Date: September 23rd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2112)
---------------------------------------

Vector Time (GMT): 2009/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2297990
96                 A    =         6720134
64  meter
 Y    =       -3723243
83  meter          E    =           
0013621
 Z    =        5091879
37                 I    =           51
67068
 XDOT =       7189
083305                 Wp   =          118
44233
 YDOT =      -2319
904816  meter/sec      RA   =          171
38182  deg
 ZDOT =       1538
652669                 TA   =          316
76478
                                          MA   =          316
87162
                                          Ha   =            192
855  n
mi
                                          Hp   =            180
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7539340
43                 X    =        -2280922
03
 Y    =      -12215366
91  feet           Y    =        -3748845
54  meter
 Z    =       16705640
98                 Z    =         5080757
27
 XDOT =      23586
231314                 XDOT =        7207
015956
 YDOT =      -7611
236274  feet/sec       YDOT =       -2239
411883  meter/sec
 ZDOT =       5048
073060                 ZDOT =        1573
621485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7578803
65                 X    =         2310019
35
 Y    =       12251066
29  feet           Y    =         3734125
01  meter
 Z    =       16661584
35                 Z    =         5078450
91
 XDOT =     -22698
746496                 XDOT =       -6918
577932
 YDOT =       6947
058199  feet/sec       YDOT =        2117
463339  meter/sec
 ZDOT =       5185
652392                 ZDOT =        1580
586849


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   09264
55031164  
00020000  00000-0  20000-3 0  9005
2 25544  51
6398 172
1370 0008788 113
9736 246
2355 15
74277084 21135


Satellite: ISS
Catalog Number: 25544
Epoch time:      09264
55031164   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:       172
1370  deg
Eccentricity:     
0008788     
Arg of perigee:   113
9736  deg
Mean anomaly:     246
2355  deg
Mean motion:   15
74277084  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2113
Checksum:              292


Coasting Arc #2 (Orbit 2127)
---------------------------------------

Vector Time (GMT): 2009/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6116416
70                 A    =         6730640
32  meter
 Y    =        2515475
96  meter          E    =           
0013629
 Z    =       -1250855
54                 I    =           51
73593
 XDOT =      -2862
143907                 Wp   =           76
98662
 YDOT =      -4067
245340  meter/sec      RA   =          166
22364  deg
 ZDOT =       5872
457590                 TA   =          269
32200
                                          MA   =          269
47817
                                          Ha   =            192
707  n
mi
                                          Hp   =            180
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20066983
91                 X    =        -6138014
07
 Y    =        8252873
89  feet           Y    =         2446957
77  meter
 Z    =       -4103856
75                 Z    =        -1280622
13
 XDOT =      -9390
235916                 XDOT =       -2844
978331
 YDOT =     -13343
980773  feet/sec       YDOT =       -4099
155258  meter/sec
 ZDOT =      19266
593144                 ZDOT =        5858
594969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19938199
69                 X    =         6077163
27
 Y    =       -8502189
32  feet           Y    =        -2591467
30  meter
 Z    =       -4220945
48                 Z    =        -1286544
18
 XDOT =       9048
162830                 XDOT =        2757
880031
 YDOT =      11770
177211  feet/sec       YDOT =        3587
550014  meter/sec
 ZDOT =      19211
718889                 ZDOT =        5855
731917


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   09265
50249405  
00020000  00000-0  20000-3 0  9011
2 25544  51
6400 167
2450 0008753 117
1369 243
0688 15
74283601 21285


Satellite: ISS
Catalog Number: 25544
Epoch time:      09265
50249405   =   yrday
fracday
Element set:     901
Inclination:       51
6400  deg
RA of node:       167
2450  deg
Eccentricity:     
0008753     
Arg of perigee:   117
1369  deg
Mean anomaly:     243
0688  deg
Mean motion:   15
74283601  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2128
Checksum:              278


