Date: April 11th 2007

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) : 74 6 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


There are no maneuvers



Coasting Arc #1 (Orbit 7)
---------------------------------------

Vector Time (GMT): 2007/100/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2716836
55                 A    =         6714922
07  meter
 Y    =       -5321639
49  meter          E    =           
0018848
 Z    =       -3088843
35                 I    =           51
95668
 XDOT =       3598
317961                 Wp   =           62
43275
 YDOT =       4686
856929  meter/sec      RA   =           93
18434  deg
 ZDOT =      -4924
077421                 TA   =          153
23675
                                          MA   =          153
13937
                                          Ha   =            188
490  n
mi
                                          Hp   =            171
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8913505
74                 X    =         2791147
00
 Y    =      -17459447
13  feet           Y    =        -5290842
75  meter
 Z    =      -10134000
51                 Z    =        -3075464
56
 XDOT =      11805
505120                 XDOT =        3569
561680
 YDOT =      15376
827195  feet/sec       YDOT =        4726
934637  meter/sec
 ZDOT =     -16155
109650                 ZDOT =       -4906
666569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8179469
89                 X    =         2493102
42
 Y    =      -17843305
50  feet           Y    =        -5438639
52  meter
 Z    =      -10084322
80                 Z    =        -3073701
59
 XDOT =      11270
455951                 XDOT =        3435
234974
 YDOT =      14232
733819  feet/sec       YDOT =        4338
137268  meter/sec
 ZDOT =     -16088
942342                 ZDOT =       -4903
909626


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   07100
48378295  
00020000  00000-0  20000-3 0  9003
2 25544  51
6313  93
7753 0015867  51
2531 309
0049 15
78625473    80


Satellite: ISS
Catalog Number: 25544
Epoch time:      07100
48378295   =   yrday
fracday
Element set:     900
Inclination:       51
6313  deg
RA of node:        93
7753  deg
Eccentricity:     
0015867     
Arg of perigee:    51
2531  deg
Mean anomaly:     309
0049  deg
Mean motion:   15
78625473  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               8
Checksum:              285


Coasting Arc #2 (Orbit 23)
---------------------------------------

Vector Time (GMT): 2007/101/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2686604
13                 A    =         6714423
17  meter
 Y    =       -5251299
90  meter          E    =           
0027257
 Z    =        3195124
34                 I    =           51
95541
 XDOT =       3610
605912                 Wp   =           71
80892
 YDOT =      -4809
661138  meter/sec      RA   =           87
98511  deg
 ZDOT =      -4827
202574                 TA   =           70
97781
                                          MA   =           70
68272
                                          Ha   =            188
475  n
mi
                                          Hp   =            171
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8814318
01                 X    =        -2643204
95
 Y    =      -17228674
21  feet           Y    =        -5281100
37  meter
 Z    =       10482691
42                 Z    =         3182178
25
 XDOT =      11845
819921                 XDOT =        3687
569487
 YDOT =     -15779
728142  feet/sec       YDOT =       -4768
854967  meter/sec
 ZDOT =     -15837
278786                 ZDOT =       -4809
475396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9922574
02                 X    =        -3024400
56
 Y    =      -16646196
60  feet           Y    =        -5073760
72  meter
 Z    =       10433259
32                 Z    =         3180057
44
 XDOT =       9719
867968                 XDOT =        2962
615757
 YDOT =     -15764
822077  feet/sec       YDOT =       -4805
117769  meter/sec
 ZDOT =     -15771
155320                 ZDOT =       -4807
048142


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   07101
49661897  
00020000  00000-0  20000-3 0  9019
2 25544  51
6308  88
5366 0015926  54
5189 305
7460 15
78698947   241


Satellite: ISS
Catalog Number: 25544
Epoch time:      07101
49661897   =   yrday
fracday
Element set:     901
Inclination:       51
6308  deg
RA of node:        88
5366  deg
Eccentricity:     
0015926     
Arg of perigee:    54
5189  deg
Mean anomaly:     305
7460  deg
Mean motion:   15
78698947  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              24
Checksum:              322


