Date: May 7th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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


There are no maneuvers



Coasting Arc #1 (Orbit 2179)
---------------------------------------

Vector Time (GMT): 2008/126/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4999957
56                 A    =         6723743
27  meter
 Y    =       -3780042
28  meter          E    =           
0005186
 Z    =       -2441663
59                 I    =           51
38541
 XDOT =       1455
177335                 Wp   =          124
03607
 YDOT =      -5361
573634  meter/sec      RA   =          235
21714  deg
 ZDOT =       5325
826284                 TA   =          208
28339
                                          MA   =          208
31156
                                          Ha   =            188
204  n
mi
                                          Hp   =            180
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16404060
23                 X    =        -4945455
45
 Y    =      -12401713
52  feet           Y    =        -3835649
74  meter
 Z    =       -8010707
33                 Z    =        -2465821
92
 XDOT =       4774
203855                 XDOT =        1489
150564
 YDOT =     -17590
464680  feet/sec       YDOT =       -5345
111463  meter/sec
 ZDOT =      17473
183345                 ZDOT =        5332
977832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18666565
10                 X    =        -5689569
04
 Y    =        8541341
08  feet           Y    =         2603400
76  meter
 Z    =       -8103823
93                 Z    =        -2470045
53
 XDOT =     -12660
736680                 XDOT =       -3858
992540
 YDOT =     -11081
628998  feet/sec       YDOT =       -3377
680519  meter/sec
 ZDOT =      17500
068539                 ZDOT =        5334
020891


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   08126
55693765  
00020000  00000-0  20000-3 0  9002
2 25544  51
6419 236
1081 0006454 177
5338 182
5859 15
76029830 21802


Satellite: ISS
Catalog Number: 25544
Epoch time:      08126
55693765   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:       236
1081  deg
Eccentricity:     
0006454     
Arg of perigee:   177
5338  deg
Mean anomaly:     182
5859  deg
Mean motion:   15
76029830  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2180
Checksum:              306


Coasting Arc #2 (Orbit 2195)
---------------------------------------

Vector Time (GMT): 2008/127/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1566872
83                 A    =         6715610
35  meter
 Y    =        4280259
51  meter          E    =           
0012605
 Z    =       -4941421
17                 I    =           51
37530
 XDOT =      -5895
761700                 Wp   =          104
49130
 YDOT =      -4506
076073  meter/sec      RA   =          230
08612  deg
 ZDOT =      -2041
123541                 TA   =          145
70471
                                          MA   =          145
62326
                                          Ha   =            188
013  n
mi
                                          Hp   =            180
190

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5140658
90                 X    =        -1590613
83
 Y    =       14042846
16  feet           Y    =         4262605
65  meter
 Z    =      -16212011
73                 Z    =        -4949090
41
 XDOT =     -19343
050196                 XDOT =       -5835
020227
 YDOT =     -14783
714151  feet/sec       YDOT =       -4571
666000  meter/sec
 ZDOT =      -6696
599545                 ZDOT =       -2069
618767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10170905
15                 X    =         3100091
89
 Y    =       10919694
38  feet           Y    =         3328322
85  meter
 Z    =      -16241003
34                 Z    =        -4950257
82
 XDOT =     -21187
590790                 XDOT =       -6457
977673
 YDOT =       9647
652397  feet/sec       YDOT =        2940
604451  meter/sec
 ZDOT =      -6806
445900                 ZDOT =       -2074
604710


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   08127
57143121  
00020000  00000-0  20000-3 0  9012
2 25544  51
6412 230
8827 0006494 181
4056 178
7091 15
76075111 21964


Satellite: ISS
Catalog Number: 25544
Epoch time:      08127
57143121   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       230
8827  deg
Eccentricity:     
0006494     
Arg of perigee:   181
4056  deg
Mean anomaly:     178
7091  deg
Mean motion:   15
76075111  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2196
Checksum:              278


