Date: May 5th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 2068)
---------------------------------------

Vector Time (GMT): 2008/119/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3266541
92                 A    =         6720326
08  meter
 Y    =        4388451
95  meter          E    =           
0010977
 Z    =       -3908581
12                 I    =           51
31005
 XDOT =      -3037
195349                 Wp   =          112
36775
 YDOT =      -5824
087749  meter/sec      RA   =          271
75974  deg
 ZDOT =      -4013
934208                 TA   =          115
77227
                                          MA   =          115
65896
                                          Ha   =            189
352  n
mi
                                          Hp   =            179
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10717001
05                 X    =        -3296384
26
 Y    =       14397808
24  feet           Y    =         4351756
92  meter
 Z    =      -12823428
87                 Z    =        -3924522
33
 XDOT =      -9964
551669                 XDOT =       -2952
344725
 YDOT =     -19107
899438  feet/sec       YDOT =       -5857
576806  meter/sec
 ZDOT =     -13169
075485                 ZDOT =       -4028
483102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -689364
86                 X    =         -210118
41
 Y    =       17891753
68  feet           Y    =         5453406
52  meter
 Z    =      -12884147
16                 Z    =        -3927088
06
 XDOT =     -17627
154662                 XDOT =       -5372
756741
 YDOT =     -10172
272544  feet/sec       YDOT =       -3100
508671  meter/sec
 ZDOT =     -13225
492784                 ZDOT =       -4031
130200


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   08119
51825482  
00020000  00000-0  20000-3 0  9003
2 25544  51
6379 272
3532 0007188 149
5687 210
5896 15
75805196 20696


Satellite: ISS
Catalog Number: 25544
Epoch time:      08119
51825482   =   yrday
fracday
Element set:     900
Inclination:       51
6379  deg
RA of node:       272
3532  deg
Eccentricity:     
0007188     
Arg of perigee:   149
5687  deg
Mean anomaly:     210
5896  deg
Mean motion:   15
75805196  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2069
Checksum:              321


Coasting Arc #2 (Orbit 2084)
---------------------------------------

Vector Time (GMT): 2008/120/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2740908
53                 A    =         6723029
13  meter
 Y    =        5334382
35  meter          E    =           
0018095
 Z    =        3014639
88                 I    =           51
31881
 XDOT =      -3664
300026                 Wp   =          115
75280
 YDOT =       4672
439596  meter/sec      RA   =          266
53566  deg
 ZDOT =      -4921
167366                 TA   =           29
12516
                                          MA   =           29
02435
                                          Ha   =            189
247  n
mi
                                          Hp   =            179
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8992482
05                 X    =         2666410
29
 Y    =       17501254
44  feet           Y    =         5364616
14  meter
 Z    =        9890550
78                 Z    =         3027774
45
 XDOT =     -12021
981712                 XDOT =       -3692
369409
 YDOT =      15329
526235  feet/sec       YDOT =        4631
306489  meter/sec
 ZDOT =     -16145
562225                 ZDOT =       -4939
036653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17398960
88                 X    =         5303203
28
 Y    =        9133693
64  feet           Y    =         2783949
82  meter
 Z    =        9941500
68                 Z    =         3030169
41
 XDOT =       -227
887234                 XDOT =         -69
460029
 YDOT =      18135
375122  feet/sec       YDOT =        5527
662337  meter/sec
 ZDOT =     -16213
646535                 ZDOT =       -4941
919464


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   08120
53291778  
00020000  00000-0  20000-3 0  9013
2 25544  51
6371 267
1275 0007210 154
1229 206
0297 15
75809633 20857


Satellite: ISS
Catalog Number: 25544
Epoch time:      08120
53291778   =   yrday
fracday
Element set:     901
Inclination:       51
6371  deg
RA of node:       267
1275  deg
Eccentricity:     
0007210     
Arg of perigee:   154
1229  deg
Mean anomaly:     206
0297  deg
Mean motion:   15
75809633  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2085
Checksum:              282


