Date: August 6th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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


226/07:54:26 102 4 0 10 6 10 6
N/A 9 1 0 1 195 6
000/00:18:52 205 -3 6 -0 2 188 8

Coasting Arc #1 (Orbit 3566)
---------------------------------------

Vector Time (GMT): 2008/214/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4766026
54                 A    =         6726350
20  meter
 Y    =        -951821
78  meter          E    =           
0012124
 Z    =        4638231
55                 I    =           51
82799
 XDOT =       4001
649534                 Wp   =           60
23777
 YDOT =      -5915
237715  meter/sec      RA   =          142
68297  deg
 ZDOT =       2898
306138                 TA   =            1
18724
                                          MA   =            1
18436
                                          Ha   =            194
887  n
mi
                                          Hp   =            183
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15636570
00                 X    =        -4777560
00
 Y    =       -3122774
87  feet           Y    =        -1005183
19  meter
 Z    =       15217295
13                 Z    =         4615050
69
 XDOT =      13128
771437                 XDOT =        4053
418176
 YDOT =     -19406
947884  feet/sec       YDOT =       -5870
199817  meter/sec
 ZDOT =       9508
878405                 ZDOT =        2917
870780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5734568
94                 X    =         1747896
61
 Y    =       14969577
59  feet           Y    =         4562727
25  meter
 Z    =       15127676
00                 Z    =         4610915
64
 XDOT =     -22297
246017                 XDOT =       -6796
200586
 YDOT =      -1142
479209  feet/sec       YDOT =        -348
227663  meter/sec
 ZDOT =       9583
858763                 ZDOT =        2921
160151


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   08214
53195304  
00020000  00000-0  20000-3 0  9004
2 25544  51
6409 143
3468 0010141  17
7053 342
4461 15
72794588 35677


Satellite: ISS
Catalog Number: 25544
Epoch time:      08214
53195304   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       143
3468  deg
Eccentricity:     
0010141     
Arg of perigee:    17
7053  deg
Mean anomaly:     342
4461  deg
Mean motion:   15
72794588  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3567
Checksum:              283


Coasting Arc #2 (Orbit 3581)
---------------------------------------

Vector Time (GMT): 2008/215/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2634544
93                 A    =         6732036
43  meter
 Y    =        5479347
79  meter          E    =           
0013967
 Z    =       -2882343
76                 I    =           51
86954
 XDOT =      -5780
815840                 Wp   =           34
62738
 YDOT =       -117
633424  meter/sec      RA   =          137
52635  deg
 ZDOT =       5083
408456                 TA   =          292
37567
                                          MA   =          292
52360
                                          Ha   =            194
926  n
mi
                                          Hp   =            183
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8643520
12                 X    =        -2681618
51
 Y    =       17976862
82  feet           Y    =         5449623
80  meter
 Z    =       -9456508
41                 Z    =        -2895256
01
 XDOT =     -18965
931232                 XDOT =       -5803
764467
 YDOT =       -385
936432  feet/sec       YDOT =        -182
406512  meter/sec
 ZDOT =      16677
849265                 ZDOT =        5055
270200

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19746507
76                 X    =         6018735
57
 Y    =       -2649152
59  feet           Y    =         -807461
71  meter
 Z    =       -9505840
84                 Z    =        -2897380
29
 XDOT =       9915
245087                 XDOT =        3022
166703
 YDOT =      14724
496926  feet/sec       YDOT =        4488
026663  meter/sec
 ZDOT =      16569
156546                 ZDOT =        5050
278915


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   08215
48504323  
00020000  00000-0  20000-3 0  9015
2 25544  51
6408 138
4614 0010302  21
0898 339
0688 15
72766352 35826


Satellite: ISS
Catalog Number: 25544
Epoch time:      08215
48504323   =   yrday
fracday
Element set:     901
Inclination:       51
6408  deg
RA of node:       138
4614  deg
Eccentricity:     
0010302     
Arg of perigee:    21
0898  deg
Mean anomaly:     339
0688  deg
Mean motion:   15
72766352  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3582
Checksum:              283


