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

 
Date: December 12th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 ET - UTC (sec) : 68 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


346/16:46:55 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 5

348/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 215 5

348/05:14:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

349/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

351/07:21:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 7

353/08:42:47 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 215 7

Coasting Arc #1 (Orbit 931)
---------------------------------------

Vector Time (GMT): 2017/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5286256
96                 A    =         6784773
25  meter
 Y    =       -2759533
49  meter          E    =           
0002623
 Z    =       -3239758
55                 I    =           51
34069
 XDOT =        240
986662                 Wp   =          120
53580
 YDOT =      -6019
622041  meter/sec      RA   =          233
32704  deg
 ZDOT =       4735
690106                 TA   =          201
77697
                                          MA   =          201
78812
                                          Ha   =            220
312  n
mi
                                          Hp   =            215
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17343362
73                 X    =        -5239269
00
 Y    =       -9053587
57  feet           Y    =        -2818385
18  meter
 Z    =      -10629129
10                 Z    =        -3265323
65
 XDOT =        790
638655                 XDOT =         285
278012
 YDOT =     -19749
416146  feet/sec       YDOT =       -6016
679696  meter/sec
 ZDOT =      15537
041031                 ZDOT =        4736
968099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12044537
62                 X    =         3671175
07
 Y    =      -15338593
21  feet           Y    =        -4675203
21  meter
 Z    =      -10742194
18                 Z    =        -3274220
79
 XDOT =      18175
146534                 XDOT =        5539
784663
 YDOT =       3389
716319  feet/sec       YDOT =        1033
185534  meter/sec
 ZDOT =      15543
587567                 ZDOT =        4737
685490


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   17345
50679192  
00016717  00000-0  10270-3 0  9006
2 25544  51
6415 234
3641 0002987 231
6610 128
4275 15
54132487  9325


Satellite: ISS
Catalog Number: 25544
Epoch time:      17345
50679192   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:       234
3641  deg
Eccentricity:     
0002987     
Arg of perigee:   231
6610  deg
Mean anomaly:     128
4275  deg
Mean motion:   15
54132487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             932
Checksum:              305


Coasting Arc #2 (Orbit 947)
---------------------------------------

Vector Time (GMT): 2017/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5291584
94                 A    =         6788093
62  meter
 Y    =        3874167
89  meter          E    =           
0012851
 Z    =        1723427
80                 I    =           51
37209
 XDOT =      -1719
065579                 Wp   =          126
82869
 YDOT =       4877
931006  meter/sec      RA   =          228
33113  deg
 ZDOT =      -5665
350906                 TA   =           34
18521
                                          MA   =           34
10253
                                          Ha   =            220
298  n
mi
                                          Hp   =            215
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17360842
98                 X    =         5239498
04
 Y    =       12710524
57  feet           Y    =         3933050
70  meter
 Z    =        5654290
67                 Z    =         1749006
52
 XDOT =      -5639
978935                 XDOT =       -1745
964446
 YDOT =      16003
710650  feet/sec       YDOT =        4858
557082  meter/sec
 ZDOT =     -18587
109271                 ZDOT =       -5673
766781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15393644
70                 X    =        -4691982
90
 Y    =       14990050
54  feet           Y    =         4568967
40  meter
 Z    =        5767269
27                 Z    =         1757863
67
 XDOT =     -13780
097381                 XDOT =       -4200
173682
 YDOT =      -6958
330416  feet/sec       YDOT =       -2120
899111  meter/sec
 ZDOT =     -18625
166111                 ZDOT =       -5676
950631


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   17346
53562724  
00016717  00000-0  10270-3 0  9013
2 25544  51
6418 229
2358 0002919 232
7995 127
2891 15
54103759  9487


Satellite: ISS
Catalog Number: 25544
Epoch time:      17346
53562724   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:       229
2358  deg
Eccentricity:     
0002919     
Arg of perigee:   232
7995  deg
Mean anomaly:     127
2891  deg
Mean motion:   15
54103759  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             948
Checksum:              334


Coasting Arc #3 (Orbit 950)
---------------------------------------

Vector Time (GMT): 2017/346/16:46:55
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3519179
90                 A    =         6788295
74  meter
 Y    =        5599747
21  meter          E    =           
0008773
 Z    =       -1507530
89                 I    =           51
37367
 XDOT =      -4851
515381                 Wp   =          161
88118
 YDOT =       1507
184052  meter/sec      RA   =          227
35856  deg
 ZDOT =      -5744
114435                 TA   =           34
64606
                                          MA   =           34
58894
                                          Ha   =            220
270  n
mi
                                          Hp   =            215
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11545865
82                 X    =         3463623
38
 Y    =       18371874
06  feet           Y    =         5638790
52  meter
 Z    =       -4945967
49                 Z    =        -1490570
36
 XDOT =     -15917
045212                 XDOT =       -4840
106229
 YDOT =       4944
829567  feet/sec       YDOT =        1452
995139  meter/sec
 ZDOT =     -18845
519800                 ZDOT =       -5767
654005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1762017
84                 X    =          537063
04
 Y    =       21643919
90  feet           Y    =         6597066
78  meter
 Z    =       -4871487
79                 Z    =        -1484829
48
 XDOT =     -14709
204157                 XDOT =       -4483
365427
 YDOT =      -3054
846441  feet/sec       YDOT =        -931
117195  meter/sec
 ZDOT =     -18950
222567                 ZDOT =       -5776
027838


