Date: December 13th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2131)
---------------------------------------

Vector Time (GMT): 2006/346/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6433624
60                 A    =         6726961
85  meter
 Y    =        1918089
90  meter          E    =           
0012320
 Z    =         540505
75                 I    =           51
58130
 XDOT =      -1830
591681                 Wp   =          347
07522
 YDOT =      -4455
688533  meter/sec      RA   =          347
05993  deg
 ZDOT =      -5992
097939                 TA   =          187
04580
                                          MA   =          187
06314
                                          Ha   =            192
788  n
mi
                                          Hp   =            177
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21107692
25                 X    =        -6457220
47
 Y    =        6292945
87  feet           Y    =         1846013
56  meter
 Z    =        1773312
84                 Z    =          509193
93
 XDOT =      -6005
878220                 XDOT =       -1751
522859
 YDOT =     -14618
400699  feet/sec       YDOT =       -4475
716629  meter/sec
 ZDOT =     -19659
113973                 ZDOT =       -6000
799301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17372157
66                 X    =        -5295033
65
 Y    =      -13555251
33  feet           Y    =        -4131640
61  meter
 Z    =        1656435
22                 Z    =          504881
45
 XDOT =       7501
710056                 XDOT =        2286
521225
 YDOT =     -12014
188795  feet/sec       YDOT =       -3661
924745  meter/sec
 ZDOT =     -19692
163580                 ZDOT =       -6002
171459


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   06346
65766587  
00020000  00000-0  20000-3 0  9008
2 25544  51
6333 347
3813 0024092 328
1115  31
8590 15
75790757 21327


Satellite: ISS
Catalog Number: 25544
Epoch time:      06346
65766587   =   yrday
fracday
Element set:     900
Inclination:       51
6333  deg
RA of node:       347
3813  deg
Eccentricity:     
0024092     
Arg of perigee:   328
1115  deg
Mean anomaly:      31
8590  deg
Mean motion:   15
75790757  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2132
Checksum:              297


Coasting Arc #2 (Orbit 2147)
---------------------------------------

Vector Time (GMT): 2006/347/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1171781
62                 A    =         6714893
44  meter
 Y    =        4016691
64  meter          E    =           
0023298
 Z    =        5260098
51                 I    =           51
51387
 XDOT =      -7341
948165                 Wp   =          336
94725
 YDOT =       2309
190336  meter/sec      RA   =          341
90812  deg
 ZDOT =       -106
859876                 TA   =          114
19087
                                          MA   =          113
94716
                                          Ha   =            192
924  n
mi
                                          Hp   =            177
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3844427
89                 X    =         1101226
52
 Y    =       13178122
16  feet           Y    =         4029400
22  meter
 Z    =       17257541
06                 Z    =         5265620
03
 XDOT =     -24087
756446                 XDOT =       -7366
705075
 YDOT =       7576
083778  feet/sec       YDOT =        2226
950178  meter/sec
 ZDOT =       -350
590144                 ZDOT =        -142
587272

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8377166
71                 X    =        -2553360
41
 Y    =       10841430
36  feet           Y    =         3304467
97  meter
 Z    =       17278649
21                 Z    =         5266532
28
 XDOT =     -19607
176008                 XDOT =       -5976
267247
 YDOT =     -14269
912002  feet/sec       YDOT =       -4349
469178  meter/sec
 ZDOT =       -483
934458                 ZDOT =        -147
503223


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   06347
67233388  
00020000  00000-0  20000-3 0  9010
2 25544  51
6337 342
1560 0024040 331
9532  28
0335 15
75833994 21484


Satellite: ISS
Catalog Number: 25544
Epoch time:      06347
67233388   =   yrday
fracday
Element set:     901
Inclination:       51
6337  deg
RA of node:       342
1560  deg
Eccentricity:     
0024040     
Arg of perigee:   331
9532  deg
Mean anomaly:      28
0335  deg
Mean motion:   15
75833994  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2148
Checksum:              286


