Date: November 16th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7319 46 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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


There are no maneuvers



Coasting Arc #1 (Orbit 3449)
---------------------------------------

Vector Time (GMT): 2007/318/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         996938
64                 A    =         6719871
87  meter
 Y    =        5501079
91  meter          E    =           
0011837
 Z    =        3721366
86                 I    =           51
88282
 XDOT =      -6134
738941                 Wp   =          105
50949
 YDOT =      -1806
550434  meter/sec      RA   =           48
24482  deg
 ZDOT =       4299
635818                 TA   =          299
26339
                                          MA   =          299
38167
                                          Ha   =            186
756  n
mi
                                          Hp   =            180
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3270796
05                 X    =          917272
54
 Y    =       18048162
43  feet           Y    =         5511782
42  meter
 Z    =       12209208
87                 Z    =         3726017
14
 XDOT =     -20127
096264                 XDOT =       -6134
969146
 YDOT =      -5927
002736  feet/sec       YDOT =       -1875
154285  meter/sec
 ZDOT =      14106
416727                 ZDOT =        4269
831906

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17230045
42                 X    =        -5251717
84
 Y    =       -6254062
54  feet           Y    =        -1906238
26  meter
 Z    =       12227481
00                 Z    =         3726936
21
 XDOT =      14782
533553                 XDOT =        4505
716227
 YDOT =     -13276
576893  feet/sec       YDOT =       -4046
700637  meter/sec
 ZDOT =      13992
762316                 ZDOT =        4264
993954


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   07318
57630397  
00020000  00000-0  20000-3 0  9008
2 25544  51
6423  48
5045 0001908 187
7449 172
3687 15
76199520 34508


Satellite: ISS
Catalog Number: 25544
Epoch time:      07318
57630397   =   yrday
fracday
Element set:     900
Inclination:       51
6423  deg
RA of node:        48
5045  deg
Eccentricity:     
0001908     
Arg of perigee:   187
7449  deg
Mean anomaly:     172
3687  deg
Mean motion:   15
76199520  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3450
Checksum:              308


Coasting Arc #2 (Orbit 3464)
---------------------------------------

Vector Time (GMT): 2007/319/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5628635
30                 A    =         6721513
20  meter
 Y    =        1835922
83  meter          E    =           
0004177
 Z    =       -3186630
57                 I    =           51
86767
 XDOT =        797
137033                 Wp   =          100
89696
 YDOT =       5938
356154  meter/sec      RA   =           43
05904  deg
 ZDOT =       4833
833965                 TA   =          222
05125
                                          MA   =          222
08332
                                          Ha   =            186
668  n
mi
                                          Hp   =            180
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18466651
24                 X    =         5623167
73
 Y    =        6023368
87  feet           Y    =         1898835
15  meter
 Z    =      -10454824
71                 Z    =        -3159299
31
 XDOT =       2615
278981                 XDOT =         707
191911
 YDOT =      19482
795781  feet/sec       YDOT =        5946
766831  meter/sec
 ZDOT =      15859
035317                 ZDOT =        4837
488596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14255021
10                 X    =        -4344930
43
 Y    =       13276350
34  feet           Y    =         4046631
58  meter
 Z    =      -10350576
57                 Z    =        -3154855
74
 XDOT =     -17293
385094                 XDOT =       -5271
023777
 YDOT =      -6204
490968  feet/sec       YDOT =       -1891
128847  meter/sec
 ZDOT =      15873
559921                 ZDOT =        4838
261064


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   07319
52731584  
00020000  00000-0  20000-3 0  9015
2 25544  51
6418  43
6056 0001748 192
2604 167
8518 15
76224420 34652


Satellite: ISS
Catalog Number: 25544
Epoch time:      07319
52731584   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:        43
6056  deg
Eccentricity:     
0001748     
Arg of perigee:   192
2604  deg
Mean anomaly:     167
8518  deg
Mean motion:   15
76224420  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3465
Checksum:              289