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   17346
72853156  
00016717  00000-0  10270-3 0  9027
2 25544  51
6379 228
2691 0002881 233
3882 126
7006 15
54161857  9511


Satellite: ISS
Catalog Number: 25544
Epoch time:      17346
72853156   =   yrday
fracday
Element set:     902
Inclination:       51
6379  deg
RA of node:       228
2691  deg
Eccentricity:     
0002881     
Arg of perigee:   233
3882  deg
Mean anomaly:     126
7006  deg
Mean motion:   15
54161857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             951
Checksum:              322


Coasting Arc #4 (Orbit 966)
---------------------------------------

Vector Time (GMT): 2017/347/16:46:55
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2470082
71                 A    =         6785421
18  meter
 Y    =       -5536932
48  meter          E    =           
0010578
 Z    =        3038189
80                 I    =           51
38556
 XDOT =       5893
554109                 Wp   =           92
47164
 YDOT =         71
338200  meter/sec      RA   =          222
36480  deg
 ZDOT =       4906
276114                 TA   =          302
51369
                                          MA   =          302
61586
                                          Ha   =            220
295  n
mi
                                          Hp   =            215
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8103945
89                 X    =        -2422741
84
 Y    =      -18165788
97  feet           Y    =        -5564290
10  meter
 Z    =        9967814
30                 Z    =         3026305
46
 XDOT =      19335
807444                 XDOT =        5868
485850
 YDOT =        234
049214  feet/sec       YDOT =         137
103510  meter/sec
 ZDOT =      16096
706410                 ZDOT =        4934
844570

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         822060
28                 X    =          250563
97
 Y    =      -19900435
95  feet           Y    =        -6065652
88  meter
 Z    =        9915846
70                 Z    =         3022350
07
 XDOT =      15640
591632                 XDOT =        4767
252329
 YDOT =       8754
906727  feet/sec       YDOT =        2668
495570  meter/sec
 ZDOT =      16223
516828                 ZDOT =        4944
927929


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   17347
75736400  
00016717  00000-0  10270-3 0  9034
2 25544  51
6367 223
1400 0003099 232
6274 127
4596 15
54141234  9675


Satellite: ISS
Catalog Number: 25544
Epoch time:      17347
75736400   =   yrday
fracday
Element set:     903
Inclination:       51
6367  deg
RA of node:       223
1400  deg
Eccentricity:     
0003099     
Arg of perigee:   232
6274  deg
Mean anomaly:     127
4596  deg
Mean motion:   15
54141234  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             967
Checksum:              303


Coasting Arc #5 (Orbit 971)
---------------------------------------

Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2643991
67                 A    =         6777399
55  meter
 Y    =        3311610
80  meter          E    =           
0012448
 Z    =       -5299918
35                 I    =           51
37119
 XDOT =      -5886
244194                 Wp   =           96
29358
 YDOT =      -4899
424172  meter/sec      RA   =          220
52844  deg
 ZDOT =       -126
465286                 TA   =          172
50469
                                          MA   =          172
48607
                                          Ha   =            220
244  n
mi
                                          Hp   =            215
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8674513
35                 X    =        -2655081
82
 Y    =       10864864
83  feet           Y    =         3281982
19  meter
 Z    =      -17388183
56                 Z    =        -5312788
90
 XDOT =     -19311
824784                 XDOT =       -5830
405727
 YDOT =     -16074
226285  feet/sec       YDOT =       -4964
935959  meter/sec
 ZDOT =       -414
912355                 ZDOT =        -154
923803

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12665298
57                 X    =         3860383
01
 Y    =        5556614
74  feet           Y    =         1693656
17  meter
 Z    =      -17445791
52                 Z    =        -5317477
25
 XDOT =     -10303
341039                 XDOT =       -3140
458349
 YDOT =      21803
828158  feet/sec       YDOT =        6645
806822  meter/sec
 ZDOT =       -540
553056                 ZDOT =        -164
760571


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   17348
07887391  
00016717  00000-0  10270-3 0  9047
2 25544  51
6404 221
5409 0002959 236
9186 123
1683 15
54116465  9725


