Date: March 23rd 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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


083/09:18:32 836 -0 9 3 4 3 4
N/A -1 9 0 2 192 7
000/00:07:05 671 -2 6 -0 1 181 9

Coasting Arc #1 (Orbit 981)
---------------------------------------

Vector Time (GMT): 2010/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782863
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -815348
87                 A    =         6721117
93  meter
 Y    =       -4626774
50  meter          E    =           
0018105
 Z    =       -4822459
56                 I    =           51
39556
 XDOT =       6342
354326                 Wp   =           94
32006
 YDOT =      -3618
217948  meter/sec      RA   =          315
04612  deg
 ZDOT =       2405
492917                 TA   =          199
24833
                                          MA   =          199
31681
                                          Ha   =            192
073  n
mi
                                          Hp   =            180
757

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2675029
09                 X    =         -740124
27
 Y    =      -15179706
35  feet           Y    =        -4635471
73  meter
 Z    =      -15821717
72                 Z    =        -4826237
68
 XDOT =      20808
249102                 XDOT =        6370
657085
 YDOT =     -11870
793792  feet/sec       YDOT =       -3547
135664  meter/sec
 ZDOT =       7892
037130                 ZDOT =        2436
372832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2345968
00                 X    =         -715051
05
 Y    =      -15218333
70  feet           Y    =        -4638548
11  meter
 Z    =      -15836816
94                 Z    =        -4827061
80
 XDOT =      19833
487326                 XDOT =        6045
246937
 YDOT =     -11375
830170  feet/sec       YDOT =       -3467
353036  meter/sec
 ZDOT =       8014
586831                 ZDOT =        2442
846066


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   10081
51167848  
00016717  00000-0  10270-3 0  9007
2 25544  51
6469 315
5868 0006999  72
2002 287
9924 15
74335183  9825


Satellite: ISS
Catalog Number: 25544
Epoch time:      10081
51167848   =   yrday
fracday
Element set:     900
Inclination:       51
6469  deg
RA of node:       315
5868  deg
Eccentricity:     
0006999     
Arg of perigee:    72
2002  deg
Mean anomaly:     287
9924  deg
Mean motion:   15
74335183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             982
Checksum:              336


Coasting Arc #2 (Orbit 997)
---------------------------------------

Vector Time (GMT): 2010/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 782863
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5281241
65                 A    =         6728963
46  meter
 Y    =        3516063
43  meter          E    =           
0011089
 Z    =       -2246123
47                 I    =           51
40141
 XDOT =      -1226
202911                 Wp   =          103
53260
 YDOT =      -5301
422612  meter/sec      RA   =          309
93051  deg
 ZDOT =      -5440
708291                 TA   =          101
74542
                                          MA   =          101
62099
                                          Ha   =            192
024  n
mi
                                          Hp   =            180
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17326908
31                 X    =        -5309255
20
 Y    =       11535641
17  feet           Y    =         3456848
76  meter
 Z    =       -7369171
50                 Z    =        -2271847
69
 XDOT =      -4022
975430                 XDOT =       -1140
400531
 YDOT =     -17393
118806  feet/sec       YDOT =       -5314
655119  meter/sec
 ZDOT =     -17850
092819                 ZDOT =       -5446
456609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17263864
74                 X    =        -5262025
97
 Y    =       11564464
48  feet           Y    =         3524848
77  meter
 Z    =       -7471251
10                 Z    =        -2277237
33
 XDOT =      -3103
800909                 XDOT =        -946
038517
 YDOT =     -16128
043024  feet/sec       YDOT =       -4915
827514  meter/sec
 ZDOT =     -17873
034134                 ZDOT =       -5447
700804


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   10082
52729111  
00016717  00000-0  10270-3 0  9017
2 25544  51
6466 310
3692 0006859  76
5313 283
6614 15
74334563  9984


