Date: December 16th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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


352/04:03:34 300 1 5 1 7 1 7
N/A -0 8 0 2 196 5
000/00:09:28 600 0 0 0 2 184 8

Coasting Arc #1 (Orbit 1658)
---------------------------------------

Vector Time (GMT): 2008/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1125242
84                 A    =         6726540
28  meter
 Y    =        4110125
29  meter          E    =           
0020730
 Z    =       -5222462
25                 I    =           51
60676
 XDOT =      -7572
349909                 Wp   =           93
68079
 YDOT =       -919
869175  meter/sec      RA   =          181
50546  deg
 ZDOT =        909
402897                 TA   =          184
99607
                                          MA   =          185
01679
                                          Ha   =            195
679  n
mi
                                          Hp   =            184
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3691741
59                 X    =        -1145749
17
 Y    =       13484663
02  feet           Y    =         4097428
51  meter
 Z    =      -17134062
50                 Z    =        -5227977
78
 XDOT =     -24843
667679                 XDOT =       -7565
918759
 YDOT =      -3017
943487  feet/sec       YDOT =       -1004
511785  meter/sec
 ZDOT =       2983
605304                 ZDOT =         872
631350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12736620
47                 X    =        -3882121
92
 Y    =       -5702645
23  feet           Y    =        -1738166
26  meter
 Z    =      -17155160
35                 Z    =        -5228892
88
 XDOT =       6537
592582                 XDOT =        1992
658219
 YDOT =     -23129
446601  feet/sec       YDOT =       -7049
855324  meter/sec
 ZDOT =       2840
720886                 ZDOT =         865
851726


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   08347
51446436  
00010596  00000-0  82463-4 0  9005
2 25544  51
6363 182
4550 0006179  85
1784 275
0083 15
71833360 16590


Satellite: ISS
Catalog Number: 25544
Epoch time:      08347
51446436   =   yrday
fracday
Element set:     900
Inclination:       51
6363  deg
RA of node:       182
4550  deg
Eccentricity:     
0006179     
Arg of perigee:    85
1784  deg
Mean anomaly:     275
0083  deg
Mean motion:   15
71833360  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1659
Checksum:              315


Coasting Arc #2 (Orbit 1674)
---------------------------------------

Vector Time (GMT): 2008/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6723674
32                 A    =         6738256
92  meter
 Y    =        -329310
44  meter          E    =           
0016832
 Z    =        -119002
47                 I    =           51
67631
 XDOT =        138
274143                 Wp   =          120
04753
 YDOT =       4772
916452  meter/sec      RA   =          176
39540  deg
 ZDOT =      -6037
478715                 TA   =           61
24345
                                          MA   =           61
07445
                                          Ha   =            195
639  n
mi
                                          Hp   =            184
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22059298
96                 X    =         6727435
10
 Y    =       -1080414
84  feet           Y    =         -254101
38  meter
 Z    =        -390428
06                 Z    =          -86329
61
 XDOT =        453
655325                 XDOT =         114
221470
 YDOT =      15659
174711  feet/sec       YDOT =        4774
329396  meter/sec
 ZDOT =     -19808
001034                 ZDOT =       -6036
864477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2082377
38                 X    =         -634708
62
 Y    =       21989239
49  feet           Y    =         6702320
20  meter
 Z    =        -263537
82                 Z    =          -80326
33
 XDOT =     -13975
934500                 XDOT =       -4259
864836
 YDOT =      -1523
476362  feet/sec       YDOT =        -464
355595  meter/sec
 ZDOT =     -19805
240914                 ZDOT =       -6036
637431


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   08348
53169697  
00010596  00000-0  82463-4 0  9010
2 25544  51
6366 177
2477 0006145  87
5031 272
6834 15
71864668 16757


Satellite: ISS
Catalog Number: 25544
Epoch time:      08348
53169697   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       177
2477  deg
Eccentricity:     
0006145     
Arg of perigee:    87
5031  deg
Mean anomaly:     272
6834  deg
Mean motion:   15
71864668  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1675
Checksum:              347


