Date: February 27th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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


061/08:16:57 974 3 0 5 5 5 5
N/A -4 4 -0 1 187 1
000/00:07:55 947 1 1 0 1 175 2

Coasting Arc #1 (Orbit 3328)
---------------------------------------

Vector Time (GMT): 2007/057/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3977889
96                 A    =         6707336
51  meter
 Y    =       -1790648
33  meter          E    =           
0006980
 Z    =       -5088962
35                 I    =           51
39354
 XDOT =       4553
367024                 Wp   =          241
82489
 YDOT =      -6060
906871  meter/sec      RA   =          315
56925  deg
 ZDOT =      -1428
357635                 TA   =           14
47878
                                          MA   =           14
45879
                                          Ha   =            184
436  n
mi
                                          Hp   =            175
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13050820
08                 X    =        -3932850
34
 Y    =       -5874830
48  feet           Y    =        -1834879
38  meter
 Z    =      -16696070
69                 Z    =        -5108177
13
 XDOT =      14938
868188                 XDOT =        4627
741081
 YDOT =     -19884
865061  feet/sec       YDOT =       -6009
572703  meter/sec
 ZDOT =      -4686
212713                 ZDOT =       -1406
057359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7814419
67                 X    =        -2381835
11
 Y    =      -11889056
37  feet           Y    =        -3623784
38  meter
 Z    =      -16768467
38                 Z    =        -5111028
86
 XDOT =      22406
974577                 XDOT =        6829
645851
 YDOT =      -8243
363727  feet/sec       YDOT =       -2512
577264  meter/sec
 ZDOT =      -4603
208766                 ZDOT =       -1403
058032


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   07057
49733439  
00020000  00000-0  20000-3 0  9000
2 25544  51
6357 316
0153 0020843 253
6996 106
1877 15
78712949 33295


Satellite: ISS
Catalog Number: 25544
Epoch time:      07057
49733439   =   yrday
fracday
Element set:     900
Inclination:       51
6357  deg
RA of node:       316
0153  deg
Eccentricity:     
0020843     
Arg of perigee:   253
6996  deg
Mean anomaly:     106
1877  deg
Mean motion:   15
78712949  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3329
Checksum:              317


Coasting Arc #2 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2007/058/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4525274
62                 A    =         6718818
37  meter
 Y    =        4944061
14  meter          E    =           
0018297
 Z    =        -307155
71                 I    =           51
41249
 XDOT =      -3360
054135                 Wp   =          223
49613
 YDOT =      -3461
660349  meter/sec      RA   =          310
37208  deg
 ZDOT =      -6018
248197                 TA   =          319
86148
                                          MA   =          319
99649
                                          Ha   =            184
444  n
mi
                                          Hp   =            175
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14846701
52                 X    =        -4578731
43
 Y    =       16220673
03  feet           Y    =         4893158
10  meter
 Z    =       -1007728
69                 Z    =         -329268
70
 XDOT =     -11023
799654                 XDOT =       -3291
860858
 YDOT =     -11357
153375  feet/sec       YDOT =       -3498
853019  meter/sec
 ZDOT =     -19744
908782                 ZDOT =       -6034
405286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21108946
36                 X    =        -6434006
85
 Y    =        6146073
05  feet           Y    =         1873323
07  meter
 Z    =       -1090167
99                 Z    =         -332283
20
 XDOT =      -2974
319661                 XDOT =        -906
572633
 YDOT =     -13835
298983  feet/sec       YDOT =       -4216
999130  meter/sec
 ZDOT =     -19806
036292                 ZDOT =       -6036
879862


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   07058
51013645  
00020000  00000-0  20000-3 0  9015
2 25544  51
6358 310
7773 0020980 257
2942 102
5878 15
78691807 33456


Satellite: ISS
Catalog Number: 25544
Epoch time:      07058
51013645   =   yrday
fracday
Element set:     901
Inclination:       51
6358  deg
RA of node:       310
7773  deg
Eccentricity:     
0020980     
Arg of perigee:   257
2942  deg
Mean anomaly:     102
5878  deg
Mean motion:   15
78691807  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3345
Checksum:              303