Satellite: ISS
Catalog Number: 25544
Epoch time:      10082
52729111   =   yrday
fracday
Element set:     901
Inclination:       51
6466  deg
RA of node:       310
3692  deg
Eccentricity:     
0006859     
Arg of perigee:    76
5313  deg
Mean anomaly:     283
6614  deg
Mean motion:   15
74334563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             998
Checksum:              315


Coasting Arc #3 (Orbit 1011)
---------------------------------------

Vector Time (GMT): 2010/083/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5154804
46                 A    =         6728891
63  meter
 Y    =        3109723
89  meter          E    =           
0010605
 Z    =       -3011603
55                 I    =           51
37984
 XDOT =       -668
532810                 Wp   =          104
04120
 YDOT =      -5867
460235  meter/sec      RA   =          305
34346  deg
 ZDOT =      -4931
378367                 TA   =          110
89245
                                          MA   =          110
77888
                                          Ha   =            192
658  n
mi
                                          Hp   =            181
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16912088
12                 X    =        -5174565
16
 Y    =       10202506
19  feet           Y    =         3051969
22  meter
 Z    =       -9880589
06                 Z    =        -3036693
41
 XDOT =      -2193
349115                 XDOT =        -578
916649
 YDOT =     -19250
197621  feet/sec       YDOT =       -5874
435246  meter/sec
 ZDOT =     -16179
062884                 ZDOT =       -4934
408209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19540762
24                 X    =        -5956024
33
 Y    =       -2508175
74  feet           Y    =         -764491
96  meter
 Z    =       -9980158
47                 Z    =        -3041952
30
 XDOT =      10159
614129                 XDOT =        3096
650386
 YDOT =     -14946
367809  feet/sec       YDOT =       -4555
652908  meter/sec
 ZDOT =     -16191
227059                 ZDOT =       -4935
086007


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   10083
41594378  
00016717  00000-0  10270-3 0  9022
2 25544  51
6475 305
8035 0006097 102
0627 258
1220 15
73740197 10122


Satellite: ISS
Catalog Number: 25544
Epoch time:      10083
41594378   =   yrday
fracday
Element set:     902
Inclination:       51
6475  deg
RA of node:       305
8035  deg
Eccentricity:     
0006097     
Arg of perigee:   102
0627  deg
Mean anomaly:     258
1220  deg
Mean motion:   15
73740197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1012
Checksum:              288


Coasting Arc #4 (Orbit 1027)
---------------------------------------

Vector Time (GMT): 2010/084/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1097183
07                 A    =         6724530
31  meter
 Y    =        5013021
94  meter          E    =           
0014993
 Z    =        4333887
08                 I    =           51
34857
 XDOT =      -5541
966845                 Wp   =           83
39816
 YDOT =       4150
754854  meter/sec      RA   =          300
14173  deg
 ZDOT =      -3386
455327                 TA   =           40
89256
                                          MA   =           40
78018
                                          Ha   =            192
542  n
mi
                                          Hp   =            181
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3599681
98                 X    =         1019992
07
 Y    =       16446922
37  feet           Y    =         5024859
91  meter
 Z    =       14218789
63                 Z    =         4339029
38
 XDOT =     -18182
305922                 XDOT =       -5571
518875
 YDOT =      13617
962120  feet/sec       YDOT =        4088
615885  meter/sec
 ZDOT =     -11110
417738                 ZDOT =       -3413
449813

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7227569
97                 X    =        -2202963
33
 Y    =       15186724
60  feet           Y    =         4628913
66  meter
 Z    =       14239331
89                 Z    =         4340148
36
 XDOT =     -21555
309871                 XDOT =       -6570
058449
 YDOT =        295
251407  feet/sec       YDOT =          89
992629  meter/sec
 ZDOT =     -11217
524746                 ZDOT =       -3419
101543


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   10084
43192853  
00016717  00000-0  10270-3 0  9038
2 25544  51
6469 300
5886 0006068 104
5426 255
6410 15
73801971 10281


Satellite: ISS
Catalog Number: 25544
Epoch time:      10084
43192853   =   yrday
fracday
Element set:     903
Inclination:       51
6469  deg
RA of node:       300
5886  deg
Eccentricity:     
0006068     
Arg of perigee:   104
5426  deg
Mean anomaly:     255
6410  deg
Mean motion:   15
73801971  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1028
Checksum:              303


