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

 
Date: July 29th 2011

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) : 104 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


There are no maneuvers



Coasting Arc #1 (Orbit 720)
---------------------------------------

Vector Time (GMT): 2011/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4956673
14                 A    =         6762566
43  meter
 Y    =         388147
66  meter          E    =           
0012431
 Z    =        4571794
60                 I    =           51
39895
 XDOT =      -3260
081770                 Wp   =           49
51068
 YDOT =       6279
698953  meter/sec      RA   =          317
24773  deg
 ZDOT =       3003
952768                 TA   =           10
49885
                                          MA   =           10
47292
                                          Ha   =            214
447  n
mi
                                          Hp   =            203
150

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16262050
98                 X    =         4929755
81
 Y    =        1273450
34  feet           Y    =          443425
10  meter
 Z    =       14999326
13                 Z    =         4595808
41
 XDOT =     -10695
806332                 XDOT =       -3344
652708
 YDOT =      20602
686854  feet/sec       YDOT =        6242
769479  meter/sec
 ZDOT =       9855
488084                 ZDOT =        2987
910945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7994482
62                 X    =        -2436718
30
 Y    =      -14114873
71  feet           Y    =        -4302213
51  meter
 Z    =       15096832
45                 Z    =         4601514
53
 XDOT =      22064
146821                 XDOT =        6725
151951
 YDOT =      -2034
786900  feet/sec       YDOT =        -620
203047  meter/sec
 ZDOT =       9789
941647                 ZDOT =        2983
974214


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   11208
55334818  
00016717  00000-0  10270-3 0  9006
2 25544  51
6417 317
5435 0011692   9
4538 350
6836 15
60231764  7218


Satellite: ISS
Catalog Number: 25544
Epoch time:      11208
55334818   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:       317
5435  deg
Eccentricity:     
0011692     
Arg of perigee:     9
4538  deg
Mean anomaly:     350
6836  deg
Mean motion:   15
60231764  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             721
Checksum:              298


Coasting Arc #2 (Orbit 735)
---------------------------------------

Vector Time (GMT): 2011/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2265582
49                 A    =         6760028
82  meter
 Y    =       -3692238
18  meter          E    =           
0019300
 Z    =       -5202674
46                 I    =           51
36894
 XDOT =       5703
925760                 Wp   =           60
46026
 YDOT =      -5008
285216  meter/sec      RA   =          312
16949  deg
 ZDOT =       1082
790336                 TA   =          219
88367
                                          MA   =          220
02564
                                          Ha   =            214
694  n
mi
                                          Hp   =            202
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7433013
41                 X    =        -2198853
65
 Y    =      -12113642
33  feet           Y    =        -3717199
56  meter
 Z    =      -17069141
92                 Z    =        -5213518
81
 XDOT =      18713
667193                 XDOT =        5754
245558
 YDOT =     -16431
381941  feet/sec       YDOT =       -4944
219226  meter/sec
 ZDOT =       3552
461733                 ZDOT =        1110
621040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5715246
46                 X    =        -1742007
12
 Y    =       12954851
47  feet           Y    =         3948638
73  meter
 Z    =      -17112960
18                 Z    =        -5216030
26
 XDOT =     -23238
024690                 XDOT =       -7082
949926
 YDOT =      -5462
877265  feet/sec       YDOT =       -1665
084990  meter/sec
 ZDOT =       3665
806678                 ZDOT =        1117
337875


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   11209
51411855  
00016717  00000-0  10270-3 0  9011
2 25544  51
6418 312
7111 0011866  13
2522 346
8943 15
60238813  7360


Satellite: ISS
Catalog Number: 25544
Epoch time:      11209
51411855   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:       312
7111  deg
Eccentricity:     
0011866     
Arg of perigee:    13
2522  deg
Mean anomaly:     346
8943  deg
Mean motion:   15
60238813  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             736
Checksum:              285