Coasting Arc #3 (Orbit 39)
---------------------------------------

Vector Time (GMT): 2007/102/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3550017
00                 A    =         6708190
35  meter
 Y    =        2796095
88  meter          E    =           
0019272
 Z    =        4940301
76                 I    =           51
93141
 XDOT =      -2544
308417                 Wp   =           75
18042
 YDOT =      -6977
491446  meter/sec      RA   =           82
87735  deg
 ZDOT =       2118
841462                 TA   =          354
41469
                                          MA   =          354
43615
                                          Ha   =            188
592  n
mi
                                          Hp   =            171
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11647037
40                 X    =        -3605018
49
 Y    =        9173542
90  feet           Y    =         2756090
13  meter
 Z    =       16208339
12                 Z    =         4922922
23
 XDOT =      -8347
468561                 XDOT =       -2476
388905
 YDOT =     -22892
032304  feet/sec       YDOT =       -7005
563545  meter/sec
 ZDOT =       6951
579600                 ZDOT =        2106
646329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10974886
86                 X    =        -3345145
51
 Y    =       10072968
38  feet           Y    =         3070240
76  meter
 Z    =       16143258
45                 Z    =         4920465
17
 XDOT =      -9435
833723                 XDOT =       -2876
042119
 YDOT =     -21356
817832  feet/sec       YDOT =       -6509
558075  meter/sec
 ZDOT =       6904
748589                 ZDOT =        2104
567370


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   07102
50943406  
00020000  00000-0  20000-3 0  9022
2 25544  51
6301  83
2980 0015857  58
4994 301
7718 15
78699275   403


Satellite: ISS
Catalog Number: 25544
Epoch time:      07102
50943406   =   yrday
fracday
Element set:     902
Inclination:       51
6301  deg
RA of node:        83
2980  deg
Eccentricity:     
0015857     
Arg of perigee:    58
4994  deg
Mean anomaly:     301
7718  deg
Mean motion:   15
78699275  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              40
Checksum:              297


Coasting Arc #4 (Orbit 54)
---------------------------------------

Vector Time (GMT): 2007/103/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1668530
34                 A    =         6718564
95  meter
 Y    =        6490242
01  meter          E    =           
0027064
 Z    =        -317661
79                 I    =           51
96231
 XDOT =      -4541
285309                 Wp   =           54
24301
 YDOT =       1446
131678  meter/sec      RA   =           77
70778  deg
 ZDOT =       6065
161838                 TA   =          302
31035
                                          MA   =          302
57218
                                          Ha   =            188
390  n
mi
                                          Hp   =            171
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5474180
90                 X    =         1597374
64
 Y    =       21293444
93  feet           Y    =         6508502
59  meter
 Z    =       -1042197
46                 Z    =         -309729
15
 XDOT =     -14899
230018                 XDOT =       -4586
582001
 YDOT =       4744
526501  feet/sec       YDOT =        1395
095423  meter/sec
 ZDOT =      19898
824928                 ZDOT =        6042
990280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7503471
69                 X    =         2287058
17
 Y    =       20667328
06  feet           Y    =         6299401
59  meter
 Z    =       -1011480
44                 Z    =         -308299
24
 XDOT =     -12976
628450                 XDOT =       -3955
276352
 YDOT =       5619
521990  feet/sec       YDOT =        1712
830302  meter/sec
 ZDOT =      19815
520829                 ZDOT =        6039
770749


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   07103
45892634  
00020000  00000-0  20000-3 0  9034
2 25544  51
6301  78
3875 0015832  62
9218 297
3561 15
78781022   557


Satellite: ISS
Catalog Number: 25544
Epoch time:      07103
45892634   =   yrday
fracday
Element set:     903
Inclination:       51
6301  deg
RA of node:        78
3875  deg
Eccentricity:     
0015832     
Arg of perigee:    62
9218  deg
Mean anomaly:     297
3561  deg
Mean motion:   15
78781022  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              55
Checksum:              293