Coasting Arc #3 (Orbit 2100)
---------------------------------------

Vector Time (GMT): 2008/121/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3173076
76                 A    =         6717458
44  meter
 Y    =       -3711783
52  meter          E    =           
0014243
 Z    =        4609070
29                 I    =           51
30475
 XDOT =       3274
769936                 Wp   =          135
86742
 YDOT =       6364
420928  meter/sec      RA   =          261
40911  deg
 ZDOT =       2855
529442                 TA   =          285
70928
                                          MA   =          285
86635
                                          Ha   =            189
004  n
mi
                                          Hp   =            179
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10410356
83                 X    =         3191956
51
 Y    =      -12177767
45  feet           Y    =        -3676194
85  meter
 Z    =       15121621
68                 Z    =         4624531
00
 XDOT =      10743
995852                 XDOT =        3189
486870
 YDOT =      20880
646088  feet/sec       YDOT =        6400
564402  meter/sec
 ZDOT =       9368
534914                 ZDOT =        2871
231288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1128057
74                 X    =          343832
00
 Y    =      -15925296
05  feet           Y    =        -4854030
23  meter
 Z    =       15180560
70                 Z    =         4627034
90
 XDOT =      19805
026699                 XDOT =        6036
572138
 YDOT =      10439
301232  feet/sec       YDOT =        3181
899016  meter/sec
 ZDOT =       9429
451960                 ZDOT =        2874
096957


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   08121
54755611  
00020000  00000-0  20000-3 0  9027
2 25544  51
6380 261
9022 0007093 158
7289 201
4171 15
75893081 21013


Satellite: ISS
Catalog Number: 25544
Epoch time:      08121
54755611   =   yrday
fracday
Element set:     902
Inclination:       51
6380  deg
RA of node:       261
9022  deg
Eccentricity:     
0007093     
Arg of perigee:   158
7289  deg
Mean anomaly:     201
4171  deg
Mean motion:   15
75893081  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2101
Checksum:              272


Coasting Arc #4 (Orbit 2115)
---------------------------------------

Vector Time (GMT): 2008/122/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2979360
67                 A    =         6725154
89  meter
 Y    =       -5721451
55  meter          E    =           
0006798
 Z    =       -1910113
99                 I    =           51
33745
 XDOT =       3683
773181                 Wp   =          100
53037
 YDOT =      -3782
350362  meter/sec      RA   =          256
19670  deg
 ZDOT =       5599
221098                 TA   =          238
14735
                                          MA   =          238
21353
                                          Ha   =            188
976  n
mi
                                          Hp   =            179
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9774805
34                 X    =        -2905881
99
 Y    =      -18771166
50  feet           Y    =        -5754357
62  meter
 Z    =       -6266778
20                 Z    =        -1924409
39
 XDOT =      12085
870016                 XDOT =        3698
593956
 YDOT =     -12409
285963  feet/sec       YDOT =       -3741
073438  meter/sec
 ZDOT =      18370
147958                 ZDOT =        5617
153041

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19110396
91                 X    =        -5824848
98
 Y    =       -9055277
75  feet           Y    =        -2760048
66  meter
 Z    =       -6322238
12                 Z    =        -1927018
18
 XDOT =       1373
005396                 XDOT =         418
492045
 YDOT =     -15735
547196  feet/sec       YDOT =       -4796
194785  meter/sec
 ZDOT =      18438
560314                 ZDOT =        5620
073184


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   08122
49876121  
00020000  00000-0  20000-3 0  9033
2 25544  51
6389 257
0037 0007042 161
1203 199
0223 15
75898030 21167


Satellite: ISS
Catalog Number: 25544
Epoch time:      08122
49876121   =   yrday
fracday
Element set:     903
Inclination:       51
6389  deg
RA of node:       257
0037  deg
Eccentricity:     
0007042     
Arg of perigee:   161
1203  deg
Mean anomaly:     199
0223  deg
Mean motion:   15
75898030  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2116
Checksum:              272