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
07887391   =   yrday
fracday
Element set:     904
Inclination:       51
6404  deg
RA of node:       221
5409  deg
Eccentricity:     
0002959     
Arg of perigee:   236
9186  deg
Mean anomaly:     123
1683  deg
Mean motion:   15
54116465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             972
Checksum:              326


Coasting Arc #6 (Orbit 974)
---------------------------------------

Vector Time (GMT): 2017/348/05:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904510
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -101617
32                 A    =         6780059
24  meter
 Y    =       -4924778
36  meter          E    =           
0006878
 Z    =        4657180
24                 I    =           51
38115
 XDOT =       6641
311573                 Wp   =          136
83785
 YDOT =       2565
246378  meter/sec      RA   =          219
76970  deg
 ZDOT =       2850
129496                 TA   =          284
72076
                                          MA   =          284
79698
                                          Ha   =            220
118  n
mi
                                          Hp   =            215
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -333390
15                 X    =          -69162
10
 Y    =      -16157409
33  feet           Y    =        -4925733
55  meter
 Z    =       15279462
73                 Z    =         4656765
12
 XDOT =      21789
079963                 XDOT =        6598
288031
 YDOT =       8416
162657  feet/sec       YDOT =        2639
273323  meter/sec
 ZDOT =       9350
818555                 ZDOT =        2882
286924

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4896159
44                 X    =        -1492349
40
 Y    =       15402453
64  feet           Y    =         4694667
87  meter
 Z    =       15278319
64                 Z    =         4656831
83
 XDOT =     -16634
484316                 XDOT =       -5070
190820
 YDOT =     -14728
667754  feet/sec       YDOT =       -4489
297931  meter/sec
 ZDOT =       9493
214698                 ZDOT =        2893
531840


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   17348
27177885  
00016717  00000-0  10270-3 0  9050
2 25544  51
6374 220
5800 0003005 241
3071 118
7780 15
54152247  9750


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
27177885   =   yrday
fracday
Element set:     905
Inclination:       51
6374  deg
RA of node:       220
5800  deg
Eccentricity:     
0003005     
Arg of perigee:   241
3071  deg
Mean anomaly:     118
7780  deg
Mean motion:   15
54152247  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             975
Checksum:              304


Coasting Arc #7 (Orbit 989)
---------------------------------------

Vector Time (GMT): 2017/349/05:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904510
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1435701
94                 A    =         6777726
03  meter
 Y    =        4082267
20  meter          E    =           
0011599
 Z    =       -5226608
78                 I    =           51
39948
 XDOT =      -6663
684919                 Wp   =           86
41379
 YDOT =      -3639
182857  meter/sec      RA   =          214
75512  deg
 ZDOT =      -1013
184431                 TA   =          173
84920
                                          MA   =          173
83495
                                          Ha   =            220
129  n
mi
                                          Hp   =            215
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4710308
22                 X    =        -1455855
70
 Y    =       13393265
10  feet           Y    =         4066099
93  meter
 Z    =      -17147666
60                 Z    =        -5233631
67
 XDOT =     -21862
483330                 XDOT =       -6617
573738
 YDOT =     -11939
576301  feet/sec       YDOT =       -3713
442832  meter/sec
 ZDOT =      -3324
095901                 ZDOT =       -1045
443166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8547626
92                 X    =         2605316
68
 Y    =      -11287800
89  feet           Y    =        -3440521
71  meter
 Z    =      -17179425
15                 Z    =        -5236288
79
 XDOT =      16199
210842                 XDOT =        4937
519465
 YDOT =      17536
894957  feet/sec       YDOT =        5345
245583  meter/sec
 ZDOT =      -3466
808693                 ZDOT =       -1056
683290


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   17349
23630664  
00016717  00000-0  10270-3 0  9067
2 25544  51
6379 215
7712 0002853 244
8507 115
2350 15
54128220  9901


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
23630664   =   yrday
fracday
Element set:     906
Inclination:       51
6379  deg
RA of node:       215
7712  deg
Eccentricity:     
0002853     
Arg of perigee:   244
8507  deg
Mean anomaly:     115
2350  deg
Mean motion:   15
54128220  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             990
Checksum:              302


Coasting Arc #8 (Orbit 993)
---------------------------------------

Vector Time (GMT): 2017/349/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6082098
58                 A    =         6788375
79  meter
 Y    =        2598492
12  meter          E    =           
0012314
 Z    =        1498218
72                 I    =           51
44502
 XDOT =       -722
418883                 Wp   =          128
88730
 YDOT =       5021
895632  meter/sec      RA   =          213
53520  deg
 ZDOT =      -5752
900028                 TA   =           34
70251
                                          MA   =           34
62224
                                          Ha   =            220
090  n
mi
                                          Hp   =            215
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19954391
67                 X    =         6045311
83
 Y    =        8525236
62  feet           Y    =         2666300
49  meter
 Z    =        4915415
75                 Z    =         1527674
83
 XDOT =      -2370
140693                 XDOT =        -750
576340
 YDOT =      16476
035537  feet/sec       YDOT =        5013
660096  meter/sec
 ZDOT =     -18874
343925                 ZDOT =       -5756
477318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15254099
13                 X    =        -4649449
41
 Y    =       15390604
65  feet           Y    =         4691056
30  meter
 Z    =        5045836
55                 Z    =         1537970
98
 XDOT =     -13371
888047                 XDOT =       -4075
751477
 YDOT =      -7034
381787  feet/sec       YDOT =       -2144
079569  meter/sec
 ZDOT =     -18890
936617                 ZDOT =       -5757
957481