Coasting Arc #3 (Orbit 3360)
---------------------------------------

Vector Time (GMT): 2007/059/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1835970
47                 A    =         6708028
62  meter
 Y    =        4205180
32  meter          E    =           
0015515
 Z    =        4906639
64                 I    =           51
35920
 XDOT =      -5538
579298                 Wp   =          271
38144
 YDOT =       4901
069281  meter/sec      RA   =          305
16116  deg
 ZDOT =      -2133
407898                 TA   =          199
37327
                                          MA   =          199
43231
                                          Ha   =            184
151  n
mi
                                          Hp   =            175
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6023525
16                 X    =         1764976
23
 Y    =       13796523
35  feet           Y    =         4225314
28  meter
 Z    =       16097899
07                 Z    =         4915386
02
 XDOT =     -18171
191923                 XDOT =       -5582
608717
 YDOT =      16079
623624  feet/sec       YDOT =        4838
887583  meter/sec
 ZDOT =      -6999
369745                 ZDOT =       -2160
420531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1843749
17                 X    =         -561974
75
 Y    =       14904741
25  feet           Y    =         4542965
13  meter
 Z    =       16131290
83                 Z    =         4916817
44
 XDOT =     -22682
857052                 XDOT =       -6913
734829
 YDOT =       4859
345022  feet/sec       YDOT =        1481
128363  meter/sec
 ZDOT =      -7100
216409                 ZDOT =       -2164
145961


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   07059
52291442  
00020000  00000-0  20000-3 0  9021
2 25544  51
6356 305
5390 0021035 261
8931  97
9848 15
78792999 33618


Satellite: ISS
Catalog Number: 25544
Epoch time:      07059
52291442   =   yrday
fracday
Element set:     902
Inclination:       51
6356  deg
RA of node:       305
5390  deg
Eccentricity:     
0021035     
Arg of perigee:   261
8931  deg
Mean anomaly:      97
9848  deg
Mean motion:   15
78792999  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3361
Checksum:              321


Coasting Arc #4 (Orbit 3376)
---------------------------------------

Vector Time (GMT): 2007/060/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4889120
04                 A    =         6713906
65  meter
 Y    =       -3257737
30  meter          E    =           
0008192
 Z    =        3257944
33                 I    =           51
36354
 XDOT =        875
655555                 Wp   =          261
37321
 YDOT =       6023
046995  meter/sec      RA   =          300
01147  deg
 ZDOT =       4717
464432                 TA   =          137
00524
                                          MA   =          136
94119
                                          Ha   =            184
050  n
mi
                                          Hp   =            175
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16040420
06                 X    =         4909359
12
 Y    =      -10688114
51  feet           Y    =        -3202951
15  meter
 Z    =       10688793
74                 Z    =         3281744
24
 XDOT =       2872
885680                 XDOT =         785
324002
 YDOT =      19760
652870  feet/sec       YDOT =        6032
334175  meter/sec
 ZDOT =      15477
245513                 ZDOT =        4721
498601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19167914
11                 X    =         5842380
22
 Y    =       -1487188
23  feet           Y    =         -453294
97  meter
 Z    =       10777778
95                 Z    =         3285067
02
 XDOT =      -7361
291667                 XDOT =       -2243
721700
 YDOT =      17193
641372  feet/sec       YDOT =        5240
621890  meter/sec
 ZDOT =      15493
177716                 ZDOT =        4722
320568


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   07060
53567398  
00020000  00000-0  20000-3 0  9031
2 25544  51
6355 300
2997 0020939 265
9259  93
9513 15
78777089 33777


Satellite: ISS
Catalog Number: 25544
Epoch time:      07060
53567398   =   yrday
fracday
Element set:     903
Inclination:       51
6355  deg
RA of node:       300
2997  deg
Eccentricity:     
0020939     
Arg of perigee:   265
9259  deg
Mean anomaly:      93
9513  deg
Mean motion:   15
78777089  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3377
Checksum:              340