Coasting Arc #3 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2006/348/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6329825
59                 A    =         6726603
56  meter
 Y    =       -2096064
61  meter          E    =           
0029980
 Z    =         719657
23                 I    =           51
52691
 XDOT =        907
793608                 Wp   =            1
27716
 YDOT =       4788
788057  meter/sec      RA   =          336
75797  deg
 ZDOT =       5987
885827                 TA   =            6
60074
                                          MA   =            6
56134
                                          Ha   =            193
003  n
mi
                                          Hp   =            177
195

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20767144
31                 X    =         6349297
63
 Y    =       -6876852
41  feet           Y    =        -2025172
18  meter
 Z    =        2361080
16                 Z    =          750454
98
 XDOT =       2978
325486                 XDOT =         825
088853
 YDOT =      15711
246905  feet/sec       YDOT =        4798
476543  meter/sec
 ZDOT =      19645
294707                 ZDOT =        5992
095477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18071142
44                 X    =         5508084
22
 Y    =       12306228
17  feet           Y    =         3750938
35  meter
 Z    =        2476013
06                 Z    =          754688
78
 XDOT =      -9838
285706                 XDOT =       -2998
709483
 YDOT =      10506
730821  feet/sec       YDOT =        3202
451554  meter/sec
 ZDOT =      19661
584638                 ZDOT =        5992
850998


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   06348
68696937  
00020000  00000-0  20000-3 0  9026
2 25544  51
6335 336
9299 0023979 335
8603  24
1435 15
75881457 21647


Satellite: ISS
Catalog Number: 25544
Epoch time:      06348
68696937   =   yrday
fracday
Element set:     902
Inclination:       51
6335  deg
RA of node:       336
9299  deg
Eccentricity:     
0023979     
Arg of perigee:   335
8603  deg
Mean anomaly:      24
1435  deg
Mean motion:   15
75881457  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2164
Checksum:              335


Coasting Arc #4 (Orbit 2178)
---------------------------------------

Vector Time (GMT): 2006/349/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -426724
19                 A    =         6715413
47  meter
 Y    =       -4370222
85  meter          E    =           
0020248
 Z    =       -5080714
66                 I    =           51
46434
 XDOT =       7134
770902                 Wp   =           14
14025
 YDOT =      -2465
135436  meter/sec      RA   =          331
57738  deg
 ZDOT =       1541
783996                 TA   =          270
56650
                                          MA   =          270
79852
                                          Ha   =            193
171  n
mi
                                          Hp   =            176
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1400013
74                 X    =         -353142
50
 Y    =      -14338001
47  feet           Y    =        -4374582
77  meter
 Z    =      -16669011
34                 Z    =        -5082609
44
 XDOT =      23408
041018                 XDOT =        7154
316309
 YDOT =      -8087
714685  feet/sec       YDOT =       -2385
241342  meter/sec
 ZDOT =       5058
346443                 ZDOT =        1576
492411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10424550
78                 X    =         3177403
08
 Y    =       -9930466
80  feet           Y    =        -3026806
28  meter
 Z    =      -16676595
39                 Z    =        -5083026
28
 XDOT =      20136
013017                 XDOT =        6137
456768
 YDOT =      12539
244552  feet/sec       YDOT =        3821
961739  meter/sec
 ZDOT =       5187
862681                 ZDOT =        1581
260545


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   06349
63816045  
00020000  00000-0  20000-3 0  9037
2 25544  51
6339 332
0308 0023975 339
4897  20
5303 15
75928288 21794


Satellite: ISS
Catalog Number: 25544
Epoch time:      06349
63816045   =   yrday
fracday
Element set:     903
Inclination:       51
6339  deg
RA of node:       332
0308  deg
Eccentricity:     
0023975     
Arg of perigee:   339
4897  deg
Mean anomaly:      20
5303  deg
Mean motion:   15
75928288  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2179
Checksum:              313


