Date: January 2nd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 2287)
---------------------------------------

Vector Time (GMT): 2006/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4251107
34                 A    =         6714069
25  meter
 Y    =         679483
18  meter          E    =           
0022252
 Z    =        5144480
28                 I    =           51
33031
 XDOT =      -2507
920086                 Wp   =           12
40776
 YDOT =       7202
762837  meter/sec      RA   =          296
07740  deg
 ZDOT =       1141
607419                 TA   =           66
77982
                                          MA   =           66
54564
                                          Ha   =            193
730  n
mi
                                          Hp   =            174
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13947202
56                 X    =         4218202
56
 Y    =        2229275
53  feet           Y    =          726836
55  meter
 Z    =       16878216
15                 Z    =         5165052
20
 XDOT =      -8228
084271                 XDOT =       -2593
821678
 YDOT =      23631
111669  feet/sec       YDOT =        7174
237383  meter/sec
 ZDOT =       3745
431166                 ZDOT =        1129
216639

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2187005
25                 X    =         -666599
20
 Y    =       13860176
77  feet           Y    =         4224581
88  meter
 Z    =       16955259
27                 Z    =         5167963
02
 XDOT =     -22645
392706                 XDOT =       -6902
315697
 YDOT =      -8017
261234  feet/sec       YDOT =       -2443
661224  meter/sec
 ZDOT =       3699
899961                 ZDOT =        1127
729508


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
54948842  
00020000  00000-0  20000-3 0  9003
2 25544  51
6349 296
4320 0023931   4
1908 355
9452 15
76259134 22882


Satellite: ISS
Catalog Number: 25544
Epoch time:      06356
54948842   =   yrday
fracday
Element set:     900
Inclination:       51
6349  deg
RA of node:       296
4320  deg
Eccentricity:     
0023931     
Arg of perigee:     4
1908  deg
Mean anomaly:     355
9452  deg
Mean motion:   15
76259134  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2288
Checksum:              307


Coasting Arc #2 (Orbit 2302)
---------------------------------------

Vector Time (GMT): 2006/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2194354
48                 A    =         6725745
44  meter
 Y    =       -6329795
86  meter          E    =           
0034285
 Z    =        -259021
08                 I    =           51
35776
 XDOT =       4632
998214                 Wp   =           19
28063
 YDOT =       1370
099812  meter/sec      RA   =          290
89130  deg
 ZDOT =       6025
025560                 TA   =          337
88411
                                          MA   =          338
03167
                                          Ha   =            193
938  n
mi
                                          Hp   =            174
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7199325
71                 X    =         2266230
32
 Y    =      -20767046
80  feet           Y    =        -6304855
46  meter
 Z    =        -849806
68                 Z    =         -248187
40
 XDOT =      15200
125375                 XDOT =        4588
065082
 YDOT =       4495
078124  feet/sec       YDOT =        1421
656425  meter/sec
 ZDOT =      19767
144226                 ZDOT =        6047
423481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20908628
96                 X    =         6372950
11
 Y    =        6782021
73  feet           Y    =         2067160
22  meter
 Z    =        -810006
86                 Z    =         -246890
09
 XDOT =      -3693
993548                 XDOT =       -1125
929233
 YDOT =      13653
565447  feet/sec       YDOT =        4161
606748  meter/sec
 ZDOT =      19851
106633                 ZDOT =        6050
617302


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
50047482  
00020000  00000-0  20000-3 0  9011
2 25544  51
6344 291
5315 0023980   8
0444 352
1101 15
76258844 23034


Satellite: ISS
Catalog Number: 25544
Epoch time:      06357
50047482   =   yrday
fracday
Element set:     901
Inclination:       51
6344  deg
RA of node:       291
5315  deg
Eccentricity:     
0023980     
Arg of perigee:     8
0444  deg
Mean anomaly:     352
1101  deg
Mean motion:   15
76258844  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2303
Checksum:              267


