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

 
Date: June 17th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16989 6378 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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


175/23:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 216 2

175/23:25:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 216 3

176/18:02:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 216 3

180/21:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 216 3

Coasting Arc #1 (Orbit 1529)
---------------------------------------

Vector Time (GMT): 2019/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4505386
01                 A    =         6790951
88  meter
 Y    =        3106700
25  meter          E    =           
0017085
 Z    =        4004354
03                 I    =           51
63398
 XDOT =      -5738
275637                 Wp   =           81
90002
 YDOT =       3210
720061  meter/sec      RA   =          359
19172  deg
 ZDOT =       3953
199730                 TA   =          326
96290
                                          MA   =          327
06952
                                          Ha   =            228
183  n
mi
                                          Hp   =            216
758

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14781450
15                 X    =         4450860
20
 Y    =       10192586
12  feet           Y    =         3156776
99  meter
 Z    =       13137644
47                 Z    =         4026107
70
 XDOT =     -18826
363638                 XDOT =       -5792
954809
 YDOT =      10533
858469  feet/sec       YDOT =        3146
244158  meter/sec
 ZDOT =      12969
815386                 ZDOT =        3925
193114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11538984
24                 X    =         3517082
40
 Y    =      -13661631
64  feet           Y    =        -4164065
32  meter
 Z    =       13235915
01                 Z    =         4034306
89
 XDOT =       7700
282295                 XDOT =        2347
046044
 YDOT =      18984
171806  feet/sec       YDOT =        5786
375566  meter/sec
 ZDOT =      12842
365135                 ZDOT =        3914
352893


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   19168
55560996  
00016717  00000-0  10270-3 0  9007
2 25544  51
6396 359
4756 0007810  55
3822 304
8065 15
51203720 15303


Satellite: ISS
Catalog Number: 25544
Epoch time:      19168
55560996   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:       359
4756  deg
Eccentricity:     
0007810     
Arg of perigee:    55
3822  deg
Mean anomaly:     304
8065  deg
Mean motion:   15
51203720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1530
Checksum:              314


Coasting Arc #2 (Orbit 1544)
---------------------------------------

Vector Time (GMT): 2019/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4039044
62                 A    =         6789303
08  meter
 Y    =       -3154022
42  meter          E    =           
0017361
 Z    =       -4471203
77                 I    =           51
59505
 XDOT =       6123
351375                 Wp   =           64
64802
 YDOT =      -3219
383405  meter/sec      RA   =          354
22454  deg
 ZDOT =      -3263
209820                 TA   =          172
38141
                                          MA   =          172
35500
                                          Ha   =            228
353  n
mi
                                          Hp   =            216
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13251458
72                 X    =        -3981756
70
 Y    =      -10347842
60  feet           Y    =        -3198868
67  meter
 Z    =      -14669303
70                 Z    =        -4490685
34
 XDOT =      20089
735481                 XDOT =        6174
747147
 YDOT =     -10562
281512  feet/sec       YDOT =       -3150
619802  meter/sec
 ZDOT =     -10706
068964                 ZDOT =       -3233
340755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11337720
35                 X    =        -3455737
16
 Y    =       12310436
04  feet           Y    =         3752220
90  meter
 Z    =      -14757260
50                 Z    =        -4498013
00
 XDOT =      -8069
936788                 XDOT =       -2459
716733
 YDOT =     -20092
902282  feet/sec       YDOT =       -6124
316615  meter/sec
 ZDOT =     -10570
173589                 ZDOT =       -3221
788910


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   19169
52196145  
00016717  00000-0  10270-3 0  9017
2 25544  51
6394 354
6787 0007943  59
9642 300
2296 15
51212475 15458


Satellite: ISS
Catalog Number: 25544
Epoch time:      19169
52196145   =   yrday
fracday
Element set:     901
Inclination:       51
6394  deg
RA of node:       354
6787  deg
Eccentricity:     
0007943     
Arg of perigee:    59
9642  deg
Mean anomaly:     300
2296  deg
Mean motion:   15
51212475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1545
Checksum:              329


