Date: May 5th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 3907)
---------------------------------------

Vector Time (GMT): 2009/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6378125
61                 A    =         6734381
57  meter
 Y    =         547534
89  meter          E    =           
0002422
 Z    =       -2094187
56                 I    =           51
71108
 XDOT =      -2237
185169                 Wp   =          332
96413
 YDOT =       4841
275683  meter/sec      RA   =          169
94011  deg
 ZDOT =      -5543
255008                 TA   =          230
37238
                                          MA   =          230
39376
                                          Ha   =            192
878  n
mi
                                          Hp   =            187
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20925608
96                 X    =         6381702
21
 Y    =        1796374
32  feet           Y    =          618878
82  meter
 Z    =       -6870694
09                 Z    =        -2063193
69
 XDOT =      -7339
846356                 XDOT =       -2264
226505
 YDOT =      15883
450404  feet/sec       YDOT =        4816
106988  meter/sec
 ZDOT =     -18186
532178                 ZDOT =       -5554
189015

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16838688
34                 X    =         5132432
21
 Y    =      -12618172
36  feet           Y    =        -3846018
94  meter
 Z    =       -6749430
32                 Z    =        -2057226
36
 XDOT =       4257
015708                 XDOT =        1297
538388
 YDOT =      15439
754255  feet/sec       YDOT =        4706
037097  meter/sec
 ZDOT =     -18228
929095                 ZDOT =       -5556
177588


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   09124
52773644  
00010596  00000-0  82463-4 0  9004
2 25544  51
6405 170
7979 0008952 323
1581  36
8966 15
72579841 39087


Satellite: ISS
Catalog Number: 25544
Epoch time:      09124
52773644   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:       170
7979  deg
Eccentricity:     
0008952     
Arg of perigee:   323
1581  deg
Mean anomaly:      36
8966  deg
Mean motion:   15
72579841  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3908
Checksum:              341


Coasting Arc #2 (Orbit 3923)
---------------------------------------

Vector Time (GMT): 2009/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1025556
13                 A    =         6725241
16  meter
 Y    =       -4375271
48  meter          E    =           
0010729
 Z    =        5006703
37                 I    =           51
70872
 XDOT =       7440
098035                 Wp   =          358
60909
 YDOT =       -457
688393  meter/sec      RA   =          164
78658  deg
 ZDOT =      -1913
535664                 TA   =          109
91808
                                          MA   =          109
80247
                                          Ha   =            192
978  n
mi
                                          Hp   =            186
894

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3364685
48                 X    =         1050082
95
 Y    =      -14354565
22  feet           Y    =        -4363666
01  meter
 Z    =       16426192
16                 Z    =         5011745
14
 XDOT =      24409
770455                 XDOT =        7453
958749
 YDOT =      -1501
602339  feet/sec       YDOT =        -374
411362  meter/sec
 ZDOT =      -6278
004146                 ZDOT =       -1877
357523

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7338204
61                 X    =        -2236684
76
 Y    =      -12762758
30  feet           Y    =        -3890088
73  meter
 Z    =       16445582
80                 Z    =         5012613
64
 XDOT =      16007
493834                 XDOT =        4879
084121
 YDOT =     -17155
182406  feet/sec       YDOT =       -5228
899597  meter/sec
 ZDOT =      -6136
531407                 ZDOT =       -1870
414773


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   09125
54448985  
00010596  00000-0  82463-4 0  9015
2 25544  51
6395 165
5875 0009010 326
8429  33
2167 15
72605984 39249


Satellite: ISS
Catalog Number: 25544
Epoch time:      09125
54448985   =   yrday
fracday
Element set:     901
Inclination:       51
6395  deg
RA of node:       165
5875  deg
Eccentricity:     
0009010     
Arg of perigee:   326
8429  deg
Mean anomaly:      33
2167  deg
Mean motion:   15
72605984  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3924
Checksum:              334


