Date: September 9th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8557 31 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 1914)
---------------------------------------

Vector Time (GMT): 2009/251/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3910126
75                 A    =         6720279
30  meter
 Y    =       -1646203
92  meter          E    =           
0012099
 Z    =        5202819
97                 I    =           51
33954
 XDOT =       3791
949676                 Wp   =           66
10116
 YDOT =       6672
411274  meter/sec      RA   =          236
01151  deg
 ZDOT =       -732
431139                 TA   =           30
92264
                                          MA   =           30
85145
                                          Ha   =            193
197  n
mi
                                          Hp   =            180
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12828499
84                 X    =         3902969
65
 Y    =       -5400931
50  feet           Y    =        -1602518
36  meter
 Z    =       17069619
32                 Z    =         5221798
26
 XDOT =      12440
779777                 XDOT =        3720
613851
 YDOT =      21891
113103  feet/sec       YDOT =        6714
416191  meter/sec
 ZDOT =      -2402
989302                 ZDOT =        -714
183249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13446763
72                 X    =         4098573
58
 Y    =        3220825
73  feet           Y    =          981707
68  meter
 Z    =       17144188
52                 Z    =         5225548
66
 XDOT =      -2757
662861                 XDOT =        -840
535640
 YDOT =      24027
054105  feet/sec       YDOT =        7323
446091  meter/sec
 ZDOT =      -2330
777382                 ZDOT =        -710
420946


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   09251
98034546  
00020000  00000-0  20000-3 0  9005
2 25544  51
6371 236
6914 0009055  67
2252 292
9867 15
73993008 19153


Satellite: ISS
Catalog Number: 25544
Epoch time:      09251
98034546   =   yrday
fracday
Element set:     900
Inclination:       51
6371  deg
RA of node:       236
6914  deg
Eccentricity:     
0009055     
Arg of perigee:    67
2252  deg
Mean anomaly:     292
9867  deg
Mean motion:   15
73993008  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1915
Checksum:              310


Coasting Arc #2 (Orbit 1930)
---------------------------------------

Vector Time (GMT): 2009/252/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3807373
35                 A    =         6731939
52  meter
 Y    =       -5502554
91  meter          E    =           
0022062
 Z    =         650482
63                 I    =           51
39625
 XDOT =       4310
157338                 Wp   =           59
70160
 YDOT =      -2259
655261  meter/sec      RA   =          230
86811  deg
 ZDOT =       5973
790396                 TA   =          307
41054
                                          MA   =          307
61115
                                          Ha   =            193
278  n
mi
                                          Hp   =            180
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12491382
38                 X    =        -3748719
82
 Y    =      -18053001
66  feet           Y    =        -5544803
23  meter
 Z    =        2134129
37                 Z    =          632128
82
 XDOT =      14140
936149                 XDOT =        4306
084937
 YDOT =      -7413
567128  feet/sec       YDOT =       -2211
479168  meter/sec
 ZDOT =      19599
049857                 ZDOT =        5994
719533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         294539
89                 X    =           89775
76
 Y    =      -21958214
73  feet           Y    =        -6692863
85  meter
 Z    =        2061568
12                 Z    =          628365
96
 XDOT =      14123
743842                 XDOT =        4304
917123
 YDOT =       2081
683885  feet/sec       YDOT =         634
497248  meter/sec
 ZDOT =      19681
262228                 ZDOT =        5998
848727


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   09252
99616078  
00020000  00000-0  20000-3 0  9014
2 25544  51
6365 231
4734 0009059  71
2183 288
9962 15
74027763 19317


Satellite: ISS
Catalog Number: 25544
Epoch time:      09252
99616078   =   yrday
fracday
Element set:     901
Inclination:       51
6365  deg
RA of node:       231
4734  deg
Eccentricity:     
0009059     
Arg of perigee:    71
2183  deg
Mean anomaly:     288
9962  deg
Mean motion:   15
74027763  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1931
Checksum:              313


