Date: November 5th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4036 47 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 3257)
---------------------------------------

Vector Time (GMT): 2007/306/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4371724
61                 A    =         6721416
09  meter
 Y    =       -3611873
10  meter          E    =           
0006320
 Z    =       -3611662
04                 I    =           51
94146
 XDOT =       1410
719943                 Wp   =          107
83792
 YDOT =       6133
352038  meter/sec      RA   =          110
52659  deg
 ZDOT =      -4434
308145                 TA   =          115
18193
                                          MA   =          115
11637
                                          Ha   =            187
817  n
mi
                                          Hp   =            180
771

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14342928
51                 X    =         4429333
20
 Y    =      -11849977
35  feet           Y    =        -3562663
83  meter
 Z    =      -11849284
90                 Z    =        -3590284
09
 XDOT =       4628
346271                 XDOT =        1363
572337
 YDOT =      20122
546056  feet/sec       YDOT =        6148
863969  meter/sec
 ZDOT =     -14548
255070                 ZDOT =       -4427
569206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15132887
52                 X    =        -4612504
12
 Y    =       10910936
55  feet           Y    =         3325653
46  meter
 Z    =      -11768359
82                 Z    =        -3586996
07
 XDOT =      -2627
170016                 XDOT =        -800
761421
 YDOT =     -19277
598875  feet/sec       YDOT =       -5875
812137  meter/sec
 ZDOT =     -14521
882076                 ZDOT =       -4426
269657


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   07306
40151928  
00020000  00000-0  20000-3 0  9005
2 25544  51
6377 111
2061 0002792 166
7845 193
3393 15
75813177 32584


Satellite: ISS
Catalog Number: 25544
Epoch time:      07306
40151928   =   yrday
fracday
Element set:     900
Inclination:       51
6377  deg
RA of node:       111
2061  deg
Eccentricity:     
0002792     
Arg of perigee:   166
7845  deg
Mean anomaly:     193
3393  deg
Mean motion:   15
75813177  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3258
Checksum:              291


Coasting Arc #2 (Orbit 3273)
---------------------------------------

Vector Time (GMT): 2007/307/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1218562
51                 A    =         6721747
68  meter
 Y    =       -5652884
24  meter          E    =           
0013096
 Z    =        3413166
58                 I    =           51
95280
 XDOT =       4814
949598                 Wp   =          100
96124
 YDOT =      -3843
061246  meter/sec      RA   =          105
34659  deg
 ZDOT =      -4633
408426                 TA   =           38
83891
                                          MA   =           38
74487
                                          Ha   =            187
586  n
mi
                                          Hp   =            180
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3997908
51                 X    =        -1171841
30
 Y    =      -18546208
15  feet           Y    =        -5666249
67  meter
 Z    =       11198053
09                 Z    =         3407360
22
 XDOT =      15797
078733                 XDOT =        4880
073979
 YDOT =     -12608
468656  feet/sec       YDOT =       -3788
853624  meter/sec
 ZDOT =     -15201
471214                 ZDOT =       -4609
858912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3197318
28                 X    =          974542
61
 Y    =       18714476
16  feet           Y    =         5704172
33  meter
 Z    =       11175287
02                 Z    =         3406227
48
 XDOT =     -15084
853257                 XDOT =       -4597
863273
 YDOT =      11625
895036  feet/sec       YDOT =        3543
572807  meter/sec
 ZDOT =     -15112
303711                 ZDOT =       -4606
230171


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   07307
41616749  
00020000  00000-0  20000-3 0  9015
2 25544  51
6382 105
9803 0002601 172
2165 187
9040 15
75889042 32740


Satellite: ISS
Catalog Number: 25544
Epoch time:      07307
41616749   =   yrday
fracday
Element set:     901
Inclination:       51
6382  deg
RA of node:       105
9803  deg
Eccentricity:     
0002601     
Arg of perigee:   172
2165  deg
Mean anomaly:     187
9040  deg
Mean motion:   15
75889042  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3274
Checksum:              287


