Date: October 30th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 3180)
---------------------------------------

Vector Time (GMT): 2007/301/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2894768
79                 A    =         6714824
90  meter
 Y    =        2981862
02  meter          E    =           
0016736
 Z    =       -5288441
31                 I    =           51
83887
 XDOT =      -5498
379451                 Wp   =           97
19144
 YDOT =       5378
826076  meter/sec      RA   =          135
50593  deg
 ZDOT =         21
148259                 TA   =          173
02059
                                          MA   =          172
99725
                                          Ha   =            187
925  n
mi
                                          Hp   =            180
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9497272
92                 X    =         2886901
09
 Y    =        9783011
89  feet           Y    =         3014189
30  meter
 Z    =      -17350529
24                 Z    =        -5274397
02
 XDOT =     -18039
302662                 XDOT =       -5558
220376
 YDOT =      17647
067180  feet/sec       YDOT =        5317
005497  meter/sec
 ZDOT =         69
384051                 ZDOT =          -5
708724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13539234
22                 X    =        -4126758
59
 Y    =       -2111405
55  feet           Y    =         -643556
41  meter
 Z    =      -17296747
76                 Z    =        -5272048
72
 XDOT =       3766
331414                 XDOT =        1147
977815
 YDOT =     -23942
012927  feet/sec       YDOT =       -7297
525540  meter/sec
 ZDOT =        -32
109022                 ZDOT =          -9
786830


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   07301
51860703  
00020000  00000-0  20000-3 0  9000
2 25544  51
6333 136
3465 0002555 142
7217 217
4124 15
75854970 31817


Satellite: ISS
Catalog Number: 25544
Epoch time:      07301
51860703   =   yrday
fracday
Element set:     900
Inclination:       51
6333  deg
RA of node:       136
3465  deg
Eccentricity:     
0002555     
Arg of perigee:   142
7217  deg
Mean anomaly:     217
4124  deg
Mean motion:   15
75854970  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3181
Checksum:              269


Coasting Arc #2 (Orbit 3196)
---------------------------------------

Vector Time (GMT): 2007/302/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4717165
45                 A    =         6726584
14  meter
 Y    =       -4740063
37  meter          E    =           
0013216
 Z    =        -666485
96                 I    =           51
89941
 XDOT =       2968
901914                 Wp   =          141
07975
 YDOT =       3789
995531  meter/sec      RA   =          130
37912  deg
 ZDOT =      -6015
626334                 TA   =           46
16024
                                          MA   =           46
05109
                                          Ha   =            187
810  n
mi
                                          Hp   =            180
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15476264
62                 X    =         4773056
71
 Y    =      -15551389
00  feet           Y    =        -4687000
80  meter
 Z    =       -2186633
72                 Z    =         -643433
99
 XDOT =       9740
491845                 XDOT =        2955
524498
 YDOT =      12434
368541  feet/sec       YDOT =        3823
121117  meter/sec
 ZDOT =     -19736
306869                 ZDOT =       -6001
235270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2752792
56                 X    =         -839051
17
 Y    =       21775123
31  feet           Y    =         6637057
58  meter
 Z    =       -2099516
93                 Z    =         -639932
76
 XDOT =     -13809
408423                 XDOT =       -4209
107687
 YDOT =      -3619
012829  feet/sec       YDOT =       -1103
075110  meter/sec
 ZDOT =     -19681
105953                 ZDOT =       -5998
801095


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   07302
53323267  
00020000  00000-0  20000-3 0  9013
2 25544  51
6340 131
1212 0002403 145
4878 214
6443 15
75905349 31970


Satellite: ISS
Catalog Number: 25544
Epoch time:      07302
53323267   =   yrday
fracday
Element set:     901
Inclination:       51
6340  deg
RA of node:       131
1212  deg
Eccentricity:     
0002403     
Arg of perigee:   145
4878  deg
Mean anomaly:     214
6443  deg
Mean motion:   15
75905349  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3197
Checksum:              265


