Date: March 3rd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7857 65 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 3392)
---------------------------------------

Vector Time (GMT): 2007/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4062044
64                 A    =         6706400
84  meter
 Y    =        1171289
71  meter          E    =           
0018453
 Z    =        5222048
82                 I    =           51
32489
 XDOT =      -2788
777035                 Wp   =          265
71724
 YDOT =       7149
779038  meter/sec      RA   =          294
69250  deg
 ZDOT =        565
974031                 TA   =          178
87909
                                          MA   =          178
87495
                                          Ha   =            183
923  n
mi
                                          Hp   =            174
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13326918
12                 X    =         4023278
17
 Y    =        3842814
00  feet           Y    =         1216497
33  meter
 Z    =       17132706
11                 Z    =         5241687
44
 XDOT =      -9149
530955                 XDOT =       -2871
268942
 YDOT =      23457
280310  feet/sec       YDOT =        7118
132174  meter/sec
 ZDOT =       1856
870182                 ZDOT =         552
225737

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10999745
25                 X    =         3352722
35
 Y    =        8297044
06  feet           Y    =         2528939
03  meter
 Z    =       17206633
86                 Z    =         5244582
00
 XDOT =     -16298
214505                 XDOT =       -4967
695781
 YDOT =      17864
004996  feet/sec       YDOT =        5444
948723  meter/sec
 ZDOT =       1806
157901                 ZDOT =         550
516928


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   07061
54837053  
00020000  00000-0  20000-3 0  9008
2 25544  51
6350 295
0644 0020978 269
6183  90
2579 15
78858434 33936


Satellite: ISS
Catalog Number: 25544
Epoch time:      07061
54837053   =   yrday
fracday
Element set:     900
Inclination:       51
6350  deg
RA of node:       295
0644  deg
Eccentricity:     
0020978     
Arg of perigee:   269
6183  deg
Mean anomaly:      90
2579  deg
Mean motion:   15
78858434  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3393
Checksum:              316


Coasting Arc #2 (Orbit 3408)
---------------------------------------

Vector Time (GMT): 2007/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3047816
03                 A    =         6717626
39  meter
 Y    =       -5871694
94  meter          E    =           
0012797
 Z    =        1141252
42                 I    =           51
35171
 XDOT =       3872
639077                 Wp   =          312
70080
 YDOT =       3142
702146  meter/sec      RA   =          289
50315  deg
 ZDOT =       5876
992469                 TA   =           59
87138
                                          MA   =           59
74462
                                          Ha   =            183
883  n
mi
                                          Hp   =            174
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9999396
43                 X    =         3107703
79
 Y    =      -19264091
02  feet           Y    =        -5837277
62  meter
 Z    =        3744266
47                 Z    =         1156204
26
 XDOT =      12705
508784                 XDOT =        3808
660466
 YDOT =      10310
702578  feet/sec       YDOT =        3185
650903  meter/sec
 ZDOT =      19281
471355                 ZDOT =        5895
649622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15926101
28                 X    =         4854275
67
 Y    =      -14732092
74  feet           Y    =        -4490341
87  meter
 Z    =        3799658
49                 Z    =         1158135
91
 XDOT =       7274
905051                 XDOT =        2217
391059
 YDOT =      12813
908987  feet/sec       YDOT =        3905
679459  meter/sec
 ZDOT =      19351
974433                 ZDOT =        5898
481807


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   07062
56105944  
00020000  00000-0  20000-3 0  9019
2 25544  51
6340 289
8242 0021153 273
6160  86
2586 15
78921910 34097


Satellite: ISS
Catalog Number: 25544
Epoch time:      07062
56105944   =   yrday
fracday
Element set:     901
Inclination:       51
6340  deg
RA of node:       289
8242  deg
Eccentricity:     
0021153     
Arg of perigee:   273
6160  deg
Mean anomaly:      86
2586  deg
Mean motion:   15
78921910  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3409
Checksum:              288