Coasting Arc #3 (Orbit 2211)
---------------------------------------

Vector Time (GMT): 2008/128/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5266068
59                 A    =         6725604
53  meter
 Y    =        4021891
30  meter          E    =           
0017840
 Z    =        1087477
91                 I    =           51
42866
 XDOT =      -2182
965298                 Wp   =          141
29406
 YDOT =       4463
007692  meter/sec      RA   =          224
89067  deg
 ZDOT =      -5896
742349                 TA   =           26
75103
                                          MA   =           26
65912
                                          Ha   =            187
823  n
mi
                                          Hp   =            180
261

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17277127
91                 X    =         5215420
92
 Y    =       13195181
42  feet           Y    =         4080496
15  meter
 Z    =        3567840
91                 Z    =         1112938
42
 XDOT =      -7161
959640                 XDOT =       -2204
063319
 YDOT =      14642
413687  feet/sec       YDOT =        4438
479354  meter/sec
 ZDOT =     -19346
267549                 ZDOT =       -5907
398022

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19470857
87                 X    =         5934717
48
 Y    =       -9632631
58  feet           Y    =        -2936026
11  meter
 Z    =        3665999
56                 Z    =         1117396
67
 XDOT =       9305
568158                 XDOT =        2836
337175
 YDOT =      11385
145925  feet/sec       YDOT =        3470
192478  meter/sec
 ZDOT =     -19386
710306                 ZDOT =       -5909
069301


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   08128
58590121  
00020000  00000-0  20000-3 0  9021
2 25544  51
6406 225
6572 0006357 183
7606 176
3511 15
76123944 22128


Satellite: ISS
Catalog Number: 25544
Epoch time:      08128
58590121   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       225
6572  deg
Eccentricity:     
0006357     
Arg of perigee:   183
7606  deg
Mean anomaly:     176
3511  deg
Mean motion:   15
76123944  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2212
Checksum:              281


Coasting Arc #4 (Orbit 2227)
---------------------------------------

Vector Time (GMT): 2008/129/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2298711
61                 A    =         6713928
07  meter
 Y    =       -3520092
01  meter          E    =           
0007302
 Z    =        5233836
41                 I    =           51
41159
 XDOT =       6129
316315                 Wp   =          168
35629
 YDOT =       4650
627855  meter/sec      RA   =          219
73766  deg
 ZDOT =        428
683552                 TA   =          277
52097
                                          MA   =          277
60393
                                          Ha   =            187
546  n
mi
                                          Hp   =            180
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7541704
74                 X    =         2312477
70
 Y    =      -11548858
30  feet           Y    =        -3494310
27  meter
 Z    =       17171379
29                 Z    =         5245036
61
 XDOT =      20109
305494                 XDOT =        6074
774231
 YDOT =      15257
965402  feet/sec       YDOT =        4718
864352  meter/sec
 ZDOT =       1406
442100                 ZDOT =         458
328241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7262187
00                 X    =        -2213514
60
 Y    =      -11663961
10  feet           Y    =        -3555175
34  meter
 Z    =       17214016
29                 Z    =         5246832
16
 XDOT =      21531
906006                 XDOT =        6562
924951
 YDOT =     -11127
223907  feet/sec       YDOT =       -3391
577847  meter/sec
 ZDOT =       1520
745404                 ZDOT =         463
523199


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   08129
60034541  
00020000  00000-0  20000-3 0  9035
2 25544  51
6406 220
4308 0006277 189
3410 170
7639 15
76192120 22282


Satellite: ISS
Catalog Number: 25544
Epoch time:      08129
60034541   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:       220
4308  deg
Eccentricity:     
0006277     
Arg of perigee:   189
3410  deg
Mean anomaly:     170
7639  deg
Mean motion:   15
76192120  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2228
Checksum:              269


