Date: October 20th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 3767 37 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


299/14:46:00 000 0 0 0 0 0 0
N/A 0 0 0 0 189 1
000/00:00:00 000 0 0 0 0 175 3

Coasting Arc #1 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2006/293/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         163278
23                 A    =         6723067
46  meter
 Y    =        6628951
68  meter          E    =           
0021746
 Z    =       -1070090
85                 I    =           51
33679
 XDOT =      -4898
819344                 Wp   =          127
25383
 YDOT =       -815
435068  meter/sec      RA   =          261
17040  deg
 ZDOT =      -5893
779714                 TA   =           64
51917
                                          MA   =           64
29437
                                          Ha   =            189
906  n
mi
                                          Hp   =            174
784

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         535689
75                 X    =           94338
67
 Y    =       21748529
12  feet           Y    =         6630392
02  meter
 Z    =       -3510796
77                 Z    =        -1069465
46
 XDOT =     -16072
241943                 XDOT =       -4860
705374
 YDOT =      -2675
311904  feet/sec       YDOT =        -870
003611  meter/sec
 ZDOT =     -19336
547618                 ZDOT =       -5917
486089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8421668
63                 X    =        -2566924
60
 Y    =      -20059505
81  feet           Y    =        -6114137
37  meter
 Z    =       -3507549
07                 Z    =        -1069100
96
 XDOT =      14382
940676                 XDOT =        4383
920318
 YDOT =      -2696
329823  feet/sec       YDOT =        -821
841330  meter/sec
 ZDOT =     -19425
008720                 ZDOT =       -5920
742658


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   06293
51095707  
00020000  00000-0  20000-3 0  9003
2 25544  51
6306 261
7734 0012659 116
0004 244
2466 15
77030684 12932


Satellite: ISS
Catalog Number: 25544
Epoch time:      06293
51095707   =   yrday
fracday
Element set:     900
Inclination:       51
6306  deg
RA of node:       261
7734  deg
Eccentricity:     
0012659     
Arg of perigee:   116
0004  deg
Mean anomaly:     244
2466  deg
Mean motion:   15
77030684  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1293
Checksum:              277


Coasting Arc #2 (Orbit 1308)
---------------------------------------

Vector Time (GMT): 2006/294/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4377027
94                 A    =         6713201
58  meter
 Y    =        1581429
71  meter          E    =           
0016809
 Z    =        4822921
33                 I    =           51
30931
 XDOT =        -84
744502                 Wp   =           99
29179
 YDOT =       7357
169652  meter/sec      RA   =          255
95966  deg
 ZDOT =      -2331
295835                 TA   =           13
49759
                                          MA   =           13
45269
                                          Ha   =            189
683  n
mi
                                          Hp   =            174
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14360327
90                 X    =         4335589
35
 Y    =        5188417
67  feet           Y    =         1630144
59  meter
 Z    =       15823232
71                 Z    =         4844084
77
 XDOT =       -278
033142                 XDOT =        -155
681775
 YDOT =      24137
695710  feet/sec       YDOT =        7355
825255  meter/sec
 ZDOT =      -7648
608382                 ZDOT =       -2331
880186

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15174026
92                 X    =        -4625043
40
 Y    =         615131
50  feet           Y    =          187492
08  meter
 Z    =       15902324
01                 Z    =         4847028
36
 XDOT =      -8895
410325                 XDOT =       -2711
321067
 YDOT =     -21315
792800  feet/sec       YDOT =       -6497
053646  meter/sec
 ZDOT =      -7649
768079                 ZDOT =       -2331
649310


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   06294
52482841  
00020000  00000-0  20000-3 0  9015
2 25544  51
6305 256
5424 0012521 120
0641 240
1767 15
77052704 13093


Satellite: ISS
Catalog Number: 25544
Epoch time:      06294
52482841   =   yrday
fracday
Element set:     901
Inclination:       51
6305  deg
RA of node:       256
5424  deg
Eccentricity:     
0012521     
Arg of perigee:   120
0641  deg
Mean anomaly:     240
1767  deg
Mean motion:   15
77052704  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1309
Checksum:              260


