Date: June 12th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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 489)
---------------------------------------

Vector Time (GMT): 2009/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5978327
07                 A    =         6732982
19  meter
 Y    =       -2928241
46  meter          E    =           
0016277
 Z    =        -992449
61                 I    =           51
54772
 XDOT =       2910
496425                 Wp   =           66
27452
 YDOT =       3963
147720  meter/sec      RA   =          340
70284  deg
 ZDOT =       5921
733089                 TA   =          282
87246
                                          MA   =          283
05424
                                          Ha   =            193
981  n
mi
                                          Hp   =            181
236

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19613933
97                 X    =         6015447
97
 Y    =       -9607091
41  feet           Y    =        -2861180
58  meter
 Z    =       -3256068
26                 Z    =         -963317
33
 XDOT =       9548
872785                 XDOT =        2837
196875
 YDOT =      13002
453151  feet/sec       YDOT =        3995
283631  meter/sec
 ZDOT =      19428
258165                 ZDOT =        5935
694961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5393451
56                 X    =        -1643924
03
 Y    =      -21181191
29  feet           Y    =        -6456027
11  meter
 Z    =       -3142038
74                 Z    =         -957693
41
 XDOT =      13111
798474                 XDOT =        3996
476175
 YDOT =      -6187
093677  feet/sec       YDOT =       -1885
826153  meter/sec
 ZDOT =      19483
112832                 ZDOT =        5938
452791


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   09161
50184860  
00010596  00000-0  82463-4 0  9009
2 25544  51
6384 341
2153 0008852  98
7985 261
4181 15
73574283  4908


Satellite: ISS
Catalog Number: 25544
Epoch time:      09161
50184860   =   yrday
fracday
Element set:     900
Inclination:       51
6384  deg
RA of node:       341
2153  deg
Eccentricity:     
0008852     
Arg of perigee:    98
7985  deg
Mean anomaly:     261
4181  deg
Mean motion:   15
73574283  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             490
Checksum:              317


Coasting Arc #2 (Orbit 505)
---------------------------------------

Vector Time (GMT): 2009/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2956886
17                 A    =         6721703
75  meter
 Y    =       -3166900
10  meter          E    =           
0022893
 Z    =       -5158725
57                 I    =           51
48259
 XDOT =       6439
494852                 Wp   =           88
70247
 YDOT =      -4004
690935  meter/sec      RA   =          335
58141  deg
 ZDOT =      -1236
767336                 TA   =          169
44939
                                          MA   =          169
40127
                                          Ha   =            193
940  n
mi
                                          Hp   =            181
048

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9701070
12                 X    =        -2896193
55
 Y    =      -10390092
18  feet           Y    =        -3199625
47  meter
 Z    =      -16924952
65                 Z    =        -5172943
20
 XDOT =      21126
951615                 XDOT =        6489
805353
 YDOT =     -13138
749788  feet/sec       YDOT =       -3932
399226  meter/sec
 ZDOT =      -4057
635618                 ZDOT =       -1205
362890

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12006138
90                 X    =        -3659471
14
 Y    =        7484947
83  feet           Y    =         2281412
10  meter
 Z    =      -16980782
78                 Z    =        -5175742
59
 XDOT =      -8395
800954                 XDOT =       -2559
040131
 YDOT =     -22362
497485  feet/sec       YDOT =       -6816
089234  meter/sec
 ZDOT =      -3934
744862                 ZDOT =       -1199
310234


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   09162
51794647  
00010596  00000-0  82463-4 0  9012
2 25544  51
6386 336
0002 0008986 102
4239 257
7930 15
73607218  5061


Satellite: ISS
Catalog Number: 25544
Epoch time:      09162
51794647   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:       336
0002  deg
Eccentricity:     
0008986     
Arg of perigee:   102
4239  deg
Mean anomaly:     257
7930  deg
Mean motion:   15
73607218  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             506
Checksum:              313


