Date: January 26th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6565 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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


032/20:36:28 062 -2 1 6 4 6 4
N/A 4 8 -0 1 191 5
000/00:08:52 124 3 6 -0 0 176 2

Coasting Arc #1 (Orbit 2808)
---------------------------------------

Vector Time (GMT): 2007/024/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5071727
14                 A    =         6715075
52  meter
 Y    =        1557297
79  meter          E    =           
0032578
 Z    =        4103775
40                 I    =           51
88931
 XDOT =       1072
799068                 Wp   =          120
54101
 YDOT =      -6625
194545  meter/sec      RA   =          125
57662  deg
 ZDOT =       3801
536700                 TA   =          290
50049
                                          MA   =          290
84987
                                          Ha   =            192
815  n
mi
                                          Hp   =            171
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16639524
73                 X    =        -5108699
23
 Y    =        5109244
70  feet           Y    =         1500376
09  meter
 Z    =       13463830
07                 Z    =         4079047
55
 XDOT =       3519
681983                 XDOT =        1128
336293
 YDOT =     -21736
202574  feet/sec       YDOT =       -6612
887471  meter/sec
 ZDOT =      12472
233267                 ZDOT =        3806
883026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14265909
00                 X    =        -4348249
06
 Y    =      -10096844
97  feet           Y    =        -3077518
35  meter
 Z    =       13371254
49                 Z    =         4075558
37
 XDOT =      18569
531135                 XDOT =        5659
993090
 YDOT =      -9526
519842  feet/sec       YDOT =       -2903
683248  meter/sec
 ZDOT =      12491
428051                 ZDOT =        3807
387270


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   07024
56829726  
00020000  00000-0  20000-3 0  9007
2 25544  51
6345 126
1471 0022622 128
2207 232
0999 15
77466206 28091


Satellite: ISS
Catalog Number: 25544
Epoch time:      07024
56829726   =   yrday
fracday
Element set:     900
Inclination:       51
6345  deg
RA of node:       126
1471  deg
Eccentricity:     
0022622     
Arg of perigee:   128
2207  deg
Mean anomaly:     232
0999  deg
Mean motion:   15
77466206  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2809
Checksum:              290


Coasting Arc #2 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2007/025/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1476923
52                 A    =         6719987
24  meter
 Y    =        6138807
90  meter          E    =           
0023488
 Z    =       -2337292
12                 I    =           51
92134
 XDOT =      -5383
024240                 Wp   =          117
54061
 YDOT =        762
296879  meter/sec      RA   =          120
38756  deg
 ZDOT =       5434
491774                 TA   =          216
29041
                                          MA   =          216
44994
                                          Ha   =            192
623  n
mi
                                          Hp   =            171
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4845549
60                 X    =        -1534104
75
 Y    =       20140445
87  feet           Y    =         6121972
50  meter
 Z    =       -7668281
23                 Z    =        -2344605
57
 XDOT =     -17660
840683                 XDOT =       -5417
547758
 YDOT =       2500
974013  feet/sec       YDOT =         701
907647  meter/sec
 ZDOT =      17829
697422                 ZDOT =        5408
257510

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18721396
97                 X    =        -5706281
80
 Y    =        8844027
69  feet           Y    =         2695659
64  meter
 Z    =       -7694928
05                 Z    =        -2345414
07
 XDOT =     -12410
639448                 XDOT =       -3782
762904
 YDOT =     -10931
545515  feet/sec       YDOT =       -3331
935073  meter/sec
 ZDOT =      17731
359996                 ZDOT =        5404
518527


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   07025
51855319  
00020000  00000-0  20000-3 0  9011
2 25544  51
6344 121
2420 0022398 131
4260 228
8834 15
77442595 28248


Satellite: ISS
Catalog Number: 25544
Epoch time:      07025
51855319   =   yrday
fracday
Element set:     901
Inclination:       51
6344  deg
RA of node:       121
2420  deg
Eccentricity:     
0022398     
Arg of perigee:   131
4260  deg
Mean anomaly:     228
8834  deg
Mean motion:   15
77442595  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2824
Checksum:              281