Coasting Arc #3 (Orbit 751)
---------------------------------------

Vector Time (GMT): 2011/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1078391
12                 A    =         6767029
48  meter
 Y    =        5804205
58  meter          E    =           
0019540
 Z    =        3305570
00                 I    =           51
37246
 XDOT =      -5880
422830                 Wp   =           55
71874
 YDOT =       1585
659909  meter/sec      RA   =          307
10400  deg
 ZDOT =      -4672
031166                 TA   =           85
57140
                                          MA   =           85
34818
                                          Ha   =            214
882  n
mi
                                          Hp   =            202
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3538028
61                 X    =        -1159272
19
 Y    =       19042669
22  feet           Y    =         5791693
76  meter
 Z    =       10845045
92                 Z    =         3300135
48
 XDOT =     -19292
725821                 XDOT =       -5875
021618
 YDOT =       5202
296290  feet/sec       YDOT =        1519
932146  meter/sec
 ZDOT =     -15328
186241                 ZDOT =       -4700
584270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17523753
26                 X    =         5341239
99
 Y    =       -8279178
21  feet           Y    =        -2523493
52  meter
 Z    =       10822624
38                 Z    =         3298735
91
 XDOT =      14890
630044                 XDOT =        4538
664037
 YDOT =      11197
174026  feet/sec       YDOT =        3412
898643  meter/sec
 ZDOT =     -15444
256606                 ZDOT =       -4707
409413


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   11210
53892853  
00016717  00000-0  10270-3 0  9027
2 25544  51
6416 307
5550 0011871  17
4396 342
7165 15
60222901  7528


Satellite: ISS
Catalog Number: 25544
Epoch time:      11210
53892853   =   yrday
fracday
Element set:     902
Inclination:       51
6416  deg
RA of node:       307
5550  deg
Eccentricity:     
0011871     
Arg of perigee:    17
4396  deg
Mean anomaly:     342
7165  deg
Mean motion:   15
60222901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             752
Checksum:              289


Coasting Arc #4 (Orbit 767)
---------------------------------------

Vector Time (GMT): 2011/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3687947
38                 A    =         6771638
29  meter
 Y    =       -5660979
24  meter          E    =           
0023892
 Z    =         148005
50                 I    =           51
37109
 XDOT =       3945
089425                 Wp   =           33
72507
 YDOT =       2738
686194  meter/sec      RA   =          302
07991  deg
 ZDOT =       6003
166995                 TA   =          327
88142
                                          MA   =          328
02676
                                          Ha   =            214
970  n
mi
                                          Hp   =            202
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12099564
89                 X    =         3750256
49
 Y    =      -18572766
52  feet           Y    =        -5619389
99  meter
 Z    =         485582
36                 Z    =          166071
93
 XDOT =      12943
206775                 XDOT =        3885
010189
 YDOT =       8985
190924  feet/sec       YDOT =        2782
466160  meter/sec
 ZDOT =      19695
429772                 ZDOT =        6022
186024

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22112958
06                 X    =        -6740029
62
 Y    =        1512346
76  feet           Y    =          460963
29  meter
 Z    =         559294
50                 Z    =          170472
96
 XDOT =       -427
904334                 XDOT =        -130
425241
 YDOT =     -14037
669603  feet/sec       YDOT =       -4278
681695  meter/sec
 ZDOT =      19772
523468                 ZDOT =        6026
665153


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   11211
56372598  
00016717  00000-0  10270-3 0  9031
2 25544  51
6420 302
3992 0012075  20
6414 339
5227 15
60234231  7689


Satellite: ISS
Catalog Number: 25544
Epoch time:      11211
56372598   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:       302
3992  deg
Eccentricity:     
0012075     
Arg of perigee:    20
6414  deg
Mean anomaly:     339
5227  deg
Mean motion:   15
60234231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             768
Checksum:              284


Coasting Arc #5 (Orbit 782)
---------------------------------------

Vector Time (GMT): 2011/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4819423
02                 A    =         6766025
57  meter
 Y    =        3149532
38  meter          E    =           
0015507
 Z    =       -3574179
07                 I    =           51
33649
 XDOT =       -789
582034                 Wp   =           41
03810
 YDOT =      -6215
989906  meter/sec      RA   =          297
05228  deg
 ZDOT =      -4412
225948                 TA   =          181
45355
                                          MA   =          181
45806
                                          Ha   =            215
010  n
mi
                                          Hp   =            202
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15811755
30                 X    =        -4836921
27
 Y    =       10333111
47  feet           Y    =         3095541
02  meter
 Z    =      -11726309
28                 Z    =        -3597633
51
 XDOT =      -2590
492237                 XDOT =        -698
581734
 YDOT =     -20393
667671  feet/sec       YDOT =       -6224
310430  meter/sec
 ZDOT =     -14475
806917                 ZDOT =       -4415
840957

