Date: December 15th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 95 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 3436)
---------------------------------------

Vector Time (GMT): 2009/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3008168
72                 A    =         6721842
22  meter
 Y    =       -5381379
00  meter          E    =           
0011486
 Z    =       -2686022
32                 I    =           51
98486
 XDOT =       3405
974762                 Wp   =           97
81670
 YDOT =       4504
380548  meter/sec      RA   =           99
29292  deg
 ZDOT =      -5230
383602                 TA   =          112
64590
                                          MA   =          112
52439
                                          Ha   =            188
900  n
mi
                                          Hp   =            177
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9869319
96                 X    =         3081169
07
 Y    =      -17655442
90  feet           Y    =        -5347331
32  meter
 Z    =       -8812409
17                 Z    =        -2671231
88
 XDOT =      11174
457881                 XDOT =        3380
761466
 YDOT =      14778
151403  feet/sec       YDOT =        4542
327952  meter/sec
 ZDOT =     -17160
051187                 ZDOT =       -5213
897727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16214058
02                 X    =         4942044
88
 Y    =       12134570
87  feet           Y    =         3698617
20  meter
 Z    =       -8754039
55                 Z    =        -2668231
25
 XDOT =     -15234
756431                 XDOT =       -4643
553760
 YDOT =       8072
833854  feet/sec       YDOT =        2460
599759  meter/sec
 ZDOT =     -17094
706250                 ZDOT =       -5210
466465


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   09348
52640251  
00016717  00000-0  10270-3 0  9006
2 25544  51
6439  99
9460 0007448  80
3331 279
8675 15
76542327 34371


Satellite: ISS
Catalog Number: 25544
Epoch time:      09348
52640251   =   yrday
fracday
Element set:     900
Inclination:       51
6439  deg
RA of node:        99
9460  deg
Eccentricity:     
0007448     
Arg of perigee:    80
3331  deg
Mean anomaly:     279
8675  deg
Mean motion:   15
76542327  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3437
Checksum:              331


Coasting Arc #2 (Orbit 3452)
---------------------------------------

Vector Time (GMT): 2009/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2856251
30                 A    =         6717801
21  meter
 Y    =       -4516666
07  meter          E    =           
0018279
 Z    =        4057635
52                 I    =           51
97547
 XDOT =       3456
770626                 Wp   =           79
78410
 YDOT =      -5693
745961  meter/sec      RA   =           94
11465  deg
 ZDOT =      -3886
720683                 TA   =           50
07155
                                          MA   =           49
91107
                                          Ha   =            189
006  n
mi
                                          Hp   =            177
133

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9370903
22                 X    =        -2825244
33
 Y    =      -14818458
24  feet           Y    =        -4548433
62  meter
 Z    =       13312452
48                 Z    =         4043834
31
 XDOT =      11341
110978                 XDOT =        3539
063355
 YDOT =     -18680
268901  feet/sec       YDOT =       -5654
629580  meter/sec
 ZDOT =     -12751
708276                 ZDOT =       -3869
728514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15791659
98                 X    =         4813297
96
 Y    =       -7712195
43  feet           Y    =        -2350677
17  meter
 Z    =       13257731
30                 Z    =         4040956
50
 XDOT =      16707
298772                 XDOT =        5092
384666
 YDOT =      12303
484265  feet/sec       YDOT =        3750
102004  meter/sec
 ZDOT =     -12684
620146                 ZDOT =       -3866
272221


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   09349
54058844  
00016717  00000-0  10270-3 0  9011
2 25544  51
6445  94
7192 0007584  83
6846 276
5182 15
76546966 34539


Satellite: ISS
Catalog Number: 25544
Epoch time:      09349
54058844   =   yrday
fracday
Element set:     901
Inclination:       51
6445  deg
RA of node:        94
7192  deg
Eccentricity:     
0007584     
Arg of perigee:    83
6846  deg
Mean anomaly:     276
5182  deg
Mean motion:   15
76546966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3453
Checksum:              354