Coasting Arc #5 (Orbit 2243)
---------------------------------------

Vector Time (GMT): 2008/130/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5358034
83                 A    =         6725971
65  meter
 Y    =       -4045642
17  meter          E    =           
0008851
 Z    =         365438
69                 I    =           51
47437
 XDOT =       3160
689918                 Wp   =           72
49504
 YDOT =      -3632
627656  meter/sec      RA   =          214
57129  deg
 ZDOT =       6009
616065                 TA   =          291
48864
                                          MA   =          291
58299
                                          Ha   =            187
465  n
mi
                                          Hp   =            180
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17578854
44                 X    =        -5314172
85
 Y    =      -13273104
25  feet           Y    =        -4105313
59  meter
 Z    =        1198945
82                 Z    =          339515
25
 XDOT =      10369
717580                 XDOT =        3171
881872
 YDOT =     -11918
069737  feet/sec       YDOT =       -3597
221223  meter/sec
 ZDOT =      19716
588141                 ZDOT =        6024
997474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19334337
96                 X    =        -5893106
21
 Y    =       10564303
86  feet           Y    =         3219999
82  meter
 Z    =        1098976
94                 Z    =          334968
17
 XDOT =      -5869
952607                 XDOT =       -1789
161555
 YDOT =     -12843
541010  feet/sec       YDOT =       -3914
711300  meter/sec
 ZDOT =      19775
273362                 ZDOT =        6027
503321


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   08130
61477042  
00020000  00000-0  20000-3 0  9046
2 25544  51
6397 215
2046 0005951 192
1704 167
9317 15
76167599 22449


Satellite: ISS
Catalog Number: 25544
Epoch time:      08130
61477042   =   yrday
fracday
Element set:     904
Inclination:       51
6397  deg
RA of node:       215
2046  deg
Eccentricity:     
0005951     
Arg of perigee:   192
1704  deg
Mean anomaly:     167
9317  deg
Mean motion:   15
76167599  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2244
Checksum:              297


Coasting Arc #6 (Orbit 2258)
---------------------------------------

Vector Time (GMT): 2008/131/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3263026
84                 A    =         6714314
40  meter
 Y    =        2858496
37  meter          E    =           
0014783
 Z    =       -5136933
14                 I    =           51
45976
 XDOT =      -6046
361078                 Wp   =          123
46879
 YDOT =      -4581
513422  meter/sec      RA   =          209
39209  deg
 ZDOT =       1285
909073                 TA   =          158
89914
                                          MA   =          158
83809
                                          Ha   =            187
230  n
mi
                                          Hp   =            180
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10705468
63                 X    =        -3269794
17
 Y    =        9378268
91  feet           Y    =         2821970
07  meter
 Z    =      -16853455
17                 Z    =        -5152801
05
 XDOT =     -19837
142644                 XDOT =       -6000
927214
 YDOT =     -15031
212013  feet/sec       YDOT =       -4648
873397  meter/sec
 ZDOT =       4218
861789                 ZDOT =        1256
645679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4412811
55                 X    =         1345024
96
 Y    =       13455052
12  feet           Y    =         4101099
89  meter
 Z    =      -16914094
84                 Z    =        -5155416
11
 XDOT =     -20683
779624                 XDOT =       -6304
416030
 YDOT =      11967
218274  feet/sec       YDOT =        3647
608130  meter/sec
 ZDOT =       4105
993424                 ZDOT =        1251
506796


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   08131
56576962  
00020000  00000-0  20000-3 0  9053
2 25544  51
6390 210
3044 0005938 196
3418 163
7556 15
76216501 22592


Satellite: ISS
Catalog Number: 25544
Epoch time:      08131
56576962   =   yrday
fracday
Element set:     905
Inclination:       51
6390  deg
RA of node:       210
3044  deg
Eccentricity:     
0005938     
Arg of perigee:   196
3418  deg
Mean anomaly:     163
7556  deg
Mean motion:   15
76216501  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2259
Checksum:              297


