Date: August 13th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6200 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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


233/15:32:27 000 0 0 0 0 0 0
012/16:55:45 047 0 0 0 0 184 6
000/00:00:00 000 0 0 0 0 184 3

Coasting Arc #1 (Orbit 1952)
---------------------------------------

Vector Time (GMT): 2007/223/15:32:27
000
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3602234
20                 A    =         6717608
88  meter
 Y    =        3660045
04  meter          E    =           
0008524
 Z    =       -4337081
58                 I    =           51
64538
 XDOT =      -6491
296115                 Wp   =          167
87229
 YDOT =      -2318
367245  meter/sec      RA   =          176
47947  deg
 ZDOT =       3428
021189                 TA   =          136
76154
                                          MA   =          136
69460
                                          Ha   =            186
445  n
mi
                                          Hp   =            182
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11818353
66                 X    =        -3621825
40
 Y    =       12008021
79  feet           Y    =         3619653
66  meter
 Z    =      -14229270
28                 Z    =        -4354628
08
 XDOT =     -21296
903265                 XDOT =       -6481
541638
 YDOT =      -7606
191749  feet/sec       YDOT =       -2390
902325  meter/sec
 ZDOT =      11246
788678                 ZDOT =        3396
510751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8961791
51                 X    =         2731554
05
 Y    =      -14200998
40  feet           Y    =        -4328464
31  meter
 Z    =      -14295318
84                 Z    =        -4357213
18
 XDOT =      21443
715372                 XDOT =        6536
044445
 YDOT =       2308
574627  feet/sec       YDOT =         703
653546  meter/sec
 ZDOT =      11127
042417                 ZDOT =        3391
522529


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   07223
65737267  
00020000  00000-0  20000-3 0  9006
2 25544  51
6335 177
4451 0008378 232
4419 127
5985 15
76215856 19536


Satellite: ISS
Catalog Number: 25544
Epoch time:      07223
65737267   =   yrday
fracday
Element set:     900
Inclination:       51
6335  deg
RA of node:       177
4451  deg
Eccentricity:     
0008378     
Arg of perigee:   232
4419  deg
Mean anomaly:     127
5985  deg
Mean motion:   15
76215856  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1953
Checksum:              314


Coasting Arc #2 (Orbit 1968)
---------------------------------------

Vector Time (GMT): 2007/224/15:37:05
805
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3749894
87                 A    =         6716577
63  meter
 Y    =        3122332
40  meter          E    =           
0003059
 Z    =       -4617371
59                 I    =           51
67155
 XDOT =      -6324
702225                 Wp   =          109
42161
 YDOT =       3291
006242  meter/sec      RA   =          171
35867  deg
 ZDOT =      -2913
597033                 TA   =          131
76081
                                          MA   =          131
73466
                                          Ha   =            186
281  n
mi
                                          Hp   =            182
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12302804
68                 X    =         3737131
58
 Y    =       10243872
72  feet           Y    =         3164194
74  meter
 Z    =      -15148856
93                 Z    =        -4599185
88
 XDOT =     -20750
335384                 XDOT =       -6346
879310
 YDOT =      10797
264575  feet/sec       YDOT =        3220
156028  meter/sec
 ZDOT =      -9559
045383                 ZDOT =       -2944
375345

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14527448
77                 X    =        -4427966
39
 Y    =       -6880800
59  feet           Y    =        -2097268
02  meter
 Z    =      -15079509
71                 Z    =        -4596234
56
 XDOT =      16901
392557                 XDOT =        5151
544451
 YDOT =     -14498
646615  feet/sec       YDOT =       -4419
187488  meter/sec
 ZDOT =      -9675
308601                 ZDOT =       -2949
034062


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   07224
67177215  
00020000  00000-0  20000-3 0  9011
2 25544  51
6343 172
2179 0008378 236
8906 123
1455 15
76246452 19691


