -5861.422108 feet/sec YDOT = -1858.386559 meter/sec
ZDOT = -12511.847685 ZDOT = -3844.814726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13454883.78 X = -4101048.57
Y = -11356575.88 feet Y = -3461484.33 meter
Z = 13306511.45 Z = 4055824.69
XDOT = 4506.902540 XDOT = 1373.703894
YDOT = -20220.931789 feet/sec YDOT = -6163.340009 meter/sec
ZDOT = -12636.113014 ZDOT = -3851.487247
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.12301315 .00020000 00000-0 20000-3 0 9000
2 36572 51.6440 348.9210 0011304 347.3969 12.6910 15.73955012 1651
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.12301315 = yrday.fracday
Element set: 900
Inclination: 51.6440 deg
RA of node: 348.9210 deg
Eccentricity: .0011304
Arg of perigee: 347.3969 deg
Mean anomaly: 12.6910 deg
</pre>
<p> Mean motion: 15.73955012 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 165
Checksum: 252
</pre>
<p> Coasting Arc #2 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.529
Vector Time (MET): 010/21:03:19.574
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284247.40 A = 6723350.68 meter
Y = 2584512.06 meter E = .0013265
Z = 4482276.08 I = 51.55234
XDOT = -5742.180619 Wp = 9.07042
YDOT = 4049.389236 meter/sec RA = 345.76447 deg
ZDOT = 3165.196910 TA = 49.35717
MA = 49.24191
Ha = 194.030 n.mi
Hp = 181.883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055929.81 X = 4233254.00
Y = 8479370.28 feet Y = 2632135.44 meter
Z = 14705630.17 Z = 4502965.78
XDOT = -18839.175258 XDOT = -5802.411091
YDOT = 13285.397757 feet/sec YDOT = 3984.839627 meter/sec
ZDOT = 10384.504298 ZDOT = 3137.155016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2291735.14 X = 698520.87
Y = -16179830.67 feet Y = -4931612.39 meter
Z = 14788017.83 Z = 4507387.83
XDOT = 18476.611363 XDOT = 5631.671144
YDOT = 11971.546591 feet/sec YDOT = 3648.927401 meter/sec
ZDOT = 10272.807379 ZDOT = 3131.151689
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69444688 .00020000 00000-0 20000-3 0 9014
2 36572 51.6440 345.9822 0017583 340.6204 19.4289 15.73989642 1740
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69444688 = yrday.fracday
Element set: 901
Inclination: 51.6440 deg
RA of node: 345.9822 deg
Eccentricity: .0017583
Arg of perigee: 340.6204 deg
Mean anomaly: 19.4289 deg
</pre>
<p> Mean motion: 15.73989642 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 315
</pre>
<p> Coasting Arc #3 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:07.947
Vector Time (MET): 011/21:03:58.992
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859413.54 A = 6729444.61 meter
Y = -3868065.22 meter E = .0020285
Z = -2558488.24 I = 51.54449
XDOT = 4924.838215 Wp = 357.82024
YDOT = 2708.111398 meter/sec RA = 340.57592 deg
ZDOT = 5278.178461 TA = 333.07664
MA = 333.18174
Ha = 194.365 n.mi
Hp = 181.674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15942957.80 X = 4914734.67
Y = -12690502.71 feet Y = -3813414.70 meter
Z = -8393990.30 Z = -2534746.93
XDOT = 16157.605692 XDOT = 4868.548693
YDOT = 8884.879914 feet/sec YDOT = 2762.868410 meter/sec
ZDOT = 17316.858469 ZDOT = 5301.967411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18155278.61 X = -5533728.92
Y = -9337630.91 feet Y = -2846109.90 meter
Z = -8299418.23 Z = -2529662.68
XDOT = 794.954864 XDOT = 242.302243
YDOT = -16966.568591 feet/sec YDOT = -5171.410107 meter/sec
ZDOT = 17411.586358 ZDOT = 5307.051522
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64680877 .00020000 00000-0 20000-3 0 9023
2 36572 51.6450 341.0926 0017579 344.6561 15.4067 15.73979475 1897
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64680877 = yrday.fracday
Element set: 902
Inclination: 51.6450 deg
RA of node: 341.0926 deg
Eccentricity: .0017579
Arg of perigee: 344.6561 deg
Mean anomaly: 15.4067 deg
</pre>
<p> Mean motion: 15.73979475 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 321
</pre>
<p> Coasting Arc #4 (Orbit 204)
</p><hr/>
<p> Vector Time (GMT): 2010/147/15:25:10.509
Vector Time (MET): 012/21:05:01.554
Weight (LBS) : 219942.2
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150549.74 A = 6722138.59 meter
Y = -2288073.62 meter E = .0022289
Z = -4781846.83 I = 51.49224
XDOT = 5521.837894 Wp = 19.75566
YDOT = -4720.940980 meter/sec RA = 335.47069 deg
ZDOT = -2516.702975 TA = 225.42535
MA = 225.60750
Ha = 194.445 n.mi
Hp = 181.261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13617289.19 X = -4101425.91
Y = -7506803.22 feet Y = -2334212.12 meter
Z = -15688473.87 Z = -4801891.56
XDOT = 18116.266056 XDOT = 5586.443784
YDOT = -15488.651510 feet/sec YDOT = -4658.830874 meter/sec
ZDOT = -8256.899524 ZDOT = -2489.721283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927861.25 X = -282812.11
Y = 15440560.24 feet Y = 4706282.76 meter
Z = -15768292.38 Z = -4806175.52
XDOT = -20690.334280 XDOT = -6306.413889
YDOT = -9623.103333 feet/sec YDOT = -2933.121896 meter/sec
ZDOT = -8149.412873 ZDOT = -2483.941044
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10147.66264701 .00020000 00000-0 20000-3 0 9031
2 36572 51.6450 335.8768 0017669 348.4819 11.5937 15.74010473 2057
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10147.66264701 = yrday.fracday
Element set: 903
Inclination: 51.6450 deg
RA of node: 335.8768 deg
Eccentricity: .0017669
Arg of perigee: 348.4819 deg
Mean anomaly: 11.5937 deg
</pre>
<p> Mean motion: 15.74010473 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 205
Checksum: 299</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
<p>The following information is a reminder of your current mailing
list subscription:
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[STSTLE LIST] Current STS TLEs @ 12:30 UTCtag:www.aus-city.com,2010-05-25:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100525224502%2F2010-05-25T22:45:02Z2010-05-25T22:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.259 11.3 -0.1 17.6
010/21:03:13.304 6.7 -0.0 193.9
000/00:00:12.608 11.7 -17.6 181.7
</pre>
<p> Coasting Arc #1 (Orbit 150)
</p><hr/>
<p> Vector Time (GMT): 2010/144/05:06:55.000
Vector Time (MET): 009/10:46:46.045
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739169.20 A = 6722925.08 meter
Y = -3210263.48 meter E = .0016348
Z = -4586272.80 I = 51.59510
XDOT = 6357.177738 Wp = 26.96158
YDOT = -3142.358338 meter/sec RA = 353.10948 deg
ZDOT = -2973.239778 TA = 213.42123
MA = 213.52452
Ha = 192.297 n.mi
Hp = 183.054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12267615.50 X = -3680713.90
Y = -10532360.49 feet Y = -3251749.89 meter
Z = -15046826.78 Z = -4604296.24
XDOT = 20856.882344 XDOT = 6406.287369
YDOT = -10309.574601 feet/sec YDOT = -3070.993772 meter/sec
ZDOT = -9754.723682 ZDOT = -2942.237058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1905214.81 X = -580709.47
Y = -15988436.72 feet Y = -4873275.51 meter
Z = -15118599.51 Z = -4608149.13
XDOT = 21235.882470 XDOT = 6472.696977
YDOT = 6608.172546 feet/sec YDOT = 2014.170992 meter/sec
ZDOT = -9631.239121 ZDOT = -2935.601684
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10144.23415742 .00020000 00000-0 20000-3 0 9001
2 36572 51.6454 353.4871 0011187 347.7804 12.3086 15.74016213 1519
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10144.23415742 = yrday.fracday
Element set: 900
Inclination: 51.6454 deg
RA of node: 353.4871 deg
Eccentricity: .0011187
Arg of perigee: 347.7804 deg
Mean anomaly: 12.3086 deg
</pre>
<p> Mean motion: 15.74016213 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 151
Checksum: 261
</pre>
<p> Coasting Arc #2 (Orbit 166)
</p><hr/>
<p> Vector Time (GMT): 2010/145/05:07:29.776
Vector Time (MET): 010/10:47:20.821
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479639.18 A = 6729692.90 meter
Y = 3100864.13 meter E = .0013693
Z = 2378578.25 I = 51.58816
XDOT = -4295.064985 Wp = 58.17708
YDOT = -3441.964680 meter/sec RA = 347.92575 deg
ZDOT = -5377.869431 TA = 95.01376
