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

 
Date: September 19th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12647 59 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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


271/15:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 215 0

Coasting Arc #1 (Orbit 225)
---------------------------------------

Vector Time (GMT): 2015/259/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6666946
94                 A    =         6789111
94  meter
 Y    =        -580657
59  meter          E    =           
0010247
 Z    =        1104566
35                 I    =           51
58864
 XDOT =       -550
618726                 Wp   =           35
45786
 YDOT =       4895
835632  meter/sec      RA   =          347
50235  deg
 ZDOT =       5877
913391                 TA   =          336
53738
                                          MA   =          336
58411
                                          Ha   =            219
272  n
mi
                                          Hp   =            216
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21873185
49                 X    =         6667578
88
 Y    =       -1905044
58  feet           Y    =         -506099
71  meter
 Z    =        3623905
33                 Z    =         1136954
88
 XDOT =      -1806
491882                 XDOT =        -633
877102
 YDOT =      16062
452860  feet/sec       YDOT =        4889
213515  meter/sec
 ZDOT =      19284
492753                 ZDOT =        5875
035691

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21865615
48                 X    =        -6664639
60
 Y    =        1711149
95  feet           Y    =          521558
50  meter
 Z    =        3763635
68                 Z    =         1147156
16
 XDOT =       2196
519794                 XDOT =         669
499233
 YDOT =     -14451
988646  feet/sec       YDOT =       -4404
966139  meter/sec
 ZDOT =      19271
135243                 ZDOT =        5873
842022


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   15259
57653182  
00016717  00000-0  10270-3 0  9006
2 25544  51
6456 347
7403 0005609 280
0692  79
9827 15
54012208  2264


Satellite: ISS
Catalog Number: 25544
Epoch time:      15259
57653182   =   yrday
fracday
Element set:     900
Inclination:       51
6456  deg
RA of node:       347
7403  deg
Eccentricity:     
0005609     
Arg of perigee:   280
0692  deg
Mean anomaly:      79
9827  deg
Mean motion:   15
54012208  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             226
Checksum:              314


Coasting Arc #2 (Orbit 240)
---------------------------------------

Vector Time (GMT): 2015/260/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6228130
14                 A    =         6786475
94  meter
 Y    =        -269382
68  meter          E    =           
0001952
 Z    =       -2678947
82                 I    =           51
54805
 XDOT =       2450
306783                 Wp   =          225
82914
 YDOT =      -5087
094789  meter/sec      RA   =          342
52429  deg
 ZDOT =      -5184
024921                 TA   =          344
44642
                                          MA   =          344
45242
                                          Ha   =            219
406  n
mi
                                          Hp   =            216
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20433497
85                 X    =        -6211641
52
 Y    =        -883801
46  feet           Y    =         -338937
88  meter
 Z    =       -8789198
90                 Z    =        -2709163
03
 XDOT =       8039
064248                 XDOT =        2532
192055
 YDOT =     -16689
943534  feet/sec       YDOT =       -5059
236639  meter/sec
 ZDOT =     -17007
955779                 ZDOT =       -5171
922190

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20383645
78                 X    =         6212935
23
 Y    =         714486
68  feet           Y    =          217775
54  meter
 Z    =       -8919386
20                 Z    =        -2718628
91
 XDOT =      -7955
774100                 XDOT =       -2424
919946
 YDOT =      15272
481241  feet/sec       YDOT =        4655
052282  meter/sec
 ZDOT =     -16954
798670                 ZDOT =       -5167
822635


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   15260
54112355  
00016717  00000-0  10270-3 0  9018
2 25544  51
6443 342
9331 0005620 283
5930  76
4596 15
54031906  2411


Satellite: ISS
Catalog Number: 25544
Epoch time:      15260
54112355   =   yrday
fracday
Element set:     901
Inclination:       51
6443  deg
RA of node:       342
9331  deg
Eccentricity:     
0005620     
Arg of perigee:   283
5930  deg
Mean anomaly:      76
4596  deg
Mean motion:   15
54031906  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             241
Checksum:              283