Coasting Arc #3 (Orbit 1560)
---------------------------------------

Vector Time (GMT): 2019/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3528246
42                 A    =         6787971
10  meter
 Y    =        3218503
56  meter          E    =           
0013252
 Z    =        4812269
89                 I    =           51
55767
 XDOT =      -6457
124426                 Wp   =           89
22167
 YDOT =       3275
727828  meter/sec      RA   =          349
25346  deg
 ZDOT =       2537
498597                 TA   =          335
76922
                                          MA   =          335
83149
                                          Ha   =            228
324  n
mi
                                          Hp   =            216
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11575611
62                 X    =         3468618
80
 Y    =       10559394
88  feet           Y    =         3257624
59  meter
 Z    =       15788287
04                 Z    =         4829264
44
 XDOT =     -21184
791424                 XDOT =       -6505
600315
 YDOT =      10747
138544  feet/sec       YDOT =        3203
248226  meter/sec
 ZDOT =       8325
126632                 ZDOT =        2506
015390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11233867
53                 X    =         3424082
82
 Y    =      -10810598
38  feet           Y    =        -3295070
39  meter
 Z    =       15864954
93                 Z    =         4835638
26
 XDOT =       8657
014810                 XDOT =        2638
658114
 YDOT =      21031
353624  feet/sec       YDOT =        6410
356585  meter/sec
 ZDOT =       8181
908576                 ZDOT =        2493
845734


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   19170
55273396  
00016717  00000-0  10270-3 0  9027
2 25544  51
6397 349
5620 0007935  63
0841 297
1120 15
51190386 15612


Satellite: ISS
Catalog Number: 25544
Epoch time:      19170
55273396   =   yrday
fracday
Element set:     902
Inclination:       51
6397  deg
RA of node:       349
5620  deg
Eccentricity:     
0007935     
Arg of perigee:    63
0841  deg
Mean anomaly:     297
1120  deg
Mean motion:   15
51190386  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1561
Checksum:              313


Coasting Arc #4 (Orbit 1575)
---------------------------------------

Vector Time (GMT): 2019/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2998958
06                 A    =         6786815
80  meter
 Y    =       -3362683
75  meter          E    =           
0021376
 Z    =       -5094762
71                 I    =           51
52134
 XDOT =       6669
284481                 Wp   =           73
35418
 YDOT =      -3313
213552  meter/sec      RA   =          344
27932  deg
 ZDOT =      -1739
057207                 TA   =          179
75896
                                          MA   =          179
75793
                                          Ha   =            228
474  n
mi
                                          Hp   =            216
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9839101
24                 X    =        -2936385
40
 Y    =      -11032426
99  feet           Y    =        -3395869
46  meter
 Z    =      -16715100
75                 Z    =        -5109178
98
 XDOT =      21880
854598                 XDOT =        6714
285400
 YDOT =     -10870
123203  feet/sec       YDOT =       -3238
381028  meter/sec
 ZDOT =      -5705
568266                 ZDOT =       -1706
551903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11443591
13                 X    =        -3488006
58
 Y    =        9240716
93  feet           Y    =         2816570
52  meter
 Z    =      -16780057
33                 Z    =        -5114561
48
 XDOT =      -9239
323669                 XDOT =       -2816
145854
 YDOT =     -21533
483171  feet/sec       YDOT =       -6563
405671  meter/sec
 ZDOT =      -5557
717932                 ZDOT =       -1693
992426


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   19171
51908121  
00016717  00000-0  10270-3 0  9036
2 25544  51
6396 344
7661 0008086  68
2884 291
9127 15
51213593 15766


Satellite: ISS
Catalog Number: 25544
Epoch time:      19171
51908121   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       344
7661  deg
Eccentricity:     
0008086     
Arg of perigee:    68
2884  deg
Mean anomaly:     291
9127  deg
Mean motion:   15
51213593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1576
Checksum:              326


Coasting Arc #5 (Orbit 1591)
---------------------------------------

Vector Time (GMT): 2019/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2447678
76                 A    =         6786205
00  meter
 Y    =        3534273
28  meter          E    =           
0010579
 Z    =        5241486
73                 I    =           51
48652
 XDOT =      -6832
862177                 Wp   =           84
94434
 YDOT =       3365
234398  meter/sec      RA   =          339
30152  deg
 ZDOT =        920
993730                 TA   =          356
22655
                                          MA   =          356
23453
                                          Ha   =            228
472  n
mi
                                          Hp   =            216
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8030442
12                 X    =         2382515
64
 Y    =       11595384
77  feet           Y    =         3561279
78  meter
 Z    =       17196478
77                 Z    =         5253218
78
 XDOT =     -22417
526828                 XDOT =       -6874
458987
 YDOT =      11040
795268  feet/sec       YDOT =        3288
591820  meter/sec
 ZDOT =       3021
632971                 ZDOT =         887
702097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11798593
70                 X    =         3596211
36
 Y    =       -7610300
31  feet           Y    =        -2319619
53  meter
 Z    =       17249241
91                 Z    =         5257568
93
 XDOT =       9898
441306                 XDOT =        3017
044910
 YDOT =      21856
660509  feet/sec       YDOT =        6661
910123  meter/sec
 ZDOT =       2870
220499                 ZDOT =         874
843208