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   17349
49351412  
00016717  00000-0  10270-3 0  9077
2 25544  51
6414 214
4914 0002920 245
9089 114
1758 15
54112354  9948


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
49351412   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       214
4914  deg
Eccentricity:     
0002920     
Arg of perigee:   245
9089  deg
Mean anomaly:     114
1758  deg
Mean motion:   15
54112354  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             994
Checksum:              309


Coasting Arc #9 (Orbit 1009)
---------------------------------------

Vector Time (GMT): 2017/350/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5880997
68                 A    =         6789230
50  meter
 Y    =       -3376079
09  meter          E    =           
0009826
 Z    =         194304
03                 I    =           51
47551
 XDOT =       2531
807121                 Wp   =           39
61734
 YDOT =      -4056
060441  meter/sec      RA   =          208
55151  deg
 ZDOT =       5995
054543                 TA   =          322
48075
                                          MA   =          322
54929
                                          Ha   =            219
935  n
mi
                                          Hp   =            215
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19294611
80                 X    =        -5843752
21
 Y    =      -11076374
97  feet           Y    =        -3441636
19  meter
 Z    =         637480
43                 Z    =          165825
86
 XDOT =       8306
453810                 XDOT =        2547
853641
 YDOT =     -13307
284910  feet/sec       YDOT =       -4027
658916  meter/sec
 ZDOT =      19668
814119                 ZDOT =        6007
391952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17155648
09                 X    =         5229041
54
 Y    =      -14170272
49  feet           Y    =        -4319099
06  meter
 Z    =         511492
50                 Z    =          155902
91
 XDOT =       8546
663944                 XDOT =        2605
023170
 YDOT =      11082
861311  feet/sec       YDOT =        3378
056128  meter/sec
 ZDOT =      19724
171291                 ZDOT =        6011
927410


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   17350
52233701  
00016717  00000-0  10270-3 0  9084
2 25544  51
6408 209
3619 0002979 253
8255 106
2570 15
54159278 10103


Satellite: ISS
Catalog Number: 25544
Epoch time:      17350
52233701   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       209
3619  deg
Eccentricity:     
0002979     
Arg of perigee:   253
8255  deg
Mean anomaly:     106
2570  deg
Mean motion:   15
54159278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1010
Checksum:              301


Coasting Arc #10 (Orbit 1022)
---------------------------------------

Vector Time (GMT): 2017/351/07:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -555052
08                 A    =         6778776
68  meter
 Y    =       -4586499
24  meter          E    =           
0004823
 Z    =        4959909
19                 I    =           51
46317
 XDOT =       7232
755934                 Wp   =          150
17244
 YDOT =       1419
601312  meter/sec      RA   =          204
32967  deg
 ZDOT =       2117
136818                 TA   =          279
13307
                                          MA   =          279
18763
                                          Ha   =            219
918  n
mi
                                          Hp   =            215
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1821037
00                 X    =         -527816
31
 Y    =      -15047569
69  feet           Y    =        -4592554
47  meter
 Z    =       16272667
93                 Z    =         4957278
55
 XDOT =      23729
514219                 XDOT =        7206
059944
 YDOT =       4657
484620  feet/sec       YDOT =        1500
333435  meter/sec
 ZDOT =       6945
986935                 ZDOT =        2152
206833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5877757
09                 X    =         1791540
36
 Y    =       13984158
31  feet           Y    =         4262371
45  meter
 Z    =       16261627
81                 Z    =         4956544
16
 XDOT =     -23047
178303                 XDOT =       -7024
779947
 YDOT =       1409
928582  feet/sec       YDOT =         429
746232  meter/sec
 ZDOT =       7101
542572                 ZDOT =        2164
550176


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   17351
35825686  
00016717  00000-0  10270-3 0  9096
2 25544  51
6386 205
1945 0002990 255
4180 104
6641 15
54172125 10233


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
35825686   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       205
1945  deg
Eccentricity:     
0002990     
Arg of perigee:   255
4180  deg
Mean anomaly:     104
6641  deg
Mean motion:   15
54172125  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1023
Checksum:              303