Coasting Arc #3 (Orbit 256)
---------------------------------------

Vector Time (GMT): 2015/261/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5355860
55                 A    =         6782645
00  meter
 Y    =        1208609
41  meter          E    =           
0005246
 Z    =        3977971
21                 I    =           51
50602
 XDOT =      -4107
426903                 Wp   =           93
72581
 YDOT =       5115
819270  meter/sec      RA   =          337
53409  deg
 ZDOT =       3970
978891                 TA   =          314
83188
                                          MA   =          314
87451
                                          Ha   =            219
378  n
mi
                                          Hp   =            216
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17571720
96                 X    =         5322623
86
 Y    =        3965253
97  feet           Y    =         1268316
77  meter
 Z    =       13051086
63                 Z    =         4003908
30
 XDOT =     -13475
810049                 XDOT =       -4183
617663
 YDOT =      16784
183957  feet/sec       YDOT =        5069
461749  meter/sec
 ZDOT =      13028
145969                 ZDOT =        3950
840005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17583664
13                 X    =        -5359500
83
 Y    =       -3518383
35  feet           Y    =        -1072403
24  meter
 Z    =       13162644
61                 Z    =         4011974
08
 XDOT =      12868
916609                 XDOT =        3922
445782
 YDOT =     -15844
014968  feet/sec       YDOT =       -4829
255762  meter/sec
 ZDOT =      12940
350044                 ZDOT =        3944
218693


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   15261
57000564  
00016717  00000-0  10270-3 0  9021
2 25544  51
6447 337
8041 0005673 288
2488  71
8047 15
54079142  2575


Satellite: ISS
Catalog Number: 25544
Epoch time:      15261
57000564   =   yrday
fracday
Element set:     902
Inclination:       51
6447  deg
RA of node:       337
8041  deg
Eccentricity:     
0005673     
Arg of perigee:   288
2488  deg
Mean anomaly:      71
8047  deg
Mean motion:   15
54079142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             257
Checksum:              310


Coasting Arc #4 (Orbit 271)
---------------------------------------

Vector Time (GMT): 2015/262/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4150349
10                 A    =         6779298
21  meter
 Y    =       -2226289
63  meter          E    =           
0008553
 Z    =       -4883790
78                 I    =           51
46466
 XDOT =       5395
227293                 Wp   =           47
81786
 YDOT =      -4908
965200  meter/sec      RA   =          332
53231  deg
 ZDOT =      -2344
226005                 TA   =          199
14002
                                          MA   =          199
17218
                                          Ha   =            219
723  n
mi
                                          Hp   =            216
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13616630
91                 X    =        -4101421
90
 Y    =       -7304099
85  feet           Y    =        -2272428
48  meter
 Z    =      -16022935
64                 Z    =        -4903833
48
 XDOT =      17700
876945                 XDOT =        5461
107015
 YDOT =     -16105
528871  feet/sec       YDOT =       -4848
264088  meter/sec
 ZDOT =      -7691
030200                 ZDOT =       -2317
856325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13813936
82                 X    =         4210487
94
 Y    =        6721301
18  feet           Y    =         2048652
60  meter
 Z    =      -16108886
94                 Z    =        -4909988
74
 XDOT =     -16554
925773                 XDOT =       -5045
941375
 YDOT =      15842
748095  feet/sec       YDOT =        4828
869619  meter/sec
 ZDOT =      -7576
425500                 ZDOT =       -2309
294492


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   15262
53457111  
00016717  00000-0  10270-3 0  9033
2 25544  51
6437 332
9963 0005657 293
0258  67
0297 15
54067740  2726


Satellite: ISS
Catalog Number: 25544
Epoch time:      15262
53457111   =   yrday
fracday
Element set:     903
Inclination:       51
6437  deg
RA of node:       332
9963  deg
Eccentricity:     
0005657     
Arg of perigee:   293
0258  deg
Mean anomaly:      67
0297  deg
Mean motion:   15
54067740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             272
Checksum:              313


