Date: July 29th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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


213/08:19:49 531 2 0 3 3 3 3
N/A 1 7 0 0 189 2
000/00:05:39 061 -1 9 0 0 187 2

Coasting Arc #1 (Orbit 1227)
---------------------------------------

Vector Time (GMT): 2009/208/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3359922
62                 A    =         6721478
27  meter
 Y    =       -3115251
58  meter          E    =           
0005393
 Z    =        4919953
79                 I    =           51
95228
 XDOT =       2968
428083                 Wp   =          355
41244
 YDOT =      -6742
333676  meter/sec      RA   =          100
01516  deg
 ZDOT =      -2236
878023                 TA   =          116
26576
                                          MA   =          116
21033
                                          Ha   =            188
406  n
mi
                                          Hp   =            185
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11023368
19                 X    =        -3348737
68
 Y    =      -10220641
68  feet           Y    =        -3152762
00  meter
 Z    =       16141580
68                 Z    =         4903658
38
 XDOT =       9738
937281                 XDOT =        3054
467648
 YDOT =     -22120
517311  feet/sec       YDOT =       -6708
657749  meter/sec
 ZDOT =      -7338
838657                 ZDOT =       -2222
248988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14636109
18                 X    =        -4461086
08
 Y    =        3718881
27  feet           Y    =         1133515
01  meter
 Z    =       16077344
92                 Z    =         4900374
73
 XDOT =     -12900
332907                 XDOT =       -3932
021470
 YDOT =     -19218
453465  feet/sec       YDOT =       -5857
784616  meter/sec
 ZDOT =      -7281
675007                 ZDOT =       -2219
454542


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   09208
35632049  
00010596  00000-0  82463-4 0  9001
2 25544  51
6389 100
6175 0006191 287
8925  72
1563 15
74088899 12288


Satellite: ISS
Catalog Number: 25544
Epoch time:      09208
35632049   =   yrday
fracday
Element set:     900
Inclination:       51
6389  deg
RA of node:       100
6175  deg
Eccentricity:     
0006191     
Arg of perigee:   287
8925  deg
Mean anomaly:      72
1563  deg
Mean motion:   15
74088899  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1228
Checksum:              329


Coasting Arc #2 (Orbit 1243)
---------------------------------------

Vector Time (GMT): 2009/209/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2092495
75                 A    =         6730098
98  meter
 Y    =        6069056
72  meter          E    =           
0010434
 Z    =        1998710
20                 I    =           51
98598
 XDOT =      -4126
037971                 Wp   =           44
49627
 YDOT =      -3276
662750  meter/sec      RA   =           94
93770  deg
 ZDOT =       5619
635949                 TA   =          337
67091
                                          MA   =          337
71630
                                          Ha   =            188
529  n
mi
                                          Hp   =            185
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6865143
55                 X    =        -2169914
78
 Y    =       19911603
41  feet           Y    =         6045224
17  meter
 Z    =        6557448
16                 Z    =         1988357
35
 XDOT =     -13536
869985                 XDOT =       -4116
390130
 YDOT =     -10750
205874  feet/sec       YDOT =       -3322
749033  meter/sec
 ZDOT =      18437
125817                 ZDOT =        5599
614940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13180856
19                 X    =         4017524
97
 Y    =       16443702
14  feet           Y    =         5012040
41  meter
 Z    =        6517051
72                 Z    =         1986397
36
 XDOT =     -15164
284701                 XDOT =       -4622
073977
 YDOT =       4866
051677  feet/sec       YDOT =        1483
172551  meter/sec
 ZDOT =      18358
235151                 ZDOT =        5595
590074


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   09209
37208560  
00010596  00000-0  82463-4 0  9012
2 25544  51
6392  95
4000 0006204 291
1447  68
9053 15
74127956 12445


