Date: October 31st 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6113 9 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 1451)
---------------------------------------

Vector Time (GMT): 2006/303/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4250166
98                 A    =         6712112
69  meter
 Y    =       -1997044
83  meter          E    =           
0013398
 Z    =        4783437
85                 I    =           51
46688
 XDOT =       5196
681502                 Wp   =          123
44061
 YDOT =       5139
749067  meter/sec      RA   =          209
04710  deg
 ZDOT =      -2473
866953                 TA   =          350
74207
                                          MA   =          350
76674
                                          Ha   =            188
301  n
mi
                                          Hp   =            175
570

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13944117
40                 X    =         4248944
98
 Y    =       -6551984
35  feet           Y    =        -1949524
02  meter
 Z    =       15693693
74                 Z    =         4804082
40
 XDOT =      17049
479992                 XDOT =        5150
839624
 YDOT =      16862
693788  feet/sec       YDOT =        5197
604971  meter/sec
 ZDOT =      -8116
361394                 ZDOT =       -2448
732432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3112470
74                 X    =         -948681
08
 Y    =       15008848
66  feet           Y    =         4574697
07  meter
 Z    =       15770412
80                 Z    =         4806821
82
 XDOT =     -22661
543094                 XDOT =       -6907
238335
 YDOT =       3721
503756  feet/sec       YDOT =        1134
314345  meter/sec
 ZDOT =      -8021
902989                 ZDOT =       -2445
076031


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
58500863  
00020000  00000-0  20000-3 0  9006
2 25544  51
6344 209
7903 0012088 154
7685 205
4073 15
77497190 14523


Satellite: ISS
Catalog Number: 25544
Epoch time:      06303
58500863   =   yrday
fracday
Element set:     900
Inclination:       51
6344  deg
RA of node:       209
7903  deg
Eccentricity:     
0012088     
Arg of perigee:   154
7685  deg
Mean anomaly:     205
4073  deg
Mean motion:   15
77497190  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1452
Checksum:              291


Coasting Arc #2 (Orbit 1467)
---------------------------------------

Vector Time (GMT): 2006/304/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3902438
68                 A    =         6718028
96  meter
 Y    =       -4469005
09  meter          E    =           
0020313
 Z    =        3148155
74                 I    =           51
51241
 XDOT =       5783
315691                 Wp   =          120
63954
 YDOT =      -1629
522071  meter/sec      RA   =          203
91835  deg
 ZDOT =       4822
570514                 TA   =          276
14540
                                          MA   =          276
37680
                                          Ha   =            188
376  n
mi
                                          Hp   =            175
786

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12803276
49                 X    =        -3867468
97
 Y    =      -14662090
20  feet           Y    =        -4512448
78  meter
 Z    =       10328594
94                 Z    =         3129282
42
 XDOT =      18974
132843                 XDOT =        5777
679923
 YDOT =      -5346
201021  feet/sec       YDOT =       -1564
881308  meter/sec
 ZDOT =      15822
081738                 ZDOT =        4850
652546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19422087
15                 X    =         5919852
16
 Y    =       -1773524
14  feet           Y    =         -540570
16  meter
 Z    =       10257572
54                 Z    =         3126508
11
 XDOT =      -6916
897499                 XDOT =       -2108
270358
 YDOT =      17001
380000  feet/sec       YDOT =        5182
020624  meter/sec
 ZDOT =      15926
597574                 ZDOT =        4854
426941


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
59860050  
00020000  00000-0  20000-3 0  9016
2 25544  51
6348 204
5570 0012107 158
3593 201
8085 15
77482840 14686


Satellite: ISS
Catalog Number: 25544
Epoch time:      06304
59860050   =   yrday
fracday
Element set:     901
Inclination:       51
6348  deg
RA of node:       204
5570  deg
Eccentricity:     
0012107     
Arg of perigee:   158
3593  deg
Mean anomaly:     201
8085  deg
Mean motion:   15
77482840  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1468
Checksum:              284