Coasting Arc #3 (Orbit 1324)
---------------------------------------

Vector Time (GMT): 2006/295/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         372579
48                 A    =         6719629
67  meter
 Y    =       -6034923
60  meter          E    =           
0024222
 Z    =        2918090
79                 I    =           51
34039
 XDOT =       5187
138414                 Wp   =          102
75663
 YDOT =       2753
985900  meter/sec      RA   =          250
82142  deg
 ZDOT =       4993
193763                 TA   =          291
06538
                                          MA   =          291
32423
                                          Ha   =            189
680  n
mi
                                          Hp   =            174
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1222373
61                 X    =          425859
15
 Y    =      -19799618
13  feet           Y    =        -6030459
23  meter
 Z    =        9573788
68                 Z    =         2920030
44
 XDOT =      17018
170651                 XDOT =        5131
700672
 YDOT =       9035
386812  feet/sec       YDOT =        2811
681540  meter/sec
 ZDOT =      16381
869302                 ZDOT =        5018
258897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6752222
41                 X    =         2058077
39
 Y    =       18649506
04  feet           Y    =         5684369
44  meter
 Z    =        9580183
81                 Z    =         2920040
03
 XDOT =     -17760
411020                 XDOT =       -5413
373279
 YDOT =      -2100
632091  feet/sec       YDOT =        -640
272661  meter/sec
 ZDOT =      16475
665644                 ZDOT =        5021
782888


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   06295
53868411  
00020000  00000-0  20000-3 0  9029
2 25544  51
6313 251
3115 0012568 124
6653 235
5698 15
77110534 13251


Satellite: ISS
Catalog Number: 25544
Epoch time:      06295
53868411   =   yrday
fracday
Element set:     902
Inclination:       51
6313  deg
RA of node:       251
3115  deg
Eccentricity:     
0012568     
Arg of perigee:   124
6653  deg
Mean anomaly:     235
5698  deg
Mean motion:   15
77110534  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1325
Checksum:              282


Coasting Arc #4 (Orbit 1339)
---------------------------------------

Vector Time (GMT): 2006/296/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4668126
35                 A    =         6717429
29  meter
 Y    =       -3139494
39  meter          E    =           
0017976
 Z    =       -3692177
11                 I    =           51
34355
 XDOT =        882
035469                 Wp   =          119
47425
 YDOT =      -6330
898968  meter/sec      RA   =          245
58970  deg
 ZDOT =       4274
950650                 TA   =          195
88682
                                          MA   =          195
94328
                                          Ha   =            189
658  n
mi
                                          Hp   =            174
979

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15315375
16                 X    =        -4614736
64
 Y    =      -10300178
45  feet           Y    =        -3191397
49  meter
 Z    =      -12113441
98                 Z    =        -3714725
88
 XDOT =       2893
817157                 XDOT =         931
995306
 YDOT =     -20770
665907  feet/sec       YDOT =       -6320
756182  meter/sec
 ZDOT =      14025
428642                 ZDOT =        4279
357127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18134263
34                 X    =         5527323
47
 Y    =        3122372
70  feet           Y    =          951699
20  meter
 Z    =      -12197915
83                 Z    =        -3717924
75
 XDOT =       6197
549389                 XDOT =        1889
013054
 YDOT =      18770
389019  feet/sec       YDOT =        5721
214573  meter/sec
 ZDOT =      14040
979736                 ZDOT =        4279
690624


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   06296
48916324  
00020000  00000-0  20000-3 0  9032
2 25544  51
6314 246
4068 0012454 127
2369 232
9933 15
77072753 13401


Satellite: ISS
Catalog Number: 25544
Epoch time:      06296
48916324   =   yrday
fracday
Element set:     903
Inclination:       51
6314  deg
RA of node:       246
4068  deg
Eccentricity:     
0012454     
Arg of perigee:   127
2369  deg
Mean anomaly:     232
9933  deg
Mean motion:   15
77072753  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1340
Checksum:              295


