Date: September 12th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5651 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2423)
---------------------------------------

Vector Time (GMT): 2007/253/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6016489
02                 A    =         6720723
69  meter
 Y    =         -16119
77  meter          E    =           
0013569
 Z    =        2993875
01                 I    =           51
76790
 XDOT =      -2474
530098                 Wp   =           58
38210
 YDOT =      -5330
383062  meter/sec      RA   =           23
23451  deg
 ZDOT =      -4978
087770                 TA   =           87
06629
                                          MA   =           86
91101
                                          Ha   =            187
564  n
mi
                                          Hp   =            179
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19739137
19                 X    =        -6030405
17
 Y    =         -52886
39  feet           Y    =          -83477
18  meter
 Z    =        9822424
57                 Z    =         2964613
39
 XDOT =      -8118
537066                 XDOT =       -2390
558631
 YDOT =     -17488
133406  feet/sec       YDOT =       -5357
585450  meter/sec
 ZDOT =     -16332
308957                 ZDOT =       -4989
904630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18685226
81                 X    =         5695257
13
 Y    =        6532119
01  feet           Y    =         1990989
88  meter
 Z    =        9711337
63                 Z    =         2960015
71
 XDOT =       2333
437775                 XDOT =         711
231834
 YDOT =      17789
700804  feet/sec       YDOT =        5422
300805  meter/sec
 ZDOT =     -16377
798245                 ZDOT =       -4991
952905


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   07253
51691485  
00020000  00000-0  20000-3 0  9005
2 25544  51
6343  23
5691 0008856 349
5619  10
5360 15
76688168 24247


Satellite: ISS
Catalog Number: 25544
Epoch time:      07253
51691485   =   yrday
fracday
Element set:     900
Inclination:       51
6343  deg
RA of node:        23
5691  deg
Eccentricity:     
0008856     
Arg of perigee:   349
5619  deg
Mean anomaly:      10
5360  deg
Mean motion:   15
76688168  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2424
Checksum:              304


Coasting Arc #2 (Orbit 2439)
---------------------------------------

Vector Time (GMT): 2007/254/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1481310
51                 A    =         6714257
40  meter
 Y    =        4460958
39  meter          E    =           
0007252
 Z    =        4788145
28                 I    =           51
72133
 XDOT =      -7279
756814                 Wp   =           43
08348
 YDOT =       -288
099689  meter/sec      RA   =           18
12967  deg
 ZDOT =       2523
524514                 TA   =           22
29079
                                          MA   =           22
25928
                                          Ha   =            187
547  n
mi
                                          Hp   =            179
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4859942
62                 X    =         1408057
49
 Y    =       14635690
24  feet           Y    =         4477114
01  meter
 Z    =       15709138
05                 Z    =         4795163
19
 XDOT =     -23883
716582                 XDOT =       -7288
252957
 YDOT =       -945
208952  feet/sec       YDOT =        -369
553364  meter/sec
 ZDOT =       8279
279900                 ZDOT =        2488
139027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          19549
33                 X    =            5958
64
 Y    =      -15393757
21  feet           Y    =        -4692017
20  meter
 Z    =       15736306
63                 Z    =         4796426
26
 XDOT =      21325
134605                 XDOT =        6499
901028
 YDOT =       8343
300687  feet/sec       YDOT =        2543
038050  meter/sec
 ZDOT =       8144
917957                 ZDOT =        2482
570993


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   07254
53099360  
00020000  00000-0  20000-3 0  9013
2 25544  51
6357  18
3397 0008960 352
7432   7
3601 15
76766136 24404


Satellite: ISS
Catalog Number: 25544
Epoch time:      07254
53099360   =   yrday
fracday
Element set:     901
Inclination:       51
6357  deg
RA of node:        18
3397  deg
Eccentricity:     
0008960     
Arg of perigee:   352
7432  deg
Mean anomaly:       7
3601  deg
Mean motion:   15
76766136  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2440
Checksum:              289