MA = 94.85743
Ha = 192.466 n.mi
Hp = 182.940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17977818.82 X = -5525461.26
Y = 10173438.73 feet Y = 3039331.09 meter
Z = 7803734.40 Z = 2351846.67
XDOT = -14091.420555 XDOT = -4230.131886
YDOT = -11292.535040 feet/sec YDOT = -3489.631043 meter/sec
ZDOT = -17643.928578 ZDOT = -5398.577879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20261101.26 X = -6175583.66
Y = -4223629.88 feet Y = -1287362.39 meter
Z = 7697260.71 Z = 2346125.06
XDOT = -3387.760093 XDOT = -1032.589276
YDOT = -16233.772562 feet/sec YDOT = -4948.053877 meter/sec
ZDOT = -17726.388959 ZDOT = -5403.003355
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.24997835 .00020000 00000-0 20000-3 0 9012
2 36572 51.6456 348.2709 0011274 351.5455 8.5517 15.74033977 1674
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.24997835 = yrday.fracday
Element set: 901
Inclination: 51.6456 deg
RA of node: 348.2709 deg
Eccentricity: .0011274
Arg of perigee: 351.5455 deg
Mean anomaly: 8.5517 deg
</pre>
<p> Mean motion: 15.74033977 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 167
Checksum: 307
</pre>
<p> Coasting Arc #3 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.563
Vector Time (MET): 010/21:03:19.608
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262066.21 A = 6723050.91 meter
Y = 2599573.09 meter E = .0013333
Z = 4493725.11 I = 51.55255
XDOT = -5764.116617 Wp = 12.07650
YDOT = 4036.590451 meter/sec RA = 345.76578 deg
ZDOT = 3142.990439 TA = 46.59888
MA = 46.48795
Ha = 193.910 n.mi
Hp = 181.696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13983156.86 X = 4210850.42
Y = 8528783.10 feet Y = 2646947.18 meter
Z = 14743192.62 Z = 4514306.52
XDOT = -18911.143757 XDOT = -5824.094464
YDOT = 13243.406991 feet/sec YDOT = 3971.796955 meter/sec
ZDOT = 10311.648421 ZDOT = 3114.842590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2365866.47 X = 721116.10
Y = -16132209.43 feet Y = -4917097.43 meter
Z = 14825148.91 Z = 4518705.39
XDOT = 18469.695762 XDOT = 5629.563268
YDOT = 12048.387081 feet/sec YDOT = 3672.348382 meter/sec
ZDOT = 10199.529579 ZDOT = 3108.816616
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69440136 .00020000 00000-0 20000-3 0 9029
2 36572 51.6443 345.9838 0017293 342.9630 17.0950 15.74078594 1741
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69440136 = yrday.fracday
Element set: 902
Inclination: 51.6443 deg
RA of node: 345.9838 deg
Eccentricity: .0017293
Arg of perigee: 342.9630 deg
Mean anomaly: 17.0950 deg
</pre>
<p> Mean motion: 15.74078594 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 301
</pre>
<p> Coasting Arc #4 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:03.568
Vector Time (MET): 011/21:03:54.613
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880170.62 A = 6729240.37 meter
Y = -3856550.09 meter E = .0020258
Z = -2536322.42 I = 51.54501
XDOT = 4897.378121 Wp = 359.98214
YDOT = 2729.737006 meter/sec RA = 340.57710 deg
ZDOT = 5292.364101 TA = 331.19102
MA = 331.30274
Ha = 194.240 n.mi
Hp = 181.481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16011058.48 X = 4935253.77
Y = -12652723.41 feet Y = -3801668.78 meter
Z = -8321267.79 Z = -2512480.85
XDOT = 16067.513521 XDOT = 4840.779906
YDOT = 8955.830072 feet/sec YDOT = 2784.185215 meter/sec
ZDOT = 17363.399282 ZDOT = 5316.018901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18145749.25 X = -5530824.37
Y = -9420654.50 feet Y = -2871415.49 meter
Z = -8226296.47 Z = -2507375.17
XDOT = 896.621390 XDOT = 273.290200
YDOT = -16913.682960 feet/sec YDOT = -5155.290566 meter/sec
ZDOT = 17457.592792 ZDOT = 5321.074283
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64670948 .00020000 00000-0 20000-3 0 9032
2 36572 51.6453 341.0938 0017293 347.0084 13.0632 15.74068320 1894
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64670948 = yrday.fracday
Element set: 903
Inclination: 51.6453 deg
RA of node: 341.0938 deg
Eccentricity: .0017293
Arg of perigee: 347.0084 deg
Mean anomaly: 13.0632 deg
</pre>
<p> Mean motion: 15.74068320 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 287</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
<p>The following information is a reminder of your current mailing
list subscription:
</p><p>You are subscribed to the following list:
</p><p><strong>[STSTLE LIST]</strong>
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[STSTLE LIST] Current STS TLEs @ 06:30 UTCtag:www.aus-city.com,2010-05-25:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100525164502%2F2010-05-25T16:45:02Z2010-05-25T16:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.259 11.3 -0.1 17.6
010/21:03:13.304 6.7 -0.0 193.9
000/00:00:12.608 11.7 -17.6 181.7
</pre>
<p> Coasting Arc #1 (Orbit 150)
</p><hr/>
<p> Vector Time (GMT): 2010/144/05:06:55.000
Vector Time (MET): 009/10:46:46.045
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739169.20 A = 6722925.08 meter
Y = -3210263.48 meter E = .0016348
Z = -4586272.80 I = 51.59510
XDOT = 6357.177738 Wp = 26.96158
YDOT = -3142.358338 meter/sec RA = 353.10948 deg
ZDOT = -2973.239778 TA = 213.42123
MA = 213.52452
Ha = 192.297 n.mi
Hp = 183.054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12267615.50 X = -3680713.90
Y = -10532360.49 feet Y = -3251749.89 meter
Z = -15046826.78 Z = -4604296.24
XDOT = 20856.882344 XDOT = 6406.287369
YDOT = -10309.574601 feet/sec YDOT = -3070.993772 meter/sec
ZDOT = -9754.723682 ZDOT = -2942.237058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1905214.81 X = -580709.47
Y = -15988436.72 feet Y = -4873275.51 meter
Z = -15118599.51 Z = -4608149.13
XDOT = 21235.882470 XDOT = 6472.696977
YDOT = 6608.172546 feet/sec YDOT = 2014.170992 meter/sec
ZDOT = -9631.239121 ZDOT = -2935.601684
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10144.23415742 .00020000 00000-0 20000-3 0 9001
2 36572 51.6454 353.4871 0011187 347.7804 12.3086 15.74016213 1519
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10144.23415742 = yrday.fracday
Element set: 900
Inclination: 51.6454 deg
RA of node: 353.4871 deg
Eccentricity: .0011187
Arg of perigee: 347.7804 deg
Mean anomaly: 12.3086 deg
</pre>
<p> Mean motion: 15.74016213 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 151
Checksum: 261
</pre>
<p> Coasting Arc #2 (Orbit 166)
</p><hr/>
<p> Vector Time (GMT): 2010/145/05:07:29.776
Vector Time (MET): 010/10:47:20.821
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479639.18 A = 6729692.90 meter
Y = 3100864.13 meter E = .0013693
Z = 2378578.25 I = 51.58816
XDOT = -4295.064985 Wp = 58.17708
YDOT = -3441.964680 meter/sec RA = 347.92575 deg
ZDOT = -5377.869431 TA = 95.01376
MA = 94.85743
Ha = 192.466 n.mi
Hp = 182.940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17977818.82 X = -5525461.26
Y = 10173438.73 feet Y = 3039331.09 meter
Z = 7803734.40 Z = 2351846.67
XDOT = -14091.420555 XDOT = -4230.131886
YDOT = -11292.535040 feet/sec YDOT = -3489.631043 meter/sec
ZDOT = -17643.928578 ZDOT = -5398.577879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20261101.26 X = -6175583.66
Y = -4223629.88 feet Y = -1287362.39 meter
Z = 7697260.71 Z = 2346125.06
XDOT = -3387.760093 XDOT = -1032.589276
YDOT = -16233.772562 feet/sec YDOT = -4948.053877 meter/sec
ZDOT = -17726.388959 ZDOT = -5403.003355
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.24997835 .00020000 00000-0 20000-3 0 9012
2 36572 51.6456 348.2709 0011274 351.5455 8.5517 15.74033977 1674
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.24997835 = yrday.fracday
Element set: 901
Inclination: 51.6456 deg
RA of node: 348.2709 deg
Eccentricity: .0011274
Arg of perigee: 351.5455 deg
Mean anomaly: 8.5517 deg
</pre>
<p> Mean motion: 15.74033977 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 167
Checksum: 307
</pre>
<p> Coasting Arc #3 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.563