Coasting Arc #3 (Orbit 3423)
---------------------------------------

Vector Time (GMT): 2007/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2660502
64                 A    =         6709137
65  meter
 Y    =       -4185794
22  meter          E    =           
0011513
 Z    =       -4508673
27                 I    =           51
31398
 XDOT =       4008
220233                 Wp   =          265
82062
 YDOT =      -5843
224574  meter/sec      RA   =          284
27248  deg
 ZDOT =       3052
077640                 TA   =           34
66722
                                          MA   =           34
59223
                                          Ha   =            183
861  n
mi
                                          Hp   =            174
822

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8728683
19                 X    =        -2591596
89
 Y    =      -13732920
66  feet           Y    =        -4215160
58  meter
 Z    =      -14792235
15                 Z    =        -4521429
98
 XDOT =      13150
328849                 XDOT =        4058
435976
 YDOT =     -19170
684299  feet/sec       YDOT =       -5798
121370  meter/sec
 ZDOT =      10013
378084                 ZDOT =        3071
671660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3742405
20                 X    =        -1140685
11
 Y    =      -15790529
24  feet           Y    =        -4812953
31  meter
 Z    =      -14840715
29                 Z    =        -4523450
02
 XDOT =      17437
372324                 XDOT =        5314
911084
 YDOT =     -13635
286913  feet/sec       YDOT =       -4156
035451  meter/sec
 ZDOT =      10086
204880                 ZDOT =        3074
275247


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   07063
51043297  
00020000  00000-0  20000-3 0  9028
2 25544  51
6330 284
9116 0021189 277
3686  82
5072 15
78953821 34247


Satellite: ISS
Catalog Number: 25544
Epoch time:      07063
51043297   =   yrday
fracday
Element set:     902
Inclination:       51
6330  deg
RA of node:       284
9116  deg
Eccentricity:     
0021189     
Arg of perigee:   277
3686  deg
Mean anomaly:      82
5072  deg
Mean motion:   15
78953821  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3424
Checksum:              297


Coasting Arc #4 (Orbit 3439)
---------------------------------------

Vector Time (GMT): 2007/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3802632
22                 A    =         6711266
18  meter
 Y    =        3895755
52  meter          E    =           
0015581
 Z    =       -3917255
44                 I    =           51
31456
 XDOT =      -2236
095907                 Wp   =          293
52639
 YDOT =      -6210
676270  meter/sec      RA   =          279
12507  deg
 ZDOT =      -3987
277891                 TA   =          294
91175
                                          MA   =          295
07360
                                          Ha   =            184
007  n
mi
                                          Hp   =            174
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12475827
48                 X    =        -3826883
48
 Y    =       12781350
13  feet           Y    =         3853096
40  meter
 Z    =      -12851887
93                 Z    =        -3935787
60
 XDOT =      -7336
272661                 XDOT =       -2147
111876
 YDOT =     -20376
234481  feet/sec       YDOT =       -6235
184381  meter/sec
 ZDOT =     -13081
620376                 ZDOT =       -3997
923953

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15728648
41                 X    =        -4794092
04
 Y    =        8356917
39  feet           Y    =         2547188
42  meter
 Z    =      -12920981
26                 Z    =        -3938315
09
 XDOT =        -48
752028                 XDOT =         -14
859618
 YDOT =     -20475
001495  feet/sec       YDOT =       -6240
780456  meter/sec
 ZDOT =     -13122
447357                 ZDOT =       -3999
721954


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   07064
52307182  
00020000  00000-0  20000-3 0  9037
2 25544  51
6320 279
6724 0021272 281
3457  78
5319 15
78974807 34400


Satellite: ISS
Catalog Number: 25544
Epoch time:      07064
52307182   =   yrday
fracday
Element set:     903
Inclination:       51
6320  deg
RA of node:       279
6724  deg
Eccentricity:     
0021272     
Arg of perigee:   281
3457  deg
Mean anomaly:      78
5319  deg
Mean motion:   15
78974807  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3440
Checksum:              299


