Date: January 12th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13723 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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


012/00:42:49 251 -0 7 8 2 8 2
N/A 7 9 0 0 183 6
000/00:01:38 502 -1 9 -0 0 180 5

Coasting Arc #1 (Orbit 302)
---------------------------------------

Vector Time (GMT): 2008/007/14:13:36
877
Vector Time (MET): N/A
Weight (LBS)     : 540573
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5300345
98                 A    =         6714282
85  meter
 Y    =       -2258123
40  meter          E    =           
0006294
 Z    =       -3454938
79                 I    =           51
89409
 XDOT =       -356
215465                 Wp   =           73
44550
 YDOT =       6175
026018  meter/sec      RA   =          128
87010  deg
 ZDOT =      -4587
521215                 TA   =          147
36749
                                          MA   =          147
32858
                                          Ha   =            183
670  n
mi
                                          Hp   =            176
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17389586
54                 X    =         5341985
98
 Y    =       -7408541
34  feet           Y    =        -2198618
54  meter
 Z    =      -11335101
02                 Z    =        -3429089
26
 XDOT =      -1168
685910                 XDOT =        -402
954017
 YDOT =      20259
271714  feet/sec       YDOT =        6170
782029  meter/sec
 ZDOT =     -15050
922623                 ZDOT =       -4589
364215

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18051809
91                 X    =         5502191
66
 Y    =        5800020
83  feet           Y    =         1767846
35  meter
 Z    =      -11236575
86                 Z    =        -3424908
32
 XDOT =     -13638
231277                 XDOT =       -4156
932893
 YDOT =      13308
787011  feet/sec       YDOT =        4056
518281  meter/sec
 ZDOT =     -15057
311986                 ZDOT =       -4589
468693


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   08007
61734392  
00020000  00000-0  20000-3 0  9009
2 25544  51
6389 129
6211 0001943  32
7115 327
4171 15
78497908  3031


Satellite: ISS
Catalog Number: 25544
Epoch time:      08007
61734392   =   yrday
fracday
Element set:     900
Inclination:       51
6389  deg
RA of node:       129
6211  deg
Eccentricity:     
0001943     
Arg of perigee:    32
7115  deg
Mean anomaly:     327
4171  deg
Mean motion:   15
78497908  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             303
Checksum:              282


Coasting Arc #2 (Orbit 318)
---------------------------------------

Vector Time (GMT): 2008/008/14:13:36
877
Vector Time (MET): N/A
Weight (LBS)     : 540573
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1279303
71                 A    =         6715651
93  meter
 Y    =       -5941182
99  meter          E    =           
0014605
 Z    =        2844643
18                 I    =           51
91718
 XDOT =       5638
969570                 Wp   =           91
38278
 YDOT =      -1242
815945  meter/sec      RA   =          123
66957  deg
 ZDOT =      -5109
651184                 TA   =           56
02989
                                          MA   =           55
89117
                                          Ha   =            183
638  n
mi
                                          Hp   =            176
273

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4197190
66                 X    =         1331825
33
 Y    =      -19492070
16  feet           Y    =        -5926583
85  meter
 Z    =        9332818
82                 Z    =         2850984
61
 XDOT =      18500
556332                 XDOT =        5677
269158
 YDOT =      -4077
480135  feet/sec       YDOT =       -1179
542873  meter/sec
 ZDOT =     -16763
947454                 ZDOT =       -5082
164699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15666803
82                 X    =         4775241
80
 Y    =      -12315327
89  feet           Y    =        -3753711
94  meter
 Z    =        9356424
16                 Z    =         2851838
08
 XDOT =      15994
209179                 XDOT =        4875
034958
 YDOT =       7635
608007  feet/sec       YDOT =        2327
333321  meter/sec
 ZDOT =     -16659
047490                 ZDOT =       -5077
677675


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   08008
63025534  
00020000  00000-0  20000-3 0  9014
2 25544  51
6392 124
3846 0002194  35
5535 324
5776 15
78569912  3198


Satellite: ISS
Catalog Number: 25544
Epoch time:      08008
63025534   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       124
3846  deg
Eccentricity:     
0002194     
Arg of perigee:    35
5535  deg
Mean anomaly:     324
5776  deg
Mean motion:   15
78569912  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             319
Checksum:              294