Vector Time (MET): 010/21:03:19.608
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262066.21 A = 6723050.91 meter
Y = 2599573.09 meter E = .0013333
Z = 4493725.11 I = 51.55255
XDOT = -5764.116617 Wp = 12.07650
YDOT = 4036.590451 meter/sec RA = 345.76578 deg
ZDOT = 3142.990439 TA = 46.59888
MA = 46.48795
Ha = 193.910 n.mi
Hp = 181.696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13983156.86 X = 4210850.42
Y = 8528783.10 feet Y = 2646947.18 meter
Z = 14743192.62 Z = 4514306.52
XDOT = -18911.143757 XDOT = -5824.094464
YDOT = 13243.406991 feet/sec YDOT = 3971.796955 meter/sec
ZDOT = 10311.648421 ZDOT = 3114.842590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2365866.47 X = 721116.10
Y = -16132209.43 feet Y = -4917097.43 meter
Z = 14825148.91 Z = 4518705.39
XDOT = 18469.695762 XDOT = 5629.563268
YDOT = 12048.387081 feet/sec YDOT = 3672.348382 meter/sec
ZDOT = 10199.529579 ZDOT = 3108.816616
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69440136 .00020000 00000-0 20000-3 0 9029
2 36572 51.6443 345.9838 0017293 342.9630 17.0950 15.74078594 1741
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69440136 = yrday.fracday
Element set: 902
Inclination: 51.6443 deg
RA of node: 345.9838 deg
Eccentricity: .0017293
Arg of perigee: 342.9630 deg
Mean anomaly: 17.0950 deg
</pre>
<p> Mean motion: 15.74078594 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 301
</pre>
<p> Coasting Arc #4 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:03.568
Vector Time (MET): 011/21:03:54.613
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880170.62 A = 6729240.37 meter
Y = -3856550.09 meter E = .0020258
Z = -2536322.42 I = 51.54501
XDOT = 4897.378121 Wp = 359.98214
YDOT = 2729.737006 meter/sec RA = 340.57710 deg
ZDOT = 5292.364101 TA = 331.19102
MA = 331.30274
Ha = 194.240 n.mi
Hp = 181.481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16011058.48 X = 4935253.77
Y = -12652723.41 feet Y = -3801668.78 meter
Z = -8321267.79 Z = -2512480.85
XDOT = 16067.513521 XDOT = 4840.779906
YDOT = 8955.830072 feet/sec YDOT = 2784.185215 meter/sec
ZDOT = 17363.399282 ZDOT = 5316.018901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18145749.25 X = -5530824.37
Y = -9420654.50 feet Y = -2871415.49 meter
Z = -8226296.47 Z = -2507375.17
XDOT = 896.621390 XDOT = 273.290200
YDOT = -16913.682960 feet/sec YDOT = -5155.290566 meter/sec
ZDOT = 17457.592792 ZDOT = 5321.074283
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64670948 .00020000 00000-0 20000-3 0 9032
2 36572 51.6453 341.0938 0017293 347.0084 13.0632 15.74068320 1894
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64670948 = yrday.fracday
Element set: 903
Inclination: 51.6453 deg
RA of node: 341.0938 deg
Eccentricity: .0017293
Arg of perigee: 347.0084 deg
Mean anomaly: 13.0632 deg
</pre>
<p> Mean motion: 15.74068320 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 287</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
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[STSTLE LIST] Current STS TLEs @ 00:30 UTCtag:www.aus-city.com,2010-05-25:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100525104502%2F2010-05-25T10:45:02Z2010-05-25T10:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.259 11.3 -0.1 17.6
010/21:03:13.304 6.7 -0.0 193.9
000/00:00:12.608 11.7 -17.6 181.7
</pre>
<p> Coasting Arc #1 (Orbit 150)
</p><hr/>
<p> Vector Time (GMT): 2010/144/05:06:55.000
Vector Time (MET): 009/10:46:46.045
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739169.20 A = 6722925.08 meter
Y = -3210263.48 meter E = .0016348
Z = -4586272.80 I = 51.59510
XDOT = 6357.177738 Wp = 26.96158
YDOT = -3142.358338 meter/sec RA = 353.10948 deg
ZDOT = -2973.239778 TA = 213.42123
MA = 213.52452
Ha = 192.297 n.mi
Hp = 183.054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12267615.50 X = -3680713.90
Y = -10532360.49 feet Y = -3251749.89 meter
Z = -15046826.78 Z = -4604296.24
XDOT = 20856.882344 XDOT = 6406.287369
YDOT = -10309.574601 feet/sec YDOT = -3070.993772 meter/sec
ZDOT = -9754.723682 ZDOT = -2942.237058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1905214.81 X = -580709.47
Y = -15988436.72 feet Y = -4873275.51 meter
Z = -15118599.51 Z = -4608149.13
XDOT = 21235.882470 XDOT = 6472.696977
YDOT = 6608.172546 feet/sec YDOT = 2014.170992 meter/sec
ZDOT = -9631.239121 ZDOT = -2935.601684
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10144.23415742 .00020000 00000-0 20000-3 0 9001
2 36572 51.6454 353.4871 0011187 347.7804 12.3086 15.74016213 1519
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10144.23415742 = yrday.fracday
Element set: 900
Inclination: 51.6454 deg
RA of node: 353.4871 deg
Eccentricity: .0011187
Arg of perigee: 347.7804 deg
Mean anomaly: 12.3086 deg
</pre>
<p> Mean motion: 15.74016213 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 151
Checksum: 261
</pre>
<p> Coasting Arc #2 (Orbit 166)
</p><hr/>
<p> Vector Time (GMT): 2010/145/05:07:29.776
Vector Time (MET): 010/10:47:20.821
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479639.18 A = 6729692.90 meter
Y = 3100864.13 meter E = .0013693
Z = 2378578.25 I = 51.58816
XDOT = -4295.064985 Wp = 58.17708
YDOT = -3441.964680 meter/sec RA = 347.92575 deg
ZDOT = -5377.869431 TA = 95.01376
MA = 94.85743
Ha = 192.466 n.mi
Hp = 182.940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17977818.82 X = -5525461.26
Y = 10173438.73 feet Y = 3039331.09 meter
Z = 7803734.40 Z = 2351846.67
XDOT = -14091.420555 XDOT = -4230.131886
YDOT = -11292.535040 feet/sec YDOT = -3489.631043 meter/sec
ZDOT = -17643.928578 ZDOT = -5398.577879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20261101.26 X = -6175583.66
Y = -4223629.88 feet Y = -1287362.39 meter
Z = 7697260.71 Z = 2346125.06
XDOT = -3387.760093 XDOT = -1032.589276
YDOT = -16233.772562 feet/sec YDOT = -4948.053877 meter/sec
ZDOT = -17726.388959 ZDOT = -5403.003355
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.24997835 .00020000 00000-0 20000-3 0 9012
2 36572 51.6456 348.2709 0011274 351.5455 8.5517 15.74033977 1674
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.24997835 = yrday.fracday
Element set: 901
Inclination: 51.6456 deg
RA of node: 348.2709 deg
Eccentricity: .0011274
Arg of perigee: 351.5455 deg
Mean anomaly: 8.5517 deg
</pre>
<p> Mean motion: 15.74033977 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 167
Checksum: 307
</pre>
<p> Coasting Arc #3 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.563
Vector Time (MET): 010/21:03:19.608
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262066.21 A = 6723050.91 meter
Y = 2599573.09 meter E = .0013333
Z = 4493725.11 I = 51.55255
XDOT = -5764.116617 Wp = 12.07650
YDOT = 4036.590451 meter/sec RA = 345.76578 deg
ZDOT = 3142.990439 TA = 46.59888
MA = 46.48795
Ha = 193.910 n.mi
Hp = 181.696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13983156.86 X = 4210850.42
Y = 8528783.10 feet Y = 2646947.18 meter
Z = 14743192.62 Z = 4514306.52
XDOT = -18911.143757 XDOT = -5824.094464
YDOT = 13243.406991 feet/sec YDOT = 3971.796955 meter/sec
ZDOT = 10311.648421 ZDOT = 3114.842590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2365866.47 X = 721116.10
Y = -16132209.43 feet Y = -4917097.43 meter
Z = 14825148.91 Z = 4518705.39
XDOT = 18469.695762 XDOT = 5629.563268
YDOT = 12048.387081 feet/sec YDOT = 3672.348382 meter/sec
ZDOT = 10199.529579 ZDOT = 3108.816616
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69440136 .00020000 00000-0 20000-3 0 9029
2 36572 51.6443 345.9838 0017293 342.9630 17.0950 15.74078594 1741
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69440136 = yrday.fracday
Element set: 902
Inclination: 51.6443 deg
RA of node: 345.9838 deg
Eccentricity: .0017293
Arg of perigee: 342.9630 deg
Mean anomaly: 17.0950 deg
</pre>
<p> Mean motion: 15.74078594 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 301
</pre>
