Date: November 13th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2935)
---------------------------------------

Vector Time (GMT): 2009/316/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4240326
45                 A    =         6714383
56  meter
 Y    =        1167803
89  meter          E    =           
0007830
 Z    =        5075202
10                 I    =           51
29531
 XDOT =       -281
061193                 Wp   =          358
90541
 YDOT =       7551
559329  meter/sec      RA   =          263
00976  deg
 ZDOT =      -1495
095822                 TA   =          105
53884
                                          MA   =          105
45238
                                          Ha   =            186
476  n
mi
                                          Hp   =            181
491

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13911832
18                 X    =         4202297
68
 Y    =        3831377
60  feet           Y    =         1215009
12  meter
 Z    =       16650925
52                 Z    =         5095709
73
 XDOT =       -922
116775                 XDOT =        -358
220072
 YDOT =      24775
457116  feet/sec       YDOT =        7547
984911  meter/sec
 ZDOT =      -4905
170021                 ZDOT =       -1496
648715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6061715
63                 X    =         1847610
92
 Y    =       12991237
90  feet           Y    =         3959729
31  meter
 Z    =       16731861
56                 Z    =         5099871
40
 XDOT =     -18467
819584                 XDOT =       -5628
991409
 YDOT =      14974
463751  feet/sec       YDOT =        4564
216551  meter/sec
 ZDOT =      -4910
988127                 ZDOT =       -1496
869181


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   09316
76536809  
00016717  00000-0  10270-3 0  9000
2 25544  51
6458 263
5885 0006456 322
1269  37
9440 15
76267884 29365


Satellite: ISS
Catalog Number: 25544
Epoch time:      09316
76536809   =   yrday
fracday
Element set:     900
Inclination:       51
6458  deg
RA of node:       263
5885  deg
Eccentricity:     
0006456     
Arg of perigee:   322
1269  deg
Mean anomaly:      37
9440  deg
Mean motion:   15
76267884  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              349


Coasting Arc #2 (Orbit 2951)
---------------------------------------

Vector Time (GMT): 2009/317/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         283481
74                 A    =         6723867
79  meter
 Y    =       -6395564
69  meter          E    =           
0014108
 Z    =        2026496
31                 I    =           51
33175
 XDOT =       4969
742478                 Wp   =           42
36063
 YDOT =       1982
872588  meter/sec      RA   =          257
86416  deg
 ZDOT =       5550
596581                 TA   =          340
37781
                                          MA   =          340
43204
                                          Ha   =            186
609  n
mi
                                          Hp   =            181
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         930058
22                 X    =          345132
36
 Y    =      -20982823
80  feet           Y    =        -6392049
94  meter
 Z    =        6648609
94                 Z    =         2028023
20
 XDOT =      16304
929389                 XDOT =        4920
235706
 YDOT =       6505
487492  feet/sec       YDOT =        2038
170325  meter/sec
 ZDOT =      18210
618703                 ZDOT =        5574
620052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16305155
05                 X    =         4969811
26
 Y    =      -13236660
58  feet           Y    =        -4034534
14  meter
 Z    =        6654370
93                 Z    =         2028252
26
 XDOT =       4896
006647                 XDOT =        1492
302826
 YDOT =      15253
478687  feet/sec       YDOT =        4649
260304  meter/sec
 ZDOT =      18305
458197                 ZDOT =        5579
503658


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   09317
77974325  
00016717  00000-0  10270-3 0  9012
2 25544  51
6452 258
3613 0006485 325
6991  34
3754 15
76293718 29524


Satellite: ISS
Catalog Number: 25544
Epoch time:      09317
77974325   =   yrday
fracday
Element set:     901
Inclination:       51
6452  deg
RA of node:       258
3613  deg
Eccentricity:     
0006485     
Arg of perigee:   325
6991  deg
Mean anomaly:      34
3754  deg
Mean motion:   15
76293718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2952
Checksum:              340


Coasting Arc #3 (Orbit 2966)
---------------------------------------

Vector Time (GMT): 2009/318/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4466742
50                 A    =         6716668
90  meter
 Y    =       -2258164
05  meter          E    =           
0006377
 Z    =       -4483263
81                 I    =           51
31497
 XDOT =        423
739109                 Wp   =           71
44815
 YDOT =      -7026
166815  meter/sec      RA   =          252
64575  deg
 ZDOT =       3122
440029                 TA   =          229
82024
                                          MA   =          229
87609
                                          Ha   =            186
617  n
mi
                                          Hp   =            180
986