Coasting Arc #5 (Orbit 2194)
---------------------------------------

Vector Time (GMT): 2006/350/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6072865
14                 A    =         6724727
07  meter
 Y    =        2128672
14  meter          E    =           
0017998
 Z    =       -1987741
33                 I    =           51
47265
 XDOT =        -27
894790                 Wp   =          351
53239
 YDOT =      -5300
558407  meter/sec      RA   =          326
44580  deg
 ZDOT =      -5567
223188                 TA   =          210
63132
                                          MA   =          210
73652
                                          Ha   =            193
307  n
mi
                                          Hp   =            176
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19924098
21                 X    =        -6086560
66
 Y    =        6983832
48  feet           Y    =         2060685
66  meter
 Z    =       -6521461
04                 Z    =        -2017276
76
 XDOT =        -91
518339                 XDOT =          58
423842
 YDOT =     -17390
283487  feet/sec       YDOT =       -5300
387018  meter/sec
 ZDOT =     -18265
167941                 ZDOT =       -5567
149692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18016918
65                 X    =        -5491556
80
 Y    =      -10940046
27  feet           Y    =        -3334526
10  meter
 Z    =       -6631673
23                 Z    =        -2021334
00
 XDOT =      12649
428056                 XDOT =        3855
545671
 YDOT =      -9713
039038  feet/sec       YDOT =       -2960
534299  meter/sec
 ZDOT =     -18265
495066                 ZDOT =       -5567
322896


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   06350
65273244  
00020000  00000-0  20000-3 0  9040
2 25544  51
6344 326
8045 0023947 343
5181  16
5203 15
75993737 21953


Satellite: ISS
Catalog Number: 25544
Epoch time:      06350
65273244   =   yrday
fracday
Element set:     904
Inclination:       51
6344  deg
RA of node:       326
8045  deg
Eccentricity:     
0023947     
Arg of perigee:   343
5181  deg
Mean anomaly:      16
5203  deg
Mean motion:   15
75993737  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2195
Checksum:              295


Coasting Arc #6 (Orbit 2210)
---------------------------------------

Vector Time (GMT): 2006/351/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -348715
69                 A    =         6717408
42  meter
 Y    =        4936939
06  meter          E    =           
0026899
 Z    =        4553017
33                 I    =           51
42496
 XDOT =      -6698
932592                 Wp   =            5
19777
 YDOT =       2314
772243  meter/sec      RA   =          321
23990  deg
 ZDOT =      -2995
249484                 TA   =          114
80488
                                          MA   =          114
52484
                                          Ha   =            193
417  n
mi
                                          Hp   =            176
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1144080
35                 X    =         -426013
37
 Y    =       16197306
63  feet           Y    =         4932606
67  meter
 Z    =       14937720
90                 Z    =         4551136
21
 XDOT =     -21978
125303                 XDOT =       -6709
768228
 YDOT =       7594
397122  feet/sec       YDOT =        2239
800913  meter/sec
 ZDOT =      -9826
934003                 ZDOT =       -3027
819361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13135001
89                 X    =        -4003548
58
 Y    =        9556507
53  feet           Y    =         2912823
49  meter
 Z    =       14931244
32                 Z    =         4551043
27
 XDOT =     -19289
299612                 XDOT =       -5879
378522
 YDOT =     -10826
162683  feet/sec       YDOT =       -3299
814386  meter/sec
 ZDOT =      -9948
478235                 ZDOT =       -3032
296166


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   06351
66727165  
00020000  00000-0  20000-3 0  9059
2 25544  51
6343 321
5780 0023838 347
3854  12
6711 15
76030152 22112


Satellite: ISS
Catalog Number: 25544
Epoch time:      06351
66727165   =   yrday
fracday
Element set:     905
Inclination:       51
6343  deg
RA of node:       321
5780  deg
Eccentricity:     
0023838     
Arg of perigee:   347
3854  deg
Mean anomaly:      12
6711  deg
Mean motion:   15
76030152  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2211
Checksum:              273


