Date: January 5th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 2476)
---------------------------------------

Vector Time (GMT): 2007/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3433436
04                 A    =         6724446
52  meter
 Y    =        5740936
38  meter          E    =           
0025655
 Z    =        -752118
67                 I    =           51
39644
 XDOT =      -4478
400757                 Wp   =           74
10782
 YDOT =       1919
901198  meter/sec      RA   =          233
96771  deg
 ZDOT =      -5950
696174                 TA   =          114
11219
                                          MA   =          113
84364
                                          Ha   =            194
301  n
mi
                                          Hp   =            172
028

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11264553
92                 X    =         3372638
50
 Y    =       18835093
11  feet           Y    =         5778991
17  meter
 Z    =       -2467580
93                 Z    =         -735585
93
 XDOT =     -14692
915869                 XDOT =       -4470
629546
 YDOT =       6298
888445  feet/sec       YDOT =        1869
865743  meter/sec
 ZDOT =     -19523
281411                 ZDOT =       -5972
432710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16078211
79                 X    =        -4900638
95
 Y    =       14948146
89  feet           Y    =         4556195
17  meter
 Z    =       -2404968
53                 Z    =         -733034
41
 XDOT =      -8103
973281                 XDOT =       -2470
091056
 YDOT =     -11783
345246  feet/sec       YDOT =       -3591
563631  meter/sec
 ZDOT =     -19604
439941                 ZDOT =       -5975
433294


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   07003
53039150  
00020000  00000-0  20000-3 0  9005
2 25544  51
6339 234
6827 0023528  49
6103 310
7110 15
76633068 24772


Satellite: ISS
Catalog Number: 25544
Epoch time:      07003
53039150   =   yrday
fracday
Element set:     900
Inclination:       51
6339  deg
RA of node:       234
6827  deg
Eccentricity:     
0023528     
Arg of perigee:    49
6103  deg
Mean anomaly:     310
7110  deg
Mean motion:   15
76633068  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2477
Checksum:              269


Coasting Arc #2 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2007/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4364290
78                 A    =         6713452
43  meter
 Y    =       -1052219
70  meter          E    =           
0029087
 Z    =        4976362
36                 I    =           51
37770
 XDOT =       3719
308852                 Wp   =           53
47271
 YDOT =       6501
702570  meter/sec      RA   =          228
76995  deg
 ZDOT =      -1862
485466                 TA   =           54
65339
                                          MA   =           54
38186
                                          Ha   =            194
095  n
mi
                                          Hp   =            171
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14318539
29                 X    =         4351558
69
 Y    =       -3452164
38  feet           Y    =        -1003487
77  meter
 Z    =       16326648
15                 Z    =         4997532
58
 XDOT =      12202
456862                 XDOT =        3655
376912
 YDOT =      21331
045176  feet/sec       YDOT =        6542
936787  meter/sec
 ZDOT =      -6110
516620                 ZDOT =       -1844
571653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6561436
48                 X    =         1999925
84
 Y    =       13087959
34  feet           Y    =         3989210
01  meter
 Z    =       16405801
35                 Z    =         5000488
25
 XDOT =     -17081
120802                 XDOT =       -5206
325621
 YDOT =      16238
558168  feet/sec       YDOT =        4949
512530  meter/sec
 ZDOT =      -6042
622911                 ZDOT =       -1841
791463


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   07004
54449439  
00020000  00000-0  20000-3 0  9013
2 25544  51
6334 229
4525 0023546  52
9257 307
4055 15
76732286 24932


Satellite: ISS
Catalog Number: 25544
Epoch time:      07004
54449439   =   yrday
fracday
Element set:     901
Inclination:       51
6334  deg
RA of node:       229
4525  deg
Eccentricity:     
0023546     
Arg of perigee:    52
9257  deg
Mean anomaly:     307
4055  deg
Mean motion:   15
76732286  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2493
Checksum:              297