Coasting Arc #3 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2006/305/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5736618
76                 A    =         6717040
99  meter
 Y    =         905182
09  meter          E    =           
0014427
 Z    =       -3394171
68                 I    =           51
53669
 XDOT =      -3523
340216                 Wp   =          144
15960
 YDOT =      -5054
547913  meter/sec      RA   =          198
69629  deg
 ZDOT =       4605
303971                 TA   =          175
71853
                                          MA   =          175
70617
                                          Ha   =            188
120  n
mi
                                          Hp   =            175
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18820927
68                 X    =        -5729825
72
 Y    =        2969757
50  feet           Y    =          841069
93  meter
 Z    =      -11135733
85                 Z    =        -3422024
16
 XDOT =     -11559
515145                 XDOT =       -3488
929801
 YDOT =     -16583
162445  feet/sec       YDOT =       -5093
755341  meter/sec
 ZDOT =      15109
264996                 ZDOT =        4588
271016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8342135
46                 X    =         2542682
89
 Y    =      -17062642
05  feet           Y    =        -5200693
30  meter
 Z    =      -11239500
38                 Z    =        -3425799
72
 XDOT =      19018
075754                 XDOT =        5796
709490
 YDOT =       -615
801174  feet/sec       YDOT =        -187
696198  meter/sec
 ZDOT =      15045
017993                 ZDOT =        4585
721484


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   06305
54881996  
00020000  00000-0  20000-3 0  9025
2 25544  51
6351 199
6508 0012010 162
8109 197
3465 15
77528115 14835


Satellite: ISS
Catalog Number: 25544
Epoch time:      06305
54881996   =   yrday
fracday
Element set:     902
Inclination:       51
6351  deg
RA of node:       199
6508  deg
Eccentricity:     
0012010     
Arg of perigee:   162
8109  deg
Mean anomaly:     197
3465  deg
Mean motion:   15
77528115  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1483
Checksum:              302


Coasting Arc #4 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2006/306/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2083193
98                 A    =         6712482
17  meter
 Y    =        4334520
06  meter          E    =           
0015357
 Z    =       -4690569
35                 I    =           51
54866
 XDOT =      -7179
026455                 Wp   =          121
76549
 YDOT =        503
193463  meter/sec      RA   =          193
57347  deg
 ZDOT =      -2737
861365                 TA   =          121
30669
                                          MA   =          121
15624
                                          Ha   =            187
929  n
mi
                                          Hp   =            176
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6834625
90                 X    =         2057356
38
 Y    =       14220866
33  feet           Y    =         4357670
87  meter
 Z    =      -15389007
06                 Z    =        -4680511
88
 XDOT =     -23553
236402                 XDOT =       -7170
819340
 YDOT =       1650
897189  feet/sec       YDOT =         422
959404  meter/sec
 ZDOT =      -8982
484794                 ZDOT =       -2772
717926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15656580
55                 X    =        -4772125
75
 Y    =       -2233540
10  feet           Y    =         -680783
02  meter
 Z    =      -15350878
57                 Z    =        -4678947
79
 XDOT =      11634
445050                 XDOT =        3546
178851
 YDOT =     -19253
209839  feet/sec       YDOT =       -5868
378359  meter/sec
 ZDOT =      -9112
440024                 ZDOT =       -2777
471719


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   06306
56236600  
00020000  00000-0  20000-3 0  9035
2 25544  51
6349 194
4173 0011946 167
1846 192
9624 15
77569898 14994


Satellite: ISS
Catalog Number: 25544
Epoch time:      06306
56236600   =   yrday
fracday
Element set:     903
Inclination:       51
6349  deg
RA of node:       194
4173  deg
Eccentricity:     
0011946     
Arg of perigee:   167
1846  deg
Mean anomaly:     192
9624  deg
Mean motion:   15
77569898  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1499
Checksum:              331