Coasting Arc #7 (Orbit 2226)
---------------------------------------

Vector Time (GMT): 2006/352/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5598425
55                 A    =         6721733
84  meter
 Y    =       -1850031
57  meter          E    =           
0025813
 Z    =        3192778
96                 I    =           51
41901
 XDOT =       -738
109034                 Wp   =           20
56065
 YDOT =       6009
751052  meter/sec      RA   =          316
12035  deg
 ZDOT =       4788
734234                 TA   =           16
96557
                                          MA   =           16
87941
                                          Ha   =            193
403  n
mi
                                          Hp   =            176
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18367537
89                 X    =         5603186
64
 Y    =       -6069657
39  feet           Y    =        -1787400
79  meter
 Z    =       10474996
59                 Z    =         3219987
70
 XDOT =      -2421
617567                 XDOT =        -828
519143
 YDOT =      19717
031010  feet/sec       YDOT =        6000
990793  meter/sec
 ZDOT =      15711
070323                 ZDOT =        4784
929859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16653459
72                 X    =         5075974
52
 Y    =        9733016
81  feet           Y    =         2966623
52  meter
 Z    =       10576549
80                 Z    =         3223732
38
 XDOT =     -15747
857647                 XDOT =       -4799
947011
 YDOT =       9930
050485  feet/sec       YDOT =        3026
679388  meter/sec
 ZDOT =      15697
519558                 ZDOT =        4784
603961


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   06352
68177748  
00020000  00000-0  20000-3 0  9069
2 25544  51
6346 316
3507 0023816 351
3679   8
7072 15
76075314 22272


Satellite: ISS
Catalog Number: 25544
Epoch time:      06352
68177748   =   yrday
fracday
Element set:     906
Inclination:       51
6346  deg
RA of node:       316
3507  deg
Eccentricity:     
0023816     
Arg of perigee:   351
3679  deg
Mean anomaly:       8
7072  deg
Mean motion:   15
76075314  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2227
Checksum:              303


Coasting Arc #8 (Orbit 2241)
---------------------------------------

Vector Time (GMT): 2006/353/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         873557
81                 A    =         6720094
75  meter
 Y    =       -5526874
64  meter          E    =           
0022704
 Z    =       -3705272
35                 I    =           51
39492
 XDOT =       6139
528509                 Wp   =            8
89988
 YDOT =      -1877
021557  meter/sec      RA   =          310
90035  deg
 ZDOT =       4272
844963                 TA   =          306
14841
                                          MA   =          306
35829
                                          Ha   =            193
542  n
mi
                                          Hp   =            175
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2866003
30                 X    =          953294
85
 Y    =      -18132790
82  feet           Y    =        -5516659
52  meter
 Z    =      -12156405
34                 Z    =        -3700835
90
 XDOT =      20142
810068                 XDOT =        6139
304454
 YDOT =      -6158
207207  feet/sec       YDOT =       -1808
367980  meter/sec
 ZDOT =      14018
520220                 ZDOT =        4302
670146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15378535
72                 X    =         4687377
69
 Y    =      -10044936
94  feet           Y    =        -3061696
78  meter
 Z    =      -12140434
48                 Z    =        -3700404
43
 XDOT =      17333
862472                 XDOT =        5283
361282
 YDOT =       9561
702917  feet/sec       YDOT =        2914
407049  meter/sec
 ZDOT =      14129
864234                 ZDOT =        4306
782618


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   06353
63284556  
00020000  00000-0  20000-3 0  9072
2 25544  51
6351 311
4507 0023749 354
8974   5
1945 15
76141193 22421


Satellite: ISS
Catalog Number: 25544
Epoch time:      06353
63284556   =   yrday
fracday
Element set:     907
Inclination:       51
6351  deg
RA of node:       311
4507  deg
Eccentricity:     
0023749     
Arg of perigee:   354
8974  deg
Mean anomaly:       5
1945  deg
Mean motion:   15
76141193  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2242
Checksum:              295