Coasting Arc #3 (Orbit 2508)
---------------------------------------

Vector Time (GMT): 2007/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2956209
05                 A    =         6721848
82  meter
 Y    =       -5500076
02  meter          E    =           
0037004
 Z    =        2433500
36                 I    =           51
42457
 XDOT =       5546
950188                 Wp   =           63
44954
 YDOT =       -597
795804  meter/sec      RA   =          223
63293  deg
 ZDOT =       5341
435815                 TA   =          324
22666
                                          MA   =          324
47398
                                          Ha   =            194
215  n
mi
                                          Hp   =            171
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9698848
60                 X    =        -2906307
96
 Y    =      -18044868
83  feet           Y    =        -5532855
31  meter
 Z    =        7983925
05                 Z    =         2419259
86
 XDOT =      18198
655471                 XDOT =        5527
275412
 YDOT =      -1961
272324  feet/sec       YDOT =        -535
877463  meter/sec
 ZDOT =      17524
395720                 ZDOT =        5368
334439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15158373
58                 X    =         4620272
27
 Y    =      -13811894
69  feet           Y    =        -4209865
50  meter
 Z    =        7929898
49                 Z    =         2417033
06
 XDOT =       5266
940429                 XDOT =        1605
363443
 YDOT =      15986
575528  feet/sec       YDOT =        4872
708221  meter/sec
 ZDOT =      17625
068806                 ZDOT =        5372
120972


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   07005
55857810  
00020000  00000-0  20000-3 0  9022
2 25544  51
6323 224
2225 0023501  56
7058 303
6354 15
76741962 25091


Satellite: ISS
Catalog Number: 25544
Epoch time:      07005
55857810   =   yrday
fracday
Element set:     902
Inclination:       51
6323  deg
RA of node:       224
2225  deg
Eccentricity:     
0023501     
Arg of perigee:    56
7058  deg
Mean anomaly:     303
6354  deg
Mean motion:   15
76741962  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2509
Checksum:              275


Coasting Arc #4 (Orbit 2523)
---------------------------------------

Vector Time (GMT): 2007/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5288829
31                 A    =         6716674
95  meter
 Y    =          38476
81  meter          E    =           
0029356
 Z    =       -4158399
17                 I    =           51
42840
 XDOT =      -2924
818454                 Wp   =           72
82307
 YDOT =      -6078
523895  meter/sec      RA   =          218
41300  deg
 ZDOT =       3693
615085                 TA   =          234
93979
                                          MA   =          235
21550
                                          Ha   =            194
156  n
mi
                                          Hp   =            171
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17351802
20                 X    =        -5268666
19
 Y    =         126236
25  feet           Y    =          -20552
62  meter
 Z    =      -13643041
90                 Z    =        -4184042
75
 XDOT =      -9595
861071                 XDOT =       -2874
572675
 YDOT =     -19942
663697  feet/sec       YDOT =       -6110
950315  meter/sec
 ZDOT =      12118
159728                 ZDOT =        3679
528001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4581295
56                 X    =        -1396378
89
 Y    =      -16657809
22  feet           Y    =        -5077300
25  meter
 Z    =      -13739093
51                 Z    =        -4187675
70
 XDOT =      15558
012124                 XDOT =        4742
082095
 YDOT =     -14149
054518  feet/sec       YDOT =       -4312
631817  meter/sec
 ZDOT =      12064
621549                 ZDOT =        3677
296648


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   07006
50926156  
00020000  00000-0  20000-3 0  9039
2 25544  51
6314 219
3185 0023468  60
3514 299
9983 15
76767959 25247


Satellite: ISS
Catalog Number: 25544
Epoch time:      07006
50926156   =   yrday
fracday
Element set:     903
Inclination:       51
6314  deg
RA of node:       219
3185  deg
Eccentricity:     
0023468     
Arg of perigee:    60
3514  deg
Mean anomaly:     299
9983  deg
Mean motion:   15
76767959  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2524
Checksum:              318