Coasting Arc #3 (Orbit 3468)
---------------------------------------

Vector Time (GMT): 2009/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3048218
01                 A    =         6717816
45  meter
 Y    =        4446827
16  meter          E    =           
0018278
 Z    =        3993684
85                 I    =           51
97788
 XDOT =      -3204
954827                 Wp   =           95
58366
 YDOT =      -5781
176272  meter/sec      RA   =           89
03481  deg
 ZDOT =       3973
764452                 TA   =          313
49417
                                          MA   =          313
64597
                                          Ha   =            188
865  n
mi
                                          Hp   =            177
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10000715
25                 X    =        -3117117
37
 Y    =       14589327
94  feet           Y    =         4412354
30  meter
 Z    =       13102640
58                 Z    =         3978709
87
 XDOT =     -10514
943657                 XDOT =       -3159
374441
 YDOT =     -18967
113754  feet/sec       YDOT =       -5816
761755  meter/sec
 ZDOT =      13037
284948                 ZDOT =        3958
304470

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13554991
56                 X    =        -4131561
43
 Y    =      -11431165
80  feet           Y    =        -3484219
34  meter
 Z    =       13043490
24                 Z    =         3975655
83
 XDOT =      19062
252843                 XDOT =        5810
174667
 YDOT =      -7733
165665  feet/sec       YDOT =       -2357
068895  meter/sec
 ZDOT =      12975
971001                 ZDOT =        3955
075961


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   09350
55475479  
00016717  00000-0  10270-3 0  9022
2 25544  51
6452  89
4915 0007478  87
0252 273
1768 15
76622198 34694


Satellite: ISS
Catalog Number: 25544
Epoch time:      09350
55475479   =   yrday
fracday
Element set:     902
Inclination:       51
6452  deg
RA of node:        89
4915  deg
Eccentricity:     
0007478     
Arg of perigee:    87
0252  deg
Mean anomaly:     273
1768  deg
Mean motion:   15
76622198  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3469
Checksum:              350


Coasting Arc #4 (Orbit 3483)
---------------------------------------

Vector Time (GMT): 2009/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2757202
48                 A    =         6721524
51  meter
 Y    =        5477885
82  meter          E    =           
0011783
 Z    =       -2757251
12                 I    =           51
98860
 XDOT =      -3599
385092                 Wp   =           76
72083
 YDOT =       4409
667126  meter/sec      RA   =           83
85604  deg
 ZDOT =       5182
486514                 TA   =          251
91619
                                          MA   =          252
04457
                                          Ha   =            188
822  n
mi
                                          Hp   =            177
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9045939
91                 X    =         2709137
13
 Y    =       17972066
33  feet           Y    =         5508450
17  meter
 Z    =       -9046099
48                 Z    =        -2743972
49
 XDOT =     -11809
006206                 XDOT =       -3673
602867
 YDOT =      14467
411830  feet/sec       YDOT =        4369
000884  meter/sec
 ZDOT =      17002
908509                 ZDOT =        5164
821093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18633336
15                 X    =        -5679440
86
 Y    =        7653312
03  feet           Y    =         2332729
51  meter
 Z    =       -8993426
03                 Z    =        -2741196
25
 XDOT =     -12925
704230                 XDOT =       -3939
754649
 YDOT =     -11653
345447  feet/sec       YDOT =       -3551
939692  meter/sec
 ZDOT =      16933
099774                 ZDOT =        5161
208811


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   09351
50552362  
00016717  00000-0  10270-3 0  9036
2 25544  51
6454  84
5916 0007400  88
7226 271
4786 15
76592790 34849


Satellite: ISS
Catalog Number: 25544
Epoch time:      09351
50552362   =   yrday
fracday
Element set:     903
Inclination:       51
6454  deg
RA of node:        84
5916  deg
Eccentricity:     
0007400     
Arg of perigee:    88
7226  deg
Mean anomaly:     271
4786  deg
Mean motion:   15
76592790  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3484
Checksum:              329


Coasting Arc #5 (Orbit 3499)
---------------------------------------

Vector Time (GMT): 2009/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3303628
47                 A    =         6714238
95  meter
 Y    =       -3167657
03  meter          E    =           
0019681
 Z    =       -4930157
92                 I    =           51
95955
 XDOT =       3097
782462                 Wp   =           80
90525
 YDOT =       6679
319819  meter/sec      RA   =           78
76536  deg
 ZDOT =      -2220
162413                 TA   =          167
61477
                                          MA   =          167
56633
                                          Ha   =            188
760  n
mi
                                          Hp   =            177
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10838676
08                 X    =         3362754
00
 Y    =      -10392575
55  feet           Y    =        -3130382
58  meter
 Z    =      -16175058
80                 Z    =        -4913965
78
 XDOT =      10163
328288                 XDOT =        3033
648026
 YDOT =      21913
778933  feet/sec       YDOT =        6713
602787  meter/sec
 ZDOT =      -7283
997417                 ZDOT =       -2205
268200