Coasting Arc #3 (Orbit 3289)
---------------------------------------

Vector Time (GMT): 2007/308/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4057735
58                 A    =         6718530
51  meter
 Y    =        3029773
89  meter          E    =           
0010804
 Z    =        4410795
36                 I    =           51
94648
 XDOT =      -1427
939127                 Wp   =          123
13824
 YDOT =      -6794
897324  meter/sec      RA   =          100
26729  deg
 ZDOT =       3342
143076                 TA   =          293
38325
                                          MA   =          293
49684
                                          Ha   =            187
673  n
mi
                                          Hp   =            180
798

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13312780
78                 X    =        -4112740
58
 Y    =        9940203
07  feet           Y    =         2984090
50  meter
 Z    =       14471113
39                 Z    =         4390948
92
 XDOT =      -4684
839655                 XDOT =       -1368
087221
 YDOT =     -22292
970224  feet/sec       YDOT =       -6810
530658  meter/sec
 ZDOT =      10965
036337                 ZDOT =        3335
351503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13678043
30                 X    =         4169067
60
 Y    =       -9545626
44  feet           Y    =        -2909506
94  meter
 Z    =       14395938
30                 Z    =         4387881
99
 XDOT =       3398
819634                 XDOT =        1035
960224
 YDOT =      21424
439585  feet/sec       YDOT =        6530
169185  meter/sec
 ZDOT =      10938
388876                 ZDOT =        3334
020929


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   07308
43080288  
00020000  00000-0  20000-3 0  9022
2 25544  51
6368 100
7540 0002628 173
9676 186
1520 15
75847401 32904


Satellite: ISS
Catalog Number: 25544
Epoch time:      07308
43080288   =   yrday
fracday
Element set:     902
Inclination:       51
6368  deg
RA of node:       100
7540  deg
Eccentricity:     
0002628     
Arg of perigee:   173
9676  deg
Mean anomaly:     186
1520  deg
Mean motion:   15
75847401  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3290
Checksum:              288


Coasting Arc #4 (Orbit 3304)
---------------------------------------

Vector Time (GMT): 2007/309/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1305247
62                 A    =         6724364
20  meter
 Y    =        6159836
22  meter          E    =           
0004336
 Z    =       -2361510
28                 I    =           51
96981
 XDOT =      -4534
108502                 Wp   =           73
69839
 YDOT =       3038
599178  meter/sec      RA   =           95
09395  deg
 ZDOT =       5429
253336                 TA   =          259
82628
                                          MA   =          259
87519
                                          Ha   =            187
474  n
mi
                                          Hp   =            180
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4282308
45                 X    =         1247742
41
 Y    =       20209436
41  feet           Y    =         6174110
67  meter
 Z    =       -7747737
13                 Z    =        -2355309
04
 XDOT =     -14875
684062                 XDOT =       -4594
124462
 YDOT =       9969
157407  feet/sec       YDOT =        2987
560735  meter/sec
 ZDOT =      17812
510945                 ZDOT =        5407
080353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4084242
62                 X    =        -1244877
15
 Y    =      -20259682
15  feet           Y    =        -6175151
12  meter
 Z    =       -7723416
20                 Z    =        -2354097
26
 XDOT =      13616
396091                 XDOT =        4150
277528
 YDOT =      -9491
719196  feet/sec       YDOT =       -2893
076011  meter/sec
 ZDOT =      17728
478238                 ZDOT =        5403
640167


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   07309
38200548  
00020000  00000-0  20000-3 0  9031
2 25544  51
6361  95
8540 0002767 177
9475 182
1701 15
75896742 33052


Satellite: ISS
Catalog Number: 25544
Epoch time:      07309
38200548   =   yrday
fracday
Element set:     903
Inclination:       51
6361  deg
RA of node:        95
8540  deg
Eccentricity:     
0002767     
Arg of perigee:   177
9475  deg
Mean anomaly:     182
1701  deg
Mean motion:   15
75896742  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3305
Checksum:              305