Coasting Arc #3 (Orbit 1945)
---------------------------------------

Vector Time (GMT): 2009/253/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3610745
30                 A    =         6720156
48  meter
 Y    =        2265938
37  meter          E    =           
0023536
 Z    =       -5215232
30                 I    =           51
37655
 XDOT =      -4858
014042                 Wp   =           88
53138
 YDOT =      -5898
466788  meter/sec      RA   =          225
70065  deg
 ZDOT =        804
355177                 TA   =          189
14747
                                          MA   =          189
19042
                                          Ha   =            193
306  n
mi
                                          Hp   =            180
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11846277
24                 X    =        -3610480
17
 Y    =        7434181
01  feet           Y    =         2225562
36  meter
 Z    =      -17110342
18                 Z    =        -5232772
82
 XDOT =     -15938
366280                 XDOT =       -4795
602757
 YDOT =     -19351
925158  feet/sec       YDOT =       -5952
442995  meter/sec
 ZDOT =       2638
960556                 ZDOT =         780
906353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13891166
86                 X    =        -4234027
66
 Y    =        -524206
86  feet           Y    =         -159778
25  meter
 Z    =      -17179226
75                 Z    =        -5236228
31
 XDOT =      -2229
401044                 XDOT =        -679
521438
 YDOT =     -23971
188225  feet/sec       YDOT =       -7306
418171  meter/sec
 ZDOT =       2546
317747                 ZDOT =         776
117649


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   09253
94847576  
00020000  00000-0  20000-3 0  9020
2 25544  51
6364 226
5818 0009154  75
7419 284
4761 15
74053921 19460


Satellite: ISS
Catalog Number: 25544
Epoch time:      09253
94847576   =   yrday
fracday
Element set:     902
Inclination:       51
6364  deg
RA of node:       226
5818  deg
Eccentricity:     
0009154     
Arg of perigee:    75
7419  deg
Mean anomaly:     284
4761  deg
Mean motion:   15
74053921  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1946
Checksum:              322


Coasting Arc #4 (Orbit 1961)
---------------------------------------

Vector Time (GMT): 2009/254/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4657764
56                 A    =         6731593
55  meter
 Y    =        4794858
36  meter          E    =           
0016877
 Z    =        -770008
12                 I    =           51
43759
 XDOT =      -3933
999673                 Wp   =          111
93776
 YDOT =       2882
765100  meter/sec      RA   =          220
56198  deg
 ZDOT =      -5955
988499                 TA   =           76
47750
                                          MA   =           76
28952
                                          Ha   =            193
236  n
mi
                                          Hp   =            180
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15281379
80                 X    =         4607542
03
 Y    =       15731162
61  feet           Y    =         4846663
43  meter
 Z    =       -2526273
35                 Z    =         -747502
52
 XDOT =     -12906
823075                 XDOT =       -3937
009602
 YDOT =       9457
890747  feet/sec       YDOT =        2838
756035  meter/sec
 ZDOT =     -19540
644683                 ZDOT =       -5975
107248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4070891
25                 X    =         1240807
65
 Y    =       21560589
72  feet           Y    =         6571667
75  meter
 Z    =       -2437399
88                 Z    =         -742919
48
 XDOT =     -14315
459645                 XDOT =       -4363
352100
 YDOT =        527
810901  feet/sec       YDOT =         160
876763  meter/sec
 ZDOT =     -19615
709032                 ZDOT =       -5978
868113


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   09254
96426411  
00020000  00000-0  20000-3 0  9035
2 25544  51
6364 221
3641 0009169  78
0982 282
1209 15
74119778 19627


Satellite: ISS
Catalog Number: 25544
Epoch time:      09254
96426411   =   yrday
fracday
Element set:     903
Inclination:       51
6364  deg
RA of node:       221
3641  deg
Eccentricity:     
0009169     
Arg of perigee:    78
0982  deg
Mean anomaly:     282
1209  deg
Mean motion:   15
74119778  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1962
Checksum:              304


