[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: November 29th 2013

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 ET - UTC (sec) : 67 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 2008)
---------------------------------------

Vector Time (GMT): 2013/331/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -708578
75                 A    =         6788644
77  meter
 Y    =       -4429451
76  meter          E    =           
0014387
 Z    =       -5108426
82                 I    =           51
74139
 XDOT =       7404
130147                 Wp   =           76
61339
 YDOT =        826
435157  meter/sec      RA   =           17
00970  deg
 ZDOT =      -1744
494531                 TA   =          176
51270
                                          MA   =          176
50266
                                          Ha   =            226
943  n
mi
                                          Hp   =            219
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2324733
42                 X    =         -634179
20
 Y    =      -14532322
05  feet           Y    =        -4436959
55  meter
 Z    =      -16759930
52                 Z    =        -5111688
37
 XDOT =      24291
765574                 XDOT =        7402
812894
 YDOT =       2711
401435  feet/sec       YDOT =         909
225491  meter/sec
 ZDOT =      -5723
407255                 ZDOT =       -1708
528530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3857570
25                 X    =        -1175787
41
 Y    =      -14187232
55  feet           Y    =        -4324268
48  meter
 Z    =      -16772883
62                 Z    =        -5112374
93
 XDOT =      23442
860960                 XDOT =        7145
384021
 YDOT =        210
162641  feet/sec       YDOT =          64
057573  meter/sec
 ZDOT =      -5572
278534                 ZDOT =       -1698
430497


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   13331
85366743  
00016717  00000-0  10270-3 0  9000
2 25544  51
6500  17
4513 0001036  75
0844 285
0421 15
50585904 20093


Satellite: ISS
Catalog Number: 25544
Epoch time:      13331
85366743   =   yrday
fracday
Element set:     900
Inclination:       51
6500  deg
RA of node:        17
4513  deg
Eccentricity:     
0001036     
Arg of perigee:    75
0844  deg
Mean anomaly:     285
0421  deg
Mean motion:   15
50585904  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2009
Checksum:              277


Coasting Arc #2 (Orbit 2024)
---------------------------------------

Vector Time (GMT): 2013/332/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         420914
58                 A    =         6787989
26  meter
 Y    =        4308243
56  meter          E    =           
0004509
 Z    =        5225428
96                 I    =           51
70980
 XDOT =      -7547
262722                 Wp   =          114
99425
 YDOT =       -674
275200  meter/sec      RA   =           12
05431  deg
 ZDOT =       1161
219136                 TA   =          323
86272
                                          MA   =          323
89318
                                          Ha   =            226
835  n
mi
                                          Hp   =            219
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1380953
36                 X    =          347323
35
 Y    =       14134657
33  feet           Y    =         4312538
98  meter
 Z    =       17143795
80                 Z    =         5227295
04
 XDOT =     -24761
360636                 XDOT =       -7544
802892
 YDOT =      -2212
188977  feet/sec       YDOT =        -758
659753  meter/sec
 ZDOT =       3809
774068                 ZDOT =        1124
560459

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3111026
63                 X    =          948240
92
 Y    =       13848233
72  feet           Y    =         4220941
64  meter
 Z    =       17150896
20                 Z    =         5227593
16
 XDOT =     -23851
248302                 XDOT =       -7269
860482
 YDOT =        819
907060  feet/sec       YDOT =         249
907672  meter/sec
 ZDOT =       3655
714229                 ZDOT =        1114
261697


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   13332
88485484  
00016717  00000-0  10270-3 0  9019
2 25544  51
6500  12
3392 0000879  78
6968 281
4282 15
50619944 20257


Satellite: ISS
Catalog Number: 25544
Epoch time:      13332
88485484   =   yrday
fracday
Element set:     901
Inclination:       51
6500  deg
RA of node:        12
3392  deg
Eccentricity:     
0000879     
Arg of perigee:    78
6968  deg
Mean anomaly:     281
4282  deg
Mean motion:   15
50619944  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2025
Checksum:              320