Satellite: ISS
Catalog Number: 25544
Epoch time:      09209
37208560   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:        95
4000  deg
Eccentricity:     
0006204     
Arg of perigee:   291
1447  deg
Mean anomaly:      68
9053  deg
Mean motion:   15
74127956  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1244
Checksum:              297


Coasting Arc #3 (Orbit 1258)
---------------------------------------

Vector Time (GMT): 2009/210/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3830733
49                 A    =         6721559
14  meter
 Y    =        2589984
08  meter          E    =           
0006045
 Z    =       -4883600
51                 I    =           51
95892
 XDOT =      -1810
810755                 Wp   =           97
61532
 YDOT =       7102
193924  meter/sec      RA   =           89
78810  deg
 ZDOT =       2347
863259                 TA   =          195
16532
                                          MA   =          195
18345
                                          Ha   =            188
817  n
mi
                                          Hp   =            185
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12568023
28                 X    =         3825210
67
 Y    =        8497323
11  feet           Y    =         2632791
18  meter
 Z    =      -16022311
37                 Z    =        -4865004
06
 XDOT =      -5940
980166                 XDOT =       -1901
499557
 YDOT =      23301
161167  feet/sec       YDOT =        7081
437084  meter/sec
 ZDOT =       7702
963449                 ZDOT =        2338
846781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13824441
47                 X    =         4213689
76
 Y    =       -6433236
11  feet           Y    =        -1960850
36  meter
 Z    =      -15949058
35                 Z    =        -4861272
99
 XDOT =      16367
605473                 XDOT =        4988
846148
 YDOT =      16176
306158  feet/sec       YDOT =        4930
538117  meter/sec
 ZDOT =       7667
861319                 ZDOT =        2337
164130


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   09210
32435685  
00010596  00000-0  82463-4 0  9020
2 25544  51
6397  90
5087 0006313 295
9313  64
1199 15
74120609 12599


Satellite: ISS
Catalog Number: 25544
Epoch time:      09210
32435685   =   yrday
fracday
Element set:     902
Inclination:       51
6397  deg
RA of node:        90
5087  deg
Eccentricity:     
0006313     
Arg of perigee:   295
9313  deg
Mean anomaly:      64
1199  deg
Mean motion:   15
74120609  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1259
Checksum:              309


Coasting Arc #4 (Orbit 1274)
---------------------------------------

Vector Time (GMT): 2009/211/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1076950
03                 A    =         6729817
84  meter
 Y    =       -6296235
60  meter          E    =           
0002083
 Z    =       -2114183
70                 I    =           51
98660
 XDOT =       4611
548073                 Wp   =          217
96426
 YDOT =       2656
643503  meter/sec      RA   =           84
71258  deg
 ZDOT =      -5561
367632                 TA   =          345
54001
                                          MA   =          345
54597
                                          Ha   =            188
883  n
mi
                                          Hp   =            185
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3533300
62                 X    =         1157545
83
 Y    =      -20656940
95  feet           Y    =        -6283741
64  meter
 Z    =       -6936298
23                 Z    =        -2108756
84
 XDOT =      15129
750895                 XDOT =        4608
514253
 YDOT =       8716
021992  feet/sec       YDOT =        2708
196191  meter/sec
 ZDOT =     -18245
956799                 ZDOT =       -5538
971930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16057406
83                 X    =        -4894297
60
 Y    =      -13477556
20  feet           Y    =        -4107959
13  meter
 Z    =       -6915259
97                 Z    =        -2107771
24
 XDOT =      14212
752406                 XDOT =        4332
046933
 YDOT =      -7614
534537  feet/sec       YDOT =       -2320
910127  meter/sec
 ZDOT =     -18157
760568                 ZDOT =       -5534
485421


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   09211
34010154  
00010596  00000-0  82463-4 0  9034
2 25544  51
6406  85
2915 0006360 300
2677  59
7856 15
74149125 12758


Satellite: ISS
Catalog Number: 25544
Epoch time:      09211
34010154   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:        85
2915  deg
Eccentricity:     
0006360     
Arg of perigee:   300
2677  deg
Mean anomaly:      59
7856  deg
Mean motion:   15
74149125  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1275
Checksum:              292


