Date: September 8th 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) : 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 1844)
---------------------------------------

Vector Time (GMT): 2009/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2838320
14                 A    =         6730379
57  meter
 Y    =        5724684
52  meter          E    =           
0020609
 Z    =        2098063
29                 I    =           51
32453
 XDOT =      -3728
202025                 Wp   =           87
72560
 YDOT =       3884
112469  meter/sec      RA   =          258
86557  deg
 ZDOT =      -5507
028837                 TA   =           68
72140
                                          MA   =           68
50146
                                          Ha   =            193
307  n
mi
                                          Hp   =            180
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9312073
96                 X    =         2763902
85
 Y    =       18781773
36  feet           Y    =         5756008
34  meter
 Z    =        6883409
74                 Z    =         2111670
60
 XDOT =     -12231
633941                 XDOT =       -3744
605809
 YDOT =      12743
151144  feet/sec       YDOT =        3842
329436  meter/sec
 ZDOT =     -18067
679910                 ZDOT =       -5525
180401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3365897
53                 X    =        -1025925
57
 Y    =      -20673556
71  feet           Y    =        -6301300
09  meter
 Z    =        6937279
62                 Z    =         2114482
83
 XDOT =      13818
338176                 XDOT =        4211
829476
 YDOT =      -8388
267303  feet/sec       YDOT =       -2556
743874  meter/sec
 ZDOT =     -18138
861834                 ZDOT =       -5528
725087


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   09247
53598532  
00020000  00000-0  20000-3 0  9001
2 25544  51
6387 259
5149 0009289  52
5929 307
6078 15
73951261 18456


Satellite: ISS
Catalog Number: 25544
Epoch time:      09247
53598532   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:       259
5149  deg
Eccentricity:     
0009289     
Arg of perigee:    52
5929  deg
Mean anomaly:     307
6078  deg
Mean motion:   15
73951261  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1845
Checksum:              329


Coasting Arc #2 (Orbit 1860)
---------------------------------------

Vector Time (GMT): 2009/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2933406
75                 A    =         6722201
37  meter
 Y    =       -3667644
36  meter          E    =           
0013797
 Z    =        4797133
81                 I    =           51
30337
 XDOT =       3835
892169                 Wp   =           83
55522
 YDOT =       6236
345571  meter/sec      RA   =          253
74499  deg
 ZDOT =       2417
962966                 TA   =          342
73062
                                          MA   =          342
77751
                                          Ha   =            193
256  n
mi
                                          Hp   =            180
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9624037
88                 X    =         2950897
42
 Y    =      -12032953
94  feet           Y    =        -3634743
11  meter
 Z    =       15738628
00                 Z    =         4811427
03
 XDOT =      12584
948061                 XDOT =        3754
125195
 YDOT =      20460
451348  feet/sec       YDOT =        6278
783779  meter/sec
 ZDOT =       7932
949363                 ZDOT =        2436
398572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12485885
02                 X    =        -3805697
75
 Y    =        8930315
82  feet           Y    =         2721960
26  meter
 Z    =       15794639
33                 Z    =         4814206
07
 XDOT =      -5745
462961                 XDOT =       -1751
217110
 YDOT =     -22218
102598  feet/sec       YDOT =       -6772
077672  meter/sec
 ZDOT =       8005
853615                 ZDOT =        2440
184182


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   09248
55185257  
00020000  00000-0  20000-3 0  9011
2 25544  51
6381 254
2976 0009253  56
1817 304
0226 15
73951561 18614


Satellite: ISS
Catalog Number: 25544
Epoch time:      09248
55185257   =   yrday
fracday
Element set:     901
Inclination:       51
6381  deg
RA of node:       254
2976  deg
Eccentricity:     
0009253     
Arg of perigee:    56
1817  deg
Mean anomaly:     304
0226  deg
Mean motion:   15
73951561  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1861
Checksum:              297


