Date: February 7th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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


There are no maneuvers



Coasting Arc #1 (Orbit 241)
---------------------------------------

Vector Time (GMT): 2010/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2917649
44                 A    =         6716487
98  meter
 Y    =       -3337149
60  meter          E    =           
0008138
 Z    =        5052916
56                 I    =           51
52789
 XDOT =       6731
228793                 Wp   =          303
83728
 YDOT =       3333
876095  meter/sec      RA   =          196
09654  deg
 ZDOT =      -1682
389144                 TA   =          162
38691
                                          MA   =          162
35867
                                          Ha   =            185
807  n
mi
                                          Hp   =            183
794

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9572340
68                 X    =         2930203
45
 Y    =      -10948653
54  feet           Y    =        -3304452
43  meter
 Z    =       16577810
22                 Z    =         5067120
81
 XDOT =      22084
083968                 XDOT =        6701
621126
 YDOT =      10937
913696  feet/sec       YDOT =        3408
983109  meter/sec
 ZDOT =      -5519
649422                 ZDOT =       -1649
761367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14470765
42                 X    =         4410689
30
 Y    =        -483400
15  feet           Y    =         -147340
36  meter
 Z    =       16633994
85                 Z    =         5070041
63
 XDOT =       6960
525226                 XDOT =        2121
568089
 YDOT =      22605
223140  feet/sec       YDOT =        6890
072013  meter/sec
 ZDOT =      -5390
137080                 ZDOT =       -1642
913782


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   10034
54478490  
00016717  00000-0  10270-3 0  9006
2 25544  51
6406 196
9055 0011011 278
2414  81
7501 15
75582575  2421


Satellite: ISS
Catalog Number: 25544
Epoch time:      10034
54478490   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:       196
9055  deg
Eccentricity:     
0011011     
Arg of perigee:   278
2414  deg
Mean anomaly:      81
7501  deg
Mean motion:   15
75582575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             242
Checksum:              291


Coasting Arc #2 (Orbit 257)
---------------------------------------

Vector Time (GMT): 2010/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5797324
89                 A    =         6725717
17  meter
 Y    =       -2744366
44  meter          E    =           
0007866
 Z    =        2005974
00                 I    =           51
59001
 XDOT =       3723
214129                 Wp   =           16
97557
 YDOT =      -3786
310708  meter/sec      RA   =          190
97490  deg
 ZDOT =       5582
075611                 TA   =            5
41549
                                          MA   =            5
40699
                                          Ha   =            186
131  n
mi
                                          Hp   =            183
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19020094
77                 X    =        -5775950
55
 Y    =       -9003826
91  feet           Y    =        -2809076
05  meter
 Z    =        6581279
52                 Z    =         1977862
92
 XDOT =      12215
269453                 XDOT =        3738
160279
 YDOT =     -12422
279225  feet/sec       YDOT =       -3744
591939  meter/sec
 ZDOT =      18313
896360                 ZDOT =        5600
199040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6683037
13                 X    =        -2036989
72
 Y    =      -19990653
69  feet           Y    =        -6093151
24  meter
 Z    =        6469692
75                 Z    =         1971962
35
 XDOT =      15887
911952                 XDOT =        4842
635563
 YDOT =        636
717332  feet/sec       YDOT =         194
071443  meter/sec
 ZDOT =      18385
609061                 ZDOT =        5603
933642


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   10035
55955433  
00016717  00000-0  10270-3 0  9016
2 25544  51
6415 191
6814 0011089 281
9771  78
0149 15
75676602  2587


Satellite: ISS
Catalog Number: 25544
Epoch time:      10035
55955433   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       191
6814  deg
Eccentricity:     
0011089     
Arg of perigee:   281
9771  deg
Mean anomaly:      78
0149  deg
Mean motion:   15
75676602  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             258
Checksum:              317