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9698686
71                 X    =         2956159
71
 Y    =       11553561
08  feet           Y    =         3521525
42  meter
 Z    =      -16111044
52                 Z    =        -4910646
37
 XDOT =     -21658
979521                 XDOT =       -6601
656958
 YDOT =       8127
226786  feet/sec       YDOT =        2477
178724  meter/sec
 ZDOT =      -7224
904146                 ZDOT =       -2202
150784


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   09352
51966014  
00016717  00000-0  10270-3 0  9042
2 25544  51
6451  79
3639 0007407  93
2418 266
9594 15
76623648 35003


Satellite: ISS
Catalog Number: 25544
Epoch time:      09352
51966014   =   yrday
fracday
Element set:     904
Inclination:       51
6451  deg
RA of node:        79
3639  deg
Eccentricity:     
0007407     
Arg of perigee:    93
2418  deg
Mean anomaly:     266
9594  deg
Mean motion:   15
76623648  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3500
Checksum:              329


Coasting Arc #6 (Orbit 3515)
---------------------------------------

Vector Time (GMT): 2009/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2654632
96                 A    =         6724147
00  meter
 Y    =       -6076656
75  meter          E    =           
0020828
 Z    =        1063846
41                 I    =           51
98559
 XDOT =       4018
794615                 Wp   =          113
89508
 YDOT =      -2811
250660  meter/sec      RA   =           73
60579  deg
 ZDOT =      -5947
187479                 TA   =           54
50608
                                          MA   =           54
31193
                                          Ha   =            188
778  n
mi
                                          Hp   =            176
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8709425
73                 X    =        -2591653
37
 Y    =      -19936537
90  feet           Y    =        -6105990
43  meter
 Z    =        3490309
73                 Z    =         1051102
41
 XDOT =      13185
021704                 XDOT =        4078
822056
 YDOT =      -9223
263321  feet/sec       YDOT =       -2765
973693  meter/sec
 ZDOT =     -19511
769944                 ZDOT =       -5927
518832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20305291
23                 X    =         6189052
77
 Y    =       -7833596
68  feet           Y    =        -2387680
27  meter
 Z    =        3439740
29                 Z    =         1048432
84
 XDOT =       8051
366107                 XDOT =        2454
056389
 YDOT =      12215
797594  feet/sec       YDOT =        3723
375107  meter/sec
 ZDOT =     -19433
982109                 ZDOT =       -5923
477747


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   09353
53378075  
00016717  00000-0  10270-3 0  9050
2 25544  51
6445  74
1363 0007588  96
3540 263
8489 15
76658852 35164


Satellite: ISS
Catalog Number: 25544
Epoch time:      09353
53378075   =   yrday
fracday
Element set:     905
Inclination:       51
6445  deg
RA of node:        74
1363  deg
Eccentricity:     
0007588     
Arg of perigee:    96
3540  deg
Mean anomaly:     263
8489  deg
Mean motion:   15
76658852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3516
Checksum:              348


Coasting Arc #7 (Orbit 3531)
---------------------------------------

Vector Time (GMT): 2009/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3760224
85                 A    =         6712338
81  meter
 Y    =        1727942
38  meter          E    =           
0009822
 Z    =        5276708
16                 I    =           51
93722
 XDOT =      -2977
209370                 Wp   =           99
28802
 YDOT =      -7112
783837  meter/sec      RA   =           68
48438  deg
 ZDOT =        205
736359                 TA   =          348
75966
                                          MA   =          348
78159
                                          Ha   =            188
723  n
mi
                                          Hp   =            176
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12336695
71                 X    =        -3804900
69
 Y    =        5669102
29  feet           Y    =         1685642
91  meter
 Z    =       17312034
65                 Z    =         5258332
77
 XDOT =      -9767
747277                 XDOT =       -2898
451124
 YDOT =     -23335
904978  feet/sec       YDOT =       -7145
636414  meter/sec
 ZDOT =        674
988056                 ZDOT =         191
463617

