Date: May 23rd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6673 62 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


143/23:31:13 309 0 3 1 6 1 6
N/A -1 0 -0 0 183 9
000/00:02:26 618 1 1 0 0 179 7

Coasting Arc #1 (Orbit 655)
---------------------------------------

Vector Time (GMT): 2007/141/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -81639
60                 A    =         6715348
98  meter
 Y    =       -5790901
78  meter          E    =           
0011237
 Z    =        3400971
54                 I    =           51
35649
 XDOT =       5616
096258                 Wp   =          137
22525
 YDOT =       2618
518334  meter/sec      RA   =          241
18942  deg
 ZDOT =       4576
441023                 TA   =          263
19102
                                          MA   =          263
31888
                                          Ha   =            184
725  n
mi
                                          Hp   =            178
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -267846
46                 X    =          -33400
10
 Y    =      -18999021
60  feet           Y    =        -5791545
51  meter
 Z    =       11158043
09                 Z    =         3400691
24
 XDOT =      18425
512657                 XDOT =        5564
166719
 YDOT =       8590
939416  feet/sec       YDOT =        2681
029634  meter/sec
 ZDOT =      15014
570287                 ZDOT =        4603
598234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13192875
69                 X    =        -4021188
51
 Y    =      -13675594
20  feet           Y    =        -4168321
11  meter
 Z    =       11156282
70                 Z    =         3400434
97
 XDOT =      18278
446804                 XDOT =        5571
270586
 YDOT =      -5255
442152  feet/sec       YDOT =       -1601
858768  meter/sec
 ZDOT =      15117
271332                 ZDOT =        4607
744302


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   07141
51457342  
00020000  00000-0  20000-3 0  9003
2 25544  51
6335 241
7308 0009483 211
1829 148
8774 15
78151108  6561


Satellite: ISS
Catalog Number: 25544
Epoch time:      07141
51457342   =   yrday
fracday
Element set:     900
Inclination:       51
6335  deg
RA of node:       241
7308  deg
Eccentricity:     
0009483     
Arg of perigee:   211
1829  deg
Mean anomaly:     148
8774  deg
Mean motion:   15
78151108  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             656
Checksum:              286


Coasting Arc #2 (Orbit 670)
---------------------------------------

Vector Time (GMT): 2007/142/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5066028
23                 A    =         6716556
20  meter
 Y    =       -3277480
83  meter          E    =           
0006049
 Z    =       -2956934
58                 I    =           51
37548
 XDOT =        859
783549                 Wp   =          191
78477
 YDOT =      -5819
170724  meter/sec      RA   =          235
95230  deg
 ZDOT =       4969
329702                 TA   =          133
93260
                                          MA   =          133
88266
                                          Ha   =            184
472  n
mi
                                          Hp   =            178
451

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16620827
53                 X    =        -5014638
23
 Y    =      -10752889
86  feet           Y    =        -3333844
28  meter
 Z    =       -9701228
95                 Z    =        -2981420
88
 XDOT =       2820
812168                 XDOT =         900
650423
 YDOT =     -19091
767466  feet/sec       YDOT =       -5809
328279  meter/sec
 ZDOT =      16303
575139                 ZDOT =        4973
605042

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19388991
82                 X    =        -5909764
71
 Y    =        3759770
71  feet           Y    =         1145978
11  meter
 Z    =       -9793952
81                 Z    =        -2985196
82
 XDOT =     -11013
855088                 XDOT =       -3357
023031
 YDOT =     -14223
605398  feet/sec       YDOT =       -4335
354925  meter/sec
 ZDOT =      16318
980611                 ZDOT =        4974
025290


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   07142
46441838  
00020000  00000-0  20000-3 0  9012
2 25544  51
6334 236
8227 0009273 216
1053 143
9487 15
78129911  6717


Satellite: ISS
Catalog Number: 25544
Epoch time:      07142
46441838   =   yrday
fracday
Element set:     901
Inclination:       51
6334  deg
RA of node:       236
8227  deg
Eccentricity:     
0009273     
Arg of perigee:   216
1053  deg
Mean anomaly:     143
9487  deg
Mean motion:   15
78129911  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             671
Checksum:              291