Coasting Arc #11 (Orbit 1037)
---------------------------------------

Vector Time (GMT): 2017/352/07:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1173899
15                 A    =         6777297
12  meter
 Y    =        4062902
42  meter          E    =           
0011990
 Z    =       -5306286
06                 I    =           51
48894
 XDOT =      -7279
166999                 Wp   =           90
22734
 YDOT =      -2375
578113  meter/sec      RA   =          199
31898  deg
 ZDOT =       -209
026534                 TA   =          177
77678
                                          MA   =          177
77145
                                          Ha   =            219
923  n
mi
                                          Hp   =            215
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3851375
16                 X    =        -1193468
96
 Y    =       13329732
33  feet           Y    =         4049666
27  meter
 Z    =      -17409075
00                 Z    =        -5312035
58
 XDOT =     -23881
781494                 XDOT =       -7251
046293
 YDOT =      -7793
891446  feet/sec       YDOT =       -2456
821476  meter/sec
 ZDOT =       -685
782592                 ZDOT =        -244
318549

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -197997
64                 X    =          -60349
68
 Y    =      -13840736
62  feet           Y    =        -4218656
52  meter
 Z    =      -17435181
50                 Z    =        -5314243
32
 XDOT =      24097
596113                 XDOT =        7344
947295
 YDOT =        714
331022  feet/sec       YDOT =         217
728096  meter/sec
 ZDOT =       -842
215978                 ZDOT =        -256
707430


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   17352
32277846  
00016717  00000-0  10270-3 0  9105
2 25544  51
6391 200
3858 0002882 260
6811  99
4015 15
54156139 10387


Satellite: ISS
Catalog Number: 25544
Epoch time:      17352
32277846   =   yrday
fracday
Element set:     910
Inclination:       51
6391  deg
RA of node:       200
3858  deg
Eccentricity:     
0002882     
Arg of perigee:   260
6811  deg
Mean anomaly:      99
4015  deg
Mean motion:   15
54156139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1038
Checksum:              306


Coasting Arc #12 (Orbit 1053)
---------------------------------------

Vector Time (GMT): 2017/353/07:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2884235
03                 A    =         6778145
69  meter
 Y    =       -3433187
16  meter          E    =           
0003041
 Z    =        5082673
73                 I    =           51
52320
 XDOT =       6780
352913                 Wp   =           25
10817
 YDOT =       3142
161216  meter/sec      RA   =          194
31078  deg
 ZDOT =      -1722
099056                 TA   =           81
57798
                                          MA   =           81
54351
                                          Ha   =            219
759  n
mi
                                          Hp   =            215
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9462713
34                 X    =         2897722
37
 Y    =      -11263737
41  feet           Y    =        -3400858
86  meter
 Z    =       16675438
74                 Z    =         5096716
80
 XDOT =      22245
252339                 XDOT =        6753
077599
 YDOT =      10308
927875  feet/sec       YDOT =        3217
831453  meter/sec
 ZDOT =      -5649
931285                 ZDOT =       -1689
228100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5541135
59                 X    =        -1688938
13
 Y    =       13550275
01  feet           Y    =         4130123
82  meter
 Z    =       16738304
72                 Z    =         5101835
28
 XDOT =     -23360
559139                 XDOT =       -7120
298425
 YDOT =      -2741
088718  feet/sec       YDOT =        -835
483841  meter/sec
 ZDOT =      -5504
333607                 ZDOT =       -1677
720883


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   17353
35159636  
00016717  00000-0  10270-3 0  9116
2 25544  51
6390 195
2574 0002934 266
8338  93
2479 15
54175186 10540


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
35159636   =   yrday
fracday
Element set:     911
Inclination:       51
6390  deg
RA of node:       195
2574  deg
Eccentricity:     
0002934     
Arg of perigee:   266
8338  deg
Mean anomaly:      93
2479  deg
Mean motion:   15
54175186  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1054
Checksum:              330


Coasting Arc #13 (Orbit 1054)
---------------------------------------

Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1895313
97                 A    =         6779573
03  meter
 Y    =       -4401456
50  meter          E    =           
0005327
 Z    =        4793967
52                 I    =           51
53064
 XDOT =       7218
278106                 Wp   =          136
23014
 YDOT =       -299
757833  meter/sec      RA   =          194
06085  deg
 ZDOT =       2573
078731                 TA   =          288
36647
                                          MA   =          288
42439
                                          Ha   =            219
977  n
mi
                                          Hp   =            215
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6218221
69                 X    =        -1869241
56
 Y    =      -14440474
08  feet           Y    =        -4422505
98  meter
 Z    =       15728239
89                 Z    =         4784823
49
 XDOT =      23682
014785                 XDOT =        7208
594860
 YDOT =       -983
457457  feet/sec       YDOT =        -219
092557  meter/sec
 ZDOT =       8441
859354                 ZDOT =        2608
119308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13866973
62                 X    =         4226653
56
 Y    =        7493841
63  feet           Y    =         2284122
93  meter
 Z    =       15688227
52                 Z    =         4781771
75
 XDOT =     -17474
423137                 XDOT =       -5326
204172
 YDOT =      14298
914665  feet/sec       YDOT =        4358
309190  meter/sec
 ZDOT =       8597
575828                 ZDOT =        2620
541112