Coasting Arc #3 (Orbit 3597)
---------------------------------------

Vector Time (GMT): 2008/216/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5189779
82                 A    =         6727927
35  meter
 Y    =        -749856
51  meter          E    =           
0017132
 Z    =       -4233512
93                 I    =           51
87742
 XDOT =      -2037
324409                 Wp   =           45
03052
 YDOT =       6454
480886  meter/sec      RA   =          132
46495  deg
 ZDOT =      -3637
852888                 TA   =          187
95726
                                          MA   =          187
98447
                                          Ha   =            194
995  n
mi
                                          Hp   =            183
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17026836
68                 X    =         5218344
32
 Y    =       -2460159
17  feet           Y    =         -691661
49  meter
 Z    =      -13889478
13                 Z    =        -4208232
18
 XDOT =      -6684
135201                 XDOT =       -2091
676372
 YDOT =      21176
118391  feet/sec       YDOT =        6431
394634  meter/sec
 ZDOT =     -11935
212886                 ZDOT =       -3647
881700

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11642000
66                 X    =        -3548481
80
 Y    =      -12772251
90  feet           Y    =        -3892982
38  meter
 Z    =      -13791901
80                 Z    =        -4203771
67
 XDOT =      20305
487943                 XDOT =        6189
112725
 YDOT =      -5569
051298  feet/sec       YDOT =       -1697
446836  meter/sec
 ZDOT =     -11973
312937                 ZDOT =       -3649
465783


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   08216
50166184  
00020000  00000-0  20000-3 0  9029
2 25544  51
6417 133
2498 0010348  25
3848 334
7821 15
72807980 35982


Satellite: ISS
Catalog Number: 25544
Epoch time:      08216
50166184   =   yrday
fracday
Element set:     902
Inclination:       51
6417  deg
RA of node:       133
2498  deg
Eccentricity:     
0010348     
Arg of perigee:    25
3848  deg
Mean anomaly:     334
7821  deg
Mean motion:   15
72807980  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3598
Checksum:              303


Coasting Arc #4 (Orbit 3613)
---------------------------------------

Vector Time (GMT): 2008/217/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         917027
88                 A    =         6730345
00  meter
 Y    =       -5690664
64  meter          E    =           
0019689
 Z    =        3468888
26                 I    =           51
90415
 XDOT =       5913
702123                 Wp   =           61
83522
 YDOT =      -1850
054243  meter/sec      RA   =          127
30614  deg
 ZDOT =      -4569
664806                 TA   =           77
22925
                                          MA   =           77
00929
                                          Ha   =            195
053  n
mi
                                          Hp   =            183
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3008621
65                 X    =          963742
69
 Y    =      -18670159
57  feet           Y    =        -5680148
83  meter
 Z    =       11380866
99                 Z    =         3473456
38
 XDOT =      19401
909854                 XDOT =        5956
148445
 YDOT =      -6069
731770  feet/sec       YDOT =       -1783
686337  meter/sec
 ZDOT =     -14992
338602                 ZDOT =       -4540
833481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16960102
20                 X    =        -5169439
15
 Y    =        8342207
84  feet           Y    =         2542704
95  meter
 Z    =       11397951
48                 Z    =         3474095
61
 XDOT =     -15573
996119                 XDOT =       -4746
954017
 YDOT =     -11202
295094  feet/sec       YDOT =       -3414
459545  meter/sec
 ZDOT =     -14881
150966                 ZDOT =       -4535
774815


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   08217
51827070  
00020000  00000-0  20000-3 0  9030
2 25544  51
6413 128
0386 0010301  29
0141 331
1592 15
72805586 36147


Satellite: ISS
Catalog Number: 25544
Epoch time:      08217
51827070   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       128
0386  deg
Eccentricity:     
0010301     
Arg of perigee:    29
0141  deg
Mean anomaly:     331
1592  deg
Mean motion:   15
72805586  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3614
Checksum:              259


Coasting Arc #5 (Orbit 3629)
---------------------------------------

Vector Time (GMT): 2008/218/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5012860
60                 A    =         6729611
53  meter
 Y    =        2479784
64  meter          E    =           
0018866
 Z    =        3721720
64                 I    =           51
91841
 XDOT =         42
761771                 Wp   =           66
71733
 YDOT =      -6393
655900  meter/sec      RA   =          122
24994  deg
 ZDOT =       4307
882930                 TA   =          338
01757
                                          MA   =          338
09839
                                          Ha   =            195
251  n
mi
                                          Hp   =            182
979

