Date: March 18th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9472 24 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


080/02:40:34 719 0 0 0 6 0 6
N/A -0 5 -0 0 186 6
000/00:05:09 439 0 3 -0 1 180 6

Coasting Arc #1 (Orbit 1404)
---------------------------------------

Vector Time (GMT): 2008/077/09:07:03
812
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5258533
35                 A    =         6722664
35  meter
 Y    =        3235494
26  meter          E    =           
0012587
 Z    =        2645106
30                 I    =           51
90312
 XDOT =       -789
259210                 Wp   =           77
44187
 YDOT =      -5588
104263  meter/sec      RA   =          128
77050  deg
 ZDOT =       5248
182094                 TA   =          312
58440
                                          MA   =          312
69053
                                          Ha   =            186
212  n
mi
                                          Hp   =            180
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17252406
01                 X    =        -5307171
51
 Y    =       10615138
64  feet           Y    =         3176418
50  meter
 Z    =        8678170
28                 Z    =         2619442
59
 XDOT =      -2589
433105                 XDOT =        -752
207702
 YDOT =     -18333
675404  feet/sec       YDOT =       -5596
722820  meter/sec
 ZDOT =      17218
445190                 ZDOT =        5244
438187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19397149
72                 X    =        -5912251
24
 Y    =       -5980712
53  feet           Y    =        -1822921
18  meter
 Z    =        8580150
43                 Z    =         2615229
85
 XDOT =      11555
698512                 XDOT =        3522
176906
 YDOT =     -12711
471112  feet/sec       YDOT =       -3874
456395  meter/sec
 ZDOT =      17203
428446                 ZDOT =        5243
604990


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   08077
43806303  
00020000  00000-0  20000-3 0  9008
2 25544  51
6394 129
3546 0001171 259
8037 100
2995 15
76300411 14058


Satellite: ISS
Catalog Number: 25544
Epoch time:      08077
43806303   =   yrday
fracday
Element set:     900
Inclination:       51
6394  deg
RA of node:       129
3546  deg
Eccentricity:     
0001171     
Arg of perigee:   259
8037  deg
Mean anomaly:     100
2995  deg
Mean motion:   15
76300411  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1405
Checksum:              268


Coasting Arc #2 (Orbit 1419)
---------------------------------------

Vector Time (GMT): 2008/078/09:07:03
812
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         382610
93                 A    =         6718073
45  meter
 Y    =        5285381
82  meter          E    =           
0006795
 Z    =       -4136451
77                 I    =           51
90522
 XDOT =      -5796
249952                 Wp   =          113
99080
 YDOT =       3374
445223  meter/sec      RA   =          123
58925  deg
 ZDOT =       3777
725345                 TA   =          194
57820
                                          MA   =          194
59780
                                          Ha   =            186
085  n
mi
                                          Hp   =            180
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1255285
21                 X    =          343574
27
 Y    =       17340491
53  feet           Y    =         5289441
84  meter
 Z    =      -13571035
99                 Z    =        -4134688
26
 XDOT =     -19016
568084                 XDOT =       -5851
903876
 YDOT =      11071
014510  feet/sec       YDOT =        3309
317328  meter/sec
 ZDOT =      12394
112025                 ZDOT =        3749
432316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11924822
77                 X    =        -3634685
98
 Y    =       12659679
09  feet           Y    =         3858670
19  meter
 Z    =      -13563647
46                 Z    =        -4134199
74
 XDOT =     -20112
977606                 XDOT =       -6130
435574
 YDOT =      -5789
702253  feet/sec       YDOT =       -1764
701247  meter/sec
 ZDOT =      12286
020053                 ZDOT =        3744
778912


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   08078
38901334  
00020000  00000-0  20000-3 0  9014
2 25544  51
6392 124
4552 0001161 265
8306  94
2725 15
76341814 14206


Satellite: ISS
Catalog Number: 25544
Epoch time:      08078
38901334   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       124
4552  deg
Eccentricity:     
0001161     
Arg of perigee:   265
8306  deg
Mean anomaly:      94
2725  deg
Mean motion:   15
76341814  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1420
Checksum:              272


