Date: October 23rd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5112 86 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 3038)
---------------------------------------

Vector Time (GMT): 2007/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1417947
93                 A    =         6715415
68  meter
 Y    =        4057666
64  meter          E    =           
0016813
 Z    =       -5174294
63                 I    =           51
60781
 XDOT =      -7516
131739                 Wp   =          100
20250
 YDOT =      -1151
736299  meter/sec      RA   =          181
78861  deg
 ZDOT =       1156
762083                 TA   =          180
85906
                                          MA   =          180
86195
                                          Ha   =            188
198  n
mi
                                          Hp   =            180
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4652060
14                 X    =        -1438079
84
 Y    =       13312554
60  feet           Y    =         4041697
83  meter
 Z    =      -16976032
26                 Z    =        -5181231
99
 XDOT =     -24659
224864                 XDOT =       -7508
313652
 YDOT =      -3778
662399  feet/sec       YDOT =       -1235
742235  meter/sec
 ZDOT =       3795
151191                 ZDOT =        1120
267183

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1945985
39                 X    =         -593136
35
 Y    =      -13935589
70  feet           Y    =        -4247567
74  meter
 Z    =      -17001880
05                 Z    =        -5182173
04
 XDOT =      22710
790532                 XDOT =        6922
248954
 YDOT =      -7631
149366  feet/sec       YDOT =       -2325
974327  meter/sec
 ZDOT =       3656
287493                 ZDOT =        1114
436428


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   07292
51400141  
00020000  00000-0  20000-3 0  9005
2 25544  51
6373 182
7218 0002420 107
1868 252
9561 15
75791420 30391


Satellite: ISS
Catalog Number: 25544
Epoch time:      07292
51400141   =   yrday
fracday
Element set:     900
Inclination:       51
6373  deg
RA of node:       182
7218  deg
Eccentricity:     
0002420     
Arg of perigee:   107
1868  deg
Mean anomaly:     252
9561  deg
Mean motion:   15
75791420  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3039
Checksum:              268


Coasting Arc #2 (Orbit 3054)
---------------------------------------

Vector Time (GMT): 2007/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6461519
40                 A    =         6726028
04  meter
 Y    =         905782
04  meter          E    =           
0010228
 Z    =       -1619470
79                 I    =           51
67259
 XDOT =      -2090
001420                 Wp   =          137
00051
 YDOT =       4676
528271  meter/sec      RA   =          176
66411  deg
 ZDOT =      -5751
826147                 TA   =           60
88273
                                          MA   =           60
78038
                                          Ha   =            188
205  n
mi
                                          Hp   =            180
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21199210
64                 X    =         6458777
77
 Y    =        2971725
86  feet           Y    =          978023
07  meter
 Z    =       -5313224
36                 Z    =        -1588087
00
 XDOT =      -6856
960039                 XDOT =       -2114
198045
 YDOT =      15342
940523  feet/sec       YDOT =        4653
021351  meter/sec
 ZDOT =     -18870
820692                 ZDOT =       -5762
038317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20160835
73                 X    =        -6145022
73
 Y    =        7282383
58  feet           Y    =         2219670
52  meter
 Z    =       -5193807
04                 Z    =        -1583072
39
 XDOT =       -661
818679                 XDOT =        -201
722333
 YDOT =     -15249
805803  feet/sec       YDOT =       -4648
140809  meter/sec
 ZDOT =     -18909
038043                 ZDOT =       -5763
474795


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   07293
52867605  
00020000  00000-0  20000-3 0  9010
2 25544  51
6376 177
4966 0002354 115
2480 244
8928 15
75778097 30551


Satellite: ISS
Catalog Number: 25544
Epoch time:      07293
52867605   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       177
4966  deg
Eccentricity:     
0002354     
Arg of perigee:   115
2480  deg
Mean anomaly:     244
8928  deg
Mean motion:   15
75778097  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3055
Checksum:              323


