Date: April 2nd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 1642)
---------------------------------------

Vector Time (GMT): 2008/092/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3957382
56                 A    =         6712498
33  meter
 Y    =        1573503
89  meter          E    =           
0004214
 Z    =        5186798
93                 I    =           51
87250
 XDOT =      -4051
009111                 Wp   =           38
94377
 YDOT =      -6459
373784  meter/sec      RA   =           51
24072  deg
 ZDOT =      -1127
542523                 TA   =           61
79523
                                          MA   =           61
75267
                                          Ha   =            185
724  n
mi
                                          Hp   =            179
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12983538
58                 X    =        -3999879
93
 Y    =        5162414
32  feet           Y    =         1529012
78  meter
 Z    =       17017056
85                 Z    =         5167470
83
 XDOT =     -13290
712308                 XDOT =       -3973
000955
 YDOT =     -21192
171206  feet/sec       YDOT =       -6504
238364  meter/sec
 ZDOT =      -3699
286494                 ZDOT =       -1147
032412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12896789
73                 X    =        -3930941
51
 Y    =        5604287
56  feet           Y    =         1708186
85  meter
 Z    =       16943075
14                 Z    =         5164249
30
 XDOT =     -13573
964892                 XDOT =       -4137
344499
 YDOT =     -19788
110338  feet/sec       YDOT =       -6031
416031  meter/sec
 ZDOT =      -3774
732195                 ZDOT =       -1150
538373


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   08092
52478759  
00020000  00000-0  20000-3 0  9005
2 25544  51
6381  51
6004 0001202 331
8903  28
2197 15
76824082 16430


Satellite: ISS
Catalog Number: 25544
Epoch time:      08092
52478759   =   yrday
fracday
Element set:     900
Inclination:       51
6381  deg
RA of node:        51
6004  deg
Eccentricity:     
0001202     
Arg of perigee:   331
8903  deg
Mean anomaly:      28
2197  deg
Mean motion:   15
76824082  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1643
Checksum:              277


Coasting Arc #2 (Orbit 1658)
---------------------------------------

Vector Time (GMT): 2008/093/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3265731
92                 A    =         6722314
47  meter
 Y    =        5550582
41  meter          E    =           
0014048
 Z    =        1902765
23                 I    =           51
88758
 XDOT =      -5127
059866                 Wp   =           62
67237
 YDOT =       1068
954170  meter/sec      RA   =           46
12774  deg
 ZDOT =       5656
025852                 TA   =          318
43577
                                          MA   =          318
54249
                                          Ha   =            185
471  n
mi
                                          Hp   =            179
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10714343
57                 X    =         3194178
50
 Y    =       18210572
23  feet           Y    =         5586701
74  meter
 Z    =        6242668
07                 Z    =         1918455
89
 XDOT =     -16821
062551                 XDOT =       -5166
107783
 YDOT =       3507
067488  feet/sec       YDOT =        1011
402484  meter/sec
 ZDOT =      18556
515261                 ZDOT =        5631
023860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11597097
10                 X    =         3534795
19
 Y    =       17639924
68  feet           Y    =         5376649
04  meter
 Z    =        6303443
49                 Z    =         1921289
58
 XDOT =     -15438
072193                 XDOT =       -4705
524404
 YDOT =       3523
369978  feet/sec       YDOT =        1073
923169  meter/sec
 ZDOT =      18460
714196                 ZDOT =        5626
825687


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   08093
53877605  
00020000  00000-0  20000-3 0  9011
2 25544  51
6385  46
3708 0001087 330
3242  29
7861 15
76907813 16592


Satellite: ISS
Catalog Number: 25544
Epoch time:      08093
53877605   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:        46
3708  deg
Eccentricity:     
0001087     
Arg of perigee:   330
3242  deg
Mean anomaly:      29
7861  deg
Mean motion:   15
76907813  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1659
Checksum:              305