Coasting Arc #5 (Orbit 1514)
---------------------------------------

Vector Time (GMT): 2006/307/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6586958
96                 A    =         6721322
17  meter
 Y    =         -39909
63  meter          E    =           
0023695
 Z    =        1260270
43                 I    =           51
60666
 XDOT =       1159
839991                 Wp   =          144
06530
 YDOT =       4873
215230  meter/sec      RA   =          188
37285  deg
 ZDOT =      -5871
250328                 TA   =           22
06228
                                          MA   =           21
96046
                                          Ha   =            187
838  n
mi
                                          Hp   =            176
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21610757
74                 X    =         6580793
34
 Y    =        -130937
12  feet           Y    =           33714
95  meter
 Z    =        4134745
51                 Z    =         1292255
80
 XDOT =       3805
249314                 XDOT =        1133
783095
 YDOT =      15988
238942  feet/sec       YDOT =        4886
039378  meter/sec
 ZDOT =     -19262
632310                 ZDOT =       -5865
679073

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11672810
71                 X    =        -3557872
70
 Y    =       18160026
71  feet           Y    =         5535176
14  meter
 Z    =        4254061
03                 Z    =         1296637
80
 XDOT =     -14207
633026                 XDOT =       -4330
486546
 YDOT =      -4597
743259  feet/sec       YDOT =       -1401
392145  meter/sec
 ZDOT =     -19241
164004                 ZDOT =       -5864
706788


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   06307
57589143  
00020000  00000-0  20000-3 0  9041
2 25544  51
6350 189
1845 0012109 170
5638 189
5756 15
77567611 15150


Satellite: ISS
Catalog Number: 25544
Epoch time:      06307
57589143   =   yrday
fracday
Element set:     904
Inclination:       51
6350  deg
RA of node:       189
1845  deg
Eccentricity:     
0012109     
Arg of perigee:   170
5638  deg
Mean anomaly:     189
5756  deg
Mean motion:   15
77567611  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1515
Checksum:              313


Coasting Arc #6 (Orbit 1530)
---------------------------------------

Vector Time (GMT): 2006/308/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         135405
72                 A    =         6709766
79  meter
 Y    =       -4165314
38  meter          E    =           
0012638
 Z    =        5255859
48                 I    =           51
59598
 XDOT =       7700
749983                 Wp   =          164
59885
 YDOT =        368
457731  meter/sec      RA   =          183
21996  deg
 ZDOT =         81
580505                 TA   =          284
55743
                                          MA   =          284
69758
                                          Ha   =            187
615  n
mi
                                          Hp   =            176
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         444244
47                 X    =          156439
92
 Y    =      -13665729
58  feet           Y    =        -4163682
60  meter
 Z    =       17243633
45                 Z    =         5256568
38
 XDOT =      25264
927766                 XDOT =        7695
661179
 YDOT =       1208
850822  feet/sec       YDOT =         454
543336  meter/sec
 ZDOT =        267
652577                 ZDOT =         118
979618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11392031
51                 X    =         3472291
21
 Y    =        7556452
08  feet           Y    =         2303206
59  meter
 Z    =       17245696
94                 Z    =         5256488
43
 XDOT =     -13895
564622                 XDOT =       -4235
368097
 YDOT =      19929
331499  feet/sec       YDOT =        6074
460241  meter/sec
 ZDOT =        407
229163                 ZDOT =         124
123449


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   06308
58939162  
00020000  00000-0  20000-3 0  9054
2 25544  51
6343 183
9508 0011941 175
0752 185
0533 15
77632922 15310


Satellite: ISS
Catalog Number: 25544
Epoch time:      06308
58939162   =   yrday
fracday
Element set:     905
Inclination:       51
6343  deg
RA of node:       183
9508  deg
Eccentricity:     
0011941     
Arg of perigee:   175
0752  deg
Mean anomaly:     185
0533  deg
Mean motion:   15
77632922  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1531
Checksum:              296


