Date: October 2nd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


276/11:35:20 275 -0 2 2 2 2 2
N/A 1 5 -0 1 195 0
000/00:04:40 551 -1 7 -0 1 186 2

Coasting Arc #1 (Orbit 526)
---------------------------------------

Vector Time (GMT): 2008/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6131363
95                 A    =         6735950
00  meter
 Y    =       -2330551
17  meter          E    =           
0013243
 Z    =        1519028
54                 I    =           51
59911
 XDOT =       3002
496498                 Wp   =           87
11303
 YDOT =      -4108
198254  meter/sec      RA   =          190
23503  deg
 ZDOT =       5773
705237                 TA   =          289
61839
                                          MA   =          289
76129
                                          Ha   =            193
894  n
mi
                                          Hp   =            185
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20116023
46                 X    =        -6112226
98
 Y    =       -7646165
25  feet           Y    =        -2399008
52  meter
 Z    =        4983689
43                 Z    =         1489288
37
 XDOT =       9850
710296                 XDOT =        3020
163654
 YDOT =     -13478
340729  feet/sec       YDOT =       -4074
523446  meter/sec
 ZDOT =      18942
602482                 ZDOT =        5788
334862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21154381
50                 X    =         6447855
48
 Y    =        4092252
23  feet           Y    =         1247318
48  meter
 Z    =        4868369
18                 Z    =         1483878
92
 XDOT =      -6997
716194                 XDOT =       -2132
903896
 YDOT =      13401
874005  feet/sec       YDOT =        4084
891197  meter/sec
 ZDOT =      18998
776519                 ZDOT =        5790
827083


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08275
56067464  
00020000  00000-0  20000-3 0  9009
2 25544  51
6413 190
9185 0005976 171
8792 188
2468 15
72342544  5275


Satellite: ISS
Catalog Number: 25544
Epoch time:      08275
56067464   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:       190
9185  deg
Eccentricity:     
0005976     
Arg of perigee:   171
8792  deg
Mean anomaly:     188
2468  deg
Mean motion:   15
72342544  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             527
Checksum:              316


Coasting Arc #2 (Orbit 541)
---------------------------------------

Vector Time (GMT): 2008/276/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6428231
44                 A    =         6737440
94  meter
 Y    =        1561088
06  meter          E    =           
0016302
 Z    =       -1229753
66                 I    =           51
62902
 XDOT =      -2201
574909                 Wp   =          158
77067
 YDOT =       4469
631095  meter/sec      RA   =          185
18581  deg
 ZDOT =      -5873
361288                 TA   =           34
71035
                                          MA   =           34
60408
                                          Ha   =            194
967  n
mi
                                          Hp   =            186
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21089998
15                 X    =         6416271
39
 Y    =        5121679
99  feet           Y    =         1632905
33  meter
 Z    =       -4034624
88                 Z    =        -1198553
74
 XDOT =      -7223
014792                 XDOT =       -2222
859046
 YDOT =      14664
144014  feet/sec       YDOT =        4444
892536  meter/sec
 ZDOT =     -19269
558031                 ZDOT =       -5884
108686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21491517
26                 X    =        -6550614
46
 Y    =       -3177299
70  feet           Y    =         -968440
95  meter
 Z    =       -3913729
47                 Z    =        -1192904
74
 XDOT =       5515
530890                 XDOT =        1681
133815
 YDOT =     -13683
782045  feet/sec       YDOT =       -4170
816767  meter/sec
 ZDOT =     -19310
678965                 ZDOT =       -5885
894948


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08276
51401835  
00020000  00000-0  20000-3 0  9010
2 25544  51
6414 186
0346 0007817 177
4923 182
6279 15
71936842  5429


Satellite: ISS
Catalog Number: 25544
Epoch time:      08276
51401835   =   yrday
fracday
Element set:     901
Inclination:       51
6414  deg
RA of node:       186
0346  deg
Eccentricity:     
0007817     
Arg of perigee:   177
4923  deg
Mean anomaly:     182
6279  deg
Mean motion:   15
71936842  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             542
Checksum:              301