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14654666
99                 X    =        -4419379
75
 Y    =       -7408674
69  feet           Y    =        -2307848
84  meter
 Z    =      -14708870
75                 Z    =        -4504848
95
 XDOT =       1390
220173                 XDOT =         487
106706
 YDOT =     -23051
728396  feet/sec       YDOT =       -7021
074099  meter/sec
 ZDOT =      10244
225816                 ZDOT =        3124
652337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4376425
27                 X    =        -1333934
42
 Y    =      -15747377
55  feet           Y    =        -4799800
68  meter
 Z    =      -14794107
15                 Z    =        -4509243
86
 XDOT =      16748
946374                 XDOT =        5105
078855
 YDOT =     -14269
556199  feet/sec       YDOT =       -4349
360730  meter/sec
 ZDOT =      10252
665168                 ZDOT =        3125
012343


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   09318
73069364  
00016717  00000-0  10270-3 0  9028
2 25544  51
6447 253
4607 0006452 329
0230  31
0553 15
76336070 29671


Satellite: ISS
Catalog Number: 25544
Epoch time:      09318
73069364   =   yrday
fracday
Element set:     902
Inclination:       51
6447  deg
RA of node:       253
4607  deg
Eccentricity:     
0006452     
Arg of perigee:   329
0230  deg
Mean anomaly:      31
0553  deg
Mean motion:   15
76336070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2967
Checksum:              303


Coasting Arc #4 (Orbit 2982)
---------------------------------------

Vector Time (GMT): 2009/319/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -530640
38                 A    =         6720473
89  meter
 Y    =        5789016
85  meter          E    =           
0006013
 Z    =       -3379491
66                 I    =           51
33748
 XDOT =      -5294
687319                 Wp   =           18
41625
 YDOT =      -3172
028282  meter/sec      RA   =          247
51951  deg
 ZDOT =      -4598
876254                 TA   =          201
64800
                                          MA   =          201
67343
                                          Ha   =            186
783  n
mi
                                          Hp   =            180
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1740946
14                 X    =         -578917
25
 Y    =       18992837
42  feet           Y    =         5782813
16  meter
 Z    =      -11087571
06                 Z    =        -3382186
56
 XDOT =     -17371
021387                 XDOT =       -5236
482392
 YDOT =     -10406
916936  feet/sec       YDOT =       -3230
910915  meter/sec
 ZDOT =     -15088
176687                 ZDOT =       -4624
457465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14936042
39                 X    =        -4552505
72
 Y    =       11850855
50  feet           Y    =         3612140
76  meter
 Z    =      -11097966
50                 Z    =        -3382660
19
 XDOT =      -3473
988676                 XDOT =       -1058
871748
 YDOT =     -18613
062907  feet/sec       YDOT =       -5673
261574  meter/sec
 ZDOT =     -15189
218602                 ZDOT =       -4629
673830


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   09319
74501291  
00016717  00000-0  10270-3 0  9031
2 25544  51
6440 248
2344 0006443 332
3909  27
6912 15
76363523 29835


Satellite: ISS
Catalog Number: 25544
Epoch time:      09319
74501291   =   yrday
fracday
Element set:     903
Inclination:       51
6440  deg
RA of node:       248
2344  deg
Eccentricity:     
0006443     
Arg of perigee:   332
3909  deg
Mean anomaly:      27
6912  deg
Mean motion:   15
76363523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2983
Checksum:              310


Coasting Arc #5 (Orbit 2998)
---------------------------------------

Vector Time (GMT): 2009/320/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4794337
35                 A    =         6719956
47  meter
 Y    =        3214651
05  meter          E    =           
0011538
 Z    =        3438556
70                 I    =           51
34994
 XDOT =       -864
029705                 Wp   =           56
98619
 YDOT =       6162
818460  meter/sec      RA   =          242
29226  deg
 ZDOT =      -4539
616245                 TA   =           82
07117
                                          MA   =           81
94024
                                          Ha   =            186
748  n
mi
                                          Hp   =            180
574