Coasting Arc #3 (Orbit 2839)
---------------------------------------

Vector Time (GMT): 2007/026/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4303832
33                 A    =         6710850
79  meter
 Y    =         358230
26  meter          E    =           
0032456
 Z    =       -5159086
12                 I    =           51
90347
 XDOT =      -2223
473545                 Wp   =          114
47100
 YDOT =       7229
346632  meter/sec      RA   =          115
27639  deg
 ZDOT =      -1372
738275                 TA   =          142
52686
                                          MA   =          142
30015
                                          Ha   =            192
534  n
mi
                                          Hp   =            171
439

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14120184
80                 X    =         4324568
33
 Y    =        1175296
11  feet           Y    =          406474
39  meter
 Z    =      -16926135
58                 Z    =        -5138127
93
 XDOT =      -7294
860712                 XDOT =       -2297
479426
 YDOT =      23718
328846  feet/sec       YDOT =        7204
068816  meter/sec
 ZDOT =      -4503
734498                 ZDOT =       -1383
719077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8171909
49                 X    =         2490798
01
 Y    =       11689247
08  feet           Y    =         3562882
51  meter
 Z    =      -16847445
00                 Z    =        -5135101
24
 XDOT =     -22042
754771                 XDOT =       -6718
631654
 YDOT =       8955
109497  feet/sec       YDOT =        2729
517375  meter/sec
 ZDOT =      -4544
012965                 ZDOT =       -1385
015152


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   07026
53213862  
00020000  00000-0  20000-3 0  9026
2 25544  51
6339 116
0087 0022392 135
4331 224
8639 15
77474383 28407


Satellite: ISS
Catalog Number: 25544
Epoch time:      07026
53213862   =   yrday
fracday
Element set:     902
Inclination:       51
6339  deg
RA of node:       116
0087  deg
Eccentricity:     
0022392     
Arg of perigee:   135
4331  deg
Mean anomaly:     224
8639  deg
Mean motion:   15
77474383  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2840
Checksum:              285


Coasting Arc #4 (Orbit 2855)
---------------------------------------

Vector Time (GMT): 2007/027/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2299335
20                 A    =         6722204
25  meter
 Y    =       -6298342
35  meter          E    =           
0034792
 Z    =          10046
98                 I    =           51
95295
 XDOT =       4478
829272                 Wp   =          137
34876
 YDOT =       1606
103728  meter/sec      RA   =          110
12281  deg
 ZDOT =      -6079
644639                 TA   =           42
54221
                                          MA   =           42
27317
                                          Ha   =            192
427  n
mi
                                          Hp   =            171
392

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7543750
65                 X    =         2369544
46
 Y    =      -20663852
84  feet           Y    =        -6272237
34  meter
 Z    =          32962
54                 Z    =           21386
98
 XDOT =      14694
321760                 XDOT =        4490
070175
 YDOT =       5269
369186  feet/sec       YDOT =        1656
251892  meter/sec
 ZDOT =     -19946
340678                 ZDOT =       -6057
859297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20589087
69                 X    =         6275553
93
 Y    =       -7745189
45  feet           Y    =        -2360733
74  meter
 Z    =          74720
18                 Z    =           22774
71
 XDOT =       5086
819094                 XDOT =        1550
462460
 YDOT =      13161
891905  feet/sec       YDOT =        4011
744653  meter/sec
 ZDOT =     -19864
381274                 ZDOT =       -6054
663412


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   07027
54570423  
00020000  00000-0  20000-3 0  9038
2 25544  51
6336 110
7758 0022471 138
8105 221
4761 15
77516989 28569


Satellite: ISS
Catalog Number: 25544
Epoch time:      07027
54570423   =   yrday
fracday
Element set:     903
Inclination:       51
6336  deg
RA of node:       110
7758  deg
Eccentricity:     
0022471     
Arg of perigee:   138
8105  deg
Mean anomaly:     221
4761  deg
Mean motion:   15
77516989  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2856
Checksum:              299


Coasting Arc #5 (Orbit 2871)
---------------------------------------

Vector Time (GMT): 2007/028/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3522875
58                 A    =         6710392
51  meter
 Y    =       -2437480
25  meter          E    =           
0022749
 Z    =        5147751
14                 I    =           51
92339
 XDOT =       2944
975592                 Wp   =          132
06476
 YDOT =      -7016
124350  meter/sec      RA   =          104
97053  deg
 ZDOT =      -1318
030642                 TA   =          330
39312
                                          MA   =          330
52172
                                          Ha   =            192
245  n
mi
                                          Hp   =            171
554