Coasting Arc #5 (Orbit 3455)
---------------------------------------

Vector Time (GMT): 2007/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1233133
16                 A    =         6715933
05  meter
 Y    =        6272117
36  meter          E    =           
0007345
 Z    =        2067821
70                 I    =           51
32841
 XDOT =      -4618
757085                 Wp   =          275
89287
 YDOT =       2725
026679  meter/sec      RA   =          273
88216  deg
 ZDOT =      -5527
246165                 TA   =          240
88942
                                          MA   =          240
96298
                                          Ha   =            184
132  n
mi
                                          Hp   =            174
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4045712
47                 X    =         1152860
81
 Y    =       20577812
87  feet           Y    =         6285458
31  meter
 Z    =        6784191
93                 Z    =         2073616
66
 XDOT =     -15153
402510                 XDOT =       -4622
035381
 YDOT =       8940
376244  feet/sec       YDOT =        2673
358332  meter/sec
 ZDOT =     -18134
009727                 ZDOT =       -5549
692041

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2143643
97                 X    =         -653382
68
 Y    =       20854534
06  feet           Y    =         6356461
98  meter
 Z    =        6806807
73                 Z    =         2074715
00
 XDOT =     -15479
801900                 XDOT =       -4718
243619
 YDOT =       4337
926946  feet/sec       YDOT =        1322
200133  meter/sec
 ZDOT =     -18217
960133                 ZDOT =       -5552
834248


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   07065
53568319  
00020000  00000-0  20000-3 0  9041
2 25544  51
6324 274
4320 0021307 285
6996  74
1819 15
79059478 34566


Satellite: ISS
Catalog Number: 25544
Epoch time:      07065
53568319   =   yrday
fracday
Element set:     904
Inclination:       51
6324  deg
RA of node:       274
4320  deg
Eccentricity:     
0021307     
Arg of perigee:   285
6996  deg
Mean anomaly:      74
1819  deg
Mean motion:   15
79059478  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3456
Checksum:              319


Coasting Arc #6 (Orbit 3471)
---------------------------------------

Vector Time (GMT): 2007/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4173891
51                 A    =         6705887
26  meter
 Y    =        -632331
87  meter          E    =           
0018471
 Z    =        5224965
47                 I    =           51
29251
 XDOT =        562
103938                 Wp   =          288
79991
 YDOT =       7660
791920  meter/sec      RA   =          268
70593  deg
 ZDOT =        485
358773                 TA   =          156
60701
                                          MA   =          156
52287
                                          Ha   =            184
290  n
mi
                                          Hp   =            174
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13693869
77                 X    =         4155270
36
 Y    =       -2074579
61  feet           Y    =         -585760
78  meter
 Z    =       17142275
16                 Z    =         5245196
91
 XDOT =       1844
173025                 XDOT =         474
040320
 YDOT =      25133
831759  feet/sec       YDOT =        7666
585331  meter/sec
 ZDOT =       1592
384427                 ZDOT =         487
874947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13646272
75                 X    =         4159383
93
 Y    =        1731106
80  feet           Y    =          527641
35  meter
 Z    =       17218189
71                 Z    =         5248104
22
 XDOT =      -4996
346861                 XDOT =       -1522
886523
 YDOT =      23679
502814  feet/sec       YDOT =        7217
512458  meter/sec
 ZDOT =       1602
873847                 ZDOT =         488
555949


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   07066
54827019  
00020000  00000-0  20000-3 0  9059
2 25544  51
6314 269
1904 0021183 289
3017  70
5857 15
79031382 34725


Satellite: ISS
Catalog Number: 25544
Epoch time:      07066
54827019   =   yrday
fracday
Element set:     905
Inclination:       51
6314  deg
RA of node:       269
1904  deg
Eccentricity:     
0021183     
Arg of perigee:   289
3017  deg
Mean anomaly:      70
5857  deg
Mean motion:   15
79031382  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3472
Checksum:              296