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15729453
23                 X    =         4741329
82
 Y    =       10546755
41  feet           Y    =         3267967
52  meter
 Z    =       11281354
01                 Z    =         3461719
80
 XDOT =      -2834
743126                 XDOT =        -910
825877
 YDOT =      20219
220670  feet/sec       YDOT =        6152
895057  meter/sec
 ZDOT =     -14893
754084                 ZDOT =       -4543
927045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3442525
85                 X    =         1049281
88
 Y    =       18566788
67  feet           Y    =         5659157
19  meter
 Z    =       11372865
56                 Z    =         3466449
42
 XDOT =     -15001
838614                 XDOT =       -4572
560410
 YDOT =      11949
075610  feet/sec       YDOT =        3642
078246  meter/sec
 ZDOT =     -14910
511380                 ZDOT =       -4544
723868


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   09320
75930202  
00016717  00000-0  10270-3 0  9043
2 25544  51
6446 243
0069 0006571 335
6635  24
4219 15
76456952 29993


Satellite: ISS
Catalog Number: 25544
Epoch time:      09320
75930202   =   yrday
fracday
Element set:     904
Inclination:       51
6446  deg
RA of node:       243
0069  deg
Eccentricity:     
0006571     
Arg of perigee:   335
6635  deg
Mean anomaly:      24
4219  deg
Mean motion:   15
76456952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2999
Checksum:              320


Coasting Arc #6 (Orbit 3014)
---------------------------------------

Vector Time (GMT): 2009/321/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1057868
59                 A    =         6716610
90  meter
 Y    =       -4916674
38  meter          E    =           
0006744
 Z    =        4445224
06                 I    =           51
35190
 XDOT =       5688
267604                 Wp   =           67
03864
 YDOT =       4109
592869  meter/sec      RA   =          237
16656  deg
 ZDOT =       3190
526993                 TA   =          350
95360
                                          MA   =          350
96574
                                          Ha   =            186
878  n
mi
                                          Hp   =            180
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3470697
47                 X    =         1091174
37
 Y    =      -16130821
46  feet           Y    =        -4904658
86  meter
 Z    =       14584068
45                 Z    =         4450443
78
 XDOT =      18662
295288                 XDOT =        5626
391210
 YDOT =      13482
916238  feet/sec       YDOT =        4172
856168  meter/sec
 ZDOT =      10467
608245                 ZDOT =        3218
011455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13729492
14                 X    =         4184749
20
 Y    =       -9118928
51  feet           Y    =        -2779449
41  meter
 Z    =       14604464
48                 Z    =         4451440
77
 XDOT =       3129
633771                 XDOT =         953
912373
 YDOT =      21656
848800  feet/sec       YDOT =        6601
007514  meter/sec
 ZDOT =      10576
214928                 ZDOT =        3223
630310


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   09321
77356649  
00016717  00000-0  10270-3 0  9054
2 25544  51
6431 237
7790 0006448 340
2705  19
8209 15
76430112 30158


Satellite: ISS
Catalog Number: 25544
Epoch time:      09321
77356649   =   yrday
fracday
Element set:     905
Inclination:       51
6431  deg
RA of node:       237
7790  deg
Eccentricity:     
0006448     
Arg of perigee:   340
2705  deg
Mean anomaly:      19
8209  deg
Mean motion:   15
76430112  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3015
Checksum:              306


Coasting Arc #7 (Orbit 3029)
---------------------------------------

Vector Time (GMT): 2009/322/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5098518
14                 A    =         6723201
57  meter
 Y    =       -3866130
63  meter          E    =           
0011217
 Z    =       -2043806
47                 I    =           51
39131
 XDOT =       1642
350484                 Wp   =           12
69863
 YDOT =      -5090
352428  meter/sec      RA   =          231
94996  deg
 ZDOT =       5548
567619                 TA   =          324
38552
                                          MA   =          324
46032
                                          Ha   =            186
800  n
mi
                                          Hp   =            180
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16727421
72                 X    =        -5044978
77
 Y    =      -12684155
59  feet           Y    =        -3922845
69  meter
 Z    =       -6705401
80                 Z    =        -2068446
02
 XDOT =       5388
288989                 XDOT =        1672
195040
 YDOT =     -16700
631326  feet/sec       YDOT =       -5071
820401  meter/sec
 ZDOT =      18203
962004                 ZDOT =        5556
618319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3348450
82                 X    =        -1020607
81
 Y    =      -20692192
68  feet           Y    =        -6306980
33  meter
 Z    =       -6802785
68                 Z    =        -2073489
08
 XDOT =      13828
381286                 XDOT =        4214
890616
 YDOT =      -8215
289701  feet/sec       YDOT =       -2504
020301  meter/sec
 ZDOT =      18235
523532                 ZDOT =        5558
187573