Coasting Arc #9 (Orbit 2257)
---------------------------------------

Vector Time (GMT): 2006/354/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5089169
22                 A    =         6718118
42  meter
 Y    =        1308437
30  meter          E    =           
0027642
 Z    =       -4209276
25                 I    =           51
37200
 XDOT =       1272
346501                 Wp   =           15
14823
 YDOT =      -6674
741234  meter/sec      RA   =          305
78113  deg
 ZDOT =      -3592
159901                 TA   =          218
00922
                                          MA   =          218
20458
                                          Ha   =            193
615  n
mi
                                          Hp   =            175
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16696749
42                 X    =        -5082974
16
 Y    =        4292773
29  feet           Y    =         1251562
83  meter
 Z    =      -13809961
44                 Z    =        -4233984
20
 XDOT =       4174
365160                 XDOT =        1364
339935
 YDOT =     -21898
757329  feet/sec       YDOT =       -6659
998102  meter/sec
 ZDOT =     -11785
301514                 ZDOT =       -3585
756648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14526714
57                 X    =        -4427742
60
 Y    =       -9144766
01  feet           Y    =        -2787324
68  meter
 Z    =      -13902237
12                 Z    =        -4237401
87
 XDOT =      18172
524507                 XDOT =        5538
985470
 YDOT =     -10882
438864  feet/sec       YDOT =       -3316
967366  meter/sec
 ZDOT =     -11762
103317                 ZDOT =       -3585
089091


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   06354
64728591  
00020000  00000-0  20000-3 0  9087
2 25544  51
6358 306
2238 0023741 358
8937   1
2171 15
76206761 22584


Satellite: ISS
Catalog Number: 25544
Epoch time:      06354
64728591   =   yrday
fracday
Element set:     908
Inclination:       51
6358  deg
RA of node:       306
2238  deg
Eccentricity:     
0023741     
Arg of perigee:   358
8937  deg
Mean anomaly:       1
2171  deg
Mean motion:   15
76206761  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2258
Checksum:              303


Coasting Arc #10 (Orbit 2273)
---------------------------------------

Vector Time (GMT): 2006/355/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1306939
32                 A    =         6723175
63  meter
 Y    =        6117166
61  meter          E    =           
0024731
 Z    =        2484213
00                 I    =           51
37312
 XDOT =      -5494
896849                 Wp   =           35
68410
 YDOT =        992
935211  meter/sec      RA   =          300
56210  deg
 ZDOT =      -5289
551624                 TA   =          116
12172
                                          MA   =          115
86706
                                          Ha   =            193
709  n
mi
                                          Hp   =            175
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4287858
65                 X    =        -1387313
01
 Y    =       20069444
26  feet           Y    =         6102101
83  meter
 Z    =        8150305
11                 Z    =         2477669
82
 XDOT =     -18027
876801                 XDOT =       -5479
896004
 YDOT =       3257
661452  feet/sec       YDOT =         931
573086  meter/sec
 ZDOT =     -17354
171994                 ZDOT =       -5316
209126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17387440
45                 X    =        -5299691
85
 Y    =       10919356
24  feet           Y    =         3328219
78  meter
 Z    =        8126522
75                 Z    =         2476964
14
 XDOT =     -14061
098256                 XDOT =       -4285
822748
 YDOT =      -9287
112302  feet/sec       YDOT =       -2830
711830  meter/sec
 ZDOT =     -17453
784300                 ZDOT =       -5319
913455


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   06355
66169327  
00020000  00000-0  20000-3 0  9097
2 25544  51
6354 300
9962 0023603   2
7369 357
3920 15
76229434 22743


Satellite: ISS
Catalog Number: 25544
Epoch time:      06355
66169327   =   yrday
fracday
Element set:     909
Inclination:       51
6354  deg
RA of node:       300
9962  deg
Eccentricity:     
0023603     
Arg of perigee:     2
7369  deg
Mean anomaly:     357
3920  deg
Mean motion:   15
76229434  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2274
Checksum:              302


