Date: September 27th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 898)
---------------------------------------

Vector Time (GMT): 2006/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5932954
06                 A    =         6722031
98  meter
 Y    =        -636412
61  meter          E    =           
0020461
 Z    =        3091468
38                 I    =           51
80035
 XDOT =      -1969
753264                 Wp   =           61
37944
 YDOT =      -5606
637815  meter/sec      RA   =           30
18272  deg
 ZDOT =      -4900
435896                 TA   =           82
79128
                                          MA   =           82
55872
                                          Ha   =            190
471  n
mi
                                          Hp   =            177
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19465072
37                 X    =        -5940414
71
 Y    =       -2087967
87  feet           Y    =         -702799
71  meter
 Z    =       10142612
78                 Z    =         3062627
51
 XDOT =      -6462
445093                 XDOT =       -1883
106825
 YDOT =     -18394
481021  feet/sec       YDOT =       -5628
180527  meter/sec
 ZDOT =     -16077
545592                 ZDOT =       -4909
794306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19610835
44                 X    =         5977382
64
 Y    =         912835
61  feet           Y    =          278232
30  meter
 Z    =       10035093
96                 Z    =         3058696
64
 XDOT =       7532
652930                 XDOT =        2295
952613
 YDOT =      16548
590988  feet/sec       YDOT =        5044
010533  meter/sec
 ZDOT =     -16113
155837                 ZDOT =       -4911
289899


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   06268
53801820  
00020000  00000-0  20000-3 0  9008
2 25544  51
6359  30
5221 0012015  24
2426 335
9302 15
76137541  8994


Satellite: ISS
Catalog Number: 25544
Epoch time:      06268
53801820   =   yrday
fracday
Element set:     900
Inclination:       51
6359  deg
RA of node:        30
5221  deg
Eccentricity:     
0012015     
Arg of perigee:    24
2426  deg
Mean anomaly:     335
9302  deg
Mean motion:   15
76137541  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             899
Checksum:              264


Coasting Arc #2 (Orbit 914)
---------------------------------------

Vector Time (GMT): 2006/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1295776
17                 A    =         6716355
80  meter
 Y    =        4654364
19  meter          E    =           
0014488
 Z    =        4651530
18                 I    =           51
75814
 XDOT =      -7120
169545                 Wp   =           60
30926
 YDOT =       -858
986197  meter/sec      RA   =           25
08690  deg
 ZDOT =       2843
453465                 TA   =            1
70638
                                          MA   =            1
70144
                                          Ha   =            190
392  n
mi
                                          Hp   =            177
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4251234
14                 X    =         1221037
40
 Y    =       15270223
72  feet           Y    =         4668436
59  meter
 Z    =       15260925
80                 Z    =         4657643
44
 XDOT =     -23360
136302                 XDOT =       -7123
848297
 YDOT =      -2818
196184  feet/sec       YDOT =        -938
628324  meter/sec
 ZDOT =       9328
915566                 ZDOT =        2808
854134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5333033
89                 X    =        -1625508
73
 Y    =      -14902920
61  feet           Y    =        -4542410
20  meter
 Z    =       15284315
08                 Z    =         4658659
24
 XDOT =      22472
167642                 XDOT =        6849
516697
 YDOT =       1392
050759  feet/sec       YDOT =         424
297071  meter/sec
 ZDOT =       9199
918078                 ZDOT =        2804
135030


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   06269
55244982  
00020000  00000-0  20000-3 0  9012
2 25544  51
6369  25
2954 0012081  27
5332 332
6469 15
76224223  9155


Satellite: ISS
Catalog Number: 25544
Epoch time:      06269
55244982   =   yrday
fracday
Element set:     901
Inclination:       51
6369  deg
RA of node:        25
2954  deg
Eccentricity:     
0012081     
Arg of perigee:    27
5332  deg
Mean anomaly:     332
6469  deg
Mean motion:   15
76224223  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             915
Checksum:              289


