Date: July 2nd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 810)
---------------------------------------

Vector Time (GMT): 2009/181/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -22553
90                 A    =         6725265
01  meter
 Y    =        5492304
66  meter          E    =           
0009368
 Z    =       -3883173
60                 I    =           51
36154
 XDOT =      -5874
360299                 Wp   =          126
87886
 YDOT =      -2881
778464  meter/sec      RA   =          235
82049  deg
 ZDOT =      -4054
099541                 TA   =          100
77465
                                          MA   =          100
66917
                                          Ha   =            191
618  n
mi
                                          Hp   =            182
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -73995
74                 X    =          -65104
32
 Y    =       18019372
24  feet           Y    =         5491815
08  meter
 Z    =      -12740070
88                 Z    =        -3883385
75
 XDOT =     -19272
835626                 XDOT =       -5822
005043
 YDOT =      -9454
653752  feet/sec       YDOT =       -2947
175691  meter/sec
 ZDOT =     -13300
851513                 ZDOT =       -4082
510484

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13405353
01                 X    =        -4085951
60
 Y    =      -12041021
09  feet           Y    =        -3670103
23  meter
 Z    =      -12740603
56                 Z    =        -3883335
97
 XDOT =      18982
860433                 XDOT =        5785
975860
 YDOT =      -6984
671988  feet/sec       YDOT =       -2128
928022  meter/sec
 ZDOT =     -13412
420790                 ZDOT =       -4088
105857


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   09181
88395476  
00010596  00000-0  82463-4 0  9009
2 25544  51
6396 236
5844 0007542 171
0204 189
1095 15
74122983  8112


Satellite: ISS
Catalog Number: 25544
Epoch time:      09181
88395476   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:       236
5844  deg
Eccentricity:     
0007542     
Arg of perigee:   171
0204  deg
Mean anomaly:     189
1095  deg
Mean motion:   15
74122983  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             811
Checksum:              321


Coasting Arc #2 (Orbit 826)
---------------------------------------

Vector Time (GMT): 2009/182/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5337268
60                 A    =         6726459
55  meter
 Y    =        2098624
11  meter          E    =           
0014629
 Z    =        3497133
36                 I    =           51
38303
 XDOT =        489
670963                 Wp   =          118
63409
 YDOT =       6247
406279  meter/sec      RA   =          230
61367  deg
 ZDOT =      -4489
136975                 TA   =           19
58174
                                          MA   =           19
52561
                                          Ha   =            191
454  n
mi
                                          Hp   =            182
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17510723
74                 X    =         5296416
25
 Y    =        6885249
69  feet           Y    =         2158079
59  meter
 Z    =       11473534
63                 Z    =         3522962
99
 XDOT =       1606
532031                 XDOT =         441
582492
 YDOT =      20496
739761  feet/sec       YDOT =        6252
613903  meter/sec
 ZDOT =     -14728
139681                 ZDOT =       -4486
873960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16632416
99                 X    =        -5069560
70
 Y    =        8663568
18  feet           Y    =         2640655
58  meter
 Z    =       11574946
98                 Z    =         3528043
84
 XDOT =     -15958
815146                 XDOT =       -4864
246857
 YDOT =     -10941
221353  feet/sec       YDOT =       -3334
884268  meter/sec
 ZDOT =     -14718
923744                 ZDOT =       -4486
327957


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   09182
89971507  
00010596  00000-0  82463-4 0  9017
2 25544  51
6393 231
3675 0007558 175
0583 185
0656 15
74102693  8276


Satellite: ISS
Catalog Number: 25544
Epoch time:      09182
89971507   =   yrday
fracday
Element set:     901
Inclination:       51
6393  deg
RA of node:       231
3675  deg
Eccentricity:     
0007558     
Arg of perigee:   175
0583  deg
Mean anomaly:     185
0656  deg
Mean motion:   15
74102693  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             827
Checksum:              333