Coasting Arc #5 (Orbit 3320)
---------------------------------------

Vector Time (GMT): 2007/310/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3912611
24                 A    =         6715938
93  meter
 Y    =       -2220447
25  meter          E    =           
0012615
 Z    =       -4997403
72                 I    =           51
94237
 XDOT =       1567
781619                 Wp   =           87
29602
 YDOT =       7262
111879  meter/sec      RA   =           90
00284  deg
 ZDOT =      -2002
972885                 TA   =          163
41985
                                          MA   =          163
37856
                                          Ha   =            187
429  n
mi
                                          Hp   =            180
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12836651
05                 X    =         3961426
91
 Y    =       -7284931
92  feet           Y    =        -2176421
34  meter
 Z    =      -16395681
49                 Z    =        -4978277
17
 XDOT =       5143
640482                 XDOT =        1496
189390
 YDOT =      23825
826375  feet/sec       YDOT =        7279
243383  meter/sec
 ZDOT =      -6571
433350                 ZDOT =       -1995
530409

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12890297
86                 X    =        -3928962
79
 Y    =        7352781
99  feet           Y    =         2241127
95  meter
 Z    =      -16323144
09                 Z    =        -4975294
32
 XDOT =      -4769
663877                 XDOT =       -1453
793550
 YDOT =     -22858
293421  feet/sec       YDOT =       -6967
207835  meter/sec
 ZDOT =      -6542
267999                 ZDOT =       -1994
083286


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   07310
39660670  
00020000  00000-0  20000-3 0  9041
2 25544  51
6356  90
6281 0002730 179
0989 181
0181 15
75923937 33219


Satellite: ISS
Catalog Number: 25544
Epoch time:      07310
39660670   =   yrday
fracday
Element set:     904
Inclination:       51
6356  deg
RA of node:        90
6281  deg
Eccentricity:     
0002730     
Arg of perigee:   179
0989  deg
Mean anomaly:     181
0181  deg
Mean motion:   15
75923937  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3321
Checksum:              292


Coasting Arc #6 (Orbit 3336)
---------------------------------------

Vector Time (GMT): 2007/311/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1452583
77                 A    =         6725983
05  meter
 Y    =       -6464673
48  meter          E    =           
0015076
 Z    =        1107701
60                 I    =           51
97632
 XDOT =       4477
475272                 Wp   =          131
55273
 YDOT =      -2030
345990  meter/sec      RA   =           84
84774  deg
 ZDOT =      -5936
065517                 TA   =           36
36498
                                          MA   =           36
26265
                                          Ha   =            187
156  n
mi
                                          Hp   =            180
788

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4765694
77                 X    =        -1385568
02
 Y    =      -21209558
67  feet           Y    =        -6480542
39  meter
 Z    =        3634191
60                 Z    =         1100807
54
 XDOT =      14689
879500                 XDOT =        4528
683301
 YDOT =      -6661
240124  feet/sec       YDOT =       -1979
990015  meter/sec
 ZDOT =     -19475
280568                 ZDOT =       -5914
188919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5261266
07                 X    =         1603633
90
 Y    =       21096721
37  feet           Y    =         6430280
67  meter
 Z    =        3607215
13                 Z    =         1099479
17
 XDOT =     -13107
600002                 XDOT =       -3995
196481
 YDOT =       6608
238726  feet/sec       YDOT =        2014
191164  meter/sec
 ZDOT =     -19392
250630                 ZDOT =       -5910
757992


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   07311
41118902  
00020000  00000-0  20000-3 0  9052
2 25544  51
6363  85
4018 0002472 187
3856 172
7272 15
75995968 33373


Satellite: ISS
Catalog Number: 25544
Epoch time:      07311
41118902   =   yrday
fracday
Element set:     905
Inclination:       51
6363  deg
RA of node:        85
4018  deg
Eccentricity:     
0002472     
Arg of perigee:   187
3856  deg
Mean anomaly:     172
7272  deg
Mean motion:   15
75995968  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3337
Checksum:              307