Coasting Arc #3 (Orbit 3212)
---------------------------------------

Vector Time (GMT): 2007/303/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2331925
43                 A    =         6715393
61  meter
 Y    =       -3661800
40  meter          E    =           
0004984
 Z    =        5119319
52                 I    =           51
87905
 XDOT =       5263
103872                 Wp   =           84
90885
 YDOT =      -5431
687432  meter/sec      RA   =          125
22722  deg
 ZDOT =      -1486
149951                 TA   =           19
28723
                                          MA   =           19
26838
                                          Ha   =            187
857  n
mi
                                          Hp   =            180
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7650673
98                 X    =        -2315674
50
 Y    =      -12013780
83  feet           Y    =        -3687786
80  meter
 Z    =       16795667
70                 Z    =         5108030
03
 XDOT =      17267
401154                 XDOT =        5330
670232
 YDOT =     -17820
496824  feet/sec       YDOT =       -5372
454540  meter/sec
 ZDOT =      -4875
820049                 ZDOT =       -1460
417574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13553260
89                 X    =         4131033
92
 Y    =        4541858
21  feet           Y    =         1384358
38  meter
 Z    =       16752278
63                 Z    =         5106094
53
 XDOT =      -2039
357205                 XDOT =        -621
596076
 YDOT =      23731
158414  feet/sec       YDOT =        7233
257084  meter/sec
 ZDOT =      -4778
572819                 ZDOT =       -1456
508995


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   07303
54783665  
00020000  00000-0  20000-3 0  9028
2 25544  51
6336 125
8946 0002531 151
3153 208
8151 15
75898087 32133


Satellite: ISS
Catalog Number: 25544
Epoch time:      07303
54783665   =   yrday
fracday
Element set:     902
Inclination:       51
6336  deg
RA of node:       125
8946  deg
Eccentricity:     
0002531     
Arg of perigee:   151
3153  deg
Mean anomaly:     208
8151  deg
Mean motion:   15
75898087  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3213
Checksum:              293


Coasting Arc #4 (Orbit 3228)
---------------------------------------

Vector Time (GMT): 2007/304/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4442180
44                 A    =         6725058
59  meter
 Y    =        4663034
01  meter          E    =           
0014473
 Z    =        1917375
43                 I    =           51
92753
 XDOT =      -2422
422200                 Wp   =           77
29122
 YDOT =      -4644
420261  meter/sec      RA   =          120
12443  deg
 ZDOT =       5650
510986                 TA   =          303
96016
                                          MA   =          304
09763
                                          Ha   =            187
669  n
mi
                                          Hp   =            180
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14574082
81                 X    =        -4503307
43
 Y    =       15298668
01  feet           Y    =         4613017
15  meter
 Z    =        6290601
80                 Z    =         1895646
79
 XDOT =      -7947
579396                 XDOT =       -2397
757097
 YDOT =     -15237
599281  feet/sec       YDOT =       -4671
371559  meter/sec
 ZDOT =      18538
421871                 ZDOT =        5638
802350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1486585
10                 X    =          453111
14
 Y    =      -21101412
61  feet           Y    =        -6431710
56  meter
 Z    =        6208482
47                 Z    =         1892345
46
 XDOT =      14383
907217                 XDOT =        4384
214920
 YDOT =       6486
144156  feet/sec       YDOT =        1976
976739  meter/sec
 ZDOT =      18493
317835                 ZDOT =        5636
763276


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   07304
56241612  
00020000  00000-0  20000-3 0  9033
2 25544  51
6334 120
6677 0002546 154
7671 205
3617 15
75958598 32293


Satellite: ISS
Catalog Number: 25544
Epoch time:      07304
56241612   =   yrday
fracday
Element set:     903
Inclination:       51
6334  deg
RA of node:       120
6677  deg
Eccentricity:     
0002546     
Arg of perigee:   154
7671  deg
Mean anomaly:     205
3617  deg
Mean motion:   15
75958598  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3229
Checksum:              298