Coasting Arc #3 (Orbit 842)
---------------------------------------

Vector Time (GMT): 2009/183/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -862155
12                 A    =         6725117
05  meter
 Y    =       -5374515
38  meter          E    =           
0014596
 Z    =        3947263
42                 I    =           51
39828
 XDOT =       6317
193754                 Wp   =          131
12254
 YDOT =       1913
112155  meter/sec      RA   =          225
51113  deg
 ZDOT =       3965
671990                 TA   =          277
57116
                                          MA   =          277
73694
                                          Ha   =            191
458  n
mi
                                          Hp   =            183
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2828592
91                 X    =         -821167
43
 Y    =      -17632924
47  feet           Y    =        -5383928
03  meter
 Z    =       12950339
30                 Z    =         3943173
67
 XDOT =      20725
701293                 XDOT =        6276
066942
 YDOT =       6276
614683  feet/sec       YDOT =        1983
524054  meter/sec
 ZDOT =      13010
734874                 ZDOT =        3996
261433

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15380330
50                 X    =         4687924
74
 Y    =        9098856
67  feet           Y    =         2773331
51  meter
 Z    =       12934005
27                 Z    =         3942284
81
 XDOT =     -17409
985295                 XDOT =       -5306
563518
 YDOT =      10675
085836  feet/sec       YDOT =        3253
766163  meter/sec
 ZDOT =      13130
815635                 ZDOT =        4002
272606


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   09183
91547470  
00010596  00000-0  82463-4 0  9020
2 25544  51
6394 226
1499 0007490 178
9494 181
1686 15
74106707  8439


Satellite: ISS
Catalog Number: 25544
Epoch time:      09183
91547470   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:       226
1499  deg
Eccentricity:     
0007490     
Arg of perigee:   178
9494  deg
Mean anomaly:     181
1686  deg
Mean motion:   15
74106707  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             843
Checksum:              339


Coasting Arc #4 (Orbit 857)
---------------------------------------

Vector Time (GMT): 2009/184/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5667425
45                 A    =         6726649
00  meter
 Y    =       -1231337
47  meter          E    =           
0009003
 Z    =       -3419395
21                 I    =           51
42597
 XDOT =      -1452
748280                 Wp   =          149
09722
 YDOT =      -6012
504558  meter/sec      RA   =          220
30672  deg
 ZDOT =       4570
683932                 TA   =          170
38888
                                          MA   =          170
37164
                                          Ha   =            191
292  n
mi
                                          Hp   =            183
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18593915
53                 X    =        -5636624
42
 Y    =       -4039821
11  feet           Y    =        -1294541
07  meter
 Z    =      -11218488
23                 Z    =        -3446852
98
 XDOT =      -4766
234513                 XDOT =       -1407
611005
 YDOT =     -19726
064822  feet/sec       YDOT =       -6028
498540  meter/sec
 ZDOT =      14995
682192                 ZDOT =        4563
734966

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14794658
76                 X    =         4509411
99
 Y    =      -11863481
95  feet           Y    =        -3615989
30  meter
 Z    =      -11326261
32                 Z    =        -3452244
45
 XDOT =      17522
883340                 XDOT =        5340
974842
 YDOT =       7555
005436  feet/sec       YDOT =        2302
765657  meter/sec
 ZDOT =      14968
095235                 ZDOT =        4562
275428


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   09184
86774897  
00010596  00000-0  82463-4 0  9031
2 25544  51
6397 221
2585 0007449 182
7770 177
3353 15
74123436  8580


Satellite: ISS
Catalog Number: 25544
Epoch time:      09184
86774897   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       221
2585  deg
Eccentricity:     
0007449     
Arg of perigee:   182
7770  deg
Mean anomaly:     177
3353  deg
Mean motion:   15
74123436  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             858
Checksum:              351


Coasting Arc #5 (Orbit 873)
---------------------------------------

Vector Time (GMT): 2009/185/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1655409
71                 A    =         6724746
63  meter
 Y    =        5112890
40  meter          E    =           
0007781
 Z    =       -4043855
59                 I    =           51
44304
 XDOT =      -6603
294142                 Wp   =          129
91228
 YDOT =       -901
253370  meter/sec      RA   =          215
20724  deg
 ZDOT =      -3852
462423                 TA   =          100
34117
                                          MA   =          100
25345
                                          Ha   =            191
138  n
mi
                                          Hp   =            183
399