Coasting Arc #3 (Orbit 1673)
---------------------------------------

Vector Time (GMT): 2008/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4988651
37                 A    =         6715227
88  meter
 Y    =        -343106
92  meter          E    =           
0008851
 Z    =       -4490674
19                 I    =           51
84279
 XDOT =       3296
190112                 Wp   =          104
50984
 YDOT =       6180
653021  meter/sec      RA   =           40
94481  deg
 ZDOT =       3192
516636                 TA   =          197
30689
                                          MA   =          197
33708
                                          Ha   =            185
514  n
mi
                                          Hp   =            179
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16366966
44                 X    =         5013932
08
 Y    =       -1125678
87  feet           Y    =         -287179
98  meter
 Z    =      -14733183
05                 Z    =        -4466377
99
 XDOT =      10814
272022                 XDOT =        3211
323496
 YDOT =      20277
733009  feet/sec       YDOT =        6217
038649  meter/sec
 ZDOT =      10474
135944                 ZDOT =        3208
322822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16334902
79                 X    =         4978878
37
 Y    =       -2247738
95  feet           Y    =         -685110
83  meter
 Z    =      -14640015
26                 Z    =        -4462276
65
 XDOT =      11951
958975                 XDOT =        3642
957095
 YDOT =      18303
792935  feet/sec       YDOT =        5578
996086  meter/sec
 ZDOT =      10535
418679                 ZDOT =        3211
195613


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   08094
48936426  
00020000  00000-0  20000-3 0  9024
2 25544  51
6389  41
4677 0001264 335
4058  24
7046 15
76910231 16740


Satellite: ISS
Catalog Number: 25544
Epoch time:      08094
48936426   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:        41
4677  deg
Eccentricity:     
0001264     
Arg of perigee:   335
4058  deg
Mean anomaly:      24
7046  deg
Mean motion:   15
76910231  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1674
Checksum:              296


Coasting Arc #4 (Orbit 1689)
---------------------------------------

Vector Time (GMT): 2008/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2348450
61                 A    =         6718041
29  meter
 Y    =       -5175947
10  meter          E    =           
0005378
 Z    =       -3587564
08                 I    =           51
83127
 XDOT =       6282
029541                 Wp   =           67
23859
 YDOT =        228
448153  meter/sec      RA   =           35
85010  deg
 ZDOT =      -4445
079914                 TA   =          155
52022
                                          MA   =          155
49468
                                          Ha   =            185
400  n
mi
                                          Hp   =            179
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7704890
45                 X    =        -2272970
05
 Y    =      -16981453
73  feet           Y    =        -5201787
11  meter
 Z    =      -11770223
35                 Z    =        -3598789
05
 XDOT =      20610
333140                 XDOT =        6300
601535
 YDOT =        749
501814  feet/sec       YDOT =         298
800833  meter/sec
 ZDOT =     -14583
595517                 ZDOT =       -4414
516679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9062236
07                 X    =        -2762169
55
 Y    =      -16265999
17  feet           Y    =        -4957876
55  meter
 Z    =      -11813822
99                 Z    =        -3600853
25
 XDOT =      19494
961974                 XDOT =        5942
064410
 YDOT =       -362
071970  feet/sec       YDOT =        -110
359536  meter/sec
 ZDOT =     -14466
330889                 ZDOT =       -4409
337655


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   08095
50329350  
00020000  00000-0  20000-3 0  9031
2 25544  51
6399  36
2376 0001279 339
5636  20
5478 15
76985200 16901


Satellite: ISS
Catalog Number: 25544
Epoch time:      08095
50329350   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:        36
2376  deg
Eccentricity:     
0001279     
Arg of perigee:   339
5636  deg
Mean anomaly:      20
5478  deg
Mean motion:   15
76985200  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1690
Checksum:              304


Coasting Arc #5 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2008/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5911937
39                 A    =         6719419
93  meter
 Y    =        -655724
15  meter          E    =           
0012660
 Z    =        3114954
98                 I    =           51
81226
 XDOT =      -1959
360782                 Wp   =           89
46284
 YDOT =      -5629
375243  meter/sec      RA   =           30
65429  deg
 ZDOT =      -4886
659190                 TA   =           54
36354
                                          MA   =           54
24569
                                          Ha   =            185
414  n
mi
                                          Hp   =            179
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19396120
06                 X    =        -5919297
61
 Y    =       -2151325
96  feet           Y    =         -721875
69  meter
 Z    =       10219668
56                 Z    =         3086216
74
 XDOT =      -6428
349023                 XDOT =       -1872
527905
 YDOT =     -18469
078881  feet/sec       YDOT =       -5650
800862  meter/sec
 ZDOT =     -16032
346423                 ZDOT =       -4895
966422

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19571907
37                 X    =        -5965517
37
 Y    =        -143094
07  feet           Y    =          -43615
07  meter
 Z    =       10109365
37                 Z    =         3081334
56
 XDOT =      -8209
975929                 XDOT =       -2502
400663
 YDOT =     -16293
778807  feet/sec       YDOT =       -4966
343780  meter/sec
 ZDOT =     -16068
630811                 ZDOT =       -4897
718671


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   08096
51719147  
00020000  00000-0  20000-3 0  9041
2 25544  51
6406  31
0079 0001288 340
8576  19
2540 15
77032646 17062