Coasting Arc #3 (Orbit 2143)
---------------------------------------

Vector Time (GMT): 2009/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2663143
02                 A    =         6719757
00  meter
 Y    =        3397796
67  meter          E    =           
0021509
 Z    =       -5167482
02                 I    =           51
72844
 XDOT =      -6781
798832                 Wp   =           95
63816
 YDOT =       3384
260456  meter/sec      RA   =          161
11517  deg
 ZDOT =      -1276
442674                 TA   =          162
18730
                                          MA   =          162
11178
                                          Ha   =            192
618  n
mi
                                          Hp   =            180
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8737345
87                 X    =         2650053
39
 Y    =       11147626
87  feet           Y    =         3427504
16  meter
 Z    =      -16953681
18                 Z    =        -5154576
19
 XDOT =     -22249
996167                 XDOT =       -6812
937359
 YDOT =      11103
216720  feet/sec       YDOT =        3308
248247  meter/sec
 ZDOT =      -4187
804049                 ZDOT =       -1309
464855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9162953
51                 X    =        -2792868
23
 Y    =      -10880251
44  feet           Y    =        -3316300
64  meter
 Z    =      -16902618
57                 Z    =        -5151918
14
 XDOT =      21092
546194                 XDOT =        6429
008080
 YDOT =     -11089
567429  feet/sec       YDOT =       -3380
100152  meter/sec
 ZDOT =      -4317
676432                 ZDOT =       -1316
027777


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   09266
51813764  
00020000  00000-0  20000-3 0  9029
2 25544  51
6403 162
0265 0008702 120
7187 239
4835 15
74323399 21447


Satellite: ISS
Catalog Number: 25544
Epoch time:      09266
51813764   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       162
0265  deg
Eccentricity:     
0008702     
Arg of perigee:   120
7187  deg
Mean anomaly:     239
4835  deg
Mean motion:   15
74323399  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2144
Checksum:              288


Coasting Arc #4 (Orbit 2159)
---------------------------------------

Vector Time (GMT): 2009/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5714666
38                 A    =         6730892
89  meter
 Y    =       -3396175
74  meter          E    =           
0022516
 Z    =         983590
00                 I    =           51
79346
 XDOT =       3229
230106                 Wp   =          124
93699
 YDOT =       3686
878743  meter/sec      RA   =          155
96523  deg
 ZDOT =      -5948
944778                 TA   =           44
32795
                                          MA   =           44
14788
                                          Ha   =            192
625  n
mi
                                          Hp   =            180
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18748905
46                 X    =         5747440
12
 Y    =      -11142308
85  feet           Y    =        -3332087
71  meter
 Z    =        3227001
30                 Z    =         1011431
83
 XDOT =      10594
586961                 XDOT =        3216
662014
 YDOT =      12096
058867  feet/sec       YDOT =        3722
919514  meter/sec
 ZDOT =     -19517
535362                 ZDOT =       -5933
287595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18187038
48                 X    =        -5543409
33
 Y    =       12007729
68  feet           Y    =         3659956
01  meter
 Z    =        3336480
06                 Z    =         1016959
12
 XDOT =     -10387
689925                 XDOT =       -3166
167889
 YDOT =     -10254
418217  feet/sec       YDOT =       -3125
546673  meter/sec
 ZDOT =     -19455
611772                 ZDOT =       -5930
070468


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   09267
53376562  
00020000  00000-0  20000-3 0  9033
2 25544  51
6400 156
8081 0008769 125
4505 234
7478 15
74296896 21600


Satellite: ISS
Catalog Number: 25544
Epoch time:      09267
53376562   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:       156
8081  deg
Eccentricity:     
0008769     
Arg of perigee:   125
4505  deg
Mean anomaly:     234
7478  deg
Mean motion:   15
74296896  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2160
Checksum:              315