Coasting Arc #3 (Orbit 929)
---------------------------------------

Vector Time (GMT): 2006/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6418125
90                 A    =         6724534
42  meter
 Y    =         809852
28  meter          E    =           
0019777
 Z    =       -1806569
70                 I    =           51
75932
 XDOT =        944
198325                 Wp   =           33
10655
 YDOT =       5112
099623  meter/sec      RA   =           19
90548  deg
 ZDOT =       5691
364260                 TA   =          306
86669
                                          MA   =          307
04783
                                          Ha   =            190
636  n
mi
                                          Hp   =            177
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21056843
52                 X    =         6417369
17
 Y    =        2656995
66  feet           Y    =          881619
04  meter
 Z    =       -5927065
96                 Z    =        -1775391
73
 XDOT =       3097
763532                 XDOT =         859
315813
 YDOT =      16771
980391  feet/sec       YDOT =        5122
183692  meter/sec
 ZDOT =      18672
454922                 ZDOT =        5695
744967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21245802
48                 X    =        -6475720
60
 Y    =        -656239
80  feet           Y    =         -200021
89  meter
 Z    =       -5810819
39                 Z    =        -1771137
75
 XDOT =      -4611
034198                 XDOT =       -1405
443223
 YDOT =     -14865
299493  feet/sec       YDOT =       -4530
943286  meter/sec
 ZDOT =      18689
445785                 ZDOT =        5696
543075


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   06270
50345897  
00020000  00000-0  20000-3 0  9027
2 25544  51
6371  20
3959 0012326  30
7623 329
4261 15
76205574  9309


Satellite: ISS
Catalog Number: 25544
Epoch time:      06270
50345897   =   yrday
fracday
Element set:     902
Inclination:       51
6371  deg
RA of node:        20
3959  deg
Eccentricity:     
0012326     
Arg of perigee:    30
7623  deg
Mean anomaly:     329
4261  deg
Mean motion:   15
76205574  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             930
Checksum:              278


Coasting Arc #4 (Orbit 945)
---------------------------------------

Vector Time (GMT): 2006/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -264941
25                 A    =         6714136
07  meter
 Y    =       -4295855
58  meter          E    =           
0024454
 Z    =       -5173342
66                 I    =           51
69782
 XDOT =       7525
656816                 Wp   =           59
22517
 YDOT =        999
925075  meter/sec      RA   =           14
78627  deg
 ZDOT =      -1207
677784                 TA   =          199
18049
                                          MA   =          199
27272
                                          Ha   =            190
544  n
mi
                                          Hp   =            177
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -869229
81                 X    =         -191753
13
 Y    =      -14094014
36  feet           Y    =        -4298409
10  meter
 Z    =      -16972908
98                 Z    =        -5174451
97
 XDOT =      24690
475119                 XDOT =        7519
782967
 YDOT =       3280
594079  feet/sec       YDOT =        1084
048290  meter/sec
 ZDOT =      -3962
197455                 ZDOT =       -1171
131818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2341158
34                 X    =          713585
06
 Y    =       13919641
66  feet           Y    =         4242706
78  meter
 Z    =      -16977602
72                 Z    =        -5174773
31
 XDOT =     -23908
574648                 XDOT =       -7287
333553
 YDOT =       -677
440841  feet/sec       YDOT =        -206
483968  meter/sec
 ZDOT =      -3825
927228                 ZDOT =       -1166
142619


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   06271
51784253  
00020000  00000-0  20000-3 0  9033
2 25544  51
6373  15
1692 0012265  34
4352 325
7605 15
76258820  9469


Satellite: ISS
Catalog Number: 25544
Epoch time:      06271
51784253   =   yrday
fracday
Element set:     903
Inclination:       51
6373  deg
RA of node:        15
1692  deg
Eccentricity:     
0012265     
Arg of perigee:    34
4352  deg
Mean anomaly:     325
7605  deg
Mean motion:   15
76258820  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             946
Checksum:              284