Coasting Arc #5 (Orbit 287)
---------------------------------------

Vector Time (GMT): 2015/263/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2713024
52                 A    =         6777422
05  meter
 Y    =        3267447
13  meter          E    =           
0003078
 Z    =        5283817
31                 I    =           51
43156
 XDOT =      -6244
951975                 Wp   =          304
42584
 YDOT =       4422
818843  meter/sec      RA   =          327
52053  deg
 ZDOT =        473
414920                 TA   =          141
05572
                                          MA   =          141
03355
                                          Ha   =            219
789  n
mi
                                          Hp   =            216
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8900999
07                 X    =         2650618
51
 Y    =       10719970
91  feet           Y    =         3297437
49  meter
 Z    =       17335358
61                 Z    =         5296844
88
 XDOT =     -20488
687583                 XDOT =       -6296
244556
 YDOT =      14510
560508  feet/sec       YDOT =        4352
696924  meter/sec
 ZDOT =       1553
198555                 ZDOT =         442
952988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9416753
92                 X    =        -2870226
60
 Y    =      -10175583
50  feet           Y    =        -3101517
85  meter
 Z    =       17390873
04                 Z    =         5300738
10
 XDOT =      18849
899902                 XDOT =        5745
449490
 YDOT =     -15026
134820  feet/sec       YDOT =       -4579
965893  meter/sec
 ZDOT =       1421
057506                 ZDOT =         433
138328


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   15263
56342422  
00016717  00000-0  10270-3 0  9046
2 25544  51
6442 327
8674 0005694 297
6019  62
4556 15
54124149  2881


Satellite: ISS
Catalog Number: 25544
Epoch time:      15263
56342422   =   yrday
fracday
Element set:     904
Inclination:       51
6442  deg
RA of node:       327
8674  deg
Eccentricity:     
0005694     
Arg of perigee:   297
6019  deg
Mean anomaly:      62
4556  deg
Mean motion:   15
54124149  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             288
Checksum:              321


Coasting Arc #6 (Orbit 302)
---------------------------------------

Vector Time (GMT): 2015/264/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1199438
26                 A    =         6778132
40  meter
 Y    =       -4255369
58  meter          E    =           
0008717
 Z    =       -5145176
70                 I    =           51
40689
 XDOT =       6602
278676                 Wp   =           86
88457
 YDOT =      -3608
616195  meter/sec      RA   =          322
50504  deg
 ZDOT =       1448
016148                 TA   =          197
09298
                                          MA   =          197
12236
                                          Ha   =            220
064  n
mi
                                          Hp   =            216
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3935164
88                 X    =        -1126771
09
 Y    =      -13961186
28  feet           Y    =        -4268376
60  meter
 Z    =      -16880500
99                 Z    =        -5150826
52
 XDOT =      21661
019278                 XDOT =        6635
106452
 YDOT =     -11839
291978  feet/sec       YDOT =       -3534
601498  meter/sec
 ZDOT =       4750
709147                 ZDOT =        1480
168890

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4892151
25                 X    =         1491127
70
 Y    =       13626157
16  feet           Y    =         4153252
70  meter
 Z    =      -16904030
76                 Z    =        -5152348
57
 XDOT =     -19659
733706                 XDOT =       -5992
286834
 YDOT =      13114
128938  feet/sec       YDOT =        3997
186500  meter/sec
 ZDOT =       4889
973544                 ZDOT =        1490
463936


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   15264
52796250  
00016717  00000-0  10270-3 0  9056
2 25544  51
6437 323
0589 0005680 303
2274  56
8333 15
54112281  3032


Satellite: ISS
Catalog Number: 25544
Epoch time:      15264
52796250   =   yrday
fracday
Element set:     905
Inclination:       51
6437  deg
RA of node:       323
0589  deg
Eccentricity:     
0005680     
Arg of perigee:   303
2274  deg
Mean anomaly:      56
8333  deg
Mean motion:   15
54112281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             303
Checksum:              292