Coasting Arc #5 (Orbit 2175)
---------------------------------------

Vector Time (GMT): 2009/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2968092
77                 A    =         6719399
52  meter
 Y    =       -3034542
98  meter          E    =           
0012245
 Z    =        5201614
23                 I    =           51
78246
 XDOT =       6256
656709                 Wp   =          127
39885
 YDOT =      -4390
268829  meter/sec      RA   =          150
85595  deg
 ZDOT =        999
998428                 TA   =          313
04586
                                          MA   =          313
14833
                                          Ha   =            192
516  n
mi
                                          Hp   =            180
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9737837
17                 X    =        -2959208
10
 Y    =       -9955849
68  feet           Y    =        -3067684
19  meter
 Z    =       17065663
49                 Z    =         5187216
74
 XDOT =      20527
088939                 XDOT =        6300
426591
 YDOT =     -14403
769125  feet/sec       YDOT =       -4320
058468  meter/sec
 ZDOT =       3280
834736                 ZDOT =        1030
499892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10454550
18                 X    =         3186546
89
 Y    =        9305181
82  feet           Y    =         2836219
42  meter
 Z    =       17008740
63                 Z    =         5184264
15
 XDOT =     -18864
587000                 XDOT =       -5749
926118
 YDOT =      14925
049821  feet/sec       YDOT =        4549
155185  meter/sec
 ZDOT =       3400
745682                 ZDOT =        1036
547284


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   09268
54937389  
00020000  00000-0  20000-3 0  9046
2 25544  51
6402 151
5897 0008577 128
8354 231
3576 15
74369118 21762


Satellite: ISS
Catalog Number: 25544
Epoch time:      09268
54937389   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       151
5897  deg
Eccentricity:     
0008577     
Arg of perigee:   128
8354  deg
Mean anomaly:     231
3576  deg
Mean motion:   15
74369118  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2176
Checksum:              330


Coasting Arc #6 (Orbit 2190)
---------------------------------------

Vector Time (GMT): 2009/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5176471
31                 A    =         6730766
82  meter
 Y    =        4236710
71  meter          E    =           
0013089
 Z    =        -743944
56                 I    =           51
84680
 XDOT =      -3537
654490                 Wp   =           79
96692
 YDOT =      -3286
050670  meter/sec      RA   =          145
71359  deg
 ZDOT =       5992
749322                 TA   =          271
95261
                                          MA   =          272
10250
                                          Ha   =            192
259  n
mi
                                          Hp   =            180
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16983173
58                 X    =        -5219848
24
 Y    =       13899969
52  feet           Y    =         4178581
81  meter
 Z    =       -2440762
98                 Z    =         -769197
42
 XDOT =     -11606
477986                 XDOT =       -3529
758220
 YDOT =     -10781
006134  feet/sec       YDOT =       -3325
566549  meter/sec
 ZDOT =      19661
251055                 ZDOT =        5975
582546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15784028
73                 X    =         4810971
96
 Y    =      -15231789
80  feet           Y    =        -4642649
53  meter
 Z    =       -2540015
29                 Z    =         -774196
66
 XDOT =      11446
875053                 XDOT =        3489
007516
 YDOT =       8642
422507  feet/sec       YDOT =        2634
210380  meter/sec
 ZDOT =      19593
394629                 ZDOT =        5972
066683


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   09269
50149243  
00020000  00000-0  20000-3 0  9058
2 25544  51
6403 146
6970 0008459 132
6076 227
5802 15
74400608 21919


Satellite: ISS
Catalog Number: 25544
Epoch time:      09269
50149243   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       146
6970  deg
Eccentricity:     
0008459     
Arg of perigee:   132
6076  deg
Mean anomaly:     227
5802  deg
Mean motion:   15
74400608  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2191
Checksum:              289


Coasting Arc #7 (Orbit 2206)
---------------------------------------

Vector Time (GMT): 2009/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3187995
12                 A    =         6719041
05  meter
 Y    =        2733880
80  meter          E    =           
0021002
 Z    =       -5261861
75                 I    =           51
83107
 XDOT =      -5576
538277                 Wp   =          103
10461
 YDOT =       5249
638013  meter/sec      RA   =          140
60162  deg
 ZDOT =       -657
963788                 TA   =          160
68495
                                          MA   =          160
60522
                                          Ha   =            192
130  n
mi
                                          Hp   =            180
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10459301
59                 X    =         3182748
71
 Y    =        8969425
18  feet           Y    =         2769501
35  meter
 Z    =      -17263325
94                 Z    =        -5246387
24
 XDOT =     -18295
729254                 XDOT =       -5631
629896
 YDOT =      17223
221826  feet/sec       YDOT =        5186
969827  meter/sec
 ZDOT =      -2158
673845                 ZDOT =        -685
188652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11390561
71                 X    =        -3471843
21
 Y    =       -7887364
86  feet           Y    =        -2404068
81  meter
 Z    =      -17202167
88                 Z    =        -5243220
77
 XDOT =      15925
575461                 XDOT =        4854
115400
 YDOT =     -18106
801570  feet/sec       YDOT =       -5518
953118  meter/sec
 ZDOT =      -2265
646962                 ZDOT =        -690
569194