Coasting Arc #3 (Orbit 2318)
---------------------------------------

Vector Time (GMT): 2006/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3850783
79                 A    =         6713630
99  meter
 Y    =       -1762556
23  meter          E    =           
0029692
 Z    =       -5224418
24                 I    =           51
30887
 XDOT =       2533
887706                 Wp   =           41
55276
 YDOT =      -7237
925071  meter/sec      RA   =          285
71357  deg
 ZDOT =        598
022300                 TA   =          234
02592
                                          MA   =          234
30163
                                          Ha   =            193
954  n
mi
                                          Hp   =            174
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12633805
09                 X    =        -3805409
48
 Y    =       -5782664
78  feet           Y    =        -1805363
48  meter
 Z    =      -17140479
77                 Z    =        -5243015
12
 XDOT =       8313
279874                 XDOT =        2611
729831
 YDOT =     -23746
473329  feet/sec       YDOT =       -7209
154567  meter/sec
 ZDOT =       1962
015420                 ZDOT =         610
519956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5309070
66                 X    =         1618204
74
 Y    =      -12746315
54  feet           Y    =        -3885076
98  meter
 Z    =      -17210273
06                 Z    =        -5245691
23
 XDOT =      23111
194701                 XDOT =        7044
292145
 YDOT =       7020
251653  feet/sec       YDOT =        2139
772704  meter/sec
 ZDOT =       2007
926954                 ZDOT =         612
016136


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   06358
51482846  
00020000  00000-0  20000-3 0  9021
2 25544  51
6347 286
3040 0023901  11
8942 348
2781 15
76315592 23193


Satellite: ISS
Catalog Number: 25544
Epoch time:      06358
51482846   =   yrday
fracday
Element set:     902
Inclination:       51
6347  deg
RA of node:       286
3040  deg
Eccentricity:     
0023901     
Arg of perigee:    11
8942  deg
Mean anomaly:     348
2781  deg
Mean motion:   15
76315592  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2319
Checksum:              296


Coasting Arc #4 (Orbit 2334)
---------------------------------------

Vector Time (GMT): 2006/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2241882
24                 A    =         6724632
37  meter
 Y    =        6211713
21  meter          E    =           
0019831
 Z    =       -1332615
31                 I    =           51
34037
 XDOT =      -4210
805877                 Wp   =           36
50194
 YDOT =      -2759
208839  meter/sec      RA   =          280
55505  deg
 ZDOT =      -5806
273817                 TA   =          158
17174
                                          MA   =          158
08713
                                          Ha   =            194
038  n
mi
                                          Hp   =            174
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7355256
70                 X    =        -2304702
34
 Y    =       20379636
53  feet           Y    =         6186292
13  meter
 Z    =       -4372097
49                 Z    =        -1343658
25
 XDOT =     -13814
979911                 XDOT =       -4151
433533
 YDOT =      -9052
522439  feet/sec       YDOT =       -2805
963877  meter/sec
 ZDOT =     -19049
454779                 ZDOT =       -5826
585752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20749675
85                 X    =        -6324501
20
 Y    =       -6206757
55  feet           Y    =        -1891819
70  meter
 Z    =       -4412678
91                 Z    =        -1344984
53
 XDOT =       7837
447767                 XDOT =        2388
854079
 YDOT =     -12670
095283  feet/sec       YDOT =       -3861
845042  meter/sec
 ZDOT =     -19125
790206                 ZDOT =       -5829
540855


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   06359
52915051  
00020000  00000-0  20000-3 0  9033
2 25544  51
6349 281
0759 0023855  15
8580 344
3326 15
76372146 23352


Satellite: ISS
Catalog Number: 25544
Epoch time:      06359
52915051   =   yrday
fracday
Element set:     903
Inclination:       51
6349  deg
RA of node:       281
0759  deg
Eccentricity:     
0023855     
Arg of perigee:    15
8580  deg
Mean anomaly:     344
3326  deg
Mean motion:   15
76372146  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2335
Checksum:              297


Coasting Arc #5 (Orbit 2350)
---------------------------------------

Vector Time (GMT): 2006/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3571549
88                 A    =         6715167
50  meter
 Y    =        3054239
93  meter          E    =           
0029570
 Z    =        4794565
54                 I    =           51
30432
 XDOT =      -2579
893340                 Wp   =           28
19565
 YDOT =       6849
993197  meter/sec      RA   =          275
34599  deg
 ZDOT =      -2409
980009                 TA   =           85
59464
                                          MA   =           85
25685
                                          Ha   =            194
001  n
mi
                                          Hp   =            173
719

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11717683
33                 X    =         3513840
52
 Y    =       10020472
20  feet           Y    =         3093855
93  meter
 Z    =       15730201
91                 Z    =         4811776
09
 XDOT =      -8464
216996                 XDOT =       -2644
592019
 YDOT =      22473
730960  feet/sec       YDOT =        6820
781839  meter/sec
 ZDOT =      -7906
758561                 ZDOT =       -2422
669652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9159569
20                 X    =        -2791836
69
 Y    =       12319672
84  feet           Y    =         3755036
28  meter
 Z    =       15794972
97                 Z    =         4814307
76
 XDOT =     -22121
924169                 XDOT =       -6742
762487
 YDOT =      -6117
190666  feet/sec       YDOT =       -1864
519715  meter/sec
 ZDOT =      -7953
418756                 ZDOT =       -2424
202037