Coasting Arc #5 (Orbit 3243)
---------------------------------------

Vector Time (GMT): 2007/305/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1938944
84                 A    =         6717169
17  meter
 Y    =        4461050
03  meter          E    =           
0012675
 Z    =       -4644818
48                 I    =           51
91528
 XDOT =      -4912
025098                 Wp   =          118
45061
 YDOT =       5159
705002  meter/sec      RA   =          114
95382  deg
 ZDOT =       2905
131006                 TA   =          180
21787
                                          MA   =          180
21842
                                          Ha   =            187
583  n
mi
                                          Hp   =            180
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6361367
58                 X    =         1911480
55
 Y    =       14635990
92  feet           Y    =         4482579
02  meter
 Z    =      -15238905
76                 Z    =        -4635465
53
 XDOT =     -16115
567908                 XDOT =       -4983
469388
 YDOT =      16928
166018  feet/sec       YDOT =        5104
376389  meter/sec
 ZDOT =       9531
269704                 ZDOT =        2881
094753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14424121
63                 X    =        -4396472
27
 Y    =       -6908221
46  feet           Y    =        -2105625
90  meter
 Z    =      -15202784
88                 Z    =        -4633808
83
 XDOT =        742
064986                 XDOT =         226
181408
 YDOT =     -22324
357812  feet/sec       YDOT =       -6804
464261  meter/sec
 ZDOT =       9440
419051                 ZDOT =        2877
439727


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   07305
51356371  
00020000  00000-0  20000-3 0  9049
2 25544  51
6339 115
7678 0002617 156
2582 203
8703 15
75994051 32441


Satellite: ISS
Catalog Number: 25544
Epoch time:      07305
51356371   =   yrday
fracday
Element set:     904
Inclination:       51
6339  deg
RA of node:       115
7678  deg
Eccentricity:     
0002617     
Arg of perigee:   156
2582  deg
Mean anomaly:     203
8703  deg
Mean motion:   15
75994051  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3244
Checksum:              292


Coasting Arc #6 (Orbit 3259)
---------------------------------------

Vector Time (GMT): 2007/306/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4146401
18                 A    =         6722148
57  meter
 Y    =       -4267559
56  meter          E    =           
0006293
 Z    =       -3128311
65                 I    =           51
94388
 XDOT =       2057
237575                 Wp   =          122
40132
 YDOT =       5578
161290  meter/sec      RA   =          109
87020  deg
 ZDOT =      -4893
216679                 TA   =           93
82638
                                          MA   =           93
75443
                                          Ha   =            187
483  n
mi
                                          Hp   =            180
308

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13603678
40                 X    =         4209010
45
 Y    =      -14001179
67  feet           Y    =        -4220842
05  meter
 Z    =      -10263489
66                 Z    =        -3108016
19
 XDOT =       6749
467110                 XDOT =        2018
479467
 YDOT =      18301
054100  feet/sec       YDOT =        5600
949852  meter/sec
 ZDOT =     -16053
860494                 ZDOT =       -4883
316565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -912982
53                 X    =         -278277
07
 Y    =       19540437
06  feet           Y    =         5955925
22  meter
 Z    =      -10186761
05                 Z    =        -3104924
77
 XDOT =     -15843
801844                 XDOT =       -4829
190802
 YDOT =      -9071
524865  feet/sec       YDOT =       -2765
000779  meter/sec
 ZDOT =     -16015
523482                 ZDOT =       -4881
531557


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   07306
52809733  
00020000  00000-0  20000-3 0  9057
2 25544  51
6342 110
5418 0002451 157
8305 202
2965 15
76049105 32609


Satellite: ISS
Catalog Number: 25544
Epoch time:      07306
52809733   =   yrday
fracday
Element set:     905
Inclination:       51
6342  deg
RA of node:       110
5418  deg
Eccentricity:     
0002451     
Arg of perigee:   157
8305  deg
Mean anomaly:     202
2965  deg
Mean motion:   15
76049105  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3260
Checksum:              268