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   09270
51706833  
00020000  00000-0  20000-3 0  9066
2 25544  51
6399 141
4778 0008319 136
4531 223
7291 15
74429096 22075


Satellite: ISS
Catalog Number: 25544
Epoch time:      09270
51706833   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       141
4778  deg
Eccentricity:     
0008319     
Arg of perigee:   136
4531  deg
Mean anomaly:     223
7291  deg
Mean motion:   15
74429096  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2207
Checksum:              303


Coasting Arc #8 (Orbit 2222)
---------------------------------------

Vector Time (GMT): 2009/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4552100
35                 A    =         6730972
46  meter
 Y    =       -4926573
66  meter          E    =           
0021406
 Z    =         407610
69                 I    =           51
89357
 XDOT =       3756
766662                 Wp   =          134
87354
 YDOT =       2956
297547  meter/sec      RA   =          135
46930  deg
 ZDOT =      -6046
373054                 TA   =           40
70539
                                          MA   =           40
54561
                                          Ha   =            192
166  n
mi
                                          Hp   =            180
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14934712
42                 X    =         4604871
72
 Y    =      -16163299
42  feet           Y    =        -4875374
32  meter
 Z    =        1337305
40                 Z    =          429853
22
 XDOT =      12325
349942                 XDOT =        3752
801864
 YDOT =       9699
138933  feet/sec       YDOT =        2998
285498  meter/sec
 ZDOT =     -19837
181936                 ZDOT =       -6028
132405

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12961151
76                 X    =        -3950559
06
 Y    =       17778220
56  feet           Y    =         5418801
63  meter
 Z    =        1424671
19                 Z    =          434239
78
 XDOT =     -12180
830049                 XDOT =       -3712
716999
 YDOT =      -7252
790835  feet/sec       YDOT =       -2210
650646  meter/sec
 ZDOT =     -19765
102477                 ZDOT =       -6024
403235


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   09271
53262879  
00020000  00000-0  20000-3 0  9077
2 25544  51
6401 136
2595 0008461 141
0251 219
1524 15
74398023 22238


Satellite: ISS
Catalog Number: 25544
Epoch time:      09271
53262879   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:       136
2595  deg
Eccentricity:     
0008461     
Arg of perigee:   141
0251  deg
Mean anomaly:     219
1524  deg
Mean motion:   15
74398023  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2223
Checksum:              277


Coasting Arc #9 (Orbit 2238)
---------------------------------------

Vector Time (GMT): 2009/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3371166
39                 A    =         6718817
89  meter
 Y    =       -2426582
83  meter          E    =           
0010341
 Z    =        5275195
26                 I    =           51
87326
 XDOT =       4807
364577                 Wp   =          135
76246
 YDOT =      -6017
351835  meter/sec      RA   =          130
35405  deg
 ZDOT =        296
614976                 TA   =          311
38905
                                          MA   =          311
47790
                                          Ha   =            192
045  n
mi
                                          Hp   =            180
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11060257
19                 X    =        -3369407
37
 Y    =       -7961229
74  feet           Y    =        -2464271
04  meter
 Z    =       17307071
06                 Z    =         5258822
52
 XDOT =      15772
193493                 XDOT =        4872
853445
 YDOT =     -19741
967964  feet/sec       YDOT =       -5963
226868  meter/sec
 ZDOT =        973
146246                 ZDOT =         320
128636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12117450
28                 X    =         3693398
84
 Y    =        6411927
18  feet           Y    =         1954355
40  meter
 Z    =       17242382
82                 Z    =         5255478
28
 XDOT =     -12543
875958                 XDOT =       -3823
373392
 YDOT =      20773
287864  feet/sec       YDOT =        6331
698141  meter/sec
 ZDOT =       1065
463026                 ZDOT =         324
753130