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5327562
67                 X    =        -1623841
10
 Y    =      -12588153
78  feet           Y    =        -3836869
27  meter
 Z    =       17239338
32                 Z    =         5254550
32
 XDOT =      22676
231197                 XDOT =        6911
715269
 YDOT =      -8741
763393  feet/sec       YDOT =       -2664
489482  meter/sec
 ZDOT =        618
346879                 ZDOT =         188
472129


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   09354
54788286  
00016717  00000-0  10270-3 0  9062
2 25544  51
6449  68
9078 0007404  99
6998 260
5004 15
76725099 35325


Satellite: ISS
Catalog Number: 25544
Epoch time:      09354
54788286   =   yrday
fracday
Element set:     906
Inclination:       51
6449  deg
RA of node:        68
9078  deg
Eccentricity:     
0007404     
Arg of perigee:    99
6998  deg
Mean anomaly:     260
5004  deg
Mean motion:   15
76725099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3532
Checksum:              361


Coasting Arc #8 (Orbit 3547)
---------------------------------------

Vector Time (GMT): 2009/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2481246
25                 A    =         6724297
75  meter
 Y    =        6201492
32  meter          E    =           
0019306
 Z    =         719998
45                 I    =           51
96444
 XDOT =      -4679
592130                 Wp   =           69
63298
 YDOT =       1160
159671  meter/sec      RA   =           63
35621  deg
 ZDOT =       6011
793835                 TA   =          298
18749
                                          MA   =          298
38235
                                          Ha   =            188
696  n
mi
                                          Hp   =            176
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8140571
69                 X    =         2408218
06
 Y    =       20346103
40  feet           Y    =         6228830
68  meter
 Z    =        2362199
64                 Z    =          731875
53
 XDOT =     -15352
992553                 XDOT =       -4721
421503
 YDOT =       3806
298132  feet/sec       YDOT =        1107
595222  meter/sec
 ZDOT =      19723
733055                 ZDOT =        5988
958999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20427402
24                 X    =        -6226272
20
 Y    =        7920173
43  feet           Y    =         2414068
86  meter
 Z    =        2409337
83                 Z    =          734366
17
 XDOT =      -3072
424927                 XDOT =        -936
475118
 YDOT =     -14016
421450  feet/sec       YDOT =       -4272
205258  meter/sec
 ZDOT =      19633
370732                 ZDOT =        5984
251399


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   09355
56197299  
00016717  00000-0  10270-3 0  9074
2 25544  51
6444  63
6799 0007550 101
6512 258
5500 15
76691842 35483


Satellite: ISS
Catalog Number: 25544
Epoch time:      09355
56197299   =   yrday
fracday
Element set:     907
Inclination:       51
6444  deg
RA of node:        63
6799  deg
Eccentricity:     
0007550     
Arg of perigee:   101
6512  deg
Mean anomaly:     258
5500  deg
Mean motion:   15
76691842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3548
Checksum:              341


Coasting Arc #9 (Orbit 3562)
---------------------------------------

Vector Time (GMT): 2009/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4450074
71                 A    =         6713506
65  meter
 Y    =        -312216
47  meter          E    =           
0020723
 Z    =       -5035583
10                 I    =           51
91300
 XDOT =       2606
728739                 Wp   =          104
14558
 YDOT =       6987
790244  meter/sec      RA   =           58
19854  deg
 ZDOT =       1871
813027                 TA   =          183
86218
                                          MA   =          183
87820
                                          Ha   =            188
596  n
mi
                                          Hp   =            177
029

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14599982
64                 X    =         4477697
10
 Y    =       -1024332
27  feet           Y    =         -262298
23  meter
 Z    =      -16520941
92                 Z    =        -5013897
63
 XDOT =       8552
259642                 XDOT =        2519
303402
 YDOT =      22925
821010  feet/sec       YDOT =        7016
451242  meter/sec
 ZDOT =       6141
118856                 ZDOT =        1884
264725