Coasting Arc #3 (Orbit 2454)
---------------------------------------

Vector Time (GMT): 2007/255/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6566009
40                 A    =         6723613
11  meter
 Y    =         429752
44  meter          E    =           
0016981
 Z    =       -1333700
12                 I    =           51
72554
 XDOT =        859
533538                 Wp   =           16
72301
 YDOT =       4940
079468  meter/sec      RA   =           12
94738  deg
 ZDOT =       5857
708249                 TA   =          328
61959
                                          MA   =          328
72080
                                          Ha   =            187
809  n
mi
                                          Hp   =            178
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21542025
58                 X    =         6567194
71
 Y    =        1409948
96  feet           Y    =          503183
80  meter
 Z    =       -4375656
56                 Z    =        -1301799
61
 XDOT =       2819
991924                 XDOT =         775
773265
 YDOT =      16207
609803  feet/sec       YDOT =        4949
223381  meter/sec
 ZDOT =      19218
202917                 ZDOT =        5861
680028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20192330
74                 X    =        -6154622
41
 Y    =       -7704679
90  feet           Y    =        -2348386
43  meter
 Z    =       -4254512
79                 Z    =        -1296775
50
 XDOT =       1624
403586                 XDOT =         495
118213
 YDOT =     -14814
268759  feet/sec       YDOT =       -4515
389118  meter/sec
 ZDOT =      19233
863754                 ZDOT =        5862
481672


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   07255
48167654  
00020000  00000-0  20000-3 0  9021
2 25544  51
6365  13
4378 0009095 357
2379   2
8734 15
76755223 24556


Satellite: ISS
Catalog Number: 25544
Epoch time:      07255
48167654   =   yrday
fracday
Element set:     902
Inclination:       51
6365  deg
RA of node:        13
4378  deg
Eccentricity:     
0009095     
Arg of perigee:   357
2379  deg
Mean anomaly:       2
8734  deg
Mean motion:   15
76755223  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2455
Checksum:              309


Coasting Arc #4 (Orbit 2470)
---------------------------------------

Vector Time (GMT): 2007/256/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          53978
90                 A    =         6712169
18  meter
 Y    =       -4189622
61  meter          E    =           
0018148
 Z    =       -5257343
24                 I    =           51
65922
 XDOT =       7649
847113                 Wp   =           56
04630
 YDOT =        684
062603  meter/sec      RA   =            7
81184  deg
 ZDOT =       -457
771507                 TA   =          209
55188
                                          MA   =          209
65457
                                          Ha   =            187
810  n
mi
                                          Hp   =            178
553

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         177096
13                 X    =          126363
22
 Y    =      -13745480
99  feet           Y    =        -4188614
65  meter
 Z    =      -17248501
46                 Z    =        -5256904
88
 XDOT =      25097
923600                 XDOT =        7643
853051
 YDOT =       2244
299879  feet/sec       YDOT =         769
573969  meter/sec
 ZDOT =      -1501
875023                 ZDOT =        -420
622994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4088557
69                 X    =        -1246192
38
 Y    =       13126067
79  feet           Y    =         4000825
46  meter
 Z    =      -17247331
78                 Z    =        -5256986
73
 XDOT =     -22532
362100                 XDOT =       -6867
863968
 YDOT =      -8844
533213  feet/sec       YDOT =       -2695
813723  meter/sec
 ZDOT =      -1360
786576                 ZDOT =        -414
767748


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   07256
49571733  
00020000  00000-0  20000-3 0  9031
2 25544  51
6367   8
2093 0009178   1
0975 359
0208 15
76808956 24715


Satellite: ISS
Catalog Number: 25544
Epoch time:      07256
49571733   =   yrday
fracday
Element set:     903
Inclination:       51
6367  deg
RA of node:         8
2093  deg
Eccentricity:     
0009178     
Arg of perigee:     1
0975  deg
Mean anomaly:     359
0208  deg
Mean motion:   15
76808956  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2471
Checksum:              308