Coasting Arc #5 (Orbit 1977)
---------------------------------------

Vector Time (GMT): 2009/255/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3235704
74                 A    =         6720194
02  meter
 Y    =       -2774867
82  meter          E    =           
0012399
 Z    =        5185272
95                 I    =           51
42146
 XDOT =       5785
029039                 Wp   =           77
49880
 YDOT =       5013
307515  meter/sec      RA   =          215
39527  deg
 ZDOT =       -922
625234                 TA   =           21
33159
                                          MA   =           21
27996
                                          Ha   =            193
276  n
mi
                                          Hp   =            180
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10615829
20                 X    =         3241304
19
 Y    =       -9103897
06  feet           Y    =        -2738653
03  meter
 Z    =       17012050
36                 Z    =         5201005
57
 XDOT =      18979
754065                 XDOT =        5733
021359
 YDOT =      16447
859301  feet/sec       YDOT =        5077
708332  meter/sec
 ZDOT =      -3026
985677                 ZDOT =        -894
647827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13761519
28                 X    =         4194511
08
 Y    =       -2023001
99  feet           Y    =         -616611
01  meter
 Z    =       17073800
95                 Z    =         5204094
53
 XDOT =       7029
317688                 XDOT =        2142
536031
 YDOT =      23077
867513  feet/sec       YDOT =        7034
134018  meter/sec
 ZDOT =      -2916
546954                 ZDOT =        -888
963511


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   09255
98004236  
00020000  00000-0  20000-3 0  9046
2 25544  51
6357 216
1462 0009255  83
9063 276
3155 15
74055798 19786


Satellite: ISS
Catalog Number: 25544
Epoch time:      09255
98004236   =   yrday
fracday
Element set:     904
Inclination:       51
6357  deg
RA of node:       216
1462  deg
Eccentricity:     
0009255     
Arg of perigee:    83
9063  deg
Mean anomaly:     276
3155  deg
Mean motion:   15
74055798  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1978
Checksum:              314


Coasting Arc #6 (Orbit 1993)
---------------------------------------

Vector Time (GMT): 2009/256/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5394734
19                 A    =         6731525
76  meter
 Y    =       -3923962
11  meter          E    =           
0021737
 Z    =         842641
92                 I    =           51
48616
 XDOT =       3463
501689                 Wp   =           67
86073
 YDOT =      -3459
859673  meter/sec      RA   =          210
26149  deg
 ZDOT =       5948
281053                 TA   =          301
35562
                                          MA   =          301
56814
                                          Ha   =            193
232  n
mi
                                          Hp   =            180
253

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17699259
14                 X    =        -5354548
20
 Y    =      -12873891
43  feet           Y    =        -3984064
51  meter
 Z    =        2764573
24                 Z    =          816532
04
 XDOT =      11363
194517                 XDOT =        3473
037482
 YDOT =     -11351
245646  feet/sec       YDOT =       -3421
075440  meter/sec
 ZDOT =      19515
357784                 ZDOT =        5965
129828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8366438
77                 X    =        -2550090
54
 Y    =      -20237654
02  feet           Y    =        -6168436
95  meter
 Z    =        2661537
51                 Z    =          811236
63
 XDOT =      14048
796732                 XDOT =        4282
073244
 YDOT =      -3181
584863  feet/sec       YDOT =        -969
747066  meter/sec
 ZDOT =      19581
463439                 ZDOT =        5968
430056


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   09256
99580249  
00020000  00000-0  20000-3 0  9052
2 25544  51
6365 210
9284 0009187  88
4338 271
7877 15
74132542 19949


Satellite: ISS
Catalog Number: 25544
Epoch time:      09256
99580249   =   yrday
fracday
Element set:     905
Inclination:       51
6365  deg
RA of node:       210
9284  deg
Eccentricity:     
0009187     
Arg of perigee:    88
4338  deg
Mean anomaly:     271
7877  deg
Mean motion:   15
74132542  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1994
Checksum:              333


Coasting Arc #7 (Orbit 2008)
---------------------------------------

Vector Time (GMT): 2009/257/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2822513
02                 A    =         6720043
54  meter
 Y    =        3239055
56  meter          E    =           
0023744
 Z    =       -5187972
19                 I    =           51
47472
 XDOT =      -6493
222194                 Wp   =           95
92476
 YDOT =      -3969
624038  meter/sec      RA   =          205
09718  deg
 ZDOT =       1055
972641                 TA   =          184
18314
                                          MA   =          184
20303
                                          Ha   =            193
242  n
mi
                                          Hp   =            180
075