Satellite: ISS
Catalog Number: 25544
Epoch time:      07224
67177215   =   yrday
fracday
Element set:     901
Inclination:       51
6343  deg
RA of node:       172
2179  deg
Eccentricity:     
0008378     
Arg of perigee:   236
8906  deg
Mean anomaly:     123
1455  deg
Mean motion:   15
76246452  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1969
Checksum:              304


Coasting Arc #3 (Orbit 1984)
---------------------------------------

Vector Time (GMT): 2007/225/15:41:36
106
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6465793
01                 A    =         6725878
53  meter
 Y    =       -1801898
92  meter          E    =           
0013056
 Z    =         258559
95                 I    =           51
73136
 XDOT =       1507
979465                 Wp   =          170
61660
 YDOT =       4539
472636  meter/sec      RA   =          166
16918  deg
 ZDOT =      -6044
571489                 TA   =            6
57319
                                          MA   =            6
55608
                                          Ha   =            186
172  n
mi
                                          Hp   =            182
884

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21213231
66                 X    =         6484205
55
 Y    =       -5911741
85  feet           Y    =        -1729491
83  meter
 Z    =         848293
79                 Z    =          290014
71
 XDOT =       4947
439188                 XDOT =        1486
469091
 YDOT =      14893
282925  feet/sec       YDOT =        4556
215643  meter/sec
 ZDOT =     -19831
271289                 ZDOT =       -6037
297990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18684304
45                 X    =        -5694976
00
 Y    =       11646052
95  feet           Y    =         3549716
94  meter
 Z    =         967320
86                 Z    =          294839
40
 XDOT =      -8199
614931                 XDOT =       -2499
242631
 YDOT =     -11503
035369  feet/sec       YDOT =       -3506
125180  meter/sec
 ZDOT =     -19803
105814                 ZDOT =       -6035
986652


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   07225
68616377  
00020000  00000-0  20000-3 0  9021
2 25544  51
6345 166
9906 0008490 239
6660 120
3665 15
76204916 19853


Satellite: ISS
Catalog Number: 25544
Epoch time:      07225
68616377   =   yrday
fracday
Element set:     902
Inclination:       51
6345  deg
RA of node:       166
9906  deg
Eccentricity:     
0008490     
Arg of perigee:   239
6660  deg
Mean anomaly:     120
3665  deg
Mean motion:   15
76204916  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1985
Checksum:              316


Coasting Arc #4 (Orbit 2000)
---------------------------------------

Vector Time (GMT): 2007/226/15:46:13
272
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1310686
01                 A    =         6715435
37  meter
 Y    =       -4481163
48  meter          E    =           
0001847
 Z    =        4828447
95                 I    =           51
72533
 XDOT =       7293
440940                 Wp   =          272
78895
 YDOT =       -484
622490  meter/sec      RA   =          160
98956  deg
 ZDOT =      -2430
282634                 TA   =          200
90337
                                          MA   =          200
91093
                                          Ha   =            185
734  n
mi
                                          Hp   =            183
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4300150
95                 X    =         1337242
36
 Y    =      -14701979
91  feet           Y    =        -4466358
23  meter
 Z    =       15841364
67                 Z    =         4834879
58
 XDOT =      23928
612007                 XDOT =        7310
123643
 YDOT =      -1589
968800  feet/sec       YDOT =        -402
969809  meter/sec
 ZDOT =      -7973
368223                 ZDOT =       -2394
811274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         672409
26                 X    =          204950
34
 Y    =       15278502
64  feet           Y    =         4656887
60  meter
 Z    =       15865168
41                 Z    =         4835703
33
 XDOT =     -21114
991746                 XDOT =       -6435
849484
 YDOT =       9066
805932  feet/sec       YDOT =        2763
562448  meter/sec
 ZDOT =      -7838
933688                 ZDOT =       -2389
306988


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   07226
70054231  
00020000  00000-0  20000-3 0  9031
2 25544  51
6349 161
7630 0008504 245
8195 114
2081 15
76302108 20018


Satellite: ISS
Catalog Number: 25544
Epoch time:      07226
70054231   =   yrday
fracday
Element set:     903
Inclination:       51
6349  deg
RA of node:       161
7630  deg
Eccentricity:     
0008504     
Arg of perigee:   245
8195  deg
Mean anomaly:     114
2081  deg
Mean motion:   15
76302108  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2001
Checksum:              251