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17830500
58                 X    =         5434736
58
 Y    =        6050657
31  feet           Y    =         1844240
35  meter
 Z    =      -11821756
34                 Z    =        -3603271
33
 XDOT =     -14095
081314                 XDOT =       -4296
180785
 YDOT =      13221
934935  feet/sec       YDOT =        4030
045768  meter/sec
 ZDOT =     -14490
142603                 ZDOT =       -4416
595465


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   11212
52446223  
00016717  00000-0  10270-3 0  9046
2 25544  51
6409 297
5659 0011966  24
2163 335
9553 15
60262542  7835


Satellite: ISS
Catalog Number: 25544
Epoch time:      11212
52446223   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:       297
5659  deg
Eccentricity:     
0011966     
Arg of perigee:    24
2163  deg
Mean anomaly:     335
9553  deg
Mean motion:   15
60262542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             783
Checksum:              305


Coasting Arc #6 (Orbit 798)
---------------------------------------

Vector Time (GMT): 2011/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4181182
84                 A    =         6759528
45  meter
 Y    =         845996
10  meter          E    =           
0012431
 Z    =        5235356
80                 I    =           51
30252
 XDOT =      -2338
486584                 Wp   =           41
22776
 YDOT =       7288
465109  meter/sec      RA   =          291
97857  deg
 ZDOT =        698
114605                 TA   =           42
13695
                                          MA   =           42
04144
                                          Ha   =            214
897  n
mi
                                          Hp   =            202
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13717791
46                 X    =         4145980
21
 Y    =        2775577
75  feet           Y    =          892555
63  meter
 Z    =       17176367
46                 Z    =         5255583
00
 XDOT =      -7672
200080                 XDOT =       -2423
205045
 YDOT =      23912
287102  feet/sec       YDOT =        7261
841016  meter/sec
 ZDOT =       2290
402246                 ZDOT =         686
548992

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6401365
87                 X    =        -1951136
32
 Y    =      -12331935
00  feet           Y    =        -3758773
79  meter
 Z    =       17258479
87                 Z    =         5260384
66
 XDOT =      22527
369246                 XDOT =        6866
342146
 YDOT =      -8592
343179  feet/sec       YDOT =       -2618
946201  meter/sec
 ZDOT =       2243
029352                 ZDOT =         683
675346


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   11213
54923547  
00016717  00000-0  10270-3 0  9059
2 25544  51
6410 292
4092 0012019  27
5632 332
6159 15
60317729  7990


Satellite: ISS
Catalog Number: 25544
Epoch time:      11213
54923547   =   yrday
fracday
Element set:     905
Inclination:       51
6410  deg
RA of node:       292
4092  deg
Eccentricity:     
0012019     
Arg of perigee:    27
5632  deg
Mean anomaly:     332
6159  deg
Mean motion:   15
60317729  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             799
Checksum:              303


Coasting Arc #7 (Orbit 813)
---------------------------------------

Vector Time (GMT): 2011/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2261513
02                 A    =         6763112
15  meter
 Y    =       -4635677
76  meter          E    =           
0016536
 Z    =       -4383097
13                 I    =           51
30307
 XDOT =       4414
776841                 Wp   =           64
07322
 YDOT =      -5304
177801  meter/sec      RA   =          286
89528  deg
 ZDOT =       3348
932113                 TA   =          239
85865
                                          MA   =          240
02262
                                          Ha   =            215
111  n
mi
                                          Hp   =            201
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7419662
15                 X    =        -2188216
05
 Y    =      -15208916
53  feet           Y    =        -4660557
47  meter
 Z    =      -14380239
94                 Z    =        -4393905
38
 XDOT =      14484
175986                 XDOT =        4457
492908
 YDOT =     -17402
158139  feet/sec       YDOT =       -5254
570296  meter/sec
 ZDOT =      10987
310082                 ZDOT =        3370
482305