Coasting Arc #3 (Orbit 521)
---------------------------------------

Vector Time (GMT): 2009/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5240568
55                 A    =         6732571
43  meter
 Y    =        4045837
51  meter          E    =           
0022295
 Z    =        1170276
10                 I    =           51
49302
 XDOT =      -3810
047681                 Wp   =          115
50413
 YDOT =      -3213
104092  meter/sec      RA   =          330
41585  deg
 ZDOT =      -5876
114667                 TA   =           51
64364
                                          MA   =           51
44350
                                          Ha   =            193
736  n
mi
                                          Hp   =            181
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17193466
36                 X    =        -5291105
26
 Y    =       13273745
11  feet           Y    =         3986951
66  meter
 Z    =        3839488
53                 Z    =         1144695
42
 XDOT =     -12500
156433                 XDOT =       -3745
290069
 YDOT =     -10541
680092  feet/sec       YDOT =       -3255
347261  meter/sec
 ZDOT =     -19278
591426                 ZDOT =       -5894
467009

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10143945
75                 X    =         3091874
66
 Y    =       19226709
76  feet           Y    =         5860301
14  meter
 Z    =        3739420
16                 Z    =         1139775
27
 XDOT =     -11097
928005                 XDOT =       -3382
648456
 YDOT =       9669
383019  feet/sec       YDOT =        2947
227944  meter/sec
 ZDOT =     -19350
627685                 ZDOT =       -5898
071318


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   09163
53402461  
00010596  00000-0  82463-4 0  9026
2 25544  51
6385 330
7841 0008693 105
2496 254
9629 15
73665148  5221


Satellite: ISS
Catalog Number: 25544
Epoch time:      09163
53402461   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       330
7841  deg
Eccentricity:     
0008693     
Arg of perigee:   105
2496  deg
Mean anomaly:     254
9629  deg
Mean motion:   15
73665148  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             522
Checksum:              317


Coasting Arc #4 (Orbit 537)
---------------------------------------

Vector Time (GMT): 2009/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3662571
38                 A    =         6721797
51  meter
 Y    =        2400727
24  meter          E    =           
0013307
 Z    =        5090260
20                 I    =           51
43131
 XDOT =      -5477
784790                 Wp   =          114
50450
 YDOT =       5220
512934  meter/sec      RA   =          325
29376  deg
 ZDOT =       1470
798885                 TA   =          321
32329
                                          MA   =          321
41851
                                          Ha   =            193
707  n
mi
                                          Hp   =            181
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12016310
29                 X    =         3610726
36
 Y    =        7876401
71  feet           Y    =         2441393
65  meter
 Z    =       16700328
73                 Z    =         5107927
31
 XDOT =     -17971
734874                 XDOT =       -5542
899176
 YDOT =      17127
667105  feet/sec       YDOT =        5158
892862  meter/sec
 ZDOT =       4825
455661                 ZDOT =        1444
030477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9613350
03                 X    =         2930149
09
 Y    =      -10568477
79  feet           Y    =        -3221272
03  meter
 Z    =       16769650
42                 Z    =         5111389
45
 XDOT =      13390
373370                 XDOT =        4081
385803
 YDOT =      19714
771892  feet/sec       YDOT =        6009
062473  meter/sec
 ZDOT =       4720
785475                 ZDOT =        1438
895413


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   09164
55008880  
00010596  00000-0  82463-4 0  9037
2 25544  51
6384 325
5687 0008861 109
5506 250
6615 15
73641914  5386


Satellite: ISS
Catalog Number: 25544
Epoch time:      09164
55008880   =   yrday
fracday
Element set:     903
Inclination:       51
6384  deg
RA of node:       325
5687  deg
Eccentricity:     
0008861     
Arg of perigee:   109
5506  deg
Mean anomaly:     250
6615  deg
Mean motion:   15
73641914  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             538
Checksum:              323


Coasting Arc #5 (Orbit 552)
---------------------------------------

Vector Time (GMT): 2009/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4280405
80                 A    =         6732268
16  meter
 Y    =       -5009778
91  meter          E    =           
0013941
 Z    =       -1380236
35                 I    =           51
44429
 XDOT =       4508
564578                 Wp   =           75
50520
 YDOT =       2266
186033  meter/sec      RA   =          320
12133  deg
 ZDOT =       5808
866464                 TA   =          269
29614
                                          MA   =          269
45588
                                          Ha   =            193
758  n
mi
                                          Hp   =            181
195