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   19172
54985197  
00016717  00000-0  10270-3 0  9049
2 25544  51
6390 339
6499 0008053  71
7729 288
4298 15
51175528 15926


Satellite: ISS
Catalog Number: 25544
Epoch time:      19172
54985197   =   yrday
fracday
Element set:     904
Inclination:       51
6390  deg
RA of node:       339
6499  deg
Eccentricity:     
0008053     
Arg of perigee:    71
7729  deg
Mean anomaly:     288
4298  deg
Mean motion:   15
51175528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1592
Checksum:              359


Coasting Arc #6 (Orbit 1606)
---------------------------------------

Vector Time (GMT): 2019/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1917927
54                 A    =         6785839
05  meter
 Y    =       -3779693
44  meter          E    =           
0022741
 Z    =       -5319021
86                 I    =           51
45684
 XDOT =       6863
936744                 Wp   =           84
37570
 YDOT =      -3369
668773  meter/sec      RA   =          334
32181  deg
 ZDOT =        -78
618875                 TA   =          184
86006
                                          MA   =          184
88218
                                          Ha   =            228
488  n
mi
                                          Hp   =            216
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6292413
19                 X    =        -1849682
82
 Y    =      -12400569
04  feet           Y    =        -3800758
74  meter
 Z    =      -17450859
11                 Z    =        -5328173
10
 XDOT =      22519
477507                 XDOT =        6901
489088
 YDOT =     -11055
343743  feet/sec       YDOT =       -3292
701442  meter/sec
 ZDOT =       -257
935943                 ZDOT =         -45
186060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12455758
43                 X    =        -3796515
17
 Y    =        6065386
04  feet           Y    =         1848729
66  meter
 Z    =      -17491890
53                 Z    =        -5331528
23
 XDOT =     -10413
937904                 XDOT =       -3174
168273
 YDOT =     -21709
072742  feet/sec       YDOT =       -6616
925372  meter/sec
 ZDOT =       -105
895457                 ZDOT =         -32
276935


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   19173
51619553  
00016717  00000-0  10270-3 0  9058
2 25544  51
6409 334
8544 0008050  75
7779 284
4266 15
51222563 16071


Satellite: ISS
Catalog Number: 25544
Epoch time:      19173
51619553   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:       334
8544  deg
Eccentricity:     
0008050     
Arg of perigee:    75
7779  deg
Mean anomaly:     284
4266  deg
Mean motion:   15
51222563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1607
Checksum:              323


Coasting Arc #7 (Orbit 1622)
---------------------------------------

Vector Time (GMT): 2019/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1385737
80                 A    =         6786154
64  meter
 Y    =        4051280
53  meter          E    =           
0011300
 Z    =        5255809
07                 I    =           51
42725
 XDOT =      -6858
089317                 Wp   =           73
64011
 YDOT =       3351
379013  meter/sec      RA   =          329
33829  deg
 ZDOT =       -770
614119                 TA   =           23
76755
                                          MA   =           23
71540
                                          Ha   =            228
567  n
mi
                                          Hp   =            216
344

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4546383
87                 X    =         1314802
68
 Y    =       13291602
77  feet           Y    =         4066379
54  meter
 Z    =       17243468
09                 Z    =         5262368
62
 XDOT =     -22500
293035                 XDOT =       -6891
312512
 YDOT =      10995
337969  feet/sec       YDOT =        3274
501383  meter/sec
 ZDOT =      -2528
261546                 ZDOT =        -804
008113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13255186
16                 X    =         4040180
74
 Y    =       -4541671
00  feet           Y    =        -1384301
32  meter
 Z    =       17272717
41                 Z    =         5264724
27
 XDOT =      10851
980661                 XDOT =        3307
683705
 YDOT =      21423
293605  feet/sec       YDOT =        6529
819891  meter/sec
 ZDOT =      -2680
109522                 ZDOT =        -816
897382


