[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: June 15th 2012

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12109 4 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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


172/13:49:37 925 -0 8 4 2 4 2
N/A 4 1 0 0 221 1
000/00:09:15 850 -0 4 -0 2 209 8

Coasting Arc #1 (Orbit 1774)
---------------------------------------

Vector Time (GMT): 2012/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923792
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4766421
42                 A    =         6773057
38  meter
 Y    =         202925
34  meter          E    =           
0021914
 Z    =       -4828552
80                 I    =           51
88720
 XDOT =      -2887
246812                 Wp   =           69
49435
 YDOT =       6605
327584  meter/sec      RA   =          129
87999  deg
 ZDOT =      -2574
472447                 TA   =          175
20958
                                          MA   =          175
18857
                                          Ha   =            221
239  n
mi
                                          Hp   =            207
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15637865
55                 X    =         4787254
23
 Y    =         665765
56  feet           Y    =          256343
54  meter
 Z    =      -15841708
67                 Z    =        -4805346
91
 XDOT =      -9472
594526                 XDOT =       -2948
388036
 YDOT =      21671
022258  feet/sec       YDOT =        6572
699084  meter/sec
 ZDOT =      -8446
431912                 ZDOT =       -2588
646320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2476869
15                 X    =          754949
72
 Y    =      -15552197
90  feet           Y    =        -4740309
92  meter
 Z    =      -15746113
04                 Z    =        -4799415
25
 XDOT =      19303
797037                 XDOT =        5883
797337
 YDOT =      11679
239147  feet/sec       YDOT =        3559
832092  meter/sec
 ZDOT =      -8505
428179                 ZDOT =       -2592
454509


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   12167
52066289  
00016717  00000-0  10270-3 0  9002
2 25544  51
6343 130
7361 0010548  66
6282 293
5980 15
56375300 17754


Satellite: ISS
Catalog Number: 25544
Epoch time:      12167
52066289   =   yrday
fracday
Element set:     900
Inclination:       51
6343  deg
RA of node:       130
7361  deg
Eccentricity:     
0010548     
Arg of perigee:    66
6282  deg
Mean anomaly:     293
5980  deg
Mean motion:   15
56375300  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1775
Checksum:              310


Coasting Arc #2 (Orbit 1790)
---------------------------------------

Vector Time (GMT): 2012/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923792
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3325517
31                 A    =         6770714
14  meter
 Y    =       -2524039
63  meter          E    =           
0012851
 Z    =        5319888
87                 I    =           51
89900
 XDOT =       4486
960812                 Wp   =           72
67028
 YDOT =      -6233
763280  meter/sec      RA   =          124
87557  deg
 ZDOT =       -148
753357                 TA   =           18
76337
                                          MA   =           18
71605
                                          Ha   =            221
308  n
mi
                                          Hp   =            207
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10910489
87                 X    =        -3322888
84
 Y    =       -8280969
91  feet           Y    =        -2561213
71  meter
 Z    =       17453703
64                 Z    =         5303739
54
 XDOT =      14721
000040                 XDOT =        4557
057159
 YDOT =     -20451
979264  feet/sec       YDOT =       -6183
195353  meter/sec
 ZDOT =       -488
035947                 ZDOT =        -126
786390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9323197
59                 X    =        -2841710
62
 Y    =       10148973
39  feet           Y    =         3093407
09  meter
 Z    =       17387390
50                 Z    =         5299676
62
 XDOT =     -18164
697268                 XDOT =       -5536
599727
 YDOT =     -15983
919924  feet/sec       YDOT =       -4871
898793  meter/sec
 ZDOT =       -396
943721                 ZDOT =        -120
988446


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   12168
54799531  
00016717  00000-0  10270-3 0  9019
2 25544  51
6347 125
5968 0010490  69
8932 290
3350 15
56408215 17912