Coasting Arc #3 (Orbit 1690)
---------------------------------------

Vector Time (GMT): 2008/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1373356
29                 A    =         6726510
32  meter
 Y    =       -3980056
86  meter          E    =           
0009120
 Z    =        5238351
01                 I    =           51
66480
 XDOT =       7486
652430                 Wp   =          101
11529
 YDOT =      -1689
246597  meter/sec      RA   =          171
28245  deg
 ZDOT =        676
607668                 TA   =          342
44083
                                          MA   =          342
47234
                                          Ha   =            195
794  n
mi
                                          Hp   =            184
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4505762
09                 X    =        -1354195
48
 Y    =      -13057929
32  feet           Y    =        -3995308
31  meter
 Z    =       17186190
99                 Z    =         5231725
10
 XDOT =      24562
507973                 XDOT =        7501
698605
 YDOT =      -5542
147628  feet/sec       YDOT =       -1605
442512  meter/sec
 ZDOT =       2219
841432                 ZDOT =         713
014020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13533301
02                 X    =         4124950
15
 Y    =       -2925076
33  feet           Y    =         -891563
26  meter
 Z    =       17160135
86                 Z    =         5230409
41
 XDOT =       2196
073184                 XDOT =         669
363106
 YDOT =      24064
678581  feet/sec       YDOT =        7334
914031  meter/sec
 ZDOT =       2361
151218                 ZDOT =         719
678891


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   08349
54892357  
00010596  00000-0  82463-4 0  9029
2 25544  51
6359 172
0390 0006251  92
5727 267
6151 15
71810047 16918


Satellite: ISS
Catalog Number: 25544
Epoch time:      08349
54892357   =   yrday
fracday
Element set:     902
Inclination:       51
6359  deg
RA of node:       172
0390  deg
Eccentricity:     
0006251     
Arg of perigee:    92
5727  deg
Mean anomaly:     267
6151  deg
Mean motion:   15
71810047  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1691
Checksum:              317


Coasting Arc #4 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2008/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6100317
69                 A    =         6737494
59  meter
 Y    =        2548967
16  meter          E    =           
0013165
 Z    =       -1285852
45                 I    =           51
73139
 XDOT =      -2914
262985                 Wp   =           61
80311
 YDOT =      -4043
693673  meter/sec      RA   =          166
14827  deg
 ZDOT =       5861
346243                 TA   =          284
12353
                                          MA   =          284
26979
                                          Ha   =            195
612  n
mi
                                          Hp   =            184
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20014165
66                 X    =        -6122120
87
 Y    =        8362753
15  feet           Y    =         2480628
16  meter
 Z    =       -4218676
01                 Z    =        -1315540
20
 XDOT =      -9561
230267                 XDOT =       -2897
302336
 YDOT =     -13266
711524  feet/sec       YDOT =       -4076
188685  meter/sec
 ZDOT =      19230
138592                 ZDOT =        5847
229431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6139594
96                 X    =        -1871348
54
 Y    =      -20780350
59  feet           Y    =        -6333850
86  meter
 Z    =       -4333831
77                 Z    =        -1320951
92
 XDOT =      12724
148649                 XDOT =        3878
320508
 YDOT =      -7724
137288  feet/sec       YDOT =       -2354
317045  meter/sec
 ZDOT =      19174
965230                 ZDOT =        5844
529402


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   08350
50256269  
00010596  00000-0  82463-4 0  9034
2 25544  51
6360 167
1560 0006210  97
0749 263
1119 15
71865210 17067


Satellite: ISS
Catalog Number: 25544
Epoch time:      08350
50256269   =   yrday
fracday
Element set:     903
Inclination:       51
6360  deg
RA of node:       167
1560  deg
Eccentricity:     
0006210     
Arg of perigee:    97
0749  deg
Mean anomaly:     263
1119  deg
Mean motion:   15
71865210  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1706
Checksum:              291


