Date: August 15th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 1482)
---------------------------------------

Vector Time (GMT): 2009/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -294957
26                 A    =         6721581
29  meter
 Y    =        4223497
64  meter          E    =           
0005046
 Z    =        5221581
70                 I    =           51
71827
 XDOT =      -7480
998114                 Wp   =          338
75363
 YDOT =      -1598
859675  meter/sec      RA   =           17
24636  deg
 ZDOT =        875
531817                 TA   =          102
94568
                                          MA   =          102
88933
                                          Ha   =            191
163  n
mi
                                          Hp   =            185
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -967707
55                 X    =         -367528
70
 Y    =       13856619
55  feet           Y    =         4219793
31  meter
 Z    =       17131173
55                 Z    =         5219972
66
 XDOT =     -24543
957068                 XDOT =       -7466
816559
 YDOT =      -5245
602607  feet/sec       YDOT =       -1682
437322  meter/sec
 ZDOT =       2872
479714                 ZDOT =         839
223536

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9671815
51                 X    =         2947969
37
 Y    =       -9980437
42  feet           Y    =        -3042037
32  meter
 Z    =       17125020
42                 Z    =         5219706
22
 XDOT =      14819
782894                 XDOT =        4517
069826
 YDOT =      19017
692907  feet/sec       YDOT =        5796
592798  meter/sec
 ZDOT =       2729
613645                 ZDOT =         831
986239


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   09224
54904545  
00010596  00000-0  82463-4 0  9003
2 25544  51
6387  17
4993 0007858 324
1680  35
8954 15
73558160 14838


Satellite: ISS
Catalog Number: 25544
Epoch time:      09224
54904545   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:        17
4993  deg
Eccentricity:     
0007858     
Arg of perigee:   324
1680  deg
Mean anomaly:      35
8954  deg
Mean motion:   15
73558160  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1483
Checksum:              331


Coasting Arc #2 (Orbit 1497)
---------------------------------------

Vector Time (GMT): 2009/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6627259
98                 A    =         6733036
40  meter
 Y    =         703386
37  meter          E    =           
0014714
 Z    =        -889812
24                 I    =           51
72953
 XDOT =        280
024820                 Wp   =            8
46397
 YDOT =       4871
369261  meter/sec      RA   =           12
10475  deg
 ZDOT =       5963
041032                 TA   =          341
83152
                                          MA   =          341
88404
                                          Ha   =            191
247  n
mi
                                          Hp   =            185
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21742978
93                 X    =         6623224
58
 Y    =        2307698
07  feet           Y    =          777473
77  meter
 Z    =       -2919331
50                 Z    =         -857626
77
 XDOT =        918
716600                 XDOT =         196
564147
 YDOT =      15982
182616  feet/sec       YDOT =        4874
033685  meter/sec
 ZDOT =      19563
782912                 ZDOT =        5964
198932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15536401
80                 X    =        -4735495
27
 Y    =      -15408635
15  feet           Y    =        -4696551
99  meter
 Z    =       -2792719
33                 Z    =         -851220
85
 XDOT =       8243
452569                 XDOT =        2512
604343
 YDOT =     -11841
901219  feet/sec       YDOT =       -3609
411492  meter/sec
 ZDOT =      19568
534320                 ZDOT =        5964
489261


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   09225
50164011  
00010596  00000-0  82463-4 0  9017
2 25544  51
6401  12
6106 0007785 327
5438  32
5245 15
73587728 14980


Satellite: ISS
Catalog Number: 25544
Epoch time:      09225
50164011   =   yrday
fracday
Element set:     901
Inclination:       51
6401  deg
RA of node:        12
6106  deg
Eccentricity:     
0007785     
Arg of perigee:   327
5438  deg
Mean anomaly:      32
5245  deg
Mean motion:   15
73587728  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1498
Checksum:              297