Coasting Arc #5 (Orbit 1043)
---------------------------------------

Vector Time (GMT): 2010/085/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4473378
44                 A    =         6729015
56  meter
 Y    =       -4092459
47  meter          E    =           
0018995
 Z    =        2902582
00                 I    =           51
34980
 XDOT =       1822
051977                 Wp   =           89
98390
 YDOT =       5563
883442  meter/sec      RA   =          295
03522  deg
 ZDOT =       5008
426614                 TA   =          303
58297
                                          MA   =          303
76417
                                          Ha   =            192
505  n
mi
                                          Hp   =            181
929

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14676438
47                 X    =         4504708
57
 Y    =      -13426704
28  feet           Y    =        -4042260
10  meter
 Z    =        9522906
82                 Z    =         2924389
76
 XDOT =       5977
860818                 XDOT =        1735
370538
 YDOT =      18254
210768  feet/sec       YDOT =        5583
774423  meter/sec
 ZDOT =      16431
845847                 ZDOT =        5017
067052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19740032
44                 X    =         6016761
89
 Y    =       -2085743
07  feet           Y    =         -635734
49  meter
 Z    =        9609411
18                 Z    =         2928948
53
 XDOT =      -6292
765286                 XDOT =       -1918
034859
 YDOT =      16729
452445  feet/sec       YDOT =        5099
137105  meter/sec
 ZDOT =      16466
303799                 ZDOT =        5018
929398


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   10085
44789193  
00016717  00000-0  10270-3 0  9040
2 25544  51
6470 295
3731 0006042 107
9796 252
2026 15
73801569 10449


Satellite: ISS
Catalog Number: 25544
Epoch time:      10085
44789193   =   yrday
fracday
Element set:     904
Inclination:       51
6470  deg
RA of node:       295
3731  deg
Eccentricity:     
0006042     
Arg of perigee:   107
9796  deg
Mean anomaly:     252
2026  deg
Mean motion:   15
73801569  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1044
Checksum:              313


Coasting Arc #6 (Orbit 1058)
---------------------------------------

Vector Time (GMT): 2010/086/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2052974
55                 A    =         6724179
93  meter
 Y    =       -4672983
17  meter          E    =           
0015127
 Z    =       -4392820
68                 I    =           51
32205
 XDOT =       4662
904579                 Wp   =          111
04024
 YDOT =      -5145
864842  meter/sec      RA   =          289
83123  deg
 ZDOT =       3298
654997                 TA   =          192
28214
                                          MA   =          192
31906
                                          Ha   =            192
373  n
mi
                                          Hp   =            181
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6735480
82                 X    =        -1979228
57
 Y    =      -15331309
60  feet           Y    =        -4695528
85  meter
 Z    =      -14412141
34                 Z    =        -4402614
32
 XDOT =      15298
243370                 XDOT =        4704
075927
 YDOT =     -16882
758668  feet/sec       YDOT =       -5093
490942  meter/sec
 ZDOT =      10822
358914                 ZDOT =        3321
407619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3501869
44                 X    =         1067369
81
 Y    =      -16340940
51  feet           Y    =        -4980718
67  meter
 Z    =      -14451164
24                 Z    =        -4404714
86
 XDOT =      21018
508054                 XDOT =        6406
441255
 YDOT =      -5135
311936  feet/sec       YDOT =       -1565
243078  meter/sec
 ZDOT =      10912
580212                 ZDOT =        3326
154449


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   10086
40033528  
00016717  00000-0  10270-3 0  9052
2 25544  51
6468 290
4835 0005831 111
9797 248
1987 15
73853884 10591


Satellite: ISS
Catalog Number: 25544
Epoch time:      10086
40033528   =   yrday
fracday
Element set:     905
Inclination:       51
6468  deg
RA of node:       290
4835  deg
Eccentricity:     
0005831     
Arg of perigee:   111
9797  deg
Mean anomaly:     248
1987  deg
Mean motion:   15
73853884  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1059
Checksum:              337