Coasting Arc #3 (Orbit 1435)
---------------------------------------

Vector Time (GMT): 2008/079/09:07:03
812
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4853153
64                 A    =         6719032
06  meter
 Y    =       -2554585
72  meter          E    =           
0005385
 Z    =       -3887301
38                 I    =           51
92255
 XDOT =        132
945468                 Wp   =           70
38235
 YDOT =       6506
456081  meter/sec      RA   =          118
50663  deg
 ZDOT =      -4112
631553                 TA   =          156
89146
                                          MA   =          156
86723
                                          Ha   =            186
095  n
mi
                                          Hp   =            180
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15922420
09                 X    =         4900242
21
 Y    =       -8381186
76  feet           Y    =        -2500052
05  meter
 Z    =      -12753613
45                 Z    =        -3863610
56
 XDOT =        436
172794                 XDOT =          80
157466
 YDOT =      21346
640686  feet/sec       YDOT =        6507
647229  meter/sec
 ZDOT =     -13492
885671                 ZDOT =       -4112
114521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17069366
75                 X    =         5202742
99
 Y    =        5891166
34  feet           Y    =         1795627
50  meter
 Z    =      -12663067
83                 Z    =        -3859703
07
 XDOT =     -14753
167396                 XDOT =       -4496
765422
 YDOT =      13769
524436  feet/sec       YDOT =        4196
951048  meter/sec
 ZDOT =     -13490
132148                 ZDOT =       -4111
792279


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   08079
40333919  
00020000  00000-0  20000-3 0  9027
2 25544  51
6384 119
2279 0001183 271
9495  88
1534 15
76341091 14360


Satellite: ISS
Catalog Number: 25544
Epoch time:      08079
40333919   =   yrday
fracday
Element set:     902
Inclination:       51
6384  deg
RA of node:       119
2279  deg
Eccentricity:     
0001183     
Arg of perigee:   271
9495  deg
Mean anomaly:      88
1534  deg
Mean motion:   15
76341091  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1436
Checksum:              299


Coasting Arc #4 (Orbit 1447)
---------------------------------------

Vector Time (GMT): 2008/080/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4445769
83                 A    =         6714889
06  meter
 Y    =         240876
77  meter          E    =           
0004752
 Z    =        5023908
01                 I    =           51
91353
 XDOT =       1730
355401                 Wp   =          122
59293
 YDOT =      -7272
042213  meter/sec      RA   =          114
72847  deg
 ZDOT =       1876
114564                 TA   =          309
36985
                                          MA   =          309
41194
                                          Ha   =            186
583  n
mi
                                          Hp   =            180
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14585859
03                 X    =        -4472537
84
 Y    =         790278
12  feet           Y    =          191012
47  meter
 Z    =       16482637
83                 Z    =         5002245
72
 XDOT =       5677
019032                 XDOT =        1802
430203
 YDOT =     -23858
406209  feet/sec       YDOT =       -7252
289209  meter/sec
 ZDOT =       6155
231509                 ZDOT =        1884
696316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11072294
82                 X    =         3374835
46
 Y    =       -9669888
01  feet           Y    =        -2947381
86  meter
 Z    =       16399595
31                 Z    =         4998596
65
 XDOT =       9557
283920                 XDOT =        2913
060139
 YDOT =      21457
796837  feet/sec       YDOT =        6540
336476  meter/sec
 ZDOT =       6187
280912                 ZDOT =        1885
883222


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   08080
16407427  
00020000  00000-0  20000-3 0  9039
2 25544  51
6347 115
3043 0000915 317
1792  42
9301 15
76244056 14486


Satellite: ISS
Catalog Number: 25544
Epoch time:      08080
16407427   =   yrday
fracday
Element set:     903
Inclination:       51
6347  deg
RA of node:       115
3043  deg
Eccentricity:     
0000915     
Arg of perigee:   317
1792  deg
Mean anomaly:      42
9301  deg
Mean motion:   15
76244056  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1448
Checksum:              267