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5431134
21                 X    =         1617757
70
 Y    =       16774574
81  feet           Y    =         5131192
45  meter
 Z    =      -13267242
76                 Z    =        -4035904
08
 XDOT =     -21664
350858                 XDOT =       -6574
010911
 YDOT =      -2956
868013  feet/sec       YDOT =        -974
930764  meter/sec
 ZDOT =     -12639
312413                 ZDOT =       -3884
470161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16610694
87                 X    =        -5062939
80
 Y    =       -5983526
92  feet           Y    =        -1823779
01  meter
 Z    =      -13235767
10                 Z    =        -4034261
81
 XDOT =      15183
335749                 XDOT =        4627
880736
 YDOT =     -13984
850036  feet/sec       YDOT =       -4262
582291  meter/sec
 ZDOT =     -12764
931158                 ZDOT =       -3890
751017


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   09185
88350801  
00010596  00000-0  82463-4 0  9040
2 25544  51
6399 216
0412 0007363 187
3259 172
7798 15
74122415  8747


Satellite: ISS
Catalog Number: 25544
Epoch time:      09185
88350801   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       216
0412  deg
Eccentricity:     
0007363     
Arg of perigee:   187
3259  deg
Mean anomaly:     172
7798  deg
Mean motion:   15
74122415  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             874
Checksum:              327


Coasting Arc #6 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2009/186/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5831775
03                 A    =         6726978
68  meter
 Y    =         314891
65  meter          E    =           
0013454
 Z    =        3320752
69                 I    =           51
47491
 XDOT =       2358
661234                 Wp   =          123
34701
 YDOT =       5657
883621  meter/sec      RA   =          210
00702  deg
 ZDOT =      -4672
408995                 TA   =           17
46977
                                          MA   =           17
42353
                                          Ha   =            190
949  n
mi
                                          Hp   =            183
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19133120
19                 X    =         5811688
94
 Y    =        1033109
09  feet           Y    =          379993
00  meter
 Z    =       10894857
92                 Z    =         3349034
52
 XDOT =       7738
389874                 XDOT =        2317
916051
 YDOT =      18562
610306  feet/sec       YDOT =        5684
032669  meter/sec
 ZDOT =     -15329
425838                 ZDOT =       -4661
048541

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12302295
23                 X    =        -3749739
58
 Y    =       14607070
16  feet           Y    =         4452234
99  meter
 Z    =       11005842
31                 Z    =         3354580
74
 XDOT =     -18469
729580                 XDOT =       -5629
573576
 YDOT =      -4023
806526  feet/sec       YDOT =       -1226
456229  meter/sec
 ZDOT =     -15284
537844                 ZDOT =       -4658
727135


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   09186
89926804  
00010596  00000-0  82463-4 0  9055
2 25544  51
6391 210
8240 0007346 190
5042 169
5968 15
74103772  8903


Satellite: ISS
Catalog Number: 25544
Epoch time:      09186
89926804   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       210
8240  deg
Eccentricity:     
0007346     
Arg of perigee:   190
5042  deg
Mean anomaly:     169
5968  deg
Mean motion:   15
74103772  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             890
Checksum:              328


Coasting Arc #7 (Orbit 905)
---------------------------------------

Vector Time (GMT): 2009/187/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2434973
13                 A    =         6724597
38  meter
 Y    =       -4734234
06  meter          E    =           
0012714
 Z    =        4107730
04                 I    =           51
49336
 XDOT =       6716
776314                 Wp   =          139
05098
 YDOT =       -178
746150  meter/sec      RA   =          204
91001  deg
 ZDOT =       3759
540298                 TA   =          272
26873
                                          MA   =          272
41430
                                          Ha   =            190
931  n
mi
                                          Hp   =            183
784

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7988757
00                 X    =        -2401807
52
 Y    =      -15532263
97  feet           Y    =        -4761278
71  meter
 Z    =       13476804
59                 Z    =         4095980
71
 XDOT =      22036
667698                 XDOT =        6700
012929
 YDOT =       -586
437501  feet/sec       YDOT =        -103
729691  meter/sec
 ZDOT =      12334
449796                 ZDOT =        3792
129270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17306509
59                 X    =         5275024
12
 Y    =        2608434
71  feet           Y    =          795050
90  meter
 Z    =       13430432
54                 Z    =         4093595
84
 XDOT =     -12251
494257                 XDOT =       -3734
255450
 YDOT =      16848
532518  feet/sec       YDOT =        5135
432711  meter/sec
 ZDOT =      12462
323431                 ZDOT =        3798
516182