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14043326
10                 X    =         4342812
79
 Y    =      -16436282
51  feet           Y    =        -4961563
80  meter
 Z    =       -4528334
48                 Z    =        -1359291
21
 XDOT =      14791
878538                 XDOT =        4454
670230
 YDOT =       7434
993545  feet/sec       YDOT =        2316
301354  meter/sec
 ZDOT =      19057
960841                 ZDOT =        5830
638427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14361734
73                 X    =        -4377456
75
 Y    =      -16181520
77  feet           Y    =        -4932127
53  meter
 Z    =       -4446477
83                 Z    =        -1355286
44
 XDOT =       8189
966305                 XDOT =        2496
301730
 YDOT =     -12481
234648  feet/sec       YDOT =       -3804
280321  meter/sec
 ZDOT =      19143
362195                 ZDOT =        5834
896797


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   09165
50263035  
00010596  00000-0  82463-4 0  9049
2 25544  51
6396 320
6794 0008939 113
6431 246
5671 15
73683963  5536


Satellite: ISS
Catalog Number: 25544
Epoch time:      09165
50263035   =   yrday
fracday
Element set:     904
Inclination:       51
6396  deg
RA of node:       320
6794  deg
Eccentricity:     
0008939     
Arg of perigee:   113
6431  deg
Mean anomaly:     246
5671  deg
Mean motion:   15
73683963  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             553
Checksum:              325


Coasting Arc #6 (Orbit 568)
---------------------------------------

Vector Time (GMT): 2009/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4155203
50                 A    =         6721749
83  meter
 Y    =       -1565034
62  meter          E    =           
0021383
 Z    =       -5064613
45                 I    =           51
38750
 XDOT =       4303
988853                 Wp   =           92
67171
 YDOT =      -6152
778400  meter/sec      RA   =          314
99946  deg
 ZDOT =      -1636
795914                 TA   =          161
54971
                                          MA   =          161
47205
                                          Ha   =            193
637  n
mi
                                          Hp   =            181
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13632557
42                 X    =        -4112791
16
 Y    =       -5134628
01  feet           Y    =        -1611262
78  meter
 Z    =      -16616185
85                 Z    =        -5084696
64
 XDOT =      14120
698336                 XDOT =        4380
421657
 YDOT =     -20186
280840  feet/sec       YDOT =       -6104
221126  meter/sec
 ZDOT =      -5370
065334                 ZDOT =       -1615
702171

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6715116
31                 X    =        -2046767
45
 Y    =       12825552
91  feet           Y    =         3909228
53  meter
 Z    =      -16694941
29                 Z    =        -5088618
10
 XDOT =     -17416
032403                 XDOT =       -5308
406677
 YDOT =     -15972
050624  feet/sec       YDOT =       -4868
281030  meter/sec
 ZDOT =      -5287
680347                 ZDOT =       -1611
684970


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   09166
51865767  
00010596  00000-0  82463-4 0  9052
2 25544  51
6398 315
4646 0008919 116
7425 243
4651 15
73724005  5695


Satellite: ISS
Catalog Number: 25544
Epoch time:      09166
51865767   =   yrday
fracday
Element set:     905
Inclination:       51
6398  deg
RA of node:       315
4646  deg
Eccentricity:     
0008919     
Arg of perigee:   116
7425  deg
Mean anomaly:     243
4651  deg
Mean motion:   15
73724005  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             569
Checksum:              337