Coasting Arc #7 (Orbit 318)
---------------------------------------

Vector Time (GMT): 2015/265/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -297989
90                 A    =         6780762
50  meter
 Y    =        5101390
81  meter          E    =           
0007840
 Z    =        4457431
87                 I    =           51
39184
 XDOT =      -6502
551149                 Wp   =           30
34668
 YDOT =       2455
265826  meter/sec      RA   =          317
49280  deg
 ZDOT =      -3235
548976                 TA   =           92
38585
                                          MA   =           92
29609
                                          Ha   =            220
182  n
mi
                                          Hp   =            216
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -977657
17                 X    =         -376665
31
 Y    =       16736846
48  feet           Y    =         5097618
96  meter
 Z    =       14624120
32                 Z    =         4455792
78
 XDOT =     -21333
829228                 XDOT =       -6513
806137
 YDOT =       8055
334075  feet/sec       YDOT =        2382
486818  meter/sec
 ZDOT =     -10615
318162                 ZDOT =       -3267
164683

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -510782
33                 X    =         -155686
45
 Y    =      -16764606
54  feet           Y    =        -5109852
07  meter
 Z    =       14616080
45                 Z    =         4454981
32
 XDOT =      19189
658478                 XDOT =        5849
007904
 YDOT =      -9984
893055  feet/sec       YDOT =       -3043
395403  meter/sec
 ZDOT =     -10752
040860                 ZDOT =       -3277
222054


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   15265
55678664  
00016717  00000-0  10270-3 0  9069
2 25544  51
6439 317
9300 0005729 307
4967  52
5664 15
54180774  3195


Satellite: ISS
Catalog Number: 25544
Epoch time:      15265
55678664   =   yrday
fracday
Element set:     906
Inclination:       51
6439  deg
RA of node:       317
9300  deg
Eccentricity:     
0005729     
Arg of perigee:   307
4967  deg
Mean anomaly:      52
5664  deg
Mean motion:   15
54180774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             319
Checksum:              338


Coasting Arc #8 (Orbit 333)
---------------------------------------

Vector Time (GMT): 2015/266/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1626484
24                 A    =         6784499
49  meter
 Y    =       -5691603
04  meter          E    =           
0004195
 Z    =       -3311058
55                 I    =           51
38180
 XDOT =       5990
296877                 Wp   =            7
95058
 YDOT =      -1007
028630  meter/sec      RA   =          312
48793  deg
 ZDOT =       4678
437446                 TA   =          313
38159
                                          MA   =          313
41652
                                          Ha   =            220
315  n
mi
                                          Hp   =            215
995

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5336234
37                 X    =         1706092
10
 Y    =      -18673238
31  feet           Y    =        -5672969
81  meter
 Z    =      -10863053
00                 Z    =        -3302963
53
 XDOT =      19653
204976                 XDOT =        5978
386430
 YDOT =      -3303
899705  feet/sec       YDOT =        -940
107345  meter/sec
 ZDOT =      15349
204220                 ZDOT =        4707
508273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3292913
96                 X    =        -1003680
18
 Y    =       19159907
39  feet           Y    =         5839939
77  meter
 Z    =      -10827087
00                 Z    =        -3300096
12
 XDOT =     -17668
408309                 XDOT =       -5385
330853
 YDOT =       5699
116432  feet/sec       YDOT =        1737
090688  meter/sec
 ZDOT =      15474
679002                 ZDOT =        4716
682160


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   15266
52129807  
00016717  00000-0  10270-3 0  9078
2 25544  51
6440 313
1214 0005506 312
6085  47
4602 15
54200102  3341


Satellite: ISS
Catalog Number: 25544
Epoch time:      15266
52129807   =   yrday
fracday
Element set:     907
Inclination:       51
6440  deg
RA of node:       313
1214  deg
Eccentricity:     
0005506     
Arg of perigee:   312
6085  deg
Mean anomaly:      47
4602  deg
Mean motion:   15
54200102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             334
Checksum:              263