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   09272
54816931  
00020000  00000-0  20000-3 0  9084
2 25544  51
6397 131
0403 0008252 144
5377 215
6336 15
74459901 22390


Satellite: ISS
Catalog Number: 25544
Epoch time:      09272
54816931   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:       131
0403  deg
Eccentricity:     
0008252     
Arg of perigee:   144
5377  deg
Mean anomaly:     215
6336  deg
Mean motion:   15
74459901  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2239
Checksum:              296


Coasting Arc #10 (Orbit 2253)
---------------------------------------

Vector Time (GMT): 2009/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3822292
00                 A    =         6730753
24  meter
 Y    =        5538220
19  meter          E    =           
0012753
 Z    =         -92477
75                 I    =           51
93125
 XDOT =      -3947
957399                 Wp   =           82
76799
 YDOT =      -2635
436187  meter/sec      RA   =          125
22885  deg
 ZDOT =       6058
506842                 TA   =          276
23189
                                          MA   =          276
37715
                                          Ha   =            191
751  n
mi
                                          Hp   =            181
109

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12540328
07                 X    =        -3883488
01
 Y    =       18170013
75  feet           Y    =         5495134
90  meter
 Z    =        -303404
69                 Z    =         -111195
59
 XDOT =     -12952
616139                 XDOT =       -3947
625326
 YDOT =      -8646
444182  feet/sec       YDOT =       -2679
582242  meter/sec
 ZDOT =      19876
990953                 ZDOT =        6039
328603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9680427
32                 X    =         2950594
25
 Y    =      -19840579
42  feet           Y    =        -6047408
61  meter
 Z    =        -376852
53                 Z    =         -114864
65
 XDOT =      12767
485447                 XDOT =        3891
529564
 YDOT =       5888
905553  feet/sec       YDOT =        1794
938413  meter/sec
 ZDOT =      19801
227629                 ZDOT =        6035
414181


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   09273
50022314  
00020000  00000-0  20000-3 0  9096
2 25544  51
6387 126
1466 0008143 148
6482 211
5168 15
74495445 22542


Satellite: ISS
Catalog Number: 25544
Epoch time:      09273
50022314   =   yrday
fracday
Element set:     909
Inclination:       51
6387  deg
RA of node:       126
1466  deg
Eccentricity:     
0008143     
Arg of perigee:   148
6482  deg
Mean anomaly:     211
5168  deg
Mean motion:   15
74495445  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2254
Checksum:              290


Coasting Arc #11 (Orbit 2269)
---------------------------------------

Vector Time (GMT): 2009/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3519277
86                 A    =         6718610
67  meter
 Y    =        2207876
12  meter          E    =           
0020205
 Z    =       -5296289
39                 I    =           51
90549
 XDOT =      -3940
894003                 Wp   =          111
71832
 YDOT =       6599
795267  meter/sec      RA   =          120
10788  deg
 ZDOT =        125
703981                 TA   =          159
51276
                                          MA   =          159
43161
                                          Ha   =            191
633  n
mi
                                          Hp   =            181
277

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11546187
19                 X    =         3520056
05
 Y    =        7243688
06  feet           Y    =         2247234
61  meter
 Z    =      -17376277
54                 Z    =        -5279190
94
 XDOT =     -12929
442266                 XDOT =       -4015
011810
 YDOT =      21652
871610  feet/sec       YDOT =        6555
311466  meter/sec
 ZDOT =        412
414636                 ZDOT =         106
378327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12690892
32                 X    =        -3868183
98
 Y    =       -5202819
38  feet           Y    =        -1585819
35  meter
 Z    =      -17308737
66                 Z    =        -5275703
24
 XDOT =       8766
156987                 XDOT =        2671
924650
 YDOT =     -22578
457985  feet/sec       YDOT =       -6881
913994  meter/sec
 ZDOT =        336
629330                 ZDOT =         102
604620


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   09274
51573018  
00020000  00000-0  20000-3 0  9102
2 25544  51
6374 120
9261 0008112 152
5248 207
6346 15
74526878 22700