Coasting Arc #3 (Orbit 1875)
---------------------------------------

Vector Time (GMT): 2009/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3826121
66                 A    =         6730187
25  meter
 Y    =       -5114325
35  meter          E    =           
0015427
 Z    =       -2113518
69                 I    =           51
34095
 XDOT =       2971
797941                 Wp   =           52
73342
 YDOT =      -4484
012016  meter/sec      RA   =          248
54916  deg
 ZDOT =       5507
351414                 TA   =          283
54430
                                          MA   =          283
71612
                                          Ha   =            193
287  n
mi
                                          Hp   =            180
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12552892
59                 X    =        -3758380
92
 Y    =      -16779282
65  feet           Y    =        -5156732
71  meter
 Z    =       -6934116
44                 Z    =        -2131941
07
 XDOT =       9749
993245                 XDOT =        2994
964296
 YDOT =     -14711
325511  feet/sec       YDOT =       -4450
649651  meter/sec
 ZDOT =      18068
738235                 ZDOT =        5521
845064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7724410
58                 X    =         2354400
35
 Y    =       19453486
65  feet           Y    =         5929422
73  meter
 Z    =       -7006907
17                 Z    =        -2135705
31
 XDOT =     -11716
057459                 XDOT =       -3571
054313
 YDOT =      11137
713865  feet/sec       YDOT =        3394
775186  meter/sec
 ZDOT =      18125
485398                 ZDOT =        5524
647949


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   09249
50421447  
00020000  00000-0  20000-3 0  9022
2 25544  51
6386 249
4076 0009289  60
1134 300
0950 15
73999379 18767


Satellite: ISS
Catalog Number: 25544
Epoch time:      09249
50421447   =   yrday
fracday
Element set:     902
Inclination:       51
6386  deg
RA of node:       249
4076  deg
Eccentricity:     
0009289     
Arg of perigee:    60
1134  deg
Mean anomaly:     300
0950  deg
Mean motion:   15
73999379  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1876
Checksum:              311


Coasting Arc #4 (Orbit 1891)
---------------------------------------

Vector Time (GMT): 2009/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2267284
51                 A    =         6722044
91  meter
 Y    =        4111078
13  meter          E    =           
0021193
 Z    =       -4830730
26                 I    =           51
32460
 XDOT =      -4855
092934                 Wp   =           68
68873
 YDOT =      -5463
527485  meter/sec      RA   =          243
42871  deg
 ZDOT =      -2371
669132                 TA   =          178
02819
                                          MA   =          178
01983
                                          Ha   =            193
353  n
mi
                                          Hp   =            180
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7438597
48                 X    =        -2289619
82
 Y    =       13487789
14  feet           Y    =         4085598
79  meter
 Z    =      -15848852
55                 Z    =        -4841799
34
 XDOT =     -15928
782593                 XDOT =       -4782
116771
 YDOT =     -17924
958941  feet/sec       YDOT =       -5517
412132  meter/sec
 ZDOT =      -7781
066707                 ZDOT =       -2395
077663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10404511
65                 X    =         3171295
15
 Y    =      -11297127
13  feet           Y    =        -3443364
35  meter
 Z    =      -15892148
10                 Z    =        -4843926
74
 XDOT =      10225
355140                 XDOT =        3116
688247
 YDOT =      20489
807020  feet/sec       YDOT =        6245
293180  meter/sec
 ZDOT =      -7873
500909                 ZDOT =       -2399
843077


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   09250
52005368  
00020000  00000-0  20000-3 0  9037
2 25544  51
6378 244
1894 0009238  63
1825 297
0282 15
73991169 18922


Satellite: ISS
Catalog Number: 25544
Epoch time:      09250
52005368   =   yrday
fracday
Element set:     903
Inclination:       51
6378  deg
RA of node:       244
1894  deg
Eccentricity:     
0009238     
Arg of perigee:    63
1825  deg
Mean anomaly:     297
0282  deg
Mean motion:   15
73991169  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1892
Checksum:              311