Coasting Arc #7 (Orbit 584)
---------------------------------------

Vector Time (GMT): 2009/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3216963
34                 A    =         6732004
73  meter
 Y    =        5710914
24  meter          E    =           
0022829
 Z    =        1486102
57                 I    =           51
40109
 XDOT =      -4944
500738                 Wp   =          119
18127
 YDOT =      -1268
072015  meter/sec      RA   =          309
81975  deg
 ZDOT =      -5774
731896                 TA   =           44
38402
                                          MA   =           44
20126
                                          Ha   =            193
541  n
mi
                                          Hp   =            181
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10554341
65                 X    =        -3287803
92
 Y    =       18736595
27  feet           Y    =         5674544
01  meter
 Z    =        4875664
61                 Z    =         1470303
08
 XDOT =     -16222
115281                 XDOT =       -4901
900674
 YDOT =      -4160
341255  feet/sec       YDOT =       -1323
125426  meter/sec
 ZDOT =     -18945
970788                 ZDOT =       -5798
649113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17555006
07                 X    =         5350765
85
 Y    =       12444811
00  feet           Y    =         3793178
39  meter
 Z    =        4814008
37                 Z    =         1467309
75
 XDOT =      -4880
572790                 XDOT =       -1487
598586
 YDOT =      14321
217643  feet/sec       YDOT =        4365
107137  meter/sec
 ZDOT =     -19039
735159                 ZDOT =       -5803
311276


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   09167
53466688  
00010596  00000-0  82463-4 0  9065
2 25544  51
6390 310
2476 0008786 120
9723 239
2304 15
73734136  5853


Satellite: ISS
Catalog Number: 25544
Epoch time:      09167
53466688   =   yrday
fracday
Element set:     906
Inclination:       51
6390  deg
RA of node:       310
2476  deg
Eccentricity:     
0008786     
Arg of perigee:   120
9723  deg
Mean anomaly:     239
2304  deg
Mean motion:   15
73734136  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             585
Checksum:              328


Coasting Arc #8 (Orbit 600)
---------------------------------------

Vector Time (GMT): 2009/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4432170
36                 A    =         6721721
20  meter
 Y    =         631358
01  meter          E    =           
0014021
 Z    =        5006058
43                 I    =           51
35006
 XDOT =      -3012
129092                 Wp   =          124
59005
 YDOT =       6864
944161  meter/sec      RA   =          304
69626  deg
 ZDOT =       1789
617494                 TA   =          308
05030
                                          MA   =          308
17674
                                          Ha   =            193
252  n
mi
                                          Hp   =            181
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14541241
33                 X    =         4400462
22
 Y    =        2071384
54  feet           Y    =          680743
19  meter
 Z    =       16424076
21                 Z    =         5027513
20
 XDOT =      -9882
313294                 XDOT =       -3097
363918
 YDOT =      22522
782682  feet/sec       YDOT =        6830
783969  meter/sec
 ZDOT =       5871
448470                 ZDOT =        1774
778272

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3295425
62                 X    =         1004445
73
 Y    =      -14216514
40  feet           Y    =        -4333193
59  meter
 Z    =       16508164
68                 Z    =         5031688
59
 XDOT =      20559
005326                 XDOT =        6266
384823
 YDOT =      11559
605354  feet/sec       YDOT =        3523
367712  meter/sec
 ZDOT =       5813
606984                 ZDOT =        1771
987409


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   09168
55065741  
00010596  00000-0  82463-4 0  9074
2 25544  51
6400 305
0321 0008657 124
8145 235
3834 15
73794467  6011


Satellite: ISS
Catalog Number: 25544
Epoch time:      09168
55065741   =   yrday
fracday
Element set:     907
Inclination:       51
6400  deg
RA of node:       305
0321  deg
Eccentricity:     
0008657     
Arg of perigee:   124
8145  deg
Mean anomaly:     235
3834  deg
Mean motion:   15
73794467  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             601
Checksum:              305


Coasting Arc #9 (Orbit 615)
---------------------------------------

Vector Time (GMT): 2009/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2029864
54                 A    =         6731638
86  meter
 Y    =       -6212610
35  meter          E    =           
0011823
 Z    =       -1619062
11                 I    =           51
36823
 XDOT =       5140
566325                 Wp   =           84
68382
 YDOT =        198
546235  meter/sec      RA   =          299
51269  deg
 ZDOT =       5719
944745                 TA   =          257
38886
                                          MA   =          257
52110
                                          Ha   =            193
368  n
mi
                                          Hp   =            181
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6659660
58                 X    =         2107049
35
 Y    =      -20382579
90  feet           Y    =        -6189479
42  meter
 Z    =       -5311883
57                 Z    =        -1609014
34
 XDOT =      16865
375083                 XDOT =        5110
177273
 YDOT =        651
398410  feet/sec       YDOT =         255
860292  meter/sec
 ZDOT =      18766
222918                 ZDOT =        5744
844157