Satellite: ISS
Catalog Number: 25544
Epoch time:      12168
54799531   =   yrday
fracday
Element set:     901
Inclination:       51
6347  deg
RA of node:       125
5968  deg
Eccentricity:     
0010490     
Arg of perigee:    69
8932  deg
Mean anomaly:     290
3350  deg
Mean motion:   15
56408215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1791
Checksum:              325


Coasting Arc #3 (Orbit 1805)
---------------------------------------

Vector Time (GMT): 2012/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923792
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1611265
21                 A    =         6773311
62  meter
 Y    =        4608027
78  meter          E    =           
0020211
 Z    =       -4713175
06                 I    =           51
92479
 XDOT =      -5293
871634                 Wp   =           91
79574
 YDOT =       4747
292723  meter/sec      RA   =          119
87243  deg
 ZDOT =       2841
482263                 TA   =          206
27723
                                          MA   =          206
37991
                                          Ha   =            221
192  n
mi
                                          Hp   =            207
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5286303
18                 X    =         1582513
21
 Y    =       15118201
37  feet           Y    =         4625885
94  meter
 Z    =      -15463172
78                 Z    =        -4705416
67
 XDOT =     -17368
345256                 XDOT =       -5360
366730
 YDOT =      15575
107358  feet/sec       YDOT =        4687
721123  meter/sec
 ZDOT =       9322
448368                 ZDOT =        2815
603969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15504249
48                 X    =         4725695
24
 Y    =       -4134935
68  feet           Y    =        -1260328
39  meter
 Z    =      -15431632
50                 Z    =        -4703561
59
 XDOT =      13807
517609                 XDOT =        4208
531367
 YDOT =      17501
738253  feet/sec       YDOT =        5334
529819  meter/sec
 ZDOT =       9215
356512                 ZDOT =        2808
840665


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   12169
51110474  
00016717  00000-0  10270-3 0  9021
2 25544  51
6351 120
7781 0010457  73
2684 286
9616 15
56416484 18063


Satellite: ISS
Catalog Number: 25544
Epoch time:      12169
51110474   =   yrday
fracday
Element set:     902
Inclination:       51
6351  deg
RA of node:       120
7781  deg
Eccentricity:     
0010457     
Arg of perigee:    73
2684  deg
Mean anomaly:     286
9616  deg
Mean motion:   15
56416484  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1806
Checksum:              308


Coasting Arc #4 (Orbit 1821)
---------------------------------------

Vector Time (GMT): 2012/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923792
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         186784
72                 A    =         6778634
71  meter
 Y    =       -6048170
50  meter          E    =           
0023231
 Z    =        3036393
52                 I    =           51
95824
 XDOT =       5368
526643                 Wp   =           87
77284
 YDOT =      -2343
014750  meter/sec      RA   =          114
88746  deg
 ZDOT =      -4963
776392                 TA   =           57
51350
                                          MA   =           57
28915
                                          Ha   =            221
147  n
mi
                                          Hp   =            207
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         612810
76                 X    =          239652
57
 Y    =      -19843079
07  feet           Y    =        -6045786
67  meter
 Z    =        9961920
99                 Z    =         3037428
31
 XDOT =      17613
276389                 XDOT =        5418
440673
 YDOT =      -7687
056265  feet/sec       YDOT =       -2282
700638  meter/sec
 ZDOT =     -16285
355617                 ZDOT =       -4937
575415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19766308
86                 X    =        -6024770
94
 Y    =       -1822045
73  feet           Y    =         -555359
54  meter
 Z    =        9966763
63                 Z    =         3037869
55
 XDOT =      -6670
514526                 XDOT =       -2033
172828
 YDOT =     -16727
005219  feet/sec       YDOT =       -5098
391191  meter/sec
 ZDOT =     -16177
144371                 ZDOT =       -4930
793604


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   12170
53840591  
00016717  00000-0  10270-3 0  9036
2 25544  51
6360 115
6381 0010469  76
8640 283
3681 15
56461017 18229