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   19174
54696190  
00016717  00000-0  10270-3 0  9065
2 25544  51
6402 329
7375 0008164  79
5169 280
6902 15
51182114 16230


Satellite: ISS
Catalog Number: 25544
Epoch time:      19174
54696190   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:       329
7375  deg
Eccentricity:     
0008164     
Arg of perigee:    79
5169  deg
Mean anomaly:     280
6902  deg
Mean motion:   15
51182114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1623
Checksum:              319


Coasting Arc #8 (Orbit 1637)
---------------------------------------

Vector Time (GMT): 2019/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -914390
04                 A    =         6786722
90  meter
 Y    =       -4377369
19  meter          E    =           
0021260
 Z    =       -5123944
11                 I    =           51
40172
 XDOT =       6730
810845                 Wp   =           94
77085
 YDOT =      -3263
765938  meter/sec      RA   =          324
35591  deg
 ZDOT =       1591
077270                 TA   =          190
64490
                                          MA   =          190
68998
                                          Ha   =            228
525  n
mi
                                          Hp   =            216
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2999967
33                 X    =         -840483
99
 Y    =      -14361447
46  feet           Y    =        -4387180
72  meter
 Z    =      -16810840
25                 Z    =        -5128206
83
 XDOT =      22082
712747                 XDOT =        6759
078450
 YDOT =     -10707
893499  feet/sec       YDOT =       -3188
339418  meter/sec
 ZDOT =       5220
069783                 ZDOT =        1623
841086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14284045
02                 X    =        -4353776
92
 Y    =        3253397
22  feet           Y    =          991635
47  meter
 Z    =      -16829640
27                 Z    =        -5129674
35
 XDOT =     -11030
728011                 XDOT =       -3362
165898
 YDOT =     -20724
434336  feet/sec       YDOT =       -6316
807586  meter/sec
 ZDOT =       5369
034808                 ZDOT =        1636
481809


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   19175
51330199  
00016717  00000-0  10270-3 0  9078
2 25544  51
6406 324
9430 0008086  83
2055 277
0016 15
51222240 16389


Satellite: ISS
Catalog Number: 25544
Epoch time:      19175
51330199   =   yrday
fracday
Element set:     907
Inclination:       51
6406  deg
RA of node:       324
9430  deg
Eccentricity:     
0008086     
Arg of perigee:    83
2055  deg
Mean anomaly:     277
0016  deg
Mean motion:   15
51222240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1638
Checksum:              291


Coasting Arc #9 (Orbit 1645)
---------------------------------------

Vector Time (GMT): 2019/175/23:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5573158
11                 A    =         6797558
07  meter
 Y    =       -3847611
13  meter          E    =           
0020280
 Z    =         491453
11                 I    =           51
42468
 XDOT =       2355
768056                 Wp   =           62
75588
 YDOT =       4197
460106  meter/sec      RA   =          322
06139  deg
 ZDOT =       5966
485918                 TA   =          302
55614
                                          MA   =          302
75186
                                          Ha   =            228
467  n
mi
                                          Hp   =            216
190

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18284639
45                 X    =         5613381
79
 Y    =      -12623396
09  feet           Y    =        -3785063
32  meter
 Z    =        1612378
97                 Z    =          518622
54
 XDOT =       7728
897821                 XDOT =        2279
674066
 YDOT =      13771
194575  feet/sec       YDOT =        4223
377833  meter/sec
 ZDOT =      19575
085033                 ZDOT =        5977
744936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9055057
00                 X    =         2759981
37
 Y    =       20279793
94  feet           Y    =         6181281
19  meter
 Z    =        1736040
08                 Z    =          529145
02
 XDOT =     -13454
099228                 XDOT =       -4100
809445
 YDOT =       4280
125842  feet/sec       YDOT =        1304
582357  meter/sec
 ZDOT =      19625
633830                 ZDOT =        5981
893191


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   19176
02868124  
00016717  00000-0  10270-3 0  9080
2 25544  51
6393 322
3888 0008103  83
5231 276
6842 15
51262839 16461


Satellite: ISS
Catalog Number: 25544
Epoch time:      19176
02868124   =   yrday
fracday
Element set:     908
Inclination:       51
6393  deg
RA of node:       322
3888  deg
Eccentricity:     
0008103     
Arg of perigee:    83
5231  deg
Mean anomaly:     276
6842  deg
Mean motion:   15
51262839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1646
Checksum:              325