Coasting Arc #7 (Orbit 3275)
---------------------------------------

Vector Time (GMT): 2007/307/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1712581
76                 A    =         6720031
81  meter
 Y    =       -5250945
69  meter          E    =           
0012091
 Z    =        3817003
78                 I    =           51
94470
 XDOT =       4590
073707                 Wp   =           94
00002
 YDOT =      -4555
010500  meter/sec      RA   =          104
68906  deg
 ZDOT =      -4196
284611                 TA   =           39
77824
                                          MA   =           39
68965
                                          Ha   =            187
450  n
mi
                                          Hp   =            180
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5618706
57                 X    =        -1672280
17
 Y    =      -17227512
10  feet           Y    =        -5269871
40  meter
 Z    =       12522978
30                 Z    =         3808781
86
 XDOT =      15059
296940                 XDOT =        4661
052436
 YDOT =     -14944
260170  feet/sec       YDOT =       -4503
284842  meter/sec
 ZDOT =     -13767
337962                 ZDOT =       -4173
813322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15849708
52                 X    =         4830991
16
 Y    =        8828476
95  feet           Y    =         2690919
77  meter
 Z    =       12491067
07                 Z    =         3807277
24
 XDOT =       -380
396919                 XDOT =        -115
944981
 YDOT =      20090
328485  feet/sec       YDOT =        6123
532122  meter/sec
 ZDOT =     -13682
357396                 ZDOT =       -4170
382534


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   07307
54260772  
00020000  00000-0  20000-3 0  9065
2 25544  51
6335 105
3146 0002535 164
0789 196
0455 15
76047403 32760


Satellite: ISS
Catalog Number: 25544
Epoch time:      07307
54260772   =   yrday
fracday
Element set:     906
Inclination:       51
6335  deg
RA of node:       105
3146  deg
Eccentricity:     
0002535     
Arg of perigee:   164
0789  deg
Mean anomaly:     196
0455  deg
Mean motion:   15
76047403  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3276
Checksum:              287


Coasting Arc #8 (Orbit 3291)
---------------------------------------

Vector Time (GMT): 2007/308/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3886597
98                 A    =         6718776
68  meter
 Y    =        3598314
32  meter          E    =           
0011804
 Z    =        4128177
07                 I    =           51
94786
 XDOT =      -1917
726784                 Wp   =          115
44312
 YDOT =      -6431
653280  meter/sec      RA   =           99
61015  deg
 ZDOT =       3787
324527                 TA   =          295
87914
                                          MA   =          296
00079
                                          Ha   =            187
276  n
mi
                                          Hp   =            180
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12751305
70                 X    =        -3946600
28
 Y    =       11805493
18  feet           Y    =         3554516
75  meter
 Z    =       13543888
04                 Z    =         4109149
87
 XDOT =      -6291
754540                 XDOT =       -1864
062981
 YDOT =     -21101
224671  feet/sec       YDOT =       -6452
798286  meter/sec
 ZDOT =      12425
605402                 ZDOT =        3778
138494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1150331
33                 X    =          350620
99
 Y    =      -17395030
70  feet           Y    =        -5302005
36  meter
 Z    =       13471897
20                 Z    =         4106234
27
 XDOT =      17888
828375                 XDOT =        5452
514889
 YDOT =      10812
550741  feet/sec       YDOT =        3295
665466  meter/sec
 ZDOT =      12389
888358                 ZDOT =        3776
437972


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   07308
55709205  
00020000  00000-0  20000-3 0  9077
2 25544  51
6341 100
0876 0002521 169
0987 191
0232 15
76128009 32927


Satellite: ISS
Catalog Number: 25544
Epoch time:      07308
55709205   =   yrday
fracday
Element set:     907
Inclination:       51
6341  deg
RA of node:       100
0876  deg
Eccentricity:     
0002521     
Arg of perigee:   169
0987  deg
Mean anomaly:     191
0232  deg
Mean motion:   15
76128009  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3292
Checksum:              276