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1128718
26                 X    =          344033
33
 Y    =       14688886
91  feet           Y    =         4477172
73  meter
 Z    =      -16435110
83                 Z    =        -5009421
78
 XDOT =     -21794
001176                 XDOT =       -6642
811559
 YDOT =       8595
864561  feet/sec       YDOT =        2620
019518  meter/sec
 ZDOT =       6190
544147                 ZDOT =        1886
877856


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   09356
51266506  
00016717  00000-0  10270-3 0  9089
2 25544  51
6436  58
7781 0007513 104
8562 255
3436 15
76732408 35633


Satellite: ISS
Catalog Number: 25544
Epoch time:      09356
51266506   =   yrday
fracday
Element set:     908
Inclination:       51
6436  deg
RA of node:        58
7781  deg
Eccentricity:     
0007513     
Arg of perigee:   104
8562  deg
Mean anomaly:     255
3436  deg
Mean motion:   15
76732408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3563
Checksum:              326


Coasting Arc #10 (Orbit 3578)
---------------------------------------

Vector Time (GMT): 2009/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1980627
10                 A    =         6721538
70  meter
 Y    =       -5912654
17  meter          E    =           
0012662
 Z    =       -2509911
54                 I    =           51
92387
 XDOT =       5533
543792                 Wp   =          116
77350
 YDOT =        402
136213  meter/sec      RA   =           53
09870  deg
 ZDOT =      -5340
067242                 TA   =           91
54326
                                          MA   =           91
39821
                                          Ha   =            188
564  n
mi
                                          Hp   =            176
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6498120
39                 X    =        -1902170
86
 Y    =      -19398471
70  feet           Y    =        -5934363
85  meter
 Z    =       -8234617
92                 Z    =        -2519343
31
 XDOT =      18154
671232                 XDOT =        5554
576842
 YDOT =       1319
344532  feet/sec       YDOT =         464
133580  meter/sec
 ZDOT =     -17519
905648                 ZDOT =       -5313
134169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19236378
64                 X    =         5863248
21
 Y    =       -6918807
62  feet           Y    =        -2108852
56  meter
 Z    =       -8272064
02                 Z    =        -2521325
11
 XDOT =      -1379
833486                 XDOT =        -420
573247
 YDOT =      16880
888895  feet/sec       YDOT =        5145
294935  meter/sec
 ZDOT =     -17413
289353                 ZDOT =       -5307
570595


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   09357
52672292  
00016717  00000-0  10270-3 0  9095
2 25544  51
6438  53
5491 0007636 108
3287 251
8708 15
76765540 35798


Satellite: ISS
Catalog Number: 25544
Epoch time:      09357
52672292   =   yrday
fracday
Element set:     909
Inclination:       51
6438  deg
RA of node:        53
5491  deg
Eccentricity:     
0007636     
Arg of perigee:   108
3287  deg
Mean anomaly:     251
8708  deg
Mean motion:   15
76765540  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3579
Checksum:              347


Coasting Arc #11 (Orbit 3594)
---------------------------------------

Vector Time (GMT): 2009/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5202066
01                 A    =         6716797
22  meter
 Y    =        -923364
58  meter          E    =           
0017114
 Z    =        4132813
76                 I    =           51
88941
 XDOT =      -1857
374937                 Wp   =           90
11108
 YDOT =      -6468
524933  meter/sec      RA   =           47
91394  deg
 ZDOT =      -3769
859682                 TA   =           38
34790
                                          MA   =           38
22635
                                          Ha   =            188
525  n
mi
                                          Hp   =            176
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17067145
70                 X    =        -5211430
68
 Y    =       -3029411
35  feet           Y    =         -981589
82  meter
 Z    =       13559100
27                 Z    =         4107519
23
 XDOT =      -6093
749793                 XDOT =       -1766
591356
 YDOT =     -21222
194662  feet/sec       YDOT =       -6488
787322  meter/sec
 ZDOT =     -12368
306044                 ZDOT =       -3778
662800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2315426
97                 X    =          705742
14
 Y    =      -17257147
55  feet           Y    =        -5259978
57  meter
 Z    =       13458961
77                 Z    =         4102291
55
 XDOT =      19696
137934                 XDOT =        6003
382842
 YDOT =      -7064
940014  feet/sec       YDOT =       -2153
393716  meter/sec
 ZDOT =     -12403
268017                 ZDOT =       -3780
516091


