Date: May 18th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 1854)
---------------------------------------

Vector Time (GMT): 2010/136/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4772523
40                 A    =         6730774
89  meter
 Y    =        4409693
39  meter          E    =           
0014856
 Z    =        1716806
23                 I    =           51
83606
 XDOT =      -4455
743108                 Wp   =           25
87146
 YDOT =       2589
270476  meter/sec      RA   =           30
75285  deg
 ZDOT =       5730
409067                 TA   =          353
08756
                                          MA   =          353
10803
                                          Ha   =            190
661  n
mi
                                          Hp   =            185
045

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15657885
18                 X    =         4714518
69
 Y    =       14467497
99  feet           Y    =         4462738
02  meter
 Z    =        5632566
38                 Z    =         1739851
11
 XDOT =     -14618
579751                 XDOT =       -4512
203199
 YDOT =       8494
981875  feet/sec       YDOT =        2539
127212  meter/sec
 ZDOT =      18800
554681                 ZDOT =        5708
626070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17502428
53                 X    =        -5334740
22
 Y    =      -12128499
29  feet           Y    =        -3696766
58  meter
 Z    =        5724348
95                 Z    =         1744781
56
 XDOT =      12504
756811                 XDOT =        3811
449876
 YDOT =      -9204
750827  feet/sec       YDOT =       -2805
608052  meter/sec
 ZDOT =      18713
789363                 ZDOT =        5703
962998


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   10136
93339497  
00016717  00000-0  10270-3 0  9005
2 25544  51
6465  30
9730 0009637 319
9852  40
0600 15
74029215 18558


Satellite: ISS
Catalog Number: 25544
Epoch time:      10136
93339497   =   yrday
fracday
Element set:     900
Inclination:       51
6465  deg
RA of node:        30
9730  deg
Eccentricity:     
0009637     
Arg of perigee:   319
9852  deg
Mean anomaly:      40
0600  deg
Mean motion:   15
74029215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1855
Checksum:              307


Coasting Arc #2 (Orbit 1869)
---------------------------------------

Vector Time (GMT): 2010/137/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3691284
11                 A    =         6721246
92  meter
 Y    =       -2588574
13  meter          E    =           
0008078
 Z    =       -4989255
21                 I    =           51
77748
 XDOT =       5876
774485                 Wp   =           56
09790
 YDOT =       4554
593959  meter/sec      RA   =           25
59796  deg
 ZDOT =       1991
557929                 TA   =          233
09406
                                          MA   =          233
16811
                                          Ha   =            190
873  n
mi
                                          Hp   =            184
825

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12110512
16                 X    =         3744192
68
 Y    =       -8492697
29  feet           Y    =        -2546999
50  meter
 Z    =      -16368947
53                 Z    =        -4971194
69
 XDOT =      19280
756183                 XDOT =        5815
732742
 YDOT =      14942
893567  feet/sec       YDOT =        4619
969977  meter/sec
 ZDOT =       6533
982707                 ZDOT =        2019
959788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10716427
02                 X    =        -3266366
96
 Y    =       10310125
41  feet           Y    =         3142526
23  meter
 Z    =      -16297004
66                 Z    =        -4967327
02
 XDOT =     -20603
855121                 XDOT =       -6280
055041
 YDOT =     -10943
793883  feet/sec       YDOT =       -3335
668375  meter/sec
 ZDOT =       6647
103820                 ZDOT =        2026
037244


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   10137
88572043  
00016717  00000-0  10270-3 0  9017
2 25544  51
6464  26
0838 0009693 323
6842  36
3663 15
74069677 18705


Satellite: ISS
Catalog Number: 25544
Epoch time:      10137
88572043   =   yrday
fracday
Element set:     901
Inclination:       51
6464  deg
RA of node:        26
0838  deg
Eccentricity:     
0009693     
Arg of perigee:   323
6842  deg
Mean anomaly:      36
3663  deg
Mean motion:   15
74069677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1870
Checksum:              326


Coasting Arc #3 (Orbit 1885)
---------------------------------------

Vector Time (GMT): 2010/138/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5445081
54                 A    =         6730521
98  meter
 Y    =       -3534602
63  meter          E    =           
0002537
 Z    =       -1782154
40                 I    =           51
78136
 XDOT =       3999
110087                 Wp   =          343
19434
 YDOT =      -3288
995084  meter/sec      RA   =           20
50452  deg
 ZDOT =      -5691
074018                 TA   =          216
49731
                                          MA   =          216
51460
                                          Ha   =            190
975  n
mi
                                          Hp   =            184
490