Coasting Arc #3 (Orbit 1513)
---------------------------------------

Vector Time (GMT): 2009/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -769976
49                 A    =         6721590
40  meter
 Y    =       -4223586
29  meter          E    =           
0013915
 Z    =       -5182383
17                 I    =           51
66210
 XDOT =       7606
175887                 Wp   =           49
00540
 YDOT =         23
310542  meter/sec      RA   =            6
99545  deg
 ZDOT =      -1142
125068                 TA   =          210
04184
                                          MA   =          210
12174
                                          Ha   =            191
327  n
mi
                                          Hp   =            185
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2526169
57                 X    =         -697515
36
 Y    =      -13856910
41  feet           Y    =        -4231791
08  meter
 Z    =      -17002569
45                 Z    =        -5185948
02
 XDOT =      24954
645300                 XDOT =        7610
898142
 YDOT =         76
478156  feet/sec       YDOT =         108
393752  meter/sec
 ZDOT =      -3747
129488                 ZDOT =       -1105
162862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6558894
26                 X    =        -1999150
97
 Y    =       12445630
73  feet           Y    =         3793428
25  meter
 Z    =      -17016757
87                 Z    =        -5186707
80
 XDOT =     -18800
894808                 XDOT =       -5730
512738
 YDOT =     -14864
002983  feet/sec       YDOT =       -4530
548109  meter/sec
 ZDOT =      -3601
756832                 ZDOT =       -1097
815482


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   09226
51773421  
00010596  00000-0  82463-4 0  9021
2 25544  51
6403   7
3967 0007849 332
0253  28
0487 15
73618939 15141


Satellite: ISS
Catalog Number: 25544
Epoch time:      09226
51773421   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:         7
3967  deg
Eccentricity:     
0007849     
Arg of perigee:   332
0253  deg
Mean anomaly:      28
0487  deg
Mean motion:   15
73618939  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1514
Checksum:              312


Coasting Arc #4 (Orbit 1529)
---------------------------------------

Vector Time (GMT): 2009/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6609081
21                 A    =         6732777
11  meter
 Y    =         654786
62  meter          E    =           
0008155
 Z    =        1096713
44                 I    =           51
66947
 XDOT =      -1453
327398                 Wp   =           92
70614
 YDOT =      -4717
338361  meter/sec      RA   =            1
84369  deg
 ZDOT =      -5904
416512                 TA   =           75
30655
                                          MA   =           75
21617
                                          Ha   =            191
482  n
mi
                                          Hp   =            185
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21683337
31                 X    =        -6621239
55
 Y    =        2148250
06  feet           Y    =          580811
92  meter
 Z    =        3598141
20                 Z    =         1064577
23
 XDOT =      -4768
134507                 XDOT =       -1371
786880
 YDOT =     -15476
831892  feet/sec       YDOT =       -4733
133874  meter/sec
 ZDOT =     -19371
445248                 ZDOT =       -5911
279097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18677996
97                 X    =         5693053
48
 Y    =       11260903
22  feet           Y    =         3432323
30  meter
 Z    =        3471772
38                 Z    =         1058196
22
 XDOT =      -4706
127475                 XDOT =       -1434
427654
 YDOT =      13825
569703  feet/sec       YDOT =        4214
033646  meter/sec
 ZDOT =     -19398
621736                 ZDOT =       -5912
699905


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   09227
53382029  
00010596  00000-0  82463-4 0  9035
2 25544  51
6399   2
1802 0007911 335
1968  24
8814 15
73617057 15309


Satellite: ISS
Catalog Number: 25544
Epoch time:      09227
53382029   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:         2
1802  deg
Eccentricity:     
0007911     
Arg of perigee:   335
1968  deg
Mean anomaly:      24
8814  deg
Mean motion:   15
73617057  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1530
Checksum:              304