Coasting Arc #3 (Orbit 334)
---------------------------------------

Vector Time (GMT): 2008/009/14:13:36
877
Vector Time (MET): N/A
Weight (LBS)     : 540573
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4374854
71                 A    =         6707830
14  meter
 Y    =        -280198
23  meter          E    =           
0005589
 Z    =        5072782
91                 I    =           51
90683
 XDOT =       2395
498159                 Wp   =          103
00794
 YDOT =      -7138
474630  meter/sec      RA   =          118
55603  deg
 ZDOT =       1668
861450                 TA   =          331
01764
                                          MA   =          331
04867
                                          Ha   =            183
663  n
mi
                                          Hp   =            176
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14353197
88                 X    =        -4396038
50
 Y    =        -919285
53  feet           Y    =         -329239
45  meter
 Z    =       16642988
55                 Z    =         5051478
81
 XDOT =       7859
245930                 XDOT =        2467
036777
 YDOT =     -23420
192355  feet/sec       YDOT =       -7111
287036  meter/sec
 ZDOT =       5475
267226                 ZDOT =        1680
671369

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10676163
55                 X    =        -3254094
65
 Y    =       -9776669
46  feet           Y    =        -2979928
85  meter
 Z    =       16561543
08                 Z    =         5047958
33
 XDOT =      20072
569322                 XDOT =        6118
119129
 YDOT =     -12553
713088  feet/sec       YDOT =       -3826
371749  meter/sec
 ZDOT =       5519
646967                 ZDOT =        1682
388396


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   08009
64312841  
00020000  00000-0  20000-3 0  9027
2 25544  51
6396 119
1473 0002166  36
0667 324
0645 15
78643183  3352


Satellite: ISS
Catalog Number: 25544
Epoch time:      08009
64312841   =   yrday
fracday
Element set:     902
Inclination:       51
6396  deg
RA of node:       119
1473  deg
Eccentricity:     
0002166     
Arg of perigee:    36
0667  deg
Mean anomaly:     324
0645  deg
Mean motion:   15
78643183  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             335
Checksum:              281


Coasting Arc #4 (Orbit 350)
---------------------------------------

Vector Time (GMT): 2008/010/14:13:36
877
Vector Time (MET): N/A
Weight (LBS)     : 540573
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2722735
06                 A    =         6719013
96  meter
 Y    =        6134156
56  meter          E    =           
0014936
 Z    =          81068
60                 I    =           51
95692
 XDOT =      -4310
379764                 Wp   =           44
65687
 YDOT =      -2002
175694  meter/sec      RA   =          113
39316  deg
 ZDOT =       6071
607003                 TA   =          316
22190
                                          MA   =          316
34022
                                          Ha   =            183
661  n
mi
                                          Hp   =            176
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8932857
80                 X    =        -2791519
58
 Y    =       20125185
56  feet           Y    =         6103324
79  meter
 Z    =         265973
09                 Z    =           67675
42
 XDOT =     -14141
665894                 XDOT =       -4317
164891
 YDOT =      -6568
817895  feet/sec       YDOT =       -2050
415395  meter/sec
 ZDOT =      19919
970483                 ZDOT =        6050
650943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19404351
34                 X    =        -5914446
29
 Y    =       10407426
28  feet           Y    =         3172183
53  meter
 Z    =         215433
24                 Z    =           65664
05
 XDOT =      -6464
507714                 XDOT =       -1970
381951
 YDOT =     -12518
821775  feet/sec       YDOT =       -3815
736877  meter/sec
 ZDOT =      19839
665628                 ZDOT =        6047
130083


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   08010
65596802  
00020000  00000-0  20000-3 0  9032
2 25544  51
6391 113
9104 0002527  37
8876 322
2467 15
78640346  3510


Satellite: ISS
Catalog Number: 25544
Epoch time:      08010
65596802   =   yrday
fracday
Element set:     903
Inclination:       51
6391  deg
RA of node:       113
9104  deg
Eccentricity:     
0002527     
Arg of perigee:    37
8876  deg
Mean anomaly:     322
2467  deg
Mean motion:   15
78640346  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             351
Checksum:              284