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16446393
05                 X    =        -5058296
61
 Y    =        8135776
39  feet           Y    =         2423473
79  meter
 Z    =       12210369
55                 Z    =         3697258
17
 XDOT =        140
294525                 XDOT =          93
326806
 YDOT =     -20976
561352  feet/sec       YDOT =       -6392
895124  meter/sec
 ZDOT =      14133
474180                 ZDOT =        4308
213287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16310210
56                 X    =         4971352
18
 Y    =        8540761
89  feet           Y    =         2603224
23  meter
 Z    =       12116115
07                 Z    =         3692991
87
 XDOT =     -16353
241354                 XDOT =       -4984
467965
 YDOT =      11132
629263  feet/sec       YDOT =        3393
225399  meter/sec
 ZDOT =      14134
123377                 ZDOT =        4308
080805


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   08218
53486960  
00020000  00000-0  20000-3 0  9043
2 25544  51
6413 122
8270 0010349  32
7943 327
3860 15
72817244 36301


Satellite: ISS
Catalog Number: 25544
Epoch time:      08218
53486960   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       122
8270  deg
Eccentricity:     
0010349     
Arg of perigee:    32
7943  deg
Mean anomaly:     327
3860  deg
Mean motion:   15
72817244  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3630
Checksum:              286


Coasting Arc #6 (Orbit 3644)
---------------------------------------

Vector Time (GMT): 2008/219/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         810858
22                 A    =         6728454
55  meter
 Y    =        5336029
75  meter          E    =           
0014281
 Z    =       -4024252
69                 I    =           51
92992
 XDOT =      -5409
199405                 Wp   =           64
96824
 YDOT =       3785
990115  meter/sec      RA   =          117
09198  deg
 ZDOT =       3946
936558                 TA   =          245
63157
                                          MA   =          245
78070
                                          Ha   =            195
171  n
mi
                                          Hp   =            182
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2660295
99                 X    =          770678
55
 Y    =       17506659
30  feet           Y    =         5344872
73  meter
 Z    =      -13202928
77                 Z    =        -4020410
97
 XDOT =     -17746
717209                 XDOT =       -5470
306277
 YDOT =      12421
227411  feet/sec       YDOT =        3725
159526  meter/sec
 ZDOT =      12949
266923                 ZDOT =        3920
510590

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12307886
75                 X    =         3751443
88
 Y    =      -12746825
12  feet           Y    =        -3885232
30  meter
 Z    =      -13187569
74                 Z    =        -4019571
26
 XDOT =      19729
515807                 XDOT =        6013
556418
 YDOT =       5815
274337  feet/sec       YDOT =        1772
495618  meter/sec
 ZDOT =      12847
547927                 ZDOT =        3915
932608


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   08219
48792146  
00020000  00000-0  20000-3 0  9055
2 25544  51
6418 117
9411 0010343  35
9930 324
1927 15
72843895 36459


Satellite: ISS
Catalog Number: 25544
Epoch time:      08219
48792146   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:       117
9411  deg
Eccentricity:     
0010343     
Arg of perigee:    35
9930  deg
Mean anomaly:     324
1927  deg
Mean motion:   15
72843895  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3645
Checksum:              306


Coasting Arc #7 (Orbit 3660)
---------------------------------------

Vector Time (GMT): 2008/220/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4333152
00                 A    =         6731118
48  meter
 Y    =       -4061982
74  meter          E    =           
0013042
 Z    =       -3184772
02                 I    =           51
95143
 XDOT =       1784
270805                 Wp   =           57
40075
 YDOT =       5694
906191  meter/sec      RA   =          112
03630  deg
 ZDOT =      -4843
300481                 TA   =          159
47564
                                          MA   =          159
42319
                                          Ha   =            195
178  n
mi
                                          Hp   =            182
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14216377
94                 X    =         4393722
65
 Y    =      -13326715
02  feet           Y    =        -4013188
12  meter
 Z    =      -10448727
09                 Z    =        -3163574
75
 XDOT =       5853
906842                 XDOT =        1743
984592
 YDOT =      18684
075429  feet/sec       YDOT =        5714
633920  meter/sec
 ZDOT =     -15890
093440                 ZDOT =       -4834
730114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19296421
22                 X    =        -5881549
19
 Y    =       -3008554
51  feet           Y    =         -917007
41  meter
 Z    =      -10367225
31                 Z    =        -3159930
28
 XDOT =      10813
505450                 XDOT =        3295
956461
 YDOT =     -14801
109944  feet/sec       YDOT =       -4511
378311  meter/sec
 ZDOT =     -15856
437779                 ZDOT =       -4833
042235