Coasting Arc #5 (Orbit 1545)
---------------------------------------

Vector Time (GMT): 2009/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1757889
80                 A    =         6721658
18  meter
 Y    =        3970931
91  meter          E    =           
0004992
 Z    =        5129047
54                 I    =           51
60385
 XDOT =      -7424
932823                 Wp   =            6
36268
 YDOT =       1515
983291  meter/sec      RA   =          356
73253  deg
 ZDOT =       1375
829996                 TA   =           70
48933
                                          MA   =           70
43542
                                          Ha   =            191
551  n
mi
                                          Hp   =            184
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5767354
98                 X    =         1688439
80
 Y    =       13027991
82  feet           Y    =         3990200
87  meter
 Z    =       16827583
79                 Z    =         5137418
95
 XDOT =     -24360
015825                 XDOT =       -7448
016429
 YDOT =       4973
698460  feet/sec       YDOT =        1432
824142  meter/sec
 ZDOT =       4513
877941                 ZDOT =        1339
704148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3011448
08                 X    =          917889
37
 Y    =      -13885518
63  feet           Y    =        -4232306
08  meter
 Z    =       16860666
75                 Z    =         5139131
23
 XDOT =      21683
816329                 XDOT =        6609
227217
 YDOT =       9992
411849  feet/sec       YDOT =        3045
687131  meter/sec
 ZDOT =       4371
845933                 ZDOT =        1332
538640


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   09228
54989777  
00010596  00000-0  82463-4 0  9041
2 25544  51
6411 356
9650 0008005 338
7279  21
3550 15
73655517 15463


Satellite: ISS
Catalog Number: 25544
Epoch time:      09228
54989777   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:       356
9650  deg
Eccentricity:     
0008005     
Arg of perigee:   338
7279  deg
Mean anomaly:      21
3550  deg
Mean motion:   15
73655517  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1546
Checksum:              334


Coasting Arc #6 (Orbit 1560)
---------------------------------------

Vector Time (GMT): 2009/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6290007
42                 A    =         6732527
53  meter
 Y    =       -1980711
83  meter          E    =           
0015236
 Z    =       -1309745
24                 I    =           51
61102
 XDOT =       2568
610376                 Wp   =           11
62502
 YDOT =       4305
563943  meter/sec      RA   =          351
57432  deg
 ZDOT =       5850
809060                 TA   =          333
98401
                                          MA   =          334
06051
                                          Ha   =            191
834  n
mi
                                          Hp   =            184
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20636507
30                 X    =         6318050
99
 Y    =       -6498398
40  feet           Y    =        -1910216
37  meter
 Z    =       -4297064
44                 Z    =        -1279120
94
 XDOT =       8427
199396                 XDOT =        2491
852229
 YDOT =      14125
865955  feet/sec       YDOT =        4333
858006  meter/sec
 ZDOT =      19195
567782                 ZDOT =        5863
101060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20678363
28                 X    =        -6302765
13
 Y    =       -6443598
60  feet           Y    =        -1964008
85  meter
 Z    =       -4176686
14                 Z    =        -1273053
93
 XDOT =        754
735141                 XDOT =         230
043271
 YDOT =     -14838
148402  feet/sec       YDOT =       -4522
667633  meter/sec
 ZDOT =      19244
088926                 ZDOT =        5865
598305


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   09229
50246479  
00010596  00000-0  82463-4 0  9054
2 25544  51
6418 352
0762 0008058 343
3549  16
7348 15
73629101 15611


Satellite: ISS
Catalog Number: 25544
Epoch time:      09229
50246479   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:       352
0762  deg
Eccentricity:     
0008058     
Arg of perigee:   343
3549  deg
Mean anomaly:      16
7348  deg
Mean motion:   15
73629101  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1561
Checksum:              315


Coasting Arc #7 (Orbit 1576)
---------------------------------------

Vector Time (GMT): 2009/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2685064
45                 A    =         6721912
22  meter
 Y    =       -3504159
84  meter          E    =           
0015813
 Z    =       -5081532
65                 I    =           51
54652
 XDOT =       6911
467321                 Wp   =           46
89118
 YDOT =      -2968
679605  meter/sec      RA   =          346
46336  deg
 ZDOT =      -1597
338079                 TA   =          207
68479
                                          MA   =          207
76906
                                          Ha   =            191
872  n
mi
                                          Hp   =            184
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8809266
57                 X    =        -2620996
13
 Y    =      -11496587
41  feet           Y    =        -3533827
31  meter
 Z    =      -16671695
05                 Z    =        -5094420
99
 XDOT =      22675
417721                 XDOT =        6951
909347
 YDOT =      -9739
762485  feet/sec       YDOT =       -2891
165312  meter/sec
 ZDOT =      -5240
610495                 ZDOT =       -1563
664812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         848494
29                 X    =          258621
06
 Y    =       14399895
51  feet           Y    =         4389088
15  meter
 Z    =      -16722535
16                 Z    =        -5097028
72
 XDOT =     -23237
594706                 XDOT =       -7082
818866
 YDOT =      -4591
443603  feet/sec       YDOT =       -1399
472010  meter/sec
 ZDOT =      -5108
278450                 ZDOT =       -1557
003271