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17864440
75                 X    =        -5396494
89
 Y    =      -11596465
32  feet           Y    =        -3595220
90  meter
 Z    =       -5846963
25                 Z    =        -1808489
04
 XDOT =      13120
439919                 XDOT =        4063
237243
 YDOT =     -10790
666285  feet/sec       YDOT =       -3243
915429  meter/sec
 ZDOT =     -18671
502684                 ZDOT =       -5671
490935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19579688
97                 X    =         5967889
20
 Y    =        8307493
04  feet           Y    =         2532123
88  meter
 Z    =       -5951854
30                 Z    =        -1814125
19
 XDOT =     -10538
491872                 XDOT =       -3212
132323
 YDOT =      11506
539623  feet/sec       YDOT =        3507
193277  meter/sec
 ZDOT =     -18593
491277                 ZDOT =       -5667
296141


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   10138
90151730  
00016717  00000-0  10270-3 0  9028
2 25544  51
6465  20
8669 0009747 327
4264  32
6297 15
74077316 18868


Satellite: ISS
Catalog Number: 25544
Epoch time:      10138
90151730   =   yrday
fracday
Element set:     902
Inclination:       51
6465  deg
RA of node:        20
8669  deg
Eccentricity:     
0009747     
Arg of perigee:   327
4264  deg
Mean anomaly:      32
6297  deg
Mean motion:   15
74077316  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1886
Checksum:              320


Coasting Arc #4 (Orbit 1901)
---------------------------------------

Vector Time (GMT): 2010/139/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3285418
77                 A    =         6721299
26  meter
 Y    =        3148914
36  meter          E    =           
0012118
 Z    =        4949759
61                 I    =           51
72209
 XDOT =      -6527
714635                 Wp   =            2
22565
 YDOT =      -3503
042110  meter/sec      RA   =           15
34278  deg
 ZDOT =      -2092
193405                 TA   =          108
09627
                                          MA   =          107
96424
                                          Ha   =            191
194  n
mi
                                          Hp   =            184
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10778932
97                 X    =        -3344431
36
 Y    =       10331083
87  feet           Y    =         3111844
43  meter
 Z    =       16239368
81                 Z    =         4933656
00
 XDOT =     -21416
386597                 XDOT =       -6477
894331
 YDOT =     -11492
920308  feet/sec       YDOT =       -3575
760143  meter/sec
 ZDOT =      -6864
151590                 ZDOT =       -2123
784370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8695886
27                 X    =         2650506
13
 Y    =      -12222016
80  feet           Y    =        -3725270
72  meter
 Z    =       16175217
36                 Z    =         4930206
25
 XDOT =      22288
956366                 XDOT =        6793
673900
 YDOT =       6555
037961  feet/sec       YDOT =        1997
975570  meter/sec
 ZDOT =      -6989
981049                 ZDOT =       -2130
546224


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   10139
91729707  
00016717  00000-0  10270-3 0  9036
2 25544  51
6470  15
6501 0009855 331
8208  28
2421 15
74108936 19020


Satellite: ISS
Catalog Number: 25544
Epoch time:      10139
91729707   =   yrday
fracday
Element set:     903
Inclination:       51
6470  deg
RA of node:        15
6501  deg
Eccentricity:     
0009855     
Arg of perigee:   331
8208  deg
Mean anomaly:      28
2421  deg
Mean motion:   15
74108936  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1902
Checksum:              300


Coasting Arc #5 (Orbit 1917)
---------------------------------------

Vector Time (GMT): 2010/140/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5918295
53                 A    =         6730247
65  meter
 Y    =        2571461
10  meter          E    =           
0016978
 Z    =        1872557
97                 I    =           51
72328
 XDOT =      -3489
260451                 Wp   =           31
27672
 YDOT =       3905
203770  meter/sec      RA   =           10
24706  deg
 ZDOT =       5656
659377                 TA   =          349
51755
                                          MA   =          349
55290
                                          Ha   =            191
215  n
mi
                                          Hp   =            183
937