Coasting Arc #3 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2007/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2205148
36                 A    =         6716748
94  meter
 Y    =       -4156894
28  meter          E    =           
0008580
 Z    =        4787011
98                 I    =           51
67152
 XDOT =       7226
728598                 Wp   =           71
78259
 YDOT =        928
928212  meter/sec      RA   =          171
48211  deg
 ZDOT =      -2516
054726                 TA   =           42
83847
                                          MA   =           42
77164
                                          Ha   =            187
896  n
mi
                                          Hp   =            180
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7234738
71                 X    =         2228212
74
 Y    =      -13638104
60  feet           Y    =        -4132105
96  meter
 Z    =       15705419
90                 Z    =         4797780
89
 XDOT =      23709
739495                 XDOT =        7228
026774
 YDOT =       3047
664738  feet/sec       YDOT =        1009
748764  meter/sec
 ZDOT =      -8254
772723                 ZDOT =       -2480
943698

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         311976
10                 X    =           95090
32
 Y    =       15393872
71  feet           Y    =         4692052
40  meter
 Z    =       15745821
96                 Z    =         4799326
53
 XDOT =     -21160
807015                 XDOT =       -6449
813978
 YDOT =       8756
791032  feet/sec       YDOT =        2669
069907  meter/sec
 ZDOT =      -8121
172271                 ZDOT =       -2475
333308


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   07294
54332811  
00020000  00000-0  20000-3 0  9020
2 25544  51
6377 172
2712 0002171 113
8420 246
2972 15
75888769 30710


Satellite: ISS
Catalog Number: 25544
Epoch time:      07294
54332811   =   yrday
fracday
Element set:     902
Inclination:       51
6377  deg
RA of node:       172
2712  deg
Eccentricity:     
0002171     
Arg of perigee:   113
8420  deg
Mean anomaly:     246
2972  deg
Mean motion:   15
75888769  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3071
Checksum:              292


Coasting Arc #4 (Orbit 3086)
---------------------------------------

Vector Time (GMT): 2007/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6084640
11                 A    =         6723691
21  meter
 Y    =        -753949
56  meter          E    =           
0015453
 Z    =        2744460
36                 I    =           51
72254
 XDOT =       2946
669687                 Wp   =           84
10990
 YDOT =      -4905
451067  meter/sec      RA   =          166
37876  deg
 ZDOT =       5162
159443                 TA   =          307
25226
                                          MA   =          307
39312
                                          Ha   =            188
038  n
mi
                                          Hp   =            180
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19962730
03                 X    =        -6089089
41
 Y    =       -2473587
81  feet           Y    =         -822016
19  meter
 Z    =        9004135
04                 Z    =         2714889
94
 XDOT =       9667
551467                 XDOT =        2976
226939
 YDOT =     -16093
999563  feet/sec       YDOT =       -4872
334210  meter/sec
 ZDOT =      16936
218646                 ZDOT =        5176
546638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18595930
86                 X    =         5668039
73
 Y    =       -7799631
00  feet           Y    =        -2377327
53  meter
 Z    =        8891613
26                 Z    =         2710163
72
 XDOT =       -876
544754                 XDOT =        -267
170841
 YDOT =      17366
929941  feet/sec       YDOT =        5293
440246  meter/sec
 ZDOT =      16990
281433                 ZDOT =        5178
637781


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   07295
55796360  
00020000  00000-0  20000-3 0  9036
2 25544  51
6374 167
0454 0002180 115
9640 244
1749 15
75861882 30872


Satellite: ISS
Catalog Number: 25544
Epoch time:      07295
55796360   =   yrday
fracday
Element set:     903
Inclination:       51
6374  deg
RA of node:       167
0454  deg
Eccentricity:     
0002180     
Arg of perigee:   115
9640  deg
Mean anomaly:     244
1749  deg
Mean motion:   15
75861882  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3087
Checksum:              310