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   09230
51852755  
00010596  00000-0  82463-4 0  9068
2 25544  51
6421 346
8617 0008112 346
8153  13
2796 15
73648800 15778


Satellite: ISS
Catalog Number: 25544
Epoch time:      09230
51852755   =   yrday
fracday
Element set:     906
Inclination:       51
6421  deg
RA of node:       346
8617  deg
Eccentricity:     
0008112     
Arg of perigee:   346
8153  deg
Mean anomaly:      13
2796  deg
Mean motion:   15
73648800  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1577
Checksum:              316


Coasting Arc #8 (Orbit 1592)
---------------------------------------

Vector Time (GMT): 2009/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5745983
07                 A    =         6732253
71  meter
 Y    =        3180726
35  meter          E    =           
0011083
 Z    =        1474005
96                 I    =           51
55276
 XDOT =      -3518
752568                 Wp   =           83
56204
 YDOT =      -3657
886321  meter/sec      RA   =          341
29719  deg
 ZDOT =      -5785
182623                 TA   =           80
20078
                                          MA   =           80
07565
                                          Ha   =            192
013  n
mi
                                          Hp   =            184
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18851650
51                 X    =        -5788283
74
 Y    =       10435453
90  feet           Y    =         3116234
85  meter
 Z    =        4835977
57                 Z    =         1445989
93
 XDOT =     -11544
463806                 XDOT =       -3449
485202
 YDOT =     -12000
939372  feet/sec       YDOT =       -3696
847664  meter/sec
 ZDOT =     -18980
257951                 ZDOT =       -5802
108164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21522591
13                 X    =         6560085
78
 Y    =        1453940
48  feet           Y    =          443161
06  meter
 Z    =        4725910
72                 Z    =         1440457
59
 XDOT =       3216
758330                 XDOT =         980
467939
 YDOT =      14711
913611  feet/sec       YDOT =        4484
191268  meter/sec
 ZDOT =     -19046
990254                 ZDOT =       -5805
522630


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   09231
53458279  
00010596  00000-0  82463-4 0  9075
2 25544  51
6423 341
6465 0008054 351
1438   8
9582 15
73655693 15934


Satellite: ISS
Catalog Number: 25544
Epoch time:      09231
53458279   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:       341
6465  deg
Eccentricity:     
0008054     
Arg of perigee:   351
1438  deg
Mean anomaly:       8
9582  deg
Mean motion:   15
73655693  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1593
Checksum:              329


Coasting Arc #9 (Orbit 1608)
---------------------------------------

Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3435557
81                 A    =         6721929
66  meter
 Y    =        2850619
89  meter          E    =           
0006195
 Z    =        5021071
93                 I    =           51
49153
 XDOT =      -6155
601751                 Wp   =           34
70005
 YDOT =       4273
445695  meter/sec      RA   =          336
18425  deg
 ZDOT =       1789
600318                 TA   =           38
05365
                                          MA   =           38
00991
                                          Ha   =            191
996  n
mi
                                          Hp   =            183
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11271515
13                 X    =         3379035
40
 Y    =        9352427
46  feet           Y    =         2888722
33  meter
 Z    =       16473333
10                 Z    =         5037624
20
 XDOT =     -20195
543803                 XDOT =       -6211
624034
 YDOT =      14020
491125  feet/sec       YDOT =        4204
296922  meter/sec
 ZDOT =       5871
392120                 ZDOT =        1759
560905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4566879
20                 X    =        -1391984
78
 Y    =      -13838537
02  feet           Y    =        -4217986
08  meter
 Z    =       16538565
94                 Z    =         5040954
90
 XDOT =      23572
157041                 XDOT =        7184
793466
 YDOT =       -918
486713  feet/sec       YDOT =        -279
954750  meter/sec
 ZDOT =       5753
420727                 ZDOT =        1753
642638