Coasting Arc #5 (Orbit 2486)
---------------------------------------

Vector Time (GMT): 2007/257/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6658473
31                 A    =         6723950
39  meter
 Y    =        -756547
73  meter          E    =           
0007903
 Z    =        -565329
55                 I    =           51
67059
 XDOT =       1038
290584                 Wp   =           83
40157
 YDOT =      -4704
008285  meter/sec      RA   =            2
65809  deg
 ZDOT =      -6004
529558                 TA   =          102
75005
                                          MA   =          102
66170
                                          Ha   =            187
889  n
mi
                                          Hp   =            178
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21845384
88                 X    =        -6646772
31
 Y    =       -2482111
98  feet           Y    =         -830941
16  meter
 Z    =       -1854755
73                 Z    =         -597648
21
 XDOT =       3406
465172                 XDOT =        1119
983509
 YDOT =     -15433
098049  feet/sec       YDOT =       -4691
941155  meter/sec
 ZDOT =     -19699
900126                 ZDOT =       -5999
286761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20423774
22                 X    =         6225166
38
 Y    =        8110531
57  feet           Y    =         2472090
02  meter
 Z    =       -1977514
46                 Z    =         -602746
41
 XDOT =      -6842
485643                 XDOT =       -2085
589624
 YDOT =      12485
056049  feet/sec       YDOT =        3805
445084  meter/sec
 ZDOT =     -19680
552952                 ZDOT =       -5998
632540


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   07257
50973767  
00020000  00000-0  20000-3 0  9048
2 25544  51
6369   2
9791 0009197   4
9382 355
1872 15
76837428 24875


Satellite: ISS
Catalog Number: 25544
Epoch time:      07257
50973767   =   yrday
fracday
Element set:     904
Inclination:       51
6369  deg
RA of node:         2
9791  deg
Eccentricity:     
0009197     
Arg of perigee:     4
9382  deg
Mean anomaly:     355
1872  deg
Mean motion:   15
76837428  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2487
Checksum:              335


Coasting Arc #6 (Orbit 2502)
---------------------------------------

Vector Time (GMT): 2007/258/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1748773
80                 A    =         6712975
58  meter
 Y    =        4073904
44  meter          E    =           
0013648
 Z    =        5038998
91                 I    =           51
60533
 XDOT =      -7438
943408                 Wp   =           24
83871
 YDOT =      -1041
557819  meter/sec      RA   =          357
48071  deg
 ZDOT =      -1725
730512                 TA   =           81
83891
                                          MA   =           81
68413
                                          Ha   =            188
060  n
mi
                                          Hp   =            178
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5737446
84                 X    =        -1818677
65
 Y    =       13365828
23  feet           Y    =         4053958
07  meter
 Z    =       16532148
64                 Z    =         5030333
26
 XDOT =     -24405
982309                 XDOT =       -7418
360291
 YDOT =      -3417
184445  feet/sec       YDOT =       -1124
629290  meter/sec
 ZDOT =      -5661
845511                 ZDOT =       -1761
819249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8928347
96                 X    =         2721360
46
 Y    =      -11529049
30  feet           Y    =        -3514054
23  meter
 Z    =       16499734
06                 Z    =         5029118
94
 XDOT =      21952
086367                 XDOT =        6690
995925
 YDOT =       8635
819953  feet/sec       YDOT =        2632
197922  meter/sec
 ZDOT =      -5798
942997                 ZDOT =       -1767
517825


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   07258
52373747  
00020000  00000-0  20000-3 0  9054
2 25544  51
6375 357
7496 0009365   9
0287 351
1044 15
76869412 25036


Satellite: ISS
Catalog Number: 25544
Epoch time:      07258
52373747   =   yrday
fracday
Element set:     905
Inclination:       51
6375  deg
RA of node:       357
7496  deg
Eccentricity:     
0009365     
Arg of perigee:     9
0287  deg
Mean anomaly:     351
1044  deg
Mean motion:   15
76869412  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2503
Checksum:              312