Coasting Arc #3 (Orbit 2039)
---------------------------------------

Vector Time (GMT): 2013/333/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -104581
24                 A    =         6787712
81  meter
 Y    =       -4242875
41  meter          E    =           
0015765
 Z    =       -5310884
46                 I    =           51
67887
 XDOT =       7614
156170                 Wp   =           85
09315
 YDOT =        506
183903  meter/sec      RA   =            7
09533  deg
 ZDOT =       -554
434077                 TA   =          179
60778
                                          MA   =          179
60655
                                          Ha   =            226
921  n
mi
                                          Hp   =            219
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -343114
30                 X    =          -31329
28
 Y    =      -13920194
92  feet           Y    =        -4243635
20  meter
 Z    =      -17424161
61                 Z    =        -5311214
69
 XDOT =      24980
827328                 XDOT =        7610
623352
 YDOT =       1660
708342  feet/sec       YDOT =         591
310506  meter/sec
 ZDOT =      -1819
009440                 ZDOT =        -517
452941

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2288933
22                 X    =         -697666
85
 Y    =      -13734182
25  feet           Y    =        -4186178
75  meter
 Z    =      -17424809
46                 Z    =        -5311081
92
 XDOT =      23961
220584                 XDOT =        7303
380034
 YDOT =      -1883
203735  feet/sec       YDOT =        -574
000499  meter/sec
 ZDOT =      -1663
571830                 ZDOT =        -507
056694


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   13333
85158889  
00016717  00000-0  10270-3 0  9024
2 25544  51
6506   7
5457 0001057  78
3234 281
8035 15
50607360 20409


Satellite: ISS
Catalog Number: 25544
Epoch time:      13333
85158889   =   yrday
fracday
Element set:     902
Inclination:       51
6506  deg
RA of node:         7
5457  deg
Eccentricity:     
0001057     
Arg of perigee:    78
3234  deg
Mean anomaly:     281
8035  deg
Mean motion:   15
50607360  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2040
Checksum:              297


Coasting Arc #4 (Orbit 2055)
---------------------------------------

Vector Time (GMT): 2013/334/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -222991
31                 A    =         6787509
59  meter
 Y    =        4204662
40  meter          E    =           
0003323
 Z    =        5320812
00                 I    =           51
64747
 XDOT =      -7658
384891                 Wp   =           82
88674
 YDOT =       -331
703234  meter/sec      RA   =            2
13467  deg
 ZDOT =        -58
402100                 TA   =            7
67244
                                          MA   =            7
66735
                                          Ha   =            226
821  n
mi
                                          Hp   =            219
825

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -731598
78                 X    =         -295839
86
 Y    =       13794824
14  feet           Y    =         4201761
19  meter
 Z    =       17456732
28                 Z    =         5319551
95
 XDOT =     -25125
934682                 XDOT =       -7653
822809
 YDOT =      -1088
265205  feet/sec       YDOT =        -417
318660  meter/sec
 ZDOT =       -191
607940                 ZDOT =         -95
595642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1443974
88                 X    =          440123
54
 Y    =       13746203
65  feet           Y    =         4189842
87  meter
 Z    =       17450694
35                 Z    =         5318971
64
 XDOT =     -23957
884115                 XDOT =       -7302
363078
 YDOT =       2960
207843  feet/sec       YDOT =         902
271350  meter/sec
 ZDOT =       -347
963777                 ZDOT =        -106
059359


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   13334
88276204  
00016717  00000-0  10270-3 0  9031
2 25544  51
6502   2
4332 0000903  79
2074 280
9179 15
50644255 20562


Satellite: ISS
Catalog Number: 25544
Epoch time:      13334
88276204   =   yrday
fracday
Element set:     903
Inclination:       51
6502  deg
RA of node:         2
4332  deg
Eccentricity:     
0000903     
Arg of perigee:    79
2074  deg
Mean anomaly:     280
9179  deg
Mean motion:   15
50644255  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2056
Checksum:              287