Coasting Arc #5 (Orbit 2016)
---------------------------------------

Vector Time (GMT): 2007/227/15:50:49
977
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5229445
70                 A    =         6718708
80  meter
 Y    =       -1160581
08  meter          E    =           
0005915
 Z    =        4056981
25                 I    =           51
76234
 XDOT =       4159
771655                 Wp   =          153
36255
 YDOT =      -5201
643336  meter/sec      RA   =          155
87216  deg
 ZDOT =       3866
558963                 TA   =          256
87211
                                          MA   =          256
93813
                                          Ha   =            185
602  n
mi
                                          Hp   =            183
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17156974
07                 X    =        -5235787
03
 Y    =       -3807680
72  feet           Y    =        -1219095
16  meter
 Z    =       13310305
94                 Z    =         4031561
58
 XDOT =      13647
544800                 XDOT =        4198
845277
 YDOT =     -17065
758976  feet/sec       YDOT =       -5154
907963  meter/sec
 ZDOT =      12685
560901                 ZDOT =        3886
861723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17467388
39                 X    =         5324059
98
 Y    =       -2512206
38  feet           Y    =         -765720
51  meter
 Z    =       13213765
47                 Z    =         4027555
71
 XDOT =      -6870
426214                 XDOT =       -2094
105910
 YDOT =      19482
815413  feet/sec       YDOT =        5938
362138  meter/sec
 ZDOT =      12761
868862                 ZDOT =        3889
817629


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   07227
71491555  
00020000  00000-0  20000-3 0  9048
2 25544  51
6346 156
5350 0008376 249
7472 110
2792 15
76253073 20172


Satellite: ISS
Catalog Number: 25544
Epoch time:      07227
71491555   =   yrday
fracday
Element set:     904
Inclination:       51
6346  deg
RA of node:       156
5350  deg
Eccentricity:     
0008376     
Arg of perigee:   249
7472  deg
Mean anomaly:     110
2792  deg
Mean motion:   15
76253073  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2017
Checksum:              292


Coasting Arc #6 (Orbit 2031)
---------------------------------------

Vector Time (GMT): 2007/228/15:55:20
527
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5222593
32                 A    =         6724977
13  meter
 Y    =        4047102
30  meter          E    =           
0005539
 Z    =       -1233894
43                 I    =           51
80940
 XDOT =      -3837
514426                 Wp   =          331
13132
 YDOT =      -3155
554863  meter/sec      RA   =          150
67496  deg
 ZDOT =       5886
508801                 TA   =           15
36125
                                          MA   =           15
34444
                                          Ha   =            185
349  n
mi
                                          Hp   =            183
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17134492
54                 X    =        -5261466
50
 Y    =       13277894
68  feet           Y    =         3988482
96  meter
 Z    =       -4048210
09                 Z    =        -1259359
95
 XDOT =     -12590
270426                 XDOT =       -3830
538630
 YDOT =     -10352
870286  feet/sec       YDOT =       -3198
429107  meter/sec
 ZDOT =      19312
692917                 ZDOT =        5867
883296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10641856
41                 X    =         3243637
84
 Y    =      -18864183
21  feet           Y    =        -5749803
04  meter
 Z    =       -4144250
28                 Z    =        -1263167
48
 XDOT =      14339
468675                 XDOT =        4370
670052
 YDOT =       3857
819198  feet/sec       YDOT =        1175
863292  meter/sec
 ZDOT =      19241
652432                 ZDOT =        5864
855661


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   07228
66587871  
00020000  00000-0  20000-3 0  9051
2 25544  51
6341 151
6338 0008550 253
8232 106
1991 15
76286895 20323


Satellite: ISS
Catalog Number: 25544
Epoch time:      07228
66587871   =   yrday
fracday
Element set:     905
Inclination:       51
6341  deg
RA of node:       151
6338  deg
Eccentricity:     
0008550     
Arg of perigee:   253
8232  deg
Mean anomaly:     106
1991  deg
Mean motion:   15
76286895  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2032
Checksum:              306