Coasting Arc #3 (Orbit 272)
---------------------------------------

Vector Time (GMT): 2010/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3572748
21                 A    =         6717966
84  meter
 Y    =        3319492
92  meter          E    =           
0000694
 Z    =       -4620243
24                 I    =           51
59472
 XDOT =      -6495
087991                 Wp   =          216
59625
 YDOT =      -2963
006141  meter/sec      RA   =          185
78407  deg
 ZDOT =       2892
938055                 TA   =           82
04471
                                          MA   =           82
03683
                                          Ha   =            186
374  n
mi
                                          Hp   =            183
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11721614
85                 X    =        -3587157
83
 Y    =       10890724
80  feet           Y    =         3279459
84  meter
 Z    =      -15158278
34                 Z    =        -4637634
36
 XDOT =     -21309
343802                 XDOT =       -6475
525583
 YDOT =      -9721
148755  feet/sec       YDOT =       -3035
528729  meter/sec
 ZDOT =       9491
266586                 ZDOT =        2861
432815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15923634
09                 X    =        -4853523
67
 Y    =        -591954
04  feet           Y    =         -180427
59  meter
 Z    =      -15227114
36                 Z    =        -4641224
46
 XDOT =      -8183
668565                 XDOT =       -2494
382179
 YDOT =     -20854
268288  feet/sec       YDOT =       -6356
380974  meter/sec
 ZDOT =       9366
200617                 ZDOT =        2854
817948


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   10036
51088204  
00016717  00000-0  10270-3 0  9027
2 25544  51
6421 186
7847 0011036 286
1348  73
8601 15
75693239  2732


Satellite: ISS
Catalog Number: 25544
Epoch time:      10036
51088204   =   yrday
fracday
Element set:     902
Inclination:       51
6421  deg
RA of node:       186
7847  deg
Eccentricity:     
0011036     
Arg of perigee:   286
1348  deg
Mean anomaly:      73
8601  deg
Mean motion:   15
75693239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             273
Checksum:              303


Coasting Arc #4 (Orbit 288)
---------------------------------------

Vector Time (GMT): 2010/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5477058
00                 A    =         6723334
43  meter
 Y    =        2458564
79  meter          E    =           
0006553
 Z    =       -3024315
92                 I    =           51
64297
 XDOT =      -4468
406110                 Wp   =          291
34241
 YDOT =       3859
602489  meter/sec      RA   =          180
68039  deg
 ZDOT =      -4943
822385                 TA   =          283
66816
                                          MA   =          283
74111
                                          Ha   =            186
726  n
mi
                                          Hp   =            183
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17969350
40                 X    =         5463850
19
 Y    =        8066157
45  feet           Y    =         2519738
75  meter
 Z    =       -9922296
32                 Z    =        -2997740
77
 XDOT =     -14660
125032                 XDOT =       -4487
216926
 YDOT =      12662
737826  feet/sec       YDOT =        3809
529103  meter/sec
 ZDOT =     -16219
889714                 ZDOT =       -4965
575151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7282641
30                 X    =         2219749
07
 Y    =       18357726
91  feet           Y    =         5595435
16  meter
 Z    =       -9816792
38                 Z    =        -2992158
32
 XDOT =     -17929
536684                 XDOT =       -5464
922781
 YDOT =      -1626
186779  feet/sec       YDOT =        -495
661730  meter/sec
 ZDOT =     -16306
012836                 ZDOT =       -4970
072712


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   10037
52560813  
00016717  00000-0  10270-3 0  9031
2 25544  51
6419 181
5604 0011078 290
5935  69
4040 15
75738184  2894


Satellite: ISS
Catalog Number: 25544
Epoch time:      10037
52560813   =   yrday
fracday
Element set:     903
Inclination:       51
6419  deg
RA of node:       181
5604  deg
Eccentricity:     
0011078     
Arg of perigee:   290
5935  deg
Mean anomaly:      69
4040  deg
Mean motion:   15
75738184  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             289
Checksum:              309