Coasting Arc #7 (Orbit 1074)
---------------------------------------

Vector Time (GMT): 2010/087/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3662179
90                 A    =         6728902
25  meter
 Y    =        4853771
42  meter          E    =           
0010295
 Z    =       -2884391
63                 I    =           51
32860
 XDOT =      -2817
967578                 Wp   =          115
68895
 YDOT =      -5101
603765  meter/sec      RA   =          284
72195  deg
 ZDOT =      -5025
313364                 TA   =           97
60698
                                          MA   =           97
49003
                                          Ha   =            192
255  n
mi
                                          Hp   =            182
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12015025
93                 X    =        -3702171
71
 Y    =       15924446
90  feet           Y    =         4812594
80  meter
 Z    =       -9463227
15                 Z    =        -2902280
07
 XDOT =      -9245
300453                 XDOT =       -2736
299210
 YDOT =     -16737
545160  feet/sec       YDOT =       -5132
659900  meter/sec
 ZDOT =     -16487
248568                 ZDOT =       -5038
803988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18882077
90                 X    =        -5755257
34
 Y    =        6330008
81  feet           Y    =         1929386
69  meter
 Z    =       -9534130
68                 Z    =        -2906003
03
 XDOT =       2422
779525                 XDOT =         738
463199
 YDOT =     -17596
772291  feet/sec       YDOT =       -5363
496194  meter/sec
 ZDOT =     -16540
972057                 ZDOT =       -5041
688283


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   10087
41625399  
00016717  00000-0  10270-3 0  9068
2 25544  51
6464 285
2675 0005716 117
0695 243
1052 15
73859201 10752


Satellite: ISS
Catalog Number: 25544
Epoch time:      10087
41625399   =   yrday
fracday
Element set:     906
Inclination:       51
6464  deg
RA of node:       285
2675  deg
Eccentricity:     
0005716     
Arg of perigee:   117
0695  deg
Mean anomaly:     243
1052  deg
Mean motion:   15
73859201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1075
Checksum:              314


Coasting Arc #8 (Orbit 1090)
---------------------------------------

Vector Time (GMT): 2010/088/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2860823
52                 A    =         6723807
47  meter
 Y    =        4201901
56  meter          E    =           
0013575
 Z    =        4389750
72                 I    =           51
30584
 XDOT =      -3662
099837                 Wp   =           87
19706
 YDOT =       5934
223395  meter/sec      RA   =          279
51585  deg
 ZDOT =      -3284
286800                 TA   =           35
93639
                                          MA   =           35
84517
                                          Ha   =            191
982  n
mi
                                          Hp   =            181
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9385903
93                 X    =         2792299
89
 Y    =       13785766
26  feet           Y    =         4233510
37  meter
 Z    =       14402069
28                 Z    =         4403481
64
 XDOT =     -12014
763244                 XDOT =       -3712
230754
 YDOT =      19469
236861  feet/sec       YDOT =        5892
990933  meter/sec
 ZDOT =     -10775
219161                 ZDOT =       -3302
199722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         125265
91                 X    =           38181
05
 Y    =       16629779
63  feet           Y    =         5068756
83  meter
 Z    =       14456724
43                 Z    =         4406409
61
 XDOT =     -19511
415631                 XDOT =       -5947
079484
 YDOT =       9602
524178  feet/sec       YDOT =        2926
849369  meter/sec
 ZDOT =     -10846
181941                 ZDOT =       -3305
916256


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   10088
43214814  
00016717  00000-0  10270-3 0  9078
2 25544  51
6463 280
0511 0005578 118
6857 241
4868 15
73966253 10916


Satellite: ISS
Catalog Number: 25544
Epoch time:      10088
43214814   =   yrday
fracday
Element set:     907
Inclination:       51
6463  deg
RA of node:       280
0511  deg
Eccentricity:     
0005578     
Arg of perigee:   118
6857  deg
Mean anomaly:     241
4868  deg
Mean motion:   15
73966253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1091
Checksum:              318