Coasting Arc #7 (Orbit 2047)
---------------------------------------

Vector Time (GMT): 2007/229/15:59:41
430
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1135512
39                 A    =         6714003
04  meter
 Y    =        4148095
69  meter          E    =           
0007081
 Z    =       -5161377
22                 I    =           51
79612
 XDOT =      -6771
855205                 Wp   =          126
72528
 YDOT =       3438
076921  meter/sec      RA   =          145
51838  deg
 ZDOT =       1270
337881                 TA   =          155
41059
                                          MA   =          155
37681
                                          Ha   =            185
122  n
mi
                                          Hp   =            183
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3725434
36                 X    =         1114116
25
 Y    =       13609237
81  feet           Y    =         4160674
01  meter
 Z    =      -16933652
30                 Z    =        -5155912
89
 XDOT =     -22217
372720                 XDOT =       -6815
968026
 YDOT =      11279
779923  feet/sec       YDOT =        3362
103565  meter/sec
 ZDOT =       4167
775201                 ZDOT =        1237
333284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9183475
51                 X    =        -2799123
34
 Y    =      -10745862
86  feet           Y    =        -3275339
00  meter
 Z    =      -16912392
03                 Z    =        -5154897
09
 XDOT =      14661
854772                 XDOT =        4468
933334
 YDOT =     -18908
558423  feet/sec       YDOT =       -5763
328607  meter/sec
 ZDOT =       4043
059290                 ZDOT =        1232
324472


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   07229
68023109  
00020000  00000-0  20000-3 0  9064
2 25544  51
6329 146
4053 0008585 257
5395 102
4809 15
76318419 20486


Satellite: ISS
Catalog Number: 25544
Epoch time:      07229
68023109   =   yrday
fracday
Element set:     906
Inclination:       51
6329  deg
RA of node:       146
4053  deg
Eccentricity:     
0008585     
Arg of perigee:   257
5395  deg
Mean anomaly:     102
4809  deg
Mean motion:   15
76318419  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2048
Checksum:              302


Coasting Arc #8 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2007/230/16:04:23
910
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5683740
37                 A    =         6720843
69  meter
 Y    =       -1297105
43  meter          E    =           
0004160
 Z    =       -3339074
53                 I    =           51
84120
 XDOT =      -1402
031836                 Wp   =          247
99497
 YDOT =       5946
288302  meter/sec      RA   =          140
39789  deg
 ZDOT =      -4693
330773                 TA   =          331
20874
                                          MA   =          331
23169
                                          Ha   =            185
055  n
mi
                                          Hp   =            184
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18647442
17                 X    =         5714042
94
 Y    =       -4255595
23  feet           Y    =        -1233377
16  meter
 Z    =      -10954968
94                 Z    =        -3311389
43
 XDOT =      -4599
841982                 XDOT =       -1445
620635
 YDOT =      19508
819888  feet/sec       YDOT =        5930
366344  meter/sec
 ZDOT =     -15398
066840                 ZDOT =       -4700
247609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14736984
51                 X    =        -4491832
88
 Y    =       12285937
09  feet           Y    =         3744753
62  meter
 Z    =      -10850141
57                 Z    =        -3307123
15
 XDOT =      -3940
448845                 XDOT =       -1201
048808
 YDOT =     -18356
713234  feet/sec       YDOT =       -5595
126194  meter/sec
 ZDOT =     -15423
532039                 ZDOT =       -4701
092566


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   07230
69457423  
00020000  00000-0  20000-3 0  9078
2 25544  51
6320 141
1779 0008673 261
4905  98
5277 15
76309100 20642


Satellite: ISS
Catalog Number: 25544
Epoch time:      07230
69457423   =   yrday
fracday
Element set:     907
Inclination:       51
6320  deg
RA of node:       141
1779  deg
Eccentricity:     
0008673     
Arg of perigee:   261
4905  deg
Mean anomaly:      98
5277  deg
Mean motion:   15
76309100  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2064
Checksum:              292