Coasting Arc #5 (Orbit 70)
---------------------------------------

Vector Time (GMT): 2007/104/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4328014
85                 A    =         6707339
54  meter
 Y    =         348215
29  meter          E    =           
0028351
 Z    =       -5135414
69                 I    =           51
91633
 XDOT =       1135
304331                 Wp   =           82
21873
 YDOT =       7460
301852  meter/sec      RA   =           72
54655  deg
 ZDOT =       1473
301653                 TA   =          201
81084
                                          MA   =          201
93178
                                          Ha   =            188
460  n
mi
                                          Hp   =            171
121

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14199523
77                 X    =         4348746
30
 Y    =        1142438
63  feet           Y    =          396729
22  meter
 Z    =      -16848473
38                 Z    =        -5114338
85
 XDOT =       3724
751741                 XDOT =        1044
640746
 YDOT =      24476
055944  feet/sec       YDOT =        7472
490615  meter/sec
 ZDOT =       4833
666839                 ZDOT =        1478
596333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14330609
21                 X    =         4367969
69
 Y    =        -484674
84  feet           Y    =         -147728
89  meter
 Z    =      -16769061
59                 Z    =        -5111209
97
 XDOT =       6412
547694                 XDOT =        1954
544537
 YDOT =      22854
226327  feet/sec       YDOT =        6965
968185  meter/sec
 ZDOT =       4854
574634                 ZDOT =        1479
674348


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   07104
47169595  
00020000  00000-0  20000-3 0  9041
2 25544  51
6299  73
1475 0015819  65
8028 294
4789 15
78745522   711


Satellite: ISS
Catalog Number: 25544
Epoch time:      07104
47169595   =   yrday
fracday
Element set:     904
Inclination:       51
6299  deg
RA of node:        73
1475  deg
Eccentricity:     
0015819     
Arg of perigee:    65
8028  deg
Mean anomaly:     294
4789  deg
Mean motion:   15
78745522  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              71
Checksum:              324


Coasting Arc #6 (Orbit 86)
---------------------------------------

Vector Time (GMT): 2007/105/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -174437
91                 A    =         6715100
99  meter
 Y    =       -6114513
81  meter          E    =           
0019237
 Z    =       -2791072
37                 I    =           51
93380
 XDOT =       5279
390250                 Wp   =           80
15942
 YDOT =       2188
964906  meter/sec      RA   =           67
42922  deg
 ZDOT =      -5152
081593                 TA   =          131
66110
                                          MA   =          131
49625
                                          Ha   =            188
396  n
mi
                                          Hp   =            170
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -572302
86                 X    =          -92492
96
 Y    =      -20060740
85  feet           Y    =        -6116006
48  meter
 Z    =       -9157061
58                 Z    =        -2791720
36
 XDOT =      17320
834155                 XDOT =        5279
548583
 YDOT =       7181
643394  feet/sec       YDOT =        2248
002561  meter/sec
 ZDOT =     -16903
154832                 ZDOT =       -5126
433922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3132868
89                 X    =         -954898
44
 Y    =      -19821372
52  feet           Y    =        -6041554
35  meter
 Z    =       -9160292
28                 Z    =        -2792057
09
 XDOT =      16757
223685                 XDOT =        5107
601779
 YDOT =       5077
900781  feet/sec       YDOT =        1547
744158  meter/sec
 ZDOT =     -16806
289906                 ZDOT =       -5122
557163


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   07105
48444192  
00020000  00000-0  20000-3 0  9053
2 25544  51
6303  67
9073 0015883  69
5706 290
7164 15
78814524   879


Satellite: ISS
Catalog Number: 25544
Epoch time:      07105
48444192   =   yrday
fracday
Element set:     905
Inclination:       51
6303  deg
RA of node:        67
9073  deg
Eccentricity:     
0015883     
Arg of perigee:    69
5706  deg
Mean anomaly:     290
7164  deg
Mean motion:   15
78814524  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              87
Checksum:              304