Coasting Arc #3 (Orbit 3480)
---------------------------------------

Vector Time (GMT): 2007/320/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -297215
04                 A    =         6716398
20  meter
 Y    =       -4857245
39  meter          E    =           
0009934
 Z    =       -4638398
80                 I    =           51
82808
 XDOT =       6727
612654                 Wp   =           77
99332
 YDOT =       2356
441880  meter/sec      RA   =           37
96797  deg
 ZDOT =      -2901
883750                 TA   =          163
36353
                                          MA   =          163
33092
                                          Ha   =            186
579  n
mi
                                          Hp   =            180
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -975114
96                 X    =         -220345
67
 Y    =      -15935844
45  feet           Y    =        -4860138
85  meter
 Z    =      -15217843
83                 Z    =        -4639656
35
 XDOT =      22072
219994                 XDOT =        6714
859579
 YDOT =       7731
108531  feet/sec       YDOT =        2431
602776  meter/sec
 ZDOT =      -9520
615979                 ZDOT =       -2869
231331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14483488
72                 X    =         4414567
36
 Y    =        6705939
18  feet           Y    =         2043970
26  meter
 Z    =      -15223130
19                 Z    =        -4640010
08
 XDOT =     -16735
196303                 XDOT =       -5100
887833
 YDOT =      14838
380802  feet/sec       YDOT =        4522
738468  meter/sec
 ZDOT =      -9396
050497                 ZDOT =       -2863
916191


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   07320
54169877  
00020000  00000-0  20000-3 0  9020
2 25544  51
6411  38
3789 0001669 195
0970 165
0145 15
76253398 34818


Satellite: ISS
Catalog Number: 25544
Epoch time:      07320
54169877   =   yrday
fracday
Element set:     902
Inclination:       51
6411  deg
RA of node:        38
3789  deg
Eccentricity:     
0001669     
Arg of perigee:   195
0970  deg
Mean anomaly:     165
0145  deg
Mean motion:   15
76253398  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3481
Checksum:              310


Coasting Arc #4 (Orbit 3496)
---------------------------------------

Vector Time (GMT): 2007/321/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6075221
08                 A    =         6724159
84  meter
 Y    =       -2214384
97  meter          E    =           
0014395
 Z    =        1817429
72                 I    =           51
83157
 XDOT =        185
455219                 Wp   =          119
67728
 YDOT =      -5198
593304  meter/sec      RA   =           32
78997  deg
 ZDOT =      -5687
682125                 TA   =           40
19192
                                          MA   =           40
08555
                                          Ha   =            186
476  n
mi
                                          Hp   =            180
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19931827
70                 X    =        -6058836
84
 Y    =       -7265042
56  feet           Y    =        -2282230
03  meter
 Z    =        5962695
92                 Z    =         1787955
55
 XDOT =        608
448880                 XDOT =         271
203006
 YDOT =     -17055
752311  feet/sec       YDOT =       -5196
039662  meter/sec
 ZDOT =     -18660
374427                 ZDOT =       -5686
573195

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15550582
69                 X    =         4739817
60
 Y    =      -14476407
24  feet           Y    =        -4412408
93  meter
 Z    =        5850243
85                 Z    =         1783154
33
 XDOT =      13809
383631                 XDOT =        4209
100131
 YDOT =       7258
753696  feet/sec       YDOT =        2212
468127  meter/sec
 ZDOT =     -18656
685211                 ZDOT =       -5686
557652


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   07321
55605100  
00020000  00000-0  20000-3 0  9037
2 25544  51
6415  33
1520 0001396 196
8741 163
2377 15
76335070 34972


Satellite: ISS
Catalog Number: 25544
Epoch time:      07321
55605100   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:        33
1520  deg
Eccentricity:     
0001396     
Arg of perigee:   196
8741  deg
Mean anomaly:     163
2377  deg
Mean motion:   15
76335070  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3497
Checksum:              271