Coasting Arc #9 (Orbit 3306)
---------------------------------------

Vector Time (GMT): 2007/309/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1668448
22                 A    =         6722895
92  meter
 Y    =        5922749
42  meter          E    =           
0004515
 Z    =       -2711754
33                 I    =           51
96665
 XDOT =      -4367
485988                 Wp   =           86
90441
 YDOT =       3612
177240  meter/sec      RA   =           94
43252  deg
 ZDOT =       5209
836457                 TA   =          242
29858
                                          MA   =          242
34440
                                          Ha   =            187
161  n
mi
                                          Hp   =            180
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5473911
48                 X    =         1615268
63
 Y    =       19431592
59  feet           Y    =         5941109
56  meter
 Z    =       -8896831
79                 Z    =        -2703778
11
 XDOT =     -14329
022270                 XDOT =       -4432
862273
 YDOT =      11850
975197  feet/sec       YDOT =        3562
972089  meter/sec
 ZDOT =      17092
639296                 ZDOT =        5188
459900

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17573310
33                 X    =        -5356344
99
 Y    =       -9963972
71  feet           Y    =        -3037018
88  meter
 Z    =       -8865783
95                 Z    =        -2702290
95
 XDOT =       1230
469994                 XDOT =         375
047254
 YDOT =     -17284
542505  feet/sec       YDOT =       -5268
328556  meter/sec
 ZDOT =      17011
704088                 ZDOT =        5185
167406


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   07309
50815062  
00020000  00000-0  20000-3 0  9083
2 25544  51
6352  95
1877 0002479 169
3979 190
7238 15
76143727 33073


Satellite: ISS
Catalog Number: 25544
Epoch time:      07309
50815062   =   yrday
fracday
Element set:     908
Inclination:       51
6352  deg
RA of node:        95
1877  deg
Eccentricity:     
0002479     
Arg of perigee:   169
3979  deg
Mean anomaly:     190
7238  deg
Mean motion:   15
76143727  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3307
Checksum:              318


Coasting Arc #10 (Orbit 3322)
---------------------------------------

Vector Time (GMT): 2007/310/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3793812
03                 A    =         6715665
02  meter
 Y    =       -2637228
52  meter          E    =           
0012045
 Z    =       -4884289
59                 I    =           51
94387
 XDOT =       1912
528306                 Wp   =           84
01355
 YDOT =       7077
183092  meter/sec      RA   =           89
34447  deg
 ZDOT =      -2339
400627                 TA   =          163
29526
                                          MA   =          163
25555
                                          Ha   =            187
031  n
mi
                                          Hp   =            180
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12446889
85                 X    =         3846747
55
 Y    =       -8652324
55  feet           Y    =        -2594508
05  meter
 Z    =      -16024572
13                 Z    =        -4865730
16
 XDOT =       6274
699167                 XDOT =        1844
612709
 YDOT =      23219
104633  feet/sec       YDOT =        7098
190304  meter/sec
 ZDOT =      -7675
198907                 ZDOT =       -2330
274384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2599414
22                 X    =         -792301
45
 Y    =       15009328
62  feet           Y    =         4574843
36  meter
 Z    =      -15954240
79                 Z    =        -4862852
59
 XDOT =     -19907
805957                 XDOT =       -6067
899256
 YDOT =     -11555
505281  feet/sec       YDOT =       -3522
118010  meter/sec
 ZDOT =      -7639
647847                 ZDOT =       -2328
564664


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   07310
52258782  
00020000  00000-0  20000-3 0  9098
2 25544  51
6355  89
9612 0002324 173
2185 186
9011 15
76188435 33235


Satellite: ISS
Catalog Number: 25544
Epoch time:      07310
52258782   =   yrday
fracday
Element set:     909
Inclination:       51
6355  deg
RA of node:        89
9612  deg
Eccentricity:     
0002324     
Arg of perigee:   173
2185  deg
Mean anomaly:     186
9011  deg
Mean motion:   15
76188435  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3323
Checksum:              295