Coasting Arc #7 (Orbit 102)
---------------------------------------

Vector Time (GMT): 2007/106/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4751472
01                 A    =         6713338
90  meter
 Y    =       -3258511
88  meter          E    =           
0027962
 Z    =        3427232
97                 I    =           51
91579
 XDOT =        853
524206                 Wp   =           80
06163
 YDOT =      -6129
973476  meter/sec      RA   =           62
22736  deg
 ZDOT =      -4608
594115                 TA   =           59
43290
                                          MA   =           59
15730
                                          Ha   =            188
375  n
mi
                                          Hp   =            170
789

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15588818
92                 X    =        -4731330
80
 Y    =      -10690655
79  feet           Y    =        -3311532
70  meter
 Z    =       11244202
66                 Z    =         3404199
14
 XDOT =       2800
276268                 XDOT =         944
395020
 YDOT =     -20111
461535  feet/sec       YDOT =       -6119
921069  meter/sec
 ZDOT =     -15120
059431                 ZDOT =       -4604
226564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17056461
98                 X    =        -5198809
61
 Y    =       -8266249
37  feet           Y    =        -2519552
81  meter
 Z    =       11157047
82                 Z    =         3400668
18
 XDOT =       -715
075711                 XDOT =        -217
955077
 YDOT =     -19073
043197  feet/sec       YDOT =       -5813
463567  meter/sec
 ZDOT =     -15104
398147                 ZDOT =       -4603
820555


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   07106
49716386  
00020000  00000-0  20000-3 0  9063
2 25544  51
6303  62
6681 0015730  73
0458 287
2430 15
78854788  1033


Satellite: ISS
Catalog Number: 25544
Epoch time:      07106
49716386   =   yrday
fracday
Element set:     906
Inclination:       51
6303  deg
RA of node:        62
6681  deg
Eccentricity:     
0015730     
Arg of perigee:    73
0458  deg
Mean anomaly:     287
2430  deg
Mean motion:   15
78854788  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             103
Checksum:              298


Coasting Arc #8 (Orbit 118)
---------------------------------------

Vector Time (GMT): 2007/107/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1766273
08                 A    =         6707948
51  meter
 Y    =        4269404
74  meter          E    =           
0020942
 Z    =        4845172
94                 I    =           51
88475
 XDOT =      -5425
893987                 Wp   =           89
93424
 YDOT =      -4954
817030  meter/sec      RA   =           57
11846  deg
 ZDOT =       2379
321036                 TA   =          336
96758
                                          MA   =          337
06133
                                          Ha   =            188
248  n
mi
                                          Hp   =            170
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5794859
20                 X    =        -1837420
31
 Y    =       14007233
41  feet           Y    =         4249255
64  meter
 Z    =       15896236
68                 Z    =         4836419
28
 XDOT =     -17801
489460                 XDOT =       -5381
643759
 YDOT =     -16255
961383  feet/sec       YDOT =       -5015
244923  meter/sec
 ZDOT =       7806
171378                 ZDOT =        2353
069222

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3500037
28                 X    =        -1066811
36
 Y    =       14783858
61  feet           Y    =         4506120
11  meter
 Z    =       15863813
70                 Z    =         4835290
42
 XDOT =     -19196
812094                 XDOT =       -5851
188326
 YDOT =     -12845
241376  feet/sec       YDOT =       -3915
229572  meter/sec
 ZDOT =       7706
690471                 ZDOT =        2348
999255


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   07107
50986151  
00020000  00000-0  20000-3 0  9076
2 25544  51
6313  57
4296 0015555  77
1309 283
1593 15
78914003  1192


Satellite: ISS
Catalog Number: 25544
Epoch time:      07107
50986151   =   yrday
fracday
Element set:     907
Inclination:       51
6313  deg
RA of node:        57
4296  deg
Eccentricity:     
0015555     
Arg of perigee:    77
1309  deg
Mean anomaly:     283
1593  deg
Mean motion:   15
78914003  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             119
Checksum:              290