Coasting Arc #5 (Orbit 1907)
---------------------------------------

Vector Time (GMT): 2009/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4646033
30                 A    =         6730199
20  meter
 Y    =        4413892
20  meter          E    =           
0021639
 Z    =        2034941
50                 I    =           51
36722
 XDOT =      -2188
020258                 Wp   =           93
29946
 YDOT =       4881
340245  meter/sec      RA   =          238
23397  deg
 ZDOT =      -5542
929154                 TA   =           63
90564
                                          MA   =           63
68310
                                          Ha   =            193
265  n
mi
                                          Hp   =            180
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15242891
41                 X    =         4586445
62
 Y    =       14481273
61  feet           Y    =         4465513
82  meter
 Z    =        6676317
27                 Z    =         2057367
16
 XDOT =      -7178
544153                 XDOT =       -2215
514816
 YDOT =      16014
895818  feet/sec       YDOT =        4856
718472  meter/sec
 ZDOT =     -18185
463104                 ZDOT =       -5553
625719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11530791
54                 X    =        -3514585
26
 Y    =      -17547200
15  feet           Y    =        -5348386
61  meter
 Z    =        6764824
41                 Z    =         2061918
48
 XDOT =       9234
586906                 XDOT =        2814
702089
 YDOT =     -13157
005582  feet/sec       YDOT =       -4010
255301  meter/sec
 ZDOT =     -18227
245618                 ZDOT =       -5555
664464


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
53587713  
00020000  00000-0  20000-3 0  9049
2 25544  51
6378 238
9718 0009256  65
7177 294
4952 15
74048253 19087


Satellite: ISS
Catalog Number: 25544
Epoch time:      09251
53587713   =   yrday
fracday
Element set:     904
Inclination:       51
6378  deg
RA of node:       238
9718  deg
Eccentricity:     
0009256     
Arg of perigee:    65
7177  deg
Mean anomaly:     294
4952  deg
Mean motion:   15
74048253  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1908
Checksum:              328


Coasting Arc #6 (Orbit 1923)
---------------------------------------

Vector Time (GMT): 2009/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1541581
88                 A    =         6721769
98  meter
 Y    =       -4390886
59  meter          E    =           
0014350
 Z    =        4838157
28                 I    =           51
35531
 XDOT =       5753
647698                 Wp   =           91
71493
 YDOT =       4580
445140  meter/sec      RA   =          233
11605  deg
 ZDOT =       2317
385277                 TA   =          335
61994
                                          MA   =          335
68775
                                          Ha   =            193
214  n
mi
                                          Hp   =            180
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5057683
34                 X    =         1567063
80
 Y    =      -14405795
91  feet           Y    =        -4373505
07  meter
 Z    =       15873219
42                 Z    =         4845708
42
 XDOT =      18876
796909                 XDOT =        5690
743180
 YDOT =      15027
707151  feet/sec       YDOT =        4644
434175  meter/sec
 ZDOT =       7602
970070                 ZDOT =        2345
183849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7874025
40                 X    =        -2400002
94
 Y    =       13044975
95  feet           Y    =         3976108
67  meter
 Z    =       15902658
21                 Z    =         4847130
22
 XDOT =     -14312
989740                 XDOT =       -4362
599273
 YDOT =     -18066
866255  feet/sec       YDOT =       -5506
780835  meter/sec
 ZDOT =       7712
633990                 ZDOT =        2350
810840


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
55168628  
00020000  00000-0  20000-3 0  9053
2 25544  51
6375 233
7551 0009129  69
6926 290
5217 15
74053970 19247


Satellite: ISS
Catalog Number: 25544
Epoch time:      09252
55168628   =   yrday
fracday
Element set:     905
Inclination:       51
6375  deg
RA of node:       233
7551  deg
Eccentricity:     
0009129     
Arg of perigee:    69
6926  deg
Mean anomaly:     290
5217  deg
Mean motion:   15
74053970  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1924
Checksum:              312


Coasting Arc #7 (Orbit 1938)
---------------------------------------

Vector Time (GMT): 2009/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5354682
24                 A    =         6730185
56  meter
 Y    =       -3551342
51  meter          E    =           
0015314
 Z    =       -1998005
23                 I    =           51
40284
 XDOT =       1346
657865                 Wp   =           60
00324
 YDOT =      -5141
100356  meter/sec      RA   =          227
92480  deg
 ZDOT =       5568
292676                 TA   =          277
66751
                                          MA   =          277
84141
                                          Ha   =            193
288  n
mi
                                          Hp   =            180
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17567855
13                 X    =        -5304866
50
 Y    =      -11651386
20  feet           Y    =        -3610943
21  meter
 Z    =       -6555135
26                 Z    =        -2023897
49
 XDOT =       4418
168848                 XDOT =        1376
996414
 YDOT =     -16867
127151  feet/sec       YDOT =       -5125
871536  meter/sec
 ZDOT =      18268
676757                 ZDOT =        5574
908562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14954997
11                 X    =         4558283
12
 Y    =       14811593
75  feet           Y    =         4514573
78  meter
 Z    =       -6657242
99                 Z    =        -2029127
66
 XDOT =      -6401
554671                 XDOT =       -1951
193864
 YDOT =      14629
043680  feet/sec       YDOT =        4458
932514  meter/sec
 ZDOT =      18294
390868                 ZDOT =        5576
130336