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   09187
91502665  
00010596  00000-0  82463-4 0  9065
2 25544  51
6394 205
6060 0007261 195
0137 165
0812 15
74103641  9061


Satellite: ISS
Catalog Number: 25544
Epoch time:      09187
91502665   =   yrday
fracday
Element set:     906
Inclination:       51
6394  deg
RA of node:       205
6060  deg
Eccentricity:     
0007261     
Arg of perigee:   195
0137  deg
Mean anomaly:     165
0812  deg
Mean motion:   15
74103641  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             906
Checksum:              296


Coasting Arc #8 (Orbit 920)
---------------------------------------

Vector Time (GMT): 2009/188/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5867839
77                 A    =         6727199
26  meter
 Y    =         630351
22  meter          E    =           
0006711
 Z    =       -3237837
28                 I    =           51
53006
 XDOT =      -3176
857666                 Wp   =          161
60570
 YDOT =      -5148
706790  meter/sec      RA   =          199
71339  deg
 ZDOT =       4751
376634                 TA   =          160
48911
                                          MA   =          160
46341
                                          Ha   =            190
700  n
mi
                                          Hp   =            183
911

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19251442
81                 X    =        -5858723
76
 Y    =        2068081
43  feet           Y    =          564785
17  meter
 Z    =      -10622825
73                 Z    =        -3266320
57
 XDOT =     -10422
761372                 XDOT =       -3142
128824
 YDOT =     -16892
082645  feet/sec       YDOT =       -5184
038961  meter/sec
 ZDOT =      15588
506017                 ZDOT =        4736
027097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9322021
91                 X    =         2841352
28
 Y    =      -16899946
92  feet           Y    =        -5151103
82  meter
 Z    =      -10734576
80                 Z    =        -3271899
01
 XDOT =      18634
107230                 XDOT =        5679
675884
 YDOT =        408
069625  feet/sec       YDOT =         124
379622  meter/sec
 ZDOT =      15527
970475                 ZDOT =        4732
925401


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   09188
86729968  
00010596  00000-0  82463-4 0  9078
2 25544  51
6393 200
7143 0007241 200
1483 159
9395 15
74114343  9214


Satellite: ISS
Catalog Number: 25544
Epoch time:      09188
86729968   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       200
7143  deg
Eccentricity:     
0007241     
Arg of perigee:   200
1483  deg
Mean anomaly:     159
9395  deg
Mean motion:   15
74114343  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             921
Checksum:              322


Coasting Arc #9 (Orbit 936)
---------------------------------------

Vector Time (GMT): 2009/189/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3091081
20                 A    =         6724272
98  meter
 Y    =        4250009
57  meter          E    =           
0005912
 Z    =       -4196372
00                 I    =           51
54816
 XDOT =      -6663
358765                 Wp   =          130
85789
 YDOT =       1253
662342  meter/sec      RA   =          194
61998  deg
 ZDOT =      -3645
732984                 TA   =          101
96628
                                          MA   =          101
90000
                                          Ha   =            190
588  n
mi
                                          Hp   =            184
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10141342
51                 X    =         3063712
01
 Y    =       13943600
95  feet           Y    =         4284423
52  meter
 Z    =      -13767624
69                 Z    =        -4181421
55
 XDOT =     -21861
413271                 XDOT =       -6659
172182
 YDOT =       4113
065427  feet/sec       YDOT =        1179
172784  meter/sec
 ZDOT =     -11961
066221                 ZDOT =       -3678
092669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17275724
52                 X    =        -5265640
83
 Y    =         662825
02  feet           Y    =          202029
07  meter
 Z    =      -13708695
43                 Z    =        -4178410
37
 XDOT =       8840
682340                 XDOT =        2694
639977
 YDOT =     -19099
026990  feet/sec       YDOT =       -5821
383427  meter/sec
 ZDOT =     -12088
009422                 ZDOT =       -3684
425272


