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

 
Date: November 26th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17491 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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


329/19:38:37 913 5 2 5 8 5 8
N/A -2 1 -0 4 221 6
000/00:15:15 827 -1 6 0 3 215 1

Coasting Arc #1 (Orbit 1313)
---------------------------------------

Vector Time (GMT): 2015/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906699
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1486290
27                 A    =         6774138
36  meter
 Y    =       -4085166
51  meter          E    =           
0015040
 Z    =       -5207467
52                 I    =           51
61993
 XDOT =       7471
299136                 Wp   =          102
05654
 YDOT =      -1171
461592  meter/sec      RA   =          358
42646  deg
 ZDOT =      -1219
481369                 TA   =          156
26113
                                          MA   =          156
19167
                                          Ha   =            220
077  n
mi
                                          Hp   =            212
102

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4876280
41                 X    =        -1415201
98
 Y    =      -13402777
27  feet           Y    =        -4101389
47  meter
 Z    =      -17084867
18                 Z    =        -5214515
31
 XDOT =      24512
136274                 XDOT =        7489
767334
 YDOT =      -3843
377926  feet/sec       YDOT =       -1087
809276  meter/sec
 ZDOT =      -4000
923127                 ZDOT =       -1183
141633

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14116030
70                 X    =         4302566
16
 Y    =        1771528
87  feet           Y    =          539962
00  meter
 Z    =      -17114455
84                 Z    =        -5216486
14
 XDOT =      -7474
163152                 XDOT =       -2278
124929
 YDOT =      22614
652434  feet/sec       YDOT =        6892
946062  meter/sec
 ZDOT =      -3843
659183                 ZDOT =       -1171
547319


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   15329
51809983  
00016717  00000-0  10270-3 0  9000
2 25544  51
6441 358
8802 0005515 173
0304 187
0927 15
55389118 13140


Satellite: ISS
Catalog Number: 25544
Epoch time:      15329
51809983   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:       358
8802  deg
Eccentricity:     
0005515     
Arg of perigee:   173
0304  deg
Mean anomaly:     187
0927  deg
Mean motion:   15
55389118  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1314
Checksum:              314


Coasting Arc #2 (Orbit 1318)
---------------------------------------

Vector Time (GMT): 2015/329/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          69446
59                 A    =         6777021
14  meter
 Y    =       -4219843
46  meter          E    =           
0013574
 Z    =       -5312348
87                 I    =           51
60763
 XDOT =       7652
739072                 Wp   =          125
27483
 YDOT =       -217
571223  meter/sec      RA   =          356
79575  deg
 ZDOT =        265
686606                 TA   =          147
30346
                                          MA   =          147
21937
                                          Ha   =            221
593  n
mi
                                          Hp   =            215
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         227843
13                 X    =          142434
70
 Y    =      -13844630
78  feet           Y    =        -4218658
48  meter
 Z    =      -17428966
12                 Z    =        -5311834
45
 XDOT =      25107
411653                 XDOT =        7653
312600
 YDOT =       -713
816350  feet/sec       YDOT =        -131
990053  meter/sec
 ZDOT =        871
675218                 ZDOT =         302
864306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         301753
74                 X    =           91974
54
 Y    =      -13847138
82  feet           Y    =        -4220607
91  meter
 Z    =      -17425850
48                 Z    =        -5311399
23
 XDOT =      24089
541504                 XDOT =        7342
492251
 YDOT =       -803
867883  feet/sec       YDOT =        -245
018931  meter/sec
 ZDOT =       1032
357189                 ZDOT =         314
662471


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   15329
83935194  
00016717  00000-0  10270-3 0  9010
2 25544  51
6436 357
2749 0008221 207
5653 152
5065 15
54254430 13196


Satellite: ISS
Catalog Number: 25544
Epoch time:      15329
83935194   =   yrday
fracday
Element set:     901
Inclination:       51
6436  deg
RA of node:       357
2749  deg
Eccentricity:     
0008221     
Arg of perigee:   207
5653  deg
Mean anomaly:     152
5065  deg
Mean motion:   15
54254430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1319
Checksum:              310