Coasting Arc #11 (Orbit 2289)
---------------------------------------

Vector Time (GMT): 2006/356/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4535380
43                 A    =         6714900
96  meter
 Y    =        -359165
83  meter          E    =           
0021442
 Z    =        4926059
84                 I    =           51
33308
 XDOT =      -1633
345555                 Wp   =           20
47157
 YDOT =       7256
393430  meter/sec      RA   =          295
42673  deg
 ZDOT =       2050
038531                 TA   =           49
72627
                                          MA   =           49
53900
                                          Ha   =            193
612  n
mi
                                          Hp   =            174
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14879857
05                 X    =         4515129
89
 Y    =       -1178365
58  feet           Y    =         -308562
76  meter
 Z    =       16161613
65                 Z    =         4948043
29
 XDOT =      -5358
745260                 XDOT =       -1724
324805
 YDOT =      23807
065059  feet/sec       YDOT =        7237
619410  meter/sec
 ZDOT =       6725
848199                 ZDOT =        2041
884064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11341288
73                 X    =         3456824
81
 Y    =        9566083
27  feet           Y    =         2915742
18  meter
 Z    =       16243819
38                 Z    =         4951116
15
 XDOT =     -19884
143397                 XDOT =       -6060
686907
 YDOT =      12298
675465  feet/sec       YDOT =        3748
636282  meter/sec
 ZDOT =       6696
173235                 ZDOT =        2040
993602


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   06356
67606567  
00020000  00000-0  20000-3 0  9103
2 25544  51
6358 295
7685 0023568   6
5190 353
6277 15
76300169 22901


Satellite: ISS
Catalog Number: 25544
Epoch time:      06356
67606567   =   yrday
fracday
Element set:     910
Inclination:       51
6358  deg
RA of node:       295
7685  deg
Eccentricity:     
0023568     
Arg of perigee:     6
5190  deg
Mean anomaly:     353
6277  deg
Mean motion:   15
76300169  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2290
Checksum:              316


Coasting Arc #12 (Orbit 2304)
---------------------------------------

Vector Time (GMT): 2006/357/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1482205
12                 A    =         6725041
47  meter
 Y    =       -6455050
42  meter          E    =           
0032484
 Z    =       -1051630
90                 I    =           51
35681
 XDOT =       4965
042172                 Wp   =           17
89869
 YDOT =        190
137804  meter/sec      RA   =          290
22552  deg
 ZDOT =       5909
295569                 TA   =          330
51874
                                          MA   =          330
70154
                                          Ha   =            193
737  n
mi
                                          Hp   =            174
541

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4862877
70                 X    =         1559384
82
 Y    =      -21177986
96  feet           Y    =        -6438043
89  meter
 Z    =       -3450232
61                 Z    =        -1044243
92
 XDOT =      16289
508439                 XDOT =        4933
841060
 YDOT =        623
811692  feet/sec       YDOT =         245
484334  meter/sec
 ZDOT =      19387
452654                 ZDOT =        5933
339710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18164450
87                 X    =         5536524
63
 Y    =      -11932822
53  feet           Y    =        -3637124
31  meter
 Z    =       -3423344
43                 Z    =        -1043435
38
 XDOT =      10394
449082                 XDOT =        3168
228080
 YDOT =      10309
370596  feet/sec       YDOT =        3142
296158  meter/sec
 ZDOT =      19477
438279                 ZDOT =        5936
723188


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   06357
62701002  
00020000  00000-0  20000-3 0  9110
2 25544  51
6360 290
8680 0023578   9
9348 350
2277 15
76346264 23054


Satellite: ISS
Catalog Number: 25544
Epoch time:      06357
62701002   =   yrday
fracday
Element set:     911
Inclination:       51
6360  deg
RA of node:       290
8680  deg
Eccentricity:     
0023578     
Arg of perigee:     9
9348  deg
Mean anomaly:     350
2277  deg
Mean motion:   15
76346264  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2305
Checksum:              286

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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