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   09322
72441039  
00016717  00000-0  10270-3 0  9069
2 25544  51
6421 232
8777 0006276 343
0311  17
0642 15
76496420 30303


Satellite: ISS
Catalog Number: 25544
Epoch time:      09322
72441039   =   yrday
fracday
Element set:     906
Inclination:       51
6421  deg
RA of node:       232
8777  deg
Eccentricity:     
0006276     
Arg of perigee:   343
0311  deg
Mean anomaly:      17
0642  deg
Mean motion:   15
76496420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3030
Checksum:              286


Coasting Arc #8 (Orbit 3045)
---------------------------------------

Vector Time (GMT): 2009/323/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1897707
01                 A    =         6713549
21  meter
 Y    =        3939485
37  meter          E    =           
0015183
 Z    =       -5106718
22                 I    =           51
37762
 XDOT =      -5938
396718                 Wp   =           55
26591
 YDOT =      -4687
242111  meter/sec      RA   =          226
80820  deg
 ZDOT =      -1403
551254                 TA   =          201
20069
                                          MA   =          201
26368
                                          Ha   =            186
930  n
mi
                                          Hp   =            179
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6226072
87                 X    =        -1916809
97
 Y    =       12924820
76  feet           Y    =         3918157
83  meter
 Z    =      -16754324
86                 Z    =        -5115983
44
 XDOT =     -19482
928865                 XDOT =       -5878
723466
 YDOT =     -15378
090916  feet/sec       YDOT =       -4753
314963  meter/sec
 ZDOT =      -4604
826949                 ZDOT =       -1432
256118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13257591
20                 X    =        -4040913
80
 Y    =        5369365
99  feet           Y    =         1636582
75  meter
 Z    =      -16790728
43                 Z    =        -5117814
02
 XDOT =      -3527
298561                 XDOT =       -1075
120601
 YDOT =     -23521
094563  feet/sec       YDOT =       -7169
229623  meter/sec
 ZDOT =      -4718
301296                 ZDOT =       -1438
138235


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   09323
73861806  
00016717  00000-0  10270-3 0  9070
2 25544  51
6412 227
6501 0006187 347
9529  12
1487 15
76543870 30467


Satellite: ISS
Catalog Number: 25544
Epoch time:      09323
73861806   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       227
6501  deg
Eccentricity:     
0006187     
Arg of perigee:   347
9529  deg
Mean anomaly:      12
1487  deg
Mean motion:   15
76543870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3046
Checksum:              321


Coasting Arc #9 (Orbit 3061)
---------------------------------------

Vector Time (GMT): 2009/324/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5202786
14                 A    =         6724619
13  meter
 Y    =        4242549
19  meter          E    =           
0009032
 Z    =         356398
97                 I    =           51
43764
 XDOT =      -2785
795863                 Wp   =          104
08887
 YDOT =       3931
470896  meter/sec      RA   =          221
62076  deg
 ZDOT =      -6007
566045                 TA   =           72
02356
                                          MA   =           71
92513
                                          Ha   =            186
953  n
mi
                                          Hp   =            179
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17069508
34                 X    =         5153227
18
 Y    =       13919124
64  feet           Y    =         4300452
68  meter
 Z    =        1169287
94                 Z    =          381554
57
 XDOT =      -9139
750208                 XDOT =       -2800
367068
 YDOT =      12898
526561  feet/sec       YDOT =        3900
237633  meter/sec
 ZDOT =     -19709
862353                 ZDOT =       -6021
134650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3518417
91                 X    =         1072413
78
 Y    =       21736797
93  feet           Y    =         6625376
01  meter
 Z    =        1268751
84                 Z    =          386715
56
 XDOT =     -13726
616277                 XDOT =       -4183
872641
 YDOT =       3397
431798  feet/sec       YDOT =        1035
537212  meter/sec
 ZDOT =     -19763
253258                 ZDOT =       -6023
839593


