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

 
Date: June 29th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19909 6822 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


184/00:03:16 781 0 4 1 7 1 7
N/A -1 6 -0 2 228 4
000/00:00:33 561 0 3 0 1 217 2

184/09:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 217 3

187/16:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 217 5

194/07:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 9
000/00:00:00 000 0 0 0 0 218 1

Coasting Arc #1 (Orbit 1699)
---------------------------------------

Vector Time (GMT): 2019/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         512988
11                 A    =         6792479
78  meter
 Y    =       -5775996
63  meter          E    =           
0013246
 Z    =       -3550043
27                 I    =           51
32783
 XDOT =       5825
142418                 Wp   =           95
68877
 YDOT =      -2207
043238  meter/sec      RA   =          304
41492  deg
 ZDOT =       4445
740224                 TA   =          222
33894
                                          MA   =          222
44125
                                          Ha   =            228
521  n
mi
                                          Hp   =            216
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1683031
85                 X    =          594783
02
 Y    =      -18950120
18  feet           Y    =        -5769802
19  meter
 Z    =      -11647123
58                 Z    =        -3547353
50
 XDOT =      19111
359639                 XDOT =        5827
794268
 YDOT =      -7240
955505  feet/sec       YDOT =       -2141
888208  meter/sec
 ZDOT =      14585
761889                 ZDOT =        4474
042809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19032549
48                 X    =        -5801121
08
 Y    =          32721
02  feet           Y    =            9973
37  meter
 Z    =      -11634265
26                 Z    =        -3546124
05
 XDOT =      -8997
317621                 XDOT =       -2742
382411
 YDOT =     -16858
047587  feet/sec       YDOT =       -5138
332904  meter/sec
 ZDOT =      14714
332503                 ZDOT =        4484
928547


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
50747543  
00016717  00000-0  10270-3 0  9009
2 25544  51
6414 305
1180 0008071  96
4269 263
7801 15
51223747 17005


Satellite: ISS
Catalog Number: 25544
Epoch time:      19179
50747543   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:       305
1180  deg
Eccentricity:     
0008071     
Arg of perigee:    96
4269  deg
Mean anomaly:     263
7801  deg
Mean motion:   15
51223747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1700
Checksum:              298


Coasting Arc #2 (Orbit 1715)
---------------------------------------

Vector Time (GMT): 2019/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -743287
45                 A    =         6794178
65  meter
 Y    =        6077867
23  meter          E    =           
0021369
 Z    =        2921382
32                 I    =           51
31621
 XDOT =      -5563
271695                 Wp   =           99
03185
 YDOT =       1731
163850  meter/sec      RA   =          299
43064  deg
 ZDOT =      -4989
089335                 TA   =           47
48927
                                          MA   =           47
30896
                                          Ha   =            228
515  n
mi
                                          Hp   =            216
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2438607
12                 X    =         -825387
16
 Y    =       19940509
27  feet           Y    =         6069095
75  meter
 Z    =        9584587
66                 Z    =         2917573
27
 XDOT =     -18252
203724                 XDOT =       -5557
982292
 YDOT =       5679
671425  feet/sec       YDOT =        1668
981827  meter/sec
 ZDOT =     -16368
403330                 ZDOT =       -5016
100589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20095858
19                 X    =         6125217
58
 Y    =         266712
97  feet           Y    =           81294
11  meter
 Z    =        9566628
63                 Z    =         2915908
41
 XDOT =       7682
971504                 XDOT =        2341
769715
 YDOT =      15931
182837  feet/sec       YDOT =        4855
824529  meter/sec
 ZDOT =     -16491
061460                 ZDOT =       -5026
475533


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
53822396  
00016717  00000-0  10270-3 0  9015
2 25544  51
6421 300
0015 0008132 101
0244 259
1822 15
51229254 17166


Satellite: ISS
Catalog Number: 25544
Epoch time:      19180
53822396   =   yrday
fracday
Element set:     901
Inclination:       51
6421  deg
RA of node:       300
0015  deg
Eccentricity:     
0008132     
Arg of perigee:   101
0244  deg
Mean anomaly:     259
1822  deg
Mean motion:   15
51229254  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1716
Checksum:              265