Coasting Arc #5 (Orbit 3389)
---------------------------------------

Vector Time (GMT): 2007/061/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1896617
76                 A    =         6712281
11  meter
 Y    =       -4523855
31  meter          E    =           
0015629
 Z    =       -4569948
90                 I    =           51
33473
 XDOT =       5015
146389                 Wp   =          259
15699
 YDOT =      -5076
738928  meter/sec      RA   =          295
45170  deg
 ZDOT =       2932
785126                 TA   =           40
03326
                                          MA   =           39
91817
                                          Ha   =            187
089  n
mi
                                          Hp   =            175
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6222499
21                 X    =        -1823691
06
 Y    =      -14842044
98  feet           Y    =        -4544656
86  meter
 Z    =      -14993270
68                 Z    =        -4578985
01
 XDOT =      16453
892353                 XDOT =        5057
295948
 YDOT =     -16655
967610  feet/sec       YDOT =       -5020
420918  meter/sec
 ZDOT =       9621
998444                 ZDOT =        2957
250672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12874024
24                 X    =         3924002
59
 Y    =       -9603567
27  feet           Y    =        -2927167
30  meter
 Z    =      -15027806
12                 Z    =        -4580475
31
 XDOT =      19480
296259                 XDOT =        5937
594300
 YDOT =      10856
591538  feet/sec       YDOT =        3309
089101  meter/sec
 ZDOT =       9713
243356                 ZDOT =        2960
596575


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   07061
35852438  
00020000  00000-0  20000-3 0  9045
2 25544  51
6336 296
0427 0025244 271
5988  88
2285 15
77766744 33905


Satellite: ISS
Catalog Number: 25544
Epoch time:      07061
35852438   =   yrday
fracday
Element set:     904
Inclination:       51
6336  deg
RA of node:       296
0427  deg
Eccentricity:     
0025244     
Arg of perigee:   271
5988  deg
Mean anomaly:      88
2285  deg
Mean motion:   15
77766744  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3390
Checksum:              322


Coasting Arc #6 (Orbit 3405)
---------------------------------------

Vector Time (GMT): 2007/062/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4379355
91                 A    =         6715750
11  meter
 Y    =        3626969
75  meter          E    =           
0019988
 Z    =       -3559196
19                 I    =           51
33609
 XDOT =      -1487
528120                 Wp   =          279
28683
 YDOT =      -6148
980246  meter/sec      RA   =          290
31455  deg
 ZDOT =      -4411
564813                 TA   =          303
51721
                                          MA   =          303
70802
                                          Ha   =            187
054  n
mi
                                          Hp   =            175
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14367965
59                 X    =        -4402298
24
 Y    =       11899507
07  feet           Y    =         3577868
80  meter
 Z    =      -11677152
84                 Z    =        -3580526
55
 XDOT =      -4880
341602                 XDOT =       -1397
228758
 YDOT =     -20173
819704  feet/sec       YDOT =       -6165
110066  meter/sec
 ZDOT =     -14473
637838                 ZDOT =       -4418
571233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15240083
18                 X    =        -4645177
35
 Y    =      -10672863
98  feet           Y    =        -3253088
94  meter
 Z    =      -11756804
04                 Z    =        -3583473
87
 XDOT =      17424
968671                 XDOT =        5311
130451
 YDOT =      -8821
269942  feet/sec       YDOT =       -2688
723078  meter/sec
 ZDOT =     -14500
769806                 ZDOT =       -4419
834637


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   07062
37192274  
00020000  00000-0  20000-3 0  9054
2 25544  51
6339 290
8090 0025228 275
6971  84
1318 15
77807114 34062


Satellite: ISS
Catalog Number: 25544
Epoch time:      07062
37192274   =   yrday
fracday
Element set:     905
Inclination:       51
6339  deg
RA of node:       290
8090  deg
Eccentricity:     
0025228     
Arg of perigee:   275
6971  deg
Mean anomaly:      84
1318  deg
Mean motion:   15
77807114  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3406
Checksum:              298


Coasting Arc #7 (Orbit 3421)
---------------------------------------

Vector Time (GMT): 2007/063/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         753964
82                 A    =         6717723
38  meter
 Y    =        6032476
82  meter          E    =           
0011804
 Z    =        2870819
04                 I    =           51
33359
 XDOT =      -4983
038524                 Wp   =          280
14910
 YDOT =       3011
126318  meter/sec      RA   =          285
07738  deg
 ZDOT =      -5034
104419                 TA   =          226
69746
                                          MA   =          226
79596
                                          Ha   =            187
197  n
mi
                                          Hp   =            175
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2473637
87                 X    =          672507
15
 Y    =       19791590
60  feet           Y    =         6040452
87  meter
 Z    =        9418697
64                 Z    =         2874283
33
 XDOT =     -16348
551588                 XDOT =       -4991
884780
 YDOT =       9879
023353  feet/sec       YDOT =        2955
353287  meter/sec
 ZDOT =     -16516
090613                 ZDOT =       -5058
333246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18327189
04                 X    =        -5586127
22
 Y    =        7853636
24  feet           Y    =         2393788
33  meter
 Z    =        9432515
46                 Z    =         2875030
71
 XDOT =     -13454
478377                 XDOT =       -4100
925009
 YDOT =     -11512
962866  feet/sec       YDOT =       -3509
151082  meter/sec
 ZDOT =     -16606
706989                 ZDOT =       -5061
724290