Satellite: ISS
Catalog Number: 25544
Epoch time:      09274
51573018   =   yrday
fracday
Element set:     910
Inclination:       51
6374  deg
RA of node:       120
9261  deg
Eccentricity:     
0008112     
Arg of perigee:   152
5248  deg
Mean anomaly:     207
6346  deg
Mean motion:   15
74526878  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2270
Checksum:              284


Coasting Arc #12 (Orbit 2285)
---------------------------------------

Vector Time (GMT): 2009/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3056495
90                 A    =         6730611
95  meter
 Y    =       -5976808
08  meter          E    =           
0019448
 Z    =        -313109
12                 I    =           51
96007
 XDOT =       4108
631812                 Wp   =          145
29928
 YDOT =       2408
209271  meter/sec      RA   =          114
99350  deg
 ZDOT =      -6059
988440                 TA   =           38
09219
                                          MA   =           37
95487
                                          Ha   =            191
536  n
mi
                                          Hp   =            181
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10027873
67                 X    =         3124623
48
 Y    =      -19608950
40  feet           Y    =        -5942247
66  meter
 Z    =       -1027260
90                 Z    =         -298094
39
 XDOT =      13479
763163                 XDOT =        4110
836116
 YDOT =       7900
949053  feet/sec       YDOT =        2454
166109  meter/sec
 ZDOT =     -19881
851837                 ZDOT =       -6040
023369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6266110
00                 X    =        -1909910
33
 Y    =       21116876
38  feet           Y    =         6436423
92  meter
 Z    =        -968425
97                 Z    =         -295176
24
 XDOT =     -13274
309833                 XDOT =       -4046
009637
 YDOT =      -4815
491138  feet/sec       YDOT =       -1467
761699  meter/sec
 ZDOT =     -19802
998878                 ZDOT =       -6035
954058


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   09275
53121958  
00020000  00000-0  20000-3 0  9118
2 25544  51
6374 115
7072 0008072 156
6443 203
5089 15
74539465 22861


Satellite: ISS
Catalog Number: 25544
Epoch time:      09275
53121958   =   yrday
fracday
Element set:     911
Inclination:       51
6374  deg
RA of node:       115
7072  deg
Eccentricity:     
0008072     
Arg of perigee:   156
6443  deg
Mean anomaly:     203
5089  deg
Mean motion:   15
74539465  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2286
Checksum:              301


Coasting Arc #13 (Orbit 2301)
---------------------------------------

Vector Time (GMT): 2009/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3662835
09                 A    =         6718624
50  meter
 Y    =       -1993085
11  meter          E    =           
0008374
 Z    =        5262930
38                 I    =           51
93040
 XDOT =       3029
183804                 Wp   =          141
17154
 YDOT =      -7063
511550  meter/sec      RA   =          109
86644  deg
 ZDOT =       -572
650880                 TA   =          314
20982
                                          MA   =          314
27857
                                          Ha   =            191
534  n
mi
                                          Hp   =            181
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12017175
51                 X    =        -3665842
64
 Y    =       -6538993
15  feet           Y    =        -2034061
36  meter
 Z    =       17266831
96                 Z    =         5245128
93
 XDOT =       9938
267074                 XDOT =        3110
725958
 YDOT =     -23174
250492  feet/sec       YDOT =       -7029
181565  meter/sec
 ZDOT =      -1878
775852                 ZDOT =        -557
736048

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13181979
64                 X    =         4017867
39
 Y    =        3978571
05  feet           Y    =         1212668
46  meter
 Z    =       17196534
82                 Z    =         5241503
81
 XDOT =      -4814
647036                 XDOT =       -1467
504417
 YDOT =      23736
373144  feet/sec       YDOT =        7234
846534  meter/sec
 ZDOT =      -1820
390533                 ZDOT =        -554
855035


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   09276
54669064  
00020000  00000-0  20000-3 0  9126
2 25544  51
6365 110
4866 0008082 160
6907 199
4564 15
74550768 23024


Satellite: ISS
Catalog Number: 25544
Epoch time:      09276
54669064   =   yrday
fracday
Element set:     912
Inclination:       51
6365  deg
RA of node:       110
4866  deg
Eccentricity:     
0008082     
Arg of perigee:   160
6907  deg
Mean anomaly:     199
4564  deg
Mean motion:   15
74550768  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2302
Checksum:              312