Coasting Arc #5 (Orbit 304)
---------------------------------------

Vector Time (GMT): 2010/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4207563
05                 A    =         6720367
85  meter
 Y    =       -3458671
85  meter          E    =           
0006679
 Z    =        3941043
59                 I    =           51
66363
 XDOT =       5988
160404                 Wp   =            6
75886
 YDOT =       2707
583133  meter/sec      RA   =          175
48235  deg
 ZDOT =      -4009
738048                 TA   =          124
87974
                                          MA   =          124
81693
                                          Ha   =            186
939  n
mi
                                          Hp   =            183
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13804340
73                 X    =         4226781
28
 Y    =      -11347348
60  feet           Y    =        -3411513
10  meter
 Z    =       12929933
04                 Z    =         3961530
11
 XDOT =      19646
195552                 XDOT =        5976
916916
 YDOT =       8883
146761  feet/sec       YDOT =        2774
483594  meter/sec
 ZDOT =     -13155
308556                 ZDOT =       -3980
675273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17773574
20                 X    =         5417385
42
 Y    =        1147890
88  feet           Y    =          349877
14  meter
 Z    =       13011061
38                 Z    =         3965771
51
 XDOT =       8355
855104                 XDOT =        2546
864636
 YDOT =      18690
866389  feet/sec       YDOT =        5696
976075  meter/sec
 ZDOT =     -13039
914666                 ZDOT =       -3974
565990


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   10038
54031194  
00016717  00000-0  10270-3 0  9040
2 25544  51
6420 176
3360 0011018 294
2711  65
7302 15
75745372  3050


Satellite: ISS
Catalog Number: 25544
Epoch time:      10038
54031194   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:       176
3360  deg
Eccentricity:     
0011018     
Arg of perigee:   294
2711  deg
Mean anomaly:      65
7302  deg
Mean motion:   15
75745372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             305
Checksum:              274


Coasting Arc #6 (Orbit 320)
---------------------------------------

Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4925473
31                 A    =         6720306
16  meter
 Y    =       -2319401
19  meter          E    =           
0003497
 Z    =        3936336
34                 I    =           51
69515
 XDOT =       5140
045613                 Wp   =           20
18849
 YDOT =      -4092
824598  meter/sec      RA   =          170
38799  deg
 ZDOT =       4022
212773                 TA   =           28
11300
                                          MA   =           28
09412
                                          Ha   =            187
197  n
mi
                                          Hp   =            183
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16159689
34                 X    =        -4918292
89
 Y    =       -7609583
94  feet           Y    =        -2374440
78  meter
 Z    =       12914489
30                 Z    =         3912426
24
 XDOT =      16863
666709                 XDOT =        5165
891522
 YDOT =     -13427
902225  feet/sec       YDOT =       -4035
201235  meter/sec
 ZDOT =      13196
236132                 ZDOT =        4047
245170

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6891268
11                 X    =        -2100458
52
 Y    =      -16552800
80  feet           Y    =        -5045293
68  meter
 Z    =       12819538
64                 Z    =         3907395
38
 XDOT =      20245
581557                 XDOT =        6170
853259
 YDOT =       1862
596878  feet/sec       YDOT =         567
719528  meter/sec
 ZDOT =      13295
385642                 ZDOT =        4052
433544


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   10039
55498973  
00016717  00000-0  10270-3 0  9055
2 25544  51
6431 171
1114 0011139 298
3094  61
6946 15
75833405  3217


Satellite: ISS
Catalog Number: 25544
Epoch time:      10039
55498973   =   yrday
fracday
Element set:     905
Inclination:       51
6431  deg
RA of node:       171
1114  deg
Eccentricity:     
0011139     
Arg of perigee:   298
3094  deg
Mean anomaly:      61
6946  deg
Mean motion:   15
75833405  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             321
Checksum:              306


Coasting Arc #7 (Orbit 335)
---------------------------------------

Vector Time (GMT): 2010/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4711869
54                 A    =         6722932
33  meter
 Y    =        3711743
68  meter          E    =           
0008977
 Z    =       -3022906
36                 I    =           51
73414
 XDOT =      -5270
274263                 Wp   =          325
94694
 YDOT =      -2652
371666  meter/sec      RA   =          165
19429  deg
 ZDOT =       4958
362965                 TA   =          359
07942
                                          MA   =          359
08107
                                          Ha   =            187
376  n
mi
                                          Hp   =            182
973