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
50399306  
00020000  00000-0  20000-3 0  9069
2 25544  51
6374 228
8643 0009305  73
6396 286
5790 15
74067631 19391


Satellite: ISS
Catalog Number: 25544
Epoch time:      09253
50399306   =   yrday
fracday
Element set:     906
Inclination:       51
6374  deg
RA of node:       228
8643  deg
Eccentricity:     
0009305     
Arg of perigee:    73
6396  deg
Mean anomaly:     286
5790  deg
Mean motion:   15
74067631  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1939
Checksum:              322


Coasting Arc #8 (Orbit 1954)
---------------------------------------

Vector Time (GMT): 2009/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -842413
65                 A    =         6721537
66  meter
 Y    =        4548496
78  meter          E    =           
0021601
 Z    =       -4896383
00                 I    =           51
39496
 XDOT =      -6440
240061                 Wp   =           75
34559
 YDOT =      -3564
465331  meter/sec      RA   =          222
80699  deg
 ZDOT =      -2205
922444                 TA   =          173
11716
                                          MA   =          173
08744
                                          Ha   =            193
285  n
mi
                                          Hp   =            180
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2763824
30                 X    =         -869427
20
 Y    =       14922889
69  feet           Y    =         4538925
40  meter
 Z    =      -16064248
68                 Z    =        -4900541
06
 XDOT =     -21129
396524                 XDOT =       -6389
186892
 YDOT =     -11694
440063  feet/sec       YDOT =       -3636
198416  meter/sec
 ZDOT =      -7237
278361                 ZDOT =       -2237
085359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5252379
68                 X    =         1600925
33
 Y    =      -14220653
04  feet           Y    =        -4334455
05  meter
 Z    =      -16080329
03                 Z    =        -4901284
29
 XDOT =      17665
082693                 XDOT =        5384
317205
 YDOT =      14837
058422  feet/sec       YDOT =        4522
335407  meter/sec
 ZDOT =      -7360
140350                 ZDOT =       -2243
370779


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
51977125  
00020000  00000-0  20000-3 0  9073
2 25544  51
6378 223
6461 0009200  77
0891 283
1299 15
74083944 19558


Satellite: ISS
Catalog Number: 25544
Epoch time:      09254
51977125   =   yrday
fracday
Element set:     907
Inclination:       51
6378  deg
RA of node:       223
6461  deg
Eccentricity:     
0009200     
Arg of perigee:    77
0891  deg
Mean anomaly:     283
1299  deg
Mean motion:   15
74083944  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1955
Checksum:              313


Coasting Arc #9 (Orbit 1970)
---------------------------------------

Vector Time (GMT): 2009/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5885231
95                 A    =         6730266
54  meter
 Y    =        2662994
76  meter          E    =           
0022361
 Z    =        1861122
41                 I    =           51
44767
 XDOT =       -567
980735                 Wp   =          100
46888
 YDOT =       5227
890002  meter/sec      RA   =          217
62003  deg
 ZDOT =      -5631
115540                 TA   =           58
79816
                                          MA   =           58
57918
                                          Ha   =            193
183  n
mi
                                          Hp   =            180
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19308503
76                 X    =         5845975
46
 Y    =        8736859
45  feet           Y    =         2728587
36  meter
 Z    =        6106044
66                 Z    =         1889617
61
 XDOT =      -1863
453854                 XDOT =        -599
042683
 YDOT =      17151
870084  feet/sec       YDOT =        5221
364904  meter/sec
 ZDOT =     -18474
788516                 ZDOT =       -5633
950178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17639756
01                 X    =        -5376597
63
 Y    =      -11687845
79  feet           Y    =        -3562455
40  meter
 Z    =        6218366
39                 Z    =         1895358
07
 XDOT =       3606
009107                 XDOT =        1099
111576
 YDOT =     -15368
490782  feet/sec       YDOT =       -4684
315990  meter/sec
 ZDOT =     -18485
617217                 ZDOT =       -5634
416128