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19416980
10                 X    =         5880004
57
 Y    =        8436552
18  feet           Y    =         2637428
78  meter
 Z    =        6143562
91                 Z    =         1901216
28
 XDOT =     -11447
704893                 XDOT =       -3560
148887
 YDOT =      12812
348327  feet/sec       YDOT =        3865
788015  meter/sec
 ZDOT =      18558
593758                 ZDOT =        5639
536614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20712520
75                 X    =        -6313176
33
 Y    =       -4215498
81  feet           Y    =        -1284884
04  meter
 Z    =        6257711
08                 Z    =         1907350
34
 XDOT =       8327
670628                 XDOT =        2538
274008
 YDOT =     -13428
458968  feet/sec       YDOT =       -4092
994293  meter/sec
 ZDOT =      18490
382792                 ZDOT =        5635
868675


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   10140
93306002  
00016717  00000-0  10270-3 0  9040
2 25544  51
6472  10
4335 0009857 335
6985  24
3712 15
74123761 19186


Satellite: ISS
Catalog Number: 25544
Epoch time:      10140
93306002   =   yrday
fracday
Element set:     904
Inclination:       51
6472  deg
RA of node:        10
4335  deg
Eccentricity:     
0009857     
Arg of perigee:   335
6985  deg
Mean anomaly:      24
3712  deg
Mean motion:   15
74123761  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1918
Checksum:              290


Coasting Arc #6 (Orbit 1932)
---------------------------------------

Vector Time (GMT): 2010/141/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2788607
87                 A    =         6721263
91  meter
 Y    =       -3651132
34  meter          E    =           
0010209
 Z    =       -4911166
39                 I    =           51
66316
 XDOT =       6980
557184                 Wp   =           55
20922
 YDOT =       2373
561823  meter/sec      RA   =            5
08053  deg
 ZDOT =       2207
984999                 TA   =          236
19535
                                          MA   =          236
29260
                                          Ha   =            191
393  n
mi
                                          Hp   =            183
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9148975
96                 X    =         2853085
92
 Y    =      -11978780
63  feet           Y    =        -3619587
66  meter
 Z    =      -16112750
62                 Z    =        -4897462
85
 XDOT =      22902
090498                 XDOT =        6942
770724
 YDOT =       7787
276321  feet/sec       YDOT =        2451
411167  meter/sec
 ZDOT =       7244
045271                 ZDOT =        2241
805085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6310672
92                 X    =        -1923493
11
 Y    =       13752328
38  feet           Y    =         4191709
69  meter
 Z    =      -16058161
49                 Z    =        -4894527
62
 XDOT =     -23022
334107                 XDOT =       -7017
207436
 YDOT =      -1982
948463  feet/sec       YDOT =        -604
402692  meter/sec
 ZDOT =       7378
749821                 ZDOT =        2249
042946


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   10141
88532237  
00016717  00000-0  10270-3 0  9057
2 25544  51
6470   5
5440 0009910 339
3975  20
6787 15
74173682 19331


Satellite: ISS
Catalog Number: 25544
Epoch time:      10141
88532237   =   yrday
fracday
Element set:     905
Inclination:       51
6470  deg
RA of node:         5
5440  deg
Eccentricity:     
0009910     
Arg of perigee:   339
3975  deg
Mean anomaly:      20
6787  deg
Mean motion:   15
74173682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1933
Checksum:              312


Coasting Arc #7 (Orbit 1948)
---------------------------------------

Vector Time (GMT): 2010/142/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6228747
86                 A    =         6729881
14  meter
 Y    =       -1584621
50  meter          E    =           
0004634
 Z    =       -2006176
15                 I    =           51
66144
 XDOT =       2921
161516                 Wp   =           16
49798
 YDOT =      -4414
810893  meter/sec      RA   =          359
98202  deg
 ZDOT =      -5581
232722                 TA   =          185
82828
                                          MA   =          185
83368
                                          Ha   =            191
509  n
mi
                                          Hp   =            183
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20435524
47                 X    =        -6200819
65
 Y    =       -5198889
43  feet           Y    =        -1654118
80  meter
 Z    =       -6581942
74                 Z    =        -2036367
97
 XDOT =       9583
863240                 XDOT =        2997
424518
 YDOT =     -14484
287708  feet/sec       YDOT =       -4381
717993  meter/sec
 ZDOT =     -18311
130978                 ZDOT =       -5566
856582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21048251
02                 X    =         6415506
91
 Y    =         113317
38  feet           Y    =           34539
14  meter
 Z    =       -6702191
42                 Z    =        -2042827
94
 XDOT =      -5893
668718                 XDOT =       -1796
390225
 YDOT =      14863
498438  feet/sec       YDOT =        4530
394324  meter/sec
 ZDOT =     -18253
862437                 ZDOT =       -5563
777271