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6952328
00                 X    =        -2119069
58
 Y    =       15387334
72  feet           Y    =         4690059
62  meter
 Z    =      -14423900
11                 Z    =        -4396404
75
 XDOT =     -21476
053673                 XDOT =       -6545
901160
 YDOT =        626
360768  feet/sec       YDOT =         190
914762  meter/sec
 ZDOT =      11075
123093                 ZDOT =        3375
697519


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   11214
50995232  
00016717  00000-0  10270-3 0  9067
2 25544  51
6398 287
5761 0012204  31
7037 328
4851 15
60328910  8149


Satellite: ISS
Catalog Number: 25544
Epoch time:      11214
50995232   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       287
5761  deg
Eccentricity:     
0012204     
Arg of perigee:    31
7037  deg
Mean anomaly:     328
4851  deg
Mean motion:   15
60328910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             814
Checksum:              300


Coasting Arc #8 (Orbit 829)
---------------------------------------

Vector Time (GMT): 2011/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -289345
28                 A    =         6770570
58  meter
 Y    =        6627789
51  meter          E    =           
0019324
 Z    =        1346401
87                 I    =           51
32009
 XDOT =      -4941
176368                 Wp   =           80
47768
 YDOT =        975
621332  meter/sec      RA   =          281
85050  deg
 ZDOT =      -5790
223304                 TA   =           84
76155
                                          MA   =           84
54107
                                          Ha   =            215
261  n
mi
                                          Hp   =            201
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -949295
53                 X    =         -369977
47
 Y    =       21744716
24  feet           Y    =         6624103
02  meter
 Z    =        4417328
98                 Z    =         1344800
50
 XDOT =     -16211
208557                 XDOT =       -4923
591317
 YDOT =       3200
857389  feet/sec       YDOT =         920
464488  meter/sec
 ZDOT =     -18996
795617                 ZDOT =       -5814
184420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17067583
77                 X    =         5202199
53
 Y    =      -13508953
74  feet           Y    =        -4117529
10  meter
 Z    =        4410486
89                 Z    =         1344316
40
 XDOT =      11978
152053                 XDOT =        3650
940746
 YDOT =       8819
901723  feet/sec       YDOT =        2688
306045  meter/sec
 ZDOT =     -19094
173441                 ZDOT =       -5819
904065


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   11215
53470465  
00016717  00000-0  10270-3 0  9078
2 25544  51
6395 282
4188 0012348  35
0496 325
1470 15
60336985  8308


Satellite: ISS
Catalog Number: 25544
Epoch time:      11215
53470465   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:       282
4188  deg
Eccentricity:     
0012348     
Arg of perigee:    35
0496  deg
Mean anomaly:     325
1470  deg
Mean motion:   15
60336985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             830
Checksum:              310


Coasting Arc #9 (Orbit 845)
---------------------------------------

Vector Time (GMT): 2011/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2552261
89                 A    =         6769080
00  meter
 Y    =       -5814956
21  meter          E    =           
0025127
 Z    =        2301100
12                 I    =           51
30955
 XDOT =       3891
784483                 Wp   =           56
72813
 YDOT =       3855
432840  meter/sec      RA   =          276
82729  deg
 ZDOT =       5397
216760                 TA   =          329
15061
                                          MA   =          329
29802
                                          Ha   =            215
301  n
mi
                                          Hp   =            201
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8373562
63                 X    =         2605917
98
 Y    =      -19077940
31  feet           Y    =        -5786115
30  meter
 Z    =        7549541
07                 Z    =         2313629
06
 XDOT =      12768
321794                 XDOT =        3822
164650
 YDOT =      12649
057875  feet/sec       YDOT =        3898
563766  meter/sec
 ZDOT =      17707
404068                 ZDOT =        5415
953799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19759438
48                 X    =        -6022676
85
 Y    =        6547787
91  feet           Y    =         1995765
75  meter
 Z    =        7600723
13                 Z    =         2316700
41
 XDOT =       1431
960017                 XDOT =         436
461413
 YDOT =     -16431
537420  feet/sec       YDOT =       -5008
332605  meter/sec
 ZDOT =      17783
320220                 ZDOT =        5420
356003