Coasting Arc #7 (Orbit 2274)
---------------------------------------

Vector Time (GMT): 2008/132/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5118010
90                 A    =         6724238
57  meter
 Y    =        3931717
16  meter          E    =           
0011520
 Z    =       -1864471
74                 I    =           51
52031
 XDOT =      -4329
399545                 Wp   =          167
09349
 YDOT =       2968
368547  meter/sec      RA   =          204
25673  deg
 ZDOT =      -5642
436639                 TA   =           33
67163
                                          MA   =           33
59849
                                          Ha   =            187
093  n
mi
                                          Hp   =            180
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16791374
34                 X    =         5082722
70
 Y    =       12899334
53  feet           Y    =         3988752
55  meter
 Z    =       -6117033
28                 Z    =        -1839693
83
 XDOT =     -14204
066749                 XDOT =       -4334
860615
 YDOT =       9738
741952  feet/sec       YDOT =        2919
924689  meter/sec
 ZDOT =     -18511
931231                 ZDOT =       -5663
481857

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18325181
41                 X    =         5585515
29
 Y    =      -10662602
58  feet           Y    =        -3249961
27  meter
 Z    =       -6021446
02                 Z    =        -1835336
75
 XDOT =       2873
760353                 XDOT =         875
922156
 YDOT =      15405
246165  feet/sec       YDOT =        4695
519031  meter/sec
 ZDOT =     -18592
448587                 ZDOT =       -5666
978329


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   08132
58014862  
00020000  00000-0  20000-3 0  9063
2 25544  51
6395 205
0775 0005811 198
8396 161
2554 15
76276284 22754


Satellite: ISS
Catalog Number: 25544
Epoch time:      08132
58014862   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:       205
0775  deg
Eccentricity:     
0005811     
Arg of perigee:   198
8396  deg
Mean anomaly:     161
2554  deg
Mean motion:   15
76276284  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2275
Checksum:              309


Coasting Arc #8 (Orbit 2290)
---------------------------------------

Vector Time (GMT): 2008/133/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4281902
17                 A    =         6716246
01  meter
 Y    =       -2380106
55  meter          E    =           
0005311
 Z    =        4589259
44                 I    =           51
52114
 XDOT =       5600
136125                 Wp   =          108
42151
 YDOT =       4405
862633  meter/sec      RA   =          199
05624  deg
 ZDOT =      -2938
970439                 TA   =           10
73231
                                          MA   =           10
72098
                                          Ha   =            186
693  n
mi
                                          Hp   =            180
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14048235
45                 X    =         4285904
84
 Y    =       -7808748
53  feet           Y    =        -2332201
80  meter
 Z    =       15056625
45                 Z    =         4610070
50
 XDOT =      18373
150018                 XDOT =        5564
729860
 YDOT =      14454
929898  feet/sec       YDOT =        4468
288791  meter/sec
 ZDOT =      -9642
291467                 ZDOT =       -2911
850661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2190710
42                 X    =         -667728
54
 Y    =      -15846902
45  feet           Y    =        -4830135
87  meter
 Z    =       15136311
09                 Z    =         4613547
62
 XDOT =      19015
417581                 XDOT =        5795
899279
 YDOT =     -11742
175505  feet/sec       YDOT =       -3579
015094  meter/sec
 ZDOT =      -9537
646371                 ZDOT =       -2907
074614


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   08133
59450390  
00020000  00000-0  20000-3 0  9076
2 25544  51
6393 199
8507 0005751 204
3561 155
7332 15
76334272 22917


Satellite: ISS
Catalog Number: 25544
Epoch time:      08133
59450390   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       199
8507  deg
Eccentricity:     
0005751     
Arg of perigee:   204
3561  deg
Mean anomaly:     155
7332  deg
Mean motion:   15
76334272  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2291
Checksum:              295