Coasting Arc #5 (Orbit 2070)
---------------------------------------

Vector Time (GMT): 2013/335/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         555032
10                 A    =         6787738
87  meter
 Y    =       -4226987
32  meter          E    =           
0015580
 Z    =       -5295420
67                 I    =           51
61765
 XDOT =       7619
885105                 Wp   =           94
14935
 YDOT =        157
586738  meter/sec      RA   =          357
17109  deg
 ZDOT =        673
490091                 TA   =          182
29452
                                          MA   =          182
30168
                                          Ha   =            226
882  n
mi
                                          Hp   =            219
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1820971
46                 X    =          627982
24
 Y    =      -13868068
62  feet           Y    =        -4220372
31  meter
 Z    =      -17373427
38                 Z    =        -5292547
43
 XDOT =      24999
623049                 XDOT =        7614
284898
 YDOT =        517
016858  feet/sec       YDOT =         242
765782  meter/sec
 ZDOT =       2209
613160                 ZDOT =         710
494029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -622802
59                 X    =         -189830
23
 Y    =      -13989175
19  feet           Y    =        -4263900
60  meter
 Z    =      -17360597
27                 Z    =        -5291510
05
 XDOT =      23643
424371                 XDOT =        7206
515748
 YDOT =      -3985
330376  feet/sec       YDOT =       -1214
728699  meter/sec
 ZDOT =       2365
199608                 ZDOT =         720
912841


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   13335
84948257  
00016717  00000-0  10270-3 0  9043
2 25544  51
6507 357
6396 0001031  80
8072 279
3196 15
50628053 20717


Satellite: ISS
Catalog Number: 25544
Epoch time:      13335
84948257   =   yrday
fracday
Element set:     904
Inclination:       51
6507  deg
RA of node:       357
6396  deg
Eccentricity:     
0001031     
Arg of perigee:    80
8072  deg
Mean anomaly:     279
3196  deg
Mean motion:   15
50628053  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2071
Checksum:              314


Coasting Arc #6 (Orbit 2086)
---------------------------------------

Vector Time (GMT): 2013/336/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -888719
99                 A    =         6788028
75  meter
 Y    =        4277124
39  meter          E    =           
0005175
 Z    =        5192218
10                 I    =           51
58791
 XDOT =      -7556
386718                 Wp   =           58
91339
 YDOT =          1
236188  meter/sec      RA   =          352
20575  deg
 ZDOT =      -1290
829986                 TA   =           43
51665
                                          MA   =           43
47583
                                          Ha   =            226
801  n
mi
                                          Hp   =            219
784

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2915747
98                 X    =         -961704
53
 Y    =       14032560
35  feet           Y    =         4266777
59  meter
 Z    =       17034836
30                 Z    =         5187723
83
 XDOT =     -24791
295005                 XDOT =       -7549
568311
 YDOT =          4
055736  feet/sec       YDOT =         -83
225891  meter/sec
 ZDOT =      -4235
006517                 ZDOT =       -1327
522342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -174895
72                 X    =          -53308
22
 Y    =       14354551
33  feet           Y    =         4375267
25  meter
 Z    =       17015177
09                 Z    =         5186225
98
 XDOT =     -23223
823959                 XDOT =       -7078
621543
 YDOT =       4933
807652  feet/sec       YDOT =        1503
824572  meter/sec
 ZDOT =      -4389
311037                 ZDOT =       -1337
862004


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   13336
88064156  
00016717  00000-0  10270-3 0  9056
2 25544  51
6504 352
5266 0000911  79
3738 280
7515 15
50668723 20878


Satellite: ISS
Catalog Number: 25544
Epoch time:      13336
88064156   =   yrday
fracday
Element set:     905
Inclination:       51
6504  deg
RA of node:       352
5266  deg
Eccentricity:     
0000911     
Arg of perigee:    79
3738  deg
Mean anomaly:     280
7515  deg
Mean motion:   15
50668723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2087
Checksum:              318


Coasting Arc #7 (Orbit 2101)
---------------------------------------

Vector Time (GMT): 2013/337/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1201797
64                 A    =         6788743
64  meter
 Y    =       -4385090
75  meter          E    =           
0013804
 Z    =       -5053745
73                 I    =           51
56002
 XDOT =       7414
056005                 Wp   =          102
44626
 YDOT =       -142
527257  meter/sec      RA   =          347
23831  deg
 ZDOT =       1888
221716                 TA   =          185
90897
                                          MA   =          185
92527
                                          Ha   =            226
826  n
mi
                                          Hp   =            219
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3942905
64                 X    =         1275293
41
 Y    =      -14386780
67  feet           Y    =        -4371240
01  meter
 Z    =      -16580530
62                 Z    =        -5047729
38
 XDOT =      24324
330725                 XDOT =        7405
926157
 YDOT =       -467
609111  feet/sec       YDOT =         -59
664219  meter/sec
 ZDOT =       6194
953137                 ZDOT =        1924
219230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         851934
56                 X    =          259669
65
 Y    =      -14921942
35  feet           Y    =        -4548208
03  meter
 Z    =      -16554449
64                 Z    =        -5045796
25
 XDOT =      22526
480263                 XDOT =        6866
071184
 YDOT =      -5749
236844  feet/sec       YDOT =       -1752
367390  meter/sec
 ZDOT =       6346
363047                 ZDOT =        1934
371457