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   09232
55062824  
00010596  00000-0  82463-4 0  9086
2 25544  51
6430 336
4312 0008171 354
8085   5
2992 15
73709960 16093


Satellite: ISS
Catalog Number: 25544
Epoch time:      09232
55062824   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:       336
4312  deg
Eccentricity:     
0008171     
Arg of perigee:   354
8085  deg
Mean anomaly:       5
2992  deg
Mean motion:   15
73709960  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1609
Checksum:              309


Coasting Arc #10 (Orbit 1623)
---------------------------------------

Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4945319
20                 A    =         6732004
42  meter
 Y    =       -4244221
08  meter          E    =           
0015440
 Z    =       -1654152
13                 I    =           51
49798
 XDOT =       4320
187021                 Wp   =           17
08219
 YDOT =       2813
299944  meter/sec      RA   =          331
01190  deg
 ZDOT =       5725
420556                 TA   =          324
59481
                                          MA   =          324
69722
                                          Ha   =            192
378  n
mi
                                          Hp   =            183
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16224800
53                 X    =         5000446
71
 Y    =      -13924609
86  feet           Y    =        -4188611
44  meter
 Z    =       -5427008
29                 Z    =        -1629994
12
 XDOT =      14173
841931                 XDOT =        4260
594514
 YDOT =       9229
986694  feet/sec       YDOT =        2861
277792  meter/sec
 ZDOT =      18784
188177                 ZDOT =        5746
262855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21094987
09                 X    =        -6429752
07
 Y    =        3627771
18  feet           Y    =         1105744
65  meter
 Z    =       -5332178
44                 Z    =        -1625247
99
 XDOT =      -7083
160889                 XDOT =       -2158
947439
 YDOT =     -13594
818282  feet/sec       YDOT =       -4143
700612  meter/sec
 ZDOT =      18866
294405                 ZDOT =        5750
446535


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   09233
50316610  
00010596  00000-0  82463-4 0  9098
2 25544  51
6430 331
5430 0008425 358
6363   1
4776 15
73656199 16243


Satellite: ISS
Catalog Number: 25544
Epoch time:      09233
50316610   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       331
5430  deg
Eccentricity:     
0008425     
Arg of perigee:   358
6363  deg
Mean anomaly:       1
4776  deg
Mean motion:   15
73656199  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1624
Checksum:              301


Coasting Arc #11 (Orbit 1639)
---------------------------------------

Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4050194
79                 A    =         6722256
02  meter
 Y    =       -2046271
49  meter          E    =           
0017367
 Z    =       -4974137
75                 I    =           51
43952
 XDOT =       5137
149445                 Wp   =           47
93715
 YDOT =      -5371
208886  meter/sec      RA   =          325
89860  deg
 ZDOT =      -1966
254276                 TA   =          202
93286
                                          MA   =          203
01050
                                          Ha   =            192
353  n
mi
                                          Hp   =            183
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13288040
64                 X    =        -4002848
79
 Y    =       -6713489
14  feet           Y    =        -2091298
61  meter
 Z    =      -16319349
56                 Z    =        -4993698
31
 XDOT =      16854
164847                 XDOT =        5206
381034
 YDOT =     -17622
076399  feet/sec       YDOT =       -5313
375244  meter/sec
 ZDOT =      -6450
965472                 ZDOT =       -1941
129889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8103174
01                 X    =         2469847
44
 Y    =       12387957
32  feet           Y    =         3775849
39  meter
 Z    =      -16396378
11                 Z    =        -4997616
05
 XDOT =     -22516
959187                 XDOT =       -6863
169160
 YDOT =       6290
377924  feet/sec       YDOT =        1917
307191  meter/sec
 ZDOT =      -6352
394171                 ZDOT =       -1936
209743