Satellite: ISS
Catalog Number: 25544
Epoch time:      12170
53840591   =   yrday
fracday
Element set:     903
Inclination:       51
6360  deg
RA of node:       115
6381  deg
Eccentricity:     
0010469     
Arg of perigee:    76
8640  deg
Mean anomaly:     283
3681  deg
Mean motion:   15
56461017  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1822
Checksum:              299


Coasting Arc #5 (Orbit 1836)
---------------------------------------

Vector Time (GMT): 2012/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923792
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1729343
86                 A    =         6782266
43  meter
 Y    =        6509110
64  meter          E    =           
0019497
 Z    =        -757522
26                 I    =           51
98255
 XDOT =      -4764
644919                 Wp   =           60
29988
 YDOT =       -583
894161  meter/sec      RA   =          109
92328  deg
 ZDOT =       5984
382903                 TA   =          291
54379
                                          MA   =          291
75149
                                          Ha   =            221
111  n
mi
                                          Hp   =            207
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5673700
32                 X    =        -1798321
66
 Y    =       21355349
88  feet           Y    =         6489386
50  meter
 Z    =       -2485309
25                 Z    =         -766089
75
 XDOT =     -15632
037137                 XDOT =       -4786
832324
 YDOT =      -1915
663258  feet/sec       YDOT =        -637
300457  meter/sec
 ZDOT =      19633
802174                 ZDOT =        5961
182497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21066400
78                 X    =         6421038
96
 Y    =        6653467
99  feet           Y    =         2027977
04  meter
 Z    =       -2521255
23                 Z    =         -768478
59
 XDOT =      -2165
626591                 XDOT =        -660
082985
 YDOT =      14108
218849  feet/sec       YDOT =        4300
185105  meter/sec
 ZDOT =      19538
228203                 ZDOT =        5955
251956


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   12171
50148592  
00016717  00000-0  10270-3 0  9047
2 25544  51
6361 110
8200 0010412  80
4570 279
7760 15
56473397 18375


Satellite: ISS
Catalog Number: 25544
Epoch time:      12171
50148592   =   yrday
fracday
Element set:     904
Inclination:       51
6361  deg
RA of node:       110
8200  deg
Eccentricity:     
0010412     
Arg of perigee:    80
4570  deg
Mean anomaly:     279
7760  deg
Mean motion:   15
56473397  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1837
Checksum:              296


Coasting Arc #6 (Orbit 1852)
---------------------------------------

Vector Time (GMT): 2012/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923792
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2986796
84                 A    =         6781124
74  meter
 Y    =       -5826123
13  meter          E    =           
0015755
 Z    =       -1766933
77                 I    =           51
98975
 XDOT =       3654
976544                 Wp   =          108
00758
 YDOT =       3589
527837  meter/sec      RA   =          104
96530  deg
 ZDOT =      -5703
807327                 TA   =           91
30362
                                          MA   =           91
12312
                                          Ha   =            221
084  n
mi
                                          Hp   =            207
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9799202
23                 X    =         3060307
08
 Y    =      -19114577
20  feet           Y    =        -5792311
60  meter
 Z    =       -5797026
80                 Z    =        -1752246
53
 XDOT =      11991
392860                 XDOT =        3642
273743
 YDOT =      11776
666132  feet/sec       YDOT =        3630
329982  meter/sec
 ZDOT =     -18713
278631                 ZDOT =       -5686
081942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18814475
25                 X    =        -5734652
06
 Y    =      -10397683
38  feet           Y    =        -3169213
89  meter
 Z    =       -5735908
58                 Z    =        -1748304
93
 XDOT =      11371
531438                 XDOT =        3466
042782
 YDOT =     -10378
303136  feet/sec       YDOT =       -3163
306796  meter/sec
 ZDOT =     -18640
561107                 ZDOT =       -5681
643025


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   12172
52875558  
00016717  00000-0  10270-3 0  9050
2 25544  51
6374 105
6796 0010389  84
1698 276
0640 15
56504315 18536