Coasting Arc #3 (Orbit 557)
---------------------------------------

Vector Time (GMT): 2008/277/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         727160
64                 A    =         6725877
11  meter
 Y    =       -4149858
43  meter          E    =           
0006904
 Z    =        5240274
07                 I    =           51
61961
 XDOT =       7654
895157                 Wp   =          160
73703
 YDOT =        523
995716  meter/sec      RA   =          180
04839  deg
 ZDOT =       -653
419907                 TA   =          295
44138
                                          MA   =          295
51280
                                          Ha   =            194
645  n
mi
                                          Hp   =            186
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2385697
64                 X    =          748054
12
 Y    =      -13615021
08  feet           Y    =        -4141609
93  meter
 Z    =       17192500
23                 Z    =         5243857
56
 XDOT =      25114
485423                 XDOT =        7651
641084
 YDOT =       1719
146051  feet/sec       YDOT =         609
578960  meter/sec
 ZDOT =      -2143
766098                 ZDOT =        -616
239535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -800542
98                 X    =         -244005
50
 Y    =       13782498
20  feet           Y    =         4200905
45  meter
 Z    =       17205937
66                 Z    =         5244369
80
 XDOT =     -24159
817146                 XDOT =       -7363
912266
 YDOT =       1068
060342  feet/sec       YDOT =         325
544792  meter/sec
 ZDOT =      -1999
824280                 ZDOT =        -609
546440


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08277
53116394  
00020000  00000-0  20000-3 0  9027
2 25544  51
6408 180
8273 0007719 182
3335 177
7793 15
72016134  5583


Satellite: ISS
Catalog Number: 25544
Epoch time:      08277
53116394   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:       180
8273  deg
Eccentricity:     
0007719     
Arg of perigee:   182
3335  deg
Mean anomaly:     177
7793  deg
Mean motion:   15
72016134  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             558
Checksum:              302


Coasting Arc #4 (Orbit 572)
---------------------------------------

Vector Time (GMT): 2008/278/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6704756
20                 A    =         6737866
20  meter
 Y    =         657001
26  meter          E    =           
0007724
 Z    =         -78849
70                 I    =           51
68926
 XDOT =       -529
488251                 Wp   =           83
28262
 YDOT =      -4739
786694  meter/sec      RA   =          174
93326  deg
 ZDOT =       6035
044304                 TA   =          275
86276
                                          MA   =          275
95081
                                          Ha   =            194
551  n
mi
                                          Hp   =            186
550

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21997231
62                 X    =        -6711221
53
 Y    =        2155515
96  feet           Y    =          581988
66  meter
 Z    =        -258693
24                 Z    =         -111437
77
 XDOT =      -1737
166177                 XDOT =        -505
765579
 YDOT =     -15550
481280  feet/sec       YDOT =       -4745
575020  meter/sec
 ZDOT =      19800
014120                 ZDOT =        6032
529683

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21552020
12                 X    =         6569055
73
 Y    =       -4894258
17  feet           Y    =        -1491769
89  meter
 Z    =        -384753
89                 Z    =         -117272
98
 XDOT =       3427
384293                 XDOT =        1044
666733
 YDOT =      13624
424091  feet/sec       YDOT =        4152
724463  meter/sec
 ZDOT =      19789
793153                 ZDOT =        6031
928953


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08278
48472501  
00020000  00000-0  20000-3 0  9038
2 25544  51
6409 175
9446 0007670 185
4376 174
6704 15
71997818  5737


Satellite: ISS
Catalog Number: 25544
Epoch time:      08278
48472501   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       175
9446  deg
Eccentricity:     
0007670     
Arg of perigee:   185
4376  deg
Mean anomaly:     174
6704  deg
Mean motion:   15
71997818  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             573
Checksum:              327