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   17353
41589798  
00016717  00000-0  10270-3 0  9120
2 25544  51
6403 194
9366 0002852 265
3771  94
7055 15
54146761 10558


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
41589798   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:       194
9366  deg
Eccentricity:     
0002852     
Arg of perigee:   265
3771  deg
Mean anomaly:      94
7055  deg
Mean motion:   15
54146761  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1055
Checksum:              332


Coasting Arc #14 (Orbit 1069)
---------------------------------------

Vector Time (GMT): 2017/354/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         120357
29                 A    =         6777406
37  meter
 Y    =        4262253
76  meter          E    =           
0011667
 Z    =       -5278179
80                 I    =           51
55511
 XDOT =      -7600
380656                 Wp   =           83
08593
 YDOT =       -650
156556  meter/sec      RA   =          189
05672  deg
 ZDOT =       -698
280470                 TA   =          180
22988
                                          MA   =          180
23042
                                          Ha   =            219
846  n
mi
                                          Hp   =            215
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         394873
00                 X    =           98325
38
 Y    =       13983772
18  feet           Y    =         4263477
09  meter
 Z    =      -17316862
87                 Z    =        -5277648
18
 XDOT =     -24935
632074                 XDOT =       -7589
153667
 YDOT =      -2133
059568  feet/sec       YDOT =        -735
086355  meter/sec
 ZDOT =      -2290
946425                 ZDOT =        -735
173420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9186323
36                 X    =        -2799991
36
 Y    =      -10553419
48  feet           Y    =        -3216682
26  meter
 Z    =      -17315090
21                 Z    =        -5277639
50
 XDOT =      19950
637169                 XDOT =        6080
954209
 YDOT =     -13338
379659  feet/sec       YDOT =       -4065
538120  meter/sec
 ZDOT =      -2454
787490                 ZDOT =        -748
219227


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   17354
38041283  
00016717  00000-0  10270-3 0  9130
2 25544  51
6397 190
1287 0002942 270
6381  89
4426 15
54174714 10705


Satellite: ISS
Catalog Number: 25544
Epoch time:      17354
38041283   =   yrday
fracday
Element set:     913
Inclination:       51
6397  deg
RA of node:       190
1287  deg
Eccentricity:     
0002942     
Arg of perigee:   270
6381  deg
Mean anomaly:      89
4426  deg
Mean motion:   15
54174714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1070
Checksum:              309


Coasting Arc #15 (Orbit 1085)
---------------------------------------

Vector Time (GMT): 2017/355/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1697629
41                 A    =         6777633
44  meter
 Y    =       -4008942
00  meter          E    =           
0002456
 Z    =        5194732
45                 I    =           51
58924
 XDOT =       7412
513021                 Wp   =            5
65405
 YDOT =       1517
689981  meter/sec      RA   =          184
05217  deg
 ZDOT =      -1248
703653                 TA   =           96
35379
                                          MA   =           96
32582
                                          Ha   =            219
696  n
mi
                                          Hp   =            215
702

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5569650
29                 X    =         1717099
02
 Y    =      -13152696
85  feet           Y    =        -3989849
62  meter
 Z    =       17043085
46                 Z    =         5203025
82
 XDOT =      24319
268442                 XDOT =        7401
056440
 YDOT =       4979
297837  feet/sec       YDOT =        1600
517841  meter/sec
 ZDOT =      -4096
796763                 ZDOT =       -1212
723874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4258584
14                 X    =         1298016
44
 Y    =       13586846
10  feet           Y    =         4141270
69  meter
 Z    =       17080493
99                 Z    =         5206134
57
 XDOT =     -20871
952824                 XDOT =       -6361
771221
 YDOT =      11501
511309  feet/sec       YDOT =        3505
660647  meter/sec
 ZDOT =      -3937
106776                 ZDOT =       -1200
030145


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   17355
40922705  
00016717  00000-0  10270-3 0  9142
2 25544  51
6402 185
0000 0003122 273
6576  86
4220 15
54194508 10867


Satellite: ISS
Catalog Number: 25544
Epoch time:      17355
40922705   =   yrday
fracday
Element set:     914
Inclination:       51
6402  deg
RA of node:       185
0000  deg
Eccentricity:     
0003122     
Arg of perigee:   273
6576  deg
Mean anomaly:      86
4220  deg
Mean motion:   15
54194508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1086
Checksum:              283