Coasting Arc #5 (Orbit 2539)
---------------------------------------

Vector Time (GMT): 2007/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2009599
67                 A    =         6717527
06  meter
 Y    =        5078762
67  meter          E    =           
0030176
 Z    =       -3943633
05                 I    =           51
45363
 XDOT =      -6545
704993                 Wp   =           66
39820
 YDOT =       -497
137905  meter/sec      RA   =          213
29268  deg
 ZDOT =      -3988
029840                 TA   =          162
06033
                                          MA   =          161
95360
                                          Ha   =            194
197  n
mi
                                          Hp   =            171
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6593174
77                 X    =         1971815
93
 Y    =       16662607
17  feet           Y    =         5101024
22  meter
 Z    =      -12938428
63                 Z    =        -3933961
94
 XDOT =     -21475
410081                 XDOT =       -6520
286717
 YDOT =      -1631
029873  feet/sec       YDOT =        -570
193145  meter/sec
 ZDOT =     -13084
087402                 ZDOT =       -4019
766517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14190822
11                 X    =        -4325362
58
 Y    =       10985716
26  feet           Y    =         3348446
32  meter
 Z    =      -12901549
24                 Z    =        -3932392
21
 XDOT =      -3509
993263                 XDOT =       -1069
845947
 YDOT =     -19992
340579  feet/sec       YDOT =       -6093
665408  meter/sec
 ZDOT =     -13203
040722                 ZDOT =       -4024
286812


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   07007
52330299  
00020000  00000-0  20000-3 0  9040
2 25544  51
6305 214
0879 0023449  64
2001 296
1579 15
76794011 25409


Satellite: ISS
Catalog Number: 25544
Epoch time:      07007
52330299   =   yrday
fracday
Element set:     904
Inclination:       51
6305  deg
RA of node:       214
0879  deg
Eccentricity:     
0023449     
Arg of perigee:    64
2001  deg
Mean anomaly:     296
1579  deg
Mean motion:   15
76794011  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2540
Checksum:              281


Coasting Arc #6 (Orbit 2555)
---------------------------------------

Vector Time (GMT): 2007/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6091284
98                 A    =         6720755
53  meter
 Y    =         814612
26  meter          E    =           
0035533
 Z    =        2699266
94                 I    =           51
49091
 XDOT =       1581
548773                 Wp   =           79
92402
 YDOT =       5502
078497  meter/sec      RA   =          208
07330  deg
 ZDOT =      -5165
873569                 TA   =           69
15092
                                          MA   =           68
77076
                                          Ha   =            194
014  n
mi
                                          Hp   =            171
108

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19984530
76                 X    =         6068610
84
 Y    =        2672612
40  feet           Y    =          882601
42  meter
 Z    =        8855862
67                 Z    =         2728802
86
 XDOT =       5188
808311                 XDOT =        1545
000640
 YDOT =      18051
438639  feet/sec       YDOT =        5519
560279  meter/sec
 ZDOT =     -16948
404097                 ZDOT =       -5158
278917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3248368
54                 X    =          990102
73
 Y    =       19849394
06  feet           Y    =         6050095
31  meter
 Z    =        8966620
75                 Z    =         2733026
00
 XDOT =     -14283
447813                 XDOT =       -4353
594893
 YDOT =      10073
556046  feet/sec       YDOT =        3070
419883  meter/sec
 ZDOT =     -16919
241527                 ZDOT =       -5156
984817


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   07008
53732122  
00020000  00000-0  20000-3 0  9054
2 25544  51
6313 208
8566 0023349  67
5112 292
8522 15
76876557 25564


Satellite: ISS
Catalog Number: 25544
Epoch time:      07008
53732122   =   yrday
fracday
Element set:     905
Inclination:       51
6313  deg
RA of node:       208
8566  deg
Eccentricity:     
0023349     
Arg of perigee:    67
5112  deg
Mean anomaly:     292
8522  deg
Mean motion:   15
76876557  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2556
Checksum:              300