Coasting Arc #7 (Orbit 2518)
---------------------------------------

Vector Time (GMT): 2007/259/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6173382
76                 A    =         6721366
49  meter
 Y    =        1084280
50  meter          E    =           
0020138
 Z    =        2392272
41                 I    =           51
60534
 XDOT =      -2917
003014                 Wp   =           49
99017
 YDOT =       4695
022785  meter/sec      RA   =          352
35681  deg
 ZDOT =       5382
548896                 TA   =          337
07273
                                          MA   =          337
16251
                                          Ha   =            187
995  n
mi
                                          Hp   =            177
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20253880
43                 X    =         6149177
98
 Y    =        3557350
71  feet           Y    =         1153179
50  meter
 Z    =        7848662
76                 Z    =         2422204
24
 XDOT =      -9570
219861                 XDOT =       -2995
434436
 YDOT =      15403
618060  feet/sec       YDOT =        4661
964860  meter/sec
 ZDOT =      17659
281154                 ZDOT =        5368
187247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18862895
55                 X    =        -5749410
56
 Y    =       -8078822
51  feet           Y    =        -2462425
10  meter
 Z    =        7962394
22                 Z    =         2426937
76
 XDOT =      12342
582334                 XDOT =        3762
019095
 YDOT =     -11412
565042  feet/sec       YDOT =       -3478
549825  meter/sec
 ZDOT =      17605
317612                 ZDOT =        5366
100808


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   07259
53771588  
00020000  00000-0  20000-3 0  9062
2 25544  51
6375 352
5199 0009371  13
1312 347
0095 15
76902880 25195


Satellite: ISS
Catalog Number: 25544
Epoch time:      07259
53771588   =   yrday
fracday
Element set:     906
Inclination:       51
6375  deg
RA of node:       352
5199  deg
Eccentricity:     
0009371     
Arg of perigee:    13
1312  deg
Mean anomaly:     347
0095  deg
Mean motion:   15
76902880  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2519
Checksum:              309


Coasting Arc #8 (Orbit 2533)
---------------------------------------

Vector Time (GMT): 2007/260/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3270616
76                 A    =         6716326
92  meter
 Y    =       -4136216
04  meter          E    =           
0011904
 Z    =       -4164119
74                 I    =           51
55985
 XDOT =       6587
450606                 Wp   =           57
37894
 YDOT =       1504
327036  meter/sec      RA   =          347
14930  deg
 ZDOT =       3693
654970                 TA   =          250
31870
                                          MA   =          250
44718
                                          Ha   =            188
140  n
mi
                                          Hp   =            177
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10730369
93                 X    =         3336854
25
 Y    =      -13570262
61  feet           Y    =        -4099271
88  meter
 Z    =      -13661810
16                 Z    =        -4148069
92
 XDOT =      21612
370754                 XDOT =        6552
196073
 YDOT =       4935
456154  feet/sec       YDOT =        1577
794575  meter/sec
 ZDOT =      12118
290585                 ZDOT =        3725
571534

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13433779
73                 X    =        -4094616
06
 Y    =       10976072
22  feet           Y    =         3345506
81  meter
 Z    =      -13601372
13                 Z    =        -4145698
23
 XDOT =     -19211
326129                 XDOT =       -5855
612204
 YDOT =      -8402
806900  feet/sec       YDOT =       -2561
175543  meter/sec
 ZDOT =      12239
603086                 ZDOT =        3730
631021


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   07260
48830236  
00020000  00000-0  20000-3 0  9075
2 25544  51
6374 347
6178 0009415  16
2429 343
9036 15
76937765 25345


Satellite: ISS
Catalog Number: 25544
Epoch time:      07260
48830236   =   yrday
fracday
Element set:     907
Inclination:       51
6374  deg
RA of node:       347
6178  deg
Eccentricity:     
0009415     
Arg of perigee:    16
2429  deg
Mean anomaly:     343
9036  deg
Mean motion:   15
76937765  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2534
Checksum:              312