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   09324
75279587  
00016717  00000-0  10270-3 0  9083
2 25544  51
6414 222
4220 0006436 350
9825   9
1223 15
76635301 30623


Satellite: ISS
Catalog Number: 25544
Epoch time:      09324
75279587   =   yrday
fracday
Element set:     908
Inclination:       51
6414  deg
RA of node:       222
4220  deg
Eccentricity:     
0006436     
Arg of perigee:   350
9825  deg
Mean anomaly:       9
1223  deg
Mean motion:   15
76635301  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3062
Checksum:              300


Coasting Arc #10 (Orbit 3077)
---------------------------------------

Vector Time (GMT): 2009/325/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3014526
01                 A    =         6712844
73  meter
 Y    =       -2950842
83  meter          E    =           
0007520
 Z    =        5220550
43                 I    =           51
41978
 XDOT =       5885
017484                 Wp   =           17
01742
 YDOT =       4940
100083  meter/sec      RA   =          216
44835  deg
 ZDOT =       -598
583569                 TA   =           78
72680
                                          MA   =           78
64230
                                          Ha   =            186
980  n
mi
                                          Hp   =            179
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9890177
20                 X    =         3021937
97
 Y    =       -9681242
88  feet           Y    =        -2917091
67  meter
 Z    =       17127790
12                 Z    =         5235212
93
 XDOT =      19307
800143                 XDOT =        5832
246881
 YDOT =      16207
677438  feet/sec       YDOT =        5005
614819  meter/sec
 ZDOT =      -1963
856855                 ZDOT =        -570
121485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13733435
40                 X    =         4185951
11
 Y    =        -976268
65  feet           Y    =         -297566
69  meter
 Z    =       17185543
77                 Z    =         5238153
74
 XDOT =       4043
941689                 XDOT =        1232
593427
 YDOT =      23877
751779  feet/sec       YDOT =        7277
938742  meter/sec
 ZDOT =      -1851
296463                 ZDOT =        -564
275162


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   09325
76695035  
00016717  00000-0  10270-3 0  9096
2 25544  51
6404 217
1931 0006078 356
1850   3
9268 15
76583611 30784


Satellite: ISS
Catalog Number: 25544
Epoch time:      09325
76695035   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:       217
1931  deg
Eccentricity:     
0006078     
Arg of perigee:   356
1850  deg
Mean anomaly:       3
9268  deg
Mean motion:   15
76583611  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3078
Checksum:              324


Coasting Arc #11 (Orbit 3093)
---------------------------------------

Vector Time (GMT): 2009/326/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4955361
70                 A    =         6723793
12  meter
 Y    =       -4309645
67  meter          E    =           
0017746
 Z    =        1392478
98                 I    =           51
48244
 XDOT =       4157
092525                 Wp   =           43
28572
 YDOT =      -2890
647522  meter/sec      RA   =          211
29721  deg
 ZDOT =       5816
454935                 TA   =          332
08746
                                          MA   =          332
18255
                                          Ha   =            187
014  n
mi
                                          Hp   =            179
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16257748
36                 X    =        -4913566
69
 Y    =      -14139257
44  feet           Y    =        -4364825
87  meter
 Z    =        4568500
60                 Z    =         1368506
72
 XDOT =      13638
755004                 XDOT =        4160
851651
 YDOT =      -9483
751713  feet/sec       YDOT =       -2844
139904  meter/sec
 ZDOT =      19082
857398                 ZDOT =        5836
659243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3524339
65                 X    =        -1074218
72
 Y    =      -21276029
55  feet           Y    =        -6484933
81  meter
 Z    =        4473676
03                 Z    =         1363576
46
 XDOT =      14915
475108                 XDOT =        4546
236813
 YDOT =       1580
266201  feet/sec       YDOT =         481
665138  meter/sec
 ZDOT =      19162
495370                 ZDOT =        5840
728589