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9260213
34                 X    =        -2833320
90
 Y    =       10626822
72  feet           Y    =         3207432
00  meter
 Z    =      -17020906
15                 Z    =        -5201710
19
 XDOT =     -21303
222420                 XDOT =       -6453
480265
 YDOT =     -13023
700911  feet/sec       YDOT =       -4042
012832  meter/sec
 ZDOT =       3464
477169                 ZDOT =        1024
525453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13290307
32                 X    =        -4050885
67
 Y    =        4495742
11  feet           Y    =         1370302
20  meter
 Z    =      -17074782
35                 Z    =        -5204393
66
 XDOT =     -11416
581230                 XDOT =       -3479
773959
 YDOT =     -21084
359493  feet/sec       YDOT =       -6426
512773  meter/sec
 ZDOT =       3340
408457                 ZDOT =        1018
156498


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   09257
94806675  
00020000  00000-0  20000-3 0  9063
2 25544  51
6371 206
0374 0009267  91
9900 268
2324 15
74144298 20092


Satellite: ISS
Catalog Number: 25544
Epoch time:      09257
94806675   =   yrday
fracday
Element set:     906
Inclination:       51
6371  deg
RA of node:       206
0374  deg
Eccentricity:     
0009267     
Arg of perigee:    91
9900  deg
Mean anomaly:     268
2324  deg
Mean motion:   15
74144298  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2009
Checksum:              307


Coasting Arc #8 (Orbit 2024)
---------------------------------------

Vector Time (GMT): 2009/258/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5928532
59                 A    =         6731222
00  meter
 Y    =        3013035
29  meter          E    =           
0017518
 Z    =       -1016391
59                 I    =           51
54019
 XDOT =      -2989
617892                 Wp   =          119
55201
 YDOT =       3914
782293  meter/sec      RA   =          199
96822  deg
 ZDOT =      -5917
710304                 TA   =           71
57240
                                          MA   =           71
38203
                                          Ha   =            193
172  n
mi
                                          Hp   =            180
156

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19450566
24                 X    =         5899337
09
 Y    =        9885286
37  feet           Y    =         3079168
33  meter
 Z    =       -3334618
07                 Z    =         -987662
11
 XDOT =      -9808
457651                 XDOT =       -3004
424547
 YDOT =      12843
773927  feet/sec       YDOT =        3881
267512  meter/sec
 ZDOT =     -19415
060053                 ZDOT =       -5932
269922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12058270
90                 X    =         3675360
97
 Y    =       18203967
76  feet           Y    =         5548569
37  meter
 Z    =       -3221296
61                 Z    =         -981851
21
 XDOT =     -13442
010552                 XDOT =       -4097
124816
 YDOT =       5509
131097  feet/sec       YDOT =        1679
183158  meter/sec
 ZDOT =     -19472
127390                 ZDOT =       -5935
104429


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   09258
96379983  
00020000  00000-0  20000-3 0  9074
2 25544  51
6369 200
8181 0009195  94
9427 265
2786 15
74187583 20255


Satellite: ISS
Catalog Number: 25544
Epoch time:      09258
96379983   =   yrday
fracday
Element set:     907
Inclination:       51
6369  deg
RA of node:       200
8181  deg
Eccentricity:     
0009195     
Arg of perigee:    94
9427  deg
Mean anomaly:     265
2786  deg
Mean motion:   15
74187583  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2025
Checksum:              341


Coasting Arc #9 (Orbit 2040)
---------------------------------------

Vector Time (GMT): 2009/259/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2373282
33                 A    =         6720126
35  meter
 Y    =       -3599959
28  meter          E    =           
0012507
 Z    =        5143816
79                 I    =           51
53209
 XDOT =       7046
766878                 Wp   =           86
83723
 YDOT =       2876
967267  meter/sec      RA   =          194
80438  deg
 ZDOT =      -1234
548134                 TA   =           14
98073
                                          MA   =           14
94372
                                          Ha   =            193
174  n
mi
                                          Hp   =            180
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7786359
34                 X    =         2388373
73
 Y    =      -11810890
03  feet           Y    =        -3573335
04  meter
 Z    =       16876039
33                 Z    =         5155383
07
 XDOT =      23119
313905                 XDOT =        7020
069576
 YDOT =       9438
868985  feet/sec       YDOT =        2955
618988  meter/sec
 ZDOT =      -4050
354771                 ZDOT =       -1200
380244