Coasting Arc #9 (Orbit 349)
---------------------------------------

Vector Time (GMT): 2015/267/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2752851
71                 A    =         6787747
02  meter
 Y    =        5937419
36  meter          E    =           
0009004
 Z    =        1789009
75                 I    =           51
37181
 XDOT =      -5151
971485                 Wp   =          100
49746
 YDOT =       -683
621623  meter/sec      RA   =          307
49194  deg
 ZDOT =      -5636
198714                 TA   =           59
77598
                                          MA   =           59
68685
                                          Ha   =            220
495  n
mi
                                          Hp   =            215
836

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9031665
72                 X    =        -2827731
10
 Y    =       19479722
30  feet           Y    =         5906216
68  meter
 Z    =        5869454
57                 Z    =         1775454
44
 XDOT =     -16902
793586                 XDOT =       -5116
565677
 YDOT =      -2242
853093  feet/sec       YDOT =        -741
037019  meter/sec
 ZDOT =     -18491
465598                 ZDOT =       -5661
139856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6492494
77                 X    =         1978912
40
 Y    =      -20483490
30  feet           Y    =        -6243367
84  meter
 Z    =        5809922
59                 Z    =         1770864
40
 XDOT =      15439
953837                 XDOT =        4706
097930
 YDOT =       -402
729449  feet/sec       YDOT =        -122
751936  meter/sec
 ZDOT =     -18598
821905                 ZDOT =       -5668
920917


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   15267
55009373  
00016717  00000-0  10270-3 0  9088
2 25544  51
6438 307
9921 0005647 317
5195  42
5521 15
54215523  3503


Satellite: ISS
Catalog Number: 25544
Epoch time:      15267
55009373   =   yrday
fracday
Element set:     908
Inclination:       51
6438  deg
RA of node:       307
9921  deg
Eccentricity:     
0005647     
Arg of perigee:   317
5195  deg
Mean anomaly:      42
5521  deg
Mean motion:   15
54215523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             350
Checksum:              305


Coasting Arc #10 (Orbit 364)
---------------------------------------

Vector Time (GMT): 2015/268/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3582221
36                 A    =         6789121
02  meter
 Y    =       -5756114
35  meter          E    =           
0013898
 Z    =         -89667
92                 I    =           51
35751
 XDOT =       4107
776802                 Wp   =           20
76159
 YDOT =       2467
713445  meter/sec      RA   =          302
50124  deg
 ZDOT =       5991
665631                 TA   =          338
26825
                                          MA   =          338
32716
                                          Ha   =            220
665  n
mi
                                          Hp   =            215
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11752694
74                 X    =         3646756
96
 Y    =      -18884889
60  feet           Y    =        -5715694
76  meter
 Z    =        -294186
09                 Z    =          -72108
72
 XDOT =      13476
958013                 XDOT =        4050
771717
 YDOT =       8096
172719  feet/sec       YDOT =        2513
331364  meter/sec
 ZDOT =      19657
695641                 ZDOT =        6011
481588

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8882596
33                 X    =        -2707415
36
 Y    =       20393715
54  feet           Y    =         6216004
50  meter
 Z    =        -217447
03                 Z    =          -66277
86
 XDOT =     -12899
862807                 XDOT =       -3931
878184
 YDOT =      -5422
213133  feet/sec       YDOT =       -1652
690563  meter/sec
 ZDOT =      19742
632901                 ZDOT =        6017
554508


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   15268
51457695  
00016717  00000-0  10270-3 0  9090
2 25544  51
6436 303
1837 0005690 322
2421  37
8332 15
54200291  3657


Satellite: ISS
Catalog Number: 25544
Epoch time:      15268
51457695   =   yrday
fracday
Element set:     909
Inclination:       51
6436  deg
RA of node:       303
1837  deg
Eccentricity:     
0005690     
Arg of perigee:   322
2421  deg
Mean anomaly:      37
8332  deg
Mean motion:   15
54200291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             365
Checksum:              301