<p> Coasting Arc #4 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:03.568
Vector Time (MET): 011/21:03:54.613
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880170.62 A = 6729240.37 meter
Y = -3856550.09 meter E = .0020258
Z = -2536322.42 I = 51.54501
XDOT = 4897.378121 Wp = 359.98214
YDOT = 2729.737006 meter/sec RA = 340.57710 deg
ZDOT = 5292.364101 TA = 331.19102
MA = 331.30274
Ha = 194.240 n.mi
Hp = 181.481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16011058.48 X = 4935253.77
Y = -12652723.41 feet Y = -3801668.78 meter
Z = -8321267.79 Z = -2512480.85
XDOT = 16067.513521 XDOT = 4840.779906
YDOT = 8955.830072 feet/sec YDOT = 2784.185215 meter/sec
ZDOT = 17363.399282 ZDOT = 5316.018901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18145749.25 X = -5530824.37
Y = -9420654.50 feet Y = -2871415.49 meter
Z = -8226296.47 Z = -2507375.17
XDOT = 896.621390 XDOT = 273.290200
YDOT = -16913.682960 feet/sec YDOT = -5155.290566 meter/sec
ZDOT = 17457.592792 ZDOT = 5321.074283
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64670948 .00020000 00000-0 20000-3 0 9032
2 36572 51.6453 341.0938 0017293 347.0084 13.0632 15.74068320 1894
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64670948 = yrday.fracday
Element set: 903
Inclination: 51.6453 deg
RA of node: 341.0938 deg
Eccentricity: .0017293
Arg of perigee: 347.0084 deg
Mean anomaly: 13.0632 deg
</pre>
<p> Mean motion: 15.74068320 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 287</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
<p>The following information is a reminder of your current mailing
list subscription:
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[STSTLE LIST] Current STS TLEs @ 18:30 UTCtag:www.aus-city.com,2010-05-25:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100525044502%2F2010-05-25T04:45:02Z2010-05-25T04:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
145/15:23:22.259 11.3 -0.1 17.6
010/21:03:13.304 6.7 -0.0 193.9
000/00:00:12.608 11.7 -17.6 181.7
</pre>
<p> Coasting Arc #1 (Orbit 150)
</p><hr/>
<p> Vector Time (GMT): 2010/144/05:06:55.000
Vector Time (MET): 009/10:46:46.045
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739169.20 A = 6722925.08 meter
Y = -3210263.48 meter E = .0016348
Z = -4586272.80 I = 51.59510
XDOT = 6357.177738 Wp = 26.96158
YDOT = -3142.358338 meter/sec RA = 353.10948 deg
ZDOT = -2973.239778 TA = 213.42123
MA = 213.52452
Ha = 192.297 n.mi
Hp = 183.054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12267615.50 X = -3680713.90
Y = -10532360.49 feet Y = -3251749.89 meter
Z = -15046826.78 Z = -4604296.24
XDOT = 20856.882344 XDOT = 6406.287369
YDOT = -10309.574601 feet/sec YDOT = -3070.993772 meter/sec
ZDOT = -9754.723682 ZDOT = -2942.237058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1905214.81 X = -580709.47
Y = -15988436.72 feet Y = -4873275.51 meter
Z = -15118599.51 Z = -4608149.13
XDOT = 21235.882470 XDOT = 6472.696977
YDOT = 6608.172546 feet/sec YDOT = 2014.170992 meter/sec
ZDOT = -9631.239121 ZDOT = -2935.601684
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10144.23415742 .00020000 00000-0 20000-3 0 9001
2 36572 51.6454 353.4871 0011187 347.7804 12.3086 15.74016213 1519
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10144.23415742 = yrday.fracday
Element set: 900
Inclination: 51.6454 deg
RA of node: 353.4871 deg
Eccentricity: .0011187
Arg of perigee: 347.7804 deg
Mean anomaly: 12.3086 deg
</pre>
<p> Mean motion: 15.74016213 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 151
Checksum: 261
</pre>
<p> Coasting Arc #2 (Orbit 166)
</p><hr/>
<p> Vector Time (GMT): 2010/145/05:07:29.776
Vector Time (MET): 010/10:47:20.821
Weight (LBS) : 221081.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479639.18 A = 6729692.90 meter
Y = 3100864.13 meter E = .0013693
Z = 2378578.25 I = 51.58816
XDOT = -4295.064985 Wp = 58.17708
YDOT = -3441.964680 meter/sec RA = 347.92575 deg
ZDOT = -5377.869431 TA = 95.01376
MA = 94.85743
Ha = 192.466 n.mi
Hp = 182.940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17977818.82 X = -5525461.26
Y = 10173438.73 feet Y = 3039331.09 meter
Z = 7803734.40 Z = 2351846.67
XDOT = -14091.420555 XDOT = -4230.131886
YDOT = -11292.535040 feet/sec YDOT = -3489.631043 meter/sec
ZDOT = -17643.928578 ZDOT = -5398.577879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20261101.26 X = -6175583.66
Y = -4223629.88 feet Y = -1287362.39 meter
Z = 7697260.71 Z = 2346125.06
XDOT = -3387.760093 XDOT = -1032.589276
YDOT = -16233.772562 feet/sec YDOT = -4948.053877 meter/sec
ZDOT = -17726.388959 ZDOT = -5403.003355
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.24997835 .00020000 00000-0 20000-3 0 9012
2 36572 51.6456 348.2709 0011274 351.5455 8.5517 15.74033977 1674
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.24997835 = yrday.fracday
Element set: 901
Inclination: 51.6456 deg
RA of node: 348.2709 deg
Eccentricity: .0011274
Arg of perigee: 351.5455 deg
Mean anomaly: 8.5517 deg
</pre>
<p> Mean motion: 15.74033977 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 167
Checksum: 307
</pre>
<p> Coasting Arc #3 (Orbit 173)
</p><hr/>
<p> Vector Time (GMT): 2010/145/15:23:28.563
Vector Time (MET): 010/21:03:19.608
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262066.21 A = 6723050.91 meter
Y = 2599573.09 meter E = .0013333
Z = 4493725.11 I = 51.55255
XDOT = -5764.116617 Wp = 12.07650
YDOT = 4036.590451 meter/sec RA = 345.76578 deg
ZDOT = 3142.990439 TA = 46.59888
MA = 46.48795
Ha = 193.910 n.mi
Hp = 181.696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13983156.86 X = 4210850.42
Y = 8528783.10 feet Y = 2646947.18 meter
Z = 14743192.62 Z = 4514306.52
XDOT = -18911.143757 XDOT = -5824.094464
YDOT = 13243.406991 feet/sec YDOT = 3971.796955 meter/sec
ZDOT = 10311.648421 ZDOT = 3114.842590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2365866.47 X = 721116.10
Y = -16132209.43 feet Y = -4917097.43 meter
Z = 14825148.91 Z = 4518705.39
XDOT = 18469.695762 XDOT = 5629.563268
YDOT = 12048.387081 feet/sec YDOT = 3672.348382 meter/sec
ZDOT = 10199.529579 ZDOT = 3108.816616
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10145.69440136 .00020000 00000-0 20000-3 0 9029
2 36572 51.6443 345.9838 0017293 342.9630 17.0950 15.74078594 1741
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10145.69440136 = yrday.fracday
Element set: 902
Inclination: 51.6443 deg
RA of node: 345.9838 deg
Eccentricity: .0017293
Arg of perigee: 342.9630 deg
Mean anomaly: 17.0950 deg
</pre>
<p> Mean motion: 15.74078594 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 174
Checksum: 301
</pre>
<p> Coasting Arc #4 (Orbit 188)
</p><hr/>
<p> Vector Time (GMT): 2010/146/15:24:03.568
Vector Time (MET): 011/21:03:54.613
Weight (LBS) : 220697.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880170.62 A = 6729240.37 meter
Y = -3856550.09 meter E = .0020258
Z = -2536322.42 I = 51.54501
XDOT = 4897.378121 Wp = 359.98214
YDOT = 2729.737006 meter/sec RA = 340.57710 deg
ZDOT = 5292.364101 TA = 331.19102
MA = 331.30274
Ha = 194.240 n.mi
Hp = 181.481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16011058.48 X = 4935253.77
Y = -12652723.41 feet Y = -3801668.78 meter
Z = -8321267.79 Z = -2512480.85
XDOT = 16067.513521 XDOT = 4840.779906
YDOT = 8955.830072 feet/sec YDOT = 2784.185215 meter/sec
ZDOT = 17363.399282 ZDOT = 5316.018901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18145749.25 X = -5530824.37
Y = -9420654.50 feet Y = -2871415.49 meter
Z = -8226296.47 Z = -2507375.17
XDOT = 896.621390 XDOT = 273.290200
YDOT = -16913.682960 feet/sec YDOT = -5155.290566 meter/sec
ZDOT = 17457.592792 ZDOT = 5321.074283
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10146.64670948 .00020000 00000-0 20000-3 0 9032
2 36572 51.6453 341.0938 0017293 347.0084 13.0632 15.74068320 1894