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12400614
50                 X    =         3779707
30
 Y    =       -6694639
61  feet           Y    =        -2040526
15  meter
 Z    =       16921340
94                 Z    =         5157624
72
 XDOT =      15320
420900                 XDOT =        4669
664290
 YDOT =      18454
357994  feet/sec       YDOT =        5624
888316  meter/sec
 ZDOT =      -3915
615307                 ZDOT =       -1193
479545


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   09259
97952116  
00020000  00000-0  20000-3 0  9082
2 25544  51
6378 195
6005 0009308  99
3984 260
8231 15
74152675 20412


Satellite: ISS
Catalog Number: 25544
Epoch time:      09259
97952116   =   yrday
fracday
Element set:     908
Inclination:       51
6378  deg
RA of node:       195
6005  deg
Eccentricity:     
0009308     
Arg of perigee:    99
3984  deg
Mean anomaly:     260
8231  deg
Mean motion:   15
74152675  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2041
Checksum:              316


Coasting Arc #10 (Orbit 2056)
---------------------------------------

Vector Time (GMT): 2009/260/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6318628
65                 A    =         6731011
57  meter
 Y    =       -1997126
12  meter          E    =           
0021254
 Z    =        1142858
99                 I    =           51
60007
 XDOT =       2446
000937                 Wp   =           75
82754
 YDOT =      -4318
790768  meter/sec      RA   =          189
68373  deg
 ZDOT =       5890
440452                 TA   =          296
69721
                                          MA   =          296
91464
                                          Ha   =            193
086  n
mi
                                          Hp   =            180
168

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20730408
96                 X    =        -6301378
62
 Y    =       -6552251
05  feet           Y    =        -2067688
18  meter
 Z    =        3749537
38                 Z    =         1112205
24
 XDOT =       8024
937456                 XDOT =        2465
497949
 YDOT =     -14169
261050  feet/sec       YDOT =       -4291
328548  meter/sec
 ZDOT =      19325
592033                 ZDOT =        5902
370892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15357420
77                 X    =        -4680941
85
 Y    =      -15418272
92  feet           Y    =        -4699489
58  meter
 Z    =        3628686
76                 Z    =         1106023
72
 XDOT =      12450
342997                 XDOT =        3794
864546
 YDOT =      -7773
346382  feet/sec       YDOT =       -2369
315977  meter/sec
 ZDOT =      19372
278401                 ZDOT =        5904
670457


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   09260
99522376  
00020000  00000-0  20000-3 0  9098
2 25544  51
6393 190
3831 0009229 103
8716 256
3475 15
74226643 20578


Satellite: ISS
Catalog Number: 25544
Epoch time:      09260
99522376   =   yrday
fracday
Element set:     909
Inclination:       51
6393  deg
RA of node:       190
3831  deg
Eccentricity:     
0009229     
Arg of perigee:   103
8716  deg
Mean anomaly:     256
3475  deg
Mean motion:   15
74226643  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2057
Checksum:              308


Coasting Arc #11 (Orbit 2071)
---------------------------------------

Vector Time (GMT): 2009/261/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1915525
19                 A    =         6720042
89  meter
 Y    =        3925862
45  meter          E    =           
0023208
 Z    =       -5127103
93                 I    =           51
59334
 XDOT =      -7351
186368                 Wp   =          103
52692
 YDOT =      -1718
893174  meter/sec      RA   =          184
52190  deg
 ZDOT =       1430
377935                 TA   =          180
21503
                                          MA   =          180
21603
                                          Ha   =            193
013  n
mi
                                          Hp   =            180
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6284531
46                 X    =        -1934375
83
 Y    =       12880126
15  feet           Y    =         3904335
99  meter
 Z    =      -16821207
10                 Z    =        -5136455
78
 XDOT =     -24118
065512                 XDOT =       -7338
367600
 YDOT =      -5639
413301  feet/sec       YDOT =       -1801
026647  meter/sec
 ZDOT =       4692
840994                 ZDOT =        1394
697023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11299335
02                 X    =        -3444037
31
 Y    =        8745668
24  feet           Y    =         2665679
68  meter
 Z    =      -16857767
02                 Z    =        -5138247
39
 XDOT =     -18425
253447                 XDOT =       -5616
017250
 YDOT =     -15031
208067  feet/sec       YDOT =       -4581
512219  meter/sec
 ZDOT =       4552
205277                 ZDOT =        1387
512169