Coasting Arc #5 (Orbit 1290)
---------------------------------------

Vector Time (GMT): 2009/212/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4215010
67                 A    =         6721705
72  meter
 Y    =       -2036188
20  meter          E    =           
0007227
 Z    =        4825784
98                 I    =           51
95561
 XDOT =        645
149458                 Wp   =            7
11408
 YDOT =      -7256
360141  meter/sec      RA   =           79
56161  deg
 ZDOT =      -2490
839450                 TA   =          107
18115
                                          MA   =          107
10202
                                          Ha   =            189
103  n
mi
                                          Hp   =            185
477

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13828775
17                 X    =        -4215371
00
 Y    =       -6680407
50  feet           Y    =        -2083325
53  meter
 Z    =       15832627
88                 Z    =         4805307
49
 XDOT =       2116
632080                 XDOT =         738
343317
 YDOT =     -23806
955842  feet/sec       YDOT =       -7248
624321  meter/sec
 ZDOT =      -8172
045441                 ZDOT =       -2487
479865

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12623732
68                 X    =        -3847713
72
 Y    =        8891049
25  feet           Y    =         2709991
81  meter
 Z    =       15752002
70                 Z    =         4801210
42
 XDOT =     -19075
828729                 XDOT =       -5814
312597
 YDOT =     -12585
701260  feet/sec       YDOT =       -3836
121744  meter/sec
 ZDOT =      -8159
171424                 ZDOT =       -2486
915450


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   09212
35583565  
00010596  00000-0  82463-4 0  9048
2 25544  51
6409  80
0747 0006368 304
1255  55
9304 15
74156124 12911


Satellite: ISS
Catalog Number: 25544
Epoch time:      09212
35583565   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:        80
0747  deg
Eccentricity:     
0006368     
Arg of perigee:   304
1255  deg
Mean anomaly:      55
9304  deg
Mean motion:   15
74156124  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1291
Checksum:              299


Coasting Arc #6 (Orbit 1306)
---------------------------------------

Vector Time (GMT): 2009/213/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -57319
35                 A    =         6729513
12  meter
 Y    =        6338137
15  meter          E    =           
0011743
 Z    =        2238490
53                 I    =           51
97557
 XDOT =      -5015
585398                 Wp   =           44
47390
 YDOT =      -1990
825359  meter/sec      RA   =           74
48674  deg
 ZDOT =       5499
414715                 TA   =          340
53331
                                          MA   =          340
57812
                                          Ha   =            189
260  n
mi
                                          Hp   =            185
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -188055
62                 X    =         -139063
28
 Y    =       20794413
23  feet           Y    =         6337038
83  meter
 Z    =        7344129
05                 Z    =         2238014
34
 XDOT =     -16455
332672                 XDOT =       -5019
665733
 YDOT =      -6531
579262  feet/sec       YDOT =       -2046
936094  meter/sec
 ZDOT =      18042
699197                 ZDOT =        5475
039111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18213409
16                 X    =         5551447
11
 Y    =       10036831
72  feet           Y    =         3059226
31  meter
 Z    =        7342544
11                 Z    =         2238007
44
 XDOT =     -12853
989189                 XDOT =       -3917
895905
 YDOT =      10174
753410  feet/sec       YDOT =        3101
264839  meter/sec
 ZDOT =      17946
742391                 ZDOT =        5470
167081


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   09213
37155849  
00010596  00000-0  82463-4 0  9052
2 25544  51
6410  74
8569 0006447 308
3071  51
7512 15
74171157 13072


Satellite: ISS
Catalog Number: 25544
Epoch time:      09213
37155849   =   yrday
fracday
Element set:     905
Inclination:       51
6410  deg
RA of node:        74
8569  deg
Eccentricity:     
0006447     
Arg of perigee:   308
3071  deg
Mean anomaly:      51
7512  deg
Mean motion:   15
74171157  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1307
Checksum:              304