Coasting Arc #5 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2008/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3578103
26                 A    =         6727774
28  meter
 Y    =        2884408
38  meter          E    =           
0018359
 Z    =       -4929651
38                 I    =           51
72736
 XDOT =      -6208
286679                 Wp   =           83
02843
 YDOT =       3959
811328  meter/sec      RA   =          161
06545  deg
 ZDOT =      -2194
019872                 TA   =          165
66868
                                          MA   =          165
61653
                                          Ha   =            195
661  n
mi
                                          Hp   =            184
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11739183
94                 X    =         3569530
60
 Y    =        9463282
09  feet           Y    =         2924373
46  meter
 Z    =      -16173396
92                 Z    =        -4912289
55
 XDOT =     -20368
394617                 XDOT =       -6241
446444
 YDOT =      12991
506981  feet/sec       YDOT =        3890
201528  meter/sec
 ZDOT =      -7198
227925                 ZDOT =       -2224
259608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10507331
58                 X    =        -3202634
67
 Y    =       10915284
94  feet           Y    =         3326978
85  meter
 Z    =      -16105696
30                 Z    =        -4909016
23
 XDOT =     -10278
553800                 XDOT =       -3132
903198
 YDOT =     -20665
195116  feet/sec       YDOT =       -6298
751471  meter/sec
 ZDOT =      -7315
429256                 ZDOT =       -2229
742837


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   08351
51977119  
00010596  00000-0  82463-4 0  9041
2 25544  51
6364 161
9484 0006380 100
3673 259
8208 15
71889180 17221


Satellite: ISS
Catalog Number: 25544
Epoch time:      08351
51977119   =   yrday
fracday
Element set:     904
Inclination:       51
6364  deg
RA of node:       161
9484  deg
Eccentricity:     
0006380     
Arg of perigee:   100
3673  deg
Mean anomaly:     259
8208  deg
Mean motion:   15
71889180  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1722
Checksum:              322


Coasting Arc #6 (Orbit 1732)
---------------------------------------

Vector Time (GMT): 2008/352/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -886275
00                 A    =         6727099
25  meter
 Y    =       -4107613
25  meter          E    =           
0009988
 Z    =        5244665
41                 I    =           51
74350
 XDOT =       7281
713448                 Wp   =           87
94099
 YDOT =      -2428
542574  meter/sec      RA   =          157
60879  deg
 ZDOT =       -670
079388                 TA   =            8
42583
                                          MA   =            8
40907
                                          Ha   =            196
538  n
mi
                                          Hp   =            184
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2907726
39                 X    =         -865754
62
 Y    =      -13476421
43  feet           Y    =        -4117409
89  meter
 Z    =       17206907
51                 Z    =         5240409
33
 XDOT =      23890
135985                 XDOT =        7311
583722
 YDOT =      -7967
659364  feet/sec       YDOT =       -2346
947158  meter/sec
 ZDOT =      -2198
423189                 ZDOT =        -634
632708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4708693
08                 X    =        -1435209
65
 Y    =       12979879
06  feet           Y    =         3956267
14  meter
 Z    =       17190038
47                 Z    =         5239523
73
 XDOT =     -23491
839337                 XDOT =       -7160
312630
 YDOT =      -5786
508030  feet/sec       YDOT =       -1763
727647  meter/sec
 ZDOT =      -2060
856049                 ZDOT =        -628
148924


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   08352
21910950  
00010596  00000-0  82463-4 0  9050
2 25544  51
6390 158
3717 0007392  96
6179 263
5824 15
71588741 17338


Satellite: ISS
Catalog Number: 25544
Epoch time:      08352
21910950   =   yrday
fracday
Element set:     905
Inclination:       51
6390  deg
RA of node:       158
3717  deg
Eccentricity:     
0007392     
Arg of perigee:    96
6179  deg
Mean anomaly:     263
5824  deg
Mean motion:   15
71588741  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1733
Checksum:              328


Coasting Arc #7 (Orbit 1747)
---------------------------------------

Vector Time (GMT): 2008/353/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5888854
72                 A    =         6739086
08  meter
 Y    =        3260129
65  meter          E    =           
0017011
 Z    =        -220076
49                 I    =           51
81040
 XDOT =      -2468
070471                 Wp   =           64
93321
 YDOT =      -4075
082690  meter/sec      RA   =          152
50442  deg
 ZDOT =       6043
828174                 TA   =          292
68391
                                          MA   =          292
86368
                                          Ha   =            196
534  n
mi
                                          Hp   =            184
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19320389
49                 X    =        -5923803
26
 Y    =       10695963
43  feet           Y    =         3194081
68  meter
 Z    =        -722035
74                 Z    =         -248769
09
 XDOT =      -8097
344066                 XDOT =       -2451
678548
 YDOT =     -13369
693864  feet/sec       YDOT =       -4102
590947  meter/sec
 ZDOT =      19828
832591                 ZDOT =        6031
877783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22057620
16                 X    =         6723162
62
 Y    =         984596
12  feet           Y    =          300104
90  meter
 Z    =        -833296
41                 Z    =         -253988
74
 XDOT =         79
106244                 XDOT =          24
111583
 YDOT =      14081
287840  feet/sec       YDOT =        4291
976534  meter/sec
 ZDOT =      19782
058402                 ZDOT =        6029
571401