Coasting Arc #16 (Orbit 1100)
---------------------------------------

Vector Time (GMT): 2017/356/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3398944
79                 A    =         6780241
61  meter
 Y    =        3679822
34  meter          E    =           
0007115
 Z    =       -4576342
18                 I    =           51
63082
 XDOT =      -6630
242488                 Wp   =          115
25232
 YDOT =      -2315
816699  meter/sec      RA   =          179
05324  deg
 ZDOT =       3063
039762                 TA   =          185
40082
                                          MA   =          185
40850
                                          Ha   =            219
802  n
mi
                                          Hp   =            215
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11151393
68                 X    =        -3417611
51
 Y    =       12072907
95  feet           Y    =         3641709
06  meter
 Z    =      -15014246
00                 Z    =        -4592898
06
 XDOT =     -21752
764069                 XDOT =       -6618
732246
 YDOT =      -7597
823815  feet/sec       YDOT =       -2389
896524  meter/sec
 ZDOT =      10049
343052                 ZDOT =        3030
860122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         442913
88                 X    =          135000
15
 Y    =      -16360995
28  feet           Y    =        -4986831
36  meter
 Z    =      -15088337
58                 Z    =        -4598925
30
 XDOT =      20268
725478                 XDOT =        6177
907526
 YDOT =      -8585
036723  feet/sec       YDOT =       -2616
719193  meter/sec
 ZDOT =       9906
627869                 ZDOT =        3019
540175


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   17356
37373940  
00016717  00000-0  10270-3 0  9151
2 25544  51
6404 180
1911 0003119 279
2052  80
8748 15
54173096 11013


Satellite: ISS
Catalog Number: 25544
Epoch time:      17356
37373940   =   yrday
fracday
Element set:     915
Inclination:       51
6404  deg
RA of node:       180
1911  deg
Eccentricity:     
0003119     
Arg of perigee:   279
2052  deg
Mean anomaly:      80
8748  deg
Mean motion:   15
54173096  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1101
Checksum:              298


Coasting Arc #17 (Orbit 1116)
---------------------------------------

Vector Time (GMT): 2017/357/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4841369
07                 A    =         6783962
61  meter
 Y    =       -3251678
42  meter          E    =           
0009346
 Z    =        3458579
88                 I    =           51
67602
 XDOT =       5337
528872                 Wp   =           83
41349
 YDOT =       3075
616043  meter/sec      RA   =          174
06636  deg
 ZDOT =      -4568
276688                 TA   =           56
03071
                                          MA   =           55
94193
                                          Ha   =            219
782  n
mi
                                          Hp   =            215
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15883756
81                 X    =         4860570
47
 Y    =      -10668236
30  feet           Y    =        -3197431
83  meter
 Z    =       11347046
84                 Z    =         3482143
92
 XDOT =      17511
577663                 XDOT =        5324
930050
 YDOT =      10090
603815  feet/sec       YDOT =        3135
233844  meter/sec
 ZDOT =     -14987
784408                 ZDOT =       -4542
379233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4639118
71                 X    =        -1414003
38
 Y    =       18498248
05  feet           Y    =         5638266
00  meter
 Z    =       11452242
78                 Z    =         3490643
60
 XDOT =     -18495
454144                 XDOT =       -5637
414423
 YDOT =       4592
926753  feet/sec       YDOT =        1399
924074  meter/sec
 ZDOT =     -14873
078196                 ZDOT =       -4533
314234


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   17357
40254923  
00016717  00000-0  10270-3 0  9166
2 25544  51
6402 175
0621 0003086 286
0415  74
0398 15
54197071 11176


Satellite: ISS
Catalog Number: 25544
Epoch time:      17357
40254923   =   yrday
fracday
Element set:     916
Inclination:       51
6402  deg
RA of node:       175
0621  deg
Eccentricity:     
0003086     
Arg of perigee:   286
0415  deg
Mean anomaly:      74
0398  deg
Mean motion:   15
54197071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1117
Checksum:              296


Coasting Arc #18 (Orbit 1131)
---------------------------------------

Vector Time (GMT): 2017/358/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5879849
40                 A    =         6787502
52  meter
 Y    =        2734800
66  meter          E    =           
0006192
 Z    =       -1992803
38                 I    =           51
71933
 XDOT =      -3648
522495                 Wp   =           12
26423
 YDOT =      -3783
380214  meter/sec      RA   =          169
09200  deg
 ZDOT =       5582
127892                 TA   =          325
76028
                                          MA   =          325
80019
                                          Ha   =            219
861  n
mi
                                          Hp   =            215
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19290844
48                 X    =        -5900313
69
 Y    =        8972443
12  feet           Y    =         2668933
86  meter
 Z    =       -6538068
82                 Z    =        -2021415
15
 XDOT =     -11970
218159                 XDOT =       -3633
059557
 YDOT =     -12412
664745  feet/sec       YDOT =       -3824
094375  meter/sec
 ZDOT =      18314
067887                 ZDOT =        5564
441976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7993350
73                 X    =         2436373
30
 Y    =      -19673922
36  feet           Y    =        -5996611
54  meter
 Z    =       -6665649
48                 Z    =        -2031689
96
 XDOT =      15870
607744                 XDOT =        4837
361240
 YDOT =        279
549177  feet/sec       YDOT =          85
206589  meter/sec
 ZDOT =      18235
950340                 ZDOT =        5558
317664