Coasting Arc #5 (Orbit 588)
---------------------------------------

Vector Time (GMT): 2008/279/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1607851
33                 A    =         6725900
30  meter
 Y    =        3916539
77  meter          E    =           
0014579
 Z    =       -5236921
96                 I    =           51
67894
 XDOT =      -7388
521301                 Wp   =          114
23095
 YDOT =       1970
518574  meter/sec      RA   =          169
82378  deg
 ZDOT =       -802
359180                 TA   =          148
16945
                                          MA   =          148
08125
                                          Ha   =            194
354  n
mi
                                          Hp   =            186
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5275102
78                 X    =         1589376
91
 Y    =       12849539
93  feet           Y    =         3934416
38  meter
 Z    =      -17181502
48                 Z    =        -5229155
77
 XDOT =     -24240
555450                 XDOT =       -7406
109039
 YDOT =       6464
955950  feet/sec       YDOT =        1887
797523  meter/sec
 ZDOT =      -2632
412007                 ZDOT =        -838
295969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7147688
10                 X    =        -2178615
33
 Y    =      -11953819
63  feet           Y    =        -3643524
22  meter
 Z    =      -17151039
75                 Z    =        -5227636
92
 XDOT =      22186
561622                 XDOT =        6762
463982
 YDOT =      -9325
954274  feet/sec       YDOT =       -2842
550863  meter/sec
 ZDOT =      -2771
314718                 ZDOT =        -844
696726


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08279
50183864  
00020000  00000-0  20000-3 0  9044
2 25544  51
6414 170
7363 0007652 189
3699 170
7322 15
72049899  5893


Satellite: ISS
Catalog Number: 25544
Epoch time:      08279
50183864   =   yrday
fracday
Element set:     904
Inclination:       51
6414  deg
RA of node:       170
7363  deg
Eccentricity:     
0007652     
Arg of perigee:   189
3699  deg
Mean anomaly:     170
7322  deg
Mean motion:   15
72049899  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             589
Checksum:              329


Coasting Arc #6 (Orbit 604)
---------------------------------------

Vector Time (GMT): 2008/280/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6006287
92                 A    =         6737015
79  meter
 Y    =       -2723523
45  meter          E    =           
0017868
 Z    =        1320037
52                 I    =           51
74464
 XDOT =       3081
417626                 Wp   =          144
99965
 YDOT =       3944
746769  meter/sec      RA   =          164
68888  deg
 ZDOT =      -5857
301957                 TA   =           20
52648
                                          MA   =           20
45477
                                          Ha   =            194
277  n
mi
                                          Hp   =            186
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19705669
04                 X    =         6029883
80
 Y    =       -8935444
38  feet           Y    =        -2656225
74  meter
 Z    =        4330831
75                 Z    =         1349273
81
 XDOT =      10109
637881                 XDOT =        3065
531941
 YDOT =      12942
082576  feet/sec       YDOT =        3979
116128  meter/sec
 ZDOT =     -19216
869937                 ZDOT =       -5842
370806

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18005322
23                 X    =        -5488022
22
 Y    =       11957142
41  feet           Y    =         3644537
01  meter
 Z    =        4443734
80                 Z    =         1354450
37
 XDOT =     -11279
280387                 XDOT =       -3437
924662
 YDOT =      -9835
306707  feet/sec       YDOT =       -2997
801484  meter/sec
 ZDOT =     -19158
664947                 ZDOT =       -5839
561076


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08280
51893664  
00020000  00000-0  20000-3 0  9054
2 25544  51
6412 165
5284 0007775 193
1253 166
9708 15
72025092  6053


Satellite: ISS
Catalog Number: 25544
Epoch time:      08280
51893664   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:       165
5284  deg
Eccentricity:     
0007775     
Arg of perigee:   193
1253  deg
Mean anomaly:     166
9708  deg
Mean motion:   15
72025092  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             605
Checksum:              299


Coasting Arc #7 (Orbit 620)
---------------------------------------

Vector Time (GMT): 2008/281/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3652174
31                 A    =         6727237
10  meter
 Y    =       -2780595
97  meter          E    =           
0011215
 Z    =        4918815
81                 I    =           51
74046
 XDOT =       6115
949517                 Wp   =          163
82469
 YDOT =      -4123
384724  meter/sec      RA   =          159
60557  deg
 ZDOT =       2198
335749                 TA   =          264
78083
                                          MA   =          264
90882
                                          Ha   =            194
092  n
mi
                                          Hp   =            187
010