Coasting Arc #5 (Orbit 3512)
---------------------------------------

Vector Time (GMT): 2007/322/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -692464
39                 A    =         6713783
86  meter
 Y    =        4230918
08  meter          E    =           
0004496
 Z    =        5164966
61                 I    =           51
77207
 XDOT =      -7130
977512                 Wp   =          142
29047
 YDOT =      -2657
527027  meter/sec      RA   =           27
67495  deg
 ZDOT =       1216
841706                 TA   =          296
09123
                                          MA   =          296
13750
                                          Ha   =            186
339  n
mi
                                          Hp   =            180
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2271864
79                 X    =         -764814
55
 Y    =       13880964
83  feet           Y    =         4222769
81  meter
 Z    =       16945428
52                 Z    =         5161427
00
 XDOT =     -23395
595513                 XDOT =       -7106
641939
 YDOT =      -8718
920692  feet/sec       YDOT =       -2737
133640  meter/sec
 ZDOT =       3992
262815                 ZDOT =        1182
257882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11428652
95                 X    =        -3483453
42
 Y    =       -8226197
75  feet           Y    =        -2507345
07  meter
 Z    =       16932385
07                 Z    =         5160990
97
 XDOT =      17522
559898                 XDOT =        5340
876257
 YDOT =     -16370
893774  feet/sec       YDOT =       -4989
848422  meter/sec
 ZDOT =       3860
309600                 ZDOT =        1176
622366


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   07322
57037305  
00020000  00000-0  20000-3 0  9047
2 25544  51
6416  27
9248 0001427 202
6562 157
4540 15
76378871 35135


Satellite: ISS
Catalog Number: 25544
Epoch time:      07322
57037305   =   yrday
fracday
Element set:     904
Inclination:       51
6416  deg
RA of node:        27
9248  deg
Eccentricity:     
0001427     
Arg of perigee:   202
6562  deg
Mean anomaly:     157
4540  deg
Mean motion:   15
76378871  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3513
Checksum:              284


Coasting Arc #6 (Orbit 3527)
---------------------------------------

Vector Time (GMT): 2007/323/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6280006
04                 A    =         6725443
83  meter
 Y    =        2378497
11  meter          E    =           
0010809
 Z    =        -264150
19                 I    =           51
78453
 XDOT =      -1472
701359                 Wp   =           44
63220
 YDOT =       4542
501773  meter/sec      RA   =           22
51854  deg
 ZDOT =       6045
749563                 TA   =          312
50032
                                          MA   =          312
59159
                                          Ha   =            186
363  n
mi
                                          Hp   =            180
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20603694
34                 X    =         6254225
79
 Y    =        7803468
22  feet           Y    =         2448579
56  meter
 Z    =        -866634
47                 Z    =         -233703
89
 XDOT =      -4831
697373                 XDOT =       -1552
756566
 YDOT =      14903
221039  feet/sec       YDOT =        4525
585418  meter/sec
 ZDOT =      19835
136363                 ZDOT =        6038
400707

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15803702
84                 X    =        -4816968
63
 Y    =       15356990
91  feet           Y    =         4680810
83  meter
 Z    =        -750465
90                 Z    =         -228742
01
 XDOT =     -10282
438036                 XDOT =       -3134
087113
 YDOT =      -9642
479392  feet/sec       YDOT =       -2939
027719  meter/sec
 ZDOT =      19807
620440                 ZDOT =        6037
362710


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   07323
52127446  
00020000  00000-0  20000-3 0  9050
2 25544  51
6412  23
0242 0001053 205
4548 154
6565 15
76359568 35286


Satellite: ISS
Catalog Number: 25544
Epoch time:      07323
52127446   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:        23
0242  deg
Eccentricity:     
0001053     
Arg of perigee:   205
4548  deg
Mean anomaly:     154
6565  deg
Mean motion:   15
76359568  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3528
Checksum:              278


