Date: October 2nd 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6727 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1008)
---------------------------------------

Vector Time (GMT): 2006/275/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3993029
74                 A    =         6716499
42  meter
 Y    =        3110979
08  meter          E    =           
0018581
 Z    =        4396645
99                 I    =           51
59701
 XDOT =      -6174
066549                 Wp   =           75
81197
 YDOT =       3239
118165  meter/sec      RA   =          354
41047  deg
 ZDOT =       3308
235870                 TA   =          340
99022
                                          MA   =          341
05948
                                          Ha   =            190
363  n
mi
                                          Hp   =            176
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13100491
28                 X    =         3936587
43
 Y    =       10206624
28  feet           Y    =         3155315
84  meter
 Z    =       14424691
56                 Z    =         4415907
00
 XDOT =     -20256
123847                 XDOT =       -6225
898784
 YDOT =      10627
028100  feet/sec       YDOT =        3169
786582  meter/sec
 ZDOT =      10853
792224                 ZDOT =        3278
116252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12140383
52                 X    =        -3700388
90
 Y    =      -11239301
93  feet           Y    =        -3425739
23  meter
 Z    =       14496860
27                 Z    =         4418643
01
 XDOT =      20298
744216                 XDOT =        6187
057237
 YDOT =      -8040
783835  feet/sec       YDOT =       -2450
830913  meter/sec
 ZDOT =      10741
998891                 ZDOT =        3274
161262


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   06275
51168061  
00020000  00000-0  20000-3 0  9007
2 25544  51
6376 354
5896 0012275  50
8487 309
3767 15
76508466 10092


Satellite: ISS
Catalog Number: 25544
Epoch time:      06275
51168061   =   yrday
fracday
Element set:     900
Inclination:       51
6376  deg
RA of node:       354
5896  deg
Eccentricity:     
0012275     
Arg of perigee:    50
8487  deg
Mean anomaly:     309
3767  deg
Mean motion:   15
76508466  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1009
Checksum:              311


Coasting Arc #2 (Orbit 1023)
---------------------------------------

Vector Time (GMT): 2006/276/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5703562
66                 A    =         6723161
97  meter
 Y    =       -2825245
54  meter          E    =           
0018683
 Z    =       -2153705
96                 I    =           51
59088
 XDOT =       3901
496252                 Wp   =           48
79769
 YDOT =       3706
258452  meter/sec      RA   =          349
21030  deg
 ZDOT =       5513
170413                 TA   =          287
05806
                                          MA   =          287
26265
                                          Ha   =            190
602  n
mi
                                          Hp   =            176
019

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18712475
92                 X    =         5745193
37
 Y    =       -9269178
27  feet           Y    =        -2761232
46  meter
 Z    =       -7065964
42                 Z    =        -2125896
78
 XDOT =      12800
184555                 XDOT =        3832
980383
 YDOT =      12159
640590  feet/sec       YDOT =        3749
504298  meter/sec
 ZDOT =      18087
829438                 ZDOT =        5531
957305

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19312439
39                 X    =        -5886431
52
 Y    =        8034450
90  feet           Y    =         2448900
63  meter
 Z    =       -6962726
32                 Z    =        -2122238
98
 XDOT =     -11299
633187                 XDOT =       -3444
128195
 YDOT =     -11548
617453  feet/sec       YDOT =       -3520
018600  meter/sec
 ZDOT =      18158
314103                 ZDOT =        5534
654138


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   06276
46251659  
00020000  00000-0  20000-3 0  9019
2 25544  51
6376 349
6892 0012396  53
2591 306
9710 15
76477635 10241


Satellite: ISS
Catalog Number: 25544
Epoch time:      06276
46251659   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       349
6892  deg
Eccentricity:     
0012396     
Arg of perigee:    53
2591  deg
Mean anomaly:     306
9710  deg
Mean motion:   15
76477635  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1024
Checksum:              312