Coasting Arc #5 (Orbit 3101)
---------------------------------------

Vector Time (GMT): 2007/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2906878
41                 A    =         6719242
40  meter
 Y    =        4436389
69  meter          E    =           
0009941
 Z    =       -4135607
16                 I    =           51
73570
 XDOT =      -6658
867425                 Wp   =          112
92893
 YDOT =       -862
883592  meter/sec      RA   =          161
18639  deg
 ZDOT =       3758
144703                 TA   =          195
52137
                                          MA   =          195
55187
                                          Ha   =            187
820  n
mi
                                          Hp   =            180
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9537002
66                 X    =        -2936180
29
 Y    =       14555084
29  feet           Y    =         4403719
23  meter
 Z    =      -13568264
94                 Z    =        -4149800
52
 XDOT =     -21846
677905                 XDOT =       -6666
980396
 YDOT =      -2830
982914  feet/sec       YDOT =        -937
391941  meter/sec
 ZDOT =      12329
871073                 ZDOT =        3725
775603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         677496
24                 X    =          206500
85
 Y    =      -17346303
10  feet           Y    =        -5287153
19  meter
 Z    =      -13621654
80                 Z    =        -4151880
38
 XDOT =      19011
565308                 XDOT =        5794
725106
 YDOT =      -8834
545847  feet/sec       YDOT =       -2692
769574  meter/sec
 ZDOT =      12206
688808                 ZDOT =        3720
598749


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   07296
50916362  
00020000  00000-0  20000-3 0  9049
2 25544  51
6370 162
1462 0002062 122
7608 237
3755 15
75910738 31026


Satellite: ISS
Catalog Number: 25544
Epoch time:      07296
50916362   =   yrday
fracday
Element set:     904
Inclination:       51
6370  deg
RA of node:       162
1462  deg
Eccentricity:     
0002062     
Arg of perigee:   122
7608  deg
Mean anomaly:     237
3755  deg
Mean motion:   15
75910738  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3102
Checksum:              277


Coasting Arc #6 (Orbit 3117)
---------------------------------------

Vector Time (GMT): 2007/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5499668
29                 A    =         6720592
93  meter
 Y    =         820734
97  meter          E    =           
0007413
 Z    =       -3780873
39                 I    =           51
76610
 XDOT =      -3686
174331                 Wp   =           89
17567
 YDOT =       5274
120601  meter/sec      RA   =          156
09544  deg
 ZDOT =      -4224
020887                 TA   =          136
53560
                                          MA   =          136
47714
                                          Ha   =            187
785  n
mi
                                          Hp   =            180
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18043531
13                 X    =         5508449
26
 Y    =        2692700
03  feet           Y    =          882284
24  meter
 Z    =      -12404440
24                 Z    =        -3754133
99
 XDOT =     -12093
747806                 XDOT =       -3724
356286
 YDOT =      17303
545278  feet/sec       YDOT =        5232
685967  meter/sec
 ZDOT =     -13858
336244                 ZDOT =       -4242
021875

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16816705
02                 X    =        -5125731
69
 Y    =        7247942
27  feet           Y    =         2209172
80  meter
 Z    =      -12302664
42                 Z    =        -3749852
11
 XDOT =       1632
577676                 XDOT =         497
609676
 YDOT =     -19811
046804  feet/sec       YDOT =       -6038
407066  meter/sec
 ZDOT =     -13926
100918                 ZDOT =       -4244
675560


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   07297
52375837  
00020000  00000-0  20000-3 0  9059
2 25544  51
6360 156
9205 0001982 128
8538 231
2803 15
75920614 31188


Satellite: ISS
Catalog Number: 25544
Epoch time:      07297
52375837   =   yrday
fracday
Element set:     905
Inclination:       51
6360  deg
RA of node:       156
9205  deg
Eccentricity:     
0001982     
Arg of perigee:   128
8538  deg
Mean anomaly:     231
2803  deg
Mean motion:   15
75920614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3118
Checksum:              299