Coasting Arc #7 (Orbit 2571)
---------------------------------------

Vector Time (GMT): 2007/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -674988
38                 A    =         6713619
43  meter
 Y    =       -4516480
62  meter          E    =           
0027887
 Z    =        4896319
41                 I    =           51
49093
 XDOT =       7317
124439                 Wp   =           82
27335
 YDOT =       1241
986766  meter/sec      RA   =          202
94545  deg
 ZDOT =       2147
681116                 TA   =          346
88294
                                          MA   =          346
95531
                                          Ha   =            194
226  n
mi
                                          Hp   =            171
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2214528
81                 X    =         -648219
39
 Y    =      -14817849
80  feet           Y    =        -4523879
36  meter
 Z    =       16064040
07                 Z    =         4893105
09
 XDOT =      24006
313775                 XDOT =        7292
259647
 YDOT =       4074
759731  feet/sec       YDOT =        1323
671759  meter/sec
 ZDOT =       7046
197886                 ZDOT =        2183
166888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13390828
51                 X    =         4081524
53
 Y    =       -6750118
68  feet           Y    =        -2057436
17  meter
 Z    =       16051411
26                 Z    =         4892470
15
 XDOT =       3003
149879                 XDOT =         915
360083
 YDOT =      23081
694774  feet/sec       YDOT =        7035
300567  meter/sec
 ZDOT =       7179
310677                 ZDOT =        2188
253895


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   07009
55132222  
00020000  00000-0  20000-3 0  9063
2 25544  51
6302 203
6257 0023452  71
7942 288
5772 15
76828159 25727


Satellite: ISS
Catalog Number: 25544
Epoch time:      07009
55132222   =   yrday
fracday
Element set:     906
Inclination:       51
6302  deg
RA of node:       203
6257  deg
Eccentricity:     
0023452     
Arg of perigee:    71
7942  deg
Mean anomaly:     288
5772  deg
Mean motion:   15
76828159  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2572
Checksum:              292


Coasting Arc #8 (Orbit 2586)
---------------------------------------

Vector Time (GMT): 2007/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6523325
11                 A    =         6723535
34  meter
 Y    =       -1286545
86  meter          E    =           
0031758
 Z    =        -961762
12                 I    =           51
55152
 XDOT =        117
779554                 Wp   =           65
12171
 YDOT =      -4911
404042  meter/sec      RA   =          197
75157  deg
 ZDOT =       5936
591411                 TA   =          284
34576
                                          MA   =          284
69812
                                          Ha   =            194
056  n
mi
                                          Hp   =            170
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21401985
26                 X    =        -6503781
93
 Y    =       -4220951
00  feet           Y    =        -1359383
98  meter
 Z    =       -3155387
54                 Z    =         -993404
72
 XDOT =        386
415859                 XDOT =         143
852227
 YDOT =     -16113
530323  feet/sec       YDOT =       -4909
941572  meter/sec
 ZDOT =      19477
005943                 ZDOT =        5937
226590

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2933732
97                 X    =         -894201
81
 Y    =      -21598408
57  feet           Y    =        -6583194
93  meter
 Z    =       -3274115
00                 Z    =         -997950
25
 XDOT =      13759
981448                 XDOT =        4194
042345
 YDOT =      -4742
507850  feet/sec       YDOT =       -1445
516393  meter/sec
 ZDOT =      19478
746916                 ZDOT =        5937
122060


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   07010
50192467  
00020000  00000-0  20000-3 0  9078
2 25544  51
6298 198
7215 0023344  75
6085 284
7668 15
76885742 25879


Satellite: ISS
Catalog Number: 25544
Epoch time:      07010
50192467   =   yrday
fracday
Element set:     907
Inclination:       51
6298  deg
RA of node:       198
7215  deg
Eccentricity:     
0023344     
Arg of perigee:    75
6085  deg
Mean anomaly:     284
7668  deg
Mean motion:   15
76885742  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2587
Checksum:              329