Coasting Arc #9 (Orbit 2306)
---------------------------------------

Vector Time (GMT): 2008/134/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4547804
16                 A    =         6721140
04  meter
 Y    =       -3758306
31  meter          E    =           
0011362
 Z    =        3215461
50                 I    =           51
56513
 XDOT =       5486
746559                 Wp   =          112
38559
 YDOT =      -2540
592110  meter/sec      RA   =          193
94318  deg
 ZDOT =       4773
066407                 TA   =          285
27148
                                          MA   =          285
39705
                                          Ha   =            186
745  n
mi
                                          Hp   =            180
893

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14920617
31                 X    =        -4521060
37
 Y    =      -12330401
30  feet           Y    =        -3809013
10  meter
 Z    =       10549414
35                 Z    =         3193432
94
 XDOT =      18001
137005                 XDOT =        5491
561289
 YDOT =      -8335
275953  feet/sec       YDOT =       -2479
209504  meter/sec
 ZDOT =      15659
666691                 ZDOT =        4799
732685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16772073
95                 X    =        -5112128
14
 Y    =        9754378
29  feet           Y    =         2973134
50  meter
 Z    =       10464387
22                 Z    =         3189545
23
 XDOT =       -871
202617                 XDOT =        -265
542558
 YDOT =     -18469
681495  feet/sec       YDOT =       -5629
558920  meter/sec
 ZDOT =      15761
832544                 ZDOT =        4804
206559


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   08134
60884050  
00020000  00000-0  20000-3 0  9084
2 25544  51
6390 194
6231 0005546 205
8018 154
2870 15
76325608 23078


Satellite: ISS
Catalog Number: 25544
Epoch time:      08134
60884050   =   yrday
fracday
Element set:     908
Inclination:       51
6390  deg
RA of node:       194
6231  deg
Eccentricity:     
0005546     
Arg of perigee:   205
8018  deg
Mean anomaly:     154
2870  deg
Mean motion:   15
76325608  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2307
Checksum:              284


Coasting Arc #10 (Orbit 2321)
---------------------------------------

Vector Time (GMT): 2008/135/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5255463
81                 A    =         6719552
38  meter
 Y    =        2103166
35  meter          E    =           
0006512
 Z    =       -3628387
43                 I    =           51
59045
 XDOT =      -4714
059254                 Wp   =          154
22295
 YDOT =      -4231
564104  meter/sec      RA   =          188
73403  deg
 ZDOT =       4372
356922                 TA   =          162
25163
                                          MA   =          162
22887
                                          Ha   =            186
474  n
mi
                                          Hp   =            180
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17242335
33                 X    =        -5260964
95
 Y    =        6900152
08  feet           Y    =         2044366
17  meter
 Z    =      -11904158
23                 Z    =        -3653931
94
 XDOT =     -15466
073667                 XDOT =       -4687
631171
 YDOT =     -13883
084331  feet/sec       YDOT =       -4284
131854  meter/sec
 ZDOT =      14345
003026                 ZDOT =        4349
519828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         811806
36                 X    =          247438
58
 Y    =       18490823
34  feet           Y    =         5636002
95  meter
 Z    =      -12002067
83                 Z    =        -3658230
28
 XDOT =     -16906
291360                 XDOT =       -5153
037607
 YDOT =      10002
070584  feet/sec       YDOT =        3048
631114  meter/sec
 ZDOT =      14256
812944                 ZDOT =        4345
476585


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   08135
55975955  
00020000  00000-0  20000-3 0  9095
2 25544  51
6400 189
7226 0005499 209
5596 150
5259 15
76390300 23226


Satellite: ISS
Catalog Number: 25544
Epoch time:      08135
55975955   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       189
7226  deg
Eccentricity:     
0005499     
Arg of perigee:   209
5596  deg
Mean anomaly:     150
5259  deg
Mean motion:   15
76390300  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2322
Checksum:              313