Satellite: ISS
Catalog Number: 25544
Epoch time:      12172
52875558   =   yrday
fracday
Element set:     905
Inclination:       51
6374  deg
RA of node:       105
6796  deg
Eccentricity:     
0010389     
Arg of perigee:    84
1698  deg
Mean anomaly:     276
0640  deg
Mean motion:   15
56504315  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1853
Checksum:              330


Coasting Arc #7 (Orbit 1853)
---------------------------------------

Vector Time (GMT): 2012/172/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3516598
18                 A    =         6773481
97  meter
 Y    =        2607005
70  meter          E    =           
0020581
 Z    =       -5186912
98                 I    =           51
95814
 XDOT =      -2970
300966                 Wp   =           95
45984
 YDOT =       6903
390399  meter/sec      RA   =          104
54323  deg
 ZDOT =       1459
001055                 TA   =          188
52650
                                          MA   =          188
56152
                                          Ha   =            221
082  n
mi
                                          Hp   =            209
757

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11537395
61                 X    =         3512381
48
 Y    =        8553168
31  feet           Y    =         2646307
77  meter
 Z    =      -17017431
04                 Z    =        -5169839
39
 XDOT =      -9745
081909                 XDOT =       -3054
362792
 YDOT =      22648
918631  feet/sec       YDOT =        6869
704394  meter/sec
 ZDOT =       4786
748867                 ZDOT =        1444
368505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2349353
38                 X    =          716082
91
 Y    =      -14252388
60  feet           Y    =        -4344128
05  meter
 Z    =      -16947303
70                 Z    =        -5165538
17
 XDOT =      23580
220648                 XDOT =        7187
251254
 YDOT =      -1720
372256  feet/sec       YDOT =        -524
369464  meter/sec
 ZDOT =       4725
749138                 ZDOT =        1440
408337


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   12172
59296120  
00016717  00000-0  10270-3 0  9060
2 25544  51
6386 105
3594 0006972  84
2154 275
9794 15
55697892 18544


Satellite: ISS
Catalog Number: 25544
Epoch time:      12172
59296120   =   yrday
fracday
Element set:     906
Inclination:       51
6386  deg
RA of node:       105
3594  deg
Eccentricity:     
0006972     
Arg of perigee:    84
2154  deg
Mean anomaly:     275
9794  deg
Mean motion:   15
55697892  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1854
Checksum:              348


Coasting Arc #8 (Orbit 1869)
---------------------------------------

Vector Time (GMT): 2012/173/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2525390
31                 A    =         6777303
48  meter
 Y    =       -4687670
81  meter          E    =           
0017179
 Z    =        4180247
03                 I    =           51
97773
 XDOT =       3891
304714                 Wp   =           80
30520
 YDOT =      -5454
183120  meter/sec      RA   =           99
55641  deg
 ZDOT =      -3749
537627                 TA   =           48
07848
                                          MA   =           47
93213
                                          Ha   =            221
110  n
mi
                                          Hp   =            209
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8285401
27                 X    =        -2493090
66
 Y    =      -15379497
41  feet           Y    =        -4715731
35  meter
 Z    =       13714721
23                 Z    =         4168056
61
 XDOT =      12766
747749                 XDOT =        3970
219561
 YDOT =     -17894
301575  feet/sec       YDOT =       -5410
226318  meter/sec
 ZDOT =     -12301
632635                 ZDOT =       -3730
443154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9667860
88                 X    =        -2946764
00
 Y    =       14597005
50  feet           Y    =         4449167
28  meter
 Z    =       13664929
19                 Z    =         4165070
42
 XDOT =     -20761
040593                 XDOT =       -6327
965173
 YDOT =      -2259
557208  feet/sec       YDOT =        -688
713037  meter/sec
 ZDOT =     -12222
369120                 ZDOT =       -3725
378108


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   12173
62074933  
00016717  00000-0  10270-3 0  9072
2 25544  51
6384 100
2231 0006973  87
6335 272
5616 15
55726248 18705