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   09189
88305804  
00010596  00000-0  82463-4 0  9081
2 25544  51
6392 195
4965 0007284 205
0245 155
0566 15
74107918  9376


Satellite: ISS
Catalog Number: 25544
Epoch time:      09189
88305804   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:       195
4965  deg
Eccentricity:     
0007284     
Arg of perigee:   205
0245  deg
Mean anomaly:     155
0566  deg
Mean motion:   15
74107918  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             937
Checksum:              337


Coasting Arc #10 (Orbit 952)
---------------------------------------

Vector Time (GMT): 2009/190/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5729152
23                 A    =         6727402
37  meter
 Y    =       -1572371
10  meter          E    =           
0011911
 Z    =        3139914
11                 I    =           51
58879
 XDOT =       3905
977577                 Wp   =          126
92989
 YDOT =       4543
704251  meter/sec      RA   =          189
42856  deg
 ZDOT =      -4846
021562                 TA   =           16
46249
                                          MA   =           16
42384
                                          Ha   =            190
254  n
mi
                                          Hp   =            184
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18796431
18                 X    =         5731056
07
 Y    =       -5158697
82  feet           Y    =        -1508294
18  meter
 Z    =       10301555
48                 Z    =         3167750
26
 XDOT =      12814
887065                 XDOT =        3878
419496
 YDOT =      14907
166177  feet/sec       YDOT =        4587
229806  meter/sec
 ZDOT =     -15899
020874                 ZDOT =       -4827
112911

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5897748
82                 X    =        -1797633
84
 Y    =       18516835
16  feet           Y    =         5643931
36  meter
 Z    =       10410735
24                 Z    =         3173192
10
 XDOT =     -18184
248602                 XDOT =       -5542
558974
 YDOT =       3115
367429  feet/sec       YDOT =         949
563992  meter/sec
 ZDOT =     -15824
525400                 ZDOT =       -4823
315342


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   09190
89881676  
00010596  00000-0  82463-4 0  9091
2 25544  51
6395 190
2791 0007115 208
3540 151
7237 15
74136781  9532


Satellite: ISS
Catalog Number: 25544
Epoch time:      09190
89881676   =   yrday
fracday
Element set:     909
Inclination:       51
6395  deg
RA of node:       190
2791  deg
Eccentricity:     
0007115     
Arg of perigee:   208
3540  deg
Mean anomaly:     151
7237  deg
Mean motion:   15
74136781  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             953
Checksum:              333


Coasting Arc #11 (Orbit 968)
---------------------------------------

Vector Time (GMT): 2009/191/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3693939
23                 A    =         6724119
46  meter
 Y    =       -3665052
42  meter          E    =           
0010628
 Z    =        4259310
81                 I    =           51
60619
 XDOT =       6421
483292                 Wp   =          147
40194
 YDOT =      -2333
005888  meter/sec      RA   =          184
33805  deg
 ZDOT =       3548
709658                 TA   =          266
51381
                                          MA   =          266
63537
                                          Ha   =            190
310  n
mi
                                          Hp   =            184
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12119223
18                 X    =        -3673372
08
 Y    =      -12024450
21  feet           Y    =        -3706245
76  meter
 Z    =       13974116
84                 Z    =         4241415
43
 XDOT =      21067
858569                 XDOT =        6429
855387
 YDOT =      -7654
218794  feet/sec       YDOT =       -2261
150744  meter/sec
 ZDOT =      11642
748222                 ZDOT =        3579
924774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16667434
87                 X    =         5080234
15
 Y    =       -3952758
42  feet           Y    =        -1204800
77  meter
 Z    =       13903640
91                 Z    =         4237829
75
 XDOT =      -4954
056900                 XDOT =       -1509
996543
 YDOT =      20643
377763  feet/sec       YDOT =        6292
101542  meter/sec
 ZDOT =      11765
157339                 ZDOT =        3586
019957


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   09191
91457647  
00010596  00000-0  82463-4 0  9104
2 25544  51
6391 185
0607 0007084 212
5155 147
5572 15
74088011  9694