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   08353
17292756  
00010596  00000-0  82463-4 0  9064
2 25544  51
6391 153
4907 0007448  99
5795 260
6208 15
71563933 17480


Satellite: ISS
Catalog Number: 25544
Epoch time:      08353
17292756   =   yrday
fracday
Element set:     906
Inclination:       51
6391  deg
RA of node:       153
4907  deg
Eccentricity:     
0007448     
Arg of perigee:    99
5795  deg
Mean anomaly:     260
6208  deg
Mean motion:   15
71563933  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1748
Checksum:              344


Coasting Arc #8 (Orbit 1763)
---------------------------------------

Vector Time (GMT): 2008/354/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3257797
42                 A    =         6727396
97  meter
 Y    =        2780381
78  meter          E    =           
0021463
 Z    =       -5206323
44                 I    =           51
79764
 XDOT =      -5885
307068                 Wp   =           89
02197
 YDOT =       4807
430699  meter/sec      RA   =          147
41037  deg
 ZDOT =      -1118
904962                 TA   =          170
31611
                                          MA   =          170
27467
                                          Ha   =            196
495  n
mi
                                          Hp   =            184
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10688311
75                 X    =         3251756
02
 Y    =        9121987
46  feet           Y    =         2816778
99  meter
 Z    =      -17081113
65                 Z    =        -5190511
49
 XDOT =     -19308
750223                 XDOT =       -5933
191690
 YDOT =      15772
410430  feet/sec       YDOT =        4741
350140  meter/sec
 ZDOT =      -3670
948037                 ZDOT =       -1147
611756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4653702
97                 X    =        -1418448
67
 Y    =      -13337808
51  feet           Y    =        -4065364
03  meter
 Z    =      -17019430
66                 Z    =        -5187522
46
 XDOT =      23653
972965                 XDOT =        7209
730960
 YDOT =      -3442
109215  feet/sec       YDOT =       -1049
154889  meter/sec
 ZDOT =      -3782
150000                 ZDOT =       -1152
799320


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   08354
19032411  
00010596  00000-0  82463-4 0  9078
2 25544  51
6400 148
2841 0007489 103
2504 256
9494 15
71600107 17644


Satellite: ISS
Catalog Number: 25544
Epoch time:      08354
19032411   =   yrday
fracday
Element set:     907
Inclination:       51
6400  deg
RA of node:       148
2841  deg
Eccentricity:     
0007489     
Arg of perigee:   103
2504  deg
Mean anomaly:     256
9494  deg
Mean motion:   15
71600107  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1764
Checksum:              292


Coasting Arc #9 (Orbit 1779)
---------------------------------------

Vector Time (GMT): 2008/355/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4203810
43                 A    =         6737734
47  meter
 Y    =       -4962352
34  meter          E    =           
0021526
 Z    =        1723426
87                 I    =           51
85633
 XDOT =       4744
000463                 Wp   =          112
59176
 YDOT =       2014
005654  meter/sec      RA   =          142
28086  deg
 ZDOT =      -5724
275907                 TA   =           48
40005
                                          MA   =           48
21579
                                          Ha   =            196
478  n
mi
                                          Hp   =            184
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13792028
97                 X    =         4250615
69
 Y    =      -16280683
53  feet           Y    =        -4915081
34  meter
 Z    =        5654287
63                 Z    =         1743962
37
 XDOT =      15564
305980                 XDOT =        4748
934577
 YDOT =       6607
630100  feet/sec       YDOT =        2067
083879  meter/sec
 ZDOT =     -18780
432766                 ZDOT =       -5701
217278