Coasting Arc #7 (Orbit 1306)
---------------------------------------

Vector Time (GMT): 2009/213/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2049134
61                 A    =         6725782
45  meter
 Y    =       -4844028
91  meter          E    =           
0004898
 Z    =       -4195863
52                 I    =           51
95816
 XDOT =       4435
904124                 Wp   =            9
90597
 YDOT =       5084
827017  meter/sec      RA   =           74
30525  deg
 ZDOT =      -3699
872942                 TA   =          222
45183
                                          MA   =          222
48972
                                          Ha   =            189
179  n
mi
                                          Hp   =            187
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6722882
59                 X    =         2123531
58
 Y    =      -15892483
30  feet           Y    =        -4820697
77  meter
 Z    =      -13765956
43                 Z    =        -4185728
85
 XDOT =      14553
491219                 XDOT =        4396
688136
 YDOT =      16682
503336  feet/sec       YDOT =        5134
213103  meter/sec
 ZDOT =     -12138
690754                 ZDOT =       -3678
418168

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13586171
28                 X    =        -4141065
01
 Y    =      -10689896
31  feet           Y    =        -3258280
39  meter
 Z    =      -13726317
75                 Z    =        -4183781
65
 XDOT =      19123
227803                 XDOT =        5828
759834
 YDOT =      -8809
159502  feet/sec       YDOT =       -2685
031816  meter/sec
 ZDOT =     -12054
080708                 ZDOT =       -3674
083800


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   09213
37156423  
00010596  00000-0  82463-4 0  9062
2 25544  51
6421  74
8575 0007036 286
9954  73
0438 15
73575209 13076


Satellite: ISS
Catalog Number: 25544
Epoch time:      09213
37156423   =   yrday
fracday
Element set:     906
Inclination:       51
6421  deg
RA of node:        74
8575  deg
Eccentricity:     
0007036     
Arg of perigee:   286
9954  deg
Mean anomaly:      73
0438  deg
Mean motion:   15
73575209  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1307
Checksum:              318


Coasting Arc #8 (Orbit 1322)
---------------------------------------

Vector Time (GMT): 2009/214/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4297864
47                 A    =         6728670
06  meter
 Y    =       -3961107
22  meter          E    =           
0006466
 Z    =        3330702
93                 I    =           51
95798
 XDOT =       1721
738655                 Wp   =           70
37502
 YDOT =      -5838
743500  meter/sec      RA   =           69
14555  deg
 ZDOT =      -4712
667620                 TA   =           70
67356
                                          MA   =           70
60365
                                          Ha   =            189
402  n
mi
                                          Hp   =            187
090

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14100605
21                 X    =        -4269430
97
 Y    =      -12995758
60  feet           Y    =        -4009009
90  meter
 Z    =       10927503
05                 Z    =         3309892
79
 XDOT =       5648
748868                 XDOT =        1809
793455
 YDOT =     -19155
982610  feet/sec       YDOT =       -5818
997075  meter/sec
 ZDOT =     -15461
507938                 ZDOT =       -4704
090394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16043047
09                 X    =        -4889920
75
 Y    =       10588833
19  feet           Y    =         3227476
36  meter
 Z    =       10845477
57                 Z    =         3305701
56
 XDOT =     -16420
101060                 XDOT =       -5004
846803
 YDOT =      -9043
867088  feet/sec       YDOT =       -2756
570688  meter/sec
 ZDOT =     -15428
032604                 ZDOT =       -4702
464338


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   09214
38767730  
00010596  00000-0  82463-4 0  9074
2 25544  51
6417  69
6430 0007058 290
5559  69
4846 15
73563841 13238


Satellite: ISS
Catalog Number: 25544
Epoch time:      09214
38767730   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:        69
6430  deg
Eccentricity:     
0007058     
Arg of perigee:   290
5559  deg
Mean anomaly:      69
4846  deg
Mean motion:   15
73563841  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1323
Checksum:              332