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   09326
78107368  
00016717  00000-0  10270-3 0  9108
2 25544  51
6405 211
9642 0006008 359
5297    
5861 15
76667747 30944


Satellite: ISS
Catalog Number: 25544
Epoch time:      09326
78107368   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:       211
9642  deg
Eccentricity:     
0006008     
Arg of perigee:   359
5297  deg
Mean anomaly:        
5861  deg
Mean motion:   15
76667747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3094
Checksum:              326


Coasting Arc #12 (Orbit 3108)
---------------------------------------

Vector Time (GMT): 2009/327/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4244188
36                 A    =         6714530
05  meter
 Y    =        2134966
78  meter          E    =           
0011753
 Z    =       -4753864
63                 I    =           51
47875
 XDOT =      -5344
995400                 Wp   =           79
11987
 YDOT =      -4902
899848  meter/sec      RA   =          206
09661  deg
 ZDOT =       2577
601039                 TA   =          216
18143
                                          MA   =          216
26099
                                          Ha   =            187
003  n
mi
                                          Hp   =            179
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13924502
48                 X    =        -4244652
78
 Y    =        7004484
20  feet           Y    =         2087503
47  meter
 Z    =      -15596668
75                 Z    =        -4774484
15
 XDOT =     -17536
074147                 XDOT =       -5302
294739
 YDOT =     -16085
629422  feet/sec       YDOT =       -4962
432153  meter/sec
 ZDOT =       8456
696322                 ZDOT =        2551
738131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15178245
06                 X    =        -4626329
09
 Y    =       -3167382
30  feet           Y    =         -965418
12  meter
 Z    =      -15677984
90                 Z    =        -4778649
80
 XDOT =      -3921
602403                 XDOT =       -1195
304413
 YDOT =     -22438
053621  feet/sec       YDOT =       -6839
118744  meter/sec
 ZDOT =       8354
368075                 ZDOT =        2546
411389


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   09327
73179085  
00016717  00000-0  10270-3 0  9110
2 25544  51
6411 207
0625 0005947   4
0218 356
0993 15
76707551 31094


Satellite: ISS
Catalog Number: 25544
Epoch time:      09327
73179085   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       207
0625  deg
Eccentricity:     
0005947     
Arg of perigee:     4
0218  deg
Mean anomaly:     356
0993  deg
Mean motion:   15
76707551  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3109
Checksum:              308


Coasting Arc #13 (Orbit 3124)
---------------------------------------

Vector Time (GMT): 2009/328/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4240252
75                 A    =         6720295
54  meter
 Y    =        4229127
10  meter          E    =           
0006907
 Z    =       -3059082
97                 I    =           51
52634
 XDOT =      -5569
825019                 Wp   =           48
22037
 YDOT =       2038
774233  meter/sec      RA   =          200
97541  deg
 ZDOT =      -4904
441094                 TA   =          167
30347
                                          MA   =          167
28606
                                          Ha   =            187
085  n
mi
                                          Hp   =            178
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13911590
40                 X    =         4207507
45
 Y    =       13875088
93  feet           Y    =         4276361
18  meter
 Z    =      -10036361
45                 Z    =        -3038562
86
 XDOT =     -18273
704130                 XDOT =       -5568
383760
 YDOT =       6688
891840  feet/sec       YDOT =        1976
497470  meter/sec
 ZDOT =     -16090
686005                 ZDOT =       -4931
496082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2583476
85                 X    =          787443
74
 Y    =       19519213
06  feet           Y    =         5949456
14  meter
 Z    =       -9955147
43                 Z    =        -3034328
94
 XDOT =     -17055
181579                 XDOT =       -5198
419345
 YDOT =      -5999
291275  feet/sec       YDOT =       -1828
583981  meter/sec
 ZDOT =     -16197
423019                 ZDOT =       -4936
974536


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   09328
74586259  
00016717  00000-0  10270-3 0  9128
2 25544  51
6413 201
8337 0006069   7
8198 352
3060 15
76768219 31252


Satellite: ISS
Catalog Number: 25544
Epoch time:      09328
74586259   =   yrday
fracday
Element set:     912
Inclination:       51
6413  deg
RA of node:       201
8337  deg
Eccentricity:     
0006069     
Arg of perigee:     7
8198  deg
Mean anomaly:     352
3060  deg
Mean motion:   15
76768219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3125
Checksum:              324