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11557990
76                 X    =        -3520363
95
 Y    =       -7996982
46  feet           Y    =        -2476861
52  meter
 Z    =       16888947
30                 Z    =         5130643
12
 XDOT =       9661
993413                 XDOT =        3029
614665
 YDOT =     -23018
780676  feet/sec       YDOT =       -6982
718612  meter/sec
 ZDOT =      -4324
247514                 ZDOT =       -1303
519343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1769252
01                 X    =         -539268
01
 Y    =      -14020829
73  feet           Y    =        -4273548
90  meter
 Z    =       16824431
66                 Z    =         5128086
77
 XDOT =      22613
827731                 XDOT =        6892
694693
 YDOT =      -7933
671804  feet/sec       YDOT =       -2418
183166  meter/sec
 ZDOT =      -4270
666393                 ZDOT =       -1301
699116


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   07028
55924697  
00020000  00000-0  20000-3 0  9047
2 25544  51
6344 105
5428 0022202 142
8252 217
4456 15
77600227 28727


Satellite: ISS
Catalog Number: 25544
Epoch time:      07028
55924697   =   yrday
fracday
Element set:     904
Inclination:       51
6344  deg
RA of node:       105
5428  deg
Eccentricity:     
0022202     
Arg of perigee:   142
8252  deg
Mean anomaly:     217
4456  deg
Mean motion:   15
77600227  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2872
Checksum:              286


Coasting Arc #6 (Orbit 2887)
---------------------------------------

Vector Time (GMT): 2007/029/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2787539
44                 A    =         6719776
60  meter
 Y    =        5679796
09  meter          E    =           
0029446
 Z    =        2267023
09                 I    =           51
96064
 XDOT =      -3650
349601                 Wp   =          118
64307
 YDOT =      -4002
724984  meter/sec      RA   =           99
86045  deg
 ZDOT =       5472
814516                 TA   =          266
71569
                                          MA   =          267
05261
                                          Ha   =            192
103  n
mi
                                          Hp   =            171
754

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9145470
60                 X    =        -2861857
10
 Y    =       18634501
62  feet           Y    =         5648208
49  meter
 Z    =        7437739
80                 Z    =         2253301
63
 XDOT =     -11976
212601                 XDOT =       -3631
904632
 YDOT =     -13132
299815  feet/sec       YDOT =       -4043
442705  meter/sec
 ZDOT =      17955
428202                 ZDOT =        5455
125852

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19930757
08                 X    =        -6074894
76
 Y    =        5865340
59  feet           Y    =         1787755
81  meter
 Z    =        7386945
13                 Z    =         2251540
88
 XDOT =       1907
805168                 XDOT =         581
499015
 YDOT =     -16325
661392  feet/sec       YDOT =       -4976
061592  meter/sec
 ZDOT =      17888
532315                 ZDOT =        5452
424650


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   07029
57277327  
00020000  00000-0  20000-3 0  9052
2 25544  51
6340 100
3099 0022268 146
0913 214
1680 15
77591710 28888


Satellite: ISS
Catalog Number: 25544
Epoch time:      07029
57277327   =   yrday
fracday
Element set:     905
Inclination:       51
6340  deg
RA of node:       100
3099  deg
Eccentricity:     
0022268     
Arg of perigee:   146
0913  deg
Mean anomaly:     214
1680  deg
Mean motion:   15
77591710  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2888
Checksum:              292


Coasting Arc #7 (Orbit 2902)
---------------------------------------

Vector Time (GMT): 2007/030/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2874513
29                 A    =         6714492
78  meter
 Y    =        4477838
12  meter          E    =           
0028562
 Z    =       -4126029
14                 I    =           51
94660
 XDOT =      -3449
842568                 Wp   =          139
40128
 YDOT =       5719
443103  meter/sec      RA   =           94
67358  deg
 ZDOT =       3797
144182                 TA   =          169
50357
                                          MA   =          169
44381
                                          Ha   =            191
911  n
mi
                                          Hp   =            171
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9430817
88                 X    =         2844270
79
 Y    =       14691069
95  feet           Y    =         4509813
87  meter
 Z    =      -13536841
02                 Z    =        -4112138
12
 XDOT =     -11318
381127                 XDOT =       -3531
987137
 YDOT =      18764
577108  feet/sec       YDOT =        5680
405351  meter/sec
 ZDOT =      12457
822119                 ZDOT =        3780
186369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4075472
11                 X    =        -1242203
90
 Y    =       17017124
12  feet           Y    =         5186819
43  meter
 Z    =      -13484136
64                 Z    =        -4109964
85
 XDOT =     -20198
583049                 XDOT =       -6156
528113
 YDOT =       5001
197673  feet/sec       YDOT =        1524
365051  meter/sec
 ZDOT =      12394
875665                 ZDOT =        3777
958103