Coasting Arc #5 (Orbit 365)
---------------------------------------

Vector Time (GMT): 2008/011/14:13:36
877
Vector Time (MET): N/A
Weight (LBS)     : 540573
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3086794
27                 A    =         6707816
23  meter
 Y    =        3213783
20  meter          E    =           
0014632
 Z    =       -5026578
12                 I    =           51
92969
 XDOT =      -3690
455572                 Wp   =           95
11297
 YDOT =       6487
110894  meter/sec      RA   =          108
22720  deg
 ZDOT =       1884
685670                 TA   =          192
98785
                                          MA   =          193
02557
                                          Ha   =            183
575  n
mi
                                          Hp   =            175
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10127277
79                 X    =         3075045
52
 Y    =       10543908
13  feet           Y    =         3248236
21  meter
 Z    =      -16491398
04                 Z    =        -5011611
07
 XDOT =     -12107
793871                 XDOT =       -3771
876423
 YDOT =      21283
172225  feet/sec       YDOT =        6445
386723  meter/sec
 ZDOT =       6183
351936                 ZDOT =        1866
560580

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1850015
54                 X    =          563884
74
 Y    =       14567359
65  feet           Y    =         4440131
22  meter
 Z    =      -16433850
40                 Z    =        -5009037
60
 XDOT =     -21421
671371                 XDOT =       -6529
325434
 YDOT =       9606
146065  feet/sec       YDOT =        2927
953321  meter/sec
 ZDOT =       6114
760351                 ZDOT =        1863
778955


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   08011
60546776  
00020000  00000-0  20000-3 0  9044
2 25544  51
6385 109
0002 0002566  41
3491 318
7868 15
78724614  3664


Satellite: ISS
Catalog Number: 25544
Epoch time:      08011
60546776   =   yrday
fracday
Element set:     904
Inclination:       51
6385  deg
RA of node:       109
0002  deg
Eccentricity:     
0002566     
Arg of perigee:    41
3491  deg
Mean anomaly:     318
7868  deg
Mean motion:   15
78724614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             366
Checksum:              290


Coasting Arc #6 (Orbit 372)
---------------------------------------

Vector Time (GMT): 2008/012/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4304865
86                 A    =         6711534
44  meter
 Y    =        -402968
35  meter          E    =           
0009920
 Z    =       -5141952
90                 I    =           51
93335
 XDOT =       -994
460023                 Wp   =           72
88464
 YDOT =       7501
206976  meter/sec      RA   =          106
00198  deg
 ZDOT =      -1419
805404                 TA   =          183
56491
                                          MA   =          183
57199
                                          Ha   =            183
567  n
mi
                                          Hp   =            180
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14123575
64                 X    =         4334030
13
 Y    =       -1322074
64  feet           Y    =         -354665
46  meter
 Z    =      -16869924
23                 Z    =        -5120969
48
 XDOT =      -3262
664117                 XDOT =       -1071
368740
 YDOT =      24610
259108  feet/sec       YDOT =        7489
656442  meter/sec
 ZDOT =      -4658
154213                 ZDOT =       -1424
822666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8470152
46                 X    =        -2581702
47
 Y    =      -11496870
81  feet           Y    =        -3504246
22  meter
 Z    =      -16789761
54                 Z    =        -5117519
32
 XDOT =      21911
732474                 XDOT =        6678
696058
 YDOT =      -9310
654196  feet/sec       YDOT =       -2837
887399  meter/sec
 ZDOT =      -4676
537643                 ZDOT =       -1425
408674


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   08012
04856374  
00020000  00000-0  20000-3 0  9052
2 25544  51
6400 106
7096 0004301 273
9744  86
0929 15
77246677  3730


Satellite: ISS
Catalog Number: 25544
Epoch time:      08012
04856374   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       106
7096  deg
Eccentricity:     
0004301     
Arg of perigee:   273
9744  deg
Mean anomaly:      86
0929  deg
Mean motion:   15
77246677  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             373
Checksum:              294