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   09261
94743389  
00020000  00000-0  20000-3 0  9105
2 25544  51
6395 185
4924 0009200 106
9838 253
2334 15
74247746 20720


Satellite: ISS
Catalog Number: 25544
Epoch time:      09261
94743389   =   yrday
fracday
Element set:     910
Inclination:       51
6395  deg
RA of node:       185
4924  deg
Eccentricity:     
0009200     
Arg of perigee:   106
9838  deg
Mean anomaly:     253
2334  deg
Mean motion:   15
74247746  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2072
Checksum:              307


Coasting Arc #12 (Orbit 2087)
---------------------------------------

Vector Time (GMT): 2009/262/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6506528
53                 A    =         6730655
03  meter
 Y    =        1016044
54  meter          E    =           
0017304
 Z    =       -1369668
78                 I    =           51
65921
 XDOT =      -1939
427477                 Wp   =          126
85820
 YDOT =       4635
423676  meter/sec      RA   =          179
40741  deg
 ZDOT =      -5835
207188                 TA   =           68
18928
                                          MA   =           68
00528
                                          Ha   =            192
986  n
mi
                                          Hp   =            180
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21346878
37                 X    =         6501337
03
 Y    =        3333479
47  feet           Y    =         1088775
22  meter
 Z    =       -4493663
97                 Z    =        -1338072
45
 XDOT =      -6362
951041                 XDOT =       -1962
770764
 YDOT =      15208
082927  feet/sec       YDOT =        4613
604780  meter/sec
 ZDOT =     -19144
380539                 ZDOT =       -5844
686167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17830209
25                 X    =         5434647
78
 Y    =       12246976
29  feet           Y    =         3732878
37  meter
 Z    =       -4369156
34                 Z    =        -1331718
85
 XDOT =     -11319
216576                 XDOT =       -3450
097212
 YDOT =       9709
546539  feet/sec       YDOT =        2959
469785  meter/sec
 ZDOT =     -19181
395821                 ZDOT =       -5846
489446


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   09262
96310935  
00020000  00000-0  20000-3 0  9116
2 25544  51
6397 180
2735 0009140 110
7724 249
4419 15
74263060 20880


Satellite: ISS
Catalog Number: 25544
Epoch time:      09262
96310935   =   yrday
fracday
Element set:     911
Inclination:       51
6397  deg
RA of node:       180
2735  deg
Eccentricity:     
0009140     
Arg of perigee:   110
7724  deg
Mean anomaly:     249
4419  deg
Mean motion:   15
74263060  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2088
Checksum:              288


Coasting Arc #13 (Orbit 2103)
---------------------------------------

Vector Time (GMT): 2009/263/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1445015
69                 A    =         6720174
20  meter
 Y    =       -4167721
14  meter          E    =           
0012430
 Z    =        5058956
07                 I    =           51
65463
 XDOT =       7506
087358                 Wp   =           94
00601
 YDOT =        571
636019  meter/sec      RA   =          174
24545  deg
 ZDOT =      -1670
421352                 TA   =           12
04319
                                          MA   =           12
01350
                                          Ha   =            192
874  n
mi
                                          Hp   =            180
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4740865
12                 X    =         1466936
62
 Y    =      -13673625
79  feet           Y    =        -4151439
16  meter
 Z    =       16597624
89                 Z    =         5066029
63
 XDOT =      24626
270861                 XDOT =        7507
252073
 YDOT =       1875
446258  feet/sec       YDOT =         655
579887  meter/sec
 ZDOT =      -5480
385012                 ZDOT =       -1633
953482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9920585
19                 X    =         3023794
37
 Y    =      -10493311
52  feet           Y    =        -3198361
35  meter
 Z    =       16625203
74                 Z    =         5067362
10
 XDOT =      20866
907408                 XDOT =        6360
233378
 YDOT =      11258
951199  feet/sec       YDOT =        3431
728325  meter/sec
 ZDOT =      -5336
713357                 ZDOT =       -1626
630231


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   09263
97877011  
00020000  00000-0  20000-3 0  9122
2 25544  51
6402 175
0562 0009119 114
0033 246
2085 15
74277399 21046