Coasting Arc #9 (Orbit 2549)
---------------------------------------

Vector Time (GMT): 2007/261/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5193987
33                 A    =         6716897
85  meter
 Y    =       -1619852
07  meter          E    =           
0014885
 Z    =       -3955837
03                 I    =           51
53375
 XDOT =       4522
433763                 Wp   =           41
51589
 YDOT =      -4786
560718  meter/sec      RA   =          342
03599  deg
 ZDOT =      -3975
472119                 TA   =          187
16735
                                          MA   =          187
18865
                                          Ha   =            188
199  n
mi
                                          Hp   =            177
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17040640
83                 X    =        -5156270
93
 Y    =       -5314475
29  feet           Y    =        -1677723
30  meter
 Z    =      -12978467
94                 Z    =        -3980978
06
 XDOT =      14837
381112                 XDOT =        4594
934010
 YDOT =     -15703
939363  feet/sec       YDOT =       -4735
582949  meter/sec
 ZDOT =     -13042
887529                 ZDOT =       -3953
325789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15607466
28                 X    =         4757155
72
 Y    =        8517228
91  feet           Y    =         2596051
37  meter
 Z    =      -13074078
39                 Z    =        -3984979
09
 XDOT =     -17062
355185                 XDOT =       -5200
605860
 YDOT =      11361
037742  feet/sec       YDOT =        3462
844304  meter/sec
 ZDOT =     -12959
382826                 ZDOT =       -3950
019885


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   07261
50224082  
00020000  00000-0  20000-3 0  9086
2 25544  51
6370 342
3876 0009448  20
0376 340
1158 15
76946027 25501


Satellite: ISS
Catalog Number: 25544
Epoch time:      07261
50224082   =   yrday
fracday
Element set:     908
Inclination:       51
6370  deg
RA of node:       342
3876  deg
Eccentricity:     
0009448     
Arg of perigee:    20
0376  deg
Mean anomaly:     340
1158  deg
Mean motion:   15
76946027  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2550
Checksum:              279


Coasting Arc #10 (Orbit 2565)
---------------------------------------

Vector Time (GMT): 2007/262/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4511735
96                 A    =         6720699
33  meter
 Y    =        4217785
66  meter          E    =           
0018323
 Z    =        2643766
25                 I    =           51
51933
 XDOT =      -5200
609830                 Wp   =           71
15771
 YDOT =      -2276
559808  meter/sec      RA   =          336
82108  deg
 ZDOT =      -5208
018262                 TA   =           78
66375
                                          MA   =           78
45794
                                          Ha   =            188
324  n
mi
                                          Hp   =            177
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14802283
33                 X    =        -4571407
58
 Y    =       13837879
47  feet           Y    =         4166999
23  meter
 Z    =        8673773
77                 Z    =         2621703
15
 XDOT =     -17062
368209                 XDOT =       -5149
466672
 YDOT =      -7469
028242  feet/sec       YDOT =       -2334
429978  meter/sec
 ZDOT =     -17086
674089                 ZDOT =       -5233
158803

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17075227
89                 X    =         5204529
46
 Y    =      -10975812
42  feet           Y    =        -3345427
63  meter
 Z    =        8590517
20                 Z    =         2618389
64
 XDOT =      14566
740862                 XDOT =        4439
942615
 YDOT =       9122
286286  feet/sec       YDOT =        2780
472860  meter/sec
 ZDOT =     -17182
360842                 ZDOT =       -5237
183585


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   07262
51615832  
00020000  00000-0  20000-3 0  9096
2 25544  51
6367 337
1573 0009648  24
3167 335
8451 15
76989451 25662


Satellite: ISS
Catalog Number: 25544
Epoch time:      07262
51615832   =   yrday
fracday
Element set:     909
Inclination:       51
6367  deg
RA of node:       337
1573  deg
Eccentricity:     
0009648     
Arg of perigee:    24
3167  deg
Mean anomaly:     335
8451  deg
Mean motion:   15
76989451  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2566
Checksum:              320