Satellite: ISS
Catalog Number: 25544
Epoch time:      08096
51719147   =   yrday
fracday
Element set:     904
Inclination:       51
6406  deg
RA of node:        31
0079  deg
Eccentricity:     
0001288     
Arg of perigee:   340
8576  deg
Mean anomaly:      19
2540  deg
Mean motion:   15
77032646  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1706
Checksum:              285


Coasting Arc #6 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2008/097/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         947110
09                 A    =         6713373
08  meter
 Y    =        4620864
95  meter          E    =           
0006328
 Z    =        4773060
26                 I    =           51
76748
 XDOT =      -7171
217033                 Wp   =          113
31736
 YDOT =      -1186
898133  meter/sec      RA   =           25
55167  deg
 ZDOT =       2566
895941                 TA   =          311
57358
                                          MA   =          311
62781
                                          Ha   =            185
192  n
mi
                                          Hp   =            179
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3107316
58                 X    =          872181
48
 Y    =       15160318
07  feet           Y    =         4631037
46  meter
 Z    =       15659646
53                 Z    =         4777479
06
 XDOT =     -23527
614938                 XDOT =       -7169
881660
 YDOT =      -3894
022747  feet/sec       YDOT =       -1267
083135  meter/sec
 ZDOT =       8421
574610                 ZDOT =        2532
061019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4811968
47                 X    =         1466687
99
 Y    =       14689780
86  feet           Y    =         4477445
21  meter
 Z    =       15677068
85                 Z    =         4778370
59
 XDOT =     -22800
518667                 XDOT =       -6949
598090
 YDOT =      -1393
969361  feet/sec       YDOT =        -424
881861  meter/sec
 ZDOT =       8287
837029                 ZDOT =        2526
132727


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   08097
53105660  
00020000  00000-0  20000-3 0  9054
2 25544  51
6411  25
7783 0001198 335
8973  24
2136 15
77106154 17226


Satellite: ISS
Catalog Number: 25544
Epoch time:      08097
53105660   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:        25
7783  deg
Eccentricity:     
0001198     
Arg of perigee:   335
8973  deg
Mean anomaly:      24
2136  deg
Mean motion:   15
77106154  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1722
Checksum:              282


Coasting Arc #7 (Orbit 1736)
---------------------------------------

Vector Time (GMT): 2008/098/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6461172
66                 A    =         6722691
78  meter
 Y    =        1342137
69  meter          E    =           
0010033
 Z    =       -1257796
87                 I    =           51
77167
 XDOT =        104
614556                 Wp   =           30
94686
 YDOT =       4979
395104  meter/sec      RA   =           20
36990  deg
 ZDOT =       5879
722808                 TA   =          315
26437
                                          MA   =          315
34525
                                          Ha   =            185
289  n
mi
                                          Hp   =            179
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21198073
05                 X    =         6451794
71
 Y    =        4403338
89  feet           Y    =         1414337
73  meter
 Z    =       -4126630
16                 Z    =        -1226430
80
 XDOT =        343
223609                 XDOT =          20
363292
 YDOT =      16336
598109  feet/sec       YDOT =        4980
094128  meter/sec
 ZDOT =      19290
429160                 ZDOT =        5880
026183

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21624038
65                 X    =         6591006
98
 Y    =        1458832
16  feet           Y    =          444652
04  meter
 Z    =       -4006186
73                 Z    =        -1221085
72
 XDOT =       2572
751514                 XDOT =         784
174661
 YDOT =      14574
155687  feet/sec       YDOT =        4442
202653  meter/sec
 ZDOT =      19292
094998                 ZDOT =        5880
230555


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   08098
48152890  
00020000  00000-0  20000-3 0  9067
2 25544  51
6410  20
8747 0001315 343
1246  16
9875 15
77107855 17370


Satellite: ISS
Catalog Number: 25544
Epoch time:      08098
48152890   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:        20
8747  deg
Eccentricity:     
0001315     
Arg of perigee:   343
1246  deg
Mean anomaly:      16
9875  deg
Mean motion:   15
77107855  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1737
Checksum:              299