Coasting Arc #9 (Orbit 1106)
---------------------------------------

Vector Time (GMT): 2010/089/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2711104
74                 A    =         6728745
64  meter
 Y    =       -5449963
41  meter          E    =           
0018006
 Z    =        2853430
37                 I    =           51
31768
 XDOT =       3702
405440                 Wp   =           92
91583
 YDOT =       4496
351146  meter/sec      RA   =          274
40422  deg
 ZDOT =       5041
886485                 TA   =          300
02216
                                          MA   =          300
20069
                                          Ha   =            192
020  n
mi
                                          Hp   =            182
056

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8894700
59                 X    =         2757984
20
 Y    =      -17880457
37  feet           Y    =        -5419383
80  meter
 Z    =        9361648
20                 Z    =         2866715
43
 XDOT =      12146
999474                 XDOT =        3627
358577
 YDOT =      14751
808222  feet/sec       YDOT =        4537
334575  meter/sec
 ZDOT =      16541
622325                 ZDOT =        5059
690079

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17078191
07                 X    =         5205432
64
 Y    =      -10304092
74  feet           Y    =        -3140687
47  meter
 Z    =        9414243
15                 Z    =         2869461
31
 XDOT =       1455
298883                 XDOT =         443
575099
 YDOT =      17674
135619  feet/sec       YDOT =        5387
076537  meter/sec
 ZDOT =      16612
461762                 ZDOT =        5063
478345


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   10089
44802193  
00016717  00000-0  10270-3 0  9084
2 25544  51
6454 274
8342 0005540 122
3926 237
7774 15
73949174 11072


Satellite: ISS
Catalog Number: 25544
Epoch time:      10089
44802193   =   yrday
fracday
Element set:     908
Inclination:       51
6454  deg
RA of node:       274
8342  deg
Eccentricity:     
0005540     
Arg of perigee:   122
3926  deg
Mean anomaly:     237
7774  deg
Mean motion:   15
73949174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1107
Checksum:              320


Coasting Arc #10 (Orbit 1121)
---------------------------------------

Vector Time (GMT): 2010/090/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3573540
77                 A    =         6723716
13  meter
 Y    =       -3639081
41  meter          E    =           
0014718
 Z    =       -4396309
30                 I    =           51
29963
 XDOT =       2543
695931                 Wp   =          116
59227
 YDOT =      -6467
530616  meter/sec      RA   =          269
19644  deg
 ZDOT =       3287
911145                 TA   =          186
62601
                                          MA   =          186
64549
                                          Ha   =            191
906  n
mi
                                          Hp   =            181
984

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11724215
12                 X    =        -3511225
66
 Y    =      -11939243
47  feet           Y    =        -3678694
82  meter
 Z    =      -14423586
93                 Z    =        -4413518
02
 XDOT =       8345
459092                 XDOT =        2599
855748
 YDOT =     -21218
932467  feet/sec       YDOT =       -6438
771207  meter/sec
 ZDOT =      10787
110056                 ZDOT =        3300
405489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3656243
50                 X    =        -1114423
02
 Y    =      -16268229
67  feet           Y    =        -4958556
40  meter
 Z    =      -14492039
25                 Z    =        -4417173
56
 XDOT =      16986
660287                 XDOT =        5177
534055
 YDOT =     -13465
267104  feet/sec       YDOT =       -4104
213413  meter/sec
 ZDOT =      10836
533447                 ZDOT =        3302
975395


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   10090
40038052  
00016717  00000-0  10270-3 0  9098
2 25544  51
6449 269
9429 0005481 126
7314 233
4353 15
73999640 11226


Satellite: ISS
Catalog Number: 25544
Epoch time:      10090
40038052   =   yrday
fracday
Element set:     909
Inclination:       51
6449  deg
RA of node:       269
9429  deg
Eccentricity:     
0005481     
Arg of perigee:   126
7314  deg
Mean anomaly:     233
4353  deg
Mean motion:   15
73999640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1122
Checksum:              308