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   13337
84734852  
00016717  00000-0  10270-3 0  9061
2 25544  51
6508 347
7327 0000962  82
2631 277
8630 15
50648713 21027


Satellite: ISS
Catalog Number: 25544
Epoch time:      13337
84734852   =   yrday
fracday
Element set:     906
Inclination:       51
6508  deg
RA of node:       347
7327  deg
Eccentricity:     
0000962     
Arg of perigee:    82
2631  deg
Mean anomaly:     277
8630  deg
Mean motion:   15
50648713  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2102
Checksum:              312


Coasting Arc #8 (Orbit 2117)
---------------------------------------

Vector Time (GMT): 2013/338/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1506983
23                 A    =         6789486
32  meter
 Y    =        4515746
92  meter          E    =           
0008081
 Z    =        4836180
22                 I    =           51
53310
 XDOT =      -7248
658438                 Wp   =           62
09847
 YDOT =        246
953402  meter/sec      RA   =          342
26955  deg
 ZDOT =      -2482
436147                 TA   =           52
36869
                                          MA   =           52
29538
                                          Ha   =            226
769  n
mi
                                          Hp   =            219
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4944170
70                 X    =        -1580860
32
 Y    =       14815442
64  feet           Y    =         4498481
30  meter
 Z    =       15866733
01                 Z    =         4828680
40
 XDOT =     -23781
687790                 XDOT =       -7238
822103
 YDOT =        810
214575  feet/sec       YDOT =         165
949543  meter/sec
 ZDOT =      -8144
475547                 ZDOT =       -2517
625801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1465197
88                 X    =         -446592
31
 Y    =       15582703
57  feet           Y    =         4749608
05  meter
 Z    =       15834390
59                 Z    =         4826322
25
 XDOT =     -21757
854323                 XDOT =       -6631
793998
 YDOT =       6403
604160  feet/sec       YDOT =        1951
818548  meter/sec
 ZDOT =      -8292
509527                 ZDOT =       -2527
556904


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   13338
87849349  
00016717  00000-0  10270-3 0  9074
2 25544  51
6509 342
6194 0000900  79
2280 280
8972 15
50692331 21187


Satellite: ISS
Catalog Number: 25544
Epoch time:      13338
87849349   =   yrday
fracday
Element set:     907
Inclination:       51
6509  deg
RA of node:       342
6194  deg
Eccentricity:     
0000900     
Arg of perigee:    79
2280  deg
Mean anomaly:     280
8972  deg
Mean motion:   15
50692331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2118
Checksum:              325


Coasting Arc #9 (Orbit 2132)
---------------------------------------

Vector Time (GMT): 2013/339/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1768757
24                 A    =         6790581
70  meter
 Y    =       -4694240
79  meter          E    =           
0010740
 Z    =       -4587401
25                 I    =           51
50751
 XDOT =       7018
508924                 Wp   =          107
67795
 YDOT =       -319
337154  meter/sec      RA   =          337
29933  deg
 ZDOT =       3035
582333                 TA   =          192
75588
                                          MA   =          192
78308
                                          Ha   =            226
766  n
mi
                                          Hp   =            219
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5803009
32                 X    =         1843402
22
 Y    =      -15401052
46  feet           Y    =        -4674043
65  meter
 Z    =      -15050529
04                 Z    =        -4578627
88
 XDOT =      23026
604081                 XDOT =        7006
812122
 YDOT =      -1047
694074  feet/sec       YDOT =        -240
917391  meter/sec
 ZDOT =       9959
259624                 ZDOT =        3069
649251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1878106
19                 X    =          572446
77
 Y    =      -16385184
07  feet           Y    =        -4994204
10  meter
 Z    =      -15012801
82                 Z    =        -4575901
99
 XDOT =      20786
308175                 XDOT =        6335
666732
 YDOT =      -6865
733091  feet/sec       YDOT =       -2092
675446  meter/sec
 ZDOT =      10102
586646                 ZDOT =        3079
268410