Coasting Arc #5 (Orbit 1355)
---------------------------------------

Vector Time (GMT): 2006/297/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1265047
29                 A    =         6714817
63  meter
 Y    =        4916923
21  meter          E    =           
0018804
 Z    =       -4407444
05                 I    =           51
34886
 XDOT =      -5459
244570                 Wp   =          105
12014
 YDOT =      -4323
844137  meter/sec      RA   =          240
45905  deg
 ZDOT =      -3273
153185                 TA   =          131
95835
                                          MA   =          131
79796
                                          Ha   =            189
506  n
mi
                                          Hp   =            175
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4150417
60                 X    =        -1298523
74
 Y    =       16131637
82  feet           Y    =         4902589
63  meter
 Z    =      -14460118
28                 Z    =        -4413671
09
 XDOT =     -17910
907382                 XDOT =       -5394
588107
 YDOT =     -14185
840344  feet/sec       YDOT =       -4384
530876  meter/sec
 ZDOT =     -10738
691551                 ZDOT =       -3299
518043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3201082
38                 X    =         -975689
91
 Y    =      -16326559
66  feet           Y    =        -4976335
38  meter
 Z    =      -14482653
32                 Z    =        -4414312
73
 XDOT =      21006
817414                 XDOT =        6402
877948
 YDOT =       5447
097068  feet/sec       YDOT =        1660
275186  meter/sec
 ZDOT =     -10837
555910                 ZDOT =       -3303
287041


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   06297
50299187  
00020000  00000-0  20000-3 0  9048
2 25544  51
6323 241
1750 0012436 131
1765 229
0474 15
77121757 13568


Satellite: ISS
Catalog Number: 25544
Epoch time:      06297
50299187   =   yrday
fracday
Element set:     904
Inclination:       51
6323  deg
RA of node:       241
1750  deg
Eccentricity:     
0012436     
Arg of perigee:   131
1765  deg
Mean anomaly:     229
0474  deg
Mean motion:   15
77121757  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1356
Checksum:              288


Coasting Arc #6 (Orbit 1371)
---------------------------------------

Vector Time (GMT): 2006/298/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4815575
83                 A    =         6721642
94  meter
 Y    =        4259038
65  meter          E    =           
0026051
 Z    =        1913004
16                 I    =           51
38756
 XDOT =      -2069
027326                 Wp   =          123
12323
 YDOT =       4877
824986  meter/sec      RA   =          235
23850  deg
 ZDOT =      -5610
656237                 TA   =           35
46888
                                          MA   =           35
29593
                                          Ha   =            189
387  n
mi
                                          Hp   =            175
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15799133
30                 X    =         4758299
46
 Y    =       13973223
91  feet           Y    =         4312568
77  meter
 Z    =        6276260
37                 Z    =         1936259
95
 XDOT =      -6788
147395                 XDOT =       -2096
161703
 YDOT =      16003
362816  feet/sec       YDOT =        4854
536465  meter/sec
 ZDOT =     -18407
664820                 ZDOT =       -5620
773605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20317757
86                 X    =        -6192852
60
 Y    =       -5563201
06  feet           Y    =        -1695663
68  meter
 Z    =        6363533
08                 Z    =         1939604
88
 XDOT =      -1484
109748                 XDOT =        -452
356651
 YDOT =     -15829
047411  feet/sec       YDOT =       -4824
693651  meter/sec
 ZDOT =     -18444
710698                 ZDOT =       -5621
947821


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   06298
51680620  
00020000  00000-0  20000-3 0  9057
2 25544  51
6326 235
9440 0012418 135
0221 225
1952 15
77133478 13727


Satellite: ISS
Catalog Number: 25544
Epoch time:      06298
51680620   =   yrday
fracday
Element set:     905
Inclination:       51
6326  deg
RA of node:       235
9440  deg
Eccentricity:     
0012418     
Arg of perigee:   135
0221  deg
Mean anomaly:     225
1952  deg
Mean motion:   15
77133478  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1372
Checksum:              276


Coasting Arc #7 (Orbit 1387)
---------------------------------------

Vector Time (GMT): 2006/299/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2407322
49                 A    =         6711379
44  meter
 Y    =       -3545420
44  meter          E    =           
0015940
 Z    =        5157258
86                 I    =           51
37098
 XDOT =       5515
948453                 Wp   =          136
06769
 YDOT =       5289
004581  meter/sec      RA   =          230
08824  deg
 ZDOT =       1047
972042                 TA   =          303
84103
                                          MA   =          303
99264
                                          Ha   =            189
172  n
mi
                                          Hp   =            175
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7898039
67                 X    =         2421735
27
 Y    =      -11631956
81  feet           Y    =        -3518420
11  meter
 Z    =       16920140
61                 Z    =         5168988
76
 XDOT =      18096
943745                 XDOT =        5451
305117
 YDOT =      17352
377234  feet/sec       YDOT =        5350
325480  meter/sec
 ZDOT =       3438
228485                 ZDOT =        1074
612478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1618101
64                 X    =         -493197
38
 Y    =       13913947
15  feet           Y    =         4240971
09  meter
 Z    =       16963384
98                 Z    =         5170439
74
 XDOT =     -22998
941635                 XDOT =       -7010
077410
 YDOT =      -7041
283314  feet/sec       YDOT =       -2146
183154  meter/sec
 ZDOT =       3538
268181                 ZDOT =        1078
464142