Coasting Arc #3 (Orbit 686)
---------------------------------------

Vector Time (GMT): 2007/143/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1696048
56                 A    =         6709516
65  meter
 Y    =        4192942
58  meter          E    =           
0007652
 Z    =       -4960378
56                 I    =           51
36939
 XDOT =      -5815
420780                 Wp   =          120
16817
 YDOT =      -4658
854128  meter/sec      RA   =          230
80651  deg
 ZDOT =      -1955
696780                 TA   =          130
90135
                                          MA   =          130
83505
                                          Ha   =            184
186  n
mi
                                          Hp   =            178
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5564463
79                 X    =        -1718712
02
 Y    =       13756373
28  feet           Y    =         4173850
23  meter
 Z    =      -16274207
89                 Z    =        -4968672
55
 XDOT =     -19079
464501                 XDOT =       -5753
392176
 YDOT =     -15284
954488  feet/sec       YDOT =       -4723
538392  meter/sec
 ZDOT =      -6416
328018                 ZDOT =       -1983
797886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5844224
30                 X    =         1781319
57
 Y    =       13603093
50  feet           Y    =         4146222
90  meter
 Z    =      -16304962
28                 Z    =        -4969752
50
 XDOT =     -23284
262490                 XDOT =       -7097
043207
 YDOT =       2208
726920  feet/sec       YDOT =         673
219965  meter/sec
 ZDOT =      -6522
863281                 ZDOT =       -1988
168728


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   07143
47756140  
00020000  00000-0  20000-3 0  9020
2 25544  51
6335 231
5869 0009300 219
9390 140
1092 15
78178512  6877


Satellite: ISS
Catalog Number: 25544
Epoch time:      07143
47756140   =   yrday
fracday
Element set:     902
Inclination:       51
6335  deg
RA of node:       231
5869  deg
Eccentricity:     
0009300     
Arg of perigee:   219
9390  deg
Mean anomaly:     140
1092  deg
Mean motion:   15
78178512  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             687
Checksum:              289


Coasting Arc #4 (Orbit 694)
---------------------------------------

Vector Time (GMT): 2007/143/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5239515
56                 A    =         6719834
77  meter
 Y    =       -3872202
61  meter          E    =           
0002019
 Z    =       -1641984
28                 I    =           51
41096
 XDOT =       1784
872316                 Wp   =          299
96698
 YDOT =      -4841
949031  meter/sec      RA   =          228
06782  deg
 ZDOT =       5718
797690                 TA   =           41
81355
                                          MA   =           41
79813
                                          Ha   =            183
900  n
mi
                                          Hp   =            179
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17190011
67                 X    =        -5187850
15
 Y    =      -12704076
80  feet           Y    =        -3930504
77  meter
 Z    =       -5387087
53                 Z    =        -1667312
73
 XDOT =       5855
880303                 XDOT =        1811
102170
 YDOT =     -15885
659549  feet/sec       YDOT =       -4821
843501  meter/sec
 ZDOT =      18762
459612                 ZDOT =        5727
531824

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20411300
67                 X    =         6221364
44
 Y    =       -6263023
59  feet           Y    =        -1908969
59  meter
 Z    =       -5483075
85                 Z    =        -1671241
52
 XDOT =       8910
099627                 XDOT =        2715
798366
 YDOT =      12571
959141  feet/sec       YDOT =        3831
933146  meter/sec
 ZDOT =      18794
791922                 ZDOT =        5728
652578


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   07143
98412456  
00020000  00000-0  20000-3 0  9036
2 25544  51
6328 228
9716 0008328 231
3887 128
6533 15
77914445  6950


Satellite: ISS
Catalog Number: 25544
Epoch time:      07143
98412456   =   yrday
fracday
Element set:     903
Inclination:       51
6328  deg
RA of node:       228
9716  deg
Eccentricity:     
0008328     
Arg of perigee:   231
3887  deg
Mean anomaly:     128
6533  deg
Mean motion:   15
77914445  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             695
Checksum:              318


Coasting Arc #5 (Orbit 710)
---------------------------------------

Vector Time (GMT): 2007/144/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2525477
40                 A    =         6708873
44  meter
 Y    =        3359876
10  meter          E    =           
0009027
 Z    =       -5235774
10                 I    =           51
39530
 XDOT =      -5844
046214                 Wp   =          115
16811
 YDOT =      -5001
143267  meter/sec      RA   =          222
90419  deg
 ZDOT =       -394
745134                 TA   =          151
09647
                                          MA   =          151
04644
                                          Ha   =            183
539  n
mi
                                          Hp   =            179
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8285687
01                 X    =        -2537425
81
 Y    =       11023215
55  feet           Y    =         3331568
46  meter
 Z    =      -17177736
55                 Z    =        -5248071
63
 XDOT =     -19173
379966                 XDOT =       -5785
770753
 YDOT =     -16407
950351  feet/sec       YDOT =       -5066
168799  meter/sec
 ZDOT =      -1295
095583                 ZDOT =        -422
994492