Coasting Arc #9 (Orbit 2079)
---------------------------------------

Vector Time (GMT): 2007/231/16:09:05
639
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3190811
67                 A    =         6723434
79  meter
 Y    =       -5518328
64  meter          E    =           
0006993
 Z    =        2123889
39                 I    =           51
87249
 XDOT =       5267
172409                 Wp   =          139
29868
 YDOT =        907
765792  meter/sec      RA   =          135
19721  deg
 ZDOT =      -5549
546817                 TA   =           17
00790
                                          MA   =           16
98447
                                          Ha   =            184
566  n
mi
                                          Hp   =            184
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10468542
22                 X    =         3241963
83
 Y    =      -18104752
76  feet           Y    =        -5482361
24  meter
 Z    =        6968141
04                 Z    =         2139514
41
 XDOT =      17280
749372                 XDOT =        5283
588822
 YDOT =       2978
234226  feet/sec       YDOT =         966
758239  meter/sec
 ZDOT =     -18207
174597                 ZDOT =       -5523
919030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -283967
26                 X    =          -86553
22
 Y    =       20891920
49  feet           Y    =         6367857
36  meter
 Z    =        7026696
19                 Z    =         2141737
00
 XDOT =     -15106
833615                 XDOT =       -4604
562886
 YDOT =       5891
106934  feet/sec       YDOT =        1795
609393  meter/sec
 ZDOT =     -18109
860017                 ZDOT =       -5519
885333


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   07231
70890654  
00020000  00000-0  20000-3 0  9089
2 25544  51
6323 135
9493 0008692 266
4908  93
5262 15
76373058 20808


Satellite: ISS
Catalog Number: 25544
Epoch time:      07231
70890654   =   yrday
fracday
Element set:     908
Inclination:       51
6323  deg
RA of node:       135
9493  deg
Eccentricity:     
0008692     
Arg of perigee:   266
4908  deg
Mean anomaly:      93
5262  deg
Mean motion:   15
76373058  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2080
Checksum:              309


Coasting Arc #10 (Orbit 2095)
---------------------------------------

Vector Time (GMT): 2007/232/16:13:58
605
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2851621
33                 A    =         6713555
47  meter
 Y    =       -3038317
07  meter          E    =           
0006160
 Z    =        5269176
70                 I    =           51
85701
 XDOT =       5208
166292                 Wp   =          276
19125
 YDOT =      -5655
007619  meter/sec      RA   =          130
05689  deg
 ZDOT =       -441
980347                 TA   =          177
99506
                                          MA   =          177
99259
                                          Ha   =            184
116  n
mi
                                          Hp   =            183
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9355713
04                 X    =        -2843031
16
 Y    =       -9968231
85  feet           Y    =        -3070157
72  meter
 Z    =       17287325
12                 Z    =         5255344
26
 XDOT =      17087
159752                 XDOT =        5273
161403
 YDOT =     -18553
174602  feet/sec       YDOT =       -5596
403541  meter/sec
 ZDOT =      -1450
066755                 ZDOT =        -416
521498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13260319
13                 X    =         4041745
27
 Y    =        3589356
09  feet           Y    =         1094035
74  meter
 Z    =       17234473
65                 Z    =         5253067
57
 XDOT =      -4674
155250                 XDOT =       -1424
682520
 YDOT =      23773
637220  feet/sec       YDOT =        7246
204625  meter/sec
 ZDOT =      -1354
219020                 ZDOT =        -412
765957


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   07232
72323203  
00020000  00000-0  20000-3 0  9094
2 25544  51
6311 130
7202 0008615 268
8574  91
1603 15
76320393 20960


Satellite: ISS
Catalog Number: 25544
Epoch time:      07232
72323203   =   yrday
fracday
Element set:     909
Inclination:       51
6311  deg
RA of node:       130
7202  deg
Eccentricity:     
0008615     
Arg of perigee:   268
8574  deg
Mean anomaly:      91
1603  deg
Mean motion:   15
76320393  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2096
Checksum:              266