Coasting Arc #14 (Orbit 3140)
---------------------------------------

Vector Time (GMT): 2009/329/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5427769
67                 A    =         6718344
85  meter
 Y    =       -1490405
11  meter          E    =           
0014677
 Z    =        3662967
49                 I    =           51
54822
 XDOT =       4240
035227                 Wp   =           61
91917
 YDOT =       4764
548550  meter/sec      RA   =          195
76024  deg
 ZDOT =      -4324
327936                 TA   =           73
93498
                                          MA   =           73
77342
                                          Ha   =            187
049  n
mi
                                          Hp   =            178
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17807643
28                 X    =         5426237
90
 Y    =       -4889780
54  feet           Y    =        -1429717
30  meter
 Z    =       12017609
86                 Z    =         3689332
25
 XDOT =      13910
876730                 XDOT =        4207
449238
 YDOT =      15631
720965  feet/sec       YDOT =        4811
781104  meter/sec
 ZDOT =     -14187
427610                 ZDOT =       -4303
808456

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17146656
48                 X    =         5226300
89
 Y    =        6671037
32  feet           Y    =         2033332
18  meter
 Z    =       12121653
86                 Z    =         3694680
10
 XDOT =       2375
180760                 XDOT =         723
955096
 YDOT =      19644
492528  feet/sec       YDOT =        5987
641323  meter/sec
 ZDOT =     -14106
183682                 ZDOT =       -4299
564786


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   09329
75990892  
00016717  00000-0  10270-3 0  9133
2 25544  51
6409 196
6042 0005907  11
4190 348
7108 15
76771923 31410


Satellite: ISS
Catalog Number: 25544
Epoch time:      09329
75990892   =   yrday
fracday
Element set:     913
Inclination:       51
6409  deg
RA of node:       196
6042  deg
Eccentricity:     
0005907     
Arg of perigee:    11
4190  deg
Mean anomaly:     348
7108  deg
Mean motion:   15
76771923  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3141
Checksum:              327


Coasting Arc #15 (Orbit 3156)
---------------------------------------

Vector Time (GMT): 2009/330/17:17:16
381
Vector Time (MET): N/A
Weight (LBS)     : 731798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3041823
66                 A    =         6715806
74  meter
 Y    =       -4092197
92  meter          E    =           
0010714
 Z    =        4360394
30                 I    =           51
57056
 XDOT =       6783
691501                 Wp   =           76
97184
 YDOT =      -1445
900937  meter/sec      RA   =          190
64840  deg
 ZDOT =       3370
822916                 TA   =          339
09064
                                          MA   =          339
13442
                                          Ha   =            187
085  n
mi
                                          Hp   =            178
584

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9979736
41                 X    =        -3017020
35
 Y    =      -13425846
21  feet           Y    =        -4126074
87  meter
 Z    =       14305755
58                 Z    =         4345676
92
 XDOT =      22256
205712                 XDOT =        6782
980451
 YDOT =      -4743
769478  feet/sec       YDOT =       -1370
045794  meter/sec
 ZDOT =      11059
130302                 ZDOT =        3403
776983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -342218
44                 X    =         -104308
18
 Y    =      -16774868
27  feet           Y    =        -5112979
85  meter
 Z    =       14247449
21                 Z    =         4342622
52
 XDOT =      19568
239072                 XDOT =        5964
399269
 YDOT =       9116
838750  feet/sec       YDOT =        2778
812451  meter/sec
 ZDOT =      11189
206366                 ZDOT =        3410
470100


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   09330
77392693  
00016717  00000-0  10270-3 0  9143
2 25544  51
6419 191
3753 0005869  14
2610 345
8719 15
76857779 31574


Satellite: ISS
Catalog Number: 25544
Epoch time:      09330
77392693   =   yrday
fracday
Element set:     914
Inclination:       51
6419  deg
RA of node:       191
3753  deg
Eccentricity:     
0005869     
Arg of perigee:    14
2610  deg
Mean anomaly:     345
8719  deg
Mean motion:   15
76857779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3157
Checksum:              351

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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