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15458889
56                 X    =        -4738340
36
 Y    =       12177636
73  feet           Y    =         3658904
88  meter
 Z    =       -9917671
78                 Z    =        -3045860
18
 XDOT =     -17290
926061                 XDOT =       -5264
309495
 YDOT =      -8702
006778  feet/sec       YDOT =       -2711
273849  meter/sec
 ZDOT =      16267
595031                 ZDOT =        4932
775002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19606851
50                 X    =        -5976168
34
 Y    =       -1015664
62  feet           Y    =         -309574
58  meter
 Z    =      -10008602
09                 Z    =        -3050621
92
 XDOT =      -7392
751765                 XDOT =       -2253
310738
 YDOT =     -16582
302675  feet/sec       YDOT =       -5054
285855  meter/sec
 ZDOT =      16165
961239                 ZDOT =        4927
384986


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   10040
50623146  
00016717  00000-0  10270-3 0  9065
2 25544  51
6435 166
2141 0011216 302
9767  57
0319 15
75822455  3363


Satellite: ISS
Catalog Number: 25544
Epoch time:      10040
50623146   =   yrday
fracday
Element set:     906
Inclination:       51
6435  deg
RA of node:       166
2141  deg
Eccentricity:     
0011216     
Arg of perigee:   302
9767  deg
Mean anomaly:      57
0319  deg
Mean motion:   15
75822455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             336
Checksum:              282


Coasting Arc #8 (Orbit 351)
---------------------------------------

Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4227698
48                 A    =         6717531
99  meter
 Y    =        2373221
94  meter          E    =           
0010366
 Z    =       -4655392
97                 I    =           51
74550
 XDOT =      -5624
216739                 Wp   =            6
47887
 YDOT =       4421
100554  meter/sec      RA   =          160
09866  deg
 ZDOT =      -2844
240528                 TA   =          235
40687
                                          MA   =          235
50470
                                          Ha   =            187
625  n
mi
                                          Hp   =            182
796

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13870401
84                 X    =         4223460
89
 Y    =        7786161
23  feet           Y    =         2420475
01  meter
 Z    =      -15273599
00                 Z    =        -4634865
63
 XDOT =     -18452
154657                 XDOT =       -5659
419858
 YDOT =      14504
923079  feet/sec       YDOT =        4358
010482  meter/sec
 ZDOT =      -9331
497795                 ZDOT =       -2871
647565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5607358
29                 X    =         1709122
81
 Y    =       14968449
19  feet           Y    =         4562383
31  meter
 Z    =      -15192045
35                 Z    =        -4630535
42
 XDOT =     -22320
592111                 XDOT =       -6803
316475
 YDOT =      -1251
310722  feet/sec       YDOT =        -381
399508  meter/sec
 ZDOT =      -9440
082624                 ZDOT =       -2877
337184


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   10041
52086557  
00016717  00000-0  10270-3 0  9078
2 25544  51
6440 160
9899 0011224 306
6988  53
3144 15
75866988  3527


Satellite: ISS
Catalog Number: 25544
Epoch time:      10041
52086557   =   yrday
fracday
Element set:     907
Inclination:       51
6440  deg
RA of node:       160
9899  deg
Eccentricity:     
0011224     
Arg of perigee:   306
6988  deg
Mean anomaly:      53
3144  deg
Mean motion:   15
75866988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             352
Checksum:              329


Coasting Arc #9 (Orbit 367)
---------------------------------------

Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5057944
93                 A    =         6725159
87  meter
 Y    =       -4009197
20  meter          E    =           
0004958
 Z    =        1889851
53                 I    =           51
80015
 XDOT =       4380
917079                 Wp   =           68
72261
 YDOT =       2857
689275  meter/sec      RA   =          154
91945  deg
 ZDOT =      -5648
976409                 TA   =           90
32542
                                          MA   =           90
26860
                                          Ha   =            187
739  n
mi
                                          Hp   =            182
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16594307
50                 X    =         5093220
29
 Y    =      -13153534
11  feet           Y    =        -3952439
05  meter
 Z    =        6200300
29                 Z    =         1914507
90
 XDOT =      14373
087531                 XDOT =        4376
077153
 YDOT =       9375
620982  feet/sec       YDOT =        2906
652297  meter/sec
 ZDOT =     -18533
387168                 ZDOT =       -5627
706291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21143879
77                 X    =         6444654
55
 Y    =         319089
52  feet           Y    =           97258
49  meter
 Z    =        6297996
08                 Z    =         1919629
21
 XDOT =       5283
633243                 XDOT =        1610
451413
 YDOT =      14888
094736  feet/sec       YDOT =        4537
891276  meter/sec
 ZDOT =     -18448
856046                 ZDOT =       -5623
211323