Satellite: ISS
Catalog Number: 25544
Epoch time:      12173
62074933   =   yrday
fracday
Element set:     907
Inclination:       51
6384  deg
RA of node:       100
2231  deg
Eccentricity:     
0006973     
Arg of perigee:    87
6335  deg
Mean anomaly:     272
5616  deg
Mean motion:   15
55726248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1870
Checksum:              311


Coasting Arc #9 (Orbit 1884)
---------------------------------------

Vector Time (GMT): 2012/174/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1446447
72                 A    =         6782021
98  meter
 Y    =        6148084
81  meter          E    =           
0011450
 Z    =       -2474510
05                 I    =           51
99861
 XDOT =      -4455
116284                 Wp   =           72
62244
 YDOT =       3194
654336  meter/sec      RA   =           94
58606  deg
 ZDOT =       5356
824813                 TA   =          259
80100
                                          MA   =          259
93015
                                          Ha   =            220
979  n
mi
                                          Hp   =            209
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4745563
39                 X    =         1389611
57
 Y    =       20170881
93  feet           Y    =         6163942
44  meter
 Z    =       -8118471
30                 Z    =        -2467620
53
 XDOT =     -14616
523240                 XDOT =       -4516
530445
 YDOT =      10481
149395  feet/sec       YDOT =        3144
490334  meter/sec
 ZDOT =      17574
884556                 ZDOT =        5335
033531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15337747
44                 X    =         4674945
42
 Y    =      -13949508
75  feet           Y    =        -4251810
27  meter
 Z    =       -8090681
99                 Z    =        -2466039
87
 XDOT =      15277
117844                 XDOT =        4656
465519
 YDOT =       6701
604367  feet/sec       YDOT =        2042
649011  meter/sec
 ZDOT =      17484
717967                 ZDOT =        5329
342036


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   12174
58428617  
00016717  00000-0  10270-3 0  9081
2 25544  51
6391  95
4075 0006885  91
3795 268
8147 15
55752946 18855


Satellite: ISS
Catalog Number: 25544
Epoch time:      12174
58428617   =   yrday
fracday
Element set:     908
Inclination:       51
6391  deg
RA of node:        95
4075  deg
Eccentricity:     
0006885     
Arg of perigee:    91
3795  deg
Mean anomaly:     268
8147  deg
Mean motion:   15
55752946  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1885
Checksum:              360


Coasting Arc #10 (Orbit 1900)
---------------------------------------

Vector Time (GMT): 2012/175/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -251831
36                 A    =         6784654
80  meter
 Y    =       -6767942
89  meter          E    =           
0018604
 Z    =         266504
66                 I    =           52
00845
 XDOT =       4713
896377                 Wp   =          119
57588
 YDOT =       -425
244785  meter/sec      RA   =           89
63027  deg
 ZDOT =      -6038
735212                 TA   =           57
56434
                                          MA   =           57
38455
                                          Ha   =            220
997  n
mi
                                          Hp   =            209
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -826218
37                 X    =         -177426
73
 Y    =      -22204537
06  feet           Y    =        -6770343
04  meter
 Z    =         874359
12                 Z    =          265461
20
 XDOT =      15465
539295                 XDOT =        4747
635726
 YDOT =      -1395
160057  feet/sec       YDOT =        -372
341702  meter/sec
 ZDOT =     -19812
123399                 ZDOT =       -6015
753637

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18834612
70                 X    =        -5740789
95
 Y    =       11789307
92  feet           Y    =         3593381
05  meter
 Z    =         870740
85                 Z    =          265401
81
 XDOT =      -8120
218535                 XDOT =       -2475
042609
 YDOT =     -11442
099499  feet/sec       YDOT =       -3487
551927  meter/sec
 ZDOT =     -19717
321328                 ZDOT =       -6009
839541


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   12175
61204487  
00016717  00000-0  10270-3 0  9094
2 25544  51
6390  90
2707 0006850  96
4403 263
7531 15
55728380 19018


Satellite: ISS
Catalog Number: 25544
Epoch time:      12175
61204487   =   yrday
fracday
Element set:     909
Inclination:       51
6390  deg
RA of node:        90
2707  deg
Eccentricity:     
0006850     
Arg of perigee:    96
4403  deg
Mean anomaly:     263
7531  deg
Mean motion:   15
55728380  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1901
Checksum:              306