Coasting Arc #7 (Orbit 1546)
---------------------------------------

Vector Time (GMT): 2006/309/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6588835
87                 A    =         6721148
16  meter
 Y    =        -683266
26  meter          E    =           
0012532
 Z    =        1144851
21                 I    =           51
66214
 XDOT =       1522
731649                 Wp   =          110
97066
 YDOT =      -4714
927051  meter/sec      RA   =          178
06478  deg
 ZDOT =       5893
605283                 TA   =          261
56950
                                          MA   =          261
71157
                                          Ha   =            187
365  n
mi
                                          Hp   =            176
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21616915
58                 X    =        -6586267
46
 Y    =       -2241687
20  feet           Y    =         -756931
96  meter
 Z    =        3756073
52                 Z    =         1112847
75
 XDOT =       4995
838742                 XDOT =        1546
710388
 YDOT =     -15468
920772  feet/sec       YDOT =       -4697
765166  meter/sec
 ZDOT =      19335
975339                 ZDOT =        5901
061042

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13098430
90                 X    =         3992401
74
 Y    =      -17367519
34  feet           Y    =        -5293619
89  meter
 Z    =        3636573
80                 Z    =         1108427
70
 XDOT =       9452
152482                 XDOT =        2881
016077
 YDOT =      11222
941618  feet/sec       YDOT =        3420
752605  meter/sec
 ZDOT =      19363
141108                 ZDOT =        5901
885410


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   06309
60286927  
00020000  00000-0  20000-3 0  9063
2 25544  51
6330 178
7162 0011948 179
7088 180
4086 15
77695756 15477


Satellite: ISS
Catalog Number: 25544
Epoch time:      06309
60286927   =   yrday
fracday
Element set:     906
Inclination:       51
6330  deg
RA of node:       178
7162  deg
Eccentricity:     
0011948     
Arg of perigee:   179
7088  deg
Mean anomaly:     180
4086  deg
Mean motion:   15
77695756  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1547
Checksum:              332


Coasting Arc #8 (Orbit 1561)
---------------------------------------

Vector Time (GMT): 2006/310/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2487461
62                 A    =         6711854
46  meter
 Y    =        4080153
81  meter          E    =           
0018526
 Z    =       -4728336
82                 I    =           51
65811
 XDOT =      -7111
349161                 Wp   =          147
13715
 YDOT =      -1234
804050  meter/sec      RA   =          172
86953  deg
 ZDOT =       2665
158344                 TA   =          149
12611
                                          MA   =          149
01704
                                          Ha   =            187
166  n
mi
                                          Hp   =            176
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8160963
31                 X    =        -2509931
44
 Y    =       13386331
38  feet           Y    =         4052212
33  meter
 Z    =      -15512916
08                 Z    =        -4740475
60
 XDOT =     -23331
198034                 XDOT =       -7109
960153
 YDOT =      -4051
194389  feet/sec       YDOT =       -1314
319519  meter/sec
 ZDOT =       8743
957823                 ZDOT =        2630
613569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7526129
34                 X    =        -2293964
22
 Y    =      -13702648
61  feet           Y    =        -4176567
30  meter
 Z    =      -15557652
57                 Z    =        -4741972
50
 XDOT =      14237
845119                 XDOT =        4339
695192
 YDOT =     -17639
906182  feet/sec       YDOT =       -5376
643404  meter/sec
 ZDOT =       8614
888049                 ZDOT =        2625
817877


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   06310
55298648  
00020000  00000-0  20000-3 0  9073
2 25544  51
6317 173
8082 0011868 183
3745 176
7342 15
77708020 15620


Satellite: ISS
Catalog Number: 25544
Epoch time:      06310
55298648   =   yrday
fracday
Element set:     907
Inclination:       51
6317  deg
RA of node:       173
8082  deg
Eccentricity:     
0011868     
Arg of perigee:   183
3745  deg
Mean anomaly:     176
7342  deg
Mean motion:   15
77708020  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1562
Checksum:              305