Coasting Arc #11 (Orbit 1137)
---------------------------------------

Vector Time (GMT): 2010/091/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1742853
53                 A    =         6728414
53  meter
 Y    =        5809512
01  meter          E    =           
0009855
 Z    =       -2912841
99                 I    =           51
31677
 XDOT =      -4423
537129                 Wp   =          122
94803
 YDOT =      -3826
681539  meter/sec      RA   =          264
08536  deg
 ZDOT =      -5002
883095                 TA   =           90
73367
                                          MA   =           90
62075
                                          Ha   =            191
784  n
mi
                                          Hp   =            182
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5718023
38                 X    =        -1793536
80
 Y    =       19060078
78  feet           Y    =         5789738
83  meter
 Z    =       -9556568
19                 Z    =        -2921432
31
 XDOT =     -14512
917089                 XDOT =       -4356
114388
 YDOT =     -12554
729459  feet/sec       YDOT =       -3875
771482  meter/sec
 ZDOT =     -16413
658448                 ZDOT =       -5024
208839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14579694
01                 X    =        -4443890
73
 Y    =       13519062
92  feet           Y    =         4120610
38  meter
 Z    =       -9590508
35                 Z    =        -2923186
94
 XDOT =      -5026
005525                 XDOT =       -1531
926484
 YDOT =     -17083
803579  feet/sec       YDOT =       -5207
143331  meter/sec
 ZDOT =     -16498
469133                 ZDOT =       -5028
733392


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   10091
41620771  
00016717  00000-0  10270-3 0  9107
2 25544  51
6444 264
7266 0005401 130
9749 229
1882 15
74014891 11387


Satellite: ISS
Catalog Number: 25544
Epoch time:      10091
41620771   =   yrday
fracday
Element set:     910
Inclination:       51
6444  deg
RA of node:       264
7266  deg
Eccentricity:     
0005401     
Arg of perigee:   130
9749  deg
Mean anomaly:     229
1882  deg
Mean motion:   15
74014891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1138
Checksum:              298


Coasting Arc #12 (Orbit 1153)
---------------------------------------

Vector Time (GMT): 2010/092/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4139606
28                 A    =         6723602
18  meter
 Y    =        3016196
15  meter          E    =           
0012617
 Z    =        4344671
21                 I    =           51
30607
 XDOT =      -1410
057761                 Wp   =           92
16469
 YDOT =       6790
715831  meter/sec      RA   =          258
87715  deg
 ZDOT =      -3362
879619                 TA   =           31
85964
                                          MA   =           31
78339
                                          Ha   =            191
491  n
mi
                                          Hp   =            182
161

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13581385
43                 X    =         4084465
17
 Y    =        9895656
67  feet           Y    =         3062179
53  meter
 Z    =       14254170
64                 Z    =         4364647
53
 XDOT =      -4626
173757                 XDOT =       -1469
551566
 YDOT =      22279
251415  feet/sec       YDOT =        6774
614960  meter/sec
 ZDOT =     -11033
069617                 ZDOT =       -3369
874488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6839193
08                 X    =         2084586
05
 Y    =       15275232
30  feet           Y    =         4655890
81  meter
 Z    =       14333602
05                 Z    =         4368881
91
 XDOT =     -13866
144738                 XDOT =       -4226
400916
 YDOT =      16611
389865  feet/sec       YDOT =        5063
151631  meter/sec
 ZDOT =     -11060
644797                 ZDOT =       -3371
284534


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   10092
43200992  
00016717  00000-0  10270-3 0  9110
2 25544  51
6448 259
5093 0005260 134
7985 225
3607 15
74088594 11540


Satellite: ISS
Catalog Number: 25544
Epoch time:      10092
43200992   =   yrday
fracday
Element set:     911
Inclination:       51
6448  deg
RA of node:       259
5093  deg
Eccentricity:     
0005260     
Arg of perigee:   134
7985  deg
Mean anomaly:     225
3607  deg
Mean motion:   15
74088594  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1154
Checksum:              314