Coasting Arc #5 (Orbit 2131)
---------------------------------------

Vector Time (GMT): 2008/123/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3330663
92                 A    =         6715296
76  meter
 Y    =        2860484
00  meter          E    =           
0015944
 Z    =       -5093726
29                 I    =           51
31301
 XDOT =      -3525
360278                 Wp   =          104
42755
 YDOT =      -6681
778045  meter/sec      RA   =          251
05446  deg
 ZDOT =      -1454
853149                 TA   =          151
59611
                                          MA   =          151
50910
                                          Ha   =            188
740  n
mi
                                          Hp   =            179
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10927375
06                 X    =        -3337657
97
 Y    =        9384790
02  feet           Y    =         2823199
50  meter
 Z    =      -16711700
43                 Z    =        -5109923
89
 XDOT =     -11566
142645                 XDOT =       -3443
314054
 YDOT =     -21921
843980  feet/sec       YDOT =       -6720
741899  meter/sec
 ZDOT =      -4773
140252                 ZDOT =       -1471
780308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2706336
43                 X    =         -824891
34
 Y    =       14074315
41  feet           Y    =         4289851
34  meter
 Z    =      -16773554
47                 Z    =        -5112579
40
 XDOT =     -21600
057583                 XDOT =       -6583
697551
 YDOT =      -9890
216385  feet/sec       YDOT =       -3014
537954  meter/sec
 ZDOT =      -4838
805541                 ZDOT =       -1474
867929


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   08123
51335687  
00020000  00000-0  20000-3 0  9045
2 25544  51
6392 251
7787 0006882 165
0813 195
0556 15
75939184 21324


Satellite: ISS
Catalog Number: 25544
Epoch time:      08123
51335687   =   yrday
fracday
Element set:     904
Inclination:       51
6392  deg
RA of node:       251
7787  deg
Eccentricity:     
0006882     
Arg of perigee:   165
0813  deg
Mean anomaly:     195
0556  deg
Mean motion:   15
75939184  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2132
Checksum:              311


Coasting Arc #6 (Orbit 2147)
---------------------------------------

Vector Time (GMT): 2008/124/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3172386
66                 A    =         6726430
15  meter
 Y    =        5887369
50  meter          E    =           
0019074
 Z    =         609938
47                 I    =           51
36181
 XDOT =      -3993
531342                 Wp   =          142
17206
 YDOT =       2780
223047  meter/sec      RA   =          245
86309  deg
 ZDOT =      -5981
206706                 TA   =           31
15052
                                          MA   =           31
03760
                                          Ha   =            188
608  n
mi
                                          Hp   =            179
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10408092
71                 X    =         3103354
36
 Y    =       19315516
75  feet           Y    =         5922458
96  meter
 Z    =        2001110
45                 Z    =          625182
62
 XDOT =     -13102
136948                 XDOT =       -3995
267190
 YDOT =       9121
466689  feet/sec       YDOT =        2735
555455  meter/sec
 ZDOT =     -19623
381582                 ZDOT =       -6000
611874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20264158
08                 X    =         6176515
38
 Y    =        8398889
98  feet           Y    =         2559981
67  meter
 Z    =        2060235
01                 Z    =          627959
63
 XDOT =      -3690
355607                 XDOT =       -1124
820389
 YDOT =      13800
939678  feet/sec       YDOT =        4206
526414  meter/sec
 ZDOT =     -19697
554752                 ZDOT =       -6003
814688


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   08124
52793049  
00020000  00000-0  20000-3 0  9058
2 25544  51
6394 246
5523 0006875 169
1577 190
9737 15
75964609 21482