Coasting Arc #5 (Orbit 961)
---------------------------------------

Vector Time (GMT): 2006/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6657568
76                 A    =         6725605
51  meter
 Y    =        -918801
99  meter          E    =           
0017081
 Z    =         262567
82                 I    =           51
70871
 XDOT =        406
090208                 Wp   =           86
09024
 YDOT =      -4763
119356  meter/sec      RA   =            9
62524  deg
 ZDOT =      -6034
113360                 TA   =           91
05873
                                          MA   =           90
86303
                                          Ha   =            190
582  n
mi
                                          Hp   =            176
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21842417
21                 X    =        -6648075
31
 Y    =       -3014442
23  feet           Y    =         -993197
53  meter
 Z    =         861442
98                 Z    =          230247
99
 XDOT =       1332
316955                 XDOT =         488
634890
 YDOT =     -15627
032008  feet/sec       YDOT =       -4758
116652  meter/sec
 ZDOT =     -19796
959841                 ZDOT =       -6031
940083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22053072
41                 X    =         6721776
47
 Y    =         182117
35  feet           Y    =           55509
37  meter
 Z    =         740922
46                 Z    =          225833
17
 XDOT =        591
804116                 XDOT =         180
381894
 YDOT =      14074
353876  feet/sec       YDOT =        4289
863062  meter/sec
 ZDOT =     -19789
483468                 ZDOT =       -6031
834561


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   06272
53220063  
00020000  00000-0  20000-3 0  9041
2 25544  51
6368   9
9418 0012333  38
7222 321
4824 15
76303048  9626


Satellite: ISS
Catalog Number: 25544
Epoch time:      06272
53220063   =   yrday
fracday
Element set:     904
Inclination:       51
6368  deg
RA of node:         9
9418  deg
Eccentricity:     
0012333     
Arg of perigee:    38
7222  deg
Mean anomaly:     321
4824  deg
Mean motion:   15
76303048  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             962
Checksum:              269


Coasting Arc #6 (Orbit 977)
---------------------------------------

Vector Time (GMT): 2006/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -986465
82                 A    =         6713429
14  meter
 Y    =        4077197
52  meter          E    =           
0015165
 Z    =        5233163
04                 I    =           51
64079
 XDOT =      -7615
764322                 Wp   =           45
44082
 YDOT =      -1066
427881  meter/sec      RA   =            4
47107  deg
 ZDOT =       -593
215599                 TA   =           50
25484
                                          MA   =           50
12132
                                          Ha   =            190
584  n
mi
                                          Hp   =            176
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3236436
41                 X    =        -1057406
26
 Y    =       13376632
29  feet           Y    =         4065769
61  meter
 Z    =       17169170
09                 Z    =         5228198
48
 XDOT =     -24986
103417                 XDOT =       -7600
391598
 YDOT =      -3498
779136  feet/sec       YDOT =       -1151
505615  meter/sec
 ZDOT =      -1946
245405                 ZDOT =        -630
175963

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1348806
43                 X    =          411116
20
 Y    =      -13718823
22  feet           Y    =        -4181497
32  meter
 Z    =       17151204
75                 Z    =         5227687
21
 XDOT =      24217
879733                 XDOT =        7381
609743
 YDOT =       -271
732998  feet/sec       YDOT =         -82
824218  meter/sec
 ZDOT =      -2084
078337                 ZDOT =        -635
227077


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   06273
54653110  
00020000  00000-0  20000-3 0  9057
2 25544  51
6374   4
7139 0012417  41
7769 318
4342 15
76388021  9781


Satellite: ISS
Catalog Number: 25544
Epoch time:      06273
54653110   =   yrday
fracday
Element set:     905
Inclination:       51
6374  deg
RA of node:         4
7139  deg
Eccentricity:     
0012417     
Arg of perigee:    41
7769  deg
Mean anomaly:     318
4342  deg
Mean motion:   15
76388021  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             978
Checksum:              290