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   06360
54344123  
00020000  00000-0  20000-3 0  9044
2 25544  51
6343 275
8478 0023822  19
6501 340
5576 15
76427218 23518


Satellite: ISS
Catalog Number: 25544
Epoch time:      06360
54344123   =   yrday
fracday
Element set:     904
Inclination:       51
6343  deg
RA of node:       275
8478  deg
Eccentricity:     
0023822     
Arg of perigee:    19
6501  deg
Mean anomaly:     340
5576  deg
Mean motion:   15
76427218  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2351
Checksum:              284


Coasting Arc #6 (Orbit 2366)
---------------------------------------

Vector Time (GMT): 2006/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2269008
09                 A    =         6721735
79  meter
 Y    =       -5643641
41  meter          E    =           
0033121
 Z    =        2808789
72                 I    =           51
32561
 XDOT =       4055
706862                 Wp   =           43
48748
 YDOT =       4167
689404  meter/sec      RA   =          270
21105  deg
 ZDOT =       5086
133881                 TA   =          348
99119
                                          MA   =          349
06349
                                          Ha   =            194
048  n
mi
                                          Hp   =            173
501

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7444252
25                 X    =         2318302
88
 Y    =      -18515883
90  feet           Y    =        -5617992
69  meter
 Z    =        9215189
38                 Z    =         2819931
85
 XDOT =      13306
124875                 XDOT =        3984
094273
 YDOT =      13673
521666  feet/sec       YDOT =        4212
641780  meter/sec
 ZDOT =      16686
790949                 ZDOT =        5105
662840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19100084
35                 X    =         5821705
71
 Y    =        5717000
27  feet           Y    =         1742541
68  meter
 Z    =        9256200
58                 Z    =         2821289
94
 XDOT =     -12027
178264                 XDOT =       -3665
883935
 YDOT =      12984
336839  feet/sec       YDOT =        3957
625869  meter/sec
 ZDOT =      16760
377003                 ZDOT =        5108
562910


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   06361
55770214  
00020000  00000-0  20000-3 0  9051
2 25544  51
6346 270
6191 0023807  23
6365 336
5888 15
76451575 23673


Satellite: ISS
Catalog Number: 25544
Epoch time:      06361
55770214   =   yrday
fracday
Element set:     905
Inclination:       51
6346  deg
RA of node:       270
6191  deg
Eccentricity:     
0023807     
Arg of perigee:    23
6365  deg
Mean anomaly:     336
5888  deg
Mean motion:   15
76451575  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2367
Checksum:              306


Coasting Arc #7 (Orbit 2381)
---------------------------------------

Vector Time (GMT): 2006/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3524630
76                 A    =         6718214
48  meter
 Y    =       -4154369
85  meter          E    =           
0025789
 Z    =       -3931446
35                 I    =           51
31621
 XDOT =       2679
578757                 Wp   =           42
49383
 YDOT =      -6018
144310  meter/sec      RA   =          264
98345  deg
 ZDOT =       3991
027614                 TA   =          268
94765
                                          MA   =          269
24314
                                          Ha   =            194
026  n
mi
                                          Hp   =            173
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11563749
21                 X    =        -3458815
75
 Y    =      -13629822
33  feet           Y    =        -4193415
89  meter
 Z    =      -12898446
03                 Z    =        -3948409
55
 XDOT =       8791
268889                 XDOT =        2727
287604
 YDOT =     -19744
567946  feet/sec       YDOT =       -5987
913366  meter/sec
 ZDOT =      13093
922619                 ZDOT =        4004
160400

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12334054
82                 X    =         3759419
91
 Y    =      -12872789
05  feet           Y    =        -3923626
10  meter
 Z    =      -12962432
51                 Z    =        -3950949
43
 XDOT =      19619
254567                 XDOT =        5979
948792
 YDOT =       5675
897517  feet/sec       YDOT =        1730
013563  meter/sec
 ZDOT =      13142
337254                 ZDOT =        4005
784395


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   06362
50854272  
00020000  00000-0  20000-3 0  9065
2 25544  51
6351 265
7174 0023727  27
1047 333
1351 15
76512496 23827