Coasting Arc #13 (Orbit 1169)
---------------------------------------

Vector Time (GMT): 2010/093/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         725457
30                 A    =         6728009
06  meter
 Y    =       -5991140
98  meter          E    =           
0016818
 Z    =        2962889
60                 I    =           51
32695
 XDOT =       5028
995126                 Wp   =           98
19678
 YDOT =       3074
383458  meter/sec      RA   =          253
76585  deg
 ZDOT =       4958
887033                 TA   =          296
16993
                                          MA   =          296
34280
                                          Ha   =            191
498  n
mi
                                          Hp   =            182
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2380109
26                 X    =          778004
14
 Y    =      -19655974
34  feet           Y    =        -5982734
63  meter
 Z    =        9720766
39                 Z    =         2966541
62
 XDOT =      16499
327842                 XDOT =        4970
153551
 YDOT =      10086
559900  feet/sec       YDOT =        3130
291756  meter/sec
 ZDOT =      16269
314412                 ZDOT =        4983
175035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11461578
28                 X    =         3493489
06
 Y    =      -16136164
93  feet           Y    =        -4918303
07  meter
 Z    =        9735088
67                 Z    =         2967255
03
 XDOT =       8383
035603                 XDOT =        2555
149252
 YDOT =      15880
283029  feet/sec       YDOT =        4840
310267  meter/sec
 ZDOT =      16365
879945                 ZDOT =        4988
320207


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   10093
44778926  
00016717  00000-0  10270-3 0  9120
2 25544  51
6436 254
2919 0005280 139
5058 220
6499 15
74120542 11707


Satellite: ISS
Catalog Number: 25544
Epoch time:      10093
44778926   =   yrday
fracday
Element set:     912
Inclination:       51
6436  deg
RA of node:       254
2919  deg
Eccentricity:     
0005280     
Arg of perigee:   139
5058  deg
Mean anomaly:     220
6499  deg
Mean motion:   15
74120542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1170
Checksum:              311


Coasting Arc #14 (Orbit 1184)
---------------------------------------

Vector Time (GMT): 2010/094/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4619247
13                 A    =         6723674
79  meter
 Y    =       -2352766
05  meter          E    =           
0013701
 Z    =       -4296355
60                 I    =           51
32136
 XDOT =        279
250493                 Wp   =          122
46107
 YDOT =      -6861
783140  meter/sec      RA   =          248
55705  deg
 ZDOT =       3458
188052                 TA   =          182
71336
                                          MA   =          182
72080
                                          Ha   =            191
469  n
mi
                                          Hp   =            182
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15155010
27                 X    =        -4571723
82
 Y    =       -7719048
71  feet           Y    =        -2404155
53  meter
 Z    =      -14095654
87                 Z    =        -4318680
48
 XDOT =        916
176159                 XDOT =         339
160151
 YDOT =     -22512
411876  feet/sec       YDOT =       -6858
325393  meter/sec
 ZDOT =      11345
761327                 ZDOT =        3459
690231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9765609
12                 X    =        -2976557
66
 Y    =      -13834049
96  feet           Y    =        -4216618
43  meter
 Z    =      -14184409
59                 Z    =        -4323408
04
 XDOT =      10194
498896                 XDOT =        3107
283263
 YDOT =     -18832
795343  feet/sec       YDOT =       -5740
236021  meter/sec
 ZDOT =      11351
514513                 ZDOT =        3459
941624


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   10094
40006121  
00016717  00000-0  10270-3 0  9139
2 25544  51
6427 249
4000 0005354 141
7714 218
3830 15
74138091 11857


Satellite: ISS
Catalog Number: 25544
Epoch time:      10094
40006121   =   yrday
fracday
Element set:     913
Inclination:       51
6427  deg
RA of node:       249
4000  deg
Eccentricity:     
0005354     
Arg of perigee:   141
7714  deg
Mean anomaly:     218
3830  deg
Mean motion:   15
74138091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1185
Checksum:              270