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   10042
53547650  
00016717  00000-0  10270-3 0  9087
2 25544  51
6444 155
7654 0011140 310
9550  49
0649 15
75902929  3687


Satellite: ISS
Catalog Number: 25544
Epoch time:      10042
53547650   =   yrday
fracday
Element set:     908
Inclination:       51
6444  deg
RA of node:       155
7654  deg
Eccentricity:     
0011140     
Arg of perigee:   310
9550  deg
Mean anomaly:      49
0649  deg
Mean motion:   15
75902929  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             368
Checksum:              308


Coasting Arc #10 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3408557
61                 A    =         6715164
77  meter
 Y    =       -2685624
77  meter          E    =           
0006722
 Z    =        5127147
81                 I    =           51
79489
 XDOT =       5895
509381                 Wp   =          321
81902
 YDOT =      -4742
417418  meter/sec      RA   =          149
81012  deg
 ZDOT =       1441
445145                 TA   =          114
43821
                                          MA   =          114
36807
                                          Ha   =            187
929  n
mi
                                          Hp   =            182
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11182931
79                 X    =        -3403179
12
 Y    =       -8811104
88  feet           Y    =        -2723711
17  meter
 Z    =       16821351
09                 Z    =         5110602
65
 XDOT =      19342
222378                 XDOT =        5941
099710
 YDOT =     -15559
112264  feet/sec       YDOT =       -4676
235419  meter/sec
 ZDOT =       4729
150739                 ZDOT =        1470
195387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3382454
05                 X    =        -1030971
99
 Y    =      -13909033
24  feet           Y    =        -4239473
33  meter
 Z    =       16755571
73                 Z    =         5107098
26
 XDOT =      23786
302250                 XDOT =        7250
064926
 YDOT =         25
270925  feet/sec       YDOT =           7
702578  meter/sec
 ZDOT =       4843
074961                 ZDOT =        1476
169248


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   10043
55006212  
00016717  00000-0  10270-3 0  9095
2 25544  51
6454 150
5403 0011263 315
2224  44
8030 15
75982805  3841


Satellite: ISS
Catalog Number: 25544
Epoch time:      10043
55006212   =   yrday
fracday
Element set:     909
Inclination:       51
6454  deg
RA of node:       150
5403  deg
Eccentricity:     
0011263     
Arg of perigee:   315
2224  deg
Mean anomaly:      44
8030  deg
Mean motion:   15
75982805  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              270


Coasting Arc #11 (Orbit 398)
---------------------------------------

Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5167858
37                 A    =         6726428
22  meter
 Y    =        4245249
20  meter          E    =           
0016981
 Z    =        -602660
18                 I    =           51
85853
 XDOT =      -3453
689590                 Wp   =          359
29002
 YDOT =      -3351
044560  meter/sec      RA   =          144
65559  deg
 ZDOT =       6025
111340                 TA   =          354
15759
                                          MA   =          354
17737
                                          Ha   =            188
170  n
mi
                                          Hp   =            181
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16954915
91                 X    =        -5212017
89
 Y    =       13927982
95  feet           Y    =         4187212
22  meter
 Z    =       -1977231
57                 Z    =         -627872
23
 XDOT =     -11331
002593                 XDOT =       -3445
228929
 YDOT =     -10994
240683  feet/sec       YDOT =       -3389
618305  meter/sec
 ZDOT =      19767
425656                 ZDOT =        6008
354472

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21918676
84                 X    =        -6680812
70
 Y    =         790205
39  feet           Y    =          240854
60  meter
 Z    =       -2077139
45                 Z    =         -633112
11
 XDOT =      -2370
396560                 XDOT =        -722
496872
 YDOT =     -14086
063170  feet/sec       YDOT =       -4293
432054  meter/sec
 ZDOT =      19700
772492                 ZDOT =        6004
795456