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   06299
53060353  
00020000  00000-0  20000-3 0  9066
2 25544  51
6327 230
7135 0012276 139
6825 220
5252 15
77199869 13889


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
53060353   =   yrday
fracday
Element set:     906
Inclination:       51
6327  deg
RA of node:       230
7135  deg
Eccentricity:     
0012276     
Arg of perigee:   139
6825  deg
Mean anomaly:     220
5252  deg
Mean motion:   15
77199869  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1388
Checksum:              307


Coasting Arc #8 (Orbit 1389)
---------------------------------------

Vector Time (GMT): 2006/299/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4990221
15                 A    =         6714250
93  meter
 Y    =         342078
34  meter          E    =           
0017126
 Z    =        4462135
36                 I    =           51
38493
 XDOT =       2370
645702                 Wp   =          110
05370
 YDOT =       6632
312346  meter/sec      RA   =          229
36215  deg
 ZDOT =      -3155
698285                 TA   =           11
51945
                                          MA   =           11
48031
                                          Ha   =            189
088  n
mi
                                          Hp   =            175
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16372116
64                 X    =         4964348
30
 Y    =        1122304
27  feet           Y    =          397736
86  meter
 Z    =       14639551
69                 Z    =         4486315
64
 XDOT =       7777
708996                 XDOT =        2311
636275
 YDOT =      21759
554941  feet/sec       YDOT =        6658
492453  meter/sec
 ZDOT =     -10353
340830                 ZDOT =       -3144
324371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5136124
71                 X    =        -1565490
81
 Y    =       15500873
97  feet           Y    =         4724666
38  meter
 Z    =       14729744
50                 Z    =         4489626
12
 XDOT =     -21893
807212                 XDOT =       -6673
232438
 YDOT =       2555
012429  feet/sec       YDOT =         778
767788  meter/sec
 ZDOT =     -10310
030696                 ZDOT =       -3142
497356


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   06299
65732765  
00020000  00000-0  20000-3 0  9073
2 25544  51
6344 230
0598 0012233 139
4300 220
7779 15
77199770 13903


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
65732765   =   yrday
fracday
Element set:     907
Inclination:       51
6344  deg
RA of node:       230
0598  deg
Eccentricity:     
0012233     
Arg of perigee:   139
4300  deg
Mean anomaly:     220
7779  deg
Mean motion:   15
77199770  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1390
Checksum:              308


Coasting Arc #9 (Orbit 1405)
---------------------------------------

Vector Time (GMT): 2006/300/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1522301
47                 A    =         6717582
74  meter
 Y    =       -5470736
60  meter          E    =           
0022165
 Z    =        3581854
61                 I    =           51
41529
 XDOT =       6223
471195                 Wp   =          118
72117
 YDOT =       1165
775897  meter/sec      RA   =          224
23434  deg
 ZDOT =       4394
533421                 TA   =          284
31809
                                          MA   =          284
56410
                                          Ha   =            189
212  n
mi
                                          Hp   =            175
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4994427
39                 X    =        -1478414
16
 Y    =      -17948610
91  feet           Y    =        -5487514
65  meter
 Z    =       11751491
50                 Z    =         3574565
39
 XDOT =      20418
212581                 XDOT =        6188
624486
 YDOT =       3824
724070  feet/sec       YDOT =        1235
175101  meter/sec
 ZDOT =      14417
760566                 ZDOT =        4424
683105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18632634
82                 X    =         5679227
09
 Y    =        -759901
64  feet           Y    =         -231618
02  meter
 Z    =       11723564
31                 Z    =         3573342
40
 XDOT =      -8491
297637                 XDOT =       -2588
147520
 YDOT =      17538
614737  feet/sec       YDOT =        5345
769772  meter/sec
 ZDOT =      14530
333274                 ZDOT =        4428
845582