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
53553250  
00020000  00000-0  20000-3 0  9086
2 25544  51
6377 218
4288 0009151  80
1529 280
0667 15
74125434 19718


Satellite: ISS
Catalog Number: 25544
Epoch time:      09255
53553250   =   yrday
fracday
Element set:     908
Inclination:       51
6377  deg
RA of node:       218
4288  deg
Eccentricity:     
0009151     
Arg of perigee:    80
1529  deg
Mean anomaly:     280
0667  deg
Mean motion:   15
74125434  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1971
Checksum:              296


Coasting Arc #10 (Orbit 1986)
---------------------------------------

Vector Time (GMT): 2009/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         147794
16                 A    =         6721076
81  meter
 Y    =       -4559885
48  meter          E    =           
0014353
 Z    =        4924124
57                 I    =           51
44197
 XDOT =       6994
566707                 Wp   =          100
43762
 YDOT =       2486
394144  meter/sec      RA   =          212
50502  deg
 ZDOT =       2084
842557                 TA   =          329
29134
                                          MA   =          329
37525
                                          Ha   =            193
069  n
mi
                                          Hp   =            180
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         484888
96                 X    =          174852
16
 Y    =      -14960254
21  feet           Y    =        -4558081
51  meter
 Z    =       16155264
35                 Z    =         4924908
25
 XDOT =      22948
053501                 XDOT =        6956
115805
 YDOT =       8157
461104  feet/sec       YDOT =        2564
396498  meter/sec
 ZDOT =       6840
034637                 ZDOT =        2118
728689

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2509028
82                 X    =         -764751
99
 Y    =       14753263
35  feet           Y    =         4496794
67  meter
 Z    =       16158059
43                 Z    =         4924976
51
 XDOT =     -20443
001573                 XDOT =       -6231
026880
 YDOT =     -11141
907901  feet/sec       YDOT =       -3396
053528  meter/sec
 ZDOT =       6973
582166                 ZDOT =        2125
547844


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
55127595  
00020000  00000-0  20000-3 0  9099
2 25544  51
6381 213
2121 0008970  84
3424 275
8762 15
74180560 19876


Satellite: ISS
Catalog Number: 25544
Epoch time:      09256
55127595   =   yrday
fracday
Element set:     909
Inclination:       51
6381  deg
RA of node:       213
2121  deg
Eccentricity:     
0008970     
Arg of perigee:    84
3424  deg
Mean anomaly:     275
8762  deg
Mean motion:   15
74180560  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1987
Checksum:              307


Coasting Arc #11 (Orbit 2001)
---------------------------------------

Vector Time (GMT): 2009/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6277472
55                 A    =         6730285
04  meter
 Y    =       -1664454
06  meter          E    =           
0015011
 Z    =       -1763185
31                 I    =           51
49871
 XDOT =       -206
271313                 Wp   =           65
95098
 YDOT =      -5191
133334  meter/sec      RA   =          207
32230  deg
 ZDOT =       5678
793586                 TA   =          274
48890
                                          MA   =          274
66037
                                          Ha   =            193
111  n
mi
                                          Hp   =            180
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20595382
37                 X    =        -6249828
60
 Y    =       -5460807
28  feet           Y    =        -1734497
91  meter
 Z    =       -5784728
70                 Z    =        -1793613
89
 XDOT =       -676
743153                 XDOT =        -175
794200
 YDOT =     -17031
277343  feet/sec       YDOT =       -5193
269499  meter/sec
 ZDOT =      18631
212554                 ZDOT =        5677
865625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19718902
67                 X    =         6010321
53
 Y    =        7984578
82  feet           Y    =         2433699
62  meter
 Z    =       -5904630
04                 Z    =        -1799731
24
 XDOT =       -764
270751                 XDOT =        -232
949725
 YDOT =      15557
895304  feet/sec       YDOT =        4742
046489  meter/sec
 ZDOT =      18627
223515                 ZDOT =        5677
577727