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   13339
84518703  
00016717  00000-0  10270-3 0  9080
2 25544  51
6510 337
8255 0000876  83
7368 276
3883 15
50669147 21339


Satellite: ISS
Catalog Number: 25544
Epoch time:      13339
84518703   =   yrday
fracday
Element set:     908
Inclination:       51
6510  deg
RA of node:       337
8255  deg
Eccentricity:     
0000876     
Arg of perigee:    83
7368  deg
Mean anomaly:     276
3883  deg
Mean motion:   15
50669147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2133
Checksum:              333


Coasting Arc #10 (Orbit 2148)
---------------------------------------

Vector Time (GMT): 2013/340/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2015030
60                 A    =         6791650
62  meter
 Y    =        4884745
02  meter          E    =           
0010879
 Z    =        4259661
68                 I    =           51
48368
 XDOT =      -6771
616081                 Wp   =           73
85992
 YDOT =        335
674114  meter/sec      RA   =          332
32852  deg
 ZDOT =      -3577
663240                 TA   =           52
80697
                                          MA   =           52
70771
                                          Ha   =            226
724  n
mi
                                          Hp   =            219
734

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6610992
80                 X    =        -2090195
42
 Y    =       16026066
34  feet           Y    =         4861791
09  meter
 Z    =       13975267
97                 Z    =         4249690
62
 XDOT =     -22216
588191                 XDOT =       -6757
487069
 YDOT =       1101
293025  feet/sec       YDOT =         260
028844  meter/sec
 ZDOT =     -11737
740288                 ZDOT =       -3610
524785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2202596
81                 X    =         -671351
51
 Y    =       17230288
59  feet           Y    =         5251791
96  meter
 Z    =       13932475
19                 Z    =         4246618
44
 XDOT =     -19799
876487                 XDOT =       -6035
002353
 YDOT =       7100
053799  feet/sec       YDOT =        2164
096398  meter/sec
 ZDOT =     -11876
000845                 ZDOT =       -3619
805058


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   13340
87631808  
00016717  00000-0  10270-3 0  9098
2 25544  51
6513 332
7125 0000867  79
4981 280
6268 15
50713963 21493


Satellite: ISS
Catalog Number: 25544
Epoch time:      13340
87631808   =   yrday
fracday
Element set:     909
Inclination:       51
6513  deg
RA of node:       332
7125  deg
Eccentricity:     
0000867     
Arg of perigee:    79
4981  deg
Mean anomaly:     280
6268  deg
Mean motion:   15
50713963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2149
Checksum:              325


Coasting Arc #11 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2013/341/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2200460
01                 A    =         6792952
88  meter
 Y    =       -5107124
28  meter          E    =           
0007174
 Z    =       -3908587
99                 I    =           51
46031
 XDOT =       6482
246579                 Wp   =          103
11171
 YDOT =       -311
159396  meter/sec      RA   =          327
35632  deg
 ZDOT =       4060
670070                 TA   =          209
56703
                                          MA   =          209
60761
                                          Ha   =            226
711  n
mi
                                          Hp   =            219
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7219356
98                 X    =         2276392
31
 Y    =      -16755657
10  feet           Y    =        -5082092
57  meter
 Z    =      -12823451
40                 Z    =        -3897714
19
 XDOT =      21267
213187                 XDOT =        6465
518635
 YDOT =      -1020
864161  feet/sec       YDOT =        -238
764529  meter/sec
 ZDOT =      13322
408367                 ZDOT =        4092
119571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2276926
06                 X    =          694007
06
 Y    =      -18135057
07  feet           Y    =        -5527565
40  meter
 Z    =      -12776829
75                 Z    =        -3894377
71
 XDOT =      18713
843494                 XDOT =        5703
979497
 YDOT =      -7118
823960  feet/sec       YDOT =       -2169
817543  meter/sec
 ZDOT =      13454
724092                 ZDOT =        4100
999903