Coasting Arc #5 (Orbit 1462)
---------------------------------------

Vector Time (GMT): 2008/081/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1564363
91                 A    =         6725271
77  meter
 Y    =        6475068
69  meter          E    =           
0010256
 Z    =        -888408
14                 I    =           51
96053
 XDOT =      -4841
563528                 Wp   =           34
77470
 YDOT =       -354
633257  meter/sec      RA   =          109
57176  deg
 ZDOT =       5982
432619                 TA   =          315
56243
                                          MA   =          315
64467
                                          Ha   =            186
386  n
mi
                                          Hp   =            180
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5132427
51                 X    =        -1632337
17
 Y    =       21243663
68  feet           Y    =         6457194
92  meter
 Z    =       -2914724
86                 Z    =         -896173
56
 XDOT =     -15884
394778                 XDOT =       -4866
299454
 YDOT =      -1163
494937  feet/sec       YDOT =        -408
912044  meter/sec
 ZDOT =      19627
403605                 ZDOT =        5958
852469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9405814
32                 X    =        -2866892
21
 Y    =      -19722974
36  feet           Y    =        -6011562
59  meter
 Z    =       -2943742
30                 Z    =         -897252
65
 XDOT =      11719
096865                 XDOT =        3571
980724
 YDOT =      -8484
495074  feet/sec       YDOT =       -2586
074099  meter/sec
 ZDOT =      19536
934762                 ZDOT =        5954
857716


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   08081
11503342  
00020000  00000-0  20000-3 0  9049
2 25544  51
6350 110
4031 0000732 315
6618  44
4487 15
76304435 14637


Satellite: ISS
Catalog Number: 25544
Epoch time:      08081
11503342   =   yrday
fracday
Element set:     904
Inclination:       51
6350  deg
RA of node:       110
4031  deg
Eccentricity:     
0000732     
Arg of perigee:   315
6618  deg
Mean anomaly:      44
4487  deg
Mean motion:   15
76304435  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1463
Checksum:              248


Coasting Arc #6 (Orbit 1478)
---------------------------------------

Vector Time (GMT): 2008/082/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4043937
65                 A    =         6713431
25  meter
 Y    =         918241
42  meter          E    =           
0014761
 Z    =       -5292129
76                 I    =           51
92962
 XDOT =      -1837
924850                 Wp   =           87
06126
 YDOT =       7470
549618  meter/sec      RA   =          104
45001  deg
 ZDOT =       -107
731218                 TA   =          181
91680
                                          MA   =          181
92247
                                          Ha   =            186
390  n
mi
                                          Hp   =            180
399

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13267511
96                 X    =         4059077
30
 Y    =        3012603
10  feet           Y    =          963547
13  meter
 Z    =      -17362630
45                 Z    =        -5272447
71
 XDOT =      -6029
937171                 XDOT =       -1920
801761
 YDOT =      24509
677226  feet/sec       YDOT =        7449
533493  meter/sec
 ZDOT =       -353
448878                 ZDOT =        -116
861924

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12172928
89                 X    =        -3710308
73
 Y    =        6288202
25  feet           Y    =         1916644
05  meter
 Z    =      -17287044
34                 Z    =        -5269091
11
 XDOT =     -10687
008365                 XDOT =       -3257
400150
 YDOT =     -21758
214312  feet/sec       YDOT =       -6631
903722  meter/sec
 ZDOT =       -387
592433                 ZDOT =        -118
138174


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   08082
12936960  
00020000  00000-0  20000-3 0  9058
2 25544  51
6351 105
1758 0000628 329
0583  31
0544 15
76345808 14791


Satellite: ISS
Catalog Number: 25544
Epoch time:      08082
12936960   =   yrday
fracday
Element set:     905
Inclination:       51
6351  deg
RA of node:       105
1758  deg
Eccentricity:     
0000628     
Arg of perigee:   329
0583  deg
Mean anomaly:      31
0544  deg
Mean motion:   15
76345808  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1479
Checksum:              291


Coasting Arc #7 (Orbit 1494)
---------------------------------------

Vector Time (GMT): 2008/083/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1630021
43                 A    =         6725122
35  meter
 Y    =       -6480841
31  meter          E    =           
0009835
 Z    =        -714304
34                 I    =           51
97526
 XDOT =       4472
999184                 Wp   =          139
07405
 YDOT =       1781
940199  meter/sec      RA   =           99
32318  deg
 ZDOT =      -6013
688368                 TA   =           48
68000
                                          MA   =           48
59541
                                          Ha   =            186
305  n
mi
                                          Hp   =            180
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5347839
33                 X    =         1705840
02
 Y    =      -21262602
72  feet           Y    =        -6462189
62  meter
 Z    =       -2343518
16                 Z    =         -706200
90
 XDOT =      14675
194172                 XDOT =        4481
954252
 YDOT =       5846
260497  feet/sec       YDOT =        1832
009329  meter/sec
 ZDOT =     -19729
948715                 ZDOT =       -5991
936938