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   10142
90105323  
00016717  00000-0  10270-3 0  9064
2 25544  51
6464    
3272 0009930 342
9511  17
1317 15
74167707 19496


Satellite: ISS
Catalog Number: 25544
Epoch time:      10142
90105323   =   yrday
fracday
Element set:     906
Inclination:       51
6464  deg
RA of node:          
3272  deg
Eccentricity:     
0009930     
Arg of perigee:   342
9511  deg
Mean anomaly:      17
1317  deg
Mean motion:   15
74167707  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1949
Checksum:              284


Coasting Arc #8 (Orbit 1964)
---------------------------------------

Vector Time (GMT): 2010/143/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2306890
20                 A    =         6721391
35  meter
 Y    =        4058936
70  meter          E    =           
0013902
 Z    =        4837285
19                 I    =           51
60366
 XDOT =      -7214
743886                 Wp   =           14
60418
 YDOT =      -1241
547871  meter/sec      RA   =          354
80707  deg
 ZDOT =      -2384
213361                 TA   =           98
74799
                                          MA   =           98
59051
                                          Ha   =            191
633  n
mi
                                          Hp   =            183
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7568537
41                 X    =        -2375605
52
 Y    =       13316721
47  feet           Y    =         4032755
13  meter
 Z    =       15870358
25                 Z    =         4825911
53
 XDOT =     -23670
419575                 XDOT =       -7188
742202
 YDOT =      -4073
319788  feet/sec       YDOT =       -1322
081882  meter/sec
 ZDOT =      -7822
222314                 ZDOT =       -2419
200046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3960018
34                 X    =         1207013
59
 Y    =      -14844938
29  feet           Y    =        -4524737
19  meter
 Z    =       15825048
56                 Z    =         4823474
80
 XDOT =      22791
570935                 XDOT =        6946
870821
 YDOT =      -2458
939045  feet/sec       YDOT =        -749
484621  meter/sec
 ZDOT =      -7961
562730                 ZDOT =       -2426
684320


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   10143
91676546  
00016717  00000-0  10270-3 0  9077
2 25544  51
6471 355
1098 0010125 346
3395  13
7493 15
74234337 19656


Satellite: ISS
Catalog Number: 25544
Epoch time:      10143
91676546   =   yrday
fracday
Element set:     907
Inclination:       51
6471  deg
RA of node:       355
1098  deg
Eccentricity:     
0010125     
Arg of perigee:   346
3395  deg
Mean anomaly:      13
7493  deg
Mean motion:   15
74234337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1965
Checksum:              317


Coasting Arc #9 (Orbit 1980)
---------------------------------------

Vector Time (GMT): 2010/144/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6335118
81                 A    =         6729460
95  meter
 Y    =         585686
08  meter          E    =           
0018629
 Z    =        2155329
06                 I    =           51
60030
 XDOT =      -2328
463955                 Wp   =           38
36522
 YDOT =       4862
766453  meter/sec      RA   =          349
70661  deg
 ZDOT =       5511
650938                 TA   =          345
80326
                                          MA   =          345
85555
                                          Ha   =            191
687  n
mi
                                          Hp   =            182
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20784510
53                 X    =         6317628
33
 Y    =        1921542
26  feet           Y    =          656431
15  meter
 Z    =        7071289
56                 Z    =         2186063
20
 XDOT =      -7639
317439                 XDOT =       -2409
442319
 YDOT =      15953
958179  feet/sec       YDOT =        4836
274891  meter/sec
 ZDOT =      18082
844284                 ZDOT =        5500
142809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20471114
68                 X    =        -6239595
75
 Y    =        3856892
27  feet           Y    =         1175580
76  meter
 Z    =        7193690
62                 Z    =         2192636
90
 XDOT =       3340
619298                 XDOT =        1018
220762
 YDOT =     -15976
747878  feet/sec       YDOT =       -4869
712753  meter/sec
 ZDOT =      18036
994071                 ZDOT =        5497
675793