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   11216
55944581  
00016717  00000-0  10270-3 0  9087
2 25544  51
6392 277
2620 0012398  39
0247 321
1801 15
60327856  8469


Satellite: ISS
Catalog Number: 25544
Epoch time:      11216
55944581   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:       277
2620  deg
Eccentricity:     
0012398     
Arg of perigee:    39
0247  deg
Mean anomaly:     321
1801  deg
Mean motion:   15
60327856  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             846
Checksum:              310


Coasting Arc #10 (Orbit 860)
---------------------------------------

Vector Time (GMT): 2011/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3982271
66                 A    =         6761171
27  meter
 Y    =        2524634
45  meter          E    =           
0023566
 Z    =       -4867634
38                 I    =           51
28032
 XDOT =      -1650
799307                 Wp   =           57
45418
 YDOT =      -7107
669385  meter/sec      RA   =          271
76860  deg
 ZDOT =      -2331
721844                 TA   =          189
56053
                                          MA   =          189
60546
                                          Ha   =            215
404  n
mi
                                          Hp   =            201
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13065195
74                 X    =        -3986560
78
 Y    =        8282921
43  feet           Y    =         2480078
47  meter
 Z    =      -15969929
06                 Z    =        -4886990
39
 XDOT =      -5416
008225                 XDOT =       -1559
870299
 YDOT =     -23319
125278  feet/sec       YDOT =       -7125
621127  meter/sec
 ZDOT =      -7650
006051                 ZDOT =       -2339
520762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14895343
15                 X    =         4540100
59
 Y    =        3861793
92  feet           Y    =         1177074
79  meter
 Z    =      -16048677
87                 Z    =        -4891637
02
 XDOT =     -13144
735974                 XDOT =       -4006
515525
 YDOT =      18722
089287  feet/sec       YDOT =        5706
492815  meter/sec
 ZDOT =      -7681
335645                 ZDOT =       -2341
271105


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   11217
52013010  
00016717  00000-0  10270-3 0  9090
2 25544  51
6389 272
4270 0012378  42
4245 317
7865 15
60336118  8616


Satellite: ISS
Catalog Number: 25544
Epoch time:      11217
52013010   =   yrday
fracday
Element set:     909
Inclination:       51
6389  deg
RA of node:       272
4270  deg
Eccentricity:     
0012378     
Arg of perigee:    42
4245  deg
Mean anomaly:     317
7865  deg
Mean motion:   15
60336118  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             861
Checksum:              290


Coasting Arc #11 (Orbit 876)
---------------------------------------

Vector Time (GMT): 2011/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4127290
52                 A    =         6760320
71  meter
 Y    =        1885786
82  meter          E    =           
0018000
 Z    =        5002782
70                 I    =           51
27841
 XDOT =      -1077
667502                 Wp   =           48
68717
 YDOT =       7375
160249  meter/sec      RA   =          266
67806  deg
 ZDOT =      -1874
876164                 TA   =           59
62200
                                          MA   =           59
44418
                                          Ha   =            215
270  n
mi
                                          Hp   =            201
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13540979
40                 X    =         4081594
14
 Y    =        6186964
63  feet           Y    =         1931684
90  meter
 Z    =       16413329
07                 Z    =         5022722
01
 XDOT =      -3535
654534                 XDOT =       -1150
950156
 YDOT =      24196
719977  feet/sec       YDOT =        7362
699481  meter/sec
 ZDOT =      -6151
168518                 ZDOT =       -1880
288986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4859126
18                 X    =        -1481061
66
 Y    =      -13977236
28  feet           Y    =        -4260261
62  meter
 Z    =       16494234
89                 Z    =         5027442
79
 XDOT =      18844
430067                 XDOT =        5743
782285
 YDOT =     -13898
437249  feet/sec       YDOT =       -4236
243673  meter/sec
 ZDOT =      -6173
514939                 ZDOT =       -1881
687353


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   11218
54484722  
00016717  00000-0  10270-3 0  9107
2 25544  51
6390 267
2701 0012433  45
6883 314
5291 15
60401766  8771