Satellite: ISS
Catalog Number: 25544
Epoch time:      09263
97877011   =   yrday
fracday
Element set:     912
Inclination:       51
6402  deg
RA of node:       175
0562  deg
Eccentricity:     
0009119     
Arg of perigee:   114
0033  deg
Mean anomaly:     246
2085  deg
Mean motion:   15
74277399  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2104
Checksum:              280


Coasting Arc #14 (Orbit 2119)
---------------------------------------

Vector Time (GMT): 2009/264/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6543461
26                 A    =         6730320
11  meter
 Y    =           8841
92  meter          E    =           
0020633
 Z    =        1551175
34                 I    =           51
71861
 XDOT =       1377
523986                 Wp   =           83
83285
 YDOT =      -4905
704475  meter/sec      RA   =          169
13949  deg
 ZDOT =       5775
648234                 TA   =          293
25565
                                          MA   =          293
47275
                                          Ha   =            192
842  n
mi
                                          Hp   =            180
290

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21468048
75                 X    =        -6550609
25
 Y    =          29008
91  feet           Y    =          -64370
79  meter
 Z    =        5089157
95                 Z    =         1519369
35
 XDOT =       4519
435649                 XDOT =        1404
220540
 YDOT =     -16094
830955  feet/sec       YDOT =       -4890
150580  meter/sec
 ZDOT =      18948
977145                 ZDOT =        5782
405488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19703848
15                 X    =        -6005732
92
 Y    =       -8596265
39  feet           Y    =        -2620141
69  meter
 Z    =        4963877
17                 Z    =         1512989
76
 XDOT =       9867
538497                 XDOT =        3007
625734
 YDOT =     -11537
750171  feet/sec       YDOT =       -3516
706252  meter/sec
 ZDOT =      18975
267470                 ZDOT =        5783
661525


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   09264
99441452  
00020000  00000-0  20000-3 0  9132
2 25544  51
6403 169
8383 0009119 117
9523 242
2564 15
74306674 21200


Satellite: ISS
Catalog Number: 25544
Epoch time:      09264
99441452   =   yrday
fracday
Element set:     913
Inclination:       51
6403  deg
RA of node:       169
8383  deg
Eccentricity:     
0009119     
Arg of perigee:   117
9523  deg
Mean anomaly:     242
2564  deg
Mean motion:   15
74306674  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2120
Checksum:              294


Coasting Arc #15 (Orbit 2134)
---------------------------------------

Vector Time (GMT): 2009/265/22:24:46
878
Vector Time (MET): N/A
Weight (LBS)     : 710966
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -976965
52                 A    =         6720290
27  meter
 Y    =        4394549
96  meter          E    =           
0022016
 Z    =       -5009450
21                 I    =           51
71431
 XDOT =      -7418
918393                 Wp   =          111
55361
 YDOT =        548
203683  meter/sec      RA   =          163
97789  deg
 ZDOT =       1926
622267                 TA   =          177
07992
                                          MA   =          177
06705
                                          Ha   =            192
697  n
mi
                                          Hp   =            180
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3205267
46                 X    =        -1001698
15
 Y    =       14417814
82  feet           Y    =         4383486
47  meter
 Z    =      -16435204
09                 Z    =        -5014256
63
 XDOT =     -24340
283440                 XDOT =       -7433
856431
 YDOT =       1798
568515  feet/sec       YDOT =         465
157525  meter/sec
 ZDOT =       6320
939197                 ZDOT =        1890
544310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8424358
32                 X    =        -2567744
42
 Y    =       12106363
35  feet           Y    =         3690019
55  meter
 Z    =      -16453850
93                 Z    =        -5015133
76
 XDOT =     -22304
866997                 XDOT =       -6798
523461
 YDOT =      -7118
209975  feet/sec       YDOT =       -2169
630400  meter/sec
 ZDOT =       6178
853526                 ZDOT =        1883
314555


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   09265
94656764  
00020000  00000-0  20000-3 0  9143
2 25544  51
6401 164
9471 0009072 121
4659 238
7392 15
74349573 21350


Satellite: ISS
Catalog Number: 25544
Epoch time:      09265
94656764   =   yrday
fracday
Element set:     914
Inclination:       51
6401  deg
RA of node:       164
9471  deg
Eccentricity:     
0009072     
Arg of perigee:   121
4659  deg
Mean anomaly:     238
7392  deg
Mean motion:   15
74349573  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2135
Checksum:              315

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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