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19879856
94                 X    =        -6059380
40
 Y    =       -8062614
88  feet           Y    =        -2457485
02  meter
 Z    =       -5272786
63                 Z    =        -1607145
37
 XDOT =       1203
123907                 XDOT =         366
712167
 YDOT =     -15223
246159  feet/sec       YDOT =       -4640
045429  meter/sec
 ZDOT =      18863
789602                 ZDOT =        5749
683071


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   09169
50313390  
00010596  00000-0  82463-4 0  9087
2 25544  51
6408 300
1425 0008714 127
5485 232
6471 15
73790997  6168


Satellite: ISS
Catalog Number: 25544
Epoch time:      09169
50313390   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       300
1425  deg
Eccentricity:     
0008714     
Arg of perigee:   127
5485  deg
Mean anomaly:     232
6471  deg
Mean motion:   15
73790997  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             616
Checksum:              315


Coasting Arc #10 (Orbit 631)
---------------------------------------

Vector Time (GMT): 2009/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4507093
39                 A    =         6721765
21  meter
 Y    =         255030
93  meter          E    =           
0019460
 Z    =       -4996237
43                 I    =           51
32186
 XDOT =       1652
387238                 Wp   =           97
08547
 YDOT =      -7270
697689  meter/sec      RA   =          294
38824  deg
 ZDOT =      -1870
342686                 TA   =          154
80234
                                          MA   =          154
70727
                                          Ha   =            193
198  n
mi
                                          Hp   =            181
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14787051
80                 X    =        -4485339
06
 Y    =         836715
64  feet           Y    =          204752
48  meter
 Z    =      -16391855
10                 Z    =        -5018080
31
 XDOT =       5421
217972                 XDOT =        1742
652513
 YDOT =     -23853
995042  feet/sec       YDOT =       -7251
714704  meter/sec
 ZDOT =      -6136
294902                 ZDOT =       -1862
097284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          87334
65                 X    =           26619
60
 Y    =       14715183
09  feet           Y    =         4485187
81  meter
 Z    =      -16477429
01                 Z    =        -5022320
36
 XDOT =     -22472
293196                 XDOT =       -6849
554966
 YDOT =      -6670
539551  feet/sec       YDOT =       -2033
180455  meter/sec
 ZDOT =      -6104
303988                 ZDOT =       -1860
591856


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   09170
51909041  
00010596  00000-0  82463-4 0  9095
2 25544  51
6410 294
9267 0008571 131
2953 228
8949 15
73817392  6322


Satellite: ISS
Catalog Number: 25544
Epoch time:      09170
51909041   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:       294
9267  deg
Eccentricity:     
0008571     
Arg of perigee:   131
2953  deg
Mean anomaly:     228
8949  deg
Mean motion:   15
73817392  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             632
Checksum:              327


Coasting Arc #11 (Orbit 647)
---------------------------------------

Vector Time (GMT): 2009/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -844677
39                 A    =         6731466
88  meter
 Y    =        6456953
13  meter          E    =           
0022449
 Z    =        1657548
03                 I    =           51
34373
 XDOT =      -5116
673048                 Wp   =          123
17870
 YDOT =        807
334547  meter/sec      RA   =          289
20078  deg
 ZDOT =      -5708
881408                 TA   =           38
40735
                                          MA   =           38
24774
                                          Ha   =            193
142  n
mi
                                          Hp   =            181
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2771251
26                 X    =         -924869
51
 Y    =       21184229
44  feet           Y    =         6447058
74  meter
 Z    =        5438149
70                 Z    =         1653251
06
 XDOT =     -16786
985067                 XDOT =       -5097
587476
 YDOT =       2648
735391  feet/sec       YDOT =         750
224792  meter/sec
 ZDOT =     -18729
925878                 ZDOT =       -5733
691984

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21077744
19                 X    =         6424496
43
 Y    =        3515667
45  feet           Y    =         1071575
44  meter
 Z    =        5421592
49                 Z    =         1652501
39
 XDOT =       2340
758226                 XDOT =         713
463107
 YDOT =      15220
792199  feet/sec       YDOT =        4639
297462  meter/sec
 ZDOT =     -18827
109542                 ZDOT =       -5738
502988