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4231723
80                 X    =        -1289829
41
 Y    =      -13064285
04  feet           Y    =        -3981994
08  meter
 Z    =      -17223689
89                 Z    =        -5249780
68
 XDOT =      23528
806000                 XDOT =        7171
580069
 YDOT =      -5791
253685  feet/sec       YDOT =       -1765
174123  meter/sec
 ZDOT =      -1402
247842                 ZDOT =        -427
405142


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   07144
99742203  
00020000  00000-0  20000-3 0  9045
2 25544  51
6336 223
7364 0008227 235
5355 124
5033 15
77967511  7116


Satellite: ISS
Catalog Number: 25544
Epoch time:      07144
99742203   =   yrday
fracday
Element set:     904
Inclination:       51
6336  deg
RA of node:       223
7364  deg
Eccentricity:     
0008227     
Arg of perigee:   235
5355  deg
Mean anomaly:     124
5033  deg
Mean motion:   15
77967511  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             711
Checksum:              283


Coasting Arc #6 (Orbit 726)
---------------------------------------

Vector Time (GMT): 2007/145/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4735936
73                 A    =         6720547
08  meter
 Y    =        4654200
15  meter          E    =           
0012136
 Z    =        -982895
64                 I    =           51
45686
 XDOT =      -4029
097416                 Wp   =          184
96992
 YDOT =       2850
099840  meter/sec      RA   =          217
72885  deg
 ZDOT =      -5924
308856                 TA   =            5
82044
                                          MA   =            5
80635
                                          Ha   =            183
471  n
mi
                                          Hp   =            180
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15537850
15                 X    =         4688315
56
 Y    =       15269685
54  feet           Y    =         4706893
88  meter
 Z    =       -3224723
23                 Z    =         -960003
56
 XDOT =     -13218
823542                 XDOT =       -4031
888772
 YDOT =       9350
721261  feet/sec       YDOT =        2805
029128  meter/sec
 ZDOT =     -19436
708844                 ZDOT =       -5943
888881

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21391783
42                 X    =        -6520215
59
 Y    =        4187203
57  feet           Y    =         1276259
65  meter
 Z    =       -3137810
06                 Z    =         -956404
51
 XDOT =         12
456084                 XDOT =           3
796614
 YDOT =     -14540
571703  feet/sec       YDOT =       -4431
966255  meter/sec
 ZDOT =     -19510
190493                 ZDOT =       -5946
706062


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   07146
01069727  
00020000  00000-0  20000-3 0  9054
2 25544  51
6338 218
5013 0008347 239
3554 120
6789 15
77956373  7273


Satellite: ISS
Catalog Number: 25544
Epoch time:      07146
01069727   =   yrday
fracday
Element set:     905
Inclination:       51
6338  deg
RA of node:       218
5013  deg
Eccentricity:     
0008347     
Arg of perigee:   239
3554  deg
Mean anomaly:     120
6789  deg
Mean motion:   15
77956373  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             727
Checksum:              309


Coasting Arc #7 (Orbit 742)
---------------------------------------

Vector Time (GMT): 2007/146/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4460553
85                 A    =         6710732
14  meter
 Y    =       -1636146
43  meter          E    =           
0001104
 Z    =        4740243
08                 I    =           51
44834
 XDOT =       4759
787425                 Wp   =          278
09924
 YDOT =       5480
236318  meter/sec      RA   =          212
51942  deg
 ZDOT =      -2587
740745                 TA   =          197
32760
                                          MA   =          197
33137
                                          Ha   =            182
943  n
mi
                                          Hp   =            180
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14634363
03                 X    =         4455490
46
 Y    =       -5367934
47  feet           Y    =        -1586294
77  meter
 Z    =       15551978
60                 Z    =         4761900
24
 XDOT =      15616
100477                 XDOT =        4710
723784
 YDOT =      17979
777945  feet/sec       YDOT =        5533
188847  meter/sec
 ZDOT =      -8489
963075                 ZDOT =       -2564
736089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3545180
88                 X    =        -1080571
13
 Y    =       15095372
54  feet           Y    =         4601069
55  meter
 Z    =       15633450
05                 Z    =         4765075
58
 XDOT =     -22535
886599                 XDOT =       -6868
938236
 YDOT =       3408
211550  feet/sec       YDOT =        1038
822880  meter/sec
 ZDOT =      -8402
516861                 ZDOT =       -2561
087139