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   10044
50121727  
00016717  00000-0  10270-3 0  9102
2 25544  51
6457 145
6427 0011372 319
9440  40
0884 15
75962004  3997


Satellite: ISS
Catalog Number: 25544
Epoch time:      10044
50121727   =   yrday
fracday
Element set:     910
Inclination:       51
6457  deg
RA of node:       145
6427  deg
Eccentricity:     
0011372     
Arg of perigee:   319
9440  deg
Mean anomaly:      40
0884  deg
Mean motion:   15
75962004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             399
Checksum:              293


Coasting Arc #12 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2624040
03                 A    =         6714342
80  meter
 Y    =        3218192
56  meter          E    =           
0012293
 Z    =       -5283397
48                 I    =           51
84202
 XDOT =      -5901
159875                 Wp   =           42
87304
 YDOT =       4943
306386  meter/sec      RA   =          139
52642  deg
 ZDOT =         89
122793                 TA   =          227
91822
                                          MA   =          228
02283
                                          Ha   =            188
323  n
mi
                                          Hp   =            181
516

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8609055
22                 X    =         2613523
66
 Y    =       10558374
55  feet           Y    =         3247477
10  meter
 Z    =      -17333981
25                 Z    =        -5270675
95
 XDOT =     -19360
760744                 XDOT =       -5956
431149
 YDOT =      16218
196803  feet/sec       YDOT =        4877
007081  meter/sec
 ZDOT =        292
397616                 ZDOT =          60
321318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         752738
06                 X    =          229434
56
 Y    =       13666794
58  feet           Y    =         4165638
99  meter
 Z    =      -17283348
11                 Z    =        -5267964
50
 XDOT =     -24211
276056                 XDOT =       -7379
596942
 YDOT =       1521
735158  feet/sec       YDOT =         463
824876  meter/sec
 ZDOT =        178
262311                 ZDOT =          54
334352


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   10045
51575877  
00016717  00000-0  10270-3 0  9114
2 25544  51
6455 140
4185 0011387 323
6056  36
4333 15
76020393  4154


Satellite: ISS
Catalog Number: 25544
Epoch time:      10045
51575877   =   yrday
fracday
Element set:     911
Inclination:       51
6455  deg
RA of node:       140
4185  deg
Eccentricity:     
0011387     
Arg of perigee:   323
6056  deg
Mean anomaly:      36
4333  deg
Mean motion:   15
76020393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              292


Coasting Arc #13 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5091695
80                 A    =         6726093
68  meter
 Y    =       -4326942
84  meter          E    =           
0001577
 Z    =        -778589
42                 I    =           51
90332
 XDOT =       2564
338484                 Wp   =           25
18531
 YDOT =       4095
130437  meter/sec      RA   =          134
40047  deg
 ZDOT =      -5991
494852                 TA   =          163
27180
                                          MA   =          163
26660
                                          Ha   =            188
391  n
mi
                                          Hp   =            181
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16705038
71                 X    =         5143484
17
 Y    =      -14196006
70  feet           Y    =        -4269714
96  meter
 Z    =       -2554427
22                 Z    =         -753728
54
 XDOT =       8413
184002                 XDOT =        2547
460287
 YDOT =      13435
467313  feet/sec       YDOT =        4123
711668  meter/sec
 ZDOT =     -19657
135342                 ZDOT =       -5979
078849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21851785
82                 X    =         6660424
32
 Y    =       -1891563
90  feet           Y    =         -576548
68  meter
 Z    =       -2455904
24                 Z    =         -748559
61
 XDOT =       -964
813834                 XDOT =        -294
075256
 YDOT =      14298
417388  feet/sec       YDOT =        4358
157620  meter/sec
 ZDOT =     -19607
677183                 ZDOT =       -5976
420005


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   10046
53027737  
00016717  00000-0  10270-3 0  9125
2 25544  51
6446 135
1936 0011310 327
8133  32
2340 15
76051530  4314