Coasting Arc #3 (Orbit 1334)
---------------------------------------

Vector Time (GMT): 2015/330/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1900671
29                 A    =         6778519
58  meter
 Y    =        4232450
85  meter          E    =           
0003698
 Z    =        4939600
76                 I    =           51
58083
 XDOT =      -7311
620358                 Wp   =          160
11065
 YDOT =       -712
812112  meter/sec      RA   =          351
79266  deg
 ZDOT =      -2205
534369                 TA   =          311
40464
                                          MA   =          311
43642
                                          Ha   =            221
355  n
mi
                                          Hp   =            215
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6235798
19                 X    =        -1971853
47
 Y    =       13885993
60  feet           Y    =         4210797
94  meter
 Z    =       16206039
24                 Z    =         4930194
91
 XDOT =     -23988
255769                 XDOT =       -7292
392254
 YDOT =      -2338
622414  feet/sec       YDOT =        -794
467809  meter/sec
 ZDOT =      -7236
005147                 ZDOT =       -2241
006770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6061523
42                 X    =        -1847552
34
 Y    =       14011014
77  feet           Y    =         4270557
30  meter
 Z    =       16164501
36                 Z    =         4926940
01
 XDOT =     -22961
608362                 XDOT =       -6998
698229
 YDOT =      -1420
029062  feet/sec       YDOT =        -432
824858  meter/sec
 ZDOT =      -7389
119746                 ZDOT =       -2252
203699


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   15330
86809344  
00016717  00000-0  10270-3 0  9023
2 25544  51
6432 352
1456 0008170 211
9380 148
1278 15
54300475 13356


Satellite: ISS
Catalog Number: 25544
Epoch time:      15330
86809344   =   yrday
fracday
Element set:     902
Inclination:       51
6432  deg
RA of node:       352
1456  deg
Eccentricity:     
0008170     
Arg of perigee:   211
9380  deg
Mean anomaly:     148
1278  deg
Mean motion:   15
54300475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1335
Checksum:              293


Coasting Arc #4 (Orbit 1349)
---------------------------------------

Vector Time (GMT): 2015/331/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3586587
67                 A    =         6781999
16  meter
 Y    =       -4122919
48  meter          E    =           
0008956
 Z    =       -4024894
58                 I    =           51
56182
 XDOT =       6359
769524                 Wp   =          167
15452
 YDOT =       1701
303233  meter/sec      RA   =          346
79321  deg
 ZDOT =       3917
594397                 TA   =          143
63416
                                          MA   =          143
57327
                                          Ha   =            221
173  n
mi
                                          Hp   =            215
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11767019
91                 X    =         3651976
27
 Y    =      -13526638
72  feet           Y    =        -4082445
97  meter
 Z    =      -13205034
71                 Z    =        -4007312
90
 XDOT =      20865
385576                 XDOT =        6321
242013
 YDOT =       5581
703520  feet/sec       YDOT =        1772
206646  meter/sec
 ZDOT =      12852
999991                 ZDOT =        3948
395871

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11341081
57                 X    =         3456761
66
 Y    =      -13958367
57  feet           Y    =        -4254510
43  meter
 Z    =      -13128194
76                 Z    =        -4001473
76
 XDOT =      19957
725881                 XDOT =        6083
114849
 YDOT =       3980
816291  feet/sec       YDOT =        1213
352805  meter/sec
 ZDOT =      12985
722248                 ZDOT =        3958
048141


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   15331
83251955  
00016717  00000-0  10270-3 0  9031
2 25544  51
6439 347
3355 0008138 215
1633 144
8983 15
54318016 13501


Satellite: ISS
Catalog Number: 25544
Epoch time:      15331
83251955   =   yrday
fracday
Element set:     903
Inclination:       51
6439  deg
RA of node:       347
3355  deg
Eccentricity:     
0008138     
Arg of perigee:   215
1633  deg
Mean anomaly:     144
8983  deg
Mean motion:   15
54318016  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1350
Checksum:              306