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
50352199  
00020000  00000-0  20000-3 0  9107
2 25544  51
6378 208
3203 0009103  87
5415 272
6790 15
74166727 20026


Satellite: ISS
Catalog Number: 25544
Epoch time:      09257
50352199   =   yrday
fracday
Element set:     910
Inclination:       51
6378  deg
RA of node:       208
3203  deg
Eccentricity:     
0009103     
Arg of perigee:    87
5415  deg
Mean anomaly:     272
6790  deg
Mean motion:   15
74166727  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2002
Checksum:              285


Coasting Arc #12 (Orbit 2017)
---------------------------------------

Vector Time (GMT): 2009/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         463966
79                 A    =         6720788
63  meter
 Y    =        4487178
55  meter          E    =           
0021903
 Z    =       -5001357
65                 I    =           51
49492
 XDOT =      -7321
510974                 Wp   =           82
31994
 YDOT =      -1356
092205  meter/sec      RA   =          202
20695  deg
 ZDOT =      -1900
102121                 TA   =          169
28437
                                          MA   =          169
23763
                                          Ha   =            193
072  n
mi
                                          Hp   =            180
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1522200
75                 X    =          438051
38
 Y    =       14721714
40  feet           Y    =         4492221
79  meter
 Z    =      -16408653
71                 Z    =        -4999166
86
 XDOT =     -24020
705296                 XDOT =       -7296
572493
 YDOT =      -4449
121408  feet/sec       YDOT =       -1437
826290  meter/sec
 ZDOT =      -6233
930844                 ZDOT =       -1935
609077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -22485
53                 X    =           -6853
59
 Y    =      -14810070
02  feet           Y    =        -4514109
34  meter
 Z    =      -16399731
92                 Z    =        -4998638
29
 XDOT =      22285
076312                 XDOT =        6792
491260
 YDOT =       7008
778075  feet/sec       YDOT =        2136
275557  meter/sec
 ZDOT =      -6373
821744                 ZDOT =       -1942
740867


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
51923314  
00020000  00000-0  20000-3 0  9113
2 25544  51
6388 203
1018 0009030  91
3316 268
8882 15
74199766 20181


Satellite: ISS
Catalog Number: 25544
Epoch time:      09258
51923314   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:       203
1018  deg
Eccentricity:     
0009030     
Arg of perigee:    91
3316  deg
Mean anomaly:     268
8882  deg
Mean motion:   15
74199766  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2018
Checksum:              296


Coasting Arc #13 (Orbit 2033)
---------------------------------------

Vector Time (GMT): 2009/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6500569
90                 A    =         6730442
83  meter
 Y    =         695382
80  meter          E    =           
0022745
 Z    =        1560919
50                 I    =           51
55681
 XDOT =        858
179626                 Wp   =          108
77997
 YDOT =       5045
686781  meter/sec      RA   =          197
03125  deg
 ZDOT =      -5760
831643                 TA   =           53
97217
                                          MA   =           53
76160
                                          Ha   =            193
014  n
mi
                                          Hp   =            180
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21327329
06                 X    =         6484728
26
 Y    =        2281439
62  feet           Y    =          767987
53  meter
 Z    =        5121126
98                 Z    =         1592460
50
 XDOT =       2815
549954                 XDOT =         829
678970
 YDOT =      16554
090488  feet/sec       YDOT =        5055
123684  meter/sec
 ZDOT =     -18900
366284                 ZDOT =       -5756
732226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21002752
84                 X    =        -6401639
07
 Y    =       -4201943
98  feet           Y    =        -1280752
52  meter
 Z    =        5245370
62                 Z    =         1598788
97
 XDOT =      -1720
090720                 XDOT =        -524
283651
 YDOT =     -15219
260169  feet/sec       YDOT =       -4638
830499  meter/sec
 ZDOT =     -18883
885099                 ZDOT =       -5755
808178


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
53492705  
00020000  00000-0  20000-3 0  9122
2 25544  51
6396 197
8840 0009051  95
1244 265
0952 15
74222048 20342