Coasting Arc #9 (Orbit 2602)
---------------------------------------

Vector Time (GMT): 2007/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -972476
27                 A    =         6711810
40  meter
 Y    =        4076354
69  meter          E    =           
0038339
 Z    =       -5275406
09                 I    =           51
53947
 XDOT =      -7482
223253                 Wp   =           84
08620
 YDOT =      -1717
656444  meter/sec      RA   =          192
59557  deg
 ZDOT =         56
258046                 TA   =          186
42534
                                          MA   =          186
47464
                                          Ha   =            194
091  n
mi
                                          Hp   =            170
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3190538
93                 X    =         -992359
58
 Y    =       13373867
09  feet           Y    =         4065369
13  meter
 Z    =      -17307762
76                 Z    =        -5280178
35
 XDOT =     -24547
976551                 XDOT =       -7462
733372
 YDOT =      -5635
355788  feet/sec       YDOT =       -1801
217860  meter/sec
 ZDOT =        184
573643                 ZDOT =          19
956877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13629063
03                 X    =        -4154138
41
 Y    =        1639376
39  feet           Y    =          499681
93  meter
 Z    =      -17325114
64                 Z    =        -5280694
94
 XDOT =      -2931
624635                 XDOT =        -893
559189
 YDOT =     -24007
802619  feet/sec       YDOT =       -7317
578238  meter/sec
 ZDOT =         48
325989                 ZDOT =          14
729761


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   07011
51588088  
00020000  00000-0  20000-3 0  9089
2 25544  51
6295 193
4901 0023429  79
6401 280
7403 15
76921554 26034


Satellite: ISS
Catalog Number: 25544
Epoch time:      07011
51588088   =   yrday
fracday
Element set:     908
Inclination:       51
6295  deg
RA of node:       193
4901  deg
Eccentricity:     
0023429     
Arg of perigee:    79
6401  deg
Mean anomaly:     280
7403  deg
Mean motion:   15
76921554  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2603
Checksum:              295


Coasting Arc #10 (Orbit 2618)
---------------------------------------

Vector Time (GMT): 2007/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6416966
43                 A    =         6723170
96  meter
 Y    =        1696755
00  meter          E    =           
0029639
 Z    =       -1074278
29                 I    =           51
60701
 XDOT =      -2140
804632                 Wp   =           99
56453
 YDOT =       4444
102341  meter/sec      RA   =          187
44263  deg
 ZDOT =      -5911
181822                 TA   =           92
19760
                                          MA   =           91
85819
                                          Ha   =            194
007  n
mi
                                          Hp   =            170
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21053039
48                 X    =         6402734
78
 Y    =        5566781
51  feet           Y    =         1768433
61  meter
 Z    =       -3524535
07                 Z    =        -1043139
24
 XDOT =      -7023
637244                 XDOT =       -2161
624794
 YDOT =      14580
388258  feet/sec       YDOT =        4420
046774  meter/sec
 ZDOT =     -19393
641149                 ZDOT =       -5921
631987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2306260
33                 X    =          702948
15
 Y    =       21672820
15  feet           Y    =         6605875
58  meter
 Z    =       -3407624
53                 Z    =        -1038643
96
 XDOT =     -14507
328701                 XDOT =       -4421
833788
 YDOT =      -1435
418105  feet/sec       YDOT =        -437
515438  meter/sec
 ZDOT =     -19432
225148                 ZDOT =       -5922
942225


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   07012
52981334  
00020000  00000-0  20000-3 0  9093
2 25544  51
6297 188
2586 0023436  82
8687 277
5142 15
77001233 26192


Satellite: ISS
Catalog Number: 25544
Epoch time:      07012
52981334   =   yrday
fracday
Element set:     909
Inclination:       51
6297  deg
RA of node:       188
2586  deg
Eccentricity:     
0023436     
Arg of perigee:    82
8687  deg
Mean anomaly:     277
5142  deg
Mean motion:   15
77001233  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2619
Checksum:              307