Coasting Arc #7 (Orbit 3487)
---------------------------------------

Vector Time (GMT): 2007/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         276277
93                 A    =         6716969
40  meter
 Y    =       -6580648
61  meter          E    =           
0017241
 Z    =        1271882
25                 I    =           51
33180
 XDOT =       4857
240399                 Wp   =          333
77661
 YDOT =       1324
659019  meter/sec      RA   =          263
51445  deg
 ZDOT =       5843
911117                 TA   =           40
27756
                                          MA   =           40
14996
                                          Ha   =            184
409  n
mi
                                          Hp   =            174
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         906423
65                 X    =          343664
60
 Y    =      -21590054
48  feet           Y    =        -6577182
25  meter
 Z    =        4172842
01                 Z    =         1273388
49
 XDOT =      15935
828080                 XDOT =        4813
678328
 YDOT =       4345
994158  feet/sec       YDOT =        1378
732198  meter/sec
 ZDOT =      19172
936735                 ZDOT =        5867
401591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6411876
17                 X    =         1954339
86
 Y    =      -20634924
30  feet           Y    =        -6289524
93  meter
 Z    =        4177608
18                 Z    =         1273334
97
 XDOT =      12671
738663                 XDOT =        3862
345944
 YDOT =       7806
960604  feet/sec       YDOT =        2379
561592  meter/sec
 ZDOT =      19261
360834                 ZDOT =        5870
862782


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   07067
56082690  
00020000  00000-0  20000-3 0  9061
2 25544  51
6305 263
9487 0021279 293
0529  66
8393 15
79111975 34886


Satellite: ISS
Catalog Number: 25544
Epoch time:      07067
56082690   =   yrday
fracday
Element set:     906
Inclination:       51
6305  deg
RA of node:       263
9487  deg
Eccentricity:     
0021279     
Arg of perigee:   293
0529  deg
Mean anomaly:      66
8393  deg
Mean motion:   15
79111975  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3488
Checksum:              329


Coasting Arc #8 (Orbit 3502)
---------------------------------------

Vector Time (GMT): 2007/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4187975
27                 A    =         6708945
00  meter
 Y    =       -2823091
24  meter          E    =           
0011701
 Z    =       -4404055
34                 I    =           51
30919
 XDOT =       1228
039451                 Wp   =          301
67794
 YDOT =      -6891
048754  meter/sec      RA   =          258
27908  deg
 ZDOT =       3249
286653                 TA   =             
96914
                                          MA   =             
96687
                                          Ha   =            184
472  n
mi
                                          Hp   =            174
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13740076
34                 X    =        -4134701
76
 Y    =       -9262110
36  feet           Y    =        -2869625
85  meter
 Z    =      -14449000
46                 Z    =        -4424270
93
 XDOT =       4029
000823                 XDOT =        1289
220476
 YDOT =     -22608
427669  feet/sec       YDOT =       -6876
973904  meter/sec
 ZDOT =      10660
389283                 ZDOT =        3255
401367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11027310
70                 X    =        -3361124
30
 Y    =      -12278568
96  feet           Y    =        -3742507
82  meter
 Z    =      -14525328
33                 Z    =        -4427320
08
 XDOT =       8401
456719                 XDOT =        2560
764008
 YDOT =     -20183
314622  feet/sec       YDOT =       -6151
874297  meter/sec
 ZDOT =      10682
425870                 ZDOT =        3256
003405


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   07068
51007555  
00020000  00000-0  20000-3 0  9075
2 25544  51
6299 259
0348 0021190 296
7019  63
1978 15
79152457 35033


Satellite: ISS
Catalog Number: 25544
Epoch time:      07068
51007555   =   yrday
fracday
Element set:     907
Inclination:       51
6299  deg
RA of node:       259
0348  deg
Eccentricity:     
0021190     
Arg of perigee:   296
7019  deg
Mean anomaly:      63
1978  deg
Mean motion:   15
79152457  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3503
Checksum:              310