Satellite: ISS
Catalog Number: 25544
Epoch time:      11218
54484722   =   yrday
fracday
Element set:     910
Inclination:       51
6390  deg
RA of node:       267
2701  deg
Eccentricity:     
0012433     
Arg of perigee:    45
6883  deg
Mean anomaly:     314
5291  deg
Mean motion:   15
60401766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             877
Checksum:              302


Coasting Arc #12 (Orbit 891)
---------------------------------------

Vector Time (GMT): 2011/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2996675
85                 A    =         6767936
54  meter
 Y    =       -5426114
15  meter          E    =           
0017392
 Z    =       -2713383
11                 I    =           51
30695
 XDOT =       3503
557842                 Wp   =           52
06691
 YDOT =      -4491
333510  meter/sec      RA   =          261
61405  deg
 ZDOT =       5145
273210                 TA   =          277
01755
                                          MA   =          277
21532
                                          Ha   =            215
437  n
mi
                                          Hp   =            200
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9831613
68                 X    =        -2922596
29
 Y    =      -17802211
77  feet           Y    =        -5459210
39  meter
 Z    =       -8902175
56                 Z    =        -2727761
29
 XDOT =      11494
612342                 XDOT =        3528
525882
 YDOT =     -14735
346160  feet/sec       YDOT =       -4452
015391  meter/sec
 ZDOT =      16880
817619                 ZDOT =        5162
353602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5717411
38                 X    =        -1742666
99
 Y    =       19489788
57  feet           Y    =         5940487
56  meter
 Z    =       -8960326
41                 Z    =        -2731107
49
 XDOT =     -17058
750155                 XDOT =       -5199
507047
 YDOT =       2739
105071  feet/sec       YDOT =         834
879226  meter/sec
 ZDOT =      16950
421347                 ZDOT =        5166
488427


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   11219
50551210  
00016717  00000-0  10270-3 0  9112
2 25544  51
6391 262
4355 0012596  49
9654 310
2605 15
60409623  8926


Satellite: ISS
Catalog Number: 25544
Epoch time:      11219
50551210   =   yrday
fracday
Element set:     911
Inclination:       51
6391  deg
RA of node:       262
4355  deg
Eccentricity:     
0012596     
Arg of perigee:    49
9654  deg
Mean anomaly:     310
2605  deg
Mean motion:   15
60409623  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             892
Checksum:              292


Coasting Arc #13 (Orbit 907)
---------------------------------------

Vector Time (GMT): 2011/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         778000
20                 A    =         6770691
64  meter
 Y    =        6655622
47  meter          E    =           
0016337
 Z    =        -982952
71                 I    =           51
32208
 XDOT =      -4910
969570                 Wp   =           90
42332
 YDOT =       -282
613966  meter/sec      RA   =          256
58911  deg
 ZDOT =      -5885
570297                 TA   =          100
29095
                                          MA   =          100
10671
                                          Ha   =            215
561  n
mi
                                          Hp   =            200
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2552494
10                 X    =          708292
85
 Y    =       21836031
74  feet           Y    =         6663932
88  meter
 Z    =       -3224910
47                 Z    =         -979341
97
 XDOT =     -16112
104888                 XDOT =       -4878
853718
 YDOT =       -927
211176  feet/sec       YDOT =        -337
351329  meter/sec
 ZDOT =     -19309
613836                 ZDOT =       -5909
349454

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13361387
28                 X    =         4072550
84
 Y    =      -17461192
15  feet           Y    =        -5322171
37  meter
 Z    =       -3210553
59                 Z    =         -978576
73
 XDOT =       9559
224494                 XDOT =        2913
651626
 YDOT =      10831
452271  feet/sec       YDOT =        3301
426652  meter/sec
 ZDOT =     -19406
210701                 ZDOT =       -5915
013022


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   11220
53020843  
00016717  00000-0  10270-3 0  9121
2 25544  51
6395 257
2779 0012711  53
4380 306
7944 15
60417270  9088