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10146.64670948 = yrday.fracday
Element set: 903
Inclination: 51.6453 deg
RA of node: 341.0938 deg
Eccentricity: .0017293
Arg of perigee: 347.0084 deg
Mean anomaly: 13.0632 deg
</pre>
<p> Mean motion: 15.74068320 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 189
Checksum: 287</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
<p>The following information is a reminder of your current mailing
list subscription:
</p><p>You are subscribed to the following list:
</p><p><strong>[STSTLE LIST]</strong>
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[STSTLE LIST] Current STS TLEs @ 12:30 UTCtag:www.aus-city.com,2010-05-24:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100524224502%2F2010-05-24T22:45:02Z2010-05-24T22:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
143/14:34:09.230 0.1 -0.1 0.1
008/20:14:00.275 0.0 0.1 191.4
000/00:00:00.549 -0.1 0.0 183.1
143/16:37:14.662 -2.9 -0.0 3.0
008/22:17:05.707 0.6 -0.0 191.7
000/00:00:11.414 0.5 -3.0 182.8
143/17:05:11.808 1.5 1.5 1.5
008/22:45:02.853 0.0 0.0 192.0
000/00:00:05.705 0.2 -0.0 183.4
</pre>
<p> Coasting Arc #1 (Orbit 113)
</p><hr/>
<p> Vector Time (GMT): 2010/141/20:07:01.000
Vector Time (MET): 007/01:46:52.045
Weight (LBS) : 214758.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -717806.54 A = 6719533.18 meter
Y = 4115217.58 meter E = .0010016
Z = 5264721.13 I = 51.66005
XDOT = -7637.199375 Wp = 352.99453
YDOT = -940.649143 meter/sec RA = 5.27638 deg
ZDOT = -296.307509 TA = 99.87398
MA = 99.76088
Ha = 191.320 n.mi
Hp = 183.605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2355008.34 X = -789345.49
Y = 13501370.02 feet Y = 4106790.34 meter
Z = 17272707.12 Z = 5261060.48
XDOT = -25056.428396 XDOT = -7624.673834
YDOT = -3086.119236 feet/sec YDOT = -1025.982804 meter/sec
ZDOT = -972.137496 ZDOT = -333.378851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2377884.94 X = 724779.33
Y = -13516007.55 feet Y = -4119679.10 meter
Z = 17258118.99 Z = 5260274.67
XDOT = 24082.264144 XDOT = 7340.274111
YDOT = 2766.311354 feet/sec YDOT = 843.171701 meter/sec
ZDOT = -1119.794933 ZDOT = -341.313496
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10141.88526817 .00020000 00000-0 20000-3 0 9005
2 36572 51.6483 5.5448 0009925 338.9424 21.1329 15.74211672 1146
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10141.88526817 = yrday.fracday
Element set: 900
Inclination: 51.6483 deg
RA of node: 5.5448 deg
Eccentricity: .0009925
Arg of perigee: 338.9424 deg
Mean anomaly: 21.1329 deg
</pre>
<p> Mean motion: 15.74211672 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 114
Checksum: 282
</pre>
<p> Coasting Arc #2 (Orbit 129)
</p><hr/>
<p> Vector Time (GMT): 2010/142/20:07:47.167
Vector Time (MET): 008/01:47:38.212
Weight (LBS) : 214688.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6672574.17 A = 6731452.35 meter
Y = 499197.29 meter E = .0019356
Z = 609548.58 I = 51.66997
XDOT = -907.973768 Wp = 22.67398
YDOT = 4746.603776 meter/sec RA = .14842 deg
ZDOT = 6006.725392 TA = 343.96709
MA = 344.02826
Ha = 191.474 n.mi
Hp = 183.357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21891647.54 X = 6663535.02
Y = 1637786.38 feet Y = 573763.41 meter
Z = 1999831.30 Z = 641942.35
XDOT = -2978.916561 XDOT = -990.163546
YDOT = 15572.847034 feet/sec YDOT = 4735.990379 meter/sec
ZDOT = 19707.104304 ZDOT = 6002.115043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21915096.45 X = -6679721.40
Y = -1059450.46 feet Y = -322920.50 meter
Z = 2128852.66 Z = 648874.29
XDOT = 2605.462512 XDOT = 794.144974
YDOT = -14051.665120 feet/sec YDOT = -4282.947528 meter/sec
ZDOT = 19688.731588 ZDOT = 6001.125388
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10142.90098002 .00020000 00000-0 20000-3 0 9010
2 36572 51.6484 .3286 0009985 343.4320 16.6515 15.74195910 1302
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10142.90098002 = yrday.fracday
Element set: 901
Inclination: 51.6484 deg
RA of node: .3286 deg
Eccentricity: .0009985
Arg of perigee: 343.4320 deg
Mean anomaly: 16.6515 deg
</pre>
<p> Mean motion: 15.74195910 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 130
Checksum: 263
</pre>
<p> Coasting Arc #3 (Orbit 141)
</p><hr/>
<p> Vector Time (GMT): 2010/143/14:34:09.504
Vector Time (MET): 008/20:14:00.549
Weight (LBS) : 214684.4
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025782.05 A = 6725531.18 meter
Y = 2561971.08 meter E = .0012633
Z = 3646438.97 I = 51.62290
XDOT = -5098.897557 Wp = 46.68514
YDOT = 3796.693669 meter/sec RA = 356.21959 deg
ZDOT = 4359.231242 TA = 357.14156
MA = 357.14878
Ha = 191.403 n.mi
Hp = 183.115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16488786.25 X = 4979046.11
Y = 8405416.94 feet Y = 2617910.82 meter
Z = 11963382.45 Z = 3670741.21
XDOT = -16728.666527 XDOT = -5162.150557
YDOT = 12456.344058 feet/sec YDOT = 3739.320803 meter/sec
ZDOT = 14301.939769 ZDOT = 4334.307060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5775653.53 X = 1760419.20
Y = -17517072.26 feet Y = -5339203.62 meter
Z = 12060167.15 Z = 3675938.95
XDOT = 13621.208778 XDOT = 4151.744435
YDOT = 14271.387429 feet/sec YDOT = 4349.918888 meter/sec
ZDOT = 14202.661885 ZDOT = 4328.971342
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.66274765 .00020000 00000-0 20000-3 0 9027
2 36572 51.6437 356.4139 0010058 345.6385 14.4491 15.74267070 1429
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.66274765 = yrday.fracday
Element set: 902
Inclination: 51.6437 deg
RA of node: 356.4139 deg
Eccentricity: .0010058
Arg of perigee: 345.6385 deg
Mean anomaly: 14.4491 deg
</pre>
<p> Mean motion: 15.74267070 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 142
Checksum: 287
</pre>
<p> Coasting Arc #4 (Orbit 142)
</p><hr/>
<p> Vector Time (GMT): 2010/143/16:37:20.369
Vector Time (MET): 008/22:17:11.414
Weight (LBS) : 214609.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6530778.40 A = 6731021.85 meter
Y = 1283504.22 meter E = .0010273
Z = 1004763.55 I = 51.63959
XDOT = -1816.531334 Wp = 78.13947
YDOT = -4565.207267 meter/sec RA = 355.74347 deg
ZDOT = -5922.481185 TA = 90.88630
MA = 90.76859
Ha = 191.715 n.mi
Hp = 182.780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21426438.34 X = -6549526.42
Y = 4210971.84 feet Y = 1210368.27 meter
Z = 3296468.35 Z = 972991.12
XDOT = -5959.748470 XDOT = -1736.576600
YDOT = -14977.714129 feet/sec YDOT = -4585.073349 meter/sec
ZDOT = -19430.712550 ZDOT = -5931.112118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16949111.19 X = 5166089.09
Y = 13797480.63 feet Y = 4205472.10 meter
Z = 3169921.96 Z = 966192.21
XDOT = -6773.916181 XDOT = -2064.689652
YDOT = 12834.759957 feet/sec YDOT = 3912.034835 meter/sec
ZDOT = -19465.075909 ZDOT = -5932.955137
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.72623314 .00020000 00000-0 20000-3 0 9033
2 36572 51.6448 356.0868 0009895 353.1826 6.9201 15.74262816 1436
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.72623314 = yrday.fracday
Element set: 903
Inclination: 51.6448 deg
RA of node: 356.0868 deg
Eccentricity: .0009895
Arg of perigee: 353.1826 deg
Mean anomaly: 6.9201 deg
</pre>
<p> Mean motion: 15.74262816 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 143
Checksum: 290
</pre>
<p> Coasting Arc #5 (Orbit 142)
</p><hr/>
<p> Vector Time (GMT): 2010/143/17:05:14.660
Vector Time (MET): 008/22:45:05.705
Weight (LBS) : 214572.6
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 700139.57 A = 6720424.47 meter
Y = -4195947.19 meter E = .0014626
Z = -5212032.88 I = 51.60205
XDOT = 7636.860108 Wp = 56.17821
YDOT = 147.500282 meter/sec RA = 355.64706 deg
ZDOT = 916.950212 TA = 222.51283
MA = 222.62618
Ha = 192.008 n.mi
Hp = 183.434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2297045.83 X = 772326.85
Y = -13766230.94 feet Y = -4187713.84 meter
Z = -17099845.41 Z = -5208456.49