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   13341
84299827  
00016717  00000-0  10270-3 0  9109
2 25544  51
6508 327
9185 0000793  86
6814 273
4428 15
50687898 21644


Satellite: ISS
Catalog Number: 25544
Epoch time:      13341
84299827   =   yrday
fracday
Element set:     910
Inclination:       51
6508  deg
RA of node:       327
9185  deg
Eccentricity:     
0000793     
Arg of perigee:    86
6814  deg
Mean anomaly:     273
4428  deg
Mean motion:   15
50687898  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2164
Checksum:              347


Coasting Arc #12 (Orbit 2179)
---------------------------------------

Vector Time (GMT): 2013/342/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2366444
30                 A    =         6794144
34  meter
 Y    =        5326256
07  meter          E    =           
0013095
 Z    =        3480638
75                 I    =           51
43939
 XDOT =      -6186
411267                 Wp   =           88
23896
 YDOT =        216
266310  meter/sec      RA   =          322
38411  deg
 ZDOT =      -4521
851625                 TA   =           50
78823
                                          MA   =           50
67204
                                          Ha   =            226
665  n
mi
                                          Hp   =            219
725

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7763924
88                 X    =        -2442735
81
 Y    =       17474593
40  feet           Y    =         5299366
28  meter
 Z    =       11419418
49                 Z    =         3468957
67
 XDOT =     -20296
624893                 XDOT =       -6166
403867
 YDOT =        709
535137  feet/sec       YDOT =         147
197959  meter/sec
 ZDOT =     -14835
471211                 ZDOT =       -4551
856074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2261469
01                 X    =         -689295
76
 Y    =       19017524
13  feet           Y    =         5796541
35  meter
 Z    =       11369370
99                 Z    =         3465384
28
 XDOT =     -17684
573655                 XDOT =       -5390
258050
 YDOT =       6871
543356  feet/sec       YDOT =        2094
446415  meter/sec
 ZDOT =     -14961
689805                 ZDOT =       -4560
323053


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   13342
87411525  
00016717  00000-0  10270-3 0  9115
2 25544  51
6510 322
8055 0000814  81
2768 278
8476 15
50733312 21803


Satellite: ISS
Catalog Number: 25544
Epoch time:      13342
87411525   =   yrday
fracday
Element set:     911
Inclination:       51
6510  deg
RA of node:       322
8055  deg
Eccentricity:     
0000814     
Arg of perigee:    81
2768  deg
Mean anomaly:     278
8476  deg
Mean motion:   15
50733312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2180
Checksum:              292


Coasting Arc #13 (Orbit 2194)
---------------------------------------

Vector Time (GMT): 2013/343/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2461813
60                 A    =         6795437
42  meter
 Y    =       -5557661
60  meter          E    =           
0005208
 Z    =       -3040517
65                 I    =           51
41828
 XDOT =       5875
180784                 Wp   =           73
17025
 YDOT =        -79
427301  meter/sec      RA   =          317
41017  deg
 ZDOT =       4910
611980                 TA   =          251
92034
                                          MA   =          251
97708
                                          Ha   =            226
666  n
mi
                                          Hp   =            219
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8076816
26                 X    =         2538547
70
 Y    =      -18233797
90  feet           Y    =        -5529702
89  meter
 Z    =       -9975451
61                 Z    =        -3028372
14
 XDOT =      19275
527508                 XDOT =        5851
777793
 YDOT =       -260
588258  feet/sec       YDOT =         -13
858299  meter/sec
 ZDOT =      16110
931692                 ZDOT =        4939
096331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1983434
66                 X    =          604550
88
 Y    =      -19869769
54  feet           Y    =        -6056305
76  meter
 Z    =       -9923418
12                 Z    =        -3024657
84
 XDOT =      16668
944961                 XDOT =        5080
694424
 YDOT =      -6428
114175  feet/sec       YDOT =       -1959
289201  meter/sec
 ZDOT =      16230
730198                 ZDOT =        4947
126564


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   13343
84078202  
00016717  00000-0  10270-3 0  9125
2 25544  51
6497 318
0110 0000732  92
3528 267
7707 15
50704309 21956