Satellite: ISS
Catalog Number: 25544
Epoch time:      11220
53020843   =   yrday
fracday
Element set:     912
Inclination:       51
6395  deg
RA of node:       257
2779  deg
Eccentricity:     
0012711     
Arg of perigee:    53
4380  deg
Mean anomaly:     306
7944  deg
Mean motion:   15
60417270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             908
Checksum:              293


Coasting Arc #14 (Orbit 923)
---------------------------------------

Vector Time (GMT): 2011/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1818776
46                 A    =         6763730
63  meter
 Y    =       -5016042
42  meter          E    =           
0021262
 Z    =        4135898
84                 I    =           51
30546
 XDOT =       4734
729804                 Wp   =           78
38225
 YDOT =       4789
545957  meter/sec      RA   =          251
54891  deg
 ZDOT =       3714
718272                 TA   =          333
33391
                                          MA   =          333
44310
                                          Ha   =            215
589  n
mi
                                          Hp   =            200
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5967114
37                 X    =         1854640
59
 Y    =      -16456832
08  feet           Y    =        -4995503
59  meter
 Z    =       13569221
91                 Z    =         4144820
95
 XDOT =      15533
890433                 XDOT =        4662
775195
 YDOT =      15713
733454  feet/sec       YDOT =        4842
089944  meter/sec
 ZDOT =      12187
395905                 ZDOT =        3737
544793

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15548998
98                 X    =        -4739334
89
 Y    =        7979411
70  feet           Y    =         2432124
69  meter
 Z    =       13605703
90                 Z    =         4147018
55
 XDOT =         51
812717                 XDOT =          15
792516
 YDOT =     -20904
258471  feet/sec       YDOT =       -6371
617982  meter/sec
 ZDOT =      12279
925343                 ZDOT =        3742
921245


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   11221
55489378  
00016717  00000-0  10270-3 0  9137
2 25544  51
6381 252
1210 0012836  57
5082 302
7313 15
60417769  9246


Satellite: ISS
Catalog Number: 25544
Epoch time:      11221
55489378   =   yrday
fracday
Element set:     913
Inclination:       51
6381  deg
RA of node:       252
1210  deg
Eccentricity:     
0012836     
Arg of perigee:    57
5082  deg
Mean anomaly:     302
7313  deg
Mean motion:   15
60417769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             924
Checksum:              297


Coasting Arc #15 (Orbit 938)
---------------------------------------

Vector Time (GMT): 2011/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901745
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4023374
14                 A    =         6759133
74  meter
 Y    =        1357355
07  meter          E    =           
0026509
 Z    =       -5281094
43                 I    =           51
30165
 XDOT =      -2816
370770                 Wp   =           77
88632
 YDOT =      -7115
798490  meter/sec      RA   =          246
46577  deg
 ZDOT =        323
562070                 TA   =          195
17649
                                          MA   =          195
25617
                                          Ha   =            215
616  n
mi
                                          Hp   =            200
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13200046
39                 X    =        -4012599
33
 Y    =        4453264
67  feet           Y    =         1312423
90  meter
 Z    =      -17326425
30                 Z    =        -5300613
25
 XDOT =      -9240
061580                 XDOT =       -2738
162977
 YDOT =     -23345
795572  feet/sec       YDOT =       -7146
855607  meter/sec
 ZDOT =       1061
555349                 ZDOT =         310
069878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12694894
09                 X    =         3869403
72
 Y    =        5491404
41  feet           Y    =         1673780
06  meter
 Z    =      -17405802
09                 Z    =        -5305288
48
 XDOT =      -8419
213925                 XDOT =       -2566
176404
 YDOT =      22584
513722  feet/sec       YDOT =        6883
759782  meter/sec
 ZDOT =       1007
043146                 ZDOT =         306
946751


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   11222
51552493  
00016717  00000-0  10270-3 0  9144
2 25544  51
6391 247
2864 0012684  60
5107 299
7313 15
60421434  9395


Satellite: ISS
Catalog Number: 25544
Epoch time:      11222
51552493   =   yrday
fracday
Element set:     914
Inclination:       51
6391  deg
RA of node:       247
2864  deg
Eccentricity:     
0012684     
Arg of perigee:    60
5107  deg
Mean anomaly:     299
7313  deg
Mean motion:   15
60421434  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             939
Checksum:              303

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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