Coasting Arc #5 (Orbit 1365)
---------------------------------------

Vector Time (GMT): 2015/332/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4922630
04                 A    =         6785859
03  meter
 Y    =        3832401
90  meter          E    =           
0012533
 Z    =        2648644
35                 I    =           51
54379
 XDOT =      -4930
862946                 Wp   =          138
39454
 YDOT =      -2731
800123  meter/sec      RA   =          341
80349  deg
 ZDOT =      -5206
547072                 TA   =           11
66830
                                          MA   =           11
63928
                                          Ha   =            221
087  n
mi
                                          Hp   =            215
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16150361
01                 X    =        -4977985
26
 Y    =       12573497
05  feet           Y    =         3777044
09  meter
 Z    =        8689778
05                 Z    =         2624596
80
 XDOT =     -16177
371869                 XDOT =       -4874
657150
 YDOT =      -8962
598829  feet/sec       YDOT =       -2786
625629  meter/sec
 ZDOT =     -17081
847349                 ZDOT =       -5230
364136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15499015
45                 X    =        -4724099
91
 Y    =       13435639
71  feet           Y    =         4095182
98  meter
 Z    =        8585064
77                 Z    =         2616727
74
 XDOT =     -15550
997544                 XDOT =       -4739
944051
 YDOT =      -6948
398688  feet/sec       YDOT =       -2117
871920  meter/sec
 ZDOT =     -17184
173889                 ZDOT =       -5237
736201


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   15332
86122033  
00016717  00000-0  10270-3 0  9040
2 25544  51
6437 342
2057 0008130 218
1674 141
8903 15
54322824 13660


Satellite: ISS
Catalog Number: 25544
Epoch time:      15332
86122033   =   yrday
fracday
Element set:     904
Inclination:       51
6437  deg
RA of node:       342
2057  deg
Eccentricity:     
0008130     
Arg of perigee:   218
1674  deg
Mean anomaly:     141
8903  deg
Mean motion:   15
54322824  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1366
Checksum:              284


Coasting Arc #6 (Orbit 1380)
---------------------------------------

Vector Time (GMT): 2015/333/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5829788
15                 A    =         6788189
67  meter
 Y    =       -3336673
36  meter          E    =           
0001889
 Z    =        -972111
63                 I    =           51
52303
 XDOT =       3133
661869                 Wp   =           21
83235
 YDOT =       3758
116029  meter/sec      RA   =          336
82025  deg
 ZDOT =       5898
744714                 TA   =          327
62563
                                          MA   =          327
63722
                                          Ha   =            220
728  n
mi
                                          Hp   =            215
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19126601
53                 X    =         5871388
54
 Y    =      -10947091
08  feet           Y    =        -3271248
16  meter
 Z    =       -3189342
62                 Z    =         -943690
68
 XDOT =      10281
042878                 XDOT =        3062
750758
 YDOT =      12329
776998  feet/sec       YDOT =        3792
761839  meter/sec
 ZDOT =      19352
836989                 ZDOT =        5913
795518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18315339
18                 X    =         5582515
38
 Y    =      -12287658
74  feet           Y    =        -3745278
38  meter
 Z    =       -3065842
30                 Z    =         -934468
73
 XDOT =      10116
232379                 XDOT =        3083
427629
 YDOT =      10238
659587  feet/sec       YDOT =        3120
743442  meter/sec
 ZDOT =      19417
072248                 ZDOT =        5918
323621


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   15333
82560557  
00016717  00000-0  10270-3 0  9055
2 25544  51
6444 337
3957 0008134 222
7512 137
3009 15
54391135 13813


Satellite: ISS
Catalog Number: 25544
Epoch time:      15333
82560557   =   yrday
fracday
Element set:     905
Inclination:       51
6444  deg
RA of node:       337
3957  deg
Eccentricity:     
0008134     
Arg of perigee:   222
7512  deg
Mean anomaly:     137
3009  deg
Mean motion:   15
54391135  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1381
Checksum:              302