Coasting Arc #7 (Orbit 388)
---------------------------------------

Vector Time (GMT): 2008/013/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1151129
83                 A    =         6722941
65  meter
 Y    =       -6616389
91  meter          E    =           
0009462
 Z    =         147022
12                 I    =           51
97848
 XDOT =       4701
025662                 Wp   =          149
16092
 YDOT =        679
431107  meter/sec      RA   =          100
85041  deg
 ZDOT =      -6068
471520                 TA   =           29
24704
                                          MA   =           29
19410
                                          Ha   =            183
588  n
mi
                                          Hp   =            180
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3776672
68                 X    =         1224315
57
 Y    =      -21707315
97  feet           Y    =        -6603108
12  meter
 Z    =         482356
05                 Z    =          152791
63
 XDOT =      15423
312539                 XDOT =        4722
557808
 YDOT =       2229
104682  feet/sec       YDOT =         732
121361  meter/sec
 ZDOT =     -19909
683466                 ZDOT =       -6045
581987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20400887
98                 X    =        -6218190
66
 Y    =        8321870
93  feet           Y    =         2536506
26  meter
 Z    =         503710
52                 Z    =          153530
97
 XDOT =      -5748
925119                 XDOT =       -1752
272376
 YDOT =     -12862
636562  feet/sec       YDOT =       -3920
531624  meter/sec
 ZDOT =     -19822
116790                 ZDOT =       -6041
781198


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   08013
06230092  
00020000  00000-0  20000-3 0  9069
2 25544  51
6398 101
4781 0004322 276
8716  83
1957 15
77248370  3891


Satellite: ISS
Catalog Number: 25544
Epoch time:      08013
06230092   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       101
4781  deg
Eccentricity:     
0004322     
Arg of perigee:   276
8716  deg
Mean anomaly:      83
1957  deg
Mean motion:   15
77248370  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             389
Checksum:              292


Coasting Arc #8 (Orbit 404)
---------------------------------------

Vector Time (GMT): 2008/014/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3927129
02                 A    =         6710907
71  meter
 Y    =       -1619041
42  meter          E    =           
0003376
 Z    =        5196956
75                 I    =           51
94325
 XDOT =       1611
385382                 Wp   =          339
35083
 YDOT =      -7454
185166  meter/sec      RA   =           95
70421  deg
 ZDOT =      -1101
715110                 TA   =          121
12760
                                          MA   =          121
09448
                                          Ha   =            183
568  n
mi
                                          Hp   =            180
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12884281
55                 X    =        -3933978
34
 Y    =       -5311815
68  feet           Y    =        -1662995
34  meter
 Z    =       17050383
05                 Z    =         5177862
28
 XDOT =       5286
697447                 XDOT =        1699
971327
 YDOT =     -24455
988079  feet/sec       YDOT =       -7435
670380  meter/sec
 ZDOT =      -3614
550887                 ZDOT =       -1093
672259

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2624329
56                 X    =          799895
65
 Y    =       13777607
64  feet           Y    =         4199414
81  meter
 Z    =       16977222
42                 Z    =         5174657
39
 XDOT =     -22390
154912                 XDOT =       -6824
519217
 YDOT =       8693
559691  feet/sec       YDOT =        2649
796994  meter/sec
 ZDOT =      -3584
590114                 ZDOT =       -1092
583067


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   08014
07600152  
00020000  00000-0  20000-3 0  9070
2 25544  51
6398  96
2463 0004466 283
7440  76
3228 15
77369460  4057


Satellite: ISS
Catalog Number: 25544
Epoch time:      08014
07600152   =   yrday
fracday
Element set:     907
Inclination:       51
6398  deg
RA of node:        96
2463  deg
Eccentricity:     
0004466     
Arg of perigee:   283
7440  deg
Mean anomaly:      76
3228  deg
Mean motion:   15
77369460  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             405
Checksum:              289


Coasting Arc #9 (Orbit 420)
---------------------------------------

Vector Time (GMT): 2008/015/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1659127
59                 A    =         6720807
61  meter
 Y    =        6178063
42  meter          E    =           
0011174
 Z    =        2040046
02                 I    =           51
97828
 XDOT =      -4348
702939                 Wp   =           53
93043
 YDOT =      -3022
342146  meter/sec      RA   =           90
59294  deg
 ZDOT =       5601
441325                 TA   =          328
75571
                                          MA   =          328
82208
                                          Ha   =            183
655  n
mi
                                          Hp   =            180
134

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5443331
99                 X    =        -1737998
43
 Y    =       20269236
94  feet           Y    =         6159069
02  meter
 Z    =        6693064
36                 Z    =         2031794
77
 XDOT =     -14267
398095                 XDOT =       -4341
794026
 YDOT =      -9915
820689  feet/sec       YDOT =       -3070
933467  meter/sec
 ZDOT =      18377
432170                 ZDOT =        5580
332114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19865980
82                 X    =         6055150
95
 Y    =       -6799065
53  feet           Y    =        -2072355
17  meter
 Z    =        6662165
87                 Z    =         2030628
16
 XDOT =       -672
505661                 XDOT =        -204
979726
 YDOT =      16010
497286  feet/sec       YDOT =        4879
999573  meter/sec
 ZDOT =      18296
423264                 ZDOT =        5576
749811