Satellite: ISS
Catalog Number: 25544
Epoch time:      09191
91457647   =   yrday
fracday
Element set:     910
Inclination:       51
6391  deg
RA of node:       185
0607  deg
Eccentricity:     
0007084     
Arg of perigee:   212
5155  deg
Mean anomaly:     147
5572  deg
Mean motion:   15
74088011  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             969
Checksum:              318


Coasting Arc #12 (Orbit 983)
---------------------------------------

Vector Time (GMT): 2009/192/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5453694
82                 A    =         6727715
05  meter
 Y    =        2496586
43  meter          E    =           
0004573
 Z    =       -3052850
20                 I    =           51
64823
 XDOT =      -4509
490459                 Wp   =          180
69417
 YDOT =      -3827
413093  meter/sec      RA   =          179
15074  deg
 ZDOT =       4921
296681                 TA   =          143
96650
                                          MA   =          143
93566
                                          Ha   =            190
072  n
mi
                                          Hp   =            184
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17892699
53                 X    =        -5466376
74
 Y    =        8190900
36  feet           Y    =         2435529
45  meter
 Z    =      -10015912
73                 Z    =        -3079374
44
 XDOT =     -14794
916203                 XDOT =       -4490
262971
 YDOT =     -12557
129570  feet/sec       YDOT =       -3877
733888  meter/sec
 ZDOT =      16145
986486                 ZDOT =        4899
436146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2194848
99                 X    =          668989
97
 Y    =      -19502006
27  feet           Y    =        -5944211
51  meter
 Z    =      -10119903
28                 Z    =        -3084546
52
 XDOT =      17019
158239                 XDOT =        5187
439431
 YDOT =      -6426
025850  feet/sec       YDOT =       -1958
652679  meter/sec
 ZDOT =      16059
923971                 ZDOT =        4895
064826


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   09192
86684883  
00010596  00000-0  82463-4 0  9114
2 25544  51
6387 180
1687 0007239 217
3069 142
7592 15
74114201  9849


Satellite: ISS
Catalog Number: 25544
Epoch time:      09192
86684883   =   yrday
fracday
Element set:     911
Inclination:       51
6387  deg
RA of node:       180
1687  deg
Eccentricity:     
0007239     
Arg of perigee:   217
3069  deg
Mean anomaly:     142
7592  deg
Mean motion:   15
74114201  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             984
Checksum:              333


Coasting Arc #13 (Orbit 999)
---------------------------------------

Vector Time (GMT): 2009/193/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4157849
03                 A    =         6723769
98  meter
 Y    =        3017618
82  meter          E    =           
0004195
 Z    =       -4339231
70                 I    =           51
66356
 XDOT =      -6016
354888                 Wp   =          124
35048
 YDOT =       3356
668932  meter/sec      RA   =          174
06446  deg
 ZDOT =      -3435
222921                 TA   =          110
99895
                                          MA   =          110
95407
                                          Ha   =            189
996  n
mi
                                          Hp   =            185
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13641236
98                 X    =         4144875
49
 Y    =        9900324
21  feet           Y    =         3064042
21  meter
 Z    =      -14236324
47                 Z    =        -4319064
27
 XDOT =     -19738
697138                 XDOT =       -6036
755050
 YDOT =      11012
693348  feet/sec       YDOT =        3289
276805  meter/sec
 ZDOT =     -11270
416407                 ZDOT =       -3464
499319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15448127
94                 X    =        -4708589
40
 Y    =        6907153
07  feet           Y    =         2105300
25  meter
 Z    =      -14156951
65                 Z    =        -4315038
86
 XDOT =        843
787553                 XDOT =         257
186446
 YDOT =     -21416
355703  feet/sec       YDOT =       -6527
705218  meter/sec
 ZDOT =     -11385
168437                 ZDOT =       -3470
199339


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   09193
88260753  
00010596  00000-0  82463-4 0  9124
2 25544  51
6378 174
9511 0007244 221
2482 138
8135 15
74107484 10009


Satellite: ISS
Catalog Number: 25544
Epoch time:      09193
88260753   =   yrday
fracday
Element set:     912
Inclination:       51
6378  deg
RA of node:       174
9511  deg
Eccentricity:     
0007244     
Arg of perigee:   221
2482  deg
Mean anomaly:     138
8135  deg
Mean motion:   15
74107484  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1000
Checksum:              303