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   07030
52293499  
00020000  00000-0  20000-3 0  9068
2 25544  51
6337  95
4035 0022236 149
2941 210
9530 15
77643840 29037


Satellite: ISS
Catalog Number: 25544
Epoch time:      07030
52293499   =   yrday
fracday
Element set:     906
Inclination:       51
6337  deg
RA of node:        95
4035  deg
Eccentricity:     
0022236     
Arg of perigee:   149
2941  deg
Mean anomaly:     210
9530  deg
Mean motion:   15
77643840  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2903
Checksum:              287


Coasting Arc #8 (Orbit 2918)
---------------------------------------

Vector Time (GMT): 2007/031/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3252974
76                 A    =         6714220
69  meter
 Y    =       -4116059
83  meter          E    =           
0024477
 Z    =       -4193951
85                 I    =           51
94707
 XDOT =       2946
040323                 Wp   =          133
91912
 YDOT =       6074
877067  meter/sec      RA   =           89
58198  deg
 ZDOT =      -3706
868589                 TA   =           98
54435
                                          MA   =           98
26690
                                          Ha   =            191
858  n
mi
                                          Hp   =            172
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10672489
36                 X    =         3319132
18
 Y    =      -13504133
30  feet           Y    =        -4079312
98  meter
 Z    =      -13759684
53                 Z    =        -4177989
06
 XDOT =       9665
486623                 XDOT =        2895
897965
 YDOT =      19930
699038  feet/sec       YDOT =        6107
541296  meter/sec
 ZDOT =     -12161
642352                 ZDOT =       -3692
678431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17162110
23                 X    =         5231011
20
 Y    =       -1832264
59  feet           Y    =         -558474
25  meter
 Z    =      -13700267
98                 Z    =        -4175841
68
 XDOT =      -7486
255497                 XDOT =       -2281
810676
 YDOT =      19674
682539  feet/sec       YDOT =        5996
843238  meter/sec
 ZDOT =     -12107
610969                 ZDOT =       -3690
399823


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   07031
53642207  
00020000  00000-0  20000-3 0  9076
2 25544  51
6341  90
1693 0022172 153
1634 207
0683 15
77638367 29197


Satellite: ISS
Catalog Number: 25544
Epoch time:      07031
53642207   =   yrday
fracday
Element set:     907
Inclination:       51
6341  deg
RA of node:        90
1693  deg
Eccentricity:     
0022172     
Arg of perigee:   153
1634  deg
Mean anomaly:     207
0683  deg
Mean motion:   15
77638367  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2919
Checksum:              285


Coasting Arc #9 (Orbit 2934)
---------------------------------------

Vector Time (GMT): 2007/032/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2288391
87                 A    =         6719626
47  meter
 Y    =       -5908108
31  meter          E    =           
0033164
 Z    =        2173777
79                 I    =           51
96432
 XDOT =       4003
508453                 Wp   =          138
37494
 YDOT =      -3598
519577  meter/sec      RA   =           84
39608  deg
 ZDOT =      -5542
419905                 TA   =           17
29275
                                          MA   =           17
18005
                                          Ha   =            191
577  n
mi
                                          Hp   =            172
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7507847
34                 X    =        -2232715
95
 Y    =      -19383557
44  feet           Y    =        -5933387
22  meter
 Z    =        7131816
88                 Z    =         2162796
01
 XDOT =      13134
870254                 XDOT =        4070
373227
 YDOT =     -11806
166590  feet/sec       YDOT =       -3553
375899  meter/sec
 ZDOT =     -18183
792340                 ZDOT =       -5522
809339

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8170216
38                 X    =         2490281
95
 Y    =      -19129414
98  feet           Y    =        -5830645
69  meter
 Z    =        7089846
93                 Z    =         2160985
34
 XDOT =      16321
836940                 XDOT =        4974
895899
 YDOT =        230
223682  feet/sec       YDOT =          70
172178  meter/sec
 ZDOT =     -18110
611717                 ZDOT =       -5520
114451