Coasting Arc #9 (Orbit 3518)
---------------------------------------

Vector Time (GMT): 2007/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1920986
67                 A    =         6710030
14  meter
 Y    =        4957673
48  meter          E    =           
0017316
 Z    =       -4093299
17                 I    =           51
32029
 XDOT =      -4620
246514                 Wp   =          321
23809
 YDOT =      -4901
387526  meter/sec      RA   =          253
13095  deg
 ZDOT =      -3746
242985                 TA   =          270
15441
                                          MA   =          270
35284
                                          Ha   =            184
770  n
mi
                                          Hp   =            174
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6302449
71                 X    =        -1956396
88
 Y    =       16265332
94  feet           Y    =         4935993
83  meter
 Z    =      -13429459
23                 Z    =        -4102717
44
 XDOT =     -15158
289089                 XDOT =       -4546
896607
 YDOT =     -16080
667737  feet/sec       YDOT =       -4952
643689  meter/sec
 ZDOT =     -12290
823442                 ZDOT =       -3768
509755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9713774
82                 X    =        -2960758
57
 Y    =       14456521
06  feet           Y    =         4406347
62  meter
 Z    =      -13464170
27                 Z    =        -4103879
10
 XDOT =     -10048
738447                 XDOT =       -3062
855479
 YDOT =     -18344
398132  feet/sec       YDOT =       -5591
372551  meter/sec
 ZDOT =     -12375
144128                 ZDOT =       -3771
943930


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   07069
52258018  
00020000  00000-0  20000-3 0  9080
2 25544  51
6298 253
7949 0021160 301
0513  58
8575 15
79208300 35196


Satellite: ISS
Catalog Number: 25544
Epoch time:      07069
52258018   =   yrday
fracday
Element set:     908
Inclination:       51
6298  deg
RA of node:       253
7949  deg
Eccentricity:     
0021160     
Arg of perigee:   301
0513  deg
Mean anomaly:      58
8575  deg
Mean motion:   15
79208300  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3519
Checksum:              298


Coasting Arc #10 (Orbit 3534)
---------------------------------------

Vector Time (GMT): 2007/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3678183
54                 A    =         6715824
19  meter
 Y    =        5347785
23  meter          E    =           
0007908
 Z    =        1744255
40                 I    =           51
35051
 XDOT =      -3239
424592                 Wp   =          322
88716
 YDOT =       4075
410893  meter/sec      RA   =          247
89018  deg
 ZDOT =      -5671
001552                 TA   =          197
70381
                                          MA   =          197
73139
                                          Ha   =            185
032  n
mi
                                          Hp   =            174
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12067531
30                 X    =         3609637
24
 Y    =       17545227
14  feet           Y    =         5388533
50  meter
 Z    =        5722622
72                 Z    =         1761957
34
 XDOT =     -10628
033437                 XDOT =       -3257
207124
 YDOT =      13370
770647  feet/sec       YDOT =        4039
086330  meter/sec
 ZDOT =     -18605
648136                 ZDOT =       -5686
781832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8137610
62                 X    =         2480343
72
 Y    =       19658726
56  feet           Y    =         5991979
85  meter
 Z    =        5789860
25                 Z    =         1764749
40
 XDOT =     -11633
592398                 XDOT =       -3545
918963
 YDOT =      10305
845482  feet/sec       YDOT =        3141
221703  meter/sec
 ZDOT =     -18664
384185                 ZDOT =       -5688
904300


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   07070
53505475  
00020000  00000-0  20000-3 0  9096
2 25544  51
6299 248
5531 0021466 304
8639  55
0509 15
79281195 35352


Satellite: ISS
Catalog Number: 25544
Epoch time:      07070
53505475   =   yrday
fracday
Element set:     909
Inclination:       51
6299  deg
RA of node:       248
5531  deg
Eccentricity:     
0021466     
Arg of perigee:   304
8639  deg
Mean anomaly:      55
0509  deg
Mean motion:   15
79281195  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3535
Checksum:              310