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11982199
18                 X    =        -3644704
80
 Y    =       -9122690
18  feet           Y    =        -2821394
89  meter
 Z    =       16137847
14                 Z    =         4901091
50
 XDOT =      20065
451172                 XDOT =        6150
924073
 YDOT =     -13528
165106  feet/sec       YDOT =       -4054
797078  meter/sec
 ZDOT =       7212
387628                 ZDOT =        2228
132367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13493667
41                 X    =         4112869
83
 Y    =        6851040
79  feet           Y    =         2088197
23  meter
 Z    =       16068940
96                 Z    =         4897813
20
 XDOT =     -16825
595043                 XDOT =       -5128
441369
 YDOT =      15862
404351  feet/sec       YDOT =        4834
860846  meter/sec
 ZDOT =       7327
330405                 ZDOT =        2233
370307


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08281
53601553  
00020000  00000-0  20000-3 0  9062
2 25544  51
6416 160
3200 0007608 197
8283 162
2613 15
72081536  6214


Satellite: ISS
Catalog Number: 25544
Epoch time:      08281
53601553   =   yrday
fracday
Element set:     906
Inclination:       51
6416  deg
RA of node:       160
3200  deg
Eccentricity:     
0007608     
Arg of perigee:   197
8283  deg
Mean anomaly:     162
2613  deg
Mean motion:   15
72081536  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             621
Checksum:              268


Coasting Arc #8 (Orbit 635)
---------------------------------------

Vector Time (GMT): 2008/282/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4527354
73                 A    =         6734822
90  meter
 Y    =        4328597
15  meter          E    =           
0003711
 Z    =       -2481361
99                 I    =           51
79370
 XDOT =      -5064
415026                 Wp   =          163
37776
 YDOT =      -2236
132141  meter/sec      RA   =          154
45407  deg
 ZDOT =       5337
919373                 TA   =          168
67194
                                          MA   =          168
66359
                                          Ha   =            193
777  n
mi
                                          Hp   =            187
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14853526
02                 X    =        -4563367
19
 Y    =       14201434
21  feet           Y    =         4277768
25  meter
 Z    =       -8140951
40                 Z    =        -2503443
65
 XDOT =     -16615
534861                 XDOT =       -5064
964738
 YDOT =      -7336
391539  feet/sec       YDOT =       -2292
768324  meter/sec
 ZDOT =      17512
858835                 ZDOT =        5313
314912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11783893
60                 X    =         3591730
77
 Y    =      -16794511
97  feet           Y    =        -5118967
25  meter
 Z    =       -8226012
28                 Z    =        -2507288
54
 XDOT =      16593
425561                 XDOT =        5057
676111
 YDOT =       3109
293896  feet/sec       YDOT =         947
712779  meter/sec
 ZDOT =      17417
360666                 ZDOT =        5308
811531


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08282
48951181  
00020000  00000-0  20000-3 0  9073
2 25544  51
6417 155
4368 0007571 202
8740 157
2086 15
72113053  6363


Satellite: ISS
Catalog Number: 25544
Epoch time:      08282
48951181   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:       155
4368  deg
Eccentricity:     
0007571     
Arg of perigee:   202
8740  deg
Mean anomaly:     157
2086  deg
Mean motion:   15
72113053  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             636
Checksum:              288


Coasting Arc #9 (Orbit 651)
---------------------------------------

Vector Time (GMT): 2008/283/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5022712
22                 A    =         6729344
47  meter
 Y    =        1017661
74  meter          E    =           
0005962
 Z    =       -4363213
98                 I    =           51
80083
 XDOT =      -4090
105755                 Wp   =          127
38418
 YDOT =       5547
824947  meter/sec      RA   =          149
38953  deg
 ZDOT =      -3421
091435                 TA   =          108
19482
                                          MA   =          108
12991
                                          Ha   =            193
664  n
mi
                                          Hp   =            187
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16478714
62                 X    =         5032155
15
 Y    =        3338785
23  feet           Y    =         1073881
24  meter
 Z    =      -14315006
49                 Z    =        -4338790
52
 XDOT =     -13418
982137                 XDOT =       -4135
219250
 YDOT =      18201
525416  feet/sec       YDOT =        5501
834652  meter/sec
 ZDOT =     -11224
053265                 ZDOT =       -3441
071135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16892346
26                 X    =        -5148787
14
 Y    =         214312
09  feet           Y    =           65322
33  meter
 Z    =      -14220324
93                 Z    =        -4334355
04
 XDOT =       9248
869878                 XDOT =        2819
055539
 YDOT =     -19368
720808  feet/sec       YDOT =       -5903
586102  meter/sec
 ZDOT =     -11300
857519                 ZDOT =       -3444
501372