Coasting Arc #10 (Orbit 1645)
---------------------------------------

Vector Time (GMT): 2019/175/23:25:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4579948
67                 A    =         6787762
75  meter
 Y    =        1311341
86  meter          E    =           
0014135
 Z    =        4823876
60                 I    =           51
39178
 XDOT =      -4292
425205                 Wp   =           99
24746
 YDOT =       5857
781862  meter/sec      RA   =          322
02179  deg
 ZDOT =       2474
528344                 TA   =          326
33011
                                          MA   =          326
41983
                                          Ha   =            228
323  n
mi
                                          Hp   =            216
313

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15026078
33                 X    =         4541512
91
 Y    =        4302302
70  feet           Y    =         1362342
62  meter
 Z    =       15826366
81                 Z    =         4846030
95
 XDOT =     -14082
759859                 XDOT =       -4369
629392
 YDOT =      19218
444429  feet/sec       YDOT =        5809
349006  meter/sec
 ZDOT =       8118
531313                 ZDOT =        2453
490598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6012173
89                 X    =        -1832510
60
 Y    =       14316485
85  feet           Y    =         4363664
89  meter
 Z    =       15926667
04                 Z    =         4854448
11
 XDOT =     -16397
207627                 XDOT =       -4997
868885
 YDOT =     -15841
297265  feet/sec       YDOT =       -4828
427406  meter/sec
 ZDOT =       8022
432533                 ZDOT =        2445
237436


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   19176
02868248  
00016717  00000-0  10270-3 0  9098
2 25544  51
6396 322
3886 0007963  81
7618 278
4436 15
51235575 16460


Satellite: ISS
Catalog Number: 25544
Epoch time:      19176
02868248   =   yrday
fracday
Element set:     909
Inclination:       51
6396  deg
RA of node:       322
3886  deg
Eccentricity:     
0007963     
Arg of perigee:    81
7618  deg
Mean anomaly:     278
4436  deg
Mean motion:   15
51235575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1646
Checksum:              352


Coasting Arc #11 (Orbit 1657)
---------------------------------------

Vector Time (GMT): 2019/176/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3784598
51                 A    =         6786236
46  meter
 Y    =        2174921
59  meter          E    =           
0011311
 Z    =        5186659
47                 I    =           51
36875
 XDOT =      -4954
107624                 Wp   =           97
96117
 YDOT =       5732
464806  meter/sec      RA   =          318
15062  deg
 ZDOT =       1207
314773                 TA   =          340
39576
                                          MA   =          340
43921
                                          Ha   =            228
326  n
mi
                                          Hp   =            216
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12416661
78                 X    =         3734802
81
 Y    =        7135569
53  feet           Y    =         2216964
64  meter
 Z    =       17016599
32                 Z    =         5204922
87
 XDOT =     -16253
633936                 XDOT =       -5023
705932
 YDOT =      18807
299231  feet/sec       YDOT =        5676
675221  meter/sec
 ZDOT =       3961
006474                 ZDOT =        1183
081230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12681158
76                 X    =        -3865217
19
 Y    =       -6439077
88  feet           Y    =        -1962630
94  meter
 Z    =       17099151
54                 Z    =         5211821
39
 XDOT =      14735
388100                 XDOT =        4491
346293
 YDOT =     -18762
042065  feet/sec       YDOT =       -5718
670421  meter/sec
 ZDOT =       3850
443797                 ZDOT =        1173
615269


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   19176
80175353  
00016717  00000-0  10270-3 0  9104
2 25544  51
6417 318
5509 0007915  86
0538 274
1518 15
51234439 16584


Satellite: ISS
Catalog Number: 25544
Epoch time:      19176
80175353   =   yrday
fracday
Element set:     910
Inclination:       51
6417  deg
RA of node:       318
5509  deg
Eccentricity:     
0007915     
Arg of perigee:    86
0538  deg
Mean anomaly:     274
1518  deg
Mean motion:   15
51234439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1658
Checksum:              322