Coasting Arc #7 (Orbit 1396)
---------------------------------------

Vector Time (GMT): 2015/334/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6215858
20                 A    =         6788303
44  meter
 Y    =        2573799
66  meter          E    =           
0013558
 Z    =        -835030
74                 I    =           51
49449
 XDOT =      -1163
489358                 Wp   =          177
73653
 YDOT =      -4728
383805  meter/sec      RA   =          331
83993  deg
 ZDOT =      -5929
904208                 TA   =           11
31955
                                          MA   =           11
28909
                                          Ha   =            220
589  n
mi
                                          Hp   =            216
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20393235
58                 X    =        -6240120
80
 Y    =        8444224
61  feet           Y    =         2504154
21  meter
 Z    =       -2739602
17                 Z    =         -865285
09
 XDOT =      -3817
222303                 XDOT =       -1081
723591
 YDOT =     -15513
070227  feet/sec       YDOT =       -4740
937245  meter/sec
 ZDOT =     -19455
066298                 ZDOT =       -5935
357859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19546923
61                 X    =        -5957902
32
 Y    =       10216181
31  feet           Y    =         3113892
06  meter
 Z    =       -2870857
58                 Z    =         -875037
39
 XDOT =      -4307
898478                 XDOT =       -1313
047456
 YDOT =     -13701
291150  feet/sec       YDOT =       -4176
153542  meter/sec
 ZDOT =     -19477
635757                 ZDOT =       -5936
783379


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   15334
85426396  
00016717  00000-0  10270-3 0  9062
2 25544  51
6446 332
2658 0008256 226
0907 133
9565 15
54370757 13970


Satellite: ISS
Catalog Number: 25544
Epoch time:      15334
85426396   =   yrday
fracday
Element set:     906
Inclination:       51
6446  deg
RA of node:       332
2658  deg
Eccentricity:     
0008256     
Arg of perigee:   226
0907  deg
Mean anomaly:     133
9565  deg
Mean motion:   15
54370757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1397
Checksum:              336


Coasting Arc #8 (Orbit 1412)
---------------------------------------

Vector Time (GMT): 2015/335/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6093544
23                 A    =         6785631
17  meter
 Y    =       -1561291
99  meter          E    =           
0007285
 Z    =        2541565
72                 I    =           51
45830
 XDOT =       -786
287668                 Wp   =          104
57735
 YDOT =       5519
368963  meter/sec      RA   =          326
85285  deg
 ZDOT =       5261
274606                 TA   =          284
03987
                                          MA   =          284
12085
                                          Ha   =            220
278  n
mi
                                          Hp   =            216
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19991943
01                 X    =         6098204
08
 Y    =       -5122349
05  feet           Y    =        -1493123
98  meter
 Z    =        8338470
20                 Z    =         2571178
33
 XDOT =      -2579
683949                 XDOT =        -873
505545
 YDOT =      18108
165888  feet/sec       YDOT =        5510
088336  meter/sec
 ZDOT =      17261
399625                 ZDOT =        5257
243299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19284907
98                 X    =         5878039
95
 Y    =       -7200906
45  feet           Y    =        -2194836
29  meter
 Z    =        8466734
96                 Z    =         2580660
82
 XDOT =      -1285
380703                 XDOT =        -391
784038
 YDOT =      16886
429480  feet/sec       YDOT =        5146
983706  meter/sec
 ZDOT =      17242
830194                 ZDOT =        5255
614643


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   15335
88289951  
00016717  00000-0  10270-3 0  9071
2 25544  51
6444 327
1349 0008020 231
1506 128
8932 15
54429868 14137


Satellite: ISS
Catalog Number: 25544
Epoch time:      15335
88289951   =   yrday
fracday
Element set:     907
Inclination:       51
6444  deg
RA of node:       327
1349  deg
Eccentricity:     
0008020     
Arg of perigee:   231
1506  deg
Mean anomaly:     128
8932  deg
Mean motion:   15
54429868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1413
Checksum:              322