Coasting Arc #11 (Orbit 2337)
---------------------------------------

Vector Time (GMT): 2008/136/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3593461
27                 A    =         6717222
95  meter
 Y    =        3668320
25  meter          E    =           
0005401
 Z    =       -4333900
79                 I    =           51
61176
 XDOT =      -6494
013520                 Wp   =          105
63245
 YDOT =       2312
674611  meter/sec      RA   =          183
62832  deg
 ZDOT =      -3431
978199                 TA   =          129
73901
                                          MA   =          129
69141
                                          Ha   =            186
341  n
mi
                                          Hp   =            181
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11789571
08                 X    =         3573228
03
 Y    =       12035171
42  feet           Y    =         3708391
49  meter
 Z    =      -14218834
60                 Z    =        -4316492
49
 XDOT =     -21305
818634                 XDOT =       -6502
719418
 YDOT =       7587
515129  feet/sec       YDOT =        2240
006339  meter/sec
 ZDOT =     -11259
770994                 ZDOT =       -3463
547543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15165304
41                 X    =         4622384
79
 Y    =       -7467364
59  feet           Y    =        -2276052
73  meter
 Z    =      -14151558
32                 Z    =        -4313394
98
 XDOT =        -45
563414                 XDOT =         -13
887729
 YDOT =      21444
491870  feet/sec       YDOT =        6536
281122  meter/sec
 ZDOT =     -11380
812076                 ZDOT =       -3468
871521


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   08136
57405304  
00020000  00000-0  20000-3 0  9106
2 25544  51
6402 184
4952 0005472 213
9832 146
0983 15
76407099 23384


Satellite: ISS
Catalog Number: 25544
Epoch time:      08136
57405304   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:       184
4952  deg
Eccentricity:     
0005472     
Arg of perigee:   213
9832  deg
Mean anomaly:     146
0983  deg
Mean motion:   15
76407099  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2338
Checksum:              292


Coasting Arc #12 (Orbit 2353)
---------------------------------------

Vector Time (GMT): 2008/137/13:14:53
461
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5998252
74                 A    =         6722884
90  meter
 Y    =       -1972282
94  meter          E    =           
0013084
 Z    =        2284865
31                 I    =           51
65931
 XDOT =       3465
065549                 Wp   =          129
85051
 YDOT =       4214
289346  meter/sec      RA   =          178
42918  deg
 ZDOT =      -5446
526856                 TA   =           24
43856
                                          MA   =           24
37659
                                          Ha   =            186
021  n
mi
                                          Hp   =            181
072

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19679306
89                 X    =         6008761
66
 Y    =       -6470744
57  feet           Y    =        -1905148
44  meter
 Z    =        7496277
27                 Z    =         2314030
70
 XDOT =      11368
325292                 XDOT =        3444
141852
 YDOT =      13826
408616  feet/sec       YDOT =        4252
921062  meter/sec
 ZDOT =     -17869
182600                 ZDOT =       -5429
743833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -301229
60                 X    =          -91814
78
 Y    =      -20672819
89  feet           Y    =        -6301075
50  meter
 Z    =        7608127
64                 Z    =         2318957
31
 XDOT =      15116
570506                 XDOT =        4607
530690
 YDOT =      -6787
260366  feet/sec       YDOT =       -2068
756959  meter/sec
 ZDOT =     -17804
248623                 ZDOT =       -5426
734980


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   08137
58832532  
00020000  00000-0  20000-3 0  9116
2 25544  51
6387 179
2676 0005330 217
9960 142
0829 15
76445634 23540


Satellite: ISS
Catalog Number: 25544
Epoch time:      08137
58832532   =   yrday
fracday
Element set:     911
Inclination:       51
6387  deg
RA of node:       179
2676  deg
Eccentricity:     
0005330     
Arg of perigee:   217
9960  deg
Mean anomaly:     142
0829  deg
Mean motion:   15
76445634  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2354
Checksum:              308

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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