Coasting Arc #7 (Orbit 3352)
---------------------------------------

Vector Time (GMT): 2007/312/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3954307
32                 A    =         6714699
71  meter
 Y    =        1306252
77  meter          E    =           
0004354
 Z    =        5265565
23                 I    =           51
93322
 XDOT =      -1770
874241                 Wp   =          147
48452
 YDOT =      -7481
808407  meter/sec      RA   =           79
73381  deg
 ZDOT =        522
372604                 TA   =          297
55411
                                          MA   =          297
59833
                                          Ha   =            187
426  n
mi
                                          Hp   =            180
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12973449
20                 X    =        -3994200
12
 Y    =        4285606
20  feet           Y    =         1261810
33  meter
 Z    =       17275476
48                 Z    =         5246257
71
 XDOT =      -5809
954859                 XDOT =       -1689
617586
 YDOT =     -24546
615507  feet/sec       YDOT =       -7501
157005  meter/sec
 ZDOT =       1713
820880                 ZDOT =         513
966684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12890332
57                 X    =         3928973
37
 Y    =       -4800485
03  feet           Y    =        -1463187
84  meter
 Z    =       17202138
30                 Z    =         5243211
75
 XDOT =       6438
265286                 XDOT =        1962
383259
 YDOT =      23356
566227  feet/sec       YDOT =        7119
081386  meter/sec
 ZDOT =       1680
986635                 ZDOT =         512
364726


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   07312
42575945  
00020000  00000-0  20000-3 0  9069
2 25544  51
6358  80
1753 0002643 184
7311 175
3829 15
75926373 33531


Satellite: ISS
Catalog Number: 25544
Epoch time:      07312
42575945   =   yrday
fracday
Element set:     906
Inclination:       51
6358  deg
RA of node:        80
1753  deg
Eccentricity:     
0002643     
Arg of perigee:   184
7311  deg
Mean anomaly:     175
3829  deg
Mean motion:   15
75926373  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3353
Checksum:              302


Coasting Arc #8 (Orbit 3368)
---------------------------------------

Vector Time (GMT): 2007/313/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1621032
75                 A    =         6726461
46  meter
 Y    =        6520314
37  meter          E    =           
0010677
 Z    =         215300
07                 I    =           51
96791
 XDOT =      -4656
348675                 Wp   =           56
44453
 YDOT =        950
595986  meter/sec      RA   =           74
60234  deg
 ZDOT =       6061
986941                 TA   =          305
88587
                                          MA   =          305
98495
                                          Ha   =            187
129  n
mi
                                          Hp   =            180
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5318348
91                 X    =         1546955
20
 Y    =       21392107
50  feet           Y    =         6538027
48  meter
 Z    =         706365
07                 Z    =          222995
60
 XDOT =     -15276
734499                 XDOT =       -4696
081335
 YDOT =       3118
753236  feet/sec       YDOT =         898
303688  meter/sec
 ZDOT =      19888
408598                 ZDOT =        6039
269158

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6521545
16                 X    =        -1987766
96
 Y    =      -21055480
26  feet           Y    =        -6417710
38  meter
 Z    =         736376
11                 Z    =          224447
44
 XDOT =      13651
004914                 XDOT =        4160
826298
 YDOT =      -3512
722925  feet/sec       YDOT =       -1070
677947  meter/sec
 ZDOT =      19802
046851                 ZDOT =        6035
663880


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   07313
44030810  
00020000  00000-0  20000-3 0  9070
2 25544  51
6365  74
9488 0002743 189
5297 170
5816 15
76005356 33692


Satellite: ISS
Catalog Number: 25544
Epoch time:      07313
44030810   =   yrday
fracday
Element set:     907
Inclination:       51
6365  deg
RA of node:        74
9488  deg
Eccentricity:     
0002743     
Arg of perigee:   189
5297  deg
Mean anomaly:     170
5816  deg
Mean motion:   15
76005356  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3369
Checksum:              304