Coasting Arc #7 (Orbit 3543)
---------------------------------------

Vector Time (GMT): 2007/324/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1929119
72                 A    =         6713343
19  meter
 Y    =       -3735250
70  meter          E    =           
0014444
 Z    =       -5246473
94                 I    =           51
71747
 XDOT =       7147
043777                 Wp   =           99
14871
 YDOT =       2774
560822  meter/sec      RA   =           17
36894  deg
 ZDOT =        651
861409                 TA   =          177
05141
                                          MA   =          177
04288
                                          Ha   =            186
219  n
mi
                                          Hp   =            180
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6329132
94                 X    =         1996231
52
 Y    =      -12254759
51  feet           Y    =        -3713302
82  meter
 Z    =      -17212841
02                 Z    =        -5236939
12
 XDOT =      23448
306354                 XDOT =        7112
320328
 YDOT =       9102
889837  feet/sec       YDOT =        2854
288953  meter/sec
 ZDOT =       2138
652916                 ZDOT =         686
498302

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8563301
70                 X    =         2610094
36
 Y    =       10869327
88  feet           Y    =         3312971
14  meter
 Z    =      -17176918
40                 Z    =        -5235524
73
 XDOT =     -17085
218997                 XDOT =       -5207
574750
 YDOT =      17052
838078  feet/sec       YDOT =        5197
705046  meter/sec
 ZDOT =       2270
813249                 ZDOT =         692
143878


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   07324
53554028  
00020000  00000-0  20000-3 0  9063
2 25544  51
6417  17
7965 0001135 207
1660 152
9445 15
76430100 35446


Satellite: ISS
Catalog Number: 25544
Epoch time:      07324
53554028   =   yrday
fracday
Element set:     906
Inclination:       51
6417  deg
RA of node:        17
7965  deg
Eccentricity:     
0001135     
Arg of perigee:   207
1660  deg
Mean anomaly:     152
9445  deg
Mean motion:   15
76430100  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3544
Checksum:              271


Coasting Arc #8 (Orbit 3559)
---------------------------------------

Vector Time (GMT): 2007/325/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6096102
29                 A    =         6724149
12  meter
 Y    =       -2455188
04  meter          E    =           
0009054
 Z    =       -1403036
70                 I    =           51
72732
 XDOT =       2972
816580                 Wp   =          147
84973
 YDOT =      -4062
997046  meter/sec      RA   =           12
23995  deg
 ZDOT =      -5831
457882                 TA   =           47
57323
                                          MA   =           47
49669
                                          Ha   =            186
102  n
mi
                                          Hp   =            180
045

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20000335
59                 X    =        -6061379
03
 Y    =       -8055078
88  feet           Y    =        -2523163
92  meter
 Z    =       -4603138
77                 Z    =        -1432568
17
 XDOT =       9753
335237                 XDOT =        3046
357677
 YDOT =     -13330
042801  feet/sec       YDOT =       -4029
341932  meter/sec
 ZDOT =     -19132
079665                 ZDOT =       -5816
837022

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15248595
39                 X    =         4647771
88
 Y    =      -15209469
32  feet           Y    =        -4635846
25  meter
 Z    =       -4715823
13                 Z    =        -1437382
89
 XDOT =       7280
652869                 XDOT =        2219
142994
 YDOT =      13189
840057  feet/sec       YDOT =        4020
263249  meter/sec
 ZDOT =     -19076
823183                 ZDOT =       -5814
615706


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   07325
54977633  
00020000  00000-0  20000-3 0  9077
2 25544  51
6423  12
5690 0000974 204
3171 155
7948 15
76507513 35607


Satellite: ISS
Catalog Number: 25544
Epoch time:      07325
54977633   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:        12
5690  deg
Eccentricity:     
0000974     
Arg of perigee:   204
3171  deg
Mean anomaly:     155
7948  deg
Mean motion:   15
76507513  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3560
Checksum:              296