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9906015
36                 X    =         3019353
48
 Y    =       19562968
85  feet           Y    =         5962792
90  meter
 Z    =       -2313189
79                 Z    =         -705060
25
 XDOT =     -13568
128142                 XDOT =       -4135
565458
 YDOT =       4568
415040  feet/sec       YDOT =        1392
452904  meter/sec
 ZDOT =     -19646
327475                 ZDOT =       -5988
200614


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   08083
14368207  
00020000  00000-0  20000-3 0  9065
2 25544  51
6347  99
9468 0000850 334
3457  25
7665 15
76406062 14952


Satellite: ISS
Catalog Number: 25544
Epoch time:      08083
14368207   =   yrday
fracday
Element set:     906
Inclination:       51
6347  deg
RA of node:        99
9468  deg
Eccentricity:     
0000850     
Arg of perigee:   334
3457  deg
Mean anomaly:      25
7665  deg
Mean motion:   15
76406062  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1495
Checksum:              309


Coasting Arc #8 (Orbit 1510)
---------------------------------------

Vector Time (GMT): 2008/084/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3818216
68                 A    =         6714339
34  meter
 Y    =       -2190370
83  meter          E    =           
0005430
 Z    =        5067496
41                 I    =           51
94220
 XDOT =       1881
555577                 Wp   =           49
01340
 YDOT =      -7273
037562  meter/sec      RA   =           94
17053  deg
 ZDOT =      -1721
318975                 TA   =           57
49080
                                          MA   =           57
43834
                                          Ha   =            186
546  n
mi
                                          Hp   =            180
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12526957
62                 X    =        -3818056
93
 Y    =       -7186256
00  feet           Y    =        -2233067
02  meter
 Z    =       16625644
37                 Z    =         5048947
99
 XDOT =       6173
082603                 XDOT =        1971
105865
 YDOT =     -23861
671790  feet/sec       YDOT =       -7251
496366  meter/sec
 ZDOT =      -5647
371966                 ZDOT =       -1711
960251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14188265
32                 X    =         4324583
27
 Y    =       -3102987
98  feet           Y    =         -945790
74  meter
 Z    =       16554261
87                 Z    =         5045739
02
 XDOT =      11126
393164                 XDOT =        3391
324636
 YDOT =      20851
400285  feet/sec       YDOT =        6355
506807  meter/sec
 ZDOT =      -5612
309058                 ZDOT =       -1710
631801


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   08084
15797568  
00020000  00000-0  20000-3 0  9074
2 25544  51
6350  94
7186 0000565 344
4989  15
6157 15
76363751 15111


Satellite: ISS
Catalog Number: 25544
Epoch time:      08084
15797568   =   yrday
fracday
Element set:     907
Inclination:       51
6350  deg
RA of node:        94
7186  deg
Eccentricity:     
0000565     
Arg of perigee:   344
4989  deg
Mean anomaly:      15
6157  deg
Mean motion:   15
76363751  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1511
Checksum:              317


Coasting Arc #9 (Orbit 1526)
---------------------------------------

Vector Time (GMT): 2008/085/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1669423
50                 A    =         6722956
80  meter
 Y    =        6100038
31  meter          E    =           
0013951
 Z    =        2260694
93                 I    =           51
97448
 XDOT =      -4343
548357                 Wp   =           69
81227
 YDOT =      -3230
451981  meter/sec      RA   =           89
07322  deg
 ZDOT =       5486
842502                 TA   =          315
48410
                                          MA   =          315
59609
                                          Ha   =            186
256  n
mi
                                          Hp   =            180
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5477111
22                 X    =        -1748493
11
 Y    =       20013249
03  feet           Y    =         6080927
89  meter
 Z    =        7416978
10                 Z    =         2252392
40
 XDOT =     -14250
486735                 XDOT =       -4333
756369
 YDOT =     -10598
595739  feet/sec       YDOT =       -3278
968952  meter/sec
 ZDOT =      18001
451778                 ZDOT =        5465
765392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9605706
03                 X    =        -2927819
20
 Y    =      -18404361
09  feet           Y    =        -5609649
26  meter
 Z    =        7385821
07                 Z    =         2251198
26
 XDOT =      16383
644424                 XDOT =        4993
734820
 YDOT =      -1329
913036  feet/sec       YDOT =        -405
357493  meter/sec
 ZDOT =      17920
256864                 ZDOT =        5462
094292