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   08015
08967222  
00020000  00000-0  20000-3 0  9087
2 25544  51
6398  91
0138 0004403 289
9594  70
1097 15
77371785  4215


Satellite: ISS
Catalog Number: 25544
Epoch time:      08015
08967222   =   yrday
fracday
Element set:     908
Inclination:       51
6398  deg
RA of node:        91
0138  deg
Eccentricity:     
0004403     
Arg of perigee:   289
9594  deg
Mean anomaly:      70
1097  deg
Mean motion:   15
77371785  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             421
Checksum:              304


Coasting Arc #10 (Orbit 435)
---------------------------------------

Vector Time (GMT): 2008/016/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3682612
22                 A    =         6714325
01  meter
 Y    =        3585664
80  meter          E    =           
0004298
 Z    =       -4324411
54                 I    =           51
95612
 XDOT =      -2221
777235                 Wp   =          107
85830
 YDOT =       6493
992561  meter/sec      RA   =           85
41115  deg
 ZDOT =       3494
106379                 TA   =          197
30889
                                          MA   =          197
32355
                                          Ha   =            183
637  n
mi
                                          Hp   =            180
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12082061
08                 X    =         3663250
19
 Y    =       11763992
13  feet           Y    =         3626737
90  meter
 Z    =      -14187701
91                 Z    =        -4306568
27
 XDOT =      -7289
295389                 XDOT =       -2311
202591
 YDOT =      21305
749872  feet/sec       YDOT =        6468
647143  meter/sec
 ZDOT =      11463
603607                 ZDOT =        3483
096262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2657465
46                 X    =          809995
47
 Y    =      -16710681
45  feet           Y    =        -5093415
71  meter
 Z    =      -14119121
76                 Z    =        -4303508
31
 XDOT =      20451
029542                 XDOT =        6233
473804
 YDOT =      -6394
235659  feet/sec       YDOT =       -1948
963029  meter/sec
 ZDOT =      11422
181326                 ZDOT =        3481
480868


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   08016
03995597  
00020000  00000-0  20000-3 0  9090
2 25544  51
6399  86
1087 0004504 293
3511  66
7180 15
77437967  4369


Satellite: ISS
Catalog Number: 25544
Epoch time:      08016
03995597   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:        86
1087  deg
Eccentricity:     
0004504     
Arg of perigee:   293
3511  deg
Mean anomaly:      66
7180  deg
Mean motion:   15
77437967  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             436
Checksum:              321


Coasting Arc #11 (Orbit 451)
---------------------------------------

Vector Time (GMT): 2008/017/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2268628
39                 A    =         6715646
91  meter
 Y    =       -4959782
90  meter          E    =           
0004691
 Z    =       -3923534
87                 I    =           51
95716
 XDOT =       4098
246137                 Wp   =           30
25368
 YDOT =       5094
440918  meter/sec      RA   =           80
32209  deg
 ZDOT =      -4068
417921                 TA   =          197
60657
                                          MA   =          197
62283
                                          Ha   =            183
628  n
mi
                                          Hp   =            180
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7443006
53                 X    =         2342980
59
 Y    =      -16272253
61  feet           Y    =        -4933997
71  meter
 Z    =      -12872489
74                 Z    =        -3912333
78
 XDOT =      13445
689427                 XDOT =        4060
738300
 YDOT =      16714
045008  feet/sec       YDOT =        5140
060505  meter/sec
 ZDOT =     -13347
827825                 ZDOT =       -4048
599328

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17582383
70                 X    =        -5359110
55
 Y    =        3483117
07  feet           Y    =         1061654
08  meter
 Z    =      -12830169
71                 Z    =        -3910635
73
 XDOT =       5829
834895                 XDOT =        1776
933676
 YDOT =     -19480
493345  feet/sec       YDOT =       -5937
654372  meter/sec
 ZDOT =     -13271
545776                 ZDOT =       -4045
167152


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   08017
05356072  
00020000  00000-0  20000-3 0  9104
2 25544  51
6398  80
8764 0004579 297
0990  62
9707 15
77470391  4524