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   07147
02394785  
00020000  00000-0  20000-3 0  9062
2 25544  51
6337 213
2661 0008253 245
1544 114
8763 15
78056733  7430


Satellite: ISS
Catalog Number: 25544
Epoch time:      07147
02394785   =   yrday
fracday
Element set:     906
Inclination:       51
6337  deg
RA of node:       213
2661  deg
Eccentricity:     
0008253     
Arg of perigee:   245
1544  deg
Mean anomaly:     114
8763  deg
Mean motion:   15
78056733  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             743
Checksum:              294


Coasting Arc #8 (Orbit 758)
---------------------------------------

Vector Time (GMT): 2007/147/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3311983
41                 A    =         6715727
92  meter
 Y    =       -4755662
94  meter          E    =           
0005785
 Z    =        3392155
83                 I    =           51
49010
 XDOT =       6104
005507                 Wp   =          120
62409
 YDOT =       -962
112240  meter/sec      RA   =          207
38633  deg
 ZDOT =       4602
198711                 TA   =          279
58396
                                          MA   =          279
64932
                                          Ha   =            182
827  n
mi
                                          Hp   =            180
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10866087
31                 X    =        -3275037
46
 Y    =      -15602568
69  feet           Y    =        -4792493
19  meter
 Z    =       11129120
18                 Z    =         3376155
20
 XDOT =      20026
264786                 XDOT =        6091
953341
 YDOT =      -3156
536222  feet/sec       YDOT =        -893
921719  meter/sec
 ZDOT =      15099
077136                 ZDOT =        4631
823034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19030556
01                 X    =         5800513
47
 Y    =        -838278
76  feet           Y    =         -255507
37  meter
 Z    =       11068177
18                 Z    =         3373580
41
 XDOT =      -8108
714548                 XDOT =       -2471
536194
 YDOT =      17128
978160  feet/sec       YDOT =        5220
912543  meter/sec
 ZDOT =      15210
687170                 ZDOT =        4636
217450


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   07148
03717883  
00020000  00000-0  20000-3 0  9073
2 25544  51
6340 208
0302 0008141 249
1367 110
8927 15
78044205  7597


Satellite: ISS
Catalog Number: 25544
Epoch time:      07148
03717883   =   yrday
fracday
Element set:     907
Inclination:       51
6340  deg
RA of node:       208
0302  deg
Eccentricity:     
0008141     
Arg of perigee:   249
1367  deg
Mean anomaly:     110
8927  deg
Mean motion:   15
78044205  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             759
Checksum:              282


Coasting Arc #9 (Orbit 773)
---------------------------------------

Vector Time (GMT): 2007/148/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6006530
64                 A    =         6716539
27  meter
 Y    =         129303
04  meter          E    =           
0003758
 Z    =       -3000847
65                 I    =           51
51965
 XDOT =      -2590
747328                 Wp   =          255
33298
 YDOT =      -5304
420756  meter/sec      RA   =          202
15918  deg
 ZDOT =       4951
025744                 TA   =           69
86026
                                          MA   =           69
81984
                                          Ha   =            182
523  n
mi
                                          Hp   =            180
639

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19706465
35                 X    =        -5992952
28
 Y    =         424222
57  feet           Y    =           62210
95  meter
 Z    =       -9845300
68                 Z    =        -3029994
88
 XDOT =      -8499
827190                 XDOT =       -2555
291572
 YDOT =     -17402
955235  feet/sec       YDOT =       -5333
194337  meter/sec
 ZDOT =      16243
522781                 ZDOT =        4938
525117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9905839
09                 X    =         3019299
75
 Y    =      -16977118
66  feet           Y    =        -5174625
77  meter
 Z    =       -9955223
79                 Z    =        -3034352
21
 XDOT =      18089
029612                 XDOT =        5513
536226
 YDOT =       1046
033285  feet/sec       YDOT =         318
830945  meter/sec
 ZDOT =      16195
711030                 ZDOT =        4936
452722