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   07063
38530126  
00020000  00000-0  20000-3 0  9069
2 25544  51
6334 285
5746 0025259 279
5084  80
3227 15
77818991 34228


Satellite: ISS
Catalog Number: 25544
Epoch time:      07063
38530126   =   yrday
fracday
Element set:     906
Inclination:       51
6334  deg
RA of node:       285
5746  deg
Eccentricity:     
0025259     
Arg of perigee:   279
5084  deg
Mean anomaly:      80
3227  deg
Mean motion:   15
77818991  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3422
Checksum:              309


Coasting Arc #8 (Orbit 3437)
---------------------------------------

Vector Time (GMT): 2007/064/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4292533
40                 A    =         6710355
29  meter
 Y    =       -1449348
73  meter          E    =           
0020022
 Z    =        4966344
81                 I    =           51
30304
 XDOT =        276
512498                 Wp   =          277
17103
 YDOT =       7439
274295  meter/sec      RA   =          279
92828  deg
 ZDOT =       1941
188585                 TA   =          154
01695
                                          MA   =          153
91630
                                          Ha   =            187
240  n
mi
                                          Hp   =            174
857

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14083114
83                 X    =         4284295
99
 Y    =       -4755081
14  feet           Y    =        -1401392
82  meter
 Z    =       16293782
20                 Z    =         4987177
72
 XDOT =        907
193235                 XDOT =         183
875130
 YDOT =      24407
067897  feet/sec       YDOT =        7441
848632  meter/sec
 ZDOT =       6368
728955                 ZDOT =        1942
306155

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8681719
81                 X    =         2646188
20
 Y    =       11959206
12  feet           Y    =         3645166
03  meter
 Z    =       16371847
43                 Z    =         4990139
10
 XDOT =     -22184
599024                 XDOT =       -6761
865783
 YDOT =       7419
951622  feet/sec       YDOT =        2261
601255  meter/sec
 ZDOT =       6373
925921                 ZDOT =        1942
772621


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   07064
39865850  
00020000  00000-0  20000-3 0  9077
2 25544  51
6334 280
3390 0025301 283
4570  76
3776 15
77867583 34380


Satellite: ISS
Catalog Number: 25544
Epoch time:      07064
39865850   =   yrday
fracday
Element set:     907
Inclination:       51
6334  deg
RA of node:       280
3390  deg
Eccentricity:     
0025301     
Arg of perigee:   283
4570  deg
Mean anomaly:      76
3776  deg
Mean motion:   15
77867583  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3438
Checksum:              319


Coasting Arc #9 (Orbit 3452)
---------------------------------------

Vector Time (GMT): 2007/065/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         220098
90                 A    =         6721094
36  meter
 Y    =       -6693018
77  meter          E    =           
0023140
 Z    =        -414027
53                 I    =           51
33606
 XDOT =       4838
770329                 Wp   =          314
00563
 YDOT =       -224
112478  meter/sec      RA   =          274
71896  deg
 ZDOT =       6004
024672                 TA   =           41
46157
                                          MA   =           41
28622
                                          Ha   =            187
412  n
mi
                                          Hp   =            174
931

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         722109
26                 X    =          296936
08
 Y    =      -21958722
99  feet           Y    =        -6690127
92  meter
 Z    =       -1358358
04                 Z    =         -412771
06
 XDOT =      15875
230738                 XDOT =        4811
750634
 YDOT =       -735
277158  feet/sec       YDOT =        -170
153175  meter/sec
 ZDOT =      19698
243675                 ZDOT =        6027
465528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21088821
75                 X    =         6427872
87
 Y    =       -6162703
01  feet           Y    =        -1878391
88  meter
 Z    =       -1354541
29                 Z    =         -412864
19
 XDOT =       5171
539612                 XDOT =        1576
285274
 YDOT =      13209
824799  feet/sec       YDOT =        4026
354599  meter/sec
 ZDOT =      19786
269493                 ZDOT =        6030
854941