Coasting Arc #8 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2008/099/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         849327
59                 A    =         6711085
10  meter
 Y    =       -4082303
98  meter          E    =           
0014850
 Z    =       -5271200
31                 I    =           51
70606
 XDOT =       7466
844788                 Wp   =           83
37948
 YDOT =       1847
600473  meter/sec      RA   =           15
23124  deg
 ZDOT =       -226
643595                 TA   =          184
46330
                                          MA   =          184
47656
                                          Ha   =            185
173  n
mi
                                          Hp   =            179
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2786507
83                 X    =          920520
39
 Y    =      -13393385
76  feet           Y    =        -4072408
29  meter
 Z    =      -17293964
27                 Z    =        -5266901
25
 XDOT =      24497
522271                 XDOT =        7446
730688
 YDOT =       6061
681341  feet/sec       YDOT =        1930
986533  meter/sec
 ZDOT =       -743
581349                 ZDOT =        -190
417932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         790140
32                 X    =          240834
77
 Y    =      -13677687
95  feet           Y    =        -4168959
29  meter
 Z    =      -17277880
05                 Z    =        -5266297
84
 XDOT =      24144
776486                 XDOT =        7359
327873
 YDOT =       2163
070580  feet/sec       YDOT =         659
303913  meter/sec
 ZDOT =       -604
449926                 ZDOT =        -184
236338


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   08099
49533410  
00020000  00000-0  20000-3 0  9071
2 25544  51
6417  15
6440 0001264 346
3708  13
7423 15
77172773 17533


Satellite: ISS
Catalog Number: 25544
Epoch time:      08099
49533410   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:        15
6440  deg
Eccentricity:     
0001264     
Arg of perigee:   346
3708  deg
Mean anomaly:      13
7423  deg
Mean motion:   15
77172773  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1753
Checksum:              286


Coasting Arc #9 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2008/100/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6398627
02                 A    =         6722702
86  meter
 Y    =       -1848399
48  meter          E    =           
0008987
 Z    =        -886302
82                 I    =           51
71740
 XDOT =       2093
355203                 Wp   =          137
80840
 YDOT =      -4407
429856  meter/sec      RA   =           10
08379  deg
 ZDOT =      -5962
386528                 TA   =           51
86586
                                          MA   =           51
78489
                                          Ha   =            185
106  n
mi
                                          Hp   =            178
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20992870
82                 X    =        -6373176
82
 Y    =       -6064302
77  feet           Y    =        -1919810
27  meter
 Z    =       -2907817
65                 Z    =         -917325
98
 XDOT =       6867
963266                 XDOT =        2171
448762
 YDOT =     -14460
071705  feet/sec       YDOT =       -4383
583986  meter/sec
 ZDOT =     -19561
635590                 ZDOT =       -5952
027281

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21703564
08                 X    =        -6615246
33
 Y    =       -2392572
72  feet           Y    =         -729256
17  meter
 Z    =       -3026994
97                 Z    =         -922628
07
 XDOT =       4232
208344                 XDOT =        1289
977103
 YDOT =     -13856
908291  feet/sec       YDOT =       -4223
585647  meter/sec
 ZDOT =     -19522
332026                 ZDOT =       -5950
406802


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   08100
50910791  
00020000  00000-0  20000-3 0  9088
2 25544  51
6421  10
4133 0001210 346
3305  13
7827 15
77203966 17698


Satellite: ISS
Catalog Number: 25544
Epoch time:      08100
50910791   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:        10
4133  deg
Eccentricity:     
0001210     
Arg of perigee:   346
3305  deg
Mean anomaly:      13
7827  deg
Mean motion:   15
77203966  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1769
Checksum:              258


Coasting Arc #10 (Orbit 1784)
---------------------------------------

Vector Time (GMT): 2008/101/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2786628
31                 A    =         6712435
10  meter
 Y    =        3647442
06  meter          E    =           
0007143
 Z    =        4894883
39                 I    =           51
65384
 XDOT =      -6995
305762                 Wp   =           47
07548
 YDOT =      -2359
990789  meter/sec      RA   =            4
90039  deg
 ZDOT =      -2217
020064                 TA   =           64
47506
                                          MA   =           64
40121
                                          Ha   =            185
088  n
mi
                                          Hp   =            178
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9142481
32                 X    =        -2850986
10
 Y    =       11966673
41  feet           Y    =         3615920
36  meter
 Z    =       16059328
69                 Z    =         4881189
65
 XDOT =     -22950
478222                 XDOT =       -6957
626103
 YDOT =      -7742
751931  feet/sec       YDOT =       -2438
005531  meter/sec
 ZDOT =      -7273
687874                 ZDOT =       -2250
912087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6823021
03                 X    =        -2079656
81
 Y    =       13487239
96  feet           Y    =         4110910
74  meter
 Z    =       16007155
20                 Z    =         4878980
91
 XDOT =     -22971
499272                 XDOT =       -7001
712978
 YDOT =      -2807
134090  feet/sec       YDOT =        -855
614471  meter/sec
 ZDOT =      -7403
922794                 ZDOT =       -2256
715668