Coasting Arc #12 (Orbit 1672)
---------------------------------------

Vector Time (GMT): 2019/177/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3374092
16                 A    =         6785924
70  meter
 Y    =       -2601452
40  meter          E    =           
0022793
 Z    =       -5301588
97                 I    =           51
34396
 XDOT =       5010
833452                 Wp   =           87
54683
 YDOT =      -5764
865898  meter/sec      RA   =          313
16178  deg
 ZDOT =       -360
661334                 TA   =          178
99280
                                          MA   =          178
98820
                                          Ha   =            228
531  n
mi
                                          Hp   =            216
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11069856
17                 X    =        -3318999
04
 Y    =       -8534948
81  feet           Y    =        -2638875
22  meter
 Z    =      -17393664
61                 Z    =        -5317845
53
 XDOT =      16439
742297                 XDOT =        5076
677310
 YDOT =     -18913
602029  feet/sec       YDOT =       -5708
463048  meter/sec
 ZDOT =      -1183
272094                 ZDOT =        -336
161315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11546446
97                 X    =         3519357
04
 Y    =        7714128
08  feet           Y    =         2351266
24  meter
 Z    =      -17467066
89                 Z    =        -5323961
99
 XDOT =     -14460
774349                 XDOT =       -4407
644022
 YDOT =      19221
469078  feet/sec       YDOT =        5858
703775  meter/sec
 ZDOT =      -1071
511913                 ZDOT =        -326
596831


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   19177
76809148  
00016717  00000-0  10270-3 0  9117
2 25544  51
6424 313
7546 0008002  88
7363 271
4705 15
51205071 16738


Satellite: ISS
Catalog Number: 25544
Epoch time:      19177
76809148   =   yrday
fracday
Element set:     911
Inclination:       51
6424  deg
RA of node:       313
7546  deg
Eccentricity:     
0008002     
Arg of perigee:    88
7363  deg
Mean anomaly:     271
4705  deg
Mean motion:   15
51205071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1673
Checksum:              309


Coasting Arc #13 (Orbit 1688)
---------------------------------------

Vector Time (GMT): 2019/178/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2975634
78                 A    =         6785833
90  meter
 Y    =        3046410
05  meter          E    =           
0010683
 Z    =        5274035
39                 I    =           51
32132
 XDOT =      -5034
270997                 Wp   =           85
53162
 YDOT =       5768
878065  meter/sec      RA   =          308
17200  deg
 ZDOT =       -490
206967                 TA   =            9
17274
                                          MA   =            9
15324
                                          Ha   =            228
386  n
mi
                                          Hp   =            216
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9762581
31                 X    =         2915729
41
 Y    =        9994783
64  feet           Y    =         3079350
07  meter
 Z    =       17303265
72                 Z    =         5288344
83
 XDOT =     -16516
637128                 XDOT =       -5096
024927
 YDOT =      18926
765306  feet/sec       YDOT =        5712
236091  meter/sec
 ZDOT =      -1608
290575                 ZDOT =        -514
810886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10507662
38                 X    =        -3202735
49
 Y    =       -9086012
44  feet           Y    =        -2769416
59  meter
 Z    =       17367789
37                 Z    =         5293702
20
 XDOT =      14070
125937                 XDOT =        4288
574385
 YDOT =     -19570
830990  feet/sec       YDOT =       -5965
189286  meter/sec
 ZDOT =      -1720
509629                 ZDOT =        -524
411335


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   19178
79884824  
00016717  00000-0  10270-3 0  9126
2 25544  51
6416 308
6392 0008072  92
0634 268
1441 15
51246770 16895


Satellite: ISS
Catalog Number: 25544
Epoch time:      19178
79884824   =   yrday
fracday
Element set:     912
Inclination:       51
6416  deg
RA of node:       308
6392  deg
Eccentricity:     
0008072     
Arg of perigee:    92
0634  deg
Mean anomaly:     268
1441  deg
Mean motion:   15
51246770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1689
Checksum:              335


Coasting Arc #14 (Orbit 1703)
---------------------------------------

Vector Time (GMT): 2019/179/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2644201
79                 A    =         6786488
09  meter
 Y    =       -3532101
09  meter          E    =           
0021894
 Z    =       -5175917
36                 I    =           51
30397
 XDOT =       4969
125363                 Wp   =           98
24289
 YDOT =      -5659
505570  meter/sec      RA   =          303
18025  deg
 ZDOT =       1325
307441                 TA   =          184
57681
                                          MA   =          184
59686
                                          Ha   =            228
529  n
mi
                                          Hp   =            216
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8675202
71                 X    =        -2579366
49
 Y    =      -11588258
18  feet           Y    =        -3561307
14  meter
 Z    =      -16981356
17                 Z    =        -5188604
99
 XDOT =      16302
904735                 XDOT =        5025
604631
 YDOT =     -18567
931660  feet/sec       YDOT =       -5603
621724  meter/sec
 ZDOT =       4348
121526                 ZDOT =        1349
582029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9754335
26                 X    =         2973121
39
 Y    =       10604559
01  feet           Y    =         3232269
59  meter
 Z    =      -17038474
08                 Z    =        -5193326
90
 XDOT =     -13415
088594                 XDOT =       -4088
919003
 YDOT =      19494
334469  feet/sec       YDOT =        5941
873146  meter/sec
 ZDOT =       4458
824537                 ZDOT =        1359
049719