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   07065
34866335  
00020000  00000-0  20000-3 0  9083
2 25544  51
6337 275
4308 0025381 287
3970  72
4420 15
77878022 34532


Satellite: ISS
Catalog Number: 25544
Epoch time:      07065
34866335   =   yrday
fracday
Element set:     908
Inclination:       51
6337  deg
RA of node:       275
4308  deg
Eccentricity:     
0025381     
Arg of perigee:   287
3970  deg
Mean anomaly:      72
4420  deg
Mean motion:   15
77878022  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3453
Checksum:              307


Coasting Arc #10 (Orbit 3468)
---------------------------------------

Vector Time (GMT): 2007/066/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4141800
54                 A    =         6709218
10  meter
 Y    =       -1078983
99  meter          E    =           
0011719
 Z    =       -5157743
90                 I    =           51
29599
 XDOT =        741
013761                 Wp   =          308
21053
 YDOT =      -7614
277826  meter/sec      RA   =          269
52557  deg
 ZDOT =       1003
457953                 TA   =          331
35050
                                          MA   =          331
41484
                                          Ha   =            187
424  n
mi
                                          Hp   =            174
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13588584
46                 X    =        -4104372
16
 Y    =       -3539973
73  feet           Y    =        -1125091
07  meter
 Z    =      -16921731
95                 Z    =        -5177773
61
 XDOT =       2431
147511                 XDOT =         821
228052
 YDOT =     -24981
226464  feet/sec       YDOT =       -7605
542815  meter/sec
 ZDOT =       3292
184886                 ZDOT =        1007
253223

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1089672
69                 X    =         -332132
24
 Y    =      -13908147
62  feet           Y    =        -4239203
40  meter
 Z    =      -16997120
26                 Z    =        -5180722
26
 XDOT =      23373
224791                 XDOT =        7124
158916
 YDOT =      -5848
312946  feet/sec       YDOT =       -1782
565786  meter/sec
 ZDOT =       3305
411272                 ZDOT =        1007
489356


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   07066
36198151  
00020000  00000-0  20000-3 0  9091
2 25544  51
6341 270
1959 0025373 291
3223  68
5234 15
77936992 34695


Satellite: ISS
Catalog Number: 25544
Epoch time:      07066
36198151   =   yrday
fracday
Element set:     909
Inclination:       51
6341  deg
RA of node:       270
1959  deg
Eccentricity:     
0025373     
Arg of perigee:   291
3223  deg
Mean anomaly:      68
5234  deg
Mean motion:   15
77936992  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3469
Checksum:              318


Coasting Arc #11 (Orbit 3484)
---------------------------------------

Vector Time (GMT): 2007/067/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1087417
98                 A    =         6719048
15  meter
 Y    =        6279833
10  meter          E    =           
0019857
 Z    =       -2122856
24                 I    =           51
33089
 XDOT =      -4684
138848                 Wp   =          287
48425
 YDOT =      -2685
065371  meter/sec      RA   =          264
36439  deg
 ZDOT =      -5495
446862                 TA   =          276
39133
                                          MA   =          276
61743
                                          Ha   =            187
804  n
mi
                                          Hp   =            174
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3567644
28                 X    =        -1147246
75
 Y    =       20603126
96  feet           Y    =         6267338
32  meter
 Z    =       -6964751
44                 Z    =        -2128284
62
 XDOT =     -15367
909606                 XDOT =       -4627
070161
 YDOT =      -8809
269590  feet/sec       YDOT =       -2737
127304  meter/sec
 ZDOT =     -18029
681307                 ZDOT =       -5518
063506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20556832
50                 X    =        -6265722
54
 Y    =        3789589
18  feet           Y    =         1155066
78  meter
 Z    =       -6984292
41                 Z    =        -2128812
33
 XDOT =       3282
702292                 XDOT =        1000
567659
 YDOT =     -15869
150078  feet/sec       YDOT =       -4836
916944  meter/sec
 ZDOT =     -18115
006798                 ZDOT =       -5521
454072


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   07067
37527948  
00020000  00000-0  20000-3 0  9105
2 25544  51
6344 264
9610 0025492 294
9798  64
8720 15
77927968 34851