Coasting Arc #9 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2009/215/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -941823
46                 A    =         6726293
75  meter
 Y    =        5294158
31  meter          E    =           
0004115
 Z    =        4036824
58                 I    =           51
93893
 XDOT =      -5328
680918                 Wp   =           80
63232
 YDOT =      -3940
405109  meter/sec      RA   =           64
08517  deg
 ZDOT =       3921
770479                 TA   =          329
05392
                                          MA   =          329
07816
                                          Ha   =            189
692  n
mi
                                          Hp   =            186
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3089971
97                 X    =        -1020563
44
 Y    =       17369285
80  feet           Y    =         5283185
56  meter
 Z    =       13244175
13                 Z    =         4032058
65
 XDOT =     -17482
548942                 XDOT =       -5303
273492
 YDOT =     -12927
838285  feet/sec       YDOT =       -3999
851939  meter/sec
 ZDOT =      12866
701048                 ZDOT =        3895
945479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16205578
22                 X    =         4939460
24
 Y    =        7007801
83  feet           Y    =         2135978
00  meter
 Z    =       13225662
14                 Z    =         4031181
82
 XDOT =     -16047
608881                 XDOT =       -4891
311187
 YDOT =      13002
363987  feet/sec       YDOT =        3963
120543  meter/sec
 ZDOT =      12764
948877                 ZDOT =        3890
756418


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   09215
40377915  
00010596  00000-0  82463-4 0  9081
2 25544  51
6421  64
4276 0007115 295
1104  64
9320 15
73583766 13397


Satellite: ISS
Catalog Number: 25544
Epoch time:      09215
40377915   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:        64
4276  deg
Eccentricity:     
0007115     
Arg of perigee:   295
1104  deg
Mean anomaly:      64
9320  deg
Mean motion:   15
73583766  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1339
Checksum:              308


Coasting Arc #10 (Orbit 1353)
---------------------------------------

Vector Time (GMT): 2009/216/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4954543
51                 A    =         6727982
79  meter
 Y    =        2886338
85  meter          E    =           
0003309
 Z    =       -3515552
07                 I    =           51
93102
 XDOT =       -402
514360                 Wp   =          338
16331
 YDOT =       6210
438744  meter/sec      RA   =           58
92222  deg
 ZDOT =       4533
270637                 TA   =          340
23657
                                          MA   =          340
24939
                                          Ha   =            189
921  n
mi
                                          Hp   =            186
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16255064
02                 X    =         4938977
30
 Y    =        9469615
65  feet           Y    =         2941656
78  meter
 Z    =      -11533963
48                 Z    =        -3491520
92
 XDOT =      -1320
585169                 XDOT =        -493
951977
 YDOT =      20375
455197  feet/sec       YDOT =        6205
425876  meter/sec
 ZDOT =      14872
935161                 ZDOT =        4531
093799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12672183
86                 X    =         3862481
64
 Y    =      -13981808
79  feet           Y    =        -4261655
32  meter
 Z    =      -11439310
28                 Z    =        -3486701
77
 XDOT =      18611
820328                 XDOT =        5672
882836
 YDOT =       4711
370970  feet/sec       YDOT =        1436
025872  meter/sec
 ZDOT =      14864
644362                 ZDOT =        4530
743601


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   09216
35636468  
00010596  00000-0  82463-4 0  9098
2 25544  51
6425  59
5385 0007230 298
8047  61
2396 15
73615189 13546


Satellite: ISS
Catalog Number: 25544
Epoch time:      09216
35636468   =   yrday
fracday
Element set:     909
Inclination:       51
6425  deg
RA of node:        59
5385  deg
Eccentricity:     
0007230     
Arg of perigee:   298
8047  deg
Mean anomaly:      61
2396  deg
Mean motion:   15
73615189  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1354
Checksum:              334