Satellite: ISS
Catalog Number: 25544
Epoch time:      09259
53492705   =   yrday
fracday
Element set:     912
Inclination:       51
6396  deg
RA of node:       197
8840  deg
Eccentricity:     
0009051     
Arg of perigee:    95
1244  deg
Mean anomaly:     265
0952  deg
Mean motion:   15
74222048  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2034
Checksum:              296


Coasting Arc #14 (Orbit 2049)
---------------------------------------

Vector Time (GMT): 2009/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1029779
02                 A    =         6720264
50  meter
 Y    =       -4309282
89  meter          E    =           
0013810
 Z    =        5042866
89                 I    =           51
55251
 XDOT =       7517
086886                 Wp   =          109
44831
 YDOT =        205
330850  meter/sec      RA   =          191
91784  deg
 ZDOT =       1702
193610                 TA   =          324
13209
                                          MA   =          324
22474
                                          Ha   =            192
884  n
mi
                                          Hp   =            180
136

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3378540
10                 X    =        -1006012
59
 Y    =      -14138067
24  feet           Y    =        -4320665
13  meter
 Z    =       16544838
87                 Z    =         5037922
37
 XDOT =      24662
358549                 XDOT =        7505
963234
 YDOT =        673
657644  feet/sec       YDOT =         289
329304  meter/sec
 ZDOT =       5584
624704                 ZDOT =        1738
684437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2426870
58                 X    =          739710
15
 Y    =       14354908
30  feet           Y    =         4375376
05  meter
 Z    =       16525074
23                 Z    =         5036842
63
 XDOT =     -23466
534566                 XDOT =       -7152
599736
 YDOT =      -2658
407593  feet/sec       YDOT =        -810
282634  meter/sec
 ZDOT =       5728
335598                 ZDOT =        1745
996690


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
55060099  
00020000  00000-0  20000-3 0  9134
2 25544  51
6401 192
6668 0008851  99
5698 260
6466 15
74294865 20503


Satellite: ISS
Catalog Number: 25544
Epoch time:      09260
55060099   =   yrday
fracday
Element set:     913
Inclination:       51
6401  deg
RA of node:       192
6668  deg
Eccentricity:     
0008851     
Arg of perigee:    99
5698  deg
Mean anomaly:     260
6466  deg
Mean motion:   15
74294865  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2050
Checksum:              319


Coasting Arc #15 (Orbit 2064)
---------------------------------------

Vector Time (GMT): 2009/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6575452
95                 A    =         6730506
07  meter
 Y    =         333681
89  meter          E    =           
0014728
 Z    =       -1393815
95                 I    =           51
61655
 XDOT =      -1466
736980                 Wp   =           70
86882
 YDOT =      -4816
631770  meter/sec      RA   =          186
74858  deg
 ZDOT =       5820
959949                 TA   =          273
81093
                                          MA   =          273
97932
                                          Ha   =            192
865  n
mi
                                          Hp   =            180
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21573008
35                 X    =        -6571924
61
 Y    =        1094756
85  feet           Y    =          260170
89  meter
 Z    =       -4572886
97                 Z    =        -1425751
02
 XDOT =      -4812
129201                 XDOT =       -1441
044793
 YDOT =     -15802
597670  feet/sec       YDOT =       -4832
889434  meter/sec
 ZDOT =      19097
637628                 ZDOT =        5813
897430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21573431
23                 X    =         6575581
84
 Y    =         120175
74  feet           Y    =           36629
57  meter
 Z    =       -4698627
45                 Z    =        -1432141
65
 XDOT =       4034
634655                 XDOT =        1229
756643
 YDOT =      14481
285155  feet/sec       YDOT =        4413
895715  meter/sec
 ZDOT =      19069
494287                 ZDOT =        5812
381859


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
50278229  
00020000  00000-0  20000-3 0  9147
2 25544  51
6401 187
7748 0008902 102
2365 257
9796 15
74270477 20651


Satellite: ISS
Catalog Number: 25544
Epoch time:      09261
50278229   =   yrday
fracday
Element set:     914
Inclination:       51
6401  deg
RA of node:       187
7748  deg
Eccentricity:     
0008902     
Arg of perigee:   102
2365  deg
Mean anomaly:     257
9796  deg
Mean motion:   15
74270477  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2065
Checksum:              310

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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