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20000096
63                 X    =        -6096029
45
 Y    =        7373752
49  feet           Y    =         2247519
76  meter
 Z    =        5733724
55                 Z    =         1747639
24
 XDOT =      -9834
940844                 XDOT =       -2997
689969
 YDOT =     -12020
493142  feet/sec       YDOT =       -3663
846310  meter/sec
 ZDOT =     -18690
638019                 ZDOT =       -5696
906468


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   08355
20771237  
00010596  00000-0  82463-4 0  9088
2 25544  51
6397 143
0778 0007471 107
2501 252
9479 15
71586904 17808


Satellite: ISS
Catalog Number: 25544
Epoch time:      08355
20771237   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:       143
0778  deg
Eccentricity:     
0007471     
Arg of perigee:   107
2501  deg
Mean anomaly:     252
9479  deg
Mean motion:   15
71586904  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1780
Checksum:              326


Coasting Arc #10 (Orbit 1795)
---------------------------------------

Vector Time (GMT): 2008/356/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4792100
65                 A    =         6729557
32  meter
 Y    =        -574075
64  meter          E    =           
0015440
 Z    =        4680407
29                 I    =           51
85157
 XDOT =       3508
278973                 Wp   =          113
89060
 YDOT =      -6255
685450  meter/sec      RA   =          137
21588  deg
 ZDOT =       2811
330769                 TA   =          308
39112
                                          MA   =          308
52970
                                          Ha   =            196
531  n
mi
                                          Hp   =            184
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15722114
98                 X    =        -4808061
83
 Y    =       -1883450
27  feet           Y    =         -627753
37  meter
 Z    =       15355666
95                 Z    =         4657088
24
 XDOT =      11510
101616                 XDOT =        3564
313281
 YDOT =     -20523
902395  feet/sec       YDOT =       -6216
140805  meter/sec
 ZDOT =       9223
526145                 ZDOT =        2828
509646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12983772
33                 X    =         3957453
81
 Y    =        9215813
21  feet           Y    =         2808979
87  meter
 Z    =       15264967
57                 Z    =         4652762
12
 XDOT =     -19205
760528                 XDOT =       -5853
915809
 YDOT =      11597
495076  feet/sec       YDOT =        3534
916499  meter/sec
 ZDOT =       9289
825030                 ZDOT =        2831
538669


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   08356
22509077  
00010596  00000-0  82463-4 0  9093
2 25544  51
6399 137
8715 0007418 110
4466 249
7493 15
71617028 17968


Satellite: ISS
Catalog Number: 25544
Epoch time:      08356
22509077   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       137
8715  deg
Eccentricity:     
0007418     
Arg of perigee:   110
4466  deg
Mean anomaly:     249
7493  deg
Mean motion:   15
71617028  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1796
Checksum:              341


Coasting Arc #11 (Orbit 1810)
---------------------------------------

Vector Time (GMT): 2008/357/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1830887
77                 A    =         6734644
75  meter
 Y    =        5685135
12  meter          E    =           
0011313
 Z    =       -3123532
13                 I    =           51
89037
 XDOT =      -5878
001618                 Wp   =          100
02008
 YDOT =        786
959207  meter/sec      RA   =          132
06863  deg
 ZDOT =       4890
810744                 TA   =          223
89570
                                          MA   =          223
98564
                                          Ha   =            196
313  n
mi
                                          Hp   =            184
894

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6006849
63                 X    =        -1879150
11
 Y    =       18652018
10  feet           Y    =         5664391
57  meter
 Z    =      -10247808
82                 Z    =        -3132543
27
 XDOT =     -19284
782210                 XDOT =       -5910
123557
 YDOT =       2581
887163  feet/sec       YDOT =         721
047844  meter/sec
 ZDOT =      16045
967009                 ZDOT =        4862
177197

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13909498
46                 X    =         4239615
13
 Y    =      -13776628
86  feet           Y    =        -4199116
48  meter
 Z    =      -10282410
06                 Z    =        -3134078
59
 XDOT =      17364
797238                 XDOT =        5292
790198
 YDOT =       5670
928941  feet/sec       YDOT =        1728
499141  meter/sec
 ZDOT =      15934
702594                 ZDOT =        4856
897351


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   08357
17887519  
00010596  00000-0  82463-4 0  9100
2 25544  51
6404 132
9903 0007330 113
4857 246
7075 15
71639363 18117