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   19179
76518338  
00016717  00000-0  10270-3 0  9139
2 25544  51
6422 303
8429 0008026  95
3549 264
8518 15
51209075 17043


Satellite: ISS
Catalog Number: 25544
Epoch time:      19179
76518338   =   yrday
fracday
Element set:     913
Inclination:       51
6422  deg
RA of node:       303
8429  deg
Eccentricity:     
0008026     
Arg of perigee:    95
3549  deg
Mean anomaly:     264
8518  deg
Mean motion:   15
51209075  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1704
Checksum:              326


Coasting Arc #15 (Orbit 1719)
---------------------------------------

Vector Time (GMT): 2019/180/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2334141
94                 A    =         6787288
05  meter
 Y    =        4018830
36  meter          E    =           
0013580
 Z    =        4935635
87                 I    =           51
28937
 XDOT =      -4901
458330                 Wp   =           80
39039
 YDOT =       5496
884166  meter/sec      RA   =          298
18836  deg
 ZDOT =      -2150
548687                 TA   =           30
70113
                                          MA   =           30
62175
                                          Ha   =            228
397  n
mi
                                          Hp   =            216
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7657946
00                 X    =         2265054
11
 Y    =       13185138
99  feet           Y    =         4044545
26  meter
 Z    =       16193031
06                 Z    =         4946807
16
 XDOT =     -16080
900033                 XDOT =       -4952
115576
 YDOT =      18034
396871  feet/sec       YDOT =        5441
789740  meter/sec
 ZDOT =      -7055
605929                 ZDOT =       -2174
480330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9129732
59                 X    =        -2782742
49
 Y    =      -12145449
17  feet           Y    =        -3701932
91  meter
 Z    =       16243224
11                 Z    =         4950934
71
 XDOT =      12781
084532                 XDOT =        3895
674565
 YDOT =     -19221
510620  feet/sec       YDOT =       -5858
716437  meter/sec
 ZDOT =      -7164
727640                 ZDOT =       -2183
808985


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   19180
79593677  
00016717  00000-0  10270-3 0  9144
2 25544  51
6417 298
7271 0008124  98
6214 261
5858 15
51260040 17206


Satellite: ISS
Catalog Number: 25544
Epoch time:      19180
79593677   =   yrday
fracday
Element set:     914
Inclination:       51
6417  deg
RA of node:       298
7271  deg
Eccentricity:     
0008124     
Arg of perigee:    98
6214  deg
Mean anomaly:     261
5858  deg
Mean motion:   15
51260040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1720
Checksum:              324


Coasting Arc #16 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2019/180/21:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4169883
21                 A    =         6786037
31  meter
 Y    =        1081230
43  meter          E    =           
0011173
 Z    =        5234342
11                 I    =           51
28096
 XDOT =      -2908
480013                 Wp   =          104
32494
 YDOT =       7047
408999  meter/sec      RA   =          297
59643  deg
 ZDOT =        857
005379                 TA   =          337
41910
                                          MA   =          337
46822
                                          Ha   =            228
355  n
mi
                                          Hp   =            216
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13680719
18                 X    =         4132057
07
 Y    =        3547343
94  feet           Y    =         1127648
60  meter
 Z    =       17173038
41                 Z    =         5254506
21
 XDOT =      -9542
257261                 XDOT =       -2991
232860
 YDOT =      23121
420600  feet/sec       YDOT =        7014
421492  meter/sec
 ZDOT =       2811
697439                 ZDOT =         842
677232

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11182755
99                 X    =        -3408504
03
 Y    =        8458585
73  feet           Y    =         2578176
93  meter
 Z    =       17264335
21                 Z    =         5262169
37
 XDOT =     -11626
964701                 XDOT =       -3543
898841
 YDOT =     -21004
490133  feet/sec       YDOT =       -6402
168592  meter/sec
 ZDOT =       2745
941163                 ZDOT =         836
962866