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   08220
50450084  
00020000  00000-0  20000-3 0  9063
2 25544  51
6422 112
7291 0010279  39
3801 320
8107 15
72851748 36613


Satellite: ISS
Catalog Number: 25544
Epoch time:      08220
50450084   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       112
7291  deg
Eccentricity:     
0010279     
Arg of perigee:    39
3801  deg
Mean anomaly:     320
8107  deg
Mean motion:   15
72851748  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3661
Checksum:              268


Coasting Arc #8 (Orbit 3676)
---------------------------------------

Vector Time (GMT): 2008/221/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2257626
00                 A    =         6726823
13  meter
 Y    =       -4517836
91  meter          E    =           
0019067
 Z    =        4435944
56                 I    =           51
94684
 XDOT =       4349
212684                 Wp   =           55
03682
 YDOT =      -5434
284469  meter/sec      RA   =          106
88282  deg
 ZDOT =      -3300
497136                 TA   =           68
02832
                                          MA   =           67
82581
                                          Ha   =            195
247  n
mi
                                          Hp   =            182
515

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7406909
44                 X    =        -2228487
95
 Y    =      -14822299
56  feet           Y    =        -4542920
35  meter
 Z    =       14553623
87                 Z    =         4425047
54
 XDOT =      14269
070487                 XDOT =        4425
689624
 YDOT =     -17829
017286  feet/sec       YDOT =       -5385
221252  meter/sec
 ZDOT =     -10828
402678                 ZDOT =       -3279
183348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6780787
41                 X    =        -2066784
00
 Y    =       15159810
00  feet           Y    =         4620710
09  meter
 Z    =       14511096
52                 Z    =         4422982
22
 XDOT =     -21768
778598                 XDOT =       -6635
123717
 YDOT =        614
775652  feet/sec       YDOT =         187
383619  meter/sec
 ZDOT =     -10746
570324                 ZDOT =       -3275
554635


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   08221
52107024  
00020000  00000-0  20000-3 0  9070
2 25544  51
6418 107
5173 0010369  42
7665 317
4303 15
72893930 36771


Satellite: ISS
Catalog Number: 25544
Epoch time:      08221
52107024   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:       107
5173  deg
Eccentricity:     
0010369     
Arg of perigee:    42
7665  deg
Mean anomaly:     317
4303  deg
Mean motion:   15
72893930  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3677
Checksum:              283


Coasting Arc #9 (Orbit 3692)
---------------------------------------

Vector Time (GMT): 2008/222/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3162748
55                 A    =         6732606
48  meter
 Y    =        5349017
04  meter          E    =           
0023406
 Z    =        2557026
92                 I    =           51
97380
 XDOT =      -3302
105977                 Wp   =           63
48980
 YDOT =      -4505
286184  meter/sec      RA   =          101
82343  deg
 ZDOT =       5313
357250                 TA   =          325
39655
                                          MA   =          325
54864
                                          Ha   =            195
365  n
mi
                                          Hp   =            182
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10376471
62                 X    =        -3234748
56
 Y    =       17549268
51  feet           Y    =         5313246
59  meter
 Z    =        8389195
95                 Z    =         2541487
91
 XDOT =     -10833
681027                 XDOT =       -3277
292928
 YDOT =     -14781
122651  feet/sec       YDOT =       -4542
073926  meter/sec
 ZDOT =      17432
274443                 ZDOT =        5297
375602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20139586
64                 X    =         6138546
01
 Y    =       -3322723
50  feet           Y    =        -1012766
12  meter
 Z    =        8329655
22                 Z    =         2538878
91
 XDOT =      -4512
935919                 XDOT =       -1375
542868
 YDOT =      16413
665324  feet/sec       YDOT =        5002
885191  meter/sec
 ZDOT =      17370
106108                 ZDOT =        5294
408342