XDOT = 25055.315316 XDOT = 7630.188698
YDOT = 483.924810 feet/sec YDOT = 232.862836 meter/sec
ZDOT = 3008.366838 ZDOT = 954.034419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11180937.01 X = -3407949.60
Y = 8382093.51 feet Y = 2554862.10 meter
Z = -17085590.51 Z = -5207687.99
XDOT = -17289.954435 XDOT = -5269.978112
YDOT = -16695.814231 feet/sec YDOT = -5088.884177 meter/sec
ZDOT = 3156.065122 ZDOT = 961.968649
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.72623388 .00020000 00000-0 20000-3 0 9045
2 36572 51.6461 356.0885 0010174 347.2827 12.8079 15.73991511 1436
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.72623388 = yrday.fracday
Element set: 904
Inclination: 51.6461 deg
RA of node: 356.0885 deg
Eccentricity: .0010174
Arg of perigee: 347.2827 deg
Mean anomaly: 12.8079 deg
</pre>
<p> Mean motion: 15.73991511 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 143
Checksum: 292
</pre>
<p> Coasting Arc #6 (Orbit 158)
</p><hr/>
<p> Vector Time (GMT): 2010/144/17:05:42.445
Vector Time (MET): 009/22:45:33.490
Weight (LBS) : 214572.6
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6652890.67 A = 6731684.12 meter
Y = 312400.20 meter E = .0005025
Z = -993422.50 I = 51.60999
XDOT = 652.843751 Wp = 59.85609
YDOT = -4865.915396 meter/sec RA = 350.52454 deg
ZDOT = -5922.016161 TA = 130.99271
MA = 130.94924
Ha = 192.152 n.mi
Hp = 183.156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21827069.13 X = -6651063.57
Y = 1024935.04 feet Y = 238013.92 meter
Z = -3259260.18 Z = -1025738.36
XDOT = 2141.875822 XDOT = 735.975369
YDOT = -15964.289357 feet/sec YDOT = -4858.149563 meter/sec
ZDOT = -19429.186879 ZDOT = -5918.643095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16853228.38 X = 5136864.01
Y = 13877485.60 feet Y = 4229857.61 meter
Z = -3387964.31 Z = -1032651.52
XDOT = -11376.295240 XDOT = -3467.494789
YDOT = 9090.913687 feet/sec YDOT = 2770.910492 meter/sec
ZDOT = -19415.736378 ZDOT = -5917.916448
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10144.74207957 .00020000 00000-0 20000-3 0 9059
2 36572 51.6459 350.8711 0010291 350.8750 9.2225 15.74008173 1592
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10144.74207957 = yrday.fracday
Element set: 905
Inclination: 51.6459 deg
RA of node: 350.8711 deg
Eccentricity: .0010291
Arg of perigee: 350.8750 deg
Mean anomaly: 9.2225 deg
</pre>
<p> Mean motion: 15.74008173 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 159
Checksum: 282</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
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[STSTLE LIST] Current STS TLEs @ 06:30 UTCtag:www.aus-city.com,2010-05-24:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100524164502%2F2010-05-24T16:45:02Z2010-05-24T16:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
143/14:34:09.230 0.1 -0.1 0.1
008/20:14:00.275 0.0 0.1 191.4
000/00:00:00.549 -0.1 0.0 183.1
143/16:37:14.662 -2.9 -0.0 3.0
008/22:17:05.707 0.6 -0.0 191.7
000/00:00:11.414 0.5 -3.0 182.8
143/17:05:11.808 1.5 1.5 1.5
008/22:45:02.853 0.0 0.0 192.0
000/00:00:05.705 0.2 -0.0 183.4
</pre>
<p> Coasting Arc #1 (Orbit 113)
</p><hr/>
<p> Vector Time (GMT): 2010/141/20:07:01.000
Vector Time (MET): 007/01:46:52.045
Weight (LBS) : 214758.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -717806.54 A = 6719533.18 meter
Y = 4115217.58 meter E = .0010016
Z = 5264721.13 I = 51.66005
XDOT = -7637.199375 Wp = 352.99453
YDOT = -940.649143 meter/sec RA = 5.27638 deg
ZDOT = -296.307509 TA = 99.87398
MA = 99.76088
Ha = 191.320 n.mi
Hp = 183.605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2355008.34 X = -789345.49
Y = 13501370.02 feet Y = 4106790.34 meter
Z = 17272707.12 Z = 5261060.48
XDOT = -25056.428396 XDOT = -7624.673834
YDOT = -3086.119236 feet/sec YDOT = -1025.982804 meter/sec
ZDOT = -972.137496 ZDOT = -333.378851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2377884.94 X = 724779.33
Y = -13516007.55 feet Y = -4119679.10 meter
Z = 17258118.99 Z = 5260274.67
XDOT = 24082.264144 XDOT = 7340.274111
YDOT = 2766.311354 feet/sec YDOT = 843.171701 meter/sec
ZDOT = -1119.794933 ZDOT = -341.313496
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10141.88526817 .00020000 00000-0 20000-3 0 9005
2 36572 51.6483 5.5448 0009925 338.9424 21.1329 15.74211672 1146
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10141.88526817 = yrday.fracday
Element set: 900
Inclination: 51.6483 deg
RA of node: 5.5448 deg
Eccentricity: .0009925
Arg of perigee: 338.9424 deg
Mean anomaly: 21.1329 deg
</pre>
<p> Mean motion: 15.74211672 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 114
Checksum: 282
</pre>
<p> Coasting Arc #2 (Orbit 129)
</p><hr/>
<p> Vector Time (GMT): 2010/142/20:07:47.167
Vector Time (MET): 008/01:47:38.212
Weight (LBS) : 214688.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6672574.17 A = 6731452.35 meter
Y = 499197.29 meter E = .0019356
Z = 609548.58 I = 51.66997
XDOT = -907.973768 Wp = 22.67398
YDOT = 4746.603776 meter/sec RA = .14842 deg
ZDOT = 6006.725392 TA = 343.96709
MA = 344.02826
Ha = 191.474 n.mi
Hp = 183.357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21891647.54 X = 6663535.02
Y = 1637786.38 feet Y = 573763.41 meter
Z = 1999831.30 Z = 641942.35
XDOT = -2978.916561 XDOT = -990.163546
YDOT = 15572.847034 feet/sec YDOT = 4735.990379 meter/sec
ZDOT = 19707.104304 ZDOT = 6002.115043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21915096.45 X = -6679721.40
Y = -1059450.46 feet Y = -322920.50 meter
Z = 2128852.66 Z = 648874.29
XDOT = 2605.462512 XDOT = 794.144974
YDOT = -14051.665120 feet/sec YDOT = -4282.947528 meter/sec
ZDOT = 19688.731588 ZDOT = 6001.125388
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10142.90098002 .00020000 00000-0 20000-3 0 9010
2 36572 51.6484 .3286 0009985 343.4320 16.6515 15.74195910 1302
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10142.90098002 = yrday.fracday
Element set: 901
Inclination: 51.6484 deg
RA of node: .3286 deg
Eccentricity: .0009985
Arg of perigee: 343.4320 deg
Mean anomaly: 16.6515 deg
</pre>
<p> Mean motion: 15.74195910 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 130
Checksum: 263
</pre>
<p> Coasting Arc #3 (Orbit 141)
</p><hr/>
<p> Vector Time (GMT): 2010/143/14:34:09.504
Vector Time (MET): 008/20:14:00.549
Weight (LBS) : 214684.4
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025782.05 A = 6725531.18 meter
Y = 2561971.08 meter E = .0012633
Z = 3646438.97 I = 51.62290
XDOT = -5098.897557 Wp = 46.68514
YDOT = 3796.693669 meter/sec RA = 356.21959 deg
ZDOT = 4359.231242 TA = 357.14156
MA = 357.14878
Ha = 191.403 n.mi
Hp = 183.115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16488786.25 X = 4979046.11
Y = 8405416.94 feet Y = 2617910.82 meter
Z = 11963382.45 Z = 3670741.21
XDOT = -16728.666527 XDOT = -5162.150557
YDOT = 12456.344058 feet/sec YDOT = 3739.320803 meter/sec
ZDOT = 14301.939769 ZDOT = 4334.307060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5775653.53 X = 1760419.20
Y = -17517072.26 feet Y = -5339203.62 meter
Z = 12060167.15 Z = 3675938.95
XDOT = 13621.208778 XDOT = 4151.744435
YDOT = 14271.387429 feet/sec YDOT = 4349.918888 meter/sec
ZDOT = 14202.661885 ZDOT = 4328.971342
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.66274765 .00020000 00000-0 20000-3 0 9027
2 36572 51.6437 356.4139 0010058 345.6385 14.4491 15.74267070 1429
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.66274765 = yrday.fracday
Element set: 902
Inclination: 51.6437 deg
RA of node: 356.4139 deg
Eccentricity: .0010058
Arg of perigee: 345.6385 deg
Mean anomaly: 14.4491 deg
</pre>
<p> Mean motion: 15.74267070 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 142
Checksum: 287
</pre>
<p> Coasting Arc #4 (Orbit 142)
</p><hr/>
<p> Vector Time (GMT): 2010/143/16:37:20.369
Vector Time (MET): 008/22:17:11.414