Coasting Arc #11 (Orbit 380)
---------------------------------------

Vector Time (GMT): 2015/269/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4148274
50                 A    =         6787817
31  meter
 Y    =        5113361
87  meter          E    =           
0002198
 Z    =       -1646622
43                 I    =           51
33702
 XDOT =      -2937
463157                 Wp   =          132
74310
 YDOT =      -4212
801506  meter/sec      RA   =          297
50914  deg
 ZDOT =      -5688
350306                 TA   =           65
35847
                                          MA   =           65
33558
                                          Ha   =            220
735  n
mi
                                          Hp   =            215
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13609824
48                 X    =        -4197146
36
 Y    =       16776121
62  feet           Y    =         5066699
63  meter
 Z    =       -5402304
58                 Z    =        -1666893
43
 XDOT =      -9637
346314                 XDOT =       -2862
504370
 YDOT =     -13821
527252  feet/sec       YDOT =       -4245
231885  meter/sec
 ZDOT =     -18662
566620                 ZDOT =       -5702
437242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10669653
28                 X    =         3252110
32
 Y    =      -18757993
35  feet           Y    =        -5717436
37  meter
 Z    =       -5490597
25                 Z    =        -1673534
04
 XDOT =      10269
187190                 XDOT =        3130
048256
 YDOT =      11315
417315  feet/sec       YDOT =        3448
939198  meter/sec
 ZDOT =     -18722
497738                 ZDOT =       -5706
617311


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   15269
54334341  
00016717  00000-0  10270-3 0  9108
2 25544  51
6433 298
0539 0005593 325
6955  34
3835 15
54238769  3815


Satellite: ISS
Catalog Number: 25544
Epoch time:      15269
54334341   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:       298
0539  deg
Eccentricity:     
0005593     
Arg of perigee:   325
6955  deg
Mean anomaly:      34
3835  deg
Mean motion:   15
54238769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             381
Checksum:              327


Coasting Arc #12 (Orbit 396)
---------------------------------------

Vector Time (GMT): 2015/270/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4430054
51                 A    =         6784579
24  meter
 Y    =       -4015918
32  meter          E    =           
0011530
 Z    =        3190612
05                 I    =           51
31115
 XDOT =       1760
367471                 Wp   =           60
29675
 YDOT =       5741
968351  meter/sec      RA   =          292
50921  deg
 ZDOT =       4775
621116                 TA   =          336
79753
                                          MA   =          336
84954
                                          Ha   =            220
796  n
mi
                                          Hp   =            215
250

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14534299
57                 X    =         4459133
35
 Y    =      -13175585
04  feet           Y    =        -3966215
44  meter
 Z    =       10467887
30                 Z    =         3212203
76
 XDOT =       5775
483828                 XDOT =        1672
830251
 YDOT =      18838
478842  feet/sec       YDOT =        5761
165246  meter/sec
 ZDOT =      15668
048281                 ZDOT =        4783
959153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11869037
38                 X    =        -3617682
59
 Y    =       15556216
73  feet           Y    =         4741534
86  meter
 Z    =       10561659
08                 Z    =         3219193
69
 XDOT =      -7828
595175                 XDOT =       -2386
155809
 YDOT =     -16650
637807  feet/sec       YDOT =       -5075
114403  meter/sec
 ZDOT =      15702
934174                 ZDOT =        4786
254336


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   15270
57209510  
00016717  00000-0  10270-3 0  9113
2 25544  51
6420 292
9239 0005655 331
3272  28
7569 15
54249506  3975


Satellite: ISS
Catalog Number: 25544
Epoch time:      15270
57209510   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:       292
9239  deg
Eccentricity:     
0005655     
Arg of perigee:   331
3272  deg
Mean anomaly:      28
7569  deg
Mean motion:   15
54249506  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             397
Checksum:              312