Coasting Arc #9 (Orbit 1577)
---------------------------------------

Vector Time (GMT): 2006/311/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5596272
55                 A    =         6716675
13  meter
 Y    =        1517414
48  meter          E    =           
0012279
 Z    =       -3380733
40                 I    =           51
70149
 XDOT =      -4051
641551                 Wp   =          164
88745
 YDOT =       4631
605184  meter/sec      RA   =          167
75522  deg
 ZDOT =      -4643
388582                 TA   =           55
03962
                                          MA   =           54
92436
                                          Ha   =            187
071  n
mi
                                          Hp   =            177
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18360474
25                 X    =         5595312
13
 Y    =        4978393
97  feet           Y    =         1579990
05  meter
 Z    =      -11091645
02                 Z    =        -3353548
14
 XDOT =     -13292
787240                 XDOT =       -4080
574305
 YDOT =      15195
555065  feet/sec       YDOT =        4586
136144  meter/sec
 ZDOT =     -15234
214508                 ZDOT =       -4663
141856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13317923
97                 X    =        -4059303
23
 Y    =       13666349
25  feet           Y    =         4165503
25  meter
 Z    =      -10989986
79                 Z    =        -3349747
98
 XDOT =      -5845
031114                 XDOT =       -1781
565484
 YDOT =     -17964
611863  feet/sec       YDOT =       -5475
613696  meter/sec
 ZDOT =     -15307
303302                 ZDOT =       -4665
666046


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   06311
56642239  
00020000  00000-0  20000-3 0  9085
2 25544  51
6307 168
5744 0011832 187
5751 172
5237 15
77729196 15780


Satellite: ISS
Catalog Number: 25544
Epoch time:      06311
56642239   =   yrday
fracday
Element set:     908
Inclination:       51
6307  deg
RA of node:       168
5744  deg
Eccentricity:     
0011832     
Arg of perigee:   187
5751  deg
Mean anomaly:     172
5237  deg
Mean motion:   15
77729196  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1578
Checksum:              317


Coasting Arc #10 (Orbit 1593)
---------------------------------------

Vector Time (GMT): 2006/312/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4402985
95                 A    =         6717013
80  meter
 Y    =       -3973177
62  meter          E    =           
0016211
 Z    =        3130489
89                 I    =           51
73165
 XDOT =       5529
422576                 Wp   =          139
97213
 YDOT =       2288
850677  meter/sec      RA   =          162
54485  deg
 ZDOT =      -4870
413546                 TA   =            3
54578
                                          MA   =            3
53431
                                          Ha   =            186
618  n
mi
                                          Hp   =            177
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14445491
95                 X    =         4431879
64
 Y    =      -13035359
64  feet           Y    =        -3923779
76  meter
 Z    =       10270636
12                 Z    =         3151949
84
 XDOT =      18141
150183                 XDOT =        5527
077477
 YDOT =       7509
352615  feet/sec       YDOT =        2350
671136  meter/sec
 ZDOT =     -15979
047068                 ZDOT =       -4843
556475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4704836
27                 X    =         1434034
09
 Y    =       18836579
46  feet           Y    =         5741389
42  meter
 Z    =       10350197
81                 Z    =         3154740
29
 XDOT =     -13848
145410                 XDOT =       -4220
914721
 YDOT =      12186
638830  feet/sec       YDOT =        3714
487515  meter/sec
 ZDOT =     -15878
497008                 ZDOT =       -4839
765888


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   06312
57983467  
00020000  00000-0  20000-3 0  9099
2 25544  51
6311 163
3393 0011734 192
2865 167
8016 15
77805942 15942


Satellite: ISS
Catalog Number: 25544
Epoch time:      06312
57983467   =   yrday
fracday
Element set:     909
Inclination:       51
6311  deg
RA of node:       163
3393  deg
Eccentricity:     
0011734     
Arg of perigee:   192
2865  deg
Mean anomaly:     167
8016  deg
Mean motion:   15
77805942  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1594
Checksum:              313