Coasting Arc #3 (Orbit 1039)
---------------------------------------

Vector Time (GMT): 2006/277/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2742530
35                 A    =         6713653
96  meter
 Y    =       -3431456
88  meter          E    =           
0025803
 Z    =       -5099794
34                 I    =           51
53107
 XDOT =       6822
883437                 Wp   =           68
34143
 YDOT =      -3197
278255  meter/sec      RA   =          344
08206  deg
 ZDOT =      -1514
608185                 TA   =          187
06194
                                          MA   =          187
09836
                                          Ha   =            190
515  n
mi
                                          Hp   =            175
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8997802
98                 X    =        -2679181
54
 Y    =      -11258060
63  feet           Y    =        -3461771
54  meter
 Z    =      -16731608
74                 Z    =        -5112963
47
 XDOT =      22384
788178                 XDOT =        6865
486467
 YDOT =     -10489
758054  feet/sec       YDOT =       -3120
742896  meter/sec
 ZDOT =      -4969
186960                 ZDOT =       -1481
358812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8359036
48                 X    =         2547834
32
 Y    =       11669246
67  feet           Y    =         3556786
38  meter
 Z    =      -16781129
58                 Z    =        -5114888
30
 XDOT =     -22035
115487                 XDOT =       -6716
303200
 YDOT =       8800
771016  feet/sec       YDOT =        2682
475006  meter/sec
 ZDOT =      -4845
733187                 ZDOT =       -1476
979475


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   06277
47671913  
00020000  00000-0  20000-3 0  9021
2 25544  51
6370 344
4610 0012333  57
5053 302
7301 15
76524118 10404


Satellite: ISS
Catalog Number: 25544
Epoch time:      06277
47671913   =   yrday
fracday
Element set:     902
Inclination:       51
6370  deg
RA of node:       344
4610  deg
Eccentricity:     
0012333     
Arg of perigee:    57
5053  deg
Mean anomaly:     302
7301  deg
Mean motion:   15
76524118  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1040
Checksum:              257


Coasting Arc #4 (Orbit 1055)
---------------------------------------

Vector Time (GMT): 2006/278/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6121345
82                 A    =         6724779
61  meter
 Y    =        2741416
55  meter          E    =           
0021024
 Z    =         446058
61                 I    =           51
54148
 XDOT =      -2341
468079                 Wp   =           96
38248
 YDOT =      -4211
728186  meter/sec      RA   =          338
90286  deg
 ZDOT =      -6008
444592                 TA   =           78
75633
                                          MA   =           78
52010
                                          Ha   =            190
550  n
mi
                                          Hp   =            175
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20083155
58                 X    =        -6153712
66
 Y    =        8994148
79  feet           Y    =         2672783
34  meter
 Z    =        1463446
89                 Z    =          416242
01
 XDOT =      -7681
981887                 XDOT =       -2265
009758
 YDOT =     -13818
005858  feet/sec       YDOT =       -4237
484839  meter/sec
 ZDOT =     -19712
744724                 ZDOT =       -6019
633421

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20355403
84                 X    =         6204327
09
 Y    =       -8378376
38  feet           Y    =        -2553729
12  meter
 Z    =        1352727
38                 Z    =          412311
31
 XDOT =       6538
006767                 XDOT =        1992
784463
 YDOT =      12557
560258  feet/sec       YDOT =        3827
544366  meter/sec
 ZDOT =     -19754
993032                 ZDOT =       -6021
321876


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   06278
49089965  
00020000  00000-0  20000-3 0  9035
2 25544  51
6363 339
2326 0012546  61
4868 298
7558 15
76577291 10561


Satellite: ISS
Catalog Number: 25544
Epoch time:      06278
49089965   =   yrday
fracday
Element set:     903
Inclination:       51
6363  deg
RA of node:       339
2326  deg
Eccentricity:     
0012546     
Arg of perigee:    61
4868  deg
Mean anomaly:     298
7558  deg
Mean motion:   15
76577291  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1056
Checksum:              338