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   17358
36705807  
00016717  00000-0  10270-3 0  9175
2 25544  51
6396 170
2539 0003205 288
2646  71
8157 15
54153717 11320


Satellite: ISS
Catalog Number: 25544
Epoch time:      17358
36705807   =   yrday
fracday
Element set:     917
Inclination:       51
6396  deg
RA of node:       170
2539  deg
Eccentricity:     
0003205     
Arg of perigee:   288
2646  deg
Mean anomaly:      71
8157  deg
Mean motion:   15
54153717  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1132
Checksum:              319


Coasting Arc #19 (Orbit 1147)
---------------------------------------

Vector Time (GMT): 2017/359/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6452588
22                 A    =         6789233
97  meter
 Y    =       -2073978
77  meter          E    =           
0009848
 Z    =         291969
76                 I    =           51
75774
 XDOT =       1704
867870                 Wp   =          138
47340
 YDOT =       4442
332499  meter/sec      RA   =          164
12725  deg
 ZDOT =      -6013
364825                 TA   =           38
38535
                                          MA   =           38
31532
                                          Ha   =            219
971  n
mi
                                          Hp   =            215
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21169908
85                 X    =         6473882
20
 Y    =       -6804392
27  feet           Y    =        -2001702
46  meter
 Z    =         957906
04                 Z    =          323365
84
 XDOT =       5593
398523                 XDOT =        1684
275582
 YDOT =      14574
581689  feet/sec       YDOT =        4461
282665  meter/sec
 ZDOT =     -19728
887220                 ZDOT =       -6005
132950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10537073
51                 X    =        -3211700
01
 Y    =       19574149
07  feet           Y    =         5966200
64  meter
 Z    =        1097792
83                 Z    =          334607
26
 XDOT =     -12799
289702                 XDOT =       -3901
223501
 YDOT =      -5768
128144  feet/sec       YDOT =       -1758
125458  meter/sec
 ZDOT =     -19692
887481                 ZDOT =       -6002
392104


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   17359
39586520  
00016717  00000-0  10270-3 0  9189
2 25544  51
6404 165
1248 0003141 289
8550  70
2264 15
54144921 11486


Satellite: ISS
Catalog Number: 25544
Epoch time:      17359
39586520   =   yrday
fracday
Element set:     918
Inclination:       51
6404  deg
RA of node:       165
1248  deg
Eccentricity:     
0003141     
Arg of perigee:   289
8550  deg
Mean anomaly:      70
2264  deg
Mean motion:   15
54144921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1148
Checksum:              309


Coasting Arc #20 (Orbit 1163)
---------------------------------------

Vector Time (GMT): 2017/360/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6506365
79                 A    =         6788323
07  meter
 Y    =        1280299
10  meter          E    =           
0012230
 Z    =        1419485
41                 I    =           51
78505
 XDOT =        288
079628                 Wp   =           48
54168
 YDOT =      -5002
422104  meter/sec      RA   =          159
16471  deg
 ZDOT =       5807
914146                 TA   =          326
90941
                                          MA   =          326
98587
                                          Ha   =            219
964  n
mi
                                          Hp   =            215
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21346344
47                 X    =        -6527094
01
 Y    =        4200456
37  feet           Y    =         1207424
50  meter
 Z    =        4657104
35                 Z    =         1387829
34
 XDOT =        945
143136                 XDOT =         315
784764
 YDOT =     -16412
146010  feet/sec       YDOT =       -4999
045957  meter/sec
 ZDOT =      19054
836437                 ZDOT =        5809
380604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12186721
61                 X    =         3714512
75
 Y    =      -18057880
75  feet           Y    =        -5504042
05  meter
 Z    =        4516152
80                 Z    =         1376523
37
 XDOT =       9679
445356                 XDOT =        2950
294944
 YDOT =      11320
336243  feet/sec       YDOT =        3450
438487  meter/sec
 ZDOT =      19062
039555                 ZDOT =        5810
109656


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   17360
42466704  
00016717  00000-0  10270-3 0  9197
2 25544  51
6391 159
9948 0003189 294
5455  65
5365 15
54199470 11644


Satellite: ISS
Catalog Number: 25544
Epoch time:      17360
42466704   =   yrday
fracday
Element set:     919
Inclination:       51
6391  deg
RA of node:       159
9948  deg
Eccentricity:     
0003189     
Arg of perigee:   294
5455  deg
Mean anomaly:      65
5365  deg
Mean motion:   15
54199470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1164
Checksum:              345
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