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   07148
98706061  
00020000  00000-0  20000-3 0  9084
2 25544  51
6338 203
1218 0008275 253
5859 106
4397 15
78089276  7745


Satellite: ISS
Catalog Number: 25544
Epoch time:      07148
98706061   =   yrday
fracday
Element set:     908
Inclination:       51
6338  deg
RA of node:       203
1218  deg
Eccentricity:     
0008275     
Arg of perigee:   253
5859  deg
Mean anomaly:     106
4397  deg
Mean motion:   15
78089276  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             774
Checksum:              321


Coasting Arc #10 (Orbit 789)
---------------------------------------

Vector Time (GMT): 2007/149/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1020307
52                 A    =         6709753
52  meter
 Y    =        4423049
53  meter          E    =           
0004566
 Z    =       -4945453
49                 I    =           51
52353
 XDOT =      -7406
929345                 Wp   =           68
92634
 YDOT =       -572
448191  meter/sec      RA   =          197
02519  deg
 ZDOT =      -2040
010108                 TA   =          181
30321
                                          MA   =          181
30440
                                          Ha   =            182
210  n
mi
                                          Hp   =            180
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3347465
61                 X    =          994797
05
 Y    =       14511317
35  feet           Y    =         4434317
28  meter
 Z    =      -16225241
10                 Z    =        -4940558
05
 XDOT =     -24300
949293                 XDOT =       -7390
067465
 YDOT =      -1878
110863  feet/sec       YDOT =        -655
182043  meter/sec
 ZDOT =      -6692
946547                 ZDOT =       -2075
952755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14247300
90                 X    =        -4342577
32
 Y    =       -4406239
63  feet           Y    =        -1343021
84  meter
 Z    =      -16206226
43                 Z    =        -4939657
82
 XDOT =      13616
269369                 XDOT =        4150
238904
 YDOT =     -18910
334217  feet/sec       YDOT =       -5763
869869  meter/sec
 ZDOT =      -6828
600098                 ZDOT =       -2081
357310


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   07150
00024707  
00020000  00000-0  20000-3 0  9091
2 25544  51
6332 197
8860 0008291 258
0089 102
0147 15
78141315  7900


Satellite: ISS
Catalog Number: 25544
Epoch time:      07150
00024707   =   yrday
fracday
Element set:     909
Inclination:       51
6332  deg
RA of node:       197
8860  deg
Eccentricity:     
0008291     
Arg of perigee:   258
0089  deg
Mean anomaly:     102
0147  deg
Mean motion:   15
78141315  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             790
Checksum:              273


Coasting Arc #11 (Orbit 805)
---------------------------------------

Vector Time (GMT): 2007/150/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6618601
08                 A    =         6720392
84  meter
 Y    =        1043238
90  meter          E    =           
0010018
 Z    =         423615
21                 I    =           51
58706
 XDOT =       -370
501013                 Wp   =          169
70153
 YDOT =       4800
283957  meter/sec      RA   =          191
83103  deg
 ZDOT =      -6020
837276                 TA   =            5
67961
                                          MA   =            5
66826
                                          Ha   =            182
041  n
mi
                                          Hp   =            180
962

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21714570
47                 X    =         6604385
64
 Y    =        3422699
80  feet           Y    =         1117172
25  meter
 Z    =        1389813
69                 Z    =          455734
58
 XDOT =      -1215
554505                 XDOT =        -394
902317
 YDOT =      15748
963113  feet/sec       YDOT =        4796
005400  meter/sec
 ZDOT =     -19753
403137                 ZDOT =       -6022
695653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13676257
86                 X    =        -4168523
40
 Y    =       17200160
68  feet           Y    =         5242608
98  meter
 Z    =        1511115
52                 Z    =          460588
01
 XDOT =     -11904
476101                 XDOT =       -3628
484316
 YDOT =      -7726
330801  feet/sec       YDOT =       -2354
985628  meter/sec
 ZDOT =     -19759
822778                 ZDOT =       -6022
793983


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   07151
01341361  
00020000  00000-0  20000-3 0  9103
2 25544  51
6330 192
6505 0008252 260
4801  99
5432 15
78119008  8062