Weight (LBS) : 214609.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6530778.40 A = 6731021.85 meter
Y = 1283504.22 meter E = .0010273
Z = 1004763.55 I = 51.63959
XDOT = -1816.531334 Wp = 78.13947
YDOT = -4565.207267 meter/sec RA = 355.74347 deg
ZDOT = -5922.481185 TA = 90.88630
MA = 90.76859
Ha = 191.715 n.mi
Hp = 182.780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21426438.34 X = -6549526.42
Y = 4210971.84 feet Y = 1210368.27 meter
Z = 3296468.35 Z = 972991.12
XDOT = -5959.748470 XDOT = -1736.576600
YDOT = -14977.714129 feet/sec YDOT = -4585.073349 meter/sec
ZDOT = -19430.712550 ZDOT = -5931.112118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16949111.19 X = 5166089.09
Y = 13797480.63 feet Y = 4205472.10 meter
Z = 3169921.96 Z = 966192.21
XDOT = -6773.916181 XDOT = -2064.689652
YDOT = 12834.759957 feet/sec YDOT = 3912.034835 meter/sec
ZDOT = -19465.075909 ZDOT = -5932.955137
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.72623314 .00020000 00000-0 20000-3 0 9033
2 36572 51.6448 356.0868 0009895 353.1826 6.9201 15.74262816 1436
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.72623314 = yrday.fracday
Element set: 903
Inclination: 51.6448 deg
RA of node: 356.0868 deg
Eccentricity: .0009895
Arg of perigee: 353.1826 deg
Mean anomaly: 6.9201 deg
</pre>
<p> Mean motion: 15.74262816 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 143
Checksum: 290
</pre>
<p> Coasting Arc #5 (Orbit 142)
</p><hr/>
<p> Vector Time (GMT): 2010/143/17:05:14.660
Vector Time (MET): 008/22:45:05.705
Weight (LBS) : 214572.6
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 700139.57 A = 6720424.47 meter
Y = -4195947.19 meter E = .0014626
Z = -5212032.88 I = 51.60205
XDOT = 7636.860108 Wp = 56.17821
YDOT = 147.500282 meter/sec RA = 355.64706 deg
ZDOT = 916.950212 TA = 222.51283
MA = 222.62618
Ha = 192.008 n.mi
Hp = 183.434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2297045.83 X = 772326.85
Y = -13766230.94 feet Y = -4187713.84 meter
Z = -17099845.41 Z = -5208456.49
XDOT = 25055.315316 XDOT = 7630.188698
YDOT = 483.924810 feet/sec YDOT = 232.862836 meter/sec
ZDOT = 3008.366838 ZDOT = 954.034419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11180937.01 X = -3407949.60
Y = 8382093.51 feet Y = 2554862.10 meter
Z = -17085590.51 Z = -5207687.99
XDOT = -17289.954435 XDOT = -5269.978112
YDOT = -16695.814231 feet/sec YDOT = -5088.884177 meter/sec
ZDOT = 3156.065122 ZDOT = 961.968649
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.72623388 .00020000 00000-0 20000-3 0 9045
2 36572 51.6461 356.0885 0010174 347.2827 12.8079 15.73991511 1436
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.72623388 = yrday.fracday
Element set: 904
Inclination: 51.6461 deg
RA of node: 356.0885 deg
Eccentricity: .0010174
Arg of perigee: 347.2827 deg
Mean anomaly: 12.8079 deg
</pre>
<p> Mean motion: 15.73991511 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 143
Checksum: 292
</pre>
<p> Coasting Arc #6 (Orbit 158)
</p><hr/>
<p> Vector Time (GMT): 2010/144/17:05:42.445
Vector Time (MET): 009/22:45:33.490
Weight (LBS) : 214572.6
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6652890.67 A = 6731684.12 meter
Y = 312400.20 meter E = .0005025
Z = -993422.50 I = 51.60999
XDOT = 652.843751 Wp = 59.85609
YDOT = -4865.915396 meter/sec RA = 350.52454 deg
ZDOT = -5922.016161 TA = 130.99271
MA = 130.94924
Ha = 192.152 n.mi
Hp = 183.156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21827069.13 X = -6651063.57
Y = 1024935.04 feet Y = 238013.92 meter
Z = -3259260.18 Z = -1025738.36
XDOT = 2141.875822 XDOT = 735.975369
YDOT = -15964.289357 feet/sec YDOT = -4858.149563 meter/sec
ZDOT = -19429.186879 ZDOT = -5918.643095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16853228.38 X = 5136864.01
Y = 13877485.60 feet Y = 4229857.61 meter
Z = -3387964.31 Z = -1032651.52
XDOT = -11376.295240 XDOT = -3467.494789
YDOT = 9090.913687 feet/sec YDOT = 2770.910492 meter/sec
ZDOT = -19415.736378 ZDOT = -5917.916448
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10144.74207957 .00020000 00000-0 20000-3 0 9059
2 36572 51.6459 350.8711 0010291 350.8750 9.2225 15.74008173 1592
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10144.74207957 = yrday.fracday
Element set: 905
Inclination: 51.6459 deg
RA of node: 350.8711 deg
Eccentricity: .0010291
Arg of perigee: 350.8750 deg
Mean anomaly: 9.2225 deg
</pre>
<p> Mean motion: 15.74008173 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 159
Checksum: 282</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
<hr/>
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[STSTLE LIST] Current STS TLEs @ 00:30 UTCtag:www.aus-city.com,2010-05-24:%2Fcgi-bin%2Fdada%2Fmail.cgi%2Farchive%2FSTSTLE_LIST%2F20100524104502%2F2010-05-24T10:45:02Z2010-05-24T10:45:02Z
<p><B> SHUTTLE TRAJECTORY DATA</B>
</p><p> Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48<br/>
Drag Coefficient (Cd) : 2.00<br/>
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18<br/>
UT1 - UTC (sec) : 0.0
</p><p> Maneuvers contained within the current ephemeris are as follows:
</p><pre>
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
143/14:34:09.230 0.1 -0.1 0.1
008/20:14:00.275 0.0 0.1 191.4
000/00:00:00.549 -0.1 0.0 183.1
143/16:37:14.662 -2.9 -0.0 3.0
008/22:17:05.707 0.6 -0.0 191.7
000/00:00:11.414 0.5 -3.0 182.8
143/17:05:11.808 1.5 1.5 1.5
008/22:45:02.853 0.0 0.0 192.0
000/00:00:05.705 0.2 -0.0 183.4
</pre>
<p> Coasting Arc #1 (Orbit 113)
</p><hr/>
<p> Vector Time (GMT): 2010/141/20:07:01.000
Vector Time (MET): 007/01:46:52.045
Weight (LBS) : 214758.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -717806.54 A = 6719533.18 meter
Y = 4115217.58 meter E = .0010016
Z = 5264721.13 I = 51.66005
XDOT = -7637.199375 Wp = 352.99453
YDOT = -940.649143 meter/sec RA = 5.27638 deg
ZDOT = -296.307509 TA = 99.87398
MA = 99.76088
Ha = 191.320 n.mi
Hp = 183.605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2355008.34 X = -789345.49
Y = 13501370.02 feet Y = 4106790.34 meter
Z = 17272707.12 Z = 5261060.48
XDOT = -25056.428396 XDOT = -7624.673834
YDOT = -3086.119236 feet/sec YDOT = -1025.982804 meter/sec
ZDOT = -972.137496 ZDOT = -333.378851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2377884.94 X = 724779.33
Y = -13516007.55 feet Y = -4119679.10 meter
Z = 17258118.99 Z = 5260274.67
XDOT = 24082.264144 XDOT = 7340.274111
YDOT = 2766.311354 feet/sec YDOT = 843.171701 meter/sec
ZDOT = -1119.794933 ZDOT = -341.313496
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10141.88526817 .00020000 00000-0 20000-3 0 9005
2 36572 51.6483 5.5448 0009925 338.9424 21.1329 15.74211672 1146
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10141.88526817 = yrday.fracday
Element set: 900
Inclination: 51.6483 deg
RA of node: 5.5448 deg
Eccentricity: .0009925
Arg of perigee: 338.9424 deg
Mean anomaly: 21.1329 deg
</pre>
<p> Mean motion: 15.74211672 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 114
Checksum: 282
</pre>
<p> Coasting Arc #2 (Orbit 129)
</p><hr/>
<p> Vector Time (GMT): 2010/142/20:07:47.167
Vector Time (MET): 008/01:47:38.212
Weight (LBS) : 214688.0
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6672574.17 A = 6731452.35 meter
Y = 499197.29 meter E = .0019356
Z = 609548.58 I = 51.66997
XDOT = -907.973768 Wp = 22.67398
YDOT = 4746.603776 meter/sec RA = .14842 deg
ZDOT = 6006.725392 TA = 343.96709
MA = 344.02826
Ha = 191.474 n.mi
Hp = 183.357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21891647.54 X = 6663535.02
Y = 1637786.38 feet Y = 573763.41 meter
Z = 1999831.30 Z = 641942.35
XDOT = -2978.916561 XDOT = -990.163546
YDOT = 15572.847034 feet/sec YDOT = 4735.990379 meter/sec
ZDOT = 19707.104304 ZDOT = 6002.115043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21915096.45 X = -6679721.40
Y = -1059450.46 feet Y = -322920.50 meter
Z = 2128852.66 Z = 648874.29
XDOT = 2605.462512 XDOT = 794.144974