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   09234
51919760  
00010596  00000-0  82463-4 0  9107
2 25544  51
6426 326
3283 0008293   2
1540 357
9657 15
73683036 16402


Satellite: ISS
Catalog Number: 25544
Epoch time:      09234
51919760   =   yrday
fracday
Element set:     910
Inclination:       51
6426  deg
RA of node:       326
3283  deg
Eccentricity:     
0008293     
Arg of perigee:     2
1540  deg
Mean anomaly:     357
9657  deg
Mean motion:   15
73683036  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1640
Checksum:              309


Coasting Arc #12 (Orbit 1655)
---------------------------------------

Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4006846
39                 A    =         6731678
18  meter
 Y    =        5106962
71  meter          E    =           
0014048
 Z    =        1777064
15                 I    =           51
44658
 XDOT =      -4876
663958                 Wp   =           79
97808
 YDOT =      -1841
631785  meter/sec      RA   =          320
71931  deg
 ZDOT =      -5662
818045                 TA   =           80
28841
                                          MA   =           80
12977
                                          Ha   =            192
512  n
mi
                                          Hp   =            183
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13145821
49                 X    =        -4072288
14
 Y    =       16755127
02  feet           Y    =         5061789
96  meter
 Z    =        5830262
95                 Z    =         1757439
86
 XDOT =     -15999
553667                 XDOT =       -4828
199255
 YDOT =      -6042
099032  feet/sec       YDOT =       -1895
894713  meter/sec
 ZDOT =     -18578
799361                 ZDOT =       -5686
390981

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19629015
22                 X    =         5982923
84
 Y    =       -8315044
64  feet           Y    =        -2534425
61  meter
 Z    =        5753317
67                 Z    =         1753611
23
 XDOT =      10396
023291                 XDOT =        3168
707899
 YDOT =      11529
489244  feet/sec       YDOT =        3514
188322  meter/sec
 ZDOT =     -18671
596761                 ZDOT =       -5691
102693


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   09235
53522150  
00010596  00000-0  82463-4 0  9114
2 25544  51
6418 321
1132 0008378   7
2791 352
8492 15
73705852 16566


Satellite: ISS
Catalog Number: 25544
Epoch time:      09235
53522150   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:       321
1132  deg
Eccentricity:     
0008378     
Arg of perigee:     7
2791  deg
Mean anomaly:     352
8492  deg
Mean motion:   15
73705852  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1656
Checksum:              300


Coasting Arc #13 (Orbit 1671)
---------------------------------------

Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4433401
44                 A    =         6722260
17  meter
 Y    =        1149703
03  meter          E    =           
0008210
 Z    =        4913318
17                 I    =           51
39332
 XDOT =      -3969
387160                 Wp   =           53
17566
 YDOT =       6256
033162  meter/sec      RA   =          315
60318  deg
 ZDOT =       2120
190514                 TA   =           16
22387
                                          MA   =           16
19761
                                          Ha   =            192
413  n
mi
                                          Hp   =            182
988

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14545280
33                 X    =         4396347
79
 Y    =        3771991
57  feet           Y    =         1199072
85  meter
 Z    =       16119810
28                 Z    =         4934765
58
 XDOT =     -13022
923754                 XDOT =       -4049
347672
 YDOT =      20525
043183  feet/sec       YDOT =        6211
198102  meter/sec
 ZDOT =       6956
005623                 ZDOT =        2100
712912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11011896
84                 X    =        -3356426
16
 Y    =      -10089745
45  feet           Y    =        -3075354
41  meter
 Z    =       16204213
91                 Z    =         4939044
40
 XDOT =      20406
683939                 XDOT =        6219
957265
 YDOT =     -11235
563153  feet/sec       YDOT =       -3424
599649  meter/sec
 ZDOT =       6879
693813                 ZDOT =        2096
930674


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   09236
55123548  
00010596  00000-0  82463-4 0  9126
2 25544  51
6420 315
8971 0008418  10
2632 349
8701 15
73747053 16729


Satellite: ISS
Catalog Number: 25544
Epoch time:      09236
55123548   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:       315
8971  deg
Eccentricity:     
0008418     
Arg of perigee:    10
2632  deg
Mean anomaly:     349
8701  deg
Mean motion:   15
73747053  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1672
Checksum:              305