Coasting Arc #9 (Orbit 1427)
---------------------------------------

Vector Time (GMT): 2015/336/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5489250
99                 A    =         6781553
47  meter
 Y    =         284056
00  meter          E    =           
0002602
 Z    =       -3969960
18                 I    =           51
41843
 XDOT =       2558
657529                 Wp   =          181
49630
 YDOT =      -6039
121741  meter/sec      RA   =          321
85466  deg
 ZDOT =      -3972
446399                 TA   =           47
00758
                                          MA   =           46
98577
                                          Ha   =            219
963  n
mi
                                          Hp   =            216
282

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18009353
64                 X    =        -5472734
74
 Y    =         931942
25  feet           Y    =          222764
01  meter
 Z    =      -13024803
75                 Z    =        -3996585
89
 XDOT =       8394
545700                 XDOT =        2645
295041
 YDOT =     -19813
391539  feet/sec       YDOT =       -6010
024635  meter/sec
 ZDOT =     -13032
960626                 ZDOT =       -3959
806584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17675597
47                 X    =        -5387522
11
 Y    =        3125270
43  feet           Y    =          952582
43  meter
 Z    =      -13139892
94                 Z    =        -4005039
37
 XDOT =       6207
888563                 XDOT =        1892
164434
 YDOT =     -19416
908472  feet/sec       YDOT =       -5918
273702  meter/sec
 ZDOT =     -12977
100009                 ZDOT =       -3955
420083


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   15336
84722488  
00016717  00000-0  10270-3 0  9086
2 25544  51
6440 322
3253 0008211 235
0210 125
0172 15
54461467 14283


Satellite: ISS
Catalog Number: 25544
Epoch time:      15336
84722488   =   yrday
fracday
Element set:     908
Inclination:       51
6440  deg
RA of node:       322
3253  deg
Eccentricity:     
0008211     
Arg of perigee:   235
0210  deg
Mean anomaly:     125
0172  deg
Mean motion:   15
54461467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1428
Checksum:              283


Coasting Arc #10 (Orbit 1443)
---------------------------------------

Vector Time (GMT): 2015/337/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4518570
17                 A    =         6777895
00  meter
 Y    =        1153308
76  meter          E    =           
0007789
 Z    =        4922386
48                 I    =           51
38182
 XDOT =      -3988
798183                 Wp   =          190
04768
 YDOT =       6161
315690  meter/sec      RA   =          316
84237  deg
 ZDOT =       2210
985193                 TA   =          238
25069
                                          MA   =          238
32661
                                          Ha   =            219
810  n
mi
                                          Hp   =            216
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14824705
27                 X    =         4481426
49
 Y    =        3783821
40  feet           Y    =         1203630
63  meter
 Z    =       16149561
93                 Z    =         4944246
75
 XDOT =     -13086
608213                 XDOT =       -4068
139272
 YDOT =      20214
290320  feet/sec       YDOT =        6116
266654  meter/sec
 ZDOT =       7253
888428                 ZDOT =        2191
415657

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15105784
73                 X    =         4604243
19
 Y    =        1689075
06  feet           Y    =          514830
08  meter
 Z    =       16243762
94                 Z    =         4951098
94
 XDOT =     -10052
988719                 XDOT =       -3064
150962
 YDOT =      20751
620769  feet/sec       YDOT =        6325
094010  meter/sec
 ZDOT =       7168
075146                 ZDOT =        2184
829305


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   15337
87581917  
00016717  00000-0  10270-3 0  9091
2 25544  51
6440 317
1945 0008000 238
1746 121
8628 15
54486585 14443


Satellite: ISS
Catalog Number: 25544
Epoch time:      15337
87581917   =   yrday
fracday
Element set:     909
Inclination:       51
6440  deg
RA of node:       317
1945  deg
Eccentricity:     
0008000     
Arg of perigee:   238
1746  deg
Mean anomaly:     121
8628  deg
Mean motion:   15
54486585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1444
Checksum:              328