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   08085
17224161  
00020000  00000-0  20000-3 0  9082
2 25544  51
6364  89
4906 0000534 331
9505  28
1630 15
76469851 15278


Satellite: ISS
Catalog Number: 25544
Epoch time:      08085
17224161   =   yrday
fracday
Element set:     908
Inclination:       51
6364  deg
RA of node:        89
4906  deg
Eccentricity:     
0000534     
Arg of perigee:   331
9505  deg
Mean anomaly:      28
1630  deg
Mean motion:   15
76469851  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1527
Checksum:              292


Coasting Arc #10 (Orbit 1541)
---------------------------------------

Vector Time (GMT): 2008/086/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3803044
69                 A    =         6716935
64  meter
 Y    =        3412584
82  meter          E    =           
0008635
 Z    =       -4368394
95                 I    =           51
95298
 XDOT =      -1990
513101                 Wp   =          107
37847
 YDOT =       6599
195540  meter/sec      RA   =           83
89796  deg
 ZDOT =       3425
375093                 TA   =          197
01669
                                          MA   =          197
04567
                                          Ha   =            186
272  n
mi
                                          Hp   =            180
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12477180
73                 X    =         3785822
99
 Y    =       11196144
41  feet           Y    =         3455016
18  meter
 Z    =      -14332004
44                 Z    =        -4349961
61
 XDOT =      -6530
554792                 XDOT =       -2080
798347
 YDOT =      21650
904001  feet/sec       YDOT =        6576
431804  meter/sec
 ZDOT =      11238
107259                 ZDOT =        3415
485569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16811634
43                 X    =        -5124186
17
 Y    =         659405
18  feet           Y    =          200986
70  meter
 Z    =      -14260931
69                 Z    =        -4346731
98
 XDOT =     -10235
811539                 XDOT =       -3119
875357
 YDOT =     -18935
574247  feet/sec       YDOT =       -5771
563030  meter/sec
 ZDOT =      11200
907291                 ZDOT =        3414
036542


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   08086
12309831  
00020000  00000-0  20000-3 0  9097
2 25544  51
6370  84
5900 0000633 342
3558  17
7585 15
76466384 15427


Satellite: ISS
Catalog Number: 25544
Epoch time:      08086
12309831   =   yrday
fracday
Element set:     909
Inclination:       51
6370  deg
RA of node:        84
5900  deg
Eccentricity:     
0000633     
Arg of perigee:   342
3558  deg
Mean anomaly:      17
7585  deg
Mean motion:   15
76466384  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1542
Checksum:              296


Coasting Arc #11 (Orbit 1557)
---------------------------------------

Vector Time (GMT): 2008/087/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1864018
14                 A    =         6719259
62  meter
 Y    =       -5324139
52  meter          E    =           
0005624
 Z    =       -3656716
32                 I    =           51
95727
 XDOT =       4397
507984                 Wp   =           73
30627
 YDOT =       4548
965126  meter/sec      RA   =           78
81550  deg
 ZDOT =      -4385
542145                 TA   =          150
37792
                                          MA   =          150
34606
                                          Ha   =            186
212  n
mi
                                          Hp   =            180
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6115545
08                 X    =         1941178
71
 Y    =      -17467649
33  feet           Y    =        -5302863
65  meter
 Z    =      -11997100
78                 Z    =        -3647473
34
 XDOT =      14427
519631                 XDOT =        4367
618190
 YDOT =      14924
426265  feet/sec       YDOT =        4597
973357  meter/sec
 ZDOT =     -14388
261631                 ZDOT =       -4364
251647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7964417
87                 X    =         2427554
57
 Y    =       16730875
64  feet           Y    =         5099570
90  meter
 Z    =      -11962229
74                 Z    =        -3646087
63
 XDOT =     -19592
264124                 XDOT =       -5971
722105
 YDOT =       -892
784121  feet/sec       YDOT =        -272
120600  meter/sec
 ZDOT =     -14306
109247                 ZDOT =       -4360
502098


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   08087
13732164  
00020000  00000-0  20000-3 0  9100
2 25544  51
6375  79
3615 0000609 344
7042  15
4104 15
76506583 15589