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   10144
93246354  
00016717  00000-0  10270-3 0  9081
2 25544  51
6465 349
8931 0010112 351
0100   9
0881 15
74220932 19811


Satellite: ISS
Catalog Number: 25544
Epoch time:      10144
93246354   =   yrday
fracday
Element set:     908
Inclination:       51
6465  deg
RA of node:       349
8931  deg
Eccentricity:     
0010112     
Arg of perigee:   351
0100  deg
Mean anomaly:       9
0881  deg
Mean motion:   15
74220932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1981
Checksum:              286


Coasting Arc #10 (Orbit 1995)
---------------------------------------

Vector Time (GMT): 2010/145/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1745056
86                 A    =         6721605
20  meter
 Y    =       -4411720
84  meter          E    =           
0011953
 Z    =       -4767319
02                 I    =           51
54350
 XDOT =       7254
361356                 Wp   =           56
34439
 YDOT =        107
265262  meter/sec      RA   =          344
52541  deg
 ZDOT =       2567
273273                 TA   =          238
81046
                                          MA   =          238
92770
                                          Ha   =            191
895  n
mi
                                          Hp   =            182
603

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5725252
17                 X    =         1817419
04
 Y    =      -14474149
74  feet           Y    =        -4391801
41  meter
 Z    =      -15640810
45                 Z    =        -4758666
13
 XDOT =      23800
398148                 XDOT =        7240
151143
 YDOT =        351
920151  feet/sec       YDOT =         188
308090  meter/sec
 ZDOT =       8422
812576                 ZDOT =        2602
481136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1345154
10                 X    =         -410002
97
 Y    =       15541798
76  feet           Y    =         4737140
26  meter
 Z    =      -15606329
68                 Z    =        -4756809
29
 XDOT =     -21688
079114                 XDOT =       -6610
526514
 YDOT =       6684
785448  feet/sec       YDOT =        2037
522605  meter/sec
 ZDOT =       8563
030535                 ZDOT =        2610
011707


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   10145
88466407  
00016717  00000-0  10270-3 0  9090
2 25544  51
6455 345
0023 0010236 354
8470   5
2586 15
74256979 19964


Satellite: ISS
Catalog Number: 25544
Epoch time:      10145
88466407   =   yrday
fracday
Element set:     909
Inclination:       51
6455  deg
RA of node:       345
0023  deg
Eccentricity:     
0010236     
Arg of perigee:   354
8470  deg
Mean anomaly:       5
2586  deg
Mean motion:   15
74256979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1996
Checksum:              328


Coasting Arc #11 (Orbit 2011)
---------------------------------------

Vector Time (GMT): 2010/146/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6298886
50                 A    =         6728891
04  meter
 Y    =         369037
40  meter          E    =           
0007493
 Z    =       -2352344
42                 I    =           51
53972
 XDOT =       1706
962952                 Wp   =           30
57633
 YDOT =      -5213
852900  meter/sec      RA   =          339
42179  deg
 ZDOT =      -5389
872612                 TA   =          175
91853
                                          MA   =          175
91241
                                          Ha   =            192
001  n
mi
                                          Hp   =            182
234

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20665638
13                 X    =        -6291117
53
 Y    =        1210752
62  feet           Y    =          298643
28  meter
 Z    =       -7717665
43                 Z    =        -2382926
04
 XDOT =       5600
272151                 XDOT =        1791
321819
 YDOT =     -17105
816600  feet/sec       YDOT =       -5194
292176  meter/sec
 ZDOT =     -17683
309094                 ZDOT =       -5381
375873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19245097
82                 X    =         5865905
82
 Y    =       -7501061
56  feet           Y    =        -2286323
56  meter
 Z    =       -7839462
13                 Z    =        -2389468
06
 XDOT =       -706
782785                 XDOT =        -215
427393
 YDOT =      16628
349835  feet/sec       YDOT =        5068
321030  meter/sec
 ZDOT =     -17649
442081                 ZDOT =       -5379
549946