Coasting Arc #11 (Orbit 1458)
---------------------------------------

Vector Time (GMT): 2015/338/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3279475
15                 A    =         6776111
82  meter
 Y    =       -2683703
38  meter          E    =           
0008479
 Z    =       -5294203
78                 I    =           51
35260
 XDOT =       5008
622429                 Wp   =          114
20739
 YDOT =      -5798
317271  meter/sec      RA   =          311
81901  deg
 ZDOT =       -166
950770                 TA   =          154
21543
                                          MA   =          154
17314
                                          Ha   =            219
515  n
mi
                                          Hp   =            216
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10759432
92                 X    =        -3223504
10
 Y    =       -8804801
10  feet           Y    =        -2720063
59  meter
 Z    =      -17369434
97                 Z    =        -5309999
07
 XDOT =      16432
488284                 XDOT =        5073
899370
 YDOT =     -19023
350627  feet/sec       YDOT =       -5741
942560  meter/sec
 ZDOT =       -547
738746                 ZDOT =        -142
461189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11897767
40                 X    =        -3626439
50
 Y    =       -7026889
49  feet           Y    =        -2141795
92  meter
 Z    =      -17437119
76                 Z    =        -5314834
10
 XDOT =      12735
267012                 XDOT =        3881
709385
 YDOT =     -20498
715146  feet/sec       YDOT =       -6248
008376  meter/sec
 ZDOT =       -440
755955                 ZDOT =        -134
342415


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   15338
84010406  
00016717  00000-0  10270-3 0  9101
2 25544  51
6427 312
3834 0008100 242
1775 117
8557 15
54556137 14593


Satellite: ISS
Catalog Number: 25544
Epoch time:      15338
84010406   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:       312
3834  deg
Eccentricity:     
0008100     
Arg of perigee:   242
1775  deg
Mean anomaly:     117
8557  deg
Mean motion:   15
54556137  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1459
Checksum:              298


Coasting Arc #12 (Orbit 1474)
---------------------------------------

Vector Time (GMT): 2015/339/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1928396
53                 A    =         6777261
02  meter
 Y    =        4127557
16  meter          E    =           
0002703
 Z    =        5019845
09                 I    =           51
33632
 XDOT =      -5572
008105                 Wp   =          266
47915
 YDOT =       4912
165376  meter/sec      RA   =          306
79468  deg
 ZDOT =      -1899
554444                 TA   =          202
01450
                                          MA   =          202
02611
                                          Ha   =            219
310  n
mi
                                          Hp   =            216
766

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6326760
27                 X    =         1857713
05
 Y    =       13541854
21  feet           Y    =         4148726
44  meter
 Z    =       16469308
04                 Z    =         5029041
37
 XDOT =     -18280
866485                 XDOT =       -5617
295588
 YDOT =      16116
028137  feet/sec       YDOT =        4849
602326  meter/sec
 ZDOT =      -6232
134003                 ZDOT =       -1926
732374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8480982
22                 X    =         2585003
38
 Y    =       12255624
48  feet           Y    =         3735514
34  meter
 Z    =       16508192
74                 Z    =         5031697
15
 XDOT =     -14267
495852                 XDOT =       -4348
732736
 YDOT =      18422
694003  feet/sec       YDOT =        5615
237132  meter/sec
 ZDOT =      -6350
539611                 ZDOT =       -1935
644474


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   15339
86865423  
00016717  00000-0  10270-3 0  9112
2 25544  51
6430 307
2528 0008182 245
8537 114
1761 15
54584268 14757


Satellite: ISS
Catalog Number: 25544
Epoch time:      15339
86865423   =   yrday
fracday
Element set:     911
Inclination:       51
6430  deg
RA of node:       307
2528  deg
Eccentricity:     
0008182     
Arg of perigee:   245
8537  deg
Mean anomaly:     114
1761  deg
Mean motion:   15
54584268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1475
Checksum:              323