Satellite: ISS
Catalog Number: 25544
Epoch time:      07067
37527948   =   yrday
fracday
Element set:     910
Inclination:       51
6344  deg
RA of node:       264
9610  deg
Eccentricity:     
0025492     
Arg of perigee:   294
9798  deg
Mean anomaly:      64
8720  deg
Mean motion:   15
77927968  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3485
Checksum:              348


Coasting Arc #12 (Orbit 3500)
---------------------------------------

Vector Time (GMT): 2007/068/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4015628
24                 A    =         6713396
28  meter
 Y    =        3509251
62  meter          E    =           
0019381
 Z    =        4098805
76                 I    =           51
31680
 XDOT =      -1816
059502                 Wp   =          321
28226
 YDOT =       6464
423308  meter/sec      RA   =          259
12988  deg
 ZDOT =      -3750
056085                 TA   =          167
39729
                                          MA   =          167
34877
                                          Ha   =            187
965  n
mi
                                          Hp   =            174
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13174633
34                 X    =         3956177
64
 Y    =       11513292
73  feet           Y    =         3553824
41  meter
 Z    =       13447525
48                 Z    =         4118169
05
 XDOT =      -5958
200467                 XDOT =       -1869
993599
 YDOT =      21208
737886  feet/sec       YDOT =        6443
813376  meter/sec
 ZDOT =     -12303
333613                 ZDOT =       -3759
009787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6011224
09                 X    =        -1832221
10
 Y    =       16371239
48  feet           Y    =         4989953
79  meter
 Z    =       13520743
97                 Z    =         4121122
76
 XDOT =     -20711
455580                 XDOT =       -6312
851661
 YDOT =       2597
718244  feet/sec       YDOT =         791
784521  meter/sec
 ZDOT =     -12336
093316                 ZDOT =       -3760
041243


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   07068
38855554  
00020000  00000-0  20000-3 0  9115
2 25544  51
6343 259
7254 0025556 299
4221  60
4394 15
78012249 35014


Satellite: ISS
Catalog Number: 25544
Epoch time:      07068
38855554   =   yrday
fracday
Element set:     911
Inclination:       51
6343  deg
RA of node:       259
7254  deg
Eccentricity:     
0025556     
Arg of perigee:   299
4221  deg
Mean anomaly:      60
4394  deg
Mean motion:   15
78012249  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3501
Checksum:              301


Coasting Arc #13 (Orbit 3516)
---------------------------------------

Vector Time (GMT): 2007/069/08:20:55
947
Vector Time (MET): N/A
Weight (LBS)     : 478907
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2143928
47                 A    =         6713003
12  meter
 Y    =       -4766083
09  meter          E    =           
0016146
 Z    =        4216367
91                 I    =           51
32223
 XDOT =       4462
422706                 Wp   =          313
43344
 YDOT =       5158
145554  meter/sec      RA   =          253
99030  deg
 ZDOT =       3581
111442                 TA   =          100
11149
                                          MA   =           99
92930
                                          Ha   =            188
180  n
mi
                                          Hp   =            174
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7033886
06                 X    =         2176581
87
 Y    =      -15636755
56  feet           Y    =        -4741925
79  meter
 Z    =       13833228
05                 Z    =         4226862
53
 XDOT =      14640
494443                 XDOT =        4387
015596
 YDOT =      16923
049719  feet/sec       YDOT =        5207
625345  meter/sec
 ZDOT =      11749
053289                 ZDOT =        3602
606495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17105683
03                 X    =         5213812
19
 Y    =         552140
36  feet           Y    =          168292
38  meter
 Z    =       13872008
68                 Z    =         4228188
24
 XDOT =     -10143
638352                 XDOT =       -3091
780970
 YDOT =      18629
785822  feet/sec       YDOT =        5678
358719  meter/sec
 ZDOT =      11830
508569                 ZDOT =        3605
939012


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   07069
40181228  
00020000  00000-0  20000-3 0  9120
2 25544  51
6345 254
4891 0025539 303
4682  56
4042 15
78001783 35176


Satellite: ISS
Catalog Number: 25544
Epoch time:      07069
40181228   =   yrday
fracday
Element set:     912
Inclination:       51
6345  deg
RA of node:       254
4891  deg
Eccentricity:     
0025539     
Arg of perigee:   303
4682  deg
Mean anomaly:      56
4042  deg
Mean motion:   15
78001783  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3517
Checksum:              288

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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