Coasting Arc #14 (Orbit 1686)
---------------------------------------

Vector Time (GMT): 2009/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2885774
35                 A    =         6731434
01  meter
 Y    =       -5760013
12  meter          E    =           
0015318
 Z    =       -1926249
26                 I    =           51
40252
 XDOT =       5231
087144                 Wp   =           24
59517
 YDOT =        756
641828  meter/sec      RA   =          310
41845  deg
 ZDOT =       5603
937548                 TA   =          313
90296
                                          MA   =          314
02933
                                          Ha   =            192
766  n
mi
                                          Hp   =            182
856

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9467763
61                 X    =         2959326
70
 Y    =      -18897680
85  feet           Y    =        -5727331
45  meter
 Z    =       -6319715
40                 Z    =        -1912051
49
 XDOT =      17162
359397                 XDOT =        5195
014542
 YDOT =       2482
420697  feet/sec       YDOT =         814
937242  meter/sec
 ZDOT =      18385
621878                 ZDOT =        5629
262546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17022170
56                 X    =        -5188357
59
 Y    =       12558099
73  feet           Y    =         3827708
80  meter
 Z    =       -6264146
60                 Z    =        -1909311
88
 XDOT =     -13173
601240                 XDOT =       -4015
313658
 YDOT =      -8684
726474  feet/sec       YDOT =       -2647
104629  meter/sec
 ZDOT =      18485
256413                 ZDOT =        5634
306155


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   09237
50374356  
00010596  00000-0  82463-4 0  9138
2 25544  51
6413 311
0083 0008660  13
4632 346
6760 15
73702419 16870


Satellite: ISS
Catalog Number: 25544
Epoch time:      09237
50374356   =   yrday
fracday
Element set:     913
Inclination:       51
6413  deg
RA of node:       311
0083  deg
Eccentricity:     
0008660     
Arg of perigee:    13
4632  deg
Mean anomaly:     346
6760  deg
Mean motion:   15
73702419  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1687
Checksum:              298


Coasting Arc #15 (Orbit 1702)
---------------------------------------

Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4643667
65                 A    =         6722546
30  meter
 Y    =        -186059
54  meter          E    =           
0018656
 Z    =       -4873991
04                 I    =           51
35370
 XDOT =       2646
258367                 Wp   =           50
97891
 YDOT =      -6855
651176  meter/sec      RA   =          305
30179  deg
 ZDOT =      -2253
716897                 TA   =          196
93989
                                          MA   =          197
00226
                                          Ha   =            192
798  n
mi
                                          Hp   =            182
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15235130
08                 X    =        -4617565
01
 Y    =        -610431
55  feet           Y    =         -237841
74  meter
 Z    =      -15990784
25                 Z    =        -4896486
57
 XDOT =       8681
950023                 XDOT =        2733
670905
 YDOT =     -22492
293884  feet/sec       YDOT =       -6825
570381  meter/sec
 ZDOT =      -7394
084308                 ZDOT =       -2240
649147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13354492
41                 X    =         4070449
29
 Y    =        7162524
53  feet           Y    =         2183137
48  meter
 Z    =      -16079265
26                 Z    =        -4900960
05
 XDOT =     -17150
035884                 XDOT =       -5227
330937
 YDOT =      15449
352713  feet/sec       YDOT =        4708
962707  meter/sec
 ZDOT =      -7343
011571                 ZDOT =       -2238
149927


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   09238
51974407  
00010596  00000-0  82463-4 0  9144
2 25544  51
6406 305
7925 0008592  17
9331 342
2133 15
73728413 17033


Satellite: ISS
Catalog Number: 25544
Epoch time:      09238
51974407   =   yrday
fracday
Element set:     914
Inclination:       51
6406  deg
RA of node:       305
7925  deg
Eccentricity:     
0008592     
Arg of perigee:    17
9331  deg
Mean anomaly:     342
2133  deg
Mean motion:   15
73728413  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1703
Checksum:              307

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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