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   09358
54076321  
00016717  00000-0  10270-3 0  9101
2 25544  51
6441  48
3205 0007445 111
4580 248
7380 15
76821172 35959


Satellite: ISS
Catalog Number: 25544
Epoch time:      09358
54076321   =   yrday
fracday
Element set:     910
Inclination:       51
6441  deg
RA of node:        48
3205  deg
Eccentricity:     
0007445     
Arg of perigee:   111
4580  deg
Mean anomaly:     248
7380  deg
Mean motion:   15
76821172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3595
Checksum:              304


Coasting Arc #12 (Orbit 3610)
---------------------------------------

Vector Time (GMT): 2009/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1152245
45                 A    =         6717324
13  meter
 Y    =        5298846
45  meter          E    =           
0018562
 Z    =        3953203
71                 I    =           51
86995
 XDOT =      -6382
040427                 Wp   =          106
39992
 YDOT =      -1620
946314  meter/sec      RA   =           42
82554  deg
 ZDOT =       4012
324264                 TA   =          302
09503
                                          MA   =          302
27509
                                          Ha   =            188
461  n
mi
                                          Hp   =            176
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3780332
85                 X    =         1073703
11
 Y    =       17384666
84  feet           Y    =         5311292
08  meter
 Z    =       12969828
44                 Z    =         3958610
99
 XDOT =     -20938
452845                 XDOT =       -6382
931663
 YDOT =      -5318
065336  feet/sec       YDOT =       -1692
319358  meter/sec
 ZDOT =      13163
793517                 ZDOT =        3981
317815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17137806
56                 X    =        -5223603
44
 Y    =        4717537
67  feet           Y    =         1437905
48  meter
 Z    =       12991321
41                 Z    =         3959754
76
 XDOT =       4420
058040                 XDOT =        1347
233691
 YDOT =     -20041
211315  feet/sec       YDOT =       -6108
561209  meter/sec
 ZDOT =      13041
036549                 ZDOT =        3974
907940


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   09359
55479059  
00016717  00000-0  10270-3 0  9119
2 25544  51
6439  43
0917 0007680 114
8033 245
3931 15
76816375 36112


Satellite: ISS
Catalog Number: 25544
Epoch time:      09359
55479059   =   yrday
fracday
Element set:     911
Inclination:       51
6439  deg
RA of node:        43
0917  deg
Eccentricity:     
0007680     
Arg of perigee:   114
8033  deg
Mean anomaly:     245
3931  deg
Mean motion:   15
76816375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3611
Checksum:              325


Coasting Arc #13 (Orbit 3625)
---------------------------------------

Vector Time (GMT): 2009/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5870322
10                 A    =         6720862
17  meter
 Y    =        1818172
05  meter          E    =           
0010914
 Z    =       -2731462
24                 I    =           51
85992
 XDOT =        655
937413                 Wp   =           94
49771
 YDOT =       5648
397419  meter/sec      RA   =           37
63579  deg
 ZDOT =       5186
339181                 TA   =          234
41056
                                          MA   =          234
51232
                                          Ha   =            188
403  n
mi
                                          Hp   =            176
874

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19259586
95                 X    =         5862823
75
 Y    =        5965131
39  feet           Y    =         1883775
78  meter
 Z    =       -8961490
29                 Z    =        -2702962
00
 XDOT =       2152
025633                 XDOT =         567
532764
 YDOT =      18531
487596  feet/sec       YDOT =        5655
237729  meter/sec
 ZDOT =      17015
548494                 ZDOT =        5189
311533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4483664
02                 X    =        -1366620
79
 Y    =       19708396
21  feet           Y    =         6007119
16  meter
 Z    =       -8848653
35                 Z    =        -2697069
54
 XDOT =     -16885
828792                 XDOT =       -5146
800616
 YDOT =       3778
308596  feet/sec       YDOT =        1151
628460  meter/sec
 ZDOT =      17027
401705                 ZDOT =        5189
952040


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   09360
50542677  
00016717  00000-0  10270-3 0  9124
2 25544  51
6446  38
1897 0007725 117
9882 242
2065 15
76863156 36267