Coasting Arc #13 (Orbit 411)
---------------------------------------

Vector Time (GMT): 2015/271/12:20:48
186
Vector Time (MET): N/A
Weight (LBS)     : 926984
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4499839
79                 A    =         6780550
86  meter
 Y    =        2535155
05  meter          E    =           
0010305
 Z    =       -4403329
07                 I    =           51
28693
 XDOT =       -621
712926                 Wp   =           36
12531
 YDOT =      -6875
376285  meter/sec      RA   =          287
49782  deg
 ZDOT =      -3318
872103                 TA   =          200
12370
                                          MA   =          200
16436
                                          Ha   =            220
942  n
mi
                                          Hp   =            214
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14763253
92                 X    =        -4506464
13
 Y    =        8317437
83  feet           Y    =         2484797
16  meter
 Z    =      -14446617
68                 Z    =        -4425205
12
 XDOT =      -2039
740571                 XDOT =        -528
662588
 YDOT =     -22557
008810  feet/sec       YDOT =       -6881
808927  meter/sec
 ZDOT =     -10888
688003                 ZDOT =       -3321
665219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12752941
49                 X    =         3887096
57
 Y    =      -11034045
32  feet           Y    =        -3363177
01  meter
 Z    =      -14541338
59                 Z    =        -4432200
00
 XDOT =       5555
082492                 XDOT =        1693
189144
 YDOT =      20802
463744  feet/sec       YDOT =        6340
590949  meter/sec
 ZDOT =     -10899
484048                 ZDOT =       -3322
162738


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   15271
53653405  
00016717  00000-0  10270-3 0  9127
2 25544  51
6422 288
1147 0005665 334
0263  26
0605 15
54288345  4127


Satellite: ISS
Catalog Number: 25544
Epoch time:      15271
53653405   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:       288
1147  deg
Eccentricity:     
0005665     
Arg of perigee:   334
0263  deg
Mean anomaly:      26
0605  deg
Mean motion:   15
54288345  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             412
Checksum:              288


Coasting Arc #14 (Orbit 413)
---------------------------------------

Vector Time (GMT): 2015/271/15:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892142
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3866515
47                 A    =         6785244
11  meter
 Y    =        4772347
29  meter          E    =           
0003776
 Z    =       -2889424
10                 I    =           51
29994
 XDOT =      -2629
033722                 Wp   =           25
47592
 YDOT =      -5164
757884  meter/sec      RA   =          286
87314  deg
 ZDOT =      -5011
457997                 TA   =          187
57903
                                          MA   =          187
58474
                                          Ha   =            221
011  n
mi
                                          Hp   =            214
988

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12685418
19                 X    =        -3905557
75
 Y    =       15657307
37  feet           Y    =         4728890
62  meter
 Z    =       -9479737
85                 Z    =        -2908302
64
 XDOT =      -8625
438722                 XDOT =       -2546
740699
 YDOT =     -16944
743713  feet/sec       YDOT =       -5193
698112  meter/sec
 ZDOT =     -16441
791330                 ZDOT =       -5024
028792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6001271
34                 X    =        -1829187
50
 Y    =      -19196106
21  feet           Y    =        -5850973
17  meter
 Z    =       -9561944
75                 Z    =        -2914480
76
 XDOT =      17423
733849                 XDOT =        5310
754077
 YDOT =       2770
764389  feet/sec       YDOT =         844
528986  meter/sec
 ZDOT =     -16495
028404                 ZDOT =       -5027
684658


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   15271
66512566  
00016717  00000-0  10270-3 0  9134
2 25544  51
6407 287
4725 0005897 334
7044  25
3820 15
54295200  4146


Satellite: ISS
Catalog Number: 25544
Epoch time:      15271
66512566   =   yrday
fracday
Element set:     913
Inclination:       51
6407  deg
RA of node:       287
4725  deg
Eccentricity:     
0005897     
Arg of perigee:   334
7044  deg
Mean anomaly:      25
3820  deg
Mean motion:   15
54295200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             414
Checksum:              304