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   19180
92478201  
00016717  00000-0  10270-3 0  9155
2 25544  51
6397 298
0876 0008036  98
6129 261
5932 15
51226119 17228


Satellite: ISS
Catalog Number: 25544
Epoch time:      19180
92478201   =   yrday
fracday
Element set:     915
Inclination:       51
6397  deg
RA of node:       298
0876  deg
Eccentricity:     
0008036     
Arg of perigee:    98
6129  deg
Mean anomaly:     261
5932  deg
Mean motion:   15
51226119  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1722
Checksum:              327


Coasting Arc #17 (Orbit 1736)
---------------------------------------

Vector Time (GMT): 2019/181/21:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3928825
90                 A    =         6785839
47  meter
 Y    =       -1635322
50  meter          E    =           
0022803
 Z    =       -5305413
65                 I    =           51
26620
 XDOT =       2938
025652                 Wp   =           93
91440
 YDOT =      -7059
845175  meter/sec      RA   =          292
60191  deg
 ZDOT =         -1
128262                 TA   =          176
08370
                                          MA   =          176
06582
                                          Ha   =            228
503  n
mi
                                          Hp   =            216
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12889848
75                 X    =        -3884476
51
 Y    =       -5365231
29  feet           Y    =        -1679008
42  meter
 Z    =      -17406212
75                 Z    =        -5324391
01
 XDOT =       9639
191773                 XDOT =        3016
757982
 YDOT =     -23162
221702  feet/sec       YDOT =       -7026
549893  meter/sec
 ZDOT =         -3
701647                 ZDOT =          13
333478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12002977
08                 X    =         3658507
41
 Y    =       -6918535
48  feet           Y    =        -2108769
62  meter
 Z    =      -17492071
29                 Z    =        -5331583
33
 XDOT =      12097
859767                 XDOT =        3687
427657
 YDOT =      20817
561041  feet/sec       YDOT =        6345
192605  meter/sec
 ZDOT =         62
652067                 ZDOT =          19
096350


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   19181
89111138  
00016717  00000-0  10270-3 0  9166
2 25544  51
6402 293
2915 0008057 101
4719 258
7337 15
51222450 17374


Satellite: ISS
Catalog Number: 25544
Epoch time:      19181
89111138   =   yrday
fracday
Element set:     916
Inclination:       51
6402  deg
RA of node:       293
2915  deg
Eccentricity:     
0008057     
Arg of perigee:   101
4719  deg
Mean anomaly:     258
7337  deg
Mean motion:   15
51222450  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1737
Checksum:              304


Coasting Arc #18 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2019/182/21:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3710723
51                 A    =         6786034
58  meter
 Y    =        2190230
21  meter          E    =           
0010609
 Z    =        5233224
32                 I    =           51
25468
 XDOT =      -2948
233981                 Wp   =           91
79571
 YDOT =       7031
756347  meter/sec      RA   =          287
60699  deg
 ZDOT =       -851
282020                 TA   =            6
38994
                                          MA   =            6
37642
                                          Ha   =            228
306  n
mi
                                          Hp   =            216
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12174289
73                 X    =         3660535
96
 Y    =        7185794
64  feet           Y    =         2231444
47  meter
 Z    =       17169371
11                 Z    =         5251128
08
 XDOT =      -9672
683665                 XDOT =       -3022
510938
 YDOT =      23070
066755  feet/sec       YDOT =        6998
371988  meter/sec
 ZDOT =      -2792
920012                 ZDOT =        -865
782392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12927748
88                 X    =        -3940377
86
 Y    =        5471421
65  feet           Y    =         1667689
32  meter
 Z    =       17250308
22                 Z    =         5257893
94
 XDOT =     -12491
515265                 XDOT =       -3807
413853
 YDOT =     -20487
363480  feet/sec       YDOT =       -6244
548389  meter/sec
 ZDOT =      -2859
435277                 ZDOT =        -871
555872


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   19182
92186209  
00016717  00000-0  10270-3 0  9173
2 25544  51
6396 288
1760 0007970 105
0785 255
1249 15
51233196 17533


Satellite: ISS
Catalog Number: 25544
Epoch time:      19182
92186209   =   yrday
fracday
Element set:     917
Inclination:       51
6396  deg
RA of node:       288
1760  deg
Eccentricity:     
0007970     
Arg of perigee:   105
0785  deg
Mean anomaly:     255
1249  deg
Mean motion:   15
51233196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1753
Checksum:              330
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