Coasting Arc #11 (Orbit 2110)
---------------------------------------

Vector Time (GMT): 2007/233/15:32:27
000
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5025142
46                 A    =         6722661
74  meter
 Y    =       -3645247
19  meter          E    =           
0005463
 Z    =       -2571296
89                 I    =           51
90512
 XDOT =       1243
001306                 Wp   =          239
16031
 YDOT =       5453
858810  meter/sec      RA   =          125
09512  deg
 ZDOT =      -5297
032786                 TA   =          329
93317
                                          MA   =          329
96452
                                          Ha   =            184
578  n
mi
                                          Hp   =            184
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16486687
87                 X    =         5078021
54
 Y    =      -11959472
39  feet           Y    =        -3588757
39  meter
 Z    =       -8436013
42                 Z    =        -2546756
59
 XDOT =       4078
088273                 XDOT =        1207
655024
 YDOT =      17893
237565  feet/sec       YDOT =        5467
561444  meter/sec
 ZDOT =     -17378
716489                 ZDOT =       -5291
079823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10864710
65                 X    =        -3311563
81
 Y    =       17272874
53  feet           Y    =         5264772
16  meter
 Z    =       -8343383
43                 Z    =        -2543063
27
 XDOT =      -9301
960600                 XDOT =       -2835
237591
 YDOT =     -14243
066577  feet/sec       YDOT =       -4341
286693  meter/sec
 ZDOT =     -17355
448891                 ZDOT =       -5289
940822


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   07233
67415102  
00020000  00000-0  20000-3 0  9101
2 25544  51
6311 125
8196 0008707 273
1451  86
8716 15
76355884 21119


Satellite: ISS
Catalog Number: 25544
Epoch time:      07233
67415102   =   yrday
fracday
Element set:     910
Inclination:       51
6311  deg
RA of node:       125
8196  deg
Eccentricity:     
0008707     
Arg of perigee:   273
1451  deg
Mean anomaly:      86
8716  deg
Mean motion:   15
76355884  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2111
Checksum:              282


Coasting Arc #12 (Orbit 2126)
---------------------------------------

Vector Time (GMT): 2007/234/15:37:35
002
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         944602
71                 A    =         6721891
85  meter
 Y    =       -6037228
79  meter          E    =           
0004698
 Z    =        2795128
91                 I    =           51
91926
 XDOT =       5526
093561                 Wp   =          104
36667
 YDOT =      -1520
966041  meter/sec      RA   =          119
89530  deg
 ZDOT =      -5146
660326                 TA   =           43
73249
                                          MA   =           43
69529
                                          Ha   =            184
723  n
mi
                                          Hp   =            183
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3099090
26                 X    =          998463
54
 Y    =      -19807181
06  feet           Y    =        -6026364
76  meter
 Z    =        9170370
45                 Z    =         2799848
17
 XDOT =      18130
228217                 XDOT =        5567
691927
 YDOT =      -4990
046065  feet/sec       YDOT =       -1458
937191  meter/sec
 ZDOT =     -16885
368525                 ZDOT =       -5119
713774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5347448
65                 X    =         1629902
35
 Y    =       19313693
51  feet           Y    =         5886813
78  meter
 Z    =        9187519
36                 Z    =         2800355
90
 XDOT =     -13164
466377                 XDOT =       -4012
529352
 YDOT =      11638
083372  feet/sec       YDOT =        3547
287812  meter/sec
 ZDOT =     -16783
332527                 ZDOT =       -5115
559754


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   07234
68845472  
00020000  00000-0  20000-3 0  9111
2 25544  51
6316 120
5904 0008868 277
5711  82
4446 15
76416599 21278


Satellite: ISS
Catalog Number: 25544
Epoch time:      07234
68845472   =   yrday
fracday
Element set:     911
Inclination:       51
6316  deg
RA of node:       120
5904  deg
Eccentricity:     
0008868     
Arg of perigee:   277
5711  deg
Mean anomaly:      82
4446  deg
Mean motion:   15
76416599  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2127
Checksum:              311

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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