Coasting Arc #13 (Orbit 1489)
---------------------------------------

Vector Time (GMT): 2015/340/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -569327
33                 A    =         6780697
63  meter
 Y    =       -5352865
46  meter          E    =           
0005438
 Z    =       -4126559
38                 I    =           51
32826
 XDOT =       5696
532527                 Wp   =          184
82529
 YDOT =      -3499
832963  meter/sec      RA   =          301
77393  deg
 ZDOT =       3748
278790                 TA   =          123
98287
                                          MA   =          123
93119
                                          Ha   =            219
167  n
mi
                                          Hp   =            216
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1867871
82                 X    =         -489382
42
 Y    =      -17561894
55  feet           Y    =        -5358784
93  meter
 Z    =      -13538580
63                 Z    =        -4129131
08
 XDOT =      18689
411179                 XDOT =        5717
037163
 YDOT =     -11482
391610  feet/sec       YDOT =       -3436
016040  meter/sec
 ZDOT =      12297
502592                 ZDOT =        3776
001501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5098856
48                 X    =        -1554131
46
 Y    =      -16900865
46  feet           Y    =        -5151383
79  meter
 Z    =      -13548603
63                 Z    =        -4129614
39
 XDOT =      14845
937335                 XDOT =        4525
041700
 YDOT =     -14448
716790  feet/sec       YDOT =       -4403
968878  meter/sec
 ZDOT =      12417
967446                 ZDOT =        3784
996478


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   15340
83290052  
00016717  00000-0  10270-3 0  9122
2 25544  51
6416 302
4408 0008165 249
0077 111
0203 15
54610659 14909


Satellite: ISS
Catalog Number: 25544
Epoch time:      15340
83290052   =   yrday
fracday
Element set:     912
Inclination:       51
6416  deg
RA of node:       302
4408  deg
Eccentricity:     
0008165     
Arg of perigee:   249
0077  deg
Mean anomaly:     111
0203  deg
Mean motion:   15
54610659  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1490
Checksum:              275


Coasting Arc #14 (Orbit 1505)
---------------------------------------

Vector Time (GMT): 2015/341/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -682483
40                 A    =         6784619
10  meter
 Y    =        6175613
94  meter          E    =           
0007308
 Z    =        2713408
43                 I    =           51
32651
 XDOT =      -5445
298681                 Wp   =          132
64401
 YDOT =       1658
808122  meter/sec      RA   =          296
76573  deg
 ZDOT =      -5141
020401                 TA   =           16
51722
                                          MA   =           16
49342
                                          Ha   =            218
785  n
mi
                                          Hp   =            217
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2239118
77                 X    =         -764670
82
 Y    =       20261200
61  feet           Y    =         6167522
31  meter
 Z    =        8902258
64                 Z    =         2709893
66
 XDOT =     -17865
153154                 XDOT =       -5438
469664
 YDOT =       5442
283865  feet/sec       YDOT =        1597
953606  meter/sec
 ZDOT =     -16866
864833                 ZDOT =       -5167
456325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1960771
56                 X    =          597643
17
 Y    =       20297229
72  feet           Y    =         6186595
62  meter
 Z    =        8885828
74                 Z    =         2708400
60
 XDOT =     -14760
198111                 XDOT =       -4498
908384
 YDOT =       8865
808737  feet/sec       YDOT =        2702
298503  meter/sec
 ZDOT =     -16981
395043                 ZDOT =       -5175
929209


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   15341
86140689  
00016717  00000-0  10270-3 0  9137
2 25544  51
6421 297
3098 0008206 254
0347 105
9902 15
54677994 15065


Satellite: ISS
Catalog Number: 25544
Epoch time:      15341
86140689   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:       297
3098  deg
Eccentricity:     
0008206     
Arg of perigee:   254
0347  deg
Mean anomaly:     105
9902  deg
Mean motion:   15
54677994  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1506
Checksum:              326