Coasting Arc #11 (Orbit 1916)
---------------------------------------

Vector Time (GMT): 2012/176/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -920182
17                 A    =         6782958
16  meter
 Y    =        6427209
85  meter          E    =           
0020074
 Z    =        1936206
95                 I    =           52
00187
 XDOT =      -4640
599890                 Wp   =           77
12227
 YDOT =      -2374
592323  meter/sec      RA   =           84
67554  deg
 ZDOT =       5632
410133                 TA   =          304
14037
                                          MA   =          304
33060
                                          Ha   =            220
882  n
mi
                                          Hp   =            209
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3018970
37                 X    =        -1001389
73
 Y    =       21086646
49  feet           Y    =         6416465
55  meter
 Z    =        6352385
01                 Z    =         1931540
20
 XDOT =     -15225
065256                 XDOT =       -4641
062555
 YDOT =      -7790
657229  feet/sec       YDOT =       -2426
489554  meter/sec
 ZDOT =      18479
035868                 ZDOT =        5609
865128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19666451
87                 X    =         5994334
53
 Y    =       -8200239
16  feet           Y    =        -2499432
90  meter
 Z    =        6332486
55                 Z    =         1930141
90
 XDOT =        590
104093                 XDOT =         179
863727
 YDOT =      15727
006533  feet/sec       YDOT =        4793
591591  meter/sec
 ZDOT =      18386
315790                 ZDOT =        5604
149053


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   12176
63978651  
00016717  00000-0  10270-3 0  9100
2 25544  51
6388  85
1336 0006742  97
9948 262
1971 15
55779311 19174


Satellite: ISS
Catalog Number: 25544
Epoch time:      12176
63978651   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:        85
1336  deg
Eccentricity:     
0006742     
Arg of perigee:    97
9948  deg
Mean anomaly:     262
1971  deg
Mean motion:   15
55779311  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1917
Checksum:              348


Coasting Arc #12 (Orbit 1931)
---------------------------------------

Vector Time (GMT): 2012/177/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2122953
25                 A    =         6778234
29  meter
 Y    =       -5165388
66  meter          E    =           
0012408
 Z    =       -3852207
47                 I    =           51
98220
 XDOT =       4207
051504                 Wp   =           89
22103
 YDOT =       4843
752620  meter/sec      RA   =           79
70881  deg
 ZDOT =      -4187
885539                 TA   =          136
89387
                                          MA   =          136
79664
                                          Ha   =            220
764  n
mi
                                          Hp   =            209
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6965069
71                 X    =         2199268
95
 Y    =      -16946813
18  feet           Y    =        -5141221
42  meter
 Z    =      -12638475
96                 Z    =        -3841709
42
 XDOT =      13802
662415                 XDOT =        4172
918679
 YDOT =      15891
576836  feet/sec       YDOT =        4890
608011  meter/sec
 ZDOT =     -13739
781952                 ZDOT =       -4167
530451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18110866
59                 X    =        -5520192
14
 Y    =        2967983
19  feet           Y    =          904641
28  meter
 Z    =      -12594655
01                 Z    =        -3838850
85
 XDOT =       6379
526547                 XDOT =        1944
479691
 YDOT =     -18862
439444  feet/sec       YDOT =       -5749
271543  meter/sec
 ZDOT =     -13656
347346                 ZDOT =       -4162
454671


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   12177
60328016  
00016717  00000-0  10270-3 0  9113
2 25544  51
6385  80
3175 0006537 102
5631 257
6254 15
55795502 19323


Satellite: ISS
Catalog Number: 25544
Epoch time:      12177
60328016   =   yrday
fracday
Element set:     911
Inclination:       51
6385  deg
RA of node:        80
3175  deg
Eccentricity:     
0006537     
Arg of perigee:   102
5631  deg
Mean anomaly:     257
6254  deg
Mean motion:   15
55795502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1932
Checksum:              300