Coasting Arc #7 (Orbit 993)
---------------------------------------

Vector Time (GMT): 2006/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6518514
71                 A    =         6724661
95  meter
 Y    =         942374
82  meter          E    =           
0026382
 Z    =        1286460
50                 I    =           51
65020
 XDOT =      -1844
243497                 Wp   =           52
56814
 YDOT =       4661
354468  meter/sec      RA   =          359
33645  deg
 ZDOT =       5864
371993                 TA   =          321
58080
                                          MA   =          321
76838
                                          Ha   =            190
640  n
mi
                                          Hp   =            176
301

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21386203
12                 X    =         6501243
06
 Y    =        3091780
89  feet           Y    =         1015171
88  meter
 Z    =        4220670
95                 Z    =         1318085
63
 XDOT =      -6050
667641                 XDOT =       -1924
718522
 YDOT =      15293
157704  feet/sec       YDOT =        4640
281151  meter/sec
 ZDOT =      19240
065593                 ZDOT =        5855
217150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21581045
23                 X    =        -6577902
59
 Y    =         421600
84  feet           Y    =          128503
94  meter
 Z    =        4338616
78                 Z    =         1322410
39
 XDOT =       3619
910842                 XDOT =        1103
348825
 YDOT =     -14516
564970  feet/sec       YDOT =       -4424
649003  meter/sec
 ZDOT =      19206
565421                 ZDOT =        5854
161140


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   06274
56083868  
00020000  00000-0  20000-3 0  9068
2 25544  51
6374 359
4869 0012579  45
8012 314
4184 15
76382184  9948


Satellite: ISS
Catalog Number: 25544
Epoch time:      06274
56083868   =   yrday
fracday
Element set:     906
Inclination:       51
6374  deg
RA of node:       359
4869  deg
Eccentricity:     
0012579     
Arg of perigee:    45
8012  deg
Mean anomaly:     314
4184  deg
Mean motion:   15
76382184  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             994
Checksum:              328


Coasting Arc #8 (Orbit 1008)
---------------------------------------

Vector Time (GMT): 2006/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2229934
13                 A    =         6715053
78  meter
 Y    =       -4093759
54  meter          E    =           
0021583
 Z    =       -4849533
17                 I    =           51
58932
 XDOT =       7226
882481                 Wp   =           77
08338
 YDOT =       1147
177609  meter/sec      RA   =          354
15021  deg
 ZDOT =       2368
253778                 TA   =          215
98328
                                          MA   =          216
12879
                                          Ha   =            190
656  n
mi
                                          Hp   =            176
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7316056
87                 X    =         2299103
58
 Y    =      -13430969
62  feet           Y    =        -4068436
52  meter
 Z    =      -15910541
88                 Z    =        -4838532
04
 XDOT =      23710
244359                 XDOT =        7202
012898
 YDOT =       3763
706067  feet/sec       YDOT =        1227
853602  meter/sec
 ZDOT =       7769
861475                 ZDOT =        2403
301595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4872850
27                 X    =        -1485244
76
 Y    =       14541544
64  feet           Y    =         4432262
81  meter
 Z    =      -15870090
91                 Z    =        -4837203
71
 XDOT =     -22897
809231                 XDOT =       -6979
252253
 YDOT =        900
733820  feet/sec       YDOT =         274
543668  meter/sec
 ZDOT =       7900
590474                 ZDOT =        2408
099977


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
51172671  
00020000  00000-0  20000-3 0  9076
2 25544  51
6368 354
5865 0012652  49
2115 311
0145 15
76444672 10096


Satellite: ISS
Catalog Number: 25544
Epoch time:      06275
51172671   =   yrday
fracday
Element set:     907
Inclination:       51
6368  deg
RA of node:       354
5865  deg
Eccentricity:     
0012652     
Arg of perigee:    49
2115  deg
Mean anomaly:     311
0145  deg
Mean motion:   15
76444672  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1009
Checksum:              284