Coasting Arc #9 (Orbit 3575)
---------------------------------------

Vector Time (GMT): 2007/326/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3245979
53                 A    =         6714953
11  meter
 Y    =        3409920
92  meter          E    =           
0006569
 Z    =        4784264
00                 I    =           51
66707
 XDOT =      -6707
414886                 Wp   =           63
89427
 YDOT =      -2839
290491  meter/sec      RA   =            7
05641  deg
 ZDOT =      -2521
611651                 TA   =           50
78417
                                          MA   =           50
72587
                                          Ha   =            186
092  n
mi
                                          Hp   =            179
993

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10649539
15                 X    =        -3307110
39
 Y    =       11187404
60  feet           Y    =         3373280
44  meter
 Z    =       15696404
21                 Z    =         4768346
23
 XDOT =     -22005
954350                 XDOT =       -6662
917056
 YDOT =      -9315
257518  feet/sec       YDOT =       -2914
047648  meter/sec
 ZDOT =      -8273
004103                 ZDOT =       -2554
089441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6319422
96                 X    =        -1926160
12
 Y    =      -14160643
44  feet           Y    =        -4316164
12  meter
 Z    =       15636140
24                 Z    =         4765895
54
 XDOT =      15867
053731                 XDOT =        4836
277977
 YDOT =     -16372
819256  feet/sec       YDOT =       -4990
435309  meter/sec
 ZDOT =      -8396
939961                 ZDOT =       -2559
387300


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   07326
56398248  
00020000  00000-0  20000-3 0  9080
2 25544  51
6413   7
3415 0000911 210
6839 149
4272 15
76569507 35763


Satellite: ISS
Catalog Number: 25544
Epoch time:      07326
56398248   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:         7
3415  deg
Eccentricity:     
0000911     
Arg of perigee:   210
6839  deg
Mean anomaly:     149
4272  deg
Mean motion:   15
76569507  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3576
Checksum:              305


Coasting Arc #10 (Orbit 3591)
---------------------------------------

Vector Time (GMT): 2007/327/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5484510
34                 A    =         6721020
22  meter
 Y    =        2517901
03  meter          E    =           
0012993
 Z    =        2946040
95                 I    =           51
65849
 XDOT =      -4449
401477                 Wp   =           85
42296
 YDOT =       3811
723179  meter/sec      RA   =            1
94701  deg
 ZDOT =       5007
642390                 TA   =          308
58569
                                          MA   =          308
70201
                                          Ha   =            186
031  n
mi
                                          Hp   =            179
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17993800
32                 X    =         5441635
35
 Y    =        8260830
15  feet           Y    =         2578991
91  meter
 Z    =        9665488
68                 Z    =         2972581
71
 XDOT =     -14597
773876                 XDOT =       -4516
021092
 YDOT =      12505
653475  feet/sec       YDOT =        3761
594464  meter/sec
 ZDOT =      16429
272932                 ZDOT =        4985
865019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14174392
79                 X    =        -4320354
92
 Y    =       13752683
85  feet           Y    =         4191818
04  meter
 Z    =        9766786
18                 Z    =         2976916
43
 XDOT =      -5363
403200                 XDOT =       -1634
765295
 YDOT =     -17177
987073  feet/sec       YDOT =       -5235
850460  meter/sec
 ZDOT =      16346
732839                 ZDOT =        4982
484169


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   07327
57816221  
00020000  00000-0  20000-3 0  9099
2 25544  51
6410   2
1131 0000693 201
4679 158
6457 15
76568022 35921


Satellite: ISS
Catalog Number: 25544
Epoch time:      07327
57816221   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:         2
1131  deg
Eccentricity:     
0000693     
Arg of perigee:   201
4679  deg
Mean anomaly:     158
6457  deg
Mean motion:   15
76568022  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3592
Checksum:              282