Coasting Arc #7 (Orbit 3133)
---------------------------------------

Vector Time (GMT): 2007/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3467311
38                 A    =         6722009
27  meter
 Y    =       -4792411
64  meter          E    =           
0014484
 Z    =        3178643
57                 I    =           51
79791
 XDOT =       5911
754761                 Wp   =           97
69522
 YDOT =       1061
484234  meter/sec      RA   =          150
90357  deg
 ZDOT =      -4831
500654                 TA   =           45
26577
                                          MA   =           45
14796
                                          Ha   =            187
548  n
mi
                                          Hp   =            180
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11375693
51                 X    =         3505201
36
 Y    =      -15723135
31  feet           Y    =        -4753426
22  meter
 Z    =       10428620
63                 Z    =         3195580
55
 XDOT =      19395
520869                 XDOT =        5922
917037
 YDOT =       3482
559822  feet/sec       YDOT =        1127
655040  meter/sec
 ZDOT =     -15851
380097                 ZDOT =       -4802
753334

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1009542
33                 X    =         -307708
50
 Y    =       19346050
00  feet           Y    =         5896676
04  meter
 Z    =       10492411
00                 Z    =         3198086
87
 XDOT =     -16859
475361                 XDOT =       -5138
768090
 YDOT =       7687
523086  feet/sec       YDOT =        2343
157037  meter/sec
 ZDOT =     -15741
934621                 ZDOT =       -4798
141672


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   07298
53833183  
00020000  00000-0  20000-3 0  9065
2 25544  51
6360 151
6942 0001851 128
0625 232
0706 15
76008661 31341


Satellite: ISS
Catalog Number: 25544
Epoch time:      07298
53833183   =   yrday
fracday
Element set:     906
Inclination:       51
6360  deg
RA of node:       151
6942  deg
Eccentricity:     
0001851     
Arg of perigee:   128
0625  deg
Mean anomaly:     232
0706  deg
Mean motion:   15
76008661  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3134
Checksum:              278


Coasting Arc #8 (Orbit 3149)
---------------------------------------

Vector Time (GMT): 2007/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4788770
75                 A    =         6717566
89  meter
 Y    =       -1098855
57  meter          E    =           
0010434
 Z    =        4575521
77                 I    =           51
80534
 XDOT =       4199
590580                 Wp   =          117
74189
 YDOT =      -5717
851429  meter/sec      RA   =          145
81097  deg
 ZDOT =       3012
162808                 TA   =          302
38775
                                          MA   =          302
48867
                                          Ha   =            187
768  n
mi
                                          Hp   =            180
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15711190
12                 X    =        -4798355
12
 Y    =       -3605169
19  feet           Y    =        -1152459
88  meter
 Z    =       15011554
37                 Z    =         4552233
81
 XDOT =      13778
184318                 XDOT =        4248
583259
 YDOT =     -18759
355082  feet/sec       YDOT =       -5670
615280  meter/sec
 ZDOT =       9882
423911                 ZDOT =        3032
684195

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15137100
17                 X    =         4613788
13
 Y    =       -5775983
03  feet           Y    =        -1760519
63  meter
 Z    =       14922859
07                 Z    =         4548487
44
 XDOT =      -1411
569754                 XDOT =        -430
246461
 YDOT =      22117
657684  feet/sec       YDOT =        6741
462062  meter/sec
 ZDOT =       9959
740759                 ZDOT =        3035
728983


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   07299
55288817  
00020000  00000-0  20000-3 0  9077
2 25544  51
6344 146
4670 0001916 131
4374 228
6955 15
75963838 31504


Satellite: ISS
Catalog Number: 25544
Epoch time:      07299
55288817   =   yrday
fracday
Element set:     907
Inclination:       51
6344  deg
RA of node:       146
4670  deg
Eccentricity:     
0001916     
Arg of perigee:   131
4374  deg
Mean anomaly:     228
6955  deg
Mean motion:   15
75963838  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3150
Checksum:              323