Coasting Arc #3 (Orbit 3939)
---------------------------------------

Vector Time (GMT): 2009/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6469347
30                 A    =         6735649
32  meter
 Y    =        1355723
28  meter          E    =           
0017150
 Z    =        1235719
91                 I    =           51
77132
 XDOT =         84
753276                 Wp   =           26
49992
 YDOT =      -4973
964302  meter/sec      RA   =          159
69572  deg
 ZDOT =       5884
590096                 TA   =          347
02892
                                          MA   =          347
07298
                                          Ha   =            193
365  n
mi
                                          Hp   =            186
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21224892
73                 X    =        -6490029
42
 Y    =        4447911
01  feet           Y    =         1283263
59  meter
 Z    =        4054199
17                 Z    =         1204241
05
 XDOT =        278
061928                 XDOT =         111
779900
 YDOT =     -16318
780519  feet/sec       YDOT =       -4972
865547  meter/sec
 ZDOT =      19306
397953                 ZDOT =        5885
067383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12284019
61                 X    =        -3744169
18
 Y    =       17898751
69  feet           Y    =         5455539
52  meter
 Z    =        3931165
84                 Z    =         1198219
35
 XDOT =      -9851
835432                 XDOT =       -3002
839440
 YDOT =     -11014
009059  feet/sec       YDOT =       -3357
069961  meter/sec
 ZDOT =      19307
895214                 ZDOT =        5885
046461


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   09126
56123556  
00010596  00000-0  82463-4 0  9023
2 25544  51
6394 160
3766 0009110 332
5081  27
5598 15
72564437 39408


Satellite: ISS
Catalog Number: 25544
Epoch time:      09126
56123556   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:       160
3766  deg
Eccentricity:     
0009110     
Arg of perigee:   332
5081  deg
Mean anomaly:      27
5598  deg
Mean motion:   15
72564437  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3940
Checksum:              311


Coasting Arc #4 (Orbit 3954)
---------------------------------------

Vector Time (GMT): 2009/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         853709
81                 A    =         6724338
03  meter
 Y    =        4154531
90  meter          E    =           
0012514
 Z    =       -5226381
46                 I    =           51
76163
 XDOT =      -7175
493467                 Wp   =           59
15296
 YDOT =       2615
115419  meter/sec      RA   =          154
56069  deg
 ZDOT =        914
599970                 TA   =          219
50876
                                          MA   =          219
60005
                                          Ha   =            193
378  n
mi
                                          Hp   =            186
430

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2800885
20                 X    =          832579
03
 Y    =       13630354
00  feet           Y    =         4163960
65  meter
 Z    =      -17146920
80                 Z    =        -5222285
21
 XDOT =     -23541
645232                 XDOT =       -7208
645877
 YDOT =       8579
774997  feet/sec       YDOT =        2534
689461  meter/sec
 ZDOT =       3000
656071                 ZDOT =         879
660278

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11648809
16                 X    =         3550557
03
 Y    =        7648294
33  feet           Y    =         2331200
11  meter
 Z    =      -17130593
67                 Z    =        -5221404
95
 XDOT =     -10152
636660                 XDOT =       -3094
523654
 YDOT =      21820
145206  feet/sec       YDOT =        6650
780259  meter/sec
 ZDOT =       2864
165380                 ZDOT =         872
997608


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   09127
51442051  
00010596  00000-0  82463-4 0  9034
2 25544  51
6399 155
4916 0009059 334
9085  25
1629 15
72601246 39552


Satellite: ISS
Catalog Number: 25544
Epoch time:      09127
51442051   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       155
4916  deg
Eccentricity:     
0009059     
Arg of perigee:   334
9085  deg
Mean anomaly:      25
1629  deg
Mean motion:   15
72601246  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3955
Checksum:              316