Coasting Arc #14 (Orbit 2317)
---------------------------------------

Vector Time (GMT): 2009/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2230353
62                 A    =         6730275
40  meter
 Y    =        6309451
55  meter          E    =           
0012746
 Z    =         702702
22                 I    =           51
97802
 XDOT =      -4281
273109                 Wp   =           88
13729
 YDOT =      -2192
994863  meter/sec      RA   =          104
75868  deg
 ZDOT =       6009
288304                 TA   =          279
48054
                                          MA   =          279
62458
                                          Ha   =            191
237  n
mi
                                          Hp   =            181
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7317433
14                 X    =        -2304154
91
 Y    =       20700300
37  feet           Y    =         6284097
85  meter
 Z    =        2305453
48                 Z    =          691687
06
 XDOT =     -14046
171618                 XDOT =       -4285
625141
 YDOT =      -7194
865036  feet/sec       YDOT =       -2240
894342  meter/sec
 ZDOT =      19715
512807                 ZDOT =        5988
479066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2660597
35                 X    =          810950
07
 Y    =      -21798284
42  feet           Y    =        -6644117
09  meter
 Z    =        2262387
40                 Z    =          689575
68
 XDOT =      13795
816976                 XDOT =        4204
965014
 YDOT =       3753
694568  feet/sec       YDOT =        1144
126104  meter/sec
 ZDOT =      19633
348214                 ZDOT =        5984
244536


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   09277
56214232  
00020000  00000-0  20000-3 0  9133
2 25544  51
6354 105
2654 0008050 164
7590 195
3817 15
74597316 23180


Satellite: ISS
Catalog Number: 25544
Epoch time:      09277
56214232   =   yrday
fracday
Element set:     913
Inclination:       51
6354  deg
RA of node:       105
2654  deg
Eccentricity:     
0008050     
Arg of perigee:   164
7590  deg
Mean anomaly:     195
3817  deg
Mean motion:   15
74597316  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2318
Checksum:              295


Coasting Arc #15 (Orbit 2332)
---------------------------------------

Vector Time (GMT): 2009/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 726328
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3825383
76                 A    =         6718686
84  meter
 Y    =        1861490
47  meter          E    =           
0018898
 Z    =       -5215424
33                 I    =           51
94533
 XDOT =      -2092
135859                 Wp   =          121
94325
 YDOT =       7320
805307  meter/sec      RA   =           99
62414  deg
 ZDOT =       1071
465638                 TA   =          158
29034
                                          MA   =          158
21013
                                          Ha   =            191
135  n
mi
                                          Hp   =            181
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12550471
64                 X    =         3829620
17
 Y    =        6107252
18  feet           Y    =         1904291
45  meter
 Z    =      -17110972
22                 Z    =        -5196830
00
 XDOT =      -6863
962791                 XDOT =       -2179
047998
 YDOT =      24018
390116  feet/sec       YDOT =        7296
923943  meter/sec
 ZDOT =       3515
307212                 ZDOT =        1061
090106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13727649
43                 X    =        -4184187
55
 Y    =       -2978489
43  feet           Y    =         -907843
58  meter
 Z    =      -17037560
86                 Z    =        -5193048
55
 XDOT =        857
871449                 XDOT =         261
479218
 YDOT =     -23961
423610  feet/sec       YDOT =       -7303
441916  meter/sec
 ZDOT =       3474
805924                 ZDOT =        1059
120845


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   09278
51411151  
00020000  00000-0  20000-3 0  9149
2 25544  51
6351 100
3706 0008111 167
7125 192
4238 15
74630428 23330


Satellite: ISS
Catalog Number: 25544
Epoch time:      09278
51411151   =   yrday
fracday
Element set:     914
Inclination:       51
6351  deg
RA of node:       100
3706  deg
Eccentricity:     
0008111     
Arg of perigee:   167
7125  deg
Mean anomaly:     192
4238  deg
Mean motion:   15
74630428  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2333
Checksum:              261

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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