Coasting Arc #5 (Orbit 1071)
---------------------------------------

Vector Time (GMT): 2006/279/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1360054
24                 A    =         6712633
27  meter
 Y    =        3970046
41  meter          E    =           
0015153
 Z    =        5227819
18                 I    =           51
47548
 XDOT =      -7066
481970                 Wp   =           64
67941
 YDOT =       3061
422556  meter/sec      RA   =          333
73783  deg
 ZDOT =       -479
005139                 TA   =           29
91508
                                          MA   =           29
82856
                                          Ha   =            190
395  n
mi
                                          Hp   =            175
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4462120
21                 X    =         1290163
37
 Y    =       13025086
66  feet           Y    =         3984865
02  meter
 Z    =       17151637
72                 Z    =         5234256
27
 XDOT =     -23183
995963                 XDOT =       -7097
863067
 YDOT =      10044
037256  feet/sec       YDOT =        2982
225730  meter/sec
 ZDOT =      -1571
539169                 ZDOT =        -513
411129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4194548
18                 X    =        -1278498
28
 Y    =      -13081578
24  feet           Y    =        -3987265
05  meter
 Z    =       17176150
67                 Z    =         5235290
73
 XDOT =      22352
031346                 XDOT =        6812
899154
 YDOT =      -9430
395772  feet/sec       YDOT =       -2874
384631  meter/sec
 ZDOT =      -1699
308539                 ZDOT =        -517
949243


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   06279
50505554  
00020000  00000-0  20000-3 0  9046
2 25544  51
6366 334
0037 0012406  64
6488 295
5959 15
76650691 10728


Satellite: ISS
Catalog Number: 25544
Epoch time:      06279
50505554   =   yrday
fracday
Element set:     904
Inclination:       51
6366  deg
RA of node:       334
0037  deg
Eccentricity:     
0012406     
Arg of perigee:    64
6488  deg
Mean anomaly:     295
5959  deg
Mean motion:   15
76650691  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1072
Checksum:              306


Coasting Arc #6 (Orbit 1087)
---------------------------------------

Vector Time (GMT): 2006/280/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6085636
73                 A    =         6723988
25  meter
 Y    =       -2529717
35  meter          E    =           
0026638
 Z    =        1272696
81                 I    =           51
48781
 XDOT =        819
359338                 Wp   =           63
16130
 YDOT =       4956
533090  meter/sec      RA   =          328
58805  deg
 ZDOT =       5852
288950                 TA   =          310
86211
                                          MA   =          311
09267
                                          Ha   =            190
573  n
mi
                                          Hp   =            175
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19965999
76                 X    =         6107289
41
 Y    =       -8299597
59  feet           Y    =        -2461543
21  meter
 Z    =        4175514
48                 Z    =         1302314
26
 XDOT =       2688
186803                 XDOT =         735
443835
 YDOT =      16261
591504  feet/sec       YDOT =        4965
226902  meter/sec
 ZDOT =      19200
423063                 ZDOT =        5856
065243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19909646
69                 X    =        -6068460
31
 Y    =        8378528
58  feet           Y    =         2553775
51  meter
 Z    =        4285512
29                 Z    =         1306224
15
 XDOT =      -2035
591478                 XDOT =        -620
448283
 YDOT =     -14799
181847  feet/sec       YDOT =       -4510
790627  meter/sec
 ZDOT =      19215
153565                 ZDOT =        5856
778807


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   06280
51919321  
00020000  00000-0  20000-3 0  9051
2 25544  51
6357 328
7751 0012717  68
2350 292
0166 15
76625678 10880


Satellite: ISS
Catalog Number: 25544
Epoch time:      06280
51919321   =   yrday
fracday
Element set:     905
Inclination:       51
6357  deg
RA of node:       328
7751  deg
Eccentricity:     
0012717     
Arg of perigee:    68
2350  deg
Mean anomaly:     292
0166  deg
Mean motion:   15
76625678  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1088
Checksum:              303