Coasting Arc #9 (Orbit 1024)
---------------------------------------

Vector Time (GMT): 2006/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6004780
19                 A    =         6721630
62  meter
 Y    =       -1118932
60  meter          E    =           
0015272
 Z    =       -2825369
64                 I    =           51
58314
 XDOT =       3272
147788                 Wp   =           68
29423
 YDOT =      -4746
566521  meter/sec      RA   =          349
03455  deg
 ZDOT =      -5090
960469                 TA   =          144
10532
                                          MA   =          144
00262
                                          Ha   =            190
672  n
mi
                                          Hp   =            175
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19700722
39                 X    =        -5978096
69
 Y    =       -3671038
71  feet           Y    =        -1185932
31  meter
 Z    =       -9269585
44                 Z    =        -2854476
02
 XDOT =      10735
393006                 XDOT =        3349
712346
 YDOT =     -15572
724806  feet/sec       YDOT =       -4709
542098  meter/sec
 ZDOT =     -16702
626211                 ZDOT =       -5074
875743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19987565
12                 X    =         6092209
85
 Y    =        -259304
82  feet           Y    =          -79036
11  meter
 Z    =       -9378177
01                 Z    =        -2858468
35
 XDOT =      -7577
297301                 XDOT =       -2309
560217
 YDOT =      15938
076839  feet/sec       YDOT =        4857
925820  meter/sec
 ZDOT =     -16643
324404                 ZDOT =       -5072
885278


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
52598312  
00020000  00000-0  20000-3 0  9083
2 25544  51
6361 349
3581 0012655  53
0232 307
2089 15
76457788 10256


Satellite: ISS
Catalog Number: 25544
Epoch time:      06276
52598312   =   yrday
fracday
Element set:     908
Inclination:       51
6361  deg
RA of node:       349
3581  deg
Eccentricity:     
0012655     
Arg of perigee:    53
0232  deg
Mean anomaly:     307
2089  deg
Mean motion:   15
76457788  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1025
Checksum:              301


Coasting Arc #10 (Orbit 1040)
---------------------------------------

Vector Time (GMT): 2006/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3419190
44                 A    =         6718301
34  meter
 Y    =        4237005
24  meter          E    =           
0023360
 Z    =        3924708
40                 I    =           51
54545
 XDOT =      -6426
264854                 Wp   =           66
59674
 YDOT =      -1448
859903  meter/sec      RA   =          343
82475  deg
 ZDOT =      -4006
478320                 TA   =           65
09602
                                          MA   =           64
85340
                                          Ha   =            190
666  n
mi
                                          Hp   =            175
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11217816
41                 X    =        -3485380
68
 Y    =       13900935
83  feet           Y    =         4198400
16  meter
 Z    =       12876339
89                 Z    =         3907936
84
 XDOT =     -21083
546108                 XDOT =       -6390
123080
 YDOT =      -4753
477372  feet/sec       YDOT =       -1520
520176  meter/sec
 ZDOT =     -13144
613910                 ZDOT =       -4037
609308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8065190
87                 X    =         2458270
18
 Y    =      -15988088
48  feet           Y    =        -4873169
37  meter
 Z    =       12814416
64                 Z    =         3905834
19
 XDOT =      20375
178861                 XDOT =        6210
354517
 YDOT =       -423
982057  feet/sec       YDOT =        -129
229731  meter/sec
 ZDOT =     -13260
792505                 ZDOT =       -4041
889556


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
54021170  
00020000  00000-0  20000-3 0  9090
2 25544  51
6368 344
1297 0012717  55
7958 304
4410 15
76539925 10412


Satellite: ISS
Catalog Number: 25544
Epoch time:      06277
54021170   =   yrday
fracday
Element set:     909
Inclination:       51
6368  deg
RA of node:       344
1297  deg
Eccentricity:     
0012717     
Arg of perigee:    55
7958  deg
Mean anomaly:     304
4410  deg
Mean motion:   15
76539925  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1041
Checksum:              294