Coasting Arc #11 (Orbit 1369)
---------------------------------------

Vector Time (GMT): 2009/217/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -235054
44                 A    =         6726674
51  meter
 Y    =       -5488097
93  meter          E    =           
0005830
 Z    =       -3887165
88                 I    =           51
91056
 XDOT =       5934
450344                 Wp   =             
82362
 YDOT =       2662
007205  meter/sec      RA   =           53
86084  deg
 ZDOT =      -4111
583722                 TA   =          226
39353
                                          MA   =          226
44192
                                          Ha   =            189
987  n
mi
                                          Hp   =            186
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -771175
97                 X    =         -154785
39
 Y    =      -18005570
65  feet           Y    =        -5490277
32  meter
 Z    =      -12753168
90                 Z    =        -3888113
24
 XDOT =      19469
981445                 XDOT =        5924
215152
 YDOT =       8733
619438  feet/sec       YDOT =        2728
312823  meter/sec
 ZDOT =     -13489
447908                 ZDOT =       -4082
779437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17804059
71                 X    =        -5426677
40
 Y    =       -2776608
72  feet           Y    =         -846310
34  meter
 Z    =      -12757135
48                 Z    =        -3888374
89
 XDOT =      12125
078572                 XDOT =        3695
723949
 YDOT =     -16206
988640  feet/sec       YDOT =       -4939
890137  meter/sec
 ZDOT =     -13376
026375                 ZDOT =       -4077
012839


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   09217
37244563  
00010596  00000-0  82463-4 0  9104
2 25544  51
6427  54
3236 0007382 302
5596  57
4854 15
73626218 13705


Satellite: ISS
Catalog Number: 25544
Epoch time:      09217
37244563   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:        54
3236  deg
Eccentricity:     
0007382     
Arg of perigee:   302
5596  deg
Mean anomaly:      57
4854  deg
Mean motion:   15
73626218  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1370
Checksum:              309


Coasting Arc #12 (Orbit 1385)
---------------------------------------

Vector Time (GMT): 2009/218/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5363186
94                 A    =         6727427
69  meter
 Y    =       -1748875
73  meter          E    =           
0008135
 Z    =        3665186
81                 I    =           51
89425
 XDOT =       -948
313644                 Wp   =           47
96114
 YDOT =      -6267
726879  meter/sec      RA   =           48
69478  deg
 ZDOT =      -4366
858971                 TA   =           88
21890
                                          MA   =           88
12573
                                          Ha   =            190
184  n
mi
                                          Hp   =            186
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17595757
69                 X    =        -5361036
54
 Y    =       -5737781
26  feet           Y    =        -1808838
23  meter
 Z    =       12024891
12                 Z    =         3639138
13
 XDOT =      -3111
265235                 XDOT =        -856
943418
 YDOT =     -20563
408396  feet/sec       YDOT =       -6277
820329  meter/sec
 ZDOT =     -14326
965129                 ZDOT =       -4371
244236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8745178
86                 X    =        -2665530
52
 Y    =       16386283
72  feet           Y    =         4994539
28  meter
 Z    =       11922347
99                 Z    =         3633931
67
 XDOT =     -19581
102046                 XDOT =       -5968
319904
 YDOT =         14
217482  feet/sec       YDOT =           4
333488  meter/sec
 ZDOT =     -14344
489761                 ZDOT =       -4372
200479


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   09218
38851662  
00010596  00000-0  82463-4 0  9111
2 25544  51
6424  49
1082 0007363 307
4252  52
6241 15
73652949 13869


Satellite: ISS
Catalog Number: 25544
Epoch time:      09218
38851662   =   yrday
fracday
Element set:     911
Inclination:       51
6424  deg
RA of node:        49
1082  deg
Eccentricity:     
0007363     
Arg of perigee:   307
4252  deg
Mean anomaly:      52
6241  deg
Mean motion:   15
73652949  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1386
Checksum:              310