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08283
50655823  
00020000  00000-0  20000-3 0  9082
2 25544  51
6415 150
2283 0007618 207
9704 152
1050 15
72132828  6522


Satellite: ISS
Catalog Number: 25544
Epoch time:      08283
50655823   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:       150
2283  deg
Eccentricity:     
0007618     
Arg of perigee:   207
9704  deg
Mean anomaly:     152
1050  deg
Mean motion:   15
72132828  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             652
Checksum:              276


Coasting Arc #10 (Orbit 667)
---------------------------------------

Vector Time (GMT): 2008/284/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2526418
43                 A    =         6732052
08  meter
 Y    =       -5178949
91  meter          E    =           
0010283
 Z    =        3467783
03                 I    =           51
83561
 XDOT =       6199
505267                 Wp   =          125
78848
 YDOT =        -38
686644  meter/sec      RA   =          144
23134  deg
 ZDOT =      -4570
851688                 TA   =           13
22977
                                          MA   =           13
20283
                                          Ha   =            193
282  n
mi
                                          Hp   =            187
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8288774
38                 X    =         2567296
49
 Y    =      -16991305
47  feet           Y    =        -5150469
27  meter
 Z    =       11377240
90                 Z    =         3480156
08
 XDOT =      20339
584209                 XDOT =        6221
681696
 YDOT =       -126
924685  feet/sec       YDOT =          30
763533  meter/sec
 ZDOT =     -14996
232573                 ZDOT =       -4540
680329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4154791
75                 X    =        -1266380
52
 Y    =       18413728
20  feet           Y    =         5612504
36  meter
 Z    =       11424630
07                 Z    =         3482227
24
 XDOT =     -18521
225841                 XDOT =       -5645
269636
 YDOT =       5059
855380  feet/sec       YDOT =        1542
243920  meter/sec
 ZDOT =     -14879
391883                 ZDOT =       -4535
238646


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08284
52358763  
00020000  00000-0  20000-3 0  9099
2 25544  51
6417 145
0200 0007470 211
9434 148
1276 15
72195203  6684


Satellite: ISS
Catalog Number: 25544
Epoch time:      08284
52358763   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:       145
0200  deg
Eccentricity:     
0007470     
Arg of perigee:   211
9434  deg
Mean anomaly:     148
1276  deg
Mean motion:   15
72195203  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             668
Checksum:              285


Coasting Arc #11 (Orbit 683)
---------------------------------------

Vector Time (GMT): 2008/285/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5591108
06                 A    =         6731940
53  meter
 Y    =        1115910
45  meter          E    =           
0010223
 Z    =        3579191
95                 I    =           51
85684
 XDOT =       1653
569095                 Wp   =          130
94703
 YDOT =      -6052
300723  meter/sec      RA   =          139
17465  deg
 ZDOT =       4455
244883                 TA   =          271
58829
                                          MA   =          271
70538
                                          Ha   =            193
200  n
mi
                                          Hp   =            187
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18343530
39                 X    =        -5620558
10
 Y    =        3661123
52  feet           Y    =         1053223
06  meter
 Z    =       11742755
76                 Z    =         3551958
39
 XDOT =       5425
095455                 XDOT =        1699
480953
 YDOT =     -19856
629667  feet/sec       YDOT =       -6033
552507  meter/sec
 ZDOT =      14616
945154                 ZDOT =        4463
390011

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16964434
33                 X    =         5170759
58
 Y    =       -8034937
69  feet           Y    =        -2449049
01  meter
 Z    =       11637396
16                 Z    =         3547078
35
 XDOT =       -930
073700                 XDOT =        -283
486464
 YDOT =      19322
452815  feet/sec       YDOT =        5889
483618  meter/sec
 ZDOT =      14647
874479                 ZDOT =        4464
672141


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08285
54060125  
00020000  00000-0  20000-3 0  9106
2 25544  51
6408 139
8104 0007470 216
3554 143
7102 15
72170248  6849


Satellite: ISS
Catalog Number: 25544
Epoch time:      08285
54060125   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:       139
8104  deg
Eccentricity:     
0007470     
Arg of perigee:   216
3554  deg
Mean anomaly:     143
7102  deg
Mean motion:   15
72170248  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             684
Checksum:              267