Coasting Arc #9 (Orbit 133)
---------------------------------------

Vector Time (GMT): 2007/108/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4427653
22                 A    =         6718090
97  meter
 Y    =        5019889
32  meter          E    =           
0025406
 Z    =        -499277
57                 I    =           51
90250
 XDOT =      -3291
428603                 Wp   =           64
26892
 YDOT =       3479
443289  meter/sec      RA   =           51
93966  deg
 ZDOT =       6041
340577                 TA   =          290
30733
                                          MA   =          290
58019
                                          Ha   =            188
237  n
mi
                                          Hp   =            170
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14526421
33                 X    =         4373616
47
 Y    =       16469453
15  feet           Y    =         5069099
68  meter
 Z    =       -1638049
76                 Z    =         -477898
85
 XDOT =     -10798
650272                 XDOT =       -3359
439934
 YDOT =      11415
496354  feet/sec       YDOT =        3442
256404  meter/sec
 ZDOT =      19820
671185                 ZDOT =        6025
185308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17281422
00                 X    =         5267377
43
 Y    =       13559921
30  feet           Y    =         4133064
01  meter
 Z    =       -1556919
68                 Z    =         -474549
12
 XDOT =      -7668
733203                 XDOT =       -2337
429880
 YDOT =      11944
446897  feet/sec       YDOT =        3640
667414  meter/sec
 ZDOT =      19760
269203                 ZDOT =        6022
930053


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   07108
45924566  
00020000  00000-0  20000-3 0  9084
2 25544  51
6315  52
5177 0015692  80
9310 279
3630 15
78926518  1344


Satellite: ISS
Catalog Number: 25544
Epoch time:      07108
45924566   =   yrday
fracday
Element set:     908
Inclination:       51
6315  deg
RA of node:        52
5177  deg
Eccentricity:     
0015692     
Arg of perigee:    80
9310  deg
Mean anomaly:     279
3630  deg
Mean motion:   15
78926518  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             134
Checksum:              300


Coasting Arc #10 (Orbit 149)
---------------------------------------

Vector Time (GMT): 2007/109/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3972062
40                 A    =         6706673
67  meter
 Y    =       -1690530
73  meter          E    =           
0029380
 Z    =       -5157908
35                 I    =           51
84625
 XDOT =       4365
670053                 Wp   =           91
70735
 YDOT =       6183
394649  meter/sec      RA   =           46
77612  deg
 ZDOT =       1341
002183                 TA   =          191
07756
                                          MA   =          191
14239
                                          Ha   =            188
150  n
mi
                                          Hp   =            170
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13031700
78                 X    =         4015727
58
 Y    =       -5546360
66  feet           Y    =        -1645868
57  meter
 Z    =      -16922271
48                 Z    =        -5138505
72
 XDOT =      14323
064479                 XDOT =        4289
687509
 YDOT =      20286
727852  feet/sec       YDOT =        6231
789126  meter/sec
 ZDOT =       4399
613460                 ZDOT =        1362
026656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11765623
72                 X    =         3586162
11
 Y    =       -8038532
85  feet           Y    =        -2450144
81  meter
 Z    =      -16849412
51                 Z    =        -5135700
93
 XDOT =      17450
459360                 XDOT =        5318
900013
 YDOT =      16191
126555  feet/sec       YDOT =        4935
055374  meter/sec
 ZDOT =       4479
545386                 ZDOT =        1365
365434


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   07109
47189770  
00020000  00000-0  20000-3 0  9098
2 25544  51
6326  47
2780 0015560  84
3913 275
9027 15
78944133  1501


Satellite: ISS
Catalog Number: 25544
Epoch time:      07109
47189770   =   yrday
fracday
Element set:     909
Inclination:       51
6326  deg
RA of node:        47
2780  deg
Eccentricity:     
0015560     
Arg of perigee:    84
3913  deg
Mean anomaly:     275
9027  deg
Mean motion:   15
78944133  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             150
Checksum:              301