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   09171
53502979  
00010596  00000-0  82463-4 0  9109
2 25544  51
6412 289
7103 0008630 135
1163 225
0699 15
73834682  6486


Satellite: ISS
Catalog Number: 25544
Epoch time:      09171
53502979   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       289
7103  deg
Eccentricity:     
0008630     
Arg of perigee:   135
1163  deg
Mean anomaly:     225
0699  deg
Mean motion:   15
73834682  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             648
Checksum:              315


Coasting Arc #12 (Orbit 663)
---------------------------------------

Vector Time (GMT): 2009/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4383049
75                 A    =         6721605
40  meter
 Y    =       -1147740
17  meter          E    =           
0014148
 Z    =        4958905
07                 I    =           51
30359
 XDOT =       -262
880062                 Wp   =          132
72867
 YDOT =       7452
015212  meter/sec      RA   =          284
07551  deg
 ZDOT =       1944
135106                 TA   =          298
34012
                                          MA   =          298
48275
                                          Ha   =            192
832  n
mi
                                          Hp   =            181
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14380084
47                 X    =         4371468
58
 Y    =       -3765551
73  feet           Y    =        -1098792
22  meter
 Z    =       16269373
59                 Z    =         4980169
69
 XDOT =       -862
467394                 XDOT =        -355
634542
 YDOT =      24448
868807  feet/sec       YDOT =        7448
556476  meter/sec
 ZDOT =       6378
396018                 ZDOT =        1942
634412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3528595
08                 X    =        -1075515
78
 Y    =      -14345676
04  feet           Y    =        -4372562
06  meter
 Z    =       16352654
89                 Z    =         4984289
21
 XDOT =      23384
670910                 XDOT =        7127
647693
 YDOT =       1560
828435  feet/sec       YDOT =         475
740507  meter/sec
 ZDOT =       6372
839633                 ZDOT =        1942
441520


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   09172
55094949  
00010596  00000-0  82463-4 0  9116
2 25544  51
6421 284
4945 0008466 138
7689 221
4115 15
73909730  6649


Satellite: ISS
Catalog Number: 25544
Epoch time:      09172
55094949   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:       284
4945  deg
Eccentricity:     
0008466     
Arg of perigee:   138
7689  deg
Mean anomaly:     221
4115  deg
Mean motion:   15
73909730  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             664
Checksum:              335


Coasting Arc #13 (Orbit 678)
---------------------------------------

Vector Time (GMT): 2009/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -374840
27                 A    =         6731227
49  meter
 Y    =       -6500161
54  meter          E    =           
0009917
 Z    =       -1717421
04                 I    =           51
32980
 XDOT =       4876
877987                 Wp   =           92
33277
 YDOT =      -1774
131052  meter/sec      RA   =          278
88630  deg
 ZDOT =       5678
240849                 TA   =          248
60038
                                          MA   =          248
70621
                                          Ha   =            192
894  n
mi
                                          Hp   =            181
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1229790
90                 X    =         -293783
58
 Y    =      -21325989
32  feet           Y    =        -6503899
61  meter
 Z    =       -5634583
47                 Z    =        -1719046
67
 XDOT =      16000
255863                 XDOT =        4868
770303
 YDOT =      -5820
639933  feet/sec       YDOT =       -1719
641630  meter/sec
 ZDOT =      18629
399110                 ZDOT =        5701
912611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21325284
07                 X    =        -6499946
58
 Y    =        1211358
14  feet           Y    =          369221
96  meter
 Z    =       -5641241
69                 Z    =        -1719450
47
 XDOT =      -5742
624599                 XDOT =       -1750
351978
 YDOT =     -14332
844417  feet/sec       YDOT =       -4368
650978  meter/sec
 ZDOT =      18722
094750                 ZDOT =        5706
494480


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   09173
50336108  
00010596  00000-0  82463-4 0  9129
2 25544  51
6422 279
6050 0008308 141
0927 219
0836 15
73878595  6793