Coasting Arc #15 (Orbit 1520)
---------------------------------------

Vector Time (GMT): 2015/342/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1767361
80                 A    =         6787415
89  meter
 Y    =       -6479673
81  meter          E    =           
0005992
 Z    =        -951017
43                 I    =           51
32077
 XDOT =       4888
892452                 Wp   =          343
17083
 YDOT =        468
661588  meter/sec      RA   =          291
76540  deg
 ZDOT =       5888
588708                 TA   =            6
48328
                                          MA   =            6
47554
                                          Ha   =            218
723  n
mi
                                          Hp   =            217
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5798431
09                 X    =         1844307
49
 Y    =      -21258772
35  feet           Y    =        -6459479
72  meter
 Z    =       -3120135
92                 Z    =         -942245
30
 XDOT =      16039
673400                 XDOT =        4854
683441
 YDOT =       1537
603636  feet/sec       YDOT =         523
140779  meter/sec
 ZDOT =      19319
516759                 ZDOT =        5912
255279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         899018
65                 X    =          274020
88
 Y    =      -22022534
50  feet           Y    =        -6712468
52  meter
 Z    =       -3080940
24                 Z    =         -939070
58
 XDOT =      14249
281621                 XDOT =        4343
181038
 YDOT =      -2137
104065  feet/sec       YDOT =        -651
389319  meter/sec
 ZDOT =      19421
655803                 ZDOT =        5919
720689


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   15342
82561387  
00016717  00000-0  10270-3 0  9147
2 25544  51
6407 292
4976 0008182 256
0384 103
9859 15
54657238 15211


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
82561387   =   yrday
fracday
Element set:     914
Inclination:       51
6407  deg
RA of node:       292
4976  deg
Eccentricity:     
0008182     
Arg of perigee:   256
0384  deg
Mean anomaly:     103
9859  deg
Mean motion:   15
54657238  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1521
Checksum:              332


Coasting Arc #16 (Orbit 1536)
---------------------------------------

Vector Time (GMT): 2015/343/19:46:15
827
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2649180
54                 A    =         6787237
35  meter
 Y    =        6170210
72  meter          E    =           
0009277
 Z    =        -944198
29                 I    =           51
30997
 XDOT =      -4122
463223                 Wp   =          191
03695
 YDOT =      -2671
570562  meter/sec      RA   =          286
77037  deg
 ZDOT =      -5891
097157                 TA   =          359
23923
                                          MA   =          359
24065
                                          Ha   =            218
295  n
mi
                                          Hp   =            217
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8691537
22                 X    =        -2713393
84
 Y    =       20243473
48  feet           Y    =         6140226
87  meter
 Z    =       -3097763
43                 Z    =         -957223
15
 XDOT =     -13525
141808                 XDOT =       -4063
665560
 YDOT =      -8764
995282  feet/sec       YDOT =       -2717
341448  meter/sec
 ZDOT =     -19327
746578                 ZDOT =       -5910
980940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3534084
62                 X    =        -1077188
99
 Y    =       21736875
08  feet           Y    =         6625399
52  meter
 Z    =       -3155262
84                 Z    =         -961724
11
 XDOT =     -13534
649368                 XDOT =       -4125
361127
 YDOT =      -5018
795976  feet/sec       YDOT =       -1529
729013  meter/sec
 ZDOT =     -19413
107075                 ZDOT =       -5917
115036


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   15343
85407859  
00016717  00000-0  10270-3 0  9155
2 25544  51
6409 287
3663 0008093 259
9955 100
0285 15
54713543 15376


Satellite: ISS
Catalog Number: 25544
Epoch time:      15343
85407859   =   yrday
fracday
Element set:     915
Inclination:       51
6409  deg
RA of node:       287
3663  deg
Eccentricity:     
0008093     
Arg of perigee:   259
9955  deg
Mean anomaly:     100
0285  deg
Mean motion:   15
54713543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1537
Checksum:              335
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