Coasting Arc #13 (Orbit 1401)
---------------------------------------

Vector Time (GMT): 2009/219/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1411290
54                 A    =         6727081
16  meter
 Y    =        5403341
39  meter          E    =           
0006943
 Z    =        3742307
14                 I    =           51
87275
 XDOT =      -6264
293272                 Wp   =           59
17995
 YDOT =      -1330
083780  meter/sec      RA   =           43
62986  deg
 ZDOT =       4280
477311                 TA   =          345
86540
                                          MA   =          345
88482
                                          Ha   =            190
391  n
mi
                                          Hp   =            186
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4630218
30                 X    =         1332585
47
 Y    =       17727498
01  feet           Y    =         5418683
05  meter
 Z    =       12277910
58                 Z    =         3748972
11
 XDOT =     -20552
143281                 XDOT =       -6269
747848
 YDOT =      -4363
791929  feet/sec       YDOT =       -1400
165455  meter/sec
 ZDOT =      14043
560731                 ZDOT =        4250
032669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18225845
04                 X    =         5555237
57
 Y    =       -1694510
68  feet           Y    =         -516486
85  meter
 Z    =       12304365
14                 Z    =         3750370
49
 XDOT =      -7698
803257                 XDOT =       -2346
595233
 YDOT =      18353
429495  feet/sec       YDOT =        5594
125310  meter/sec
 ZDOT =      13923
744588                 ZDOT =        4243
957350


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   09219
40457698  
00010596  00000-0  82463-4 0  9127
2 25544  51
6426  43
8921 0007439 311
6324  48
4201 15
73639993 14027


Satellite: ISS
Catalog Number: 25544
Epoch time:      09219
40457698   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:        43
8921  deg
Eccentricity:     
0007439     
Arg of perigee:   311
6324  deg
Mean anomaly:      48
4201  deg
Mean motion:   15
73639993  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1402
Checksum:              314


Coasting Arc #14 (Orbit 1416)
---------------------------------------

Vector Time (GMT): 2009/220/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5516128
09                 A    =         6726904
56  meter
 Y    =         563586
77  meter          E    =           
0003875
 Z    =       -3805869
51                 I    =           51
84970
 XDOT =       2282
520211                 Wp   =            6
57986
 YDOT =       6032
011952  meter/sec      RA   =           38
46048  deg
 ZDOT =       4205
654289                 TA   =          307
39729
                                          MA   =          307
43256
                                          Ha   =            190
605  n
mi
                                          Hp   =            186
041

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18097533
11                 X    =         5527903
92
 Y    =        1849037
96  feet           Y    =          625337
28  meter
 Z    =      -12486448
53                 Z    =        -3779043
98
 XDOT =       7488
583368                 XDOT =        2194
469603
 YDOT =      19790
065460  feet/sec       YDOT =        6057
044022  meter/sec
 ZDOT =      13798
078376                 ZDOT =        4216
528854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4397918
92                 X    =         1340485
69
 Y    =      -17726323
61  feet           Y    =        -5402983
44  meter
 Z    =      -12380904
79                 Z    =        -3773699
78
 XDOT =      19345
934063                 XDOT =        5896
640702
 YDOT =      -4857
870825  feet/sec       YDOT =       -1480
679028  meter/sec
 ZDOT =      13841
118288                 ZDOT =        4218
772854


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   09220
35712211  
00010596  00000-0  82463-4 0  9139
2 25544  51
6424  39
0025 0007638 314
1851  45
8684 15
73675163 14172


Satellite: ISS
Catalog Number: 25544
Epoch time:      09220
35712211   =   yrday
fracday
Element set:     913
Inclination:       51
6424  deg
RA of node:        39
0025  deg
Eccentricity:     
0007638     
Arg of perigee:   314
1851  deg
Mean anomaly:      45
8684  deg
Mean motion:   15
73675163  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1417
Checksum:              291