Coasting Arc #7 (Orbit 1102)
---------------------------------------

Vector Time (GMT): 2006/281/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -92140
21                 A    =         6714518
93  meter
 Y    =       -4707081
27  meter          E    =           
0023360
 Z    =       -4807310
40                 I    =           51
43196
 XDOT =       6800
733205                 Wp   =           88
68534
 YDOT =      -2621
755054  meter/sec      RA   =          323
38688  deg
 ZDOT =       2447
505060                 TA   =          205
28276
                                          MA   =          205
39727
                                          Ha   =            190
541  n
mi
                                          Hp   =            175
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -302297
26                 X    =          -16144
49
 Y    =      -15443180
02  feet           Y    =        -4707686
97  meter
 Z    =      -15772015
74                 Z    =        -4807573
18
 XDOT =      22312
116815                 XDOT =        6817
654747
 YDOT =      -8601
558577  feet/sec       YDOT =       -2545
610746  meter/sec
 ZDOT =       8029
872243                 ZDOT =        2480
585090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         541985
53                 X    =          165197
19
 Y    =       15434986
66  feet           Y    =         4704583
93  meter
 Z    =      -15773620
76                 Z    =        -4807799
61
 XDOT =     -20954
946158                 XDOT =       -6387
067589
 YDOT =       9031
367015  feet/sec       YDOT =        2752
760666  meter/sec
 ZDOT =       8152
757028                 ZDOT =        2484
960342


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   06281
46992373  
00020000  00000-0  20000-3 0  9065
2 25544  51
6350 323
8726 0012734  71
6151 288
6397 15
76679082 11030


Satellite: ISS
Catalog Number: 25544
Epoch time:      06281
46992373   =   yrday
fracday
Element set:     906
Inclination:       51
6350  deg
RA of node:       323
8726  deg
Eccentricity:     
0012734     
Arg of perigee:    71
6151  deg
Mean anomaly:     288
6397  deg
Mean motion:   15
76679082  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1103
Checksum:              307


Coasting Arc #8 (Orbit 1118)
---------------------------------------

Vector Time (GMT): 2006/282/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5721156
33                 A    =         6720537
65  meter
 Y    =        1940934
88  meter          E    =           
0016778
 Z    =       -2960499
34                 I    =           51
43112
 XDOT =        582
836004                 Wp   =           84
02231
 YDOT =      -5837
894501  meter/sec      RA   =          318
25886  deg
 ZDOT =      -4976
134096                 TA   =          130
22813
                                          MA   =          130
08121
                                          Ha   =            190
524  n
mi
                                          Hp   =            174
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18770197
93                 X    =        -5728052
98
 Y    =        6367896
58  feet           Y    =         1876919
12  meter
 Z    =       -9712924
34                 Z    =        -2988310
22
 XDOT =       1912
191614                 XDOT =         672
246611
 YDOT =     -19153
197183  feet/sec       YDOT =       -5830
877084  meter/sec
 ZDOT =     -16325
899266                 ZDOT =       -4973
085309

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18458312
75                 X    =         5626093
73
 Y    =       -7081158
61  feet           Y    =        -2158337
14  meter
 Z    =       -9816273
21                 Z    =        -2992000
07
 XDOT =      -1782
549442                 XDOT =        -543
321070
 YDOT =      17869
715066  feet/sec       YDOT =        5446
689152  meter/sec
 ZDOT =     -16315
313235                 ZDOT =       -4972
907474


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   06282
48401562  
00020000  00000-0  20000-3 0  9074
2 25544  51
6352 318
6424 0012851  75
6390 284
6200 15
76722122 11198


Satellite: ISS
Catalog Number: 25544
Epoch time:      06282
48401562   =   yrday
fracday
Element set:     907
Inclination:       51
6352  deg
RA of node:       318
6424  deg
Eccentricity:     
0012851     
Arg of perigee:    75
6390  deg
Mean anomaly:     284
6200  deg
Mean motion:   15
76722122  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1119
Checksum:              274