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   10146
90032882  
00016717  00000-0  10270-3 0  9102
2 25544  51
6456 339
7845 0010285 359
0411   1
0731 15
74281332 20120


Satellite: ISS
Catalog Number: 25544
Epoch time:      10146
90032882   =   yrday
fracday
Element set:     910
Inclination:       51
6456  deg
RA of node:       339
7845  deg
Eccentricity:     
0010285     
Arg of perigee:   359
0411  deg
Mean anomaly:       1
0731  deg
Mean motion:   15
74281332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2012
Checksum:              276


Coasting Arc #12 (Orbit 2027)
---------------------------------------

Vector Time (GMT): 2010/147/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1226275
26                 A    =         6721858
98  meter
 Y    =        4698754
96  meter          E    =           
0015911
 Z    =        4647668
91                 I    =           51
48841
 XDOT =      -7106
082893                 Wp   =           28
02894
 YDOT =        944
966802  meter/sec      RA   =          334
23265  deg
 ZDOT =      -2812
554688                 TA   =           89
88683
                                          MA   =           89
70451
                                          Ha   =            192
064  n
mi
                                          Hp   =            182
055

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4023212
79                 X    =        -1301304
31
 Y    =       15415862
72  feet           Y    =         4684621
75  meter
 Z    =       15248257
57                 Z    =         4641530
08
 XDOT =     -23313
920253                 XDOT =       -7102
458459
 YDOT =       3100
284783  feet/sec       YDOT =         865
523073  meter/sec
 ZDOT =      -9227
541626                 ZDOT =       -2847
067591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1107821
86                 X    =         -337664
10
 Y    =      -15917086
66  feet           Y    =        -4851528
01  meter
 Z    =       15223780
94                 Z    =         4640208
43
 XDOT =      19836
602284                 XDOT =        6046
196376
 YDOT =     -10393
400301  feet/sec       YDOT =       -3167
908412  meter/sec
 ZDOT =      -9365
001821                 ZDOT =       -2854
452555


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   10147
91597463  
00016717  00000-0  10270-3 0  9116
2 25544  51
6456 334
5667 0010388   1
7977 358
3222 15
74334044 20286


Satellite: ISS
Catalog Number: 25544
Epoch time:      10147
91597463   =   yrday
fracday
Element set:     911
Inclination:       51
6456  deg
RA of node:       334
5667  deg
Eccentricity:     
0010388     
Arg of perigee:     1
7977  deg
Mean anomaly:     358
3222  deg
Mean motion:   15
74334044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2028
Checksum:              316


Coasting Arc #13 (Orbit 2043)
---------------------------------------

Vector Time (GMT): 2010/148/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6080508
40                 A    =         6728393
00  meter
 Y    =       -1267205
54  meter          E    =           
0019993
 Z    =        2553585
25                 I    =           51
48324
 XDOT =      -1067
337200                 Wp   =           47
02903
 YDOT =       5526
311410  meter/sec      RA   =          329
12747  deg
 ZDOT =       5271
440429                 TA   =          342
04798
                                          MA   =          342
11850
                                          Ha   =            192
189  n
mi
                                          Hp   =            181
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19949174
54                 X    =         6081821
62
 Y    =       -4157498
48  feet           Y    =        -1199202
77  meter
 Z    =        8377904
37                 Z    =         2583127
64
 XDOT =      -3501
762468                 XDOT =       -1154
662047
 YDOT =      18130
942947  feet/sec       YDOT =        5513
886640  meter/sec
 ZDOT =      17294
752063                 ZDOT =        5266
044092

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17295103
25                 X    =        -5271547
47
 Y    =       10684018
63  feet           Y    =         3256488
88  meter
 Z    =        8495574
71                 Z    =         2589451
17
 XDOT =      -2005
718840                 XDOT =        -611
343102
 YDOT =     -17014
005923  feet/sec       YDOT =       -5185
869005  meter/sec
 ZDOT =      17273
226035                 ZDOT =        5264
879296


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   10148
93160737  
00016717  00000-0  10270-3 0  9120
2 25544  51
6452 329
3486 0010518   7
3496 352
7819 15
74304910 20443