Coasting Arc #9 (Orbit 3383)
---------------------------------------

Vector Time (GMT): 2007/314/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4231168
97                 A    =         6714698
41  meter
 Y    =        -351962
63  meter          E    =           
0014632
 Z    =       -5214502
03                 I    =           51
92023
 XDOT =       1896
961071                 Wp   =          108
55922
 YDOT =       7383
330964  meter/sec      RA   =           69
46234  deg
 ZDOT =       1038
695118                 TA   =          171
32934
                                          MA   =          171
30403
                                          Ha   =            187
065  n
mi
                                          Hp   =            180
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13881787
94                 X    =         4260122
15
 Y    =       -1154733
05  feet           Y    =         -304485
13  meter
 Z    =      -17107946
29                 Z    =        -5193876
01
 XDOT =       6223
625560                 XDOT =        1809
212599
 YDOT =      24223
526785  feet/sec       YDOT =        7404
053173  meter/sec
 ZDOT =       3407
792382                 ZDOT =        1047
698127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13854168
98                 X    =        -4222750
70
 Y    =        2185910
76  feet           Y    =          666265
60  meter
 Z    =      -17029476
43                 Z    =        -5190584
42
 XDOT =      -7820
495739                 XDOT =       -2383
687101
 YDOT =     -22687
708169  feet/sec       YDOT =       -6915
213450  meter/sec
 ZDOT =       3442
862739                 ZDOT =        1049
384563


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   07314
39143400  
00020000  00000-0  20000-3 0  9086
2 25544  51
6373  70
0500 0002700 190
4747 169
6361 15
76026920 33848


Satellite: ISS
Catalog Number: 25544
Epoch time:      07314
39143400   =   yrday
fracday
Element set:     908
Inclination:       51
6373  deg
RA of node:        70
0500  deg
Eccentricity:     
0002700     
Arg of perigee:   190
4747  deg
Mean anomaly:     169
6361  deg
Mean motion:   15
76026920  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3384
Checksum:              266


Coasting Arc #10 (Orbit 3399)
---------------------------------------

Vector Time (GMT): 2007/315/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1650785
12                 A    =         6725150
57  meter
 Y    =       -6317120
04  meter          E    =           
0009711
 Z    =       -1591386
37                 I    =           51
94485
 XDOT =       5084
478114                 Wp   =          154
29603
 YDOT =        123
670800  meter/sec      RA   =           64
35540  deg
 ZDOT =      -5786
790767                 TA   =           43
20539
                                          MA   =           43
12925
                                          Ha   =            186
872  n
mi
                                          Hp   =            180
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5415961
69                 X    =        -1572292
53
 Y    =      -20725459
45  feet           Y    =        -6335141
06  meter
 Z    =       -5221083
90                 Z    =        -1599215
95
 XDOT =      16681
358643                 XDOT =        5110
829389
 YDOT =        405
744096  feet/sec       YDOT =         180
676086  meter/sec
 ZDOT =     -18985
534012                 ZDOT =       -5762
025568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7253056
49                 X    =         2210731
62
 Y    =       20148232
97  feet           Y    =         6141181
41  meter
 Z    =       -5251562
34                 Z    =        -1600676
20
 XDOT =     -15285
929013                 XDOT =       -4659
151163
 YDOT =        597
141509  feet/sec       YDOT =         182
008732  meter/sec
 ZDOT =     -18891
253311                 ZDOT =       -5758
054009


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   07315
40595044  
00020000  00000-0  20000-3 0  9095
2 25544  51
6375  64
8235 0002475 196
1210 163
9876 15
76078811 34006


Satellite: ISS
Catalog Number: 25544
Epoch time:      07315
40595044   =   yrday
fracday
Element set:     909
Inclination:       51
6375  deg
RA of node:        64
8235  deg
Eccentricity:     
0002475     
Arg of perigee:   196
1210  deg
Mean anomaly:     163
9876  deg
Mean motion:   15
76078811  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3400
Checksum:              293