Coasting Arc #9 (Orbit 3164)
---------------------------------------

Vector Time (GMT): 2007/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3800023
64                 A    =         6724614
86  meter
 Y    =        5167244
45  meter          E    =           
0006562
 Z    =       -2017057
23                 I    =           51
85197
 XDOT =      -5056
727440                 Wp   =           56
60596
 YDOT =      -1539
606370  meter/sec      RA   =          140
63129  deg
 ZDOT =       5599
003446                 TA   =          280
96973
                                          MA   =          281
04354
                                          Ha   =            187
468  n
mi
                                          Hp   =            180
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12467269
15                 X    =        -3847723
27
 Y    =       16952901
75  feet           Y    =         5124483
80  meter
 Z    =       -6617641
85                 Z    =        -2035634
10
 XDOT =     -16590
313124                 XDOT =       -5066
335402
 YDOT =      -5051
202000  feet/sec       YDOT =       -1596
207456  meter/sec
 ZDOT =      18369
433878                 ZDOT =        5574
413612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         557651
31                 X    =          169972
12
 Y    =      -21014072
03  feet           Y    =        -6405089
15  meter
 Z    =       -6687650
04                 Z    =        -2038395
73
 XDOT =      15064
974555                 XDOT =        4591
804244
 YDOT =      -5399
319814  feet/sec       YDOT =       -1645
712679  meter/sec
 ZDOT =      18275
726772                 ZDOT =        5570
441520


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   07300
50401269  
00020000  00000-0  20000-3 0  9084
2 25544  51
6333 141
5663 0001852 140
5864 219
5435 15
76020778 31650


Satellite: ISS
Catalog Number: 25544
Epoch time:      07300
50401269   =   yrday
fracday
Element set:     908
Inclination:       51
6333  deg
RA of node:       141
5663  deg
Eccentricity:     
0001852     
Arg of perigee:   140
5864  deg
Mean anomaly:     219
5435  deg
Mean motion:   15
76020778  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3165
Checksum:              276


Coasting Arc #10 (Orbit 3180)
---------------------------------------

Vector Time (GMT): 2007/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4035275
22                 A    =         6715059
22  meter
 Y    =        1669527
35  meter          E    =           
0014696
 Z    =       -5113894
55                 I    =           51
84045
 XDOT =      -4461
426487                 Wp   =           85
13589
 YDOT =       6075
629928  meter/sec      RA   =          135
52538  deg
 ZDOT =      -1539
472196                 TA   =          170
13514
                                          MA   =          170
10626
                                          Ha   =            187
430  n
mi
                                          Hp   =            180
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13239091
91                 X    =         4041149
53
 Y    =        5477451
92  feet           Y    =         1714685
23  meter
 Z    =      -16777869
26                 Z    =        -5094276
21
 XDOT =     -14637
226006                 XDOT =       -4521
554802
 YDOT =      19933
169054  feet/sec       YDOT =        6025
403631  meter/sec
 ZDOT =      -5050
761799                 ZDOT =       -1561
292163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14023314
64                 X    =        -4274306
30
 Y    =        3335834
11  feet           Y    =         1016762
24  meter
 Z    =      -16703047
28                 Z    =        -5091088
81
 XDOT =        468
650929                 XDOT =         142
844803
 YDOT =     -23689
570738  feet/sec       YDOT =       -7220
581161  meter/sec
 ZDOT =      -5133
011480                 ZDOT =       -1564
541899


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
51852742  
00020000  00000-0  20000-3 0  9093
2 25544  51
6323 136
3391 0001901 142
9692 217
1603 15
76056710 31813


Satellite: ISS
Catalog Number: 25544
Epoch time:      07301
51852742   =   yrday
fracday
Element set:     909
Inclination:       51
6323  deg
RA of node:       136
3391  deg
Eccentricity:     
0001901     
Arg of perigee:   142
9692  deg
Mean anomaly:     217
1603  deg
Mean motion:   15
76056710  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3181
Checksum:              268