Coasting Arc #11 (Orbit 165)
---------------------------------------

Vector Time (GMT): 2007/110/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2863880
59                 A    =         6714657
53  meter
 Y    =       -5427267
53  meter          E    =           
0019698
 Z    =       -2739854
25                 I    =           51
85400
 XDOT =       5678
358398                 Wp   =           95
36601
 YDOT =       -396
921309  meter/sec      RA   =           41
65206  deg
 ZDOT =      -5182
656067                 TA   =          115
85912
                                          MA   =          115
65587
                                          Ha   =            188
046  n
mi
                                          Hp   =            170
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9395933
68                 X    =        -2789669
35
 Y    =      -17805995
83  feet           Y    =        -5458877
94  meter
 Z    =       -8989023
14                 Z    =        -2753587
25
 XDOT =      18629
784769                 XDOT =        5707
551546
 YDOT =      -1302
235267  feet/sec       YDOT =        -333
259179  meter/sec
 ZDOT =     -17003
464787                 ZDOT =       -5154
999340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12956919
63                 X    =        -3949269
10
 Y    =      -15378912
35  feet           Y    =        -4687492
48  meter
 Z    =       -9041398
28                 Z    =        -2755818
20
 XDOT =      16884
470926                 XDOT =        5146
386738
 YDOT =      -4354
327550  feet/sec       YDOT =       -1327
199037  meter/sec
 ZDOT =     -16899
357619                 ZDOT =       -5150
924202


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   07110
48452557  
00020000  00000-0  20000-3 0  9109
2 25544  51
6333  42
0383 0015538  88
1665 272
1280 15
79000960  1661


Satellite: ISS
Catalog Number: 25544
Epoch time:      07110
48452557   =   yrday
fracday
Element set:     910
Inclination:       51
6333  deg
RA of node:        42
0383  deg
Eccentricity:     
0015538     
Arg of perigee:    88
1665  deg
Mean anomaly:     272
1280  deg
Mean motion:   15
79000960  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             166
Checksum:              272


Coasting Arc #12 (Orbit 181)
---------------------------------------

Vector Time (GMT): 2007/111/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480296
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5696287
85                 A    =         6712838
34  meter
 Y    =        -862872
66  meter          E    =           
0028011
 Z    =        3421097
42                 I    =           51
82581
 XDOT =      -1892
083018                 Wp   =           90
55068
 YDOT =      -5899
096192  meter/sec      RA   =           36
44362  deg
 ZDOT =      -4606
402759                 TA   =           48
94717
                                          MA   =           48
70544
                                          Ha   =            188
063  n
mi
                                          Hp   =            170
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18688608
43                 X    =        -5702834
93
 Y    =       -2830947
05  feet           Y    =         -926608
59  meter
 Z    =       11224072
89                 Z    =         3393408
66
 XDOT =      -6207
621449                 XDOT =       -1803
600595
 YDOT =     -19353
990130  feet/sec       YDOT =       -5919
759462  meter/sec
 ZDOT =     -15112
869944                 ZDOT =       -4615
380072

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18896312
03                 X    =        -5759595
91
 Y    =        1593772
00  feet           Y    =          485781
71  meter
 Z    =       11119687
10                 Z    =         3389280
63
 XDOT =     -10327
642343                 XDOT =       -3147
865386
 YDOT =     -16028
745380  feet/sec       YDOT =       -4885
561592  meter/sec
 ZDOT =     -15147
387793                 ZDOT =       -4616
923799


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   07111
49712939  
00020000  00000-0  20000-3 0  9115
2 25544  51
6336  36
7991 0015470  92
0014 268
2923 15
79041493  1820


Satellite: ISS
Catalog Number: 25544
Epoch time:      07111
49712939   =   yrday
fracday
Element set:     911
Inclination:       51
6336  deg
RA of node:        36
7991  deg
Eccentricity:     
0015470     
Arg of perigee:    92
0014  deg
Mean anomaly:     268
2923  deg
Mean motion:   15
79041493  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             182
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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