Coasting Arc #15 (Orbit 1200)
---------------------------------------

Vector Time (GMT): 2010/095/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         211180
40                 A    =         6727480
52  meter
 Y    =        5967502
84  meter          E    =           
0009200
 Z    =       -3098901
38                 I    =           51
34634
 XDOT =      -5502
252292                 Wp   =          126
17413
 YDOT =      -2319
708839  meter/sec      RA   =          243
44852  deg
 ZDOT =      -4857
359396                 TA   =           89
97213
                                          MA   =           89
86671
                                          Ha   =            191
320  n
mi
                                          Hp   =            182
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         692849
10                 X    =          159488
89
 Y    =       19578421
39  feet           Y    =         5969575
33  meter
 Z    =      -10166999
27                 Z    =        -3098001
08
 XDOT =     -18052
008831                 XDOT =       -5452
307834
 YDOT =      -7610
593305  feet/sec       YDOT =       -2380
959089  meter/sec
 ZDOT =     -15936
218491                 ZDOT =       -4883
967935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8116735
07                 X    =        -2473980
85
 Y    =       17832269
35  feet           Y    =         5435275
70  meter
 Z    =      -10163231
75                 Z    =        -3097753
04
 XDOT =     -11329
374412                 XDOT =       -3453
193321
 YDOT =     -14270
942347  feet/sec       YDOT =       -4349
783227  meter/sec
 ZDOT =     -16041
999452                 ZDOT =       -4889
601433


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   10095
41579318  
00016717  00000-0  10270-3 0  9145
2 25544  51
6423 244
1833 0005260 144
5252 215
6262 15
74182292 12013


Satellite: ISS
Catalog Number: 25544
Epoch time:      10095
41579318   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:       244
1833  deg
Eccentricity:     
0005260     
Arg of perigee:   144
5252  deg
Mean anomaly:     215
6262  deg
Mean motion:   15
74182292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1201
Checksum:              282


Coasting Arc #16 (Orbit 1216)
---------------------------------------

Vector Time (GMT): 2010/096/09:22:05
671
Vector Time (MET): N/A
Weight (LBS)     : 782571
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4976460
83                 A    =         6723845
13  meter
 Y    =        1675492
39  meter          E    =           
0012409
 Z    =        4188038
11                 I    =           51
34881
 XDOT =        778
158165                 Wp   =           97
89660
 YDOT =       6759
448020  meter/sec      RA   =          238
24036  deg
 ZDOT =      -3621
420384                 TA   =           29
12350
                                          MA   =           29
05436
                                          Ha   =            191
089  n
mi
                                          Hp   =            182
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16326971
24                 X    =         4937010
69
 Y    =        5497022
28  feet           Y    =         1730921
64  meter
 Z    =       13740282
51                 Z    =         4212117
77
 XDOT =       2553
012353                 XDOT =         720
107086
 YDOT =      22176
666733  feet/sec       YDOT =        6767
825196  meter/sec
 ZDOT =     -11881
300474                 ZDOT =       -3617
781250

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12256908
85                 X    =         3735905
82
 Y    =       11996487
46  feet           Y    =         3656529
38  meter
 Z    =       13836006
70                 Z    =         4217214
84
 XDOT =      -6374
947848                 XDOT =       -1943
084104
 YDOT =      20227
582120  feet/sec       YDOT =        6165
367030  meter/sec
 ZDOT =     -11866
618659                 ZDOT =       -3616
945367


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   10096
43150034  
00016717  00000-0  10270-3 0  9159
2 25544  51
6421 238
9653 0005255 149
9110 210
2356 15
74202859 12172


Satellite: ISS
Catalog Number: 25544
Epoch time:      10096
43150034   =   yrday
fracday
Element set:     915
Inclination:       51
6421  deg
RA of node:       238
9653  deg
Eccentricity:     
0005255     
Arg of perigee:   149
9110  deg
Mean anomaly:     210
2356  deg
Mean motion:   15
74202859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1217
Checksum:              285

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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