Coasting Arc #11 (Orbit 1056)
---------------------------------------

Vector Time (GMT): 2006/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5127843
12                 A    =         6717572
89  meter
 Y    =        1468300
42  meter          E    =           
0021591
 Z    =        4062538
59                 I    =           51
51595
 XDOT =      -4468
593255                 Wp   =           79
40428
 YDOT =       5000
140701  meter/sec      RA   =          338
71424  deg
 ZDOT =       3820
027532                 TA   =          331
31461
                                          MA   =          331
43320
                                          Ha   =            190
537  n
mi
                                          Hp   =            175
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16823632
29                 X    =         5091308
03
 Y    =        4817258
58  feet           Y    =         1525438
90  meter
 Z    =       13328538
70                 Z    =         4087360
97
 XDOT =     -14660
739025                 XDOT =       -4542
730560
 YDOT =      16404
661093  feet/sec       YDOT =        4949
756249  meter/sec
 ZDOT =      12532
898726                 ZDOT =        3798
138384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17408712
87                 X    =        -5306175
68
 Y    =        -835618
56  feet           Y    =         -254696
54  meter
 Z    =       13421214
00                 Z    =         4090786
03
 XDOT =      10500
938649                 XDOT =        3200
686100
 YDOT =     -18083
000557  feet/sec       YDOT =       -5511
698570  meter/sec
 ZDOT =      12452
016085                 ZDOT =        3795
374503


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
55441579  
00020000  00000-0  20000-3 0  9103
2 25544  51
6362 338
9017 0012747  60
1251 300
1179 15
76562231 10574


Satellite: ISS
Catalog Number: 25544
Epoch time:      06278
55441579   =   yrday
fracday
Element set:     910
Inclination:       51
6362  deg
RA of node:       338
9017  deg
Eccentricity:     
0012747     
Arg of perigee:    60
1251  deg
Mean anomaly:     300
1179  deg
Mean motion:   15
76562231  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1057
Checksum:              279


Coasting Arc #12 (Orbit 1071)
---------------------------------------

Vector Time (GMT): 2006/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4282673
83                 A    =         6721861
63  meter
 Y    =       -4467156
41  meter          E    =           
0017892
 Z    =       -2624174
46                 I    =           51
50376
 XDOT =       5282
449533                 Wp   =           60
05676
 YDOT =       2013
361102  meter/sec      RA   =          333
50186  deg
 ZDOT =       5228
929920                 TA   =          270
02174
                                          MA   =          270
22677
                                          Ha   =            190
706  n
mi
                                          Hp   =            175
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14050767
17                 X    =         4345055
85
 Y    =      -14656024
95  feet           Y    =        -4418916
63  meter
 Z    =       -8609496
25                 Z    =        -2603216
96
 XDOT =      17330
871172                 XDOT =        5234
141667
 YDOT =       6605
515428  feet/sec       YDOT =        2072
162783  meter/sec
 ZDOT =      17155
281889                 ZDOT =        5254
474904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10046710
25                 X    =        -3062237
28
 Y    =       17680917
44  feet           Y    =         5389143
64  meter
 Z    =       -8532017
52                 Z    =        -2600558
94
 XDOT =     -17043
441100                 XDOT =       -5194
840847
 YDOT =      -1416
440978  feet/sec       YDOT =        -431
731210  meter/sec
 ZDOT =      17250
718986                 ZDOT =        5258
019147


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
50520907  
00020000  00000-0  20000-3 0  9113
2 25544  51
6355 334
0002 0012889  63
4562 296
7922 15
76588385 10726


Satellite: ISS
Catalog Number: 25544
Epoch time:      06279
50520907   =   yrday
fracday
Element set:     911
Inclination:       51
6355  deg
RA of node:       334
0002  deg
Eccentricity:     
0012889     
Arg of perigee:    63
4562  deg
Mean anomaly:     296
7922  deg
Mean motion:   15
76588385  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1072
Checksum:              301

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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