Satellite: ISS
Catalog Number: 25544
Epoch time:      08124
52793049   =   yrday
fracday
Element set:     905
Inclination:       51
6394  deg
RA of node:       246
5523  deg
Eccentricity:     
0006875     
Arg of perigee:   169
1577  deg
Mean anomaly:     190
9737  deg
Mean motion:   15
75964609  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2148
Checksum:              332


Coasting Arc #7 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2008/125/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3688238
42                 A    =         6714320
45  meter
 Y    =       -1996109
82  meter          E    =           
0007268
 Z    =        5240763
47                 I    =           51
33588
 XDOT =       3728
928640                 Wp   =          154
37586
 YDOT =       6745
010244  meter/sec      RA   =          240
69756  deg
 ZDOT =        -61
657292                 TA   =          296
17380
                                          MA   =          296
24853
                                          Ha   =            188
290  n
mi
                                          Hp   =            179
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12100519
75                 X    =         3684825
79
 Y    =       -6548916
75  feet           Y    =        -1954885
11  meter
 Z    =       17194105
87                 Z    =         5258673
02
 XDOT =      12234
017848                 XDOT =        3653
527262
 YDOT =      22129
298702  feet/sec       YDOT =        6786
287669  meter/sec
 ZDOT =       -202
287705                 ZDOT =         -43
724598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4944536
99                 X    =         1507094
87
 Y    =      -12747605
21  feet           Y    =        -3885470
07  meter
 Z    =       17262626
71                 Z    =         5261648
62
 XDOT =      22696
111074                 XDOT =        6917
774655
 YDOT =       8652
071011  feet/sec       YDOT =        2637
151244  meter/sec
 ZDOT =       -132
754513                 ZDOT =         -40
463576


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   08125
54248092  
00020000  00000-0  20000-3 0  9065
2 25544  51
6405 241
3269 0006665 173
3021 186
8233 15
76027982 21641


Satellite: ISS
Catalog Number: 25544
Epoch time:      08125
54248092   =   yrday
fracday
Element set:     906
Inclination:       51
6405  deg
RA of node:       241
3269  deg
Eccentricity:     
0006665     
Arg of perigee:   173
3021  deg
Mean anomaly:     186
8233  deg
Mean motion:   15
76027982  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2164
Checksum:              288


Coasting Arc #8 (Orbit 2179)
---------------------------------------

Vector Time (GMT): 2008/126/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3284048
66                 A    =         6726173
71  meter
 Y    =       -5821375
64  meter          E    =           
0011249
 Z    =         734798
36                 I    =           51
39175
 XDOT =       4536
170704                 Wp   =           82
07486
 YDOT =      -1797
436924  meter/sec      RA   =          235
53475  deg
 ZDOT =       5957
375348                 TA   =          285
96397
                                          MA   =          286
08787
                                          Ha   =            188
286  n
mi
                                          Hp   =            180
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10774437
86                 X    =        -3222278
65
 Y    =      -19099001
46  feet           Y    =        -5857754
43  meter
 Z    =        2410755
79                 Z    =          718993
65
 XDOT =      14882
449816                 XDOT =        4526
992177
 YDOT =      -5897
102768  feet/sec       YDOT =       -1746
762632  meter/sec
 ZDOT =      19545
194712                 ZDOT =        5979
390214

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20693199
20                 X    =        -6307287
12
 Y    =       -7276230
61  feet           Y    =        -2217795
09  meter
 Z    =        2349486
37                 Z    =          716123
45
 XDOT =       6707
117516                 XDOT =        2044
329419
 YDOT =     -12653
517799  feet/sec       YDOT =       -3856
792225  meter/sec
 ZDOT =      19629
498946                 ZDOT =        5983
071279


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
55701087  
00020000  00000-0  20000-3 0  9076
2 25544  51
6409 236
1015 0006592 176
1644 183
9572 15
76035194 21803


Satellite: ISS
Catalog Number: 25544
Epoch time:      08126
55701087   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       236
1015  deg
Eccentricity:     
0006592     
Arg of perigee:   176
1644  deg
Mean anomaly:     183
9572  deg
Mean motion:   15
76035194  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2180
Checksum:              291