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   08222
53763135  
00020000  00000-0  20000-3 0  9084
2 25544  51
6423 102
3053 0010405  46
5202 313
6824 15
72868940 36934


Satellite: ISS
Catalog Number: 25544
Epoch time:      08222
53763135   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       102
3053  deg
Eccentricity:     
0010405     
Arg of perigee:    46
5202  deg
Mean anomaly:     313
6824  deg
Mean motion:   15
72868940  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3693
Checksum:              270


Coasting Arc #10 (Orbit 3707)
---------------------------------------

Vector Time (GMT): 2008/223/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3402969
18                 A    =         6725374
58  meter
 Y    =        3271633
49  meter          E    =           
0019102
 Z    =       -4805189
32                 I    =           51
95491
 XDOT =      -2807
036018                 Wp   =           80
88996
 YDOT =       6677
945554  meter/sec      RA   =           96
67763  deg
 ZDOT =       2570
382889                 TA   =          214
17555
                                          MA   =          214
29865
                                          Ha   =            195
266  n
mi
                                          Hp   =            182
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11164597
03                 X    =         3389474
91
 Y    =       10733705
66  feet           Y    =         3309612
44  meter
 Z    =      -15765056
83                 Z    =        -4788690
28
 XDOT =      -9209
435754                 XDOT =       -2893
987618
 YDOT =      21909
270189  feet/sec       YDOT =        6646
069251  meter/sec
 ZDOT =       8433
014729                 ZDOT =        2556
535820

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         699656
43                 X    =          213255
28
 Y    =      -15536622
47  feet           Y    =        -4735562
53  meter
 Z    =      -15701003
92                 Z    =        -4785665
99
 XDOT =      21467
365969                 XDOT =        6543
253147
 YDOT =      -7463
502435  feet/sec       YDOT =       -2274
875542  meter/sec
 ZDOT =       8380
122638                 ZDOT =        2554
261380


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   08223
49064661  
00020000  00000-0  20000-3 0  9099
2 25544  51
6427  97
4194 0010258  49
4939 310
7115 15
72905671 37084


Satellite: ISS
Catalog Number: 25544
Epoch time:      08223
49064661   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:        97
4194  deg
Eccentricity:     
0010258     
Arg of perigee:    49
4939  deg
Mean anomaly:     310
7115  deg
Mean motion:   15
72905671  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3708
Checksum:              305


Coasting Arc #11 (Orbit 3723)
---------------------------------------

Vector Time (GMT): 2008/224/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1702283
08                 A    =         6733709
25  meter
 Y    =       -6219120
46  meter          E    =           
0012521
 Z    =       -1953122
75                 I    =           51
98504
 XDOT =       4324
558092                 Wp   =           87
03940
 YDOT =       2944
178002  meter/sec      RA   =           91
61101  deg
 ZDOT =      -5635
904082                 TA   =          114
55076
                                          MA   =          114
42019
                                          Ha   =            195
276  n
mi
                                          Hp   =            182
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5584918
23                 X    =         1781187
58
 Y    =      -20403938
50  feet           Y    =        -6199643
17  meter
 Z    =       -6407883
03                 Z    =        -1944662
10
 XDOT =      14188
182718                 XDOT =        4318
692356
 YDOT =       9659
376646  feet/sec       YDOT =        2992
505466  meter/sec
 ZDOT =     -18490
498956                 ZDOT =       -5614
909526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18916319
06                 X    =        -5765694
05
 Y    =        9491871
75  feet           Y    =         2893122
51  meter
 Z    =       -6375753
02                 Z    =        -1943329
52
 XDOT =      -1708
847434                 XDOT =        -520
856698
 YDOT =     -15704
123374  feet/sec       YDOT =       -4786
616804  meter/sec
 ZDOT =     -18409
102276                 ZDOT =       -5611
094374


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   08224
50718849  
00020000  00000-0  20000-3 0  9108
2 25544  51
6428  92
2075 0010107  53
5352 306
6741 15
72884076 37246