Coasting Arc #15 (Orbit 429)
---------------------------------------

Vector Time (GMT): 2015/272/15:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892142
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4133322
94                 A    =         6781171
79  meter
 Y    =       -3368388
66  meter          E    =           
0007884
 Z    =        4181502
98                 I    =           51
27877
 XDOT =       1625
239401                 Wp   =           70
32458
 YDOT =       6543
661290  meter/sec      RA   =          281
86350  deg
 ZDOT =       3661
665076                 TA   =          341
94965
                                          MA   =          341
97763
                                          Ha   =            220
837  n
mi
                                          Hp   =            214
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13560770
81                 X    =         4150369
41
 Y    =      -11051143
89  feet           Y    =        -3322071
23  meter
 Z    =       13718841
81                 Z    =         4201624
02
 XDOT =       5332
150265                 XDOT =        1534
158542
 YDOT =      21468
705020  feet/sec       YDOT =        6561
327027  meter/sec
 ZDOT =      12013
336862                 ZDOT =        3669
338159

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1998110
31                 X    =          609024
02
 Y    =       17309732
54  feet           Y    =         5276006
48  meter
 Z    =       13806144
34                 Z    =         4208112
79
 XDOT =     -19634
841220                 XDOT =       -5984
699604
 YDOT =      -7348
593995  feet/sec       YDOT =       -2239
851450  meter/sec
 ZDOT =      12045
228454                 ZDOT =        3671
385633


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   15272
69384254  
00016717  00000-0  10270-3 0  9140
2 25544  51
6409 282
3428 0005851 336
4984  23
5901 15
54346903  4309


Satellite: ISS
Catalog Number: 25544
Epoch time:      15272
69384254   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       282
3428  deg
Eccentricity:     
0005851     
Arg of perigee:   336
4984  deg
Mean anomaly:      23
5901  deg
Mean motion:   15
54346903  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             430
Checksum:              313


Coasting Arc #16 (Orbit 444)
---------------------------------------

Vector Time (GMT): 2015/273/15:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 892142
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4255875
35                 A    =         6777946
65  meter
 Y    =        1650622
35  meter          E    =           
0013888
 Z    =       -5022221
27                 I    =           51
26251
 XDOT =       -636
606432                 Wp   =           50
55965
 YDOT =      -7395
530758  meter/sec      RA   =          276
84118  deg
 ZDOT =      -1886
017727                 TA   =          201
00836
                                          MA   =          201
06547
                                          Ha   =            221
159  n
mi
                                          Hp   =            214
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13962845
62                 X    =        -4249620
24
 Y    =        5415427
67  feet           Y    =         1603064
74  meter
 Z    =      -16477103
92                 Z    =        -5042880
81
 XDOT =      -2088
603778                 XDOT =        -544
698781
 YDOT =     -24263
552355  feet/sec       YDOT =       -7402
136043  meter/sec
 ZDOT =      -6187
722201                 ZDOT =       -1888
886192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2697592
33                 X    =          822226
14
 Y    =      -14630777
61  feet           Y    =        -4459461
01  meter
 Z    =      -16566418
15                 Z    =        -5049444
25
 XDOT =      20637
269697                 XDOT =        6290
239804
 YDOT =      10842
978659  feet/sec       YDOT =        3304
939895  meter/sec
 ZDOT =      -6198
766014                 ZDOT =       -1889
383881


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   15273
65825192  
00016717  00000-0  10270-3 0  9159
2 25544  51
6412 277
5325 0005944 341
5678  18
5259 15
54333563  4459


Satellite: ISS
Catalog Number: 25544
Epoch time:      15273
65825192   =   yrday
fracday
Element set:     915
Inclination:       51
6412  deg
RA of node:       277
5325  deg
Eccentricity:     
0005944     
Arg of perigee:   341
5678  deg
Mean anomaly:      18
5259  deg
Mean motion:   15
54333563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             445
Checksum:              322
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