Coasting Arc #9 (Orbit 2194)
---------------------------------------

Vector Time (GMT): 2008/127/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4282009
94                 A    =         6715010
70  meter
 Y    =        1162537
17  meter          E    =           
0016393
 Z    =       -5054079
20                 I    =           51
37228
 XDOT =      -3714
822778                 Wp   =          125
34330
 YDOT =      -6533
822026  meter/sec      RA   =          230
34533  deg
 ZDOT =       1638
826914                 TA   =          160
51310
                                          MA   =          160
45036
                                          Ha   =            188
049  n
mi
                                          Hp   =            180
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14048589
05                 X    =        -4270139
00
 Y    =        3814098
34  feet           Y    =         1114720
22  meter
 Z    =      -16581624
68                 Z    =        -5074852
73
 XDOT =     -12187
738772                 XDOT =       -3649
445769
 YDOT =     -21436
423970  feet/sec       YDOT =       -6574
997936  meter/sec
 ZDOT =       5376
728721                 ZDOT =        1620
937973

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7785264
93                 X    =        -2372948
75
 Y    =       12192341
58  feet           Y    =         3716225
71  meter
 Z    =      -16661240
48                 Z    =        -5078346
10
 XDOT =     -22555
132668                 XDOT =       -6874
804437
 YDOT =      -7124
562413  feet/sec       YDOT =       -2171
566623  meter/sec
 ZDOT =       5307
382611                 ZDOT =        1617
690220


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
50811197  
00020000  00000-0  20000-3 0  9087
2 25544  51
6408 231
2033 0006514 179
7510 180
3658 15
76094738 21954


Satellite: ISS
Catalog Number: 25544
Epoch time:      08127
50811197   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       231
2033  deg
Eccentricity:     
0006514     
Arg of perigee:   179
7510  deg
Mean anomaly:     180
3658  deg
Mean motion:   15
76094738  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2195
Checksum:              293


Coasting Arc #10 (Orbit 2210)
---------------------------------------

Vector Time (GMT): 2008/128/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3140673
76                 A    =         6724302
02  meter
 Y    =        5551809
22  meter          E    =           
0011974
 Z    =       -2109264
13                 I    =           51
42283
 XDOT =      -5300
592961                 Wp   =          161
94235
 YDOT =        909
133968  meter/sec      RA   =          225
20965  deg
 ZDOT =      -5519
140803                 TA   =           41
73590
                                          MA   =           41
64462
                                          Ha   =            187
945  n
mi
                                          Hp   =            180
325

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10304047
77                 X    =         3088605
74
 Y    =       18214597
19  feet           Y    =         5586639
19  meter
 Z    =       -6920157
90                 Z    =        -2094132
20
 XDOT =     -17390
396853                 XDOT =       -5283
553639
 YDOT =       2982
722993  feet/sec       YDOT =         849
955718  meter/sec
 ZDOT =     -18107
417333                 ZDOT =       -5544
850020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20001979
18                 X    =         6096603
25
 Y    =        6218866
53  feet           Y    =         1895510
52  meter
 Z    =       -6861491
41                 Z    =        -2091382
58
 XDOT =     -10121
519140                 XDOT =       -3085
039034
 YDOT =      12538
263171  feet/sec       YDOT =        3821
662614  meter/sec
 ZDOT =     -18206
017796                 ZDOT =       -5549
194224


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
52259936  
00020000  00000-0  20000-3 0  9098
2 25544  51
6404 225
9775 0006491 184
1634 175
9477 15
76099134 22117


Satellite: ISS
Catalog Number: 25544
Epoch time:      08128
52259936   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:       225
9775  deg
Eccentricity:     
0006491     
Arg of perigee:   184
1634  deg
Mean anomaly:     175
9477  deg
Mean motion:   15
76099134  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2211
Checksum:              317