Satellite: ISS
Catalog Number: 25544
Epoch time:      06362
50854272   =   yrday
fracday
Element set:     906
Inclination:       51
6351  deg
RA of node:       265
7174  deg
Eccentricity:     
0023727     
Arg of perigee:    27
1047  deg
Mean anomaly:     333
1351  deg
Mean motion:   15
76512496  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2382
Checksum:              284


Coasting Arc #8 (Orbit 2397)
---------------------------------------

Vector Time (GMT): 2006/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2481248
52                 A    =         6717567
46  meter
 Y    =        4741009
63  meter          E    =           
0029964
 Z    =       -4093637
80                 I    =           51
31872
 XDOT =      -4017
815161                 Wp   =           40
21898
 YDOT =      -5356
912167  meter/sec      RA   =          259
85648  deg
 ZDOT =      -3761
591487                 TA   =          190
89056
                                          MA   =          190
95558
                                          Ha   =            194
088  n
mi
                                          Hp   =            172
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8140579
14                 X    =        -2514192
49
 Y    =       15554493
52  feet           Y    =         4713079
18  meter
 Z    =      -13430570
21                 Z    =        -4105771
27
 XDOT =     -13181
808272                 XDOT =       -3939
341577
 YDOT =     -17575
171150  feet/sec       YDOT =       -5401
402424  meter/sec
 ZDOT =     -12341
179419                 ZDOT =       -3780
920118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16429474
20                 X    =        -5007703
74
 Y    =       -6089122
19  feet           Y    =        -1855964
44  meter
 Z    =      -13475402
85                 Z    =        -4107302
79
 XDOT =      15382
465359                 XDOT =        4688
575441
 YDOT =     -13979
626029  feet/sec       YDOT =       -4260
990014  meter/sec
 ZDOT =     -12414
167718                 ZDOT =       -3783
838321


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   06363
52274407  
00020000  00000-0  20000-3 0  9075
2 25544  51
6356 260
4883 0023684  30
8502 329
4049 15
76568459 23989


Satellite: ISS
Catalog Number: 25544
Epoch time:      06363
52274407   =   yrday
fracday
Element set:     907
Inclination:       51
6356  deg
RA of node:       260
4883  deg
Eccentricity:     
0023684     
Arg of perigee:    30
8502  deg
Mean anomaly:     329
4049  deg
Mean motion:   15
76568459  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2398
Checksum:              316


Coasting Arc #9 (Orbit 2413)
---------------------------------------

Vector Time (GMT): 2006/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3519393
85                 A    =         6721980
35  meter
 Y    =        5133232
07  meter          E    =           
0031397
 Z    =        2541181
87                 I    =           51
33967
 XDOT =      -3057
800149                 Wp   =           59
09250
 YDOT =       4728
020642  meter/sec      RA   =          254
63032  deg
 ZDOT =      -5251
879842                 TA   =           91
95498
                                          MA   =           91
59538
                                          Ha   =            194
116  n
mi
                                          Hp   =            172
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11546567
76                 X    =         3449387
09
 Y    =       16841312
56  feet           Y    =         5172196
11  meter
 Z    =        8337210
84                 Z    =         2558109
84
 XDOT =     -10032
152719                 XDOT =       -3084
929467
 YDOT =      15511
878748  feet/sec       YDOT =        4693
675665  meter/sec
 ZDOT =     -17230
576909                 ZDOT =       -5266
799954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15062630
30                 X    =        -4591089
71
 Y    =       13747700
73  feet           Y    =         4190299
18  meter
 Z    =        8401191
20                 Z    =         2560683
08
 XDOT =     -15749
346755                 XDOT =       -4800
400891
 YDOT =      -6565
198398  feet/sec       YDOT =       -2001
072472  meter/sec
 ZDOT =     -17285
845143                 ZDOT =       -5268
725600


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   06364
53691700  
00020000  00000-0  20000-3 0  9087
2 25544  51
6351 255
2590 0023618  34
9164 325
3544 15
76586311 24148


Satellite: ISS
Catalog Number: 25544
Epoch time:      06364
53691700   =   yrday
fracday
Element set:     908
Inclination:       51
6351  deg
RA of node:       255
2590  deg
Eccentricity:     
0023618     
Arg of perigee:    34
9164  deg
Mean anomaly:     325
3544  deg
Mean motion:   15
76586311  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2414
Checksum:              287

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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