Coasting Arc #12 (Orbit 698)
---------------------------------------

Vector Time (GMT): 2008/286/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -367940
11                 A    =         6729347
13  meter
 Y    =        5198780
98  meter          E    =           
0009298
 Z    =       -4265043
49                 I    =           51
86924
 XDOT =      -6328
071238                 Wp   =          161
13399
 YDOT =       2498
778383  meter/sec      RA   =          134
01747  deg
 ZDOT =       3585
304361                 TA   =          145
24372
                                          MA   =          145
18295
                                          Ha   =            192
948  n
mi
                                          Hp   =            187
933

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1207152
60                 X    =         -405327
20
 Y    =       17056368
03  feet           Y    =         5194457
04  meter
 Z    =      -13992924
85                 Z    =        -4266922
25
 XDOT =     -20761
388577                 XDOT =       -6372
959727
 YDOT =       8198
091807  feet/sec       YDOT =        2427
763568  meter/sec
 ZDOT =      11762
809582                 ZDOT =        3554
452804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3350033
96                 X    =        -1021090
35
 Y    =      -16762017
44  feet           Y    =        -5109062
92  meter
 Z    =      -13999674
91                 Z    =        -4267100
91
 XDOT =      16755
511475                 XDOT =        5107
079898
 YDOT =     -13091
114376  feet/sec       YDOT =       -3990
171662  meter/sec
 ZDOT =      11643
572540                 ZDOT =        3548
960910


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08286
49403358  
00020000  00000-0  20000-3 0  9111
2 25544  51
6398 134
9263 0007608 220
2717 139
7882 15
72224204  6995


Satellite: ISS
Catalog Number: 25544
Epoch time:      08286
49403358   =   yrday
fracday
Element set:     911
Inclination:       51
6398  deg
RA of node:       134
9263  deg
Eccentricity:     
0007608     
Arg of perigee:   220
2717  deg
Mean anomaly:     139
7882  deg
Mean motion:   15
72224204  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             699
Checksum:              308


Coasting Arc #13 (Orbit 713)
---------------------------------------

Vector Time (GMT): 2008/287/11:37:40
551
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5280508
81                 A    =         6734218
62  meter
 Y    =       -3209516
21  meter          E    =           
0008505
 Z    =       -2663244
44                 I    =           51
90400
 XDOT =        759
724430                 Wp   =          189
32255
 YDOT =       5591
761680  meter/sec      RA   =          128
96023  deg
 ZDOT =      -5238
274526                 TA   =           20
87140
                                          MA   =           20
83670
                                          Ha   =            192
880  n
mi
                                          Hp   =            188
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17324503
95                 X    =         5328943
53
 Y    =      -10529908
84  feet           Y    =        -3150195
93  meter
 Z    =       -8737678
62                 Z    =        -2637473
21
 XDOT =       2492
534218                 XDOT =         722
587164
 YDOT =      18345
674803  feet/sec       YDOT =        5600
049251  meter/sec
 ZDOT =     -17185
940046                 ZDOT =       -5234
674401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13781153
03                 X    =        -4200495
44
 Y    =       14927358
96  feet           Y    =         4549859
01  meter
 Z    =       -8638183
87                 Z    =        -2632918
44
 XDOT =      -6478
880012                 XDOT =       -1974
762628
 YDOT =     -15906
872402  feet/sec       YDOT =       -4848
414708  meter/sec
 ZDOT =     -17171
435126                 ZDOT =       -5233
853426


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08287
51101245  
00020000  00000-0  20000-3 0  9126
2 25544  51
6389 129
7177 0007655 224
6522 135
4025 15
72226715  7144


Satellite: ISS
Catalog Number: 25544
Epoch time:      08287
51101245   =   yrday
fracday
Element set:     912
Inclination:       51
6389  deg
RA of node:       129
7177  deg
Eccentricity:     
0007655     
Arg of perigee:   224
6522  deg
Mean anomaly:     135
4025  deg
Mean motion:   15
72226715  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             714
Checksum:              282

INTERNATIONAL SPACE STATION ORBITAL DATA:

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:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

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

   David Cottle
   Director Of Engineering
   IDB Communications

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