Satellite: ISS
Catalog Number: 25544
Epoch time:      07151
01341361   =   yrday
fracday
Element set:     910
Inclination:       51
6330  deg
RA of node:       192
6505  deg
Eccentricity:     
0008252     
Arg of perigee:   260
4801  deg
Mean anomaly:      99
5432  deg
Mean motion:   15
78119008  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             806
Checksum:              257


Coasting Arc #12 (Orbit 821)
---------------------------------------

Vector Time (GMT): 2007/151/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1707210
83                 A    =         6708526
17  meter
 Y    =       -3928223
95  meter          E    =           
0005377
 Z    =        5167882
39                 I    =           51
57574
 XDOT =       7417
957769                 Wp   =          286
01151
 YDOT =       1756
018485  meter/sec      RA   =          186
65367  deg
 ZDOT =      -1115
231448                 TA   =          174
63935
                                          MA   =          174
63359
                                          Ha   =            181
581  n
mi
                                          Hp   =            181
038

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5601085
39                 X    =         1725904
92
 Y    =      -12887873
85  feet           Y    =        -3909029
42  meter
 Z    =       16954994
71                 Z    =         5176220
80
 XDOT =      24337
131788                 XDOT =        7403
188063
 YDOT =       5761
215503  feet/sec       YDOT =        1838
887876  meter/sec
 ZDOT =      -3658
895828                 ZDOT =       -1079
230029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8690570
59                 X    =         2648885
92
 Y    =       10995086
81  feet           Y    =         3351302
46  meter
 Z    =       16985974
93                 Z    =         5177325
16
 XDOT =     -15897
461426                 XDOT =       -4845
546243
 YDOT =      18010
312569  feet/sec       YDOT =        5489
543271  meter/sec
 ZDOT =      -3522
845432                 ZDOT =       -1073
763288


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   07152
02655519  
00020000  00000-0  20000-3 0  9119
2 25544  51
6324 187
4137 0008326 265
8278  94
1935 15
78204983  8221


Satellite: ISS
Catalog Number: 25544
Epoch time:      07152
02655519   =   yrday
fracday
Element set:     911
Inclination:       51
6324  deg
RA of node:       187
4137  deg
Eccentricity:     
0008326     
Arg of perigee:   265
8278  deg
Mean anomaly:      94
1935  deg
Mean motion:   15
78204983  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             822
Checksum:              302


Coasting Arc #13 (Orbit 837)
---------------------------------------

Vector Time (GMT): 2007/152/23:32:26
618
Vector Time (MET): N/A
Weight (LBS)     : 480698
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5982241
23                 A    =         6717872
62  meter
 Y    =       -1987575
74  meter          E    =           
0006501
 Z    =        2310525
56                 I    =           51
63508
 XDOT =       3496
994376                 Wp   =           49
98066
 YDOT =      -4206
973126  meter/sec      RA   =          181
51235  deg
 ZDOT =       5429
301805                 TA   =          336
05401
                                          MA   =          336
08423
                                          Ha   =            180
603  n
mi
                                          Hp   =            180
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19626775
67                 X    =        -5970795
48
 Y    =       -6520917
78  feet           Y    =        -2054408
99  meter
 Z    =        7580464
43                 Z    =         2281490
93
 XDOT =      11473
078663                 XDOT =        3517
402626
 YDOT =     -13802
405268  feet/sec       YDOT =       -4167
754769  meter/sec
 ZDOT =      17812
669963                 ZDOT =        5446
339099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14880593
58                 X    =         4535604
92
 Y    =      -14420587
23  feet           Y    =        -4395394
99  meter
 Z    =        7470658
04                 Z    =         2277056
57
 XDOT =       5923
311414                 XDOT =        1805
425319
 YDOT =      15383
430463  feet/sec       YDOT =        4688
869605  meter/sec
 ZDOT =      17876
448145                 ZDOT =        5448
741395


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   07153
03967636  
00020000  00000-0  20000-3 0  9128
2 25544  51
6312 182
1763 0008423 269
9645  90
0555 15
78242348  8383


Satellite: ISS
Catalog Number: 25544
Epoch time:      07153
03967636   =   yrday
fracday
Element set:     912
Inclination:       51
6312  deg
RA of node:       182
1763  deg
Eccentricity:     
0008423     
Arg of perigee:   269
9645  deg
Mean anomaly:      90
0555  deg
Mean motion:   15
78242348  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             838
Checksum:              303

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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