Coasting Arc #11 (Orbit 3196)
---------------------------------------

Vector Time (GMT): 2007/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3935612
12                 A    =         6725941
22  meter
 Y    =       -5407106
70  meter          E    =           
0014983
 Z    =         642669
57                 I    =           51
89856
 XDOT =       4207
575506                 Wp   =          130
16154
 YDOT =       2337
395303  meter/sec      RA   =          130
37087  deg
 ZDOT =      -6018
847018                 TA   =           42
85645
                                          MA   =           42
73977
                                          Ha   =            187
249  n
mi
                                          Hp   =            180
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12912113
26                 X    =         3992660
65
 Y    =      -17739851
36  feet           Y    =        -5362777
53  meter
 Z    =        2108495
98                 Z    =          661927
43
 XDOT =      13804
381581                 XDOT =        4210
364869
 YDOT =       7668
619762  feet/sec       YDOT =        2384
462831  meter/sec
 ZDOT =     -19746
873420                 ZDOT =       -5998
399166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         258787
71                 X    =           78878
49
 Y    =       21932774
21  feet           Y    =         6685109
58  meter
 Z    =        2181099
47                 Z    =          664799
12
 XDOT =     -14140
631222                 XDOT =       -4310
064396
 YDOT =       2148
675237  feet/sec       YDOT =         654
916212  meter/sec
 ZDOT =     -19668
808043                 ZDOT =       -5995
052691


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
53302045  
00020000  00000-0  20000-3 0  9104
2 25544  51
6332 131
1123 0001677 144
9559 215
1716 15
76128094 31978


Satellite: ISS
Catalog Number: 25544
Epoch time:      07302
53302045   =   yrday
fracday
Element set:     910
Inclination:       51
6332  deg
RA of node:       131
1123  deg
Eccentricity:     
0001677     
Arg of perigee:   144
9559  deg
Mean anomaly:     215
1716  deg
Mean motion:   15
76128094  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3197
Checksum:              264


Coasting Arc #12 (Orbit 3212)
---------------------------------------

Vector Time (GMT): 2007/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3338270
41                 A    =         6714169
07  meter
 Y    =       -2455702
50  meter          E    =           
0003697
 Z    =        5279694
51                 I    =           51
87550
 XDOT =       4493
720142                 Wp   =          115
01404
 YDOT =      -6261
653404  meter/sec      RA   =          125
24173  deg
 ZDOT =        -72
614822                 TA   =          335
66343
                                          MA   =          335
68088
                                          Ha   =            187
455  n
mi
                                          Hp   =            180
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10952330
74                 X    =        -3336210
54
 Y    =       -8056766
72  feet           Y    =        -2493021
78  meter
 Z    =       17321832
37                 Z    =         5263481
72
 XDOT =      14743
176318                 XDOT =        4563
757664
 YDOT =     -20543
482295  feet/sec       YDOT =       -6211
010477  meter/sec
 ZDOT =       -238
237606                 ZDOT =         -50
614237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13669843
74                 X    =         4166568
37
 Y    =        -378964
70  feet           Y    =         -115508
44  meter
 Z    =       17259857
27                 Z    =         5260804
50
 XDOT =        862
817083                 XDOT =         262
986647
 YDOT =      24274
420847  feet/sec       YDOT =        7398
843474  meter/sec
 ZDOT =       -155
287299                 ZDOT =         -47
331569


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
54749603  
00020000  00000-0  20000-3 0  9112
2 25544  51
6326 125
8846 0001915 149
2373 210
8904 15
76082192 32138


Satellite: ISS
Catalog Number: 25544
Epoch time:      07303
54749603   =   yrday
fracday
Element set:     911
Inclination:       51
6326  deg
RA of node:       125
8846  deg
Eccentricity:     
0001915     
Arg of perigee:   149
2373  deg
Mean anomaly:     210
8904  deg
Mean motion:   15
76082192  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3213
Checksum:              282

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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