Satellite: ISS
Catalog Number: 25544
Epoch time:      08087
13732164   =   yrday
fracday
Element set:     910
Inclination:       51
6375  deg
RA of node:        79
3615  deg
Eccentricity:     
0000609     
Arg of perigee:   344
7042  deg
Mean anomaly:      15
4104  deg
Mean motion:   15
76506583  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1558
Checksum:              281


Coasting Arc #12 (Orbit 1573)
---------------------------------------

Vector Time (GMT): 2008/088/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3899523
42                 A    =         6720628
24  meter
 Y    =       -4447163
59  meter          E    =           
0012925
 Z    =        3179757
03                 I    =           51
95560
 XDOT =       2331
137512                 Wp   =           91
35001
 YDOT =      -5521
126959  meter/sec      RA   =           73
63224  deg
 ZDOT =      -4846
464941                 TA   =           51
68967
                                          MA   =           51
57352
                                          Ha   =            186
259  n
mi
                                          Hp   =            179
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12793712
02                 X    =        -3864951
45
 Y    =      -14590431
74  feet           Y    =        -4490576
96  meter
 Z    =       10432273
71                 Z    =         3160897
11
 XDOT =       7648
088950                 XDOT =        2416
245667
 YDOT =     -18113
933594  feet/sec       YDOT =       -5494
583033  meter/sec
 ZDOT =     -15900
475529                 ZDOT =       -4834
933464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19422729
39                 X    =         5920047
92
 Y    =         911772
87  feet           Y    =          277908
37  meter
 Z    =       10359457
20                 Z    =         3157562
56
 XDOT =       7700
678654                 XDOT =        2347
166854
 YDOT =      16741
666678  feet/sec       YDOT =        5102
860003  meter/sec
 ZDOT =     -15856
838889                 ZDOT =       -4833
164493


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   08088
15152168  
00020000  00000-0  20000-3 0  9114
2 25544  51
6380  74
1335 0000545 354
0524   6
0634 15
76534265 15745


Satellite: ISS
Catalog Number: 25544
Epoch time:      08088
15152168   =   yrday
fracday
Element set:     911
Inclination:       51
6380  deg
RA of node:        74
1335  deg
Eccentricity:     
0000545     
Arg of perigee:   354
0524  deg
Mean anomaly:       6
0634  deg
Mean motion:   15
76534265  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1574
Checksum:              271


Coasting Arc #13 (Orbit 1589)
---------------------------------------

Vector Time (GMT): 2008/089/02:43:09
439
Vector Time (MET): N/A
Weight (LBS)     : 567143
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2272554
06                 A    =         6715212
40  meter
 Y    =        4240242
50  meter          E    =           
0007589
 Z    =        4680485
69                 I    =           51
92985
 XDOT =      -4548
896217                 Wp   =          113
47884
 YDOT =      -5550
480207  meter/sec      RA   =           68
54498  deg
 ZDOT =       2813
215107                 TA   =          308
86785
                                          MA   =          308
93554
                                          Ha   =            186
129  n
mi
                                          Hp   =            179
786

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7455886
03                 X    =        -2342537
16
 Y    =       13911556
74  feet           Y    =         4214438
23  meter
 Z    =       15355924
18                 Z    =         4669275
61
 XDOT =     -14924
200186                 XDOT =       -4500
157884
 YDOT =     -18210
236900  feet/sec       YDOT =       -5601
076036  meter/sec
 ZDOT =       9229
708357                 ZDOT =        2791
234999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5009311
46                 X    =        -1526838
13
 Y    =      -15011108
22  feet           Y    =        -4575385
79  meter
 Z    =       15313375
97                 Z    =         4667517
00
 XDOT =      22435
316041                 XDOT =        6838
284329
 YDOT =       1864
038981  feet/sec       YDOT =         568
159082  meter/sec
 ZDOT =       9144
807152                 ZDOT =        2787
337220


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   08089
16569537  
00020000  00000-0  20000-3 0  9129
2 25544  51
6391  68
9052 0000605 350
3532   9
7620 15
76621463 15909


Satellite: ISS
Catalog Number: 25544
Epoch time:      08089
16569537   =   yrday
fracday
Element set:     912
Inclination:       51
6391  deg
RA of node:        68
9052  deg
Eccentricity:     
0000605     
Arg of perigee:   350
3532  deg
Mean anomaly:       9
7620  deg
Mean motion:   15
76621463  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1590
Checksum:              290

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 may contain past, current and future orbital data 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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