Satellite: ISS
Catalog Number: 25544
Epoch time:      08017
05356072   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:        80
8764  deg
Eccentricity:     
0004579     
Arg of perigee:   297
0990  deg
Mean anomaly:      62
9707  deg
Mean motion:   15
77470391  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             452
Checksum:              310


Coasting Arc #12 (Orbit 467)
---------------------------------------

Vector Time (GMT): 2008/018/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3457010
76                 A    =         6719226
27  meter
 Y    =       -5145143
27  meter          E    =           
0009744
 Z    =        2583815
98                 I    =           51
96419
 XDOT =       3035
486852                 Wp   =           94
15283
 YDOT =      -4706
167582  meter/sec      RA   =           75
13434  deg
 ZDOT =      -5293
765381                 TA   =           56
60579
                                          MA   =           56
51260
                                          Ha   =            183
739  n
mi
                                          Hp   =            179
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11341898
82                 X    =        -3411771
69
 Y    =      -16880391
30  feet           Y    =        -5183548
90  meter
 Z    =        8477086
54                 Z    =         2567131
16
 XDOT =       9958
946364                 XDOT =        3113
602349
 YDOT =     -15440
182357  feet/sec       YDOT =       -4671
785630  meter/sec
 ZDOT =     -17367
996658                 ZDOT =       -5278
829898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6632870
99                 X    =        -2021699
08
 Y    =       19252983
31  feet           Y    =         5868309
31  meter
 Z    =        8412783
81                 Z    =         2564216
50
 XDOT =     -16980
019215                 XDOT =       -5175
509857
 YDOT =       1738
090310  feet/sec       YDOT =         529
769927  meter/sec
 ZDOT =     -17311
362873                 ZDOT =       -5276
503404


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   08018
06713281  
00020000  00000-0  20000-3 0  9116
2 25544  51
6402  75
6440 0004468 303
8144  56
2595 15
77550101  4683


Satellite: ISS
Catalog Number: 25544
Epoch time:      08018
06713281   =   yrday
fracday
Element set:     911
Inclination:       51
6402  deg
RA of node:        75
6440  deg
Eccentricity:     
0004468     
Arg of perigee:   303
8144  deg
Mean anomaly:      56
2595  deg
Mean motion:   15
77550101  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             468
Checksum:              271


Coasting Arc #13 (Orbit 483)
---------------------------------------

Vector Time (GMT): 2008/019/00:43:38
502
Vector Time (MET): N/A
Weight (LBS)     : 540063
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3090245
01                 A    =         6710892
40  meter
 Y    =        3125755
85  meter          E    =           
0000716
 Z    =        5070611
23                 I    =           51
92706
 XDOT =      -3779
571825                 Wp   =          112
66447
 YDOT =      -6497
833412  meter/sec      RA   =           70
02894  deg
 ZDOT =       1701
670583                 TA   =          321
04521
                                          MA   =          321
05037
                                          Ha   =            183
936  n
mi
                                          Hp   =            179
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10138599
11                 X    =        -3149599
87
 Y    =       10255104
48  feet           Y    =         3090866
38  meter
 Z    =       16635863
63                 Z    =         5055455
25
 XDOT =     -12400
170029                 XDOT =       -3714
897474
 YDOT =     -21318
351089  feet/sec       YDOT =       -6539
737361  meter/sec
 ZDOT =       5582
908736                 ZDOT =        1683
465772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14379947
79                 X    =         4383008
08
 Y    =        1757848
52  feet           Y    =          535792
23  meter
 Z    =       16578220
31                 Z    =         5053041
55
 XDOT =      -9030
255476                 XDOT =       -2752
421869
 YDOT =      21867
302781  feet/sec       YDOT =        6665
153888  meter/sec
 ZDOT =       5512
662880                 ZDOT =        1680
259646


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   08019
08067253  
00020000  00000-0  20000-3 0  9121
2 25544  51
6398  70
4108 0004441 307
8171  52
2591 15
77564015  4845


Satellite: ISS
Catalog Number: 25544
Epoch time:      08019
08067253   =   yrday
fracday
Element set:     912
Inclination:       51
6398  deg
RA of node:        70
4108  deg
Eccentricity:     
0004441     
Arg of perigee:   307
8171  deg
Mean anomaly:      52
2591  deg
Mean motion:   15
77564015  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             484
Checksum:              278

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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