Coasting Arc #13 (Orbit 1947)
---------------------------------------

Vector Time (GMT): 2012/178/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3199527
36                 A    =         6773736
13  meter
 Y    =        3209939
28  meter          E    =           
0012398
 Z    =        5025935
09                 I    =           51
96102
 XDOT =      -3424
137089                 Wp   =          113
87716
 YDOT =      -6572
018945  meter/sec      RA   =           74
72401  deg
 ZDOT =       2008
779810                 TA   =          316
67249
                                          MA   =          316
76991
                                          Ha   =            220
859  n
mi
                                          Hp   =            209
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10497137
02                 X    =        -3259598
58
 Y    =       10531296
84  feet           Y    =         3173823
86  meter
 Z    =       16489288
34                 Z    =         5010246
32
 XDOT =     -11234
045566                 XDOT =       -3360
151118
 YDOT =     -21561
741947  feet/sec       YDOT =       -6609
952180  meter/sec
 ZDOT =       6590
484941                 ZDOT =        1992
300376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14597056
31                 X    =         4449182
76
 Y    =        3188157
34  feet           Y    =          971750
36  meter
 Z    =       16424260
37                 Z    =         5006114
56
 XDOT =     -11763
242996                 XDOT =       -3585
436465
 YDOT =      20103
871007  feet/sec       YDOT =        6127
659883  meter/sec
 ZDOT =       6523
218170                 ZDOT =        1988
276898


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   12178
63099327  
00016717  00000-0  10270-3 0  9128
2 25544  51
6386  75
1802 0006680 105
5875 254
6016 15
55820043 19484


Satellite: ISS
Catalog Number: 25544
Epoch time:      12178
63099327   =   yrday
fracday
Element set:     912
Inclination:       51
6386  deg
RA of node:        75
1802  deg
Eccentricity:     
0006680     
Arg of perigee:   105
5875  deg
Mean anomaly:     254
6016  deg
Mean motion:   15
55820043  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1948
Checksum:              316


Coasting Arc #14 (Orbit 1962)
---------------------------------------

Vector Time (GMT): 2012/179/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4126677
82                 A    =         6772411
05  meter
 Y    =        -848073
92  meter          E    =           
0021059
 Z    =       -5320702
46                 I    =           51
94724
 XDOT =       2227
947892                 Wp   =           98
83132
 YDOT =       7302
683738  meter/sec      RA   =           69
72629  deg
 ZDOT =        562
740629                 TA   =          176
53223
                                          MA   =          176
51761
                                          Ha   =            220
587  n
mi
                                          Hp   =            209
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13538969
24                 X    =         4161701
28
 Y    =       -2782394
74  feet           Y    =         -801730
51  meter
 Z    =      -17456372
91                 Z    =        -5300570
21
 XDOT =       7309
540329                 XDOT =        2143
388528
 YDOT =      23958
936147  feet/sec       YDOT =        7327
125180  meter/sec
 ZDOT =       1846
261907                 ZDOT =         573
359230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9910977
34                 X    =        -3020865
89
 Y    =       -9783275
36  feet           Y    =        -2981942
33  meter
 Z    =      -17373267
26                 Z    =        -5295371
86
 XDOT =      15122
118473                 XDOT =        4609
221710
 YDOT =     -18681
801300  feet/sec       YDOT =       -5694
213036  meter/sec
 ZDOT =       1889
273046                 ZDOT =         575
850425


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   12179
59445889  
00016717  00000-0  10270-3 0  9133
2 25544  51
6379  70
3630 0006494 109
3063 250
8794 15
55868682 19635


Satellite: ISS
Catalog Number: 25544
Epoch time:      12179
59445889   =   yrday
fracday
Element set:     913
Inclination:       51
6379  deg
RA of node:        70
3630  deg
Eccentricity:     
0006494     
Arg of perigee:   109
3063  deg
Mean anomaly:     250
8794  deg
Mean motion:   15
55868682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1963
Checksum:              352