Satellite: ISS
Catalog Number: 25544
Epoch time:      09360
50542677   =   yrday
fracday
Element set:     912
Inclination:       51
6446  deg
RA of node:        38
1897  deg
Eccentricity:     
0007725     
Arg of perigee:   117
9882  deg
Mean anomaly:     242
2065  deg
Mean motion:   15
76863156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3626
Checksum:              335


Coasting Arc #14 (Orbit 3641)
---------------------------------------

Vector Time (GMT): 2009/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         118470
03                 A    =         6713416
37  meter
 Y    =       -4546627
84  meter          E    =           
0018914
 Z    =       -4954028
80                 I    =           51
81083
 XDOT =       6969
820202                 Wp   =           91
47581
 YDOT =       2475
055397  meter/sec      RA   =           32
53229  deg
 ZDOT =      -2112
215258                 TA   =          158
11541
                                          MA   =          158
03451
                                          Ha   =            188
354  n
mi
                                          Hp   =            176
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         388681
19                 X    =          193368
43
 Y    =      -14916758
02  feet           Y    =        -4544883
71  meter
 Z    =      -16253375
33                 Z    =        -4953271
85
 XDOT =      22866
864181                 XDOT =        6951
886545
 YDOT =       8120
260489  feet/sec       YDOT =        2552
896009  meter/sec
 ZDOT =      -6929
840086                 ZDOT =       -2078
398808

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14897562
86                 X    =         4540777
16
 Y    =        -904798
21  feet           Y    =         -275782
49  meter
 Z    =      -16250443
48                 Z    =        -4953135
17
 XDOT =      -6021
619608                 XDOT =       -1835
389657
 YDOT =      22476
338139  feet/sec       YDOT =        6850
787865  meter/sec
 ZDOT =      -6795
953500                 ZDOT =       -2071
406627


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   09361
51942361  
00016717  00000-0  10270-3 0  9131
2 25544  51
6453  32
9605 0007653 121
5994 238
5918 15
76846322 36428


Satellite: ISS
Catalog Number: 25544
Epoch time:      09361
51942361   =   yrday
fracday
Element set:     913
Inclination:       51
6453  deg
RA of node:        32
9605  deg
Eccentricity:     
0007653     
Arg of perigee:   121
5994  deg
Mean anomaly:     238
5918  deg
Mean motion:   15
76846322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3642
Checksum:              323


Coasting Arc #15 (Orbit 3657)
---------------------------------------

Vector Time (GMT): 2009/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6199873
75                 A    =         6723656
17  meter
 Y    =       -2414419
24  meter          E    =           
0021300
 Z    =         896793
12                 I    =           51
81873
 XDOT =        984
373859                 Wp   =          124
86995
 YDOT =      -4778
237283  meter/sec      RA   =           27
36198  deg
 ZDOT =      -5971
667257                 TA   =           45
34600
                                          MA   =           45
17256
                                          Ha   =            188
285  n
mi
                                          Hp   =            176
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20340793
15                 X    =        -6176771
00
 Y    =       -7921322
96  feet           Y    =        -2483620
84  meter
 Z    =        2942234
65                 Z    =          866729
64
 XDOT =       3229
573028                 XDOT =        1066
741324
 YDOT =     -15676
631506  feet/sec       YDOT =       -4766
768067  meter/sec
 ZDOT =     -19592
084178                 ZDOT =       -5966
685713

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5632422
46                 X    =         1716762
37
 Y    =      -21105859
37  feet           Y    =        -6433065
93  meter
 Z    =        2823204
88                 Z    =          860512
85
 XDOT =      14410
911865                 XDOT =        4392
445937
 YDOT =       1187
741195  feet/sec       YDOT =         362
023516  meter/sec
 ZDOT =     -19572
426434                 ZDOT =       -5965
675577


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   09362
53340481  
00016717  00000-0  10270-3 0  9140
2 25544  51
6445  27
7314 0007687 124
3066 235
8827 15
76887487 36589


Satellite: ISS
Catalog Number: 25544
Epoch time:      09362
53340481   =   yrday
fracday
Element set:     914
Inclination:       51
6445  deg
RA of node:        27
7314  deg
Eccentricity:     
0007687     
Arg of perigee:   124
3066  deg
Mean anomaly:     235
8827  deg
Mean motion:   15
76887487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3658
Checksum:              343

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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