Coasting Arc #11 (Orbit 3606)
---------------------------------------

Vector Time (GMT): 2007/328/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4463792
90                 A    =         6718436
32  meter
 Y    =       -3277077
17  meter          E    =           
0006025
 Z    =       -3810858
88                 I    =           51
62218
 XDOT =       5744
525773                 Wp   =          110
32045
 YDOT =       2980
177743  meter/sec      RA   =          356
74144  deg
 ZDOT =       4169
262847                 TA   =          203
36346
                                          MA   =          203
39085
                                          Ha   =            185
947  n
mi
                                          Hp   =            179
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14644989
82                 X    =         4518618
93
 Y    =      -10751565
51  feet           Y    =        -3226853
44  meter
 Z    =      -12502817
86                 Z    =        -3789040
38
 XDOT =      18846
869333                 XDOT =        5690
519883
 YDOT =       9777
486032  feet/sec       YDOT =        3044
113757  meter/sec
 ZDOT =      13678
683882                 ZDOT =        4197
039828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5023264
68                 X    =         1531091
07
 Y    =       17518597
14  feet           Y    =         5339668
41  meter
 Z    =      -12420060
71                 Z    =        -3785634
51
 XDOT =     -14368
162829                 XDOT =       -4379
416030
 YDOT =      13885
195823  feet/sec       YDOT =        4232
207687  meter/sec
 ZDOT =      13784
733924                 ZDOT =        4201
586900


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   07328
52892655  
00020000  00000-0  20000-3 0  9102
2 25544  51
6420 357
2118 0000705 210
7580 149
3544 15
76636329 36076


Satellite: ISS
Catalog Number: 25544
Epoch time:      07328
52892655   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:       357
2118  deg
Eccentricity:     
0000705     
Arg of perigee:   210
7580  deg
Mean anomaly:     149
3544  deg
Mean motion:   15
76636329  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3607
Checksum:              290


Coasting Arc #12 (Orbit 3622)
---------------------------------------

Vector Time (GMT): 2007/329/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4437378
81                 A    =         6716642
92  meter
 Y    =       -2744142
60  meter          E    =           
0007969
 Z    =       -4238031
36                 I    =           51
58718
 XDOT =       5713
752432                 Wp   =           71
91654
 YDOT =      -3711
488600  meter/sec      RA   =          351
63394  deg
 ZDOT =      -3582
373841                 TA   =          161
66125
                                          MA   =          161
63250
                                          Ha   =            185
832  n
mi
                                          Hp   =            179
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14558329
43                 X    =        -4385775
51
 Y    =       -9003092
52  feet           Y    =        -2793474
68  meter
 Z    =      -13904302
36                 Z    =        -4259463
76
 XDOT =      18745
906928                 XDOT =        5772
233137
 YDOT =     -12176
799870  feet/sec       YDOT =       -3647
266635  meter/sec
 ZDOT =     -11753
195016                 ZDOT =       -3554
474295

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13258222
03                 X    =         4041106
08
 Y    =      -10720853
85  feet           Y    =        -3267716
25  meter
 Z    =      -13986175
18                 Z    =        -4262986
19
 XDOT =       4543
218420                 XDOT =        1384
772974
 YDOT =      20800
269745  feet/sec       YDOT =        6339
922218  meter/sec
 ZDOT =     -11647
315716                 ZDOT =       -3550
101830


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   07329
54304799  
00020000  00000-0  20000-3 0  9113
2 25544  51
6413 351
9829 0000709 215
2038 144
9080 15
76679887 36230


Satellite: ISS
Catalog Number: 25544
Epoch time:      07329
54304799   =   yrday
fracday
Element set:     911
Inclination:       51
6413  deg
RA of node:       351
9829  deg
Eccentricity:     
0000709     
Arg of perigee:   215
2038  deg
Mean anomaly:     144
9080  deg
Mean motion:   15
76679887  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3623
Checksum:              315

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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