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   07032
54988809  
00020000  00000-0  20000-3 0  9080
2 25544  51
6341  84
9359 0021964 156
7489 203
4675 15
77703729 29356


Satellite: ISS
Catalog Number: 25544
Epoch time:      07032
54988809   =   yrday
fracday
Element set:     908
Inclination:       51
6341  deg
RA of node:        84
9359  deg
Eccentricity:     
0021964     
Arg of perigee:   156
7489  deg
Mean anomaly:     203
4675  deg
Mean motion:   15
77703729  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2935
Checksum:              338


Coasting Arc #10 (Orbit 2939)
---------------------------------------

Vector Time (GMT): 2007/032/20:40:54
124
Vector Time (MET): N/A
Weight (LBS)     : 478859
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2668009
57                 A    =         6722590
76  meter
 Y    =        5676337
01  meter          E    =           
0015486
 Z    =       -2448132
03                 I    =           51
96136
 XDOT =      -3711
233929                 Wp   =          146
07775
 YDOT =       4059
598357  meter/sec      RA   =           82
60623  deg
 ZDOT =       5371
862625                 TA   =          186
42763
                                          MA   =          186
44752
                                          Ha   =            191
520  n
mi
                                          Hp   =            176
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8753312
24                 X    =         2616229
85
 Y    =       18623152
90  feet           Y    =         5705882
80  meter
 Z    =       -8031929
24                 Z    =        -2435296
74
 XDOT =     -12175
964333                 XDOT =       -3782
447754
 YDOT =      13318
892248  feet/sec       YDOT =        4017
698798  meter/sec
 ZDOT =      17624
221212                 ZDOT =        5353
661319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19753334
01                 X    =         6020816
21
 Y    =       -5833631
57  feet           Y    =        -1778090
90  meter
 Z    =       -7983027
29                 Z    =        -2433226
72
 XDOT =      10850
611810                 XDOT =        3307
266480
 YDOT =      12732
956952  feet/sec       YDOT =        3881
005279  meter/sec
 ZDOT =      17556
388441                 ZDOT =        5351
187197


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   07032
86659267  
00020000  00000-0  20000-3 0  9099
2 25544  51
6340  83
3009 0017192 164
5110 195
6584 15
76463196 29403


Satellite: ISS
Catalog Number: 25544
Epoch time:      07032
86659267   =   yrday
fracday
Element set:     909
Inclination:       51
6340  deg
RA of node:        83
3009  deg
Eccentricity:     
0017192     
Arg of perigee:   164
5110  deg
Mean anomaly:     195
6584  deg
Mean motion:   15
76463196  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2940
Checksum:              304


Coasting Arc #11 (Orbit 2955)
---------------------------------------

Vector Time (GMT): 2007/033/20:40:54
124
Vector Time (MET): N/A
Weight (LBS)     : 478859
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3393563
67                 A    =         6714130
27  meter
 Y    =       -2893966
60  meter          E    =           
0021267
 Z    =       -5028994
67                 I    =           51
92881
 XDOT =       3030
645483                 Wp   =          129
45274
 YDOT =       6815
757747  meter/sec      RA   =           77
50925  deg
 ZDOT =      -1895
580789                 TA   =          122
41848
                                          MA   =          122
21258
                                          Ha   =            191
381  n
mi
                                          Hp   =            176
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11133739
06                 X    =         3450101
31
 Y    =       -9494641
07  feet           Y    =        -2855701
61  meter
 Z    =      -16499326
33                 Z    =        -5012372
05
 XDOT =       9943
062608                 XDOT =        2963
413545
 YDOT =      22361
409931  feet/sec       YDOT =        6849
272258  meter/sec
 ZDOT =      -6219
097078                 ZDOT =       -1881
021515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7872867
59                 X    =        -2399650
04
 Y    =      -12416525
83  feet           Y    =        -3784557
07  meter
 Z    =      -16437273
68                 Z    =        -5010081
02
 XDOT =      22608
945384                 XDOT =        6891
206553
 YDOT =      -6256
636323  feet/sec       YDOT =       -1907
022751  meter/sec
 ZDOT =      -6163
574600                 ZDOT =       -1878
657538


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   07033
88082752  
00020000  00000-0  20000-3 0  9103
2 25544  51
6346  78
0719 0017122 168
1029 192
0543 15
76502918 29569