YDOT = -14051.665120 feet/sec YDOT = -4282.947528 meter/sec
ZDOT = 19688.731588 ZDOT = 6001.125388
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10142.90098002 .00020000 00000-0 20000-3 0 9010
2 36572 51.6484 .3286 0009985 343.4320 16.6515 15.74195910 1302
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10142.90098002 = yrday.fracday
Element set: 901
Inclination: 51.6484 deg
RA of node: .3286 deg
Eccentricity: .0009985
Arg of perigee: 343.4320 deg
Mean anomaly: 16.6515 deg
</pre>
<p> Mean motion: 15.74195910 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 130
Checksum: 263
</pre>
<p> Coasting Arc #3 (Orbit 141)
</p><hr/>
<p> Vector Time (GMT): 2010/143/14:34:09.504
Vector Time (MET): 008/20:14:00.549
Weight (LBS) : 214684.4
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025782.05 A = 6725531.18 meter
Y = 2561971.08 meter E = .0012633
Z = 3646438.97 I = 51.62290
XDOT = -5098.897557 Wp = 46.68514
YDOT = 3796.693669 meter/sec RA = 356.21959 deg
ZDOT = 4359.231242 TA = 357.14156
MA = 357.14878
Ha = 191.403 n.mi
Hp = 183.115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16488786.25 X = 4979046.11
Y = 8405416.94 feet Y = 2617910.82 meter
Z = 11963382.45 Z = 3670741.21
XDOT = -16728.666527 XDOT = -5162.150557
YDOT = 12456.344058 feet/sec YDOT = 3739.320803 meter/sec
ZDOT = 14301.939769 ZDOT = 4334.307060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5775653.53 X = 1760419.20
Y = -17517072.26 feet Y = -5339203.62 meter
Z = 12060167.15 Z = 3675938.95
XDOT = 13621.208778 XDOT = 4151.744435
YDOT = 14271.387429 feet/sec YDOT = 4349.918888 meter/sec
ZDOT = 14202.661885 ZDOT = 4328.971342
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.66274765 .00020000 00000-0 20000-3 0 9027
2 36572 51.6437 356.4139 0010058 345.6385 14.4491 15.74267070 1429
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.66274765 = yrday.fracday
Element set: 902
Inclination: 51.6437 deg
RA of node: 356.4139 deg
Eccentricity: .0010058
Arg of perigee: 345.6385 deg
Mean anomaly: 14.4491 deg
</pre>
<p> Mean motion: 15.74267070 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 142
Checksum: 287
</pre>
<p> Coasting Arc #4 (Orbit 142)
</p><hr/>
<p> Vector Time (GMT): 2010/143/16:37:20.369
Vector Time (MET): 008/22:17:11.414
Weight (LBS) : 214609.9
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6530778.40 A = 6731021.85 meter
Y = 1283504.22 meter E = .0010273
Z = 1004763.55 I = 51.63959
XDOT = -1816.531334 Wp = 78.13947
YDOT = -4565.207267 meter/sec RA = 355.74347 deg
ZDOT = -5922.481185 TA = 90.88630
MA = 90.76859
Ha = 191.715 n.mi
Hp = 182.780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21426438.34 X = -6549526.42
Y = 4210971.84 feet Y = 1210368.27 meter
Z = 3296468.35 Z = 972991.12
XDOT = -5959.748470 XDOT = -1736.576600
YDOT = -14977.714129 feet/sec YDOT = -4585.073349 meter/sec
ZDOT = -19430.712550 ZDOT = -5931.112118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16949111.19 X = 5166089.09
Y = 13797480.63 feet Y = 4205472.10 meter
Z = 3169921.96 Z = 966192.21
XDOT = -6773.916181 XDOT = -2064.689652
YDOT = 12834.759957 feet/sec YDOT = 3912.034835 meter/sec
ZDOT = -19465.075909 ZDOT = -5932.955137
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.72623314 .00020000 00000-0 20000-3 0 9033
2 36572 51.6448 356.0868 0009895 353.1826 6.9201 15.74262816 1436
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.72623314 = yrday.fracday
Element set: 903
Inclination: 51.6448 deg
RA of node: 356.0868 deg
Eccentricity: .0009895
Arg of perigee: 353.1826 deg
Mean anomaly: 6.9201 deg
</pre>
<p> Mean motion: 15.74262816 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 143
Checksum: 290
</pre>
<p> Coasting Arc #5 (Orbit 142)
</p><hr/>
<p> Vector Time (GMT): 2010/143/17:05:14.660
Vector Time (MET): 008/22:45:05.705
Weight (LBS) : 214572.6
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 700139.57 A = 6720424.47 meter
Y = -4195947.19 meter E = .0014626
Z = -5212032.88 I = 51.60205
XDOT = 7636.860108 Wp = 56.17821
YDOT = 147.500282 meter/sec RA = 355.64706 deg
ZDOT = 916.950212 TA = 222.51283
MA = 222.62618
Ha = 192.008 n.mi
Hp = 183.434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2297045.83 X = 772326.85
Y = -13766230.94 feet Y = -4187713.84 meter
Z = -17099845.41 Z = -5208456.49
XDOT = 25055.315316 XDOT = 7630.188698
YDOT = 483.924810 feet/sec YDOT = 232.862836 meter/sec
ZDOT = 3008.366838 ZDOT = 954.034419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11180937.01 X = -3407949.60
Y = 8382093.51 feet Y = 2554862.10 meter
Z = -17085590.51 Z = -5207687.99
XDOT = -17289.954435 XDOT = -5269.978112
YDOT = -16695.814231 feet/sec YDOT = -5088.884177 meter/sec
ZDOT = 3156.065122 ZDOT = 961.968649
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10143.72623388 .00020000 00000-0 20000-3 0 9045
2 36572 51.6461 356.0885 0010174 347.2827 12.8079 15.73991511 1436
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10143.72623388 = yrday.fracday
Element set: 904
Inclination: 51.6461 deg
RA of node: 356.0885 deg
Eccentricity: .0010174
Arg of perigee: 347.2827 deg
Mean anomaly: 12.8079 deg
</pre>
<p> Mean motion: 15.73991511 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 143
Checksum: 292
</pre>
<p> Coasting Arc #6 (Orbit 158)
</p><hr/>
<p> Vector Time (GMT): 2010/144/17:05:42.445
Vector Time (MET): 009/22:45:33.490
Weight (LBS) : 214572.6
</p><pre>
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6652890.67 A = 6731684.12 meter
Y = 312400.20 meter E = .0005025
Z = -993422.50 I = 51.60999
XDOT = 652.843751 Wp = 59.85609
YDOT = -4865.915396 meter/sec RA = 350.52454 deg
ZDOT = -5922.016161 TA = 130.99271
MA = 130.94924
Ha = 192.152 n.mi
Hp = 183.156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21827069.13 X = -6651063.57
Y = 1024935.04 feet Y = 238013.92 meter
Z = -3259260.18 Z = -1025738.36
XDOT = 2141.875822 XDOT = 735.975369
YDOT = -15964.289357 feet/sec YDOT = -4858.149563 meter/sec
ZDOT = -19429.186879 ZDOT = -5918.643095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16853228.38 X = 5136864.01
Y = 13877485.60 feet Y = 4229857.61 meter
Z = -3387964.31 Z = -1032651.52
XDOT = -11376.295240 XDOT = -3467.494789
YDOT = 9090.913687 feet/sec YDOT = 2770.910492 meter/sec
ZDOT = -19415.736378 ZDOT = -5917.916448
</pre>
<p> The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
</p><p><strong>TWO LINE MEAN ELEMENT SET</strong>
</p><p><strong>SHUTTLE</strong><br/>
1 36572U 10019A 10144.74207957 .00020000 00000-0 20000-3 0 9059
2 36572 51.6459 350.8711 0010291 350.8750 9.2225 15.74008173 1592
</p><p> Satellite: SHUTTLE<br/>
Catalog Number: 36572
</p><pre>
Epoch time: 10144.74207957 = yrday.fracday
Element set: 905
Inclination: 51.6459 deg
RA of node: 350.8711 deg
Eccentricity: .0010291
Arg of perigee: 350.8750 deg
Mean anomaly: 9.2225 deg
</pre>
<p> Mean motion: 15.74008173 rev/day
Decay rate: 2.00000E-04 rev/day^2
</p><pre>
Epoch rev: 159
Checksum: 282</pre>
<hr/>
<p><strong>SPACE SHUTTLE ORBITAL DATA:</strong>
</p>
<p>The state vectors and 2-Line Elements (TLEs) are obtained from
various sources at different times depending upon availability.
The data normally contains past, current and predicted orbital data.
Careful attention to the orbit # / epoch times!
These sources include:
</p><p>NASA Orbital Flight Dynamics<br/>
DOD C-Band Radar Network<br/>
Goddard Space Flight Center (GSFC)<br/>
NASA Johnson Space Center (JSC)<br/>
DoD/ USSTRATCOM/ US Space Command with permission
</p>
<p>By receiving this email, you agree not to transfer any data or
information received under this agreement, including the analysis
of tracking data, to any other entity without the express approval
of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/
US Space Command.
</p><pre>
David Cottle
Director Of Engineering
IDB Communications</pre>
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