Coasting Arc #11 (Orbit 2581)
---------------------------------------

Vector Time (GMT): 2007/263/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3817019
04                 A    =         6712693
67  meter
 Y    =        2423446
75  meter          E    =           
0010581
 Z    =        4952164
00                 I    =           51
46722
 XDOT =      -5659
080528                 Wp   =           59
87878
 YDOT =       4849
198165  meter/sec      RA   =          331
69058  deg
 ZDOT =       1990
918079                 TA   =           10
86750
                                          MA   =           10
84466
                                          Ha   =            188
176  n
mi
                                          Hp   =            176
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12523028
33                 X    =         3765579
19
 Y    =        7950940
78  feet           Y    =         2465843
16  meter
 Z    =       16247257
21                 Z    =         4970582
22
 XDOT =     -18566
537165                 XDOT =       -5722
555950
 YDOT =      15909
442798  feet/sec       YDOT =        4785
560207  meter/sec
 ZDOT =       6531
883460                 ZDOT =        1963
272004

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10990157
22                 X    =        -3349799
92
 Y    =       -9847556
87  feet           Y    =        -3001535
33  meter
 Z    =       16317448
71                 Z    =         4973558
37
 XDOT =      20202
404499                 XDOT =        6157
692891
 YDOT =     -11907
322947  feet/sec       YDOT =       -3629
352034  meter/sec
 ZDOT =       6427
507193                 ZDOT =        1959
104193


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   07263
53005313  
00020000  00000-0  20000-3 0  9108
2 25544  51
6370 331
9263 0009607  27
4219 332
7451 15
77044653 25822


Satellite: ISS
Catalog Number: 25544
Epoch time:      07263
53005313   =   yrday
fracday
Element set:     910
Inclination:       51
6370  deg
RA of node:       331
9263  deg
Eccentricity:     
0009607     
Arg of perigee:    27
4219  deg
Mean anomaly:     332
7451  deg
Mean motion:   15
77044653  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2582
Checksum:              272


Coasting Arc #12 (Orbit 2596)
---------------------------------------

Vector Time (GMT): 2007/264/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5208123
99                 A    =         6723405
32  meter
 Y    =       -4168294
72  meter          E    =           
0020463
 Z    =        -754927
10                 I    =           51
47752
 XDOT =       3539
327479                 Wp   =           34
89437
 YDOT =       3358
093715  meter/sec      RA   =          326
49702  deg
 ZDOT =       5971
547861                 TA   =          316
84172
                                          MA   =          317
00193
                                          Ha   =            188
503  n
mi
                                          Hp   =            176
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17087020
96                 X    =         5258014
71
 Y    =      -13675507
61  feet           Y    =        -4109775
58  meter
 Z    =       -2476794
96                 Z    =         -729504
83
 XDOT =      11611
966794                 XDOT =        3472
505006
 YDOT =      11017
367832  feet/sec       YDOT =        3397
298867  meter/sec
 ZDOT =      19591
692458                 ZDOT =        5988
579602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18890672
06                 X    =        -5757876
84
 Y    =       11072249
03  feet           Y    =         3374821
50  meter
 Z    =       -2380780
83                 Z    =         -725662
00
 XDOT =      -8989
068689                 XDOT =       -2739
868137
 YDOT =     -11180
199739  feet/sec       YDOT =       -3407
724880  meter/sec
 ZDOT =      19656
734056                 ZDOT =        5991
372540


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   07264
48056244  
00020000  00000-0  20000-3 0  9113
2 25544  51
6365 327
0234 0009917  30
5116 329
6624 15
77006577 25971


Satellite: ISS
Catalog Number: 25544
Epoch time:      07264
48056244   =   yrday
fracday
Element set:     911
Inclination:       51
6365  deg
RA of node:       327
0234  deg
Eccentricity:     
0009917     
Arg of perigee:    30
5116  deg
Mean anomaly:     329
6624  deg
Mean motion:   15
77006577  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2597
Checksum:              296

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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