Coasting Arc #9 (Orbit 1134)
---------------------------------------

Vector Time (GMT): 2006/283/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1017714
98                 A    =         6718154
91  meter
 Y    =        5471339
25  meter          E    =           
0024415
 Z    =        3745949
07                 I    =           51
40290
 XDOT =      -6224
482048                 Wp   =           80
52198
 YDOT =       1742
963084  meter/sec      RA   =          313
03548  deg
 ZDOT =      -4209
662756                 TA   =           53
87862
                                          MA   =           53
65287
                                          Ha   =            190
446  n
mi
                                          Hp   =            174
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3338959
90                 X    =        -1097018
18
 Y    =       17950588
09  feet           Y    =         5459515
16  meter
 Z    =       12289859
15                 Z    =         3740812
30
 XDOT =     -20421
529029                 XDOT =       -6223
059231
 YDOT =       5718
382821  feet/sec       YDOT =        1673
365461  meter/sec
 ZDOT =     -13811
229515                 ZDOT =       -4239
898518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2404559
70                 X    =          732909
80
 Y    =      -18111949
34  feet           Y    =        -5520522
16  meter
 Z    =       12271441
96                 Z    =         3740335
51
 XDOT =      18675
276201                 XDOT =        5692
224186
 YDOT =      -7014
943523  feet/sec       YDOT =       -2138
154786  meter/sec
 ZDOT =     -13923
643453                 ZDOT =       -4243
926525


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   06283
49808294  
00020000  00000-0  20000-3 0  9080
2 25544  51
6350 313
4127 0012769  78
7734 281
4865 15
76784054 11355


Satellite: ISS
Catalog Number: 25544
Epoch time:      06283
49808294   =   yrday
fracday
Element set:     908
Inclination:       51
6350  deg
RA of node:       313
4127  deg
Eccentricity:     
0012769     
Arg of perigee:    78
7734  deg
Mean anomaly:     281
4865  deg
Mean motion:   15
76784054  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1135
Checksum:              317


Coasting Arc #10 (Orbit 1150)
---------------------------------------

Vector Time (GMT): 2006/284/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5085267
46                 A    =         6716213
52  meter
 Y    =        -998613
01  meter          E    =           
0022225
 Z    =        4253814
86                 I    =           51
37785
 XDOT =      -1641
204258                 Wp   =           93
50565
 YDOT =       6673
074575  meter/sec      RA   =          307
91173  deg
 ZDOT =       3511
487347                 TA   =          320
79372
                                          MA   =          320
95451
                                          Ha   =            190
403  n
mi
                                          Hp   =            174
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16683948
35                 X    =         5075391
49
 Y    =       -3276289
39  feet           Y    =         -941802
04  meter
 Z    =       13956085
49                 Z    =         4278495
54
 XDOT =      -5384
528406                 XDOT =       -1732
760014
 YDOT =      21893
289288  feet/sec       YDOT =        6654
209731  meter/sec
 ZDOT =      11520
627778                 ZDOT =        3503
291976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16324523
76                 X    =        -4975714
84
 Y    =        4475125
55  feet           Y    =         1364018
27  meter
 Z    =       14047907
39                 Z    =         4281802
17
 XDOT =       4168
233485                 XDOT =        1270
477566
 YDOT =     -21040
915329  feet/sec       YDOT =       -6413
270992  meter/sec
 ZDOT =      11490
970207                 ZDOT =        3502
447719


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   06284
51212951  
00020000  00000-0  20000-3 0  9094
2 25544  51
6346 308
1828 0012980  83
0659 277
1982 15
76794104 11516


Satellite: ISS
Catalog Number: 25544
Epoch time:      06284
51212951   =   yrday
fracday
Element set:     909
Inclination:       51
6346  deg
RA of node:       308
1828  deg
Eccentricity:     
0012980     
Arg of perigee:    83
0659  deg
Mean anomaly:     277
1982  deg
Mean motion:   15
76794104  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1151
Checksum:              302