Satellite: ISS
Catalog Number: 25544
Epoch time:      09173
50336108   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:       279
6050  deg
Eccentricity:     
0008308     
Arg of perigee:   141
0927  deg
Mean anomaly:     219
0836  deg
Mean motion:   15
73878595  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             679
Checksum:              322


Coasting Arc #14 (Orbit 694)
---------------------------------------

Vector Time (GMT): 2009/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4117373
87                 A    =         6721613
48  meter
 Y    =        1912519
98  meter          E    =           
0017696
 Z    =       -4970651
52                 I    =           51
29415
 XDOT =      -1079
642096                 Wp   =          101
63121
 YDOT =      -7359
703248  meter/sec      RA   =          273
76047  deg
 ZDOT =      -1946
800225                 TA   =          149
48789
                                          MA   =          149
38482
                                          Ha   =            192
728  n
mi
                                          Hp   =            181
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13508444
46                 X    =        -4114307
64
 Y    =        6274671
87  feet           Y    =         1866495
39  meter
 Z    =      -16307911
82                 Z    =        -4990645
69
 XDOT =      -3542
132861                 XDOT =        -987
807274
 YDOT =     -24146
008030  feet/sec       YDOT =       -7371
262515  meter/sec
 ZDOT =      -6387
139847                 ZDOT =       -1951
823708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6513098
96                 X    =         1985192
56
 Y    =       13299237
99  feet           Y    =         4053607
74  meter
 Z    =      -16386194
73                 Z    =        -4994512
15
 XDOT =     -23109
830873                 XDOT =       -7043
876450
 YDOT =       3461
019752  feet/sec       YDOT =        1054
918820  meter/sec
 ZDOT =      -6407
163645                 ZDOT =       -1952
903479


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   09174
51924878  
00010596  00000-0  82463-4 0  9139
2 25544  51
6421 274
3892 0008304 145
7451 214
4250 15
73910324  6951


Satellite: ISS
Catalog Number: 25544
Epoch time:      09174
51924878   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:       274
3892  deg
Eccentricity:     
0008304     
Arg of perigee:   145
7451  deg
Mean anomaly:     214
4250  deg
Mean motion:   15
73910324  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             695
Checksum:              310


Coasting Arc #15 (Orbit 710)
---------------------------------------

Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1513496
29                 A    =         6731107
81  meter
 Y    =        6323503
44  meter          E    =           
0021645
 Z    =        1693187
49                 I    =           51
32484
 XDOT =      -4494
082704                 Wp   =          127
68292
 YDOT =       2610
058458  meter/sec      RA   =          268
57069  deg
 ZDOT =      -5694
107492                 TA   =           33
48539
                                          MA   =           33
34874
                                          Ha   =            192
661  n
mi
                                          Hp   =            181
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4965539
03                 X    =         1434448
23
 Y    =       20746402
37  feet           Y    =         6339985
91  meter
 Z    =        5555077
06                 Z    =         1700349
26
 XDOT =     -14744
365828                 XDOT =       -4495
274229
 YDOT =       8563
183917  feet/sec       YDOT =        2559
797511  meter/sec
 ZDOT =     -18681
455027                 ZDOT =       -5715
941826

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20560745
27                 X    =         6266915
16
 Y    =       -5657696
33  feet           Y    =        -1724465
84  meter
 Z    =        5583448
44                 Z    =         1701835
08
 XDOT =       8658
255229                 XDOT =        2639
036194
 YDOT =      12827
025915  feet/sec       YDOT =        3909
677499  meter/sec
 ZDOT =     -18766
923522                 ZDOT =       -5720
158290


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   09175
53512011  
00010596  00000-0  82463-4 0  9145
2 25544  51
6412 269
1735 0008383 148
4780 211
6886 15
73935344  7113


Satellite: ISS
Catalog Number: 25544
Epoch time:      09175
53512011   =   yrday
fracday
Element set:     914
Inclination:       51
6412  deg
RA of node:       269
1735  deg
Eccentricity:     
0008383     
Arg of perigee:   148
4780  deg
Mean anomaly:     211
6886  deg
Mean motion:   15
73935344  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             711
Checksum:              308

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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