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   06300
67111121  
00020000  00000-0  20000-3 0  9086
2 25544  51
6344 224
8280 0012268 143
1788 217
0222 15
77178389 14065


Satellite: ISS
Catalog Number: 25544
Epoch time:      06300
67111121   =   yrday
fracday
Element set:     908
Inclination:       51
6344  deg
RA of node:       224
8280  deg
Eccentricity:     
0012268     
Arg of perigee:   143
1788  deg
Mean anomaly:     217
0222  deg
Mean motion:   15
77178389  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1406
Checksum:              273


Coasting Arc #10 (Orbit 1420)
---------------------------------------

Vector Time (GMT): 2006/301/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5796417
27                 A    =         6718996
32  meter
 Y    =       -1598395
90  meter          E    =           
0014032
 Z    =       -3018915
62                 I    =           51
44176
 XDOT =       -955
714920                 Wp   =          129
66082
 YDOT =      -5828
542892  meter/sec      RA   =          219
00781  deg
 ZDOT =       4927
351256                 TA   =          195
32300
                                          MA   =          195
36553
                                          Ha   =            188
999  n
mi
                                          Hp   =            175
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19017117
02                 X    =        -5763447
39
 Y    =       -5244081
04  feet           Y    =        -1663030
14  meter
 Z    =       -9904578
80                 Z    =        -3046995
08
 XDOT =      -3135
547639                 XDOT =        -914
404888
 YDOT =     -19122
516050  feet/sec       YDOT =       -5838
999519  meter/sec
 ZDOT =      16165
850576                 ZDOT =        4922
808342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9199761
76                 X    =         2804087
38
 Y    =      -17390399
77  feet           Y    =        -5300593
85  meter
 Z    =      -10009504
80                 Z    =        -3050897
06
 XDOT =      18100
578576                 XDOT =        5517
056350
 YDOT =        292
878647  feet/sec       YDOT =          89
269412  meter/sec
 ZDOT =      16148
108980                 ZDOT =        4921
943617


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   06301
62151835  
00020000  00000-0  20000-3 0  9099
2 25544  51
6342 219
9231 0012125 147
4357 212
7558 15
77210488 14213


Satellite: ISS
Catalog Number: 25544
Epoch time:      06301
62151835   =   yrday
fracday
Element set:     909
Inclination:       51
6342  deg
RA of node:       219
9231  deg
Eccentricity:     
0012125     
Arg of perigee:   147
4357  deg
Mean anomaly:     212
7558  deg
Mean motion:   15
77210488  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1421
Checksum:              274


Coasting Arc #11 (Orbit 1436)
---------------------------------------

Vector Time (GMT): 2006/302/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          22766
97                 A    =         6712756
17  meter
 Y    =        4662883
42  meter          E    =           
0018663
 Z    =       -4841105
34                 I    =           51
44321
 XDOT =      -6926
078707                 Wp   =          112
38685
 YDOT =      -2392
650809  meter/sec      RA   =          213
87644  deg
 ZDOT =      -2351
334733                 TA   =          134
69008
                                          MA   =          134
53789
                                          Ha   =            188
827  n
mi
                                          Hp   =            175
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          74694
78                 X    =           -5858
21
 Y    =       15298173
94  feet           Y    =         4662978
15  meter
 Z    =      -15882891
55                 Z    =        -4841064
09
 XDOT =     -22723
355339                 XDOT =       -6887
386482
 YDOT =      -7849
904230  feet/sec       YDOT =       -2469
885630  meter/sec
 ZDOT =      -7714
352798                 ZDOT =       -2384
888175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15026854
39                 X    =        -4580185
22
 Y    =       -2873799
34  feet           Y    =         -875934
04  meter
 Z    =      -15882092
86                 Z    =        -4840861
90
 XDOT =      11980
991478                 XDOT =        3651
806203
 YDOT =     -19578
141452  feet/sec       YDOT =       -5967
417515  meter/sec
 ZDOT =      -7839
815456                 ZDOT =       -2389
575751


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   06302
63527268  
00020000  00000-0  20000-3 0  9100
2 25544  51
6337 214
6907 0012056 151
6349 208
5475 15
77241975 14373