Satellite: ISS
Catalog Number: 25544
Epoch time:      08357
17887519   =   yrday
fracday
Element set:     910
Inclination:       51
6404  deg
RA of node:       132
9903  deg
Eccentricity:     
0007330     
Arg of perigee:   113
4857  deg
Mean anomaly:     246
7075  deg
Mean motion:   15
71639363  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1811
Checksum:              317


Coasting Arc #12 (Orbit 1826)
---------------------------------------

Vector Time (GMT): 2008/358/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5207398
43                 A    =         6732733
28  meter
 Y    =       -1952592
28  meter          E    =           
0012421
 Z    =       -3803664
27                 I    =           51
90284
 XDOT =       -675
924454                 Wp   =           98
78811
 YDOT =       6391
442383  meter/sec      RA   =          127
01910  deg
 ZDOT =      -4219
900042                 TA   =          127
04793
                                          MA   =          126
93427
                                          Ha   =            196
270  n
mi
                                          Hp   =            185
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17084640
51                 X    =         5247323
29
 Y    =       -6406142
64  feet           Y    =        -1894136
41  meter
 Z    =      -12479213
47                 Z    =        -3778269
76
 XDOT =      -2217
599914                 XDOT =        -726
844672
 YDOT =      20969
299157  feet/sec       YDOT =        6383
599642  meter/sec
 ZDOT =     -13844
816411                 ZDOT =       -4223
306572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18208640
28                 X    =        -5549993
56
 Y    =       -1954498
32  feet           Y    =         -595731
09  meter
 Z    =      -12380619
09                 Z    =        -3773612
70
 XDOT =      11159
056127                 XDOT =        3401
280307
 YDOT =     -16464
052145  feet/sec       YDOT =       -5018
243094  meter/sec
 ZDOT =     -13857
584679                 ZDOT =       -4223
791810


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   08358
19623648  
00010596  00000-0  82463-4 0  9115
2 25544  51
6407 127
7836 0007167 117
4379 242
7512 15
71639352 18275


Satellite: ISS
Catalog Number: 25544
Epoch time:      08358
19623648   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       127
7836  deg
Eccentricity:     
0007167     
Arg of perigee:   117
4379  deg
Mean anomaly:     242
7512  deg
Mean motion:   15
71639352  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1827
Checksum:              330


Coasting Arc #13 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2008/359/04:08:18
600
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -633223
50                 A    =         6731118
88  meter
 Y    =       -5212150
79  meter          E    =           
0015974
 Z    =        4197780
64                 I    =           51
91474
 XDOT =       5684
231248                 Wp   =           92
87599
 YDOT =      -3669
476849  meter/sec      RA   =          121
86986  deg
 ZDOT =      -3687
550857                 TA   =           34
62212
                                          MA   =           34
51823
                                          Ha   =            196
163  n
mi
                                          Hp   =            184
993

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2077504
92                 X    =         -595285
52
 Y    =      -17100232
25  feet           Y    =        -5219020
36  meter
 Z    =       13772246
18                 Z    =         4194795
80
 XDOT =      18649
052651                 XDOT =        5742
755062
 YDOT =     -12038
966041  feet/sec       YDOT =       -3605
584722  meter/sec
 ZDOT =     -12098
263965                 ZDOT =       -3659
795031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5448577
82                 X    =        -1660726
52
 Y    =       16351667
52  feet           Y    =         4983988
26  meter
 Z    =       13760258
13                 Z    =         4194126
68
 XDOT =     -20891
204082                 XDOT =       -6367
639004
 YDOT =       3160
029116  feet/sec       YDOT =         963
176875  meter/sec
 ZDOT =     -11990
599881                 ZDOT =       -3654
734844


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   08359
21358883  
00010596  00000-0  82463-4 0  9126
2 25544  51
6407 122
5771 0007132 119
9650 240
2221 15
71686887 18430


Satellite: ISS
Catalog Number: 25544
Epoch time:      08359
21358883   =   yrday
fracday
Element set:     912
Inclination:       51
6407  deg
RA of node:       122
5771  deg
Eccentricity:     
0007132     
Arg of perigee:   119
9650  deg
Mean anomaly:     240
2221  deg
Mean motion:   15
71686887  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1843
Checksum:              316

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics 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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