Coasting Arc #11 (Orbit 2634)
---------------------------------------

Vector Time (GMT): 2007/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2716478
04                 A    =         6713343
54  meter
 Y    =       -3737639
88  meter          E    =           
0029347
 Z    =        4847047
90                 I    =           51
60145
 XDOT =       7061
448995                 Wp   =           81
22222
 YDOT =       2112
057961  meter/sec      RA   =          182
25260  deg
 ZDOT =      -2312
631557                 TA   =           31
32254
                                          MA   =           31
14804
                                          Ha   =            193
974  n
mi
                                          Hp   =            170
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8912329
53                 X    =         2734524
99
 Y    =      -12262598
04  feet           Y    =        -3707162
32  meter
 Z    =       15902388
13                 Z    =         4860287
94
 XDOT =      23167
483579                 XDOT =        7048
541140
 YDOT =       6929
324018  feet/sec       YDOT =        2190
951083  meter/sec
 ZDOT =      -7587
373875                 ZDOT =       -2278
358312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14666337
52                 X    =         4470299
68
 Y    =        3624123
48  feet           Y    =         1104632
84  meter
 Z    =       15951524
98                 Z    =         4862024
81
 XDOT =       2473
985364                 XDOT =         754
070739
 YDOT =      23051
080485  feet/sec       YDOT =        7025
969332  meter/sec
 ZDOT =      -7458
653505                 ZDOT =       -2273
397588


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   07013
54372580  
00020000  00000-0  20000-3 0  9105
2 25544  51
6289 183
0271 0023408  87
3254 273
0590 15
76973364 26354


Satellite: ISS
Catalog Number: 25544
Epoch time:      07013
54372580   =   yrday
fracday
Element set:     910
Inclination:       51
6289  deg
RA of node:       183
0271  deg
Eccentricity:     
0023408     
Arg of perigee:    87
3254  deg
Mean anomaly:     273
0590  deg
Mean motion:   15
76973364  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2635
Checksum:              291


Coasting Arc #12 (Orbit 2650)
---------------------------------------

Vector Time (GMT): 2007/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5720664
13                 A    =         6720015
64  meter
 Y    =       -1991869
83  meter          E    =           
0036770
 Z    =        2876163
04                 I    =           51
65317
 XDOT =       4035
093211                 Wp   =           87
80288
 YDOT =      -4207
970881  meter/sec      RA   =          177
13540  deg
 ZDOT =       5057
709930                 TA   =          305
35162
                                          MA   =          305
69473
                                          Ha   =            193
982  n
mi
                                          Hp   =            170
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18768583
11                 X    =        -5711937
39
 Y    =       -6535006
02  feet           Y    =        -2055793
05  meter
 Z    =        9436230
45                 Z    =         2848393
15
 XDOT =      13238
494786                 XDOT =        4057
278136
 YDOT =     -13805
678744  feet/sec       YDOT =       -4162
724808  meter/sec
 ZDOT =      16593
536517                 ZDOT =        5077
365675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1283961
00                 X    =         -391351
31
 Y    =      -19881543
34  feet           Y    =        -6059894
41  meter
 Z    =        9331888
30                 Z    =         2844359
55
 XDOT =      16376
745274                 XDOT =        4991
631960
 YDOT =       6849
143115  feet/sec       YDOT =        2087
618822  meter/sec
 ZDOT =      16666
667197                 ZDOT =        5080
000162


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   07014
55761338  
00020000  00000-0  20000-3 0  9111
2 25544  51
6292 177
7959 0023404  91
2815 269
1031 15
77041188 26519


Satellite: ISS
Catalog Number: 25544
Epoch time:      07014
55761338   =   yrday
fracday
Element set:     911
Inclination:       51
6292  deg
RA of node:       177
7959  deg
Eccentricity:     
0023404     
Arg of perigee:    91
2815  deg
Mean anomaly:     269
1031  deg
Mean motion:   15
77041188  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2651
Checksum:              292

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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