Coasting Arc #5 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2009/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5937077
98                 A    =         6736008
27  meter
 Y    =       -3160024
50  meter          E    =           
0004619
 Z    =        -375931
30                 I    =           51
82618
 XDOT =       1942
741907                 Wp   =           91
08151
 YDOT =       4360
089993  meter/sec      RA   =          149
45715  deg
 ZDOT =      -6032
176242                 TA   =           92
98933
                                          MA   =           92
93647
                                          Ha   =            193
467  n
mi
                                          Hp   =            186
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19478602
29                 X    =         5973798
89
 Y    =      -10367534
45  feet           Y    =        -3093427
29  meter
 Z    =       -1233370
40                 Z    =         -346999
35
 XDOT =       6373
825153                 XDOT =        1923
146118
 YDOT =      14304
757194  feet/sec       YDOT =        4381
705690  meter/sec
 ZDOT =     -19790
604467                 ZDOT =       -6022
785512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6194155
26                 X    =         1887978
52
 Y    =      -21184901
46  feet           Y    =        -6457157
96  meter
 Z    =       -1120406
66                 Z    =         -341499
95
 XDOT =      13223
021203                 XDOT =        4030
376863
 YDOT =       4898
780051  feet/sec       YDOT =        1493
148160  meter/sec
 ZDOT =     -19753
554680                 ZDOT =       -6020
883466


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   09128
53114224  
00010596  00000-0  82463-4 0  9046
2 25544  51
6386 150
2803 0009019 339
6287  20
4515 15
72634258 39717


Satellite: ISS
Catalog Number: 25544
Epoch time:      09128
53114224   =   yrday
fracday
Element set:     904
Inclination:       51
6386  deg
RA of node:       150
2803  deg
Eccentricity:     
0009019     
Arg of perigee:   339
6287  deg
Mean anomaly:      20
4515  deg
Mean motion:   15
72634258  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3971
Checksum:              303


Coasting Arc #6 (Orbit 3986)
---------------------------------------

Vector Time (GMT): 2009/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2477935
49                 A    =         6723934
28  meter
 Y    =       -3338471
57  meter          E    =           
0008512
 Z    =        5284515
25                 I    =           51
80975
 XDOT =       6225
326538                 Wp   =          359
10661
 YDOT =      -4530
054483  meter/sec      RA   =          144
34124  deg
 ZDOT =         65
581551                 TA   =           90
32121
                                          MA   =           90
22367
                                          Ha   =            193
646  n
mi
                                          Hp   =            185
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8129709
61                 X    =        -2466091
73
 Y    =      -10952990
72  feet           Y    =        -3366115
53  meter
 Z    =       17337648
47                 Z    =         5272505
67
 XDOT =      20424
299666                 XDOT =        6275
201096
 YDOT =     -14862
383474  feet/sec       YDOT =       -4460
160392  meter/sec
 ZDOT =        215
162569                 ZDOT =          95
945582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13614628
08                 X    =        -4149738
64
 Y    =       -1528814
84  feet           Y    =         -465982
76  meter
 Z    =       17290427
01                 Z    =         5270122
15
 XDOT =       3090
819243                 XDOT =         942
081705
 YDOT =     -24061
600316  feet/sec       YDOT =       -7333
975776  meter/sec
 ZDOT =        333
650447                 ZDOT =         101
696656


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   09129
54785248  
00010596  00000-0  82463-4 0  9059
2 25544  51
6378 145
0687 0009082 343
7653  16
3217 15
72654861 39875


Satellite: ISS
Catalog Number: 25544
Epoch time:      09129
54785248   =   yrday
fracday
Element set:     905
Inclination:       51
6378  deg
RA of node:       145
0687  deg
Eccentricity:     
0009082     
Arg of perigee:   343
7653  deg
Mean anomaly:      16
3217  deg
Mean motion:   15
72654861  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3987
Checksum:              344