Coasting Arc #11 (Orbit 3550)
---------------------------------------

Vector Time (GMT): 2007/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3728985
20                 A    =         6705248
77  meter
 Y    =       -1923676
50  meter          E    =           
0019234
 Z    =        5242173
02                 I    =           51
32556
 XDOT =       3535
778962                 Wp   =          313
26401
 YDOT =       6839
457882  meter/sec      RA   =          242
70826  deg
 ZDOT =          7
683404                 TA   =          136
73838
                                          MA   =          136
58718
                                          Ha   =            185
206  n
mi
                                          Hp   =            174
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12234203
41                 X    =         3724753
59
 Y    =       -6311274
59  feet           Y    =        -1882000
53  meter
 Z    =       17198730
39                 Z    =         5260278
00
 XDOT =      11600
324677                 XDOT =        3458
999053
 YDOT =      22439
166279  feet/sec       YDOT =        6878
567641  meter/sec
 ZDOT =         25
208017                 ZDOT =          24
673514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13117967
49                 X    =         3998356
49
 Y    =       -3884739
51  feet           Y    =        -1184068
60  meter
 Z    =       17266498
63                 Z    =         5262828
78
 XDOT =       6831
903830                 XDOT =        2082
364287
 YDOT =      23280
799175  feet/sec       YDOT =        7095
987589  meter/sec
 ZDOT =         89
982663                 ZDOT =          27
426716


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   07071
54750599  
00020000  00000-0  20000-3 0  9109
2 25544  51
6292 243
3110 0021058 308
9417  50
9872 15
79228758 35518


Satellite: ISS
Catalog Number: 25544
Epoch time:      07071
54750599   =   yrday
fracday
Element set:     910
Inclination:       51
6292  deg
RA of node:       243
3110  deg
Eccentricity:     
0021058     
Arg of perigee:   308
9417  deg
Mean anomaly:      50
9872  deg
Mean motion:   15
79228758  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3551
Checksum:              299


Coasting Arc #12 (Orbit 3566)
---------------------------------------

Vector Time (GMT): 2007/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2226149
73                 A    =         6715770
53  meter
 Y    =       -6080307
25  meter          E    =           
0020457
 Z    =        1735309
33                 I    =           51
37659
 XDOT =       5205
467554                 Wp   =          352
38638
 YDOT =       -289
483993  meter/sec      RA   =          237
52709  deg
 ZDOT =       5691
148405                 TA   =           26
96382
                                          MA   =           26
85767
                                          Ha   =            185
350  n
mi
                                          Hp   =            173
933

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7303640
85                 X    =        -2166423
12
 Y    =      -19948514
58  feet           Y    =        -6104867
34  meter
 Z    =        5693272
09                 Z    =         1724639
96
 XDOT =      17078
305622                 XDOT =        5180
671527
 YDOT =       -949
750632  feet/sec       YDOT =        -231
412150  meter/sec
 ZDOT =      18671
746737                 ZDOT =        5716
375998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3763036
48                 X    =        -1146973
52
 Y    =      -20918659
74  feet           Y    =        -6376007
49  meter
 Z    =        5652343
06                 Z    =         1722834
16
 XDOT =      15356
091081                 XDOT =        4680
536562
 YDOT =       2283
778575  feet/sec       YDOT =         696
095710  meter/sec
 ZDOT =      18766
510631                 ZDOT =        5720
032440


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   07072
55992300  
00020000  00000-0  20000-3 0  9110
2 25544  51
6294 238
0692 0021096 312
5958  47
3428 15
79327324 35672


Satellite: ISS
Catalog Number: 25544
Epoch time:      07072
55992300   =   yrday
fracday
Element set:     911
Inclination:       51
6294  deg
RA of node:       238
0692  deg
Eccentricity:     
0021096     
Arg of perigee:   312
5958  deg
Mean anomaly:      47
3428  deg
Mean motion:   15
79327324  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3567
Checksum:              304

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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