Satellite: ISS
Catalog Number: 25544
Epoch time:      13343
84078202   =   yrday
fracday
Element set:     912
Inclination:       51
6497  deg
RA of node:       318
0110  deg
Eccentricity:     
0000732     
Arg of perigee:    92
3528  deg
Mean anomaly:     267
7707  deg
Mean motion:   15
50704309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2195
Checksum:              295


Coasting Arc #14 (Orbit 2210)
---------------------------------------

Vector Time (GMT): 2013/344/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2538822
73                 A    =         6796500
31  meter
 Y    =        5767726
70  meter          E    =           
0014380
 Z    =        2528189
53                 I    =           51
40029
 XDOT =      -5570
564967                 Wp   =          103
21510
 YDOT =       -134
912760  meter/sec      RA   =          312
43667  deg
 ZDOT =      -5264
114790                 TA   =           48
33248
                                          MA   =           48
20947
                                          Ha   =            226
599  n
mi
                                          Hp   =            219
717

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8329470
88                 X    =        -2615411
37
 Y    =       18922987
85  feet           Y    =         5738907
64  meter
 Z    =        8294585
08                 Z    =         2515670
25
 XDOT =     -18276
131781                 XDOT =       -5543
070513
 YDOT =       -442
627166  feet/sec       YDOT =        -197
052455  meter/sec
 ZDOT =     -17270
717815                 ZDOT =       -5291
109491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1641696
04                 X    =         -500388
95
 Y    =       20631317
83  feet           Y    =         6288425
67  meter
 Z    =        8240949
87                 Z    =         2511841
52
 XDOT =     -15785
731370                 XDOT =       -4811
490922
 YDOT =       5716
953570  feet/sec       YDOT =        1742
527448  meter/sec
 ZDOT =     -17384
211807                 ZDOT =       -5298
707759


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   13344
87188469  
00016717  00000-0  10270-3 0  9137
2 25544  51
6498 312
8978 0000750  85
7600 274
3637 15
50751996 22117


Satellite: ISS
Catalog Number: 25544
Epoch time:      13344
87188469   =   yrday
fracday
Element set:     913
Inclination:       51
6498  deg
RA of node:       312
8978  deg
Eccentricity:     
0000750     
Arg of perigee:    85
7600  deg
Mean anomaly:     274
3637  deg
Mean motion:   15
50751996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2211
Checksum:              338


Coasting Arc #15 (Orbit 2225)
---------------------------------------

Vector Time (GMT): 2013/345/20:01:48
169
Vector Time (MET): N/A
Weight (LBS)     : 886492
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2544177
90                 A    =         6797560
14  meter
 Y    =       -5969820
86  meter          E    =           
0007111
 Z    =       -2017379
41                 I    =           51
38185
 XDOT =       5278
348169                 Wp   =           44
96306
 YDOT =        383
961780  meter/sec      RA   =          307
46112  deg
 ZDOT =       5537
386063                 TA   =          292
70652
                                          MA   =          292
78168
                                          Ha   =            226
631  n
mi
                                          Hp   =            219
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8347040
35                 X    =         2620544
64
 Y    =      -19586026
45  feet           Y    =        -5940943
17  meter
 Z    =       -6618698
87                 Z    =        -2004834
68
 XDOT =      17317
415254                 XDOT =        5246
762958
 YDOT =       1259
717126  feet/sec       YDOT =         442
810790  meter/sec
 ZDOT =      18167
277111                 ZDOT =        5562
951332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1063010
76                 X    =          324005
68
 Y    =      -21280611
62  feet           Y    =        -6486330
42  meter
 Z    =       -6564927
01                 Z    =        -2000989
75
 XDOT =      15019
112899                 XDOT =        4577
825612
 YDOT =      -4870
126429  feet/sec       YDOT =       -1484
414536  meter/sec
 ZDOT =      18274
715441                 ZDOT =        5570
133267


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   13345
83853808  
00016717  00000-0  10270-3 0  9141
2 25544  51
6482 308
1028 0000717 101
3514 258
7717 15
50720041 22264


Satellite: ISS
Catalog Number: 25544
Epoch time:      13345
83853808   =   yrday
fracday
Element set:     914
Inclination:       51
6482  deg
RA of node:       308
1028  deg
Eccentricity:     
0000717     
Arg of perigee:   101
3514  deg
Mean anomaly:     258
7717  deg
Mean motion:   15
50720041  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2226
Checksum:              289
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