Coasting Arc #7 (Orbit 4001)
---------------------------------------

Vector Time (GMT): 2009/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4815655
64                 A    =         6735739
35  meter
 Y    =        4667275
82  meter          E    =           
0017938
 Z    =        -496169
39                 I    =           51
87397
 XDOT =      -3636
687550                 Wp   =           17
39440
 YDOT =      -3118
414266  meter/sec      RA   =          139
22528  deg
 ZDOT =       6035
155000                 TA   =          337
22363
                                          MA   =          337
30311
                                          Ha   =            193
610  n
mi
                                          Hp   =            185
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15799395
16                 X    =        -4865077
65
 Y    =       15312584
71  feet           Y    =         4613148
07  meter
 Z    =       -1627852
32                 Z    =         -519683
84
 XDOT =     -11931
389600                 XDOT =       -3630
864870
 YDOT =     -10231
017932  feet/sec       YDOT =       -3159
049913  meter/sec
 ZDOT =      19800
377298                 ZDOT =        6017
501449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         682519
59                 X    =          208031
97
 Y    =       21984616
48  feet           Y    =         6700911
10  meter
 Z    =       -1719548
22                 Z    =         -524118
30
 XDOT =     -14072
360619                 XDOT =       -4289
255517
 YDOT =       1962
578501  feet/sec       YDOT =         598
193927  meter/sec
 ZDOT =      19731
085855                 ZDOT =        6014
034969


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   09130
50100822  
00010596  00000-0  82463-4 0  9067
2 25544  51
6384 140
1841 0009010 347
0452  13
0477 15
72708326 40022


Satellite: ISS
Catalog Number: 25544
Epoch time:      09130
50100822   =   yrday
fracday
Element set:     906
Inclination:       51
6384  deg
RA of node:       140
1841  deg
Eccentricity:     
0009010     
Arg of perigee:   347
0452  deg
Mean anomaly:      13
0477  deg
Mean motion:   15
72708326  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4002
Checksum:              259


Coasting Arc #8 (Orbit 4017)
---------------------------------------

Vector Time (GMT): 2009/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3751160
94                 A    =         6724270
95  meter
 Y    =        2016615
16  meter          E    =           
0016969
 Z    =       -5216302
43                 I    =           51
85580
 XDOT =      -4686
744298                 Wp   =           49
31658
 YDOT =       6004
793791  meter/sec      RA   =          134
12907  deg
 ZDOT =      -1040
281438                 TA   =          210
72648
                                          MA   =          210
82594
                                          Ha   =            193
881  n
mi
                                          Hp   =            185
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12306958
45                 X    =         3753672
25
 Y    =        6616191
48  feet           Y    =         2058577
50  meter
 Z    =      -17113853
12                 Z    =        -5198072
67
 XDOT =     -15376
457671                 XDOT =       -4748
489005
 YDOT =      19700
767032  feet/sec       YDOT =        5952
038774  meter/sec
 ZDOT =      -3412
996843                 ZDOT =       -1063
199259

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13163170
25                 X    =         4012134
29
 Y    =       -4940398
02  feet           Y    =        -1505833
32  meter
 Z    =      -17042376
63                 Z    =        -5194516
40
 XDOT =       4280
375914                 XDOT =        1304
658578
 YDOT =      23584
020110  feet/sec       YDOT =        7188
409329  meter/sec
 ZDOT =      -3502
286023                 ZDOT =       -1067
496780


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   09131
51769681  
00010596  00000-0  82463-4 0  9074
2 25544  51
6376 134
9724 0009177 350
7949   9
3043 15
72673298 40183


Satellite: ISS
Catalog Number: 25544
Epoch time:      09131
51769681   =   yrday
fracday
Element set:     907
Inclination:       51
6376  deg
RA of node:       134
9724  deg
Eccentricity:     
0009177     
Arg of perigee:   350
7949  deg
Mean anomaly:       9
3043  deg
Mean motion:   15
72673298  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4018
Checksum:              337