Satellite: ISS
Catalog Number: 25544
Epoch time:      08224
50718849   =   yrday
fracday
Element set:     910
Inclination:       51
6428  deg
RA of node:        92
2075  deg
Eccentricity:     
0010107     
Arg of perigee:    53
5352  deg
Mean anomaly:     306
6741  deg
Mean motion:   15
72884076  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3724
Checksum:              286


Coasting Arc #12 (Orbit 3739)
---------------------------------------

Vector Time (GMT): 2008/225/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4059806
93                 A    =         6724177
23  meter
 Y    =       -1814358
52  meter          E    =           
0015727
 Z    =        5035195
61                 I    =           51
95334
 XDOT =        997
270090                 Wp   =           55
75164
 YDOT =      -7413
486364  meter/sec      RA   =           86
47392  deg
 ZDOT =      -1854
506546                 TA   =           52
11155
                                          MA   =           51
96943
                                          Ha   =            195
321  n
mi
                                          Hp   =            182
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13319576
54                 X    =        -4063676
50
 Y    =       -5952619
83  feet           Y    =        -1859779
76  meter
 Z    =       16519670
63                 Z    =         5015463
74
 XDOT =       3271
883497                 XDOT =        1089
103501
 YDOT =     -24322
461823  feet/sec       YDOT =       -7401
820663  meter/sec
 ZDOT =      -6084
339061                 ZDOT =       -1849
439555

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4803420
30                 X    =         1464082
51
 Y    =       13866901
31  feet           Y    =         4226631
52  meter
 Z    =       16443251
55                 Z    =         5011903
07
 XDOT =     -19023
446548                 XDOT =       -5798
346508
 YDOT =      13831
777655  feet/sec       YDOT =        4215
925829  meter/sec
 ZDOT =      -6065
424321                 ZDOT =       -1848
741333


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   08225
52371867  
00020000  00000-0  20000-3 0  9117
2 25544  51
6429  86
9954 0010179  56
2875 303
9256 15
72967028 37400


Satellite: ISS
Catalog Number: 25544
Epoch time:      08225
52371867   =   yrday
fracday
Element set:     911
Inclination:       51
6429  deg
RA of node:        86
9954  deg
Eccentricity:     
0010179     
Arg of perigee:    56
2875  deg
Mean anomaly:     303
9256  deg
Mean motion:   15
72967028  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3740
Checksum:              319


Coasting Arc #13 (Orbit 3752)
---------------------------------------

Vector Time (GMT): 2008/226/08:03:52
205
Vector Time (MET): N/A
Weight (LBS)     : 661093
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4217816
81                 A    =         6730240
19  meter
 Y    =         930031
76  meter          E    =           
0014636
 Z    =       -5174207
89                 I    =           51
94823
 XDOT =        -16
462517                 Wp   =           94
37877
 YDOT =       7565
393091  meter/sec      RA   =           82
10413  deg
 ZDOT =       1348
577924                 TA   =          188
48572
                                          MA   =          188
51049
                                          Ha   =            195
584  n
mi
                                          Hp   =            188
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13837981
64                 X    =         4232238
53
 Y    =        3051285
29  feet           Y    =          977278
93  meter
 Z    =      -16975747
67                 Z    =        -5153682
94
 XDOT =        -54
010883                 XDOT =        -107
609771
 YDOT =      24820
843476  feet/sec       YDOT =        7564
699240  meter/sec
 ZDOT =       4424
468253                 ZDOT =        1348
277270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4879624
81                 X    =         1487309
64
 Y    =      -13404442
76  feet           Y    =        -4085674
15  meter
 Z    =      -16896338
73                 Z    =        -5150004
05
 XDOT =      23611
787433                 XDOT =        7196
872810
 YDOT =       3027
960013  feet/sec       YDOT =         922
922212  meter/sec
 ZDOT =       4423
983916                 ZDOT =        1348
430298


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   08226
34965928  
00020000  00000-0  20000-3 0  9126
2 25544  51
6420  82
7609 0001569  28
3220 331
8026 15
70660906 37531


Satellite: ISS
Catalog Number: 25544
Epoch time:      08226
34965928   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:        82
7609  deg
Eccentricity:     
0001569     
Arg of perigee:    28
3220  deg
Mean anomaly:     331
8026  deg
Mean motion:   15
70660906  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3753
Checksum:              289

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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