Coasting Arc #11 (Orbit 2226)
---------------------------------------

Vector Time (GMT): 2008/129/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4977840
19                 A    =         6717218
88  meter
 Y    =        -484437
60  meter          E    =           
0007767
 Z    =        4476446
80                 I    =           51
42096
 XDOT =       3426
711036                 Wp   =          110
89080
 YDOT =       6148
744988  meter/sec      RA   =          220
00041  deg
 ZDOT =      -3143
470612                 TA   =           10
55689
                                          MA   =           10
54059
                                          Ha   =            187
589  n
mi
                                          Hp   =            180
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16331496
69                 X    =         4961141
29
 Y    =       -1589362
21  feet           Y    =         -428866
54  meter
 Z    =       14686505
24                 Z    =         4500588
77
 XDOT =      11242
490277                 XDOT =        3372
970693
 YDOT =      20173
047860  feet/sec       YDOT =        6186
764394  meter/sec
 ZDOT =     -10313
223792                 ZDOT =       -3126
953147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10556611
78                 X    =         3217655
27
 Y    =      -12452793
55  feet           Y    =        -3795611
47  meter
 Z    =       14779146
57                 Z    =         4504683
87
 XDOT =      21248
907142                 XDOT =        6476
666897
 YDOT =       5843
132663  feet/sec       YDOT =        1780
986836  meter/sec
 ZDOT =     -10249
166977                 ZDOT =       -3123
946095


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
53706524  
00020000  00000-0  20000-3 0  9102
2 25544  51
6403 220
7517 0006264 187
5662 172
5409 15
76143725 22270


Satellite: ISS
Catalog Number: 25544
Epoch time:      08129
53706524   =   yrday
fracday
Element set:     910
Inclination:       51
6403  deg
RA of node:       220
7517  deg
Eccentricity:     
0006264     
Arg of perigee:   187
5662  deg
Mean anomaly:     172
5409  deg
Mean motion:   15
76143725  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2227
Checksum:              284


Coasting Arc #12 (Orbit 2242)
---------------------------------------

Vector Time (GMT): 2008/130/11:52:46
026
Vector Time (MET): N/A
Weight (LBS)     : 615213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2746498
29                 A    =         6721186
50  meter
 Y    =       -5149252
35  meter          E    =           
0012852
 Z    =        3330565
26                 I    =           51
45727
 XDOT =       6131
809318                 Wp   =          117
65349
 YDOT =       -246
541495  meter/sec      RA   =          214
88305  deg
 ZDOT =       4655
777748                 TA   =          281
67180
                                          MA   =          281
81600
                                          Ha   =            187
551  n
mi
                                          Hp   =            180
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9010821
15                 X    =        -2704893
77
 Y    =      -16893872
55  feet           Y    =        -5179733
08  meter
 Z    =       10927051
38                 Z    =         3317323
09
 XDOT =      20117
484639                 XDOT =        6111
493428
 YDOT =       -808
863173  feet/sec       YDOT =        -178
086304  meter/sec
 ZDOT =      15274
861378                 ZDOT =        4685
516835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18371776
22                 X    =        -5599717
39
 Y    =       -5495093
30  feet           Y    =        -1674904
44  meter
 Z    =       10875663
99                 Z    =         3314902
38
 XDOT =      13162
641465                 XDOT =        4011
973118
 YDOT =     -13421
814094  feet/sec       YDOT =       -4090
968936  meter/sec
 ZDOT =      15389
033107                 ZDOT =        4690
577291


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
55150928  
00020000  00000-0  20000-3 0  9118
2 25544  51
6399 215
5253 0006283 192
0478 168
0537 15
76184484 22437


Satellite: ISS
Catalog Number: 25544
Epoch time:      08130
55150928   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       215
5253  deg
Eccentricity:     
0006283     
Arg of perigee:   192
0478  deg
Mean anomaly:     168
0537  deg
Mean motion:   15
76184484  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2243
Checksum:              297

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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