Coasting Arc #15 (Orbit 1978)
---------------------------------------

Vector Time (GMT): 2012/180/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4713731
39                 A    =         6775225
14  meter
 Y    =       -1541985
18  meter          E    =           
0013684
 Z    =        4604697
09                 I    =           51
94618
 XDOT =       -681
774200                 Wp   =           85
66151
 YDOT =      -7018
648547  meter/sec      RA   =           64
73248  deg
 ZDOT =      -3039
517325                 TA   =           34
56062
                                          MA   =           34
47174
                                          Ha   =            220
578  n
mi
                                          Hp   =            209
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15464998
00                 X    =        -4718506
94
 Y    =       -5059006
51  feet           Y    =        -1594724
28  meter
 Z    =       15107273
92                 Z    =         4581786
11
 XDOT =      -2236
791994                 XDOT =        -588
474206
 YDOT =     -23027
062162  feet/sec       YDOT =       -7025
750552  meter/sec
 ZDOT =      -9972
169700                 ZDOT =       -3042
603546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4732619
38                 X    =         1442502
39
 Y    =       15658946
23  feet           Y    =         4772846
81  meter
 Z    =       15012966
13                 Z    =         4575952
08
 XDOT =     -16518
349635                 XDOT =       -5034
792969
 YDOT =      14592
317955  feet/sec       YDOT =        4447
738513  meter/sec
 ZDOT =      -9984
137534                 ZDOT =       -3043
165120


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   12180
62214109  
00016717  00000-0  10270-3 0  9149
2 25544  51
6384  65
2259 0006336 113
1635 247
0187 15
55912190 19799


Satellite: ISS
Catalog Number: 25544
Epoch time:      12180
62214109   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:        65
2259  deg
Eccentricity:     
0006336     
Arg of perigee:   113
1635  deg
Mean anomaly:     247
0187  deg
Mean motion:   15
55912190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1979
Checksum:              302


Coasting Arc #16 (Orbit 1993)
---------------------------------------

Vector Time (GMT): 2012/181/13:54:15
850
Vector Time (MET): N/A
Weight (LBS)     : 923384
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4873133
02                 A    =         6780258
51  meter
 Y    =        3586512
38  meter          E    =           
0010042
 Z    =       -3069968
67                 I    =           51
94797
 XDOT =      -1125
261208                 Wp   =           98
23318
 YDOT =       5747
351110  meter/sec      RA   =           59
75228  deg
 ZDOT =       4940
576240                 TA   =          226
69524
                                          MA   =          226
77902
                                          Ha   =            220
450  n
mi
                                          Hp   =            209
831

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15987969
23                 X    =         4847579
01
 Y    =       11766772
90  feet           Y    =         3640864
32  meter
 Z    =      -10072075
68                 Z    =        -3046356
65
 XDOT =      -3691
801865                 XDOT =       -1213
445961
 YDOT =      18856
138813  feet/sec       YDOT =        5734
273987  meter/sec
 ZDOT =      16209
239633                 ZDOT =        4934
896341

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         150490
44                 X    =           45869
49
 Y    =      -19899584
65  feet           Y    =        -6065393
40  meter
 Z    =       -9975103
84                 Z    =        -3040411
65
 XDOT =      16058
835493                 XDOT =        4894
733058
 YDOT =      -7971
171419  feet/sec       YDOT =       -2429
613049  meter/sec
 ZDOT =      16185
185033                 ZDOT =        4933
244398


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   12181
58558150  
00016717  00000-0  10270-3 0  9153
2 25544  51
6374  60
4090 0006356 117
2842 242
8959 15
55899300 19949


Satellite: ISS
Catalog Number: 25544
Epoch time:      12181
58558150   =   yrday
fracday
Element set:     915
Inclination:       51
6374  deg
RA of node:        60
4090  deg
Eccentricity:     
0006356     
Arg of perigee:   117
2842  deg
Mean anomaly:     242
8959  deg
Mean motion:   15
55899300  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1994
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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