Coasting Arc #15 (Orbit 1432)
---------------------------------------

Vector Time (GMT): 2009/221/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2542318
48                 A    =         6727385
27  meter
 Y    =       -5077931
28  meter          E    =           
0006592
 Z    =       -3613020
47                 I    =           51
82716
 XDOT =       6299
293163                 Wp   =            1
98346
 YDOT =         -6
579719  meter/sec      RA   =           33
39310  deg
 ZDOT =      -4417
067227                 TA   =          221
08055
                                          MA   =          221
13021
                                          Ha   =            190
633  n
mi
                                          Hp   =            185
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8340939
90                 X    =        -2467796
04
 Y    =      -16659879
53  feet           Y    =        -5105944
26  meter
 Z    =      -11853741
70                 Z    =        -3625189
94
 XDOT =      20666
972321                 XDOT =        6320
355617
 YDOT =        -21
587005  feet/sec       YDOT =          63
980486  meter/sec
 ZDOT =     -14491
690377                 ZDOT =       -4386
414471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17558822
37                 X    =        -5351929
06
 Y    =        6137445
76  feet           Y    =         1870693
47  meter
 Z    =      -11901830
66                 Z    =        -3627677
98
 XDOT =       3004
475569                 XDOT =         915
764153
 YDOT =     -19312
460738  feet/sec       YDOT =       -5886
438033  meter/sec
 ZDOT =     -14371
121182                 ZDOT =       -4380
317736


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   09221
37316089  
00010596  00000-0  82463-4 0  9146
2 25544  51
6422  33
7872 0007691 317
4348  42
6218 15
73675857 14333


Satellite: ISS
Catalog Number: 25544
Epoch time:      09221
37316089   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:        33
7872  deg
Eccentricity:     
0007691     
Arg of perigee:   317
4348  deg
Mean anomaly:      42
6218  deg
Mean motion:   15
73675857  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1433
Checksum:              319


Coasting Arc #16 (Orbit 1448)
---------------------------------------

Vector Time (GMT): 2009/222/08:22:39
061
Vector Time (MET): N/A
Weight (LBS)     : 672427
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5444273
52                 A    =         6726345
27  meter
 Y    =         570113
18  meter          E    =           
0010209
 Z    =        3909702
50                 I    =           51
79911
 XDOT =      -3507
599174                 Wp   =           37
77732
 YDOT =      -5514
384404  meter/sec      RA   =           28
22015  deg
 ZDOT =      -4066
756039                 TA   =           94
52606
                                          MA   =           94
40943
                                          Ha   =            190
790  n
mi
                                          Hp   =            185
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17861789
76                 X    =        -5469236
48
 Y    =        1870450
07  feet           Y    =          509092
51  meter
 Z    =       12827107
95                 Z    =         3883193
79
 XDOT =     -11507
871305                 XDOT =       -3425
920272
 YDOT =     -18091
812350  feet/sec       YDOT =       -5553
151714  meter/sec
 ZDOT =     -13342
375456                 ZDOT =       -4083
597474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -62453
12                 X    =          -19035
71
 Y    =       18033345
79  feet           Y    =         5496563
80  meter
 Z    =       12722867
38                 Z    =         3877929
98
 XDOT =     -17897
834707                 XDOT =       -5455
260019
 YDOT =       9429
673545  feet/sec       YDOT =        2874
164497  meter/sec
 ZDOT =     -13408
854974                 ZDOT =       -4087
018996


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   09222
38918749  
00010596  00000-0  82463-4 0  9150
2 25544  51
6428  28
5714 0007850 322
2617  37
7994 15
73753564 14491


Satellite: ISS
Catalog Number: 25544
Epoch time:      09222
38918749   =   yrday
fracday
Element set:     915
Inclination:       51
6428  deg
RA of node:        28
5714  deg
Eccentricity:     
0007850     
Arg of perigee:   322
2617  deg
Mean anomaly:      37
7994  deg
Mean motion:   15
73753564  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1449
Checksum:              341

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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