Satellite: ISS
Catalog Number: 25544
Epoch time:      10148
93160737   =   yrday
fracday
Element set:     912
Inclination:       51
6452  deg
RA of node:       329
3486  deg
Eccentricity:     
0010518     
Arg of perigee:     7
3496  deg
Mean anomaly:     352
7819  deg
Mean motion:   15
74304910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2044
Checksum:              307


Coasting Arc #14 (Orbit 2058)
---------------------------------------

Vector Time (GMT): 2010/149/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         626717
49                 A    =         6722262
36  meter
 Y    =       -4928558
17  meter          E    =           
0013271
 Z    =       -4534463
48                 I    =           51
43833
 XDOT =       6793
028985                 Wp   =           58
33976
 YDOT =      -1934
709741  meter/sec      RA   =          323
93168  deg
 ZDOT =       3055
133378                 TA   =          242
10442
                                          MA   =          242
23889
                                          Ha   =            192
318  n
mi
                                          Hp   =            181
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2056159
76                 X    =          703810
67
 Y    =      -16169810
28  feet           Y    =        -4921118
00  meter
 Z    =      -14876848
68                 Z    =        -4531232
47
 XDOT =      22286
840503                 XDOT =        6799
317016
 YDOT =      -6347
472902  feet/sec       YDOT =       -1858
711425  meter/sec
 ZDOT =      10023
403471                 ZDOT =        3088
149039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3763265
29                 X    =         1147043
26
 Y    =       15871734
90  feet           Y    =         4837704
80  meter
 Z    =      -14863951
35                 Z    =        -4530532
37
 XDOT =     -17345
342528                 XDOT =       -5286
860403
 YDOT =      13581
589219  feet/sec       YDOT =        4139
668394  meter/sec
 ZDOT =      10154
916018                 ZDOT =        3095
218402


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   10149
88374473  
00016717  00000-0  10270-3 0  9130
2 25544  51
6461 324
4569 0010572  10
2923 349
8455 15
74346884 20594


Satellite: ISS
Catalog Number: 25544
Epoch time:      10149
88374473   =   yrday
fracday
Element set:     913
Inclination:       51
6461  deg
RA of node:       324
4569  deg
Eccentricity:     
0010572     
Arg of perigee:    10
2923  deg
Mean anomaly:     349
8455  deg
Mean motion:   15
74346884  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2059
Checksum:              328


Coasting Arc #15 (Orbit 2074)
---------------------------------------

Vector Time (GMT): 2010/150/20:57:33
838
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5762413
21                 A    =         6727554
32  meter
 Y    =        2067652
45  meter          E    =           
0010557
 Z    =       -2806110
88                 I    =           51
43351
 XDOT =        412
969339                 Wp   =           39
36029
 YDOT =      -5750
596751  meter/sec      RA   =          318
82519  deg
 ZDOT =      -5087
737238                 TA   =          172
84167
                                          MA   =          172
82658
                                          Ha   =            192
382  n
mi
                                          Hp   =            181
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18905555
16                 X    =        -5771474
20
 Y    =        6783636
65  feet           Y    =         2003163
53  meter
 Z    =       -9206400
53                 Z    =        -2834126
39
 XDOT =       1354
886283                 XDOT =         501
958201
 YDOT =     -18866
787241  feet/sec       YDOT =       -5745
480257  meter/sec
 ZDOT =     -16692
051305                 ZDOT =       -5085
515849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14965852
18                 X    =         4561591
74
 Y    =      -13318921
69  feet           Y    =        -4059607
33  meter
 Z    =       -9318001
21                 Z    =        -2840126
77
 XDOT =       4710
254445                 XDOT =        1435
685555
 YDOT =      16958
835696  feet/sec       YDOT =        5169
053120  meter/sec
 ZDOT =     -16683
174061                 ZDOT =       -5085
031454


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   10150
89934214  
00016717  00000-0  10270-3 0  9149
2 25544  51
6466 319
2388 0010608  14
4065 345
7399 15
74392199 20753


Satellite: ISS
Catalog Number: 25544
Epoch time:      10150
89934214   =   yrday
fracday
Element set:     914
Inclination:       51
6466  deg
RA of node:       319
2388  deg
Eccentricity:     
0010608     
Arg of perigee:    14
4065  deg
Mean anomaly:     345
7399  deg
Mean motion:   15
74392199  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2075
Checksum:              326

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics 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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