Satellite: ISS
Catalog Number: 25544
Epoch time:      06302
63527268   =   yrday
fracday
Element set:     910
Inclination:       51
6337  deg
RA of node:       214
6907  deg
Eccentricity:     
0012056     
Arg of perigee:   151
6349  deg
Mean anomaly:     208
5475  deg
Mean motion:   15
77241975  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1437
Checksum:              295


Coasting Arc #12 (Orbit 1452)
---------------------------------------

Vector Time (GMT): 2006/303/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6159799
64                 A    =         6722566
21  meter
 Y    =        2458830
23  meter          E    =           
0025082
 Z    =        1003868
60                 I    =           51
50082
 XDOT =       -959
011598                 Wp   =          138
92670
 YDOT =       4848
496919  meter/sec      RA   =          208
67531  deg
 ZDOT =      -5926
509431                 TA   =           30
04921
                                          MA   =           29
90552
                                          Ha   =            188
820  n
mi
                                          Hp   =            175
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20209316
40                 X    =         6126970
17
 Y    =        8067028
32  feet           Y    =         2527528
95  meter
 Z    =        3293532
16                 Z    =         1033713
56
 XDOT =      -3146
363511                 XDOT =        -984
366636
 YDOT =      15907
142124  feet/sec       YDOT =        4837
631050  meter/sec
 ZDOT =     -19443
928581                 ZDOT =       -5931
229874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11595163
90                 X    =        -3534205
96
 Y    =       18392869
48  feet           Y    =         5606146
62  meter
 Z    =        3405186
58                 Z    =         1037900
87
 XDOT =     -13751
122095                 XDOT =       -4191
342015
 YDOT =      -5028
054597  feet/sec       YDOT =       -1532
551041  meter/sec
 ZDOT =     -19460
859090                 ZDOT =       -5931
669851


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   06303
64901483  
00020000  00000-0  20000-3 0  9118
2 25544  51
6339 209
4591 0012257 155
3470 204
8283 15
77222426 14539


Satellite: ISS
Catalog Number: 25544
Epoch time:      06303
64901483   =   yrday
fracday
Element set:     911
Inclination:       51
6339  deg
RA of node:       209
4591  deg
Eccentricity:     
0012257     
Arg of perigee:   155
3470  deg
Mean anomaly:     204
8283  deg
Mean motion:   15
77222426  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1453
Checksum:              279


Coasting Arc #13 (Orbit 1468)
---------------------------------------

Vector Time (GMT): 2006/304/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1743566
08                 A    =         6710769
83  meter
 Y    =       -3795123
84  meter          E    =           
0013028
 Z    =        5247009
76                 I    =           51
48688
 XDOT =       7044
760796                 Wp   =          149
83362
 YDOT =       3137
080910  meter/sec      RA   =          203
51335  deg
 ZDOT =        -82
938277                 TA   =          300
88987
                                          MA   =          301
01791
                                          Ha   =            188
591  n
mi
                                          Hp   =            176
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5720361
16                 X    =         1760384
74
 Y    =      -12451193
69  feet           Y    =        -3775532
23  meter
 Z    =       17214598
96                 Z    =         5255521
00
 XDOT =      23112
732270                 XDOT =        7009
560842
 YDOT =      10292
260202  feet/sec       YDOT =        3215
662519  meter/sec
 ZDOT =       -272
107209                 ZDOT =         -48
799908

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11356975
86                 X    =         3461606
24
 Y    =        7595932
31  feet           Y    =         2315240
17  meter
 Z    =       17245813
55                 Z    =         5256523
97
 XDOT =     -13398
765432                 XDOT =       -4083
943704
 YDOT =      20278
831185  feet/sec       YDOT =        6180
987745  meter/sec
 ZDOT =       -144
332957                 ZDOT =         -43
992685


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   06304
66274026  
00020000  00000-0  20000-3 0  9128
2 25544  51
6336 204
2267 0012072 159
5625 200
6025 15
77276881 14691


Satellite: ISS
Catalog Number: 25544
Epoch time:      06304
66274026   =   yrday
fracday
Element set:     912
Inclination:       51
6336  deg
RA of node:       204
2267  deg
Eccentricity:     
0012072     
Arg of perigee:   159
5625  deg
Mean anomaly:     200
6025  deg
Mean motion:   15
77276881  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1469
Checksum:              281

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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