Satellite: ISS
Catalog Number: 25544
Epoch time:      07033
88082752   =   yrday
fracday
Element set:     910
Inclination:       51
6346  deg
RA of node:        78
0719  deg
Eccentricity:     
0017122     
Arg of perigee:   168
1029  deg
Mean anomaly:     192
0543  deg
Mean motion:   15
76502918  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2956
Checksum:              294


Coasting Arc #12 (Orbit 2971)
---------------------------------------

Vector Time (GMT): 2007/034/20:40:54
124
Vector Time (MET): N/A
Weight (LBS)     : 478859
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2627009
49                 A    =         6724832
92  meter
 Y    =       -6114784
48  meter          E    =           
0028389
 Z    =         830167
93                 I    =           51
95708
 XDOT =       4106
356144                 Wp   =          151
88998
 YDOT =      -2586
993617  meter/sec      RA   =           72
35230  deg
 ZDOT =      -6003
105597                 TA   =           19
06726
                                          MA   =           18
96120
                                          Ha   =            191
274  n
mi
                                          Hp   =            176
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8618797
55                 X    =        -2562470
54
 Y    =      -20061628
86  feet           Y    =        -6143800
31  meter
 Z    =        2723648
07                 Z    =          817563
05
 XDOT =      13472
297062                 XDOT =        4164
140156
 YDOT =      -8487
511868  feet/sec       YDOT =       -2540
750927  meter/sec
 ZDOT =     -19695
228337                 ZDOT =       -5983
017221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20949519
57                 X    =        -6385413
57
 Y    =        6174945
33  feet           Y    =         1882123
34  meter
 Z    =        2675548
98                 Z    =          815507
33
 XDOT =      -6353
521488                 XDOT =       -1936
553349
 YDOT =     -12970
670666  feet/sec       YDOT =       -3953
460419  meter/sec
 ZDOT =     -19620
122645                 ZDOT =       -5980
213382


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   07034
89504557  
00020000  00000-0  20000-3 0  9118
2 25544  51
6345  72
8432 0017195 172
0897 188
0547 15
76488225 29720


Satellite: ISS
Catalog Number: 25544
Epoch time:      07034
89504557   =   yrday
fracday
Element set:     911
Inclination:       51
6345  deg
RA of node:        72
8432  deg
Eccentricity:     
0017195     
Arg of perigee:   172
0897  deg
Mean anomaly:     188
0547  deg
Mean motion:   15
76488225  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2972
Checksum:              320


Coasting Arc #13 (Orbit 2987)
---------------------------------------

Vector Time (GMT): 2007/035/20:40:54
124
Vector Time (MET): N/A
Weight (LBS)     : 478859
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3815715
02                 A    =         6712758
98  meter
 Y    =        1605862
22  meter          E    =           
0017320
 Z    =        5281151
74                 I    =           51
90732
 XDOT =      -2978
901049                 Wp   =          168
19875
 YDOT =      -7109
709539  meter/sec      RA   =           67
22585  deg
 ZDOT =         -7
025039                 TA   =          281
77048
                                          MA   =          281
96473
                                          Ha   =            191
005  n
mi
                                          Hp   =            176
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12518750
07                 X    =        -3859042
57
 Y    =        5268576
83  feet           Y    =         1562950
56  meter
 Z    =       17326613
33                 Z    =         5262510
27
 XDOT =      -9773
297405                 XDOT =       -2899
143744
 YDOT =     -23325
818696  feet/sec       YDOT =       -7142
575326  meter/sec
 ZDOT =        -23
048028                 ZDOT =         -21
302330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3949161
96                 X    =         1203704
57
 Y    =       13087968
42  feet           Y    =         3989212
78  meter
 Z    =       17256817
11                 Z    =         5259877
86
 XDOT =     -23249
466955                 XDOT =       -7086
437528
 YDOT =       7045
439120  feet/sec       YDOT =        2147
449844  meter/sec
 ZDOT =        -77
553043                 ZDOT =         -23
638167


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   07035
90924296  
00020000  00000-0  20000-3 0  9128
2 25544  51
6345  67
6144 0017032 176
3901 183
7389 15
76577572 29882


Satellite: ISS
Catalog Number: 25544
Epoch time:      07035
90924296   =   yrday
fracday
Element set:     912
Inclination:       51
6345  deg
RA of node:        67
6144  deg
Eccentricity:     
0017032     
Arg of perigee:   176
3901  deg
Mean anomaly:     183
7389  deg
Mean motion:   15
76577572  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2988
Checksum:              322

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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