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   08101
52284927  
00020000  00000-0  20000-3 0  9097
2 25544  51
6416   5
1826 0001337 347
9129  12
2004 15
77286378 17850


Satellite: ISS
Catalog Number: 25544
Epoch time:      08101
52284927   =   yrday
fracday
Element set:     909
Inclination:       51
6416  deg
RA of node:         5
1826  deg
Eccentricity:     
0001337     
Arg of perigee:   347
9129  deg
Mean anomaly:      12
2004  deg
Mean motion:   15
77286378  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1785
Checksum:              289


Coasting Arc #11 (Orbit 1800)
---------------------------------------

Vector Time (GMT): 2008/102/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5606451
95                 A    =         6719023
51  meter
 Y    =        2277198
24  meter          E    =           
0013432
 Z    =        2904919
52                 I    =           51
64763
 XDOT =      -4245
375320                 Wp   =           76
45510
 YDOT =       4003
235173  meter/sec      RA   =          359
78233  deg
 ZDOT =       5039
040558                 TA   =          317
03912
                                          MA   =          317
14393
                                          Ha   =            184
961  n
mi
                                          Hp   =            178
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18393871
21                 X    =         5566459
67
 Y    =        7471122
83  feet           Y    =         2339669
07  meter
 Z    =        9530575
87                 Z    =         2932058
67
 XDOT =     -13928
396719                 XDOT =       -4314
303391
 YDOT =      13133
973666  feet/sec       YDOT =        3955
375369  meter/sec
 ZDOT =      16532
285295                 ZDOT =        5018
249211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19480026
18                 X    =         5937511
98
 Y    =        3561076
39  feet           Y    =         1085416
08  meter
 Z    =        9634903
51                 Z    =         2936718
59
 XDOT =     -10778
767584                 XDOT =       -3285
368360
 YDOT =      14304
386510  feet/sec       YDOT =        4359
977008  meter/sec
 ZDOT =      16452
915779                 ZDOT =        5014
848730


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   08102
53656081  
00020000  00000-0  20000-3 0  9105
2 25544  51
6420 359
9508 0001318 352
6244   7
4901 15
77306937 18017


Satellite: ISS
Catalog Number: 25544
Epoch time:      08102
53656081   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:       359
9508  deg
Eccentricity:     
0001318     
Arg of perigee:   352
6244  deg
Mean anomaly:       7
4901  deg
Mean motion:   15
77306937  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1801
Checksum:              274


Coasting Arc #12 (Orbit 1815)
---------------------------------------

Vector Time (GMT): 2008/103/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4517571
85                 A    =         6716798
10  meter
 Y    =       -3353009
08  meter          E    =           
0005364
 Z    =       -3673659
41                 I    =           51
61175
 XDOT =       5669
644448                 Wp   =           86
42328
 YDOT =       2904
492046  meter/sec      RA   =          354
57016  deg
 ZDOT =       4326
830625                 TA   =          229
34688
                                          MA   =          229
39352
                                          Ha   =            184
944  n
mi
                                          Hp   =            178
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14821429
94                 X    =         4572575
89
 Y    =      -11000685
95  feet           Y    =        -3302183
37  meter
 Z    =      -12052688
36                 Z    =        -3651579
59
 XDOT =      18601
195697                 XDOT =        5615
725679
 YDOT =       9529
173379  feet/sec       YDOT =        2967
591661  meter/sec
 ZDOT =      14195
638535                 ZDOT =        4354
242794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12084671
11                 X    =         3683407
76
 Y    =      -14024173
19  feet           Y    =        -4274567
99  meter
 Z    =      -11968310
83                 Z    =        -3647941
14
 XDOT =      19147
710649                 XDOT =        5836
222206
 YDOT =       4311
182025  feet/sec       YDOT =        1314
048281  meter/sec
 ZDOT =      14301
078658                 ZDOT =        4358
968775


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   08103
48688558  
00020000  00000-0  20000-3 0  9115
2 25544  51
6425 355
0462 0001343 351
1093   9
0048 15
77368117 18166


Satellite: ISS
Catalog Number: 25544
Epoch time:      08103
48688558   =   yrday
fracday
Element set:     911
Inclination:       51
6425  deg
RA of node:       355
0462  deg
Eccentricity:     
0001343     
Arg of perigee:   351
1093  deg
Mean anomaly:       9
0048  deg
Mean motion:   15
77368117  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1816
Checksum:              283

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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