Coasting Arc #9 (Orbit 4033)
---------------------------------------

Vector Time (GMT): 2009/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3312719
73                 A    =         6735057
32  meter
 Y    =       -5716445
78  meter          E    =           
0011444
 Z    =        1305085
08                 I    =           51
91207
 XDOT =       4771
181124                 Wp   =           78
93070
 YDOT =       1415
073052  meter/sec      RA   =          128
99881  deg
 ZDOT =      -5867
200405                 TA   =           86
81563
                                          MA   =           86
68469
                                          Ha   =            193
967  n
mi
                                          Hp   =            185
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10868503
05                 X    =         3370055
84
 Y    =      -18754743
38  feet           Y    =        -5679080
60  meter
 Z    =        4281775
18                 Z    =         1321317
02
 XDOT =      15653
481378                 XDOT =        4783
505060
 YDOT =       4642
628124  feet/sec       YDOT =        1468
496821  meter/sec
 ZDOT =     -19249
345160                 ZDOT =       -5843
991622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7264599
67                 X    =        -2214249
98
 Y    =      -20409446
56  feet           Y    =        -6220799
31  meter
 Z    =        4344932
59                 Z    =         1324335
45
 XDOT =      12260
028433                 XDOT =        3736
856666
 YDOT =      -8473
696719  feet/sec       YDOT =       -2582
782760  meter/sec
 ZDOT =     -19158
414437                 ZDOT =       -5839
484720


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   09132
53437367  
00010596  00000-0  82463-4 0  9081
2 25544  51
6372 129
7606 0009349 355
0699   5
0369 15
72720324 40346


Satellite: ISS
Catalog Number: 25544
Epoch time:      09132
53437367   =   yrday
fracday
Element set:     908
Inclination:       51
6372  deg
RA of node:       129
7606  deg
Eccentricity:     
0009349     
Arg of perigee:   355
0699  deg
Mean anomaly:       5
0369  deg
Mean motion:   15
72720324  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4034
Checksum:              317


Coasting Arc #10 (Orbit 4049)
---------------------------------------

Vector Time (GMT): 2009/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4464784
81                 A    =         6725038
90  meter
 Y    =        -398187
55  meter          E    =           
0007542
 Z    =        5007697
35                 I    =           51
89553
 XDOT =       2799
908270                 Wp   =           36
80623
 YDOT =      -6906
277383  meter/sec      RA   =          123
91978  deg
 ZDOT =       1951
607779                 TA   =           34
43729
                                          MA   =           34
38845
                                          Ha   =            194
202  n
mi
                                          Hp   =            184
959

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14648244
12                 X    =        -4484327
06
 Y    =       -1306389
59  feet           Y    =         -448225
25  meter
 Z    =       16429453
25                 Z    =         4985959
73
 XDOT =       9186
050755                 XDOT =        2867
446696
 YDOT =     -22658
390363  feet/sec       YDOT =       -6874
589786  meter/sec
 ZDOT =       6402
912661                 ZDOT =        1965
373055

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10364680
07                 X    =        -3159154
49
 Y    =       10566014
48  feet           Y    =         3220521
21  meter
 Z    =       16344338
11                 Z    =         4981754
26
 XDOT =     -10936
534415                 XDOT =       -3333
455690
 YDOT =     -20692
847890  feet/sec       YDOT =       -6307
180037  meter/sec
 ZDOT =       6456
350510                 ZDOT =        1967
895635


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   09133
55103961  
00010596  00000-0  82463-4 0  9095
2 25544  51
6369 124
5490 0009350 358
2263   1
8865 15
72712782 40502


Satellite: ISS
Catalog Number: 25544
Epoch time:      09133
55103961   =   yrday
fracday
Element set:     909
Inclination:       51
6369  deg
RA of node:       124
5490  deg
Eccentricity:     
0009350     
Arg of perigee:   358
2263  deg
Mean anomaly:       1
8865  deg
Mean motion:   15
72712782  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4050
Checksum:              307