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
53027737   =   yrday
fracday
Element set:     912
Inclination:       51
6446  deg
RA of node:       135
1936  deg
Eccentricity:     
0011310     
Arg of perigee:   327
8133  deg
Mean anomaly:      32
2340  deg
Mean motion:   15
76051530  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              263


Coasting Arc #14 (Orbit 446)
---------------------------------------

Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1893405
14                 A    =         6714949
61  meter
 Y    =       -3974603
18  meter          E    =           
0013130
 Z    =        5074646
35                 I    =           51
88731
 XDOT =       5704
726546                 Wp   =          354
40501
 YDOT =      -4889
473515  meter/sec      RA   =          129
24559  deg
 ZDOT =      -1688
645263                 TA   =          111
84756
                                          MA   =          111
70786
                                          Ha   =            188
519  n
mi
                                          Hp   =            180
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6211959
12                 X    =        -1873470
90
 Y    =      -13040036
68  feet           Y    =        -3995664
56  meter
 Z    =       16649102
19                 Z    =         5065497
07
 XDOT =      18716
294443                 XDOT =        5767
180481
 YDOT =     -16041
579775  feet/sec       YDOT =       -4825
330795  meter/sec
 ZDOT =      -5540
174749                 ZDOT =       -1660
780260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2160834
52                 X    =          658622
36
 Y    =      -14323941
70  feet           Y    =        -4365937
43  meter
 Z    =       16612618
24                 Z    =         5063526
04
 XDOT =      23488
185592                 XDOT =        7159
198968
 YDOT =      -2801
402614  feet/sec       YDOT =        -853
867517  meter/sec
 ZDOT =      -5429
740898                 ZDOT =       -1654
985026


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   10047
54477047  
00016717  00000-0  10270-3 0  9131
2 25544  51
6452 129
9675 0011497 331
6773  28
3765 15
76129407  4474


Satellite: ISS
Catalog Number: 25544
Epoch time:      10047
54477047   =   yrday
fracday
Element set:     913
Inclination:       51
6452  deg
RA of node:       129
9675  deg
Eccentricity:     
0011497     
Arg of perigee:   331
6773  deg
Mean anomaly:      28
3765  deg
Mean motion:   15
76129407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             447
Checksum:              329


Coasting Arc #15 (Orbit 462)
---------------------------------------

Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4833166
95                 A    =         6724180
38  meter
 Y    =        4135521
23  meter          E    =           
0017544
 Z    =        2143556
44                 I    =           51
93580
 XDOT =      -1840
240779                 Wp   =           29
62917
 YDOT =      -5029
591645  meter/sec      RA   =          124
14687  deg
 ZDOT =       5550
022572                 TA   =          354
29985
                                          MA   =          354
31979
                                          Ha   =            188
768  n
mi
                                          Hp   =            180
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15856846
96                 X    =        -4889464
71
 Y    =       13567983
02  feet           Y    =         4081159
26  meter
 Z    =        7032665
50                 Z    =         2119940
28
 XDOT =      -6037
535365                 XDOT =       -1810
822778
 YDOT =     -16501
284925  feet/sec       YDOT =       -5050
005437  meter/sec
 ZDOT =      18208
735472                 ZDOT =        5541
154640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20741980
89                 X    =        -6322155
77
 Y    =        2570558
99  feet           Y    =          783506
38  meter
 Z    =        6939063
22                 Z    =         2115026
47
 XDOT =       4145
580732                 XDOT =        1263
573007
 YDOT =     -15644
556527  feet/sec       YDOT =       -4768
460829  meter/sec
 ZDOT =      18173
328890                 ZDOT =        5539
230646


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   10048
55924271  
00016717  00000-0  10270-3 0  9140
2 25544  51
6445 124
7422 0011459 336
3680  23
6956 15
76128322  4639


Satellite: ISS
Catalog Number: 25544
Epoch time:      10048
55924271   =   yrday
fracday
Element set:     914
Inclination:       51
6445  deg
RA of node:       124
7422  deg
Eccentricity:     
0011459     
Arg of perigee:   336
3680  deg
Mean anomaly:      23
6956  deg
Mean motion:   15
76128322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              303

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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