Coasting Arc #11 (Orbit 3415)
---------------------------------------

Vector Time (GMT): 2007/316/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4679428
07                 A    =         6716480
42  meter
 Y    =        -521134
93  meter          E    =           
0005781
 Z    =        4785456
55                 I    =           51
90156
 XDOT =      -1847
185731                 Wp   =           78
49281
 YDOT =      -7028
197910  meter/sec      RA   =           59
18932  deg
 ZDOT =      -2567
904880                 TA   =           36
57512
                                          MA   =           36
53567
                                          Ha   =            187
058  n
mi
                                          Hp   =            180
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15352454
29                 X    =        -4696500
42
 Y    =       -1709760
26  feet           Y    =         -573558
83  meter
 Z    =       15700316
77                 Z    =         4762681
72
 XDOT =      -6060
320639                 XDOT =       -1755
983297
 YDOT =     -23058
392093  feet/sec       YDOT =       -7048
344013  meter/sec
 ZDOT =      -8424
884778                 ZDOT =       -2576
657873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15535020
18                 X    =         4735074
15
 Y    =          28122
50  feet           Y    =            8571
74  meter
 Z    =       15613565
79                 Z    =         4759014
85
 XDOT =       8475
790272                 XDOT =        2583
420875
 YDOT =      21139
070000  feet/sec       YDOT =        6443
188536  meter/sec
 ZDOT =      -8458
945248                 ZDOT =       -2578
286512


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   07316
42045244  
00020000  00000-0  20000-3 0  9102
2 25544  51
6376  59
5975 0002617 197
1555 162
9521 15
76043295 34161


Satellite: ISS
Catalog Number: 25544
Epoch time:      07316
42045244   =   yrday
fracday
Element set:     910
Inclination:       51
6376  deg
RA of node:        59
5975  deg
Eccentricity:     
0002617     
Arg of perigee:   197
1555  deg
Mean anomaly:     162
9521  deg
Mean motion:   15
76043295  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3416
Checksum:              295


Coasting Arc #12 (Orbit 3431)
---------------------------------------

Vector Time (GMT): 2007/317/09:03:21
019
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1503353
65                 A    =         6722558
22  meter
 Y    =        5892934
08  meter          E    =           
0012280
 Z    =        2854583
33                 I    =           51
90827
 XDOT =      -5682
114771                 Wp   =           91
58307
 YDOT =      -1030
605280  meter/sec      RA   =           54
10061  deg
 ZDOT =       5100
960981                 TA   =          301
09230
                                          MA   =          301
21274
                                          Ha   =            186
686  n
mi
                                          Hp   =            180
836

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4932262
63                 X    =         1423478
84
 Y    =       19333773
23  feet           Y    =         5909298
54  meter
 Z    =        9365430
86                 Z    =         2861693
38
 XDOT =     -18642
108829                 XDOT =       -5694
948238
 YDOT =      -3381
250918  feet/sec       YDOT =       -1094
218177  meter/sec
 ZDOT =      16735
436289                 ZDOT =        5073
325299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7264323
94                 X    =        -2214165
94
 Y    =      -18569661
86  feet           Y    =        -5660032
94  meter
 Z    =        9393112
00                 Z    =         2863020
54
 XDOT =      17658
048988                 XDOT =        5382
173332
 YDOT =       1535
857925  feet/sec       YDOT =         468
129496  meter/sec
 ZDOT =      16630
122879                 ZDOT =        5068
861454


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   07317
43493380  
00020000  00000-0  20000-3 0  9113
2 25544  51
6388  54
3715 0002647 203
3099 156
7945 15
76129580 34326


Satellite: ISS
Catalog Number: 25544
Epoch time:      07317
43493380   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:        54
3715  deg
Eccentricity:     
0002647     
Arg of perigee:   203
3099  deg
Mean anomaly:     156
7945  deg
Mean motion:   15
76129580  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3432
Checksum:              301

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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