Coasting Arc #11 (Orbit 1165)
---------------------------------------

Vector Time (GMT): 2006/285/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1764606
04                 A    =         6721869
59  meter
 Y    =       -6083693
89  meter          E    =           
0017853
 Z    =       -2254298
98                 I    =           51
38185
 XDOT =       5433
265611                 Wp   =           73
06344
 YDOT =       -423
938120  meter/sec      RA   =          302
69086  deg
 ZDOT =       5437
660049                 TA   =          261
52488
                                          MA   =          261
72727
                                          Ha   =            190
440  n
mi
                                          Hp   =            174
682

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5789389
91                 X    =         1843454
73
 Y    =      -19959625
64  feet           Y    =        -6063520
17  meter
 Z    =       -7395994
02                 Z    =        -2245535
02
 XDOT =      17825
674578                 XDOT =        5411
186792
 YDOT =      -1390
873096  feet/sec       YDOT =        -363
303912  meter/sec
 ZDOT =      17840
092025                 ZDOT =        5464
001584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4013209
45                 X    =        -1223226
24
 Y    =       20402647
29  feet           Y    =         6218726
89  meter
 Z    =       -7364139
62                 Z    =        -2244589
76
 XDOT =     -16042
479855                 XDOT =       -4889
747860
 YDOT =       3270
817125  feet/sec       YDOT =         996
945060  meter/sec
 ZDOT =      17938
183405                 ZDOT =        5467
558302


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   06285
46277661  
00020000  00000-0  20000-3 0  9100
2 25544  51
6355 303
2800 0013001  86
6614 273
6038 15
76850272 11665


Satellite: ISS
Catalog Number: 25544
Epoch time:      06285
46277661   =   yrday
fracday
Element set:     910
Inclination:       51
6355  deg
RA of node:       303
2800  deg
Eccentricity:     
0013001     
Arg of perigee:    86
6614  deg
Mean anomaly:     273
6038  deg
Mean motion:   15
76850272  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1166
Checksum:              277


Coasting Arc #12 (Orbit 1181)
---------------------------------------

Vector Time (GMT): 2006/286/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4393521
27                 A    =         6712767
60  meter
 Y    =        -373879
45  meter          E    =           
0026676
 Z    =       -5084920
97                 I    =           51
33716
 XDOT =       2361
446913                 Wp   =           84
00276
 YDOT =      -7154
377920  meter/sec      RA   =          297
54593  deg
 ZDOT =      -1518
404576                 TA   =          171
36396
                                          MA   =          171
31797
                                          Ha   =            190
419  n
mi
                                          Hp   =            174
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14414439
86                 X    =        -4364312
09
 Y    =       -1226638
60  feet           Y    =         -422846
83  meter
 Z    =      -16682811
58                 Z    =        -5106193
96
 XDOT =       7747
529241                 XDOT =        2448
648858
 YDOT =     -23472
368503  feet/sec       YDOT =       -7127
483316  meter/sec
 ZDOT =      -4981
642310                 ZDOT =       -1506
720857

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14371161
74                 X    =         4380330
10
 Y    =        -312565
67  feet           Y    =          -95270
02  meter
 Z    =      -16762127
97                 Z    =        -5109096
60
 XDOT =      -5242
335595                 XDOT =       -1597
863889
 YDOT =      23121
341116  feet/sec       YDOT =        7047
384772  meter/sec
 ZDOT =      -4939
051252                 ZDOT =       -1505
422821


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   06286
47677704  
00020000  00000-0  20000-3 0  9115
2 25544  51
6358 298
0496 0012933  90
3322 269
9325 15
76844243 11827


Satellite: ISS
Catalog Number: 25544
Epoch time:      06286
47677704   =   yrday
fracday
Element set:     911
Inclination:       51
6358  deg
RA of node:       298
0496  deg
Eccentricity:     
0012933     
Arg of perigee:    90
3322  deg
Mean anomaly:     269
9325  deg
Mean motion:   15
76844243  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1182
Checksum:              314

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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