Coasting Arc #11 (Orbit 1609)
---------------------------------------

Vector Time (GMT): 2006/313/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3870510
22                 A    =         6711262
63  meter
 Y    =       -2542654
92  meter          E    =           
0015162
 Z    =        4860488
36                 I    =           51
73718
 XDOT =       5857
650955                 Wp   =          169
67813
 YDOT =      -4427
202411  meter/sec      RA   =          157
43001  deg
 ZDOT =       2332
821100                 TA   =          257
55325
                                          MA   =          257
72295
                                          Ha   =            186
682  n
mi
                                          Hp   =            177
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12698524
35                 X    =        -3865402
00
 Y    =       -8342043
70  feet           Y    =        -2585909
04  meter
 Z    =       15946484
11                 Z    =         4841697
26
 XDOT =      19218
014944                 XDOT =        5895
388583
 YDOT =     -14524
942294  feet/sec       YDOT =       -4361
488143  meter/sec
 ZDOT =       7653
612532                 ZDOT =        2361
369267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13259817
77                 X    =         4041592
46
 Y    =       -7567200
49  feet           Y    =        -2306482
71  meter
 Z    =       15875996
93                 Z    =         4839003
86
 XDOT =       3616
043956                 XDOT =        1102
170198
 YDOT =      22724
884673  feet/sec       YDOT =        6926
544848  meter/sec
 ZDOT =       7759
585634                 ZDOT =        2365
121701


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   06313
59322885  
00020000  00000-0  20000-3 0  9105
2 25544  51
6299 158
1039 0011722 195
2938 164
7874 15
77765183 16106


Satellite: ISS
Catalog Number: 25544
Epoch time:      06313
59322885   =   yrday
fracday
Element set:     910
Inclination:       51
6299  deg
RA of node:       158
1039  deg
Eccentricity:     
0011722     
Arg of perigee:   195
2938  deg
Mean anomaly:     164
7874  deg
Mean motion:   15
77765183  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1610
Checksum:              313


Coasting Arc #12 (Orbit 1624)
---------------------------------------

Vector Time (GMT): 2006/314/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5590064
33                 A    =         6720984
92  meter
 Y    =        3649769
00  meter          E    =           
0004143
 Z    =        -796369
23                 I    =           51
79626
 XDOT =      -3217
324634                 Wp   =          140
67227
 YDOT =      -3625
777417  meter/sec      RA   =          152
24638  deg
 ZDOT =       5980
567503                 TA   =          210
65838
                                          MA   =          210
68259
                                          Ha   =            186
402  n
mi
                                          Hp   =            177
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18340106
07                 X    =        -5626592
42
 Y    =       11974307
75  feet           Y    =         3587053
63  meter
 Z    =       -2612759
93                 Z    =         -823614
51
 XDOT =     -10555
527016                 XDOT =       -3205
594444
 YDOT =     -11895
595199  feet/sec       YDOT =       -3661
690263  meter/sec
 ZDOT =      19621
284460                 ZDOT =        5964
965719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2660798
27                 X    =         -811011
31
 Y    =      -21728425
56  feet           Y    =        -6622824
11  meter
 Z    =       -2713987
20                 Z    =         -827223
30
 XDOT =      13795
746020                 XDOT =        4204
943387
 YDOT =      -4127
426061  feet/sec       YDOT =       -1258
039463  meter/sec
 ZDOT =      19562
550380                 ZDOT =        5962
665356


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   06314
54326187  
00020000  00000-0  20000-3 0  9111
2 25544  51
6295 153
1953 0011869 199
0256 161
0467 15
77831586 16254


Satellite: ISS
Catalog Number: 25544
Epoch time:      06314
54326187   =   yrday
fracday
Element set:     911
Inclination:       51
6295  deg
RA of node:       153
1953  deg
Eccentricity:     
0011869     
Arg of perigee:   199
0256  deg
Mean anomaly:     161
0467  deg
Mean motion:   15
77831586  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1625
Checksum:              307

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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