Coasting Arc #11 (Orbit 3338)
---------------------------------------

Vector Time (GMT): 2007/311/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1691726
03                 A    =         6725131
37  meter
 Y    =       -6363465
18  meter          E    =           
0015352
 Z    =        1327357
37                 I    =           51
97425
 XDOT =       4374
969558                 Wp   =          127
77367
 YDOT =      -2396
458453  meter/sec      RA   =           84
18246  deg
 ZDOT =      -5876
326429                 TA   =           37
69777
                                          MA   =           37
59030
                                          Ha   =            186
928  n
mi
                                          Hp   =            180
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5550282
25                 X    =        -1626891
32
 Y    =      -20877510
42  feet           Y    =        -6382020
51  meter
 Z    =        4354847
02                 Z    =         1319296
21
 XDOT =      14353
574665                 XDOT =        4429
988933
 YDOT =      -7862
396498  feet/sec       YDOT =       -2347
227433  meter/sec
 ZDOT =     -19279
286183                 ZDOT =       -5854
938554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18990245
47                 X    =         5788226
82
 Y    =       10311120
12  feet           Y    =         3142829
41  meter
 Z    =        4323441
43                 Z    =         1317784
95
 XDOT =      -3486
294216                 XDOT =       -1062
622477
 YDOT =      14521
237549  feet/sec       YDOT =        4426
073205  meter/sec
 ZDOT =     -19198
157465                 ZDOT =       -5851
598395


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   07311
53700029  
00020000  00000-0  20000-3 0  9108
2 25544  51
6354  84
7331 0002320 178
4050 181
7122 15
76214865 33399


Satellite: ISS
Catalog Number: 25544
Epoch time:      07311
53700029   =   yrday
fracday
Element set:     910
Inclination:       51
6354  deg
RA of node:        84
7331  deg
Eccentricity:     
0002320     
Arg of perigee:   178
4050  deg
Mean anomaly:     181
7122  deg
Mean motion:   15
76214865  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3339
Checksum:              259


Coasting Arc #12 (Orbit 3354)
---------------------------------------

Vector Time (GMT): 2007/312/12:03:54
251
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3896284
95                 A    =         6713747
42  meter
 Y    =        1514811
54  meter          E    =           
0004291
 Z    =        5251634
58                 I    =           51
93370
 XDOT =      -1970
786283                 Wp   =          144
11815
 YDOT =      -7420
043504  meter/sec      RA   =           79
07047  deg
 ZDOT =        674
437754                 TA   =          299
47862
                                          MA   =          299
52142
                                          Ha   =            186
822  n
mi
                                          Hp   =            180
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12783087
09                 X    =        -3938446
53
 Y    =        4969854
13  feet           Y    =         1471005
24  meter
 Z    =       17229772
24                 Z    =         5232603
43
 XDOT =      -6465
834261                 XDOT =       -1890
944164
 YDOT =     -24343
974752  feet/sec       YDOT =       -7441
635545  meter/sec
 ZDOT =       2212
722290                 ZDOT =         665
057174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5029659
99                 X    =         1533040
36
 Y    =      -12856680
28  feet           Y    =        -3918716
15  meter
 Z    =       17157508
85                 Z    =         5229608
70
 XDOT =      21394
406765                 XDOT =        6521
015182
 YDOT =      11290
046610  feet/sec       YDOT =        3441
206207  meter/sec
 ZDOT =       2176
187029                 ZDOT =         663
301806


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   07312
55138682  
00020000  00000-0  20000-3 0  9112
2 25544  51
6368  79
5062 0002152 184
1903 175
9244 15
76281795 33555


Satellite: ISS
Catalog Number: 25544
Epoch time:      07312
55138682   =   yrday
fracday
Element set:     911
Inclination:       51
6368  deg
RA of node:        79
5062  deg
Eccentricity:     
0002152     
Arg of perigee:   184
1903  deg
Mean anomaly:     175
9244  deg
Mean motion:   15
76281795  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3355
Checksum:              299

INTERNATIONAL SPACE STATION ORBITAL DATA:

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

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

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

   David Cottle
   Director Of Engineering
   IDB Communications

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