Coasting Arc #14 (Orbit 1015)
---------------------------------------

Vector Time (GMT): 2009/194/20:39:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5012686
57                 A    =         6727850
49  meter
 Y    =       -3363205
04  meter          E    =           
0010322
 Z    =        2955694
29                 I    =           51
70836
 XDOT =       5000
130705                 Wp   =          129
65491
 YDOT =       3046
885274  meter/sec      RA   =          168
88282  deg
 ZDOT =      -5007
902151                 TA   =           16
26879
                                          MA   =           16
23568
                                          Ha   =            189
562  n
mi
                                          Hp   =            185
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16445822
09                 X    =         5035563
80
 Y    =      -11034137
26  feet           Y    =        -3307022
61  meter
 Z    =        9697159
74                 Z    =         2980101
04
 XDOT =      16404
628297                 XDOT =        4990
015646
 YDOT =       9996
342761  feet/sec       YDOT =        3102
743590  meter/sec
 ZDOT =     -16430
125166                 ZDOT =       -4983
635917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1664336
80                 X    =          507289
86
 Y    =       19687134
23  feet           Y    =         6000638
51  meter
 Z    =        9792797
60                 Z    =         2984844
71
 XDOT =     -15326
152891                 XDOT =       -4671
411401
 YDOT =       9429
042653  feet/sec       YDOT =        2873
972200  meter/sec
 ZDOT =     -16334
649465                 ZDOT =       -4978
801157


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   09194
89836502  
00010596  00000-0  82463-4 0  9138
2 25544  51
6386 169
7335 0007179 226
4205 133
6363 15
74157333 10162


Satellite: ISS
Catalog Number: 25544
Epoch time:      09194
89836502   =   yrday
fracday
Element set:     913
Inclination:       51
6386  deg
RA of node:       169
7335  deg
Eccentricity:     
0007179     
Arg of perigee:   226
4205  deg
Mean anomaly:     133
6363  deg
Mean motion:   15
74157333  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1016
Checksum:              320


Coasting Arc #15 (Orbit 1031)
---------------------------------------

Vector Time (GMT): 2009/195/20:43:09
674
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3079651
63                 A    =         6721069
19  meter
 Y    =       -3235166
91  meter          E    =           
0007948
 Z    =        5024984
53                 I    =           51
71213
 XDOT =       6634
516628                 Wp   =          185
42934
 YDOT =      -3444
198986  meter/sec      RA   =          163
77599  deg
 ZDOT =       1841
123788                 TA   =          246
78960
                                          MA   =          246
87333
                                          Ha   =            189
707  n
mi
                                          Hp   =            185
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10103843
92                 X    =        -3067656
98
 Y    =      -10614064
65  feet           Y    =        -3269538
83  meter
 Z    =       16486169
72                 Z    =         5010052
40
 XDOT =      21766
786837                 XDOT =        6663
593322
 YDOT =     -11299
865441  feet/sec       YDOT =       -3369
845551  meter/sec
 ZDOT =       6040
432376                 ZDOT =        1873
424497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14097060
82                 X    =         4296784
14
 Y    =       -4237381
96  feet           Y    =        -1291554
02  meter
 Z    =       16427333
70                 Z    =         5007051
31
 XDOT =       -162
089317                 XDOT =         -49
404824
 YDOT =      23465
135199  feet/sec       YDOT =        7152
173209  meter/sec
 ZDOT =       6167
075203                 ZDOT =        1879
724522


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   09195
91412645  
00010596  00000-0  82463-4 0  9141
2 25544  51
6372 164
5150 0007110 228
7140 131
3411 15
74071777 10327


Satellite: ISS
Catalog Number: 25544
Epoch time:      09195
91412645   =   yrday
fracday
Element set:     914
Inclination:       51
6372  deg
RA of node:       164
5150  deg
Eccentricity:     
0007110     
Arg of perigee:   228
7140  deg
Mean anomaly:     131
3411  deg
Mean motion:   15
74071777  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1032
Checksum:              278

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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