Coasting Arc #11 (Orbit 4064)
---------------------------------------

Vector Time (GMT): 2009/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1534122
17                 A    =         6733842
04  meter
 Y    =        6204048
40  meter          E    =           
0014927
 Z    =       -2097569
41                 I    =           51
94119
 XDOT =      -5288
333969                 Wp   =           18
38260
 YDOT =        567
600335  meter/sec      RA   =          118
77968  deg
 ZDOT =       5571
101684                 TA   =          318
28567
                                          MA   =          318
39939
                                          Ha   =            194
186  n
mi
                                          Hp   =            184
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5033209
22                 X    =        -1593193
19
 Y    =       20354489
51  feet           Y    =         6186562
91  meter
 Z    =       -6881789
39                 Z    =        -2105165
00
 XDOT =     -17350
177064                 XDOT =       -5321
351483
 YDOT =       1862
205823  feet/sec       YDOT =         508
277859  meter/sec
 ZDOT =      18277
892664                 ZDOT =        5545
330675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12849922
96                 X    =         3916656
52
 Y    =       16556365
22  feet           Y    =         5046380
12  meter
 Z    =       -6911129
73                 Z    =        -2106512
34
 XDOT =      -8175
818925                 XDOT =       -2491
989608
 YDOT =      13899
744299  feet/sec       YDOT =        4236
642062  meter/sec
 ZDOT =      18177
040866                 ZDOT =        5540
362056


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   09134
50415261  
00010596  00000-0  82463-4 0  9102
2 25544  51
6371 119
6641 0009356   2
6725 357
4486 15
72736809 40658


Satellite: ISS
Catalog Number: 25544
Epoch time:      09134
50415261   =   yrday
fracday
Element set:     910
Inclination:       51
6371  deg
RA of node:       119
6641  deg
Eccentricity:     
0009356     
Arg of perigee:     2
6725  deg
Mean anomaly:     357
4486  deg
Mean motion:   15
72736809  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4065
Checksum:              310


Coasting Arc #12 (Orbit 4080)
---------------------------------------

Vector Time (GMT): 2009/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4625713
39                 A    =         6726295
68  meter
 Y    =       -1374423
73  meter          E    =           
0017178
 Z    =       -4701246
82                 I    =           51
92906
 XDOT =       -734
463140                 Wp   =           41
15854
 YDOT =       7120
737450  meter/sec      RA   =          113
71372  deg
 ZDOT =      -2797
558704                 TA   =          201
26610
                                          MA   =          201
33758
                                          Ha   =            194
285  n
mi
                                          Hp   =            184
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15176225
02                 X    =         4663576
53
 Y    =       -4509264
20  feet           Y    =        -1322484
13  meter
 Z    =      -15424038
11                 Z    =        -4678683
17
 XDOT =      -2409
655972                 XDOT =        -800
443748
 YDOT =      23361
999507  feet/sec       YDOT =        7112
155616  meter/sec
 ZDOT =      -9178
342205                 ZDOT =       -2801
286299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5693242
35                 X    =         1735300
27
 Y    =      -14864484
51  feet           Y    =        -4530694
88  meter
 Z    =      -15335785
36                 Z    =        -4674347
38
 XDOT =      16039
670439                 XDOT =        4888
891550
 YDOT =      15650
698048  feet/sec       YDOT =        4770
332765  meter/sec
 ZDOT =      -9192
487712                 ZDOT =       -2801
870255


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   09135
52079548  
00010596  00000-0  82463-4 0  9110
2 25544  51
6372 114
4518 0009396   5
9720 354
1553 15
72745130 40814


Satellite: ISS
Catalog Number: 25544
Epoch time:      09135
52079548   =   yrday
fracday
Element set:     911
Inclination:       51
6372  deg
RA of node:       114
4518  deg
Eccentricity:     
0009396     
Arg of perigee:     5
9720  deg
Mean anomaly:     354
1553  deg
Mean motion:   15
72745130  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4081
Checksum:              304

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

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

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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