Coasting Arc #3 (Orbit 1730)
---------------------------------------

Vector Time (GMT): 2019/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         868265
80                 A    =         6795568
12  meter
 Y    =       -6341122
33  meter          E    =           
0012253
 Z    =       -2289694
54                 I    =           51
30668
 XDOT =       5297
018087                 Wp   =           78
13089
 YDOT =      -1212
565059  meter/sec      RA   =          294
44786  deg
 ZDOT =       5393
828970                 TA   =          256
30184
                                          MA   =          256
43829
                                          Ha   =            228
502  n
mi
                                          Hp   =            216
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2848641
08                 X    =          950231
59
 Y    =      -20804207
14  feet           Y    =        -6330954
06  meter
 Z    =       -7512121
18                 Z    =        -2285278
89
 XDOT =      17378
668266                 XDOT =        5283
983396
 YDOT =      -3978
231820  feet/sec       YDOT =       -1153
403947  meter/sec
 ZDOT =      17696
289273                 ZDOT =        5419
528061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21004752
81                 X    =        -6402248
66
 Y    =        -202904
99  feet           Y    =          -61845
44  meter
 Z    =       -7491391
33                 Z    =        -2283376
08
 XDOT =      -6175
650210                 XDOT =       -1882
338184
 YDOT =     -15073
915331  feet/sec       YDOT =       -4594
529393  meter/sec
 ZDOT =      17812
939557                 ZDOT =        5429
383977


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
50454742  
00016717  00000-0  10270-3 0  9020
2 25544  51
6433 295
2059 0008077 102
5614 257
6441 15
51226841 17313


Satellite: ISS
Catalog Number: 25544
Epoch time:      19181
50454742   =   yrday
fracday
Element set:     902
Inclination:       51
6433  deg
RA of node:       295
2059  deg
Eccentricity:     
0008077     
Arg of perigee:   102
5614  deg
Mean anomaly:     257
6441  deg
Mean motion:   15
51226841  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1731
Checksum:              297


Coasting Arc #4 (Orbit 1746)
---------------------------------------

Vector Time (GMT): 2019/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -993049
03                 A    =         6796751
72  meter
 Y    =        6532916
84  meter          E    =           
0022004
 Z    =        1548583
18                 I    =           51
29715
 XDOT =      -5072
738950                 Wp   =          113
64091
 YDOT =        598
193026  meter/sec      RA   =          289
46586  deg
 ZDOT =      -5720
481457                 TA   =           49
35889
                                          MA   =           49
16776
                                          Ha   =            228
496  n
mi
                                          Hp   =            216
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3258034
86                 X    =        -1073550
30
 Y    =       21433454
20  feet           Y    =         6521361
46  meter
 Z    =        5080653
47                 Z    =         1543565
08
 XDOT =     -16642
844325                 XDOT =       -5051
264251
 YDOT =       1962
575545  feet/sec       YDOT =         541
587290  meter/sec
 ZDOT =     -18767
983783                 ZDOT =       -5745
070594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21684704
47                 X    =         6609497
92
 Y    =         138914
01  feet           Y    =           42340
99  meter
 Z    =        5057181
48                 Z    =         1541428
91
 XDOT =       4353
331744                 XDOT =        1326
895516
 YDOT =      14474
033851  feet/sec       YDOT =        4411
685518  meter/sec
 ZDOT =     -18879
536115                 ZDOT =       -5754
482608


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
53529182  
00016717  00000-0  10270-3 0  9036
2 25544  51
6425 290
0902 0008212 107
4004 252
8046 15
51236448 17471


Satellite: ISS
Catalog Number: 25544
Epoch time:      19182
53529182   =   yrday
fracday
Element set:     903
Inclination:       51
6425  deg
RA of node:       290
0902  deg
Eccentricity:     
0008212     
Arg of perigee:   107
4004  deg
Mean anomaly:     252
8046  deg
Mean motion:   15
51236448  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1747
Checksum:              291


Coasting Arc #5 (Orbit 1761)
---------------------------------------

Vector Time (GMT): 2019/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1026510
16                 A    =         6797441
31  meter
 Y    =       -6664798
43  meter          E    =           
0015009
 Z    =        -839878
48                 I    =           51
29020
 XDOT =       4881
233048                 Wp   =           69
93319
 YDOT =         19
418538  meter/sec      RA   =          284
48452  deg
 ZDOT =       5903
109686                 TA   =          280
95349
                                          MA   =          281
12231
                                          Ha   =            228
454  n
mi
                                          Hp   =            216
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3367815
49                 X    =         1105041
18
 Y    =      -21866136
60  feet           Y    =        -6652880
02  meter
 Z    =       -2755506
84                 Z    =         -834702
71
 XDOT =      16014
544122                 XDOT =        4851
979320
 YDOT =         63
709114  feet/sec       YDOT =          73
839161  meter/sec
 ZDOT =      19367
157764                 ZDOT =        5926
749664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22125959
91                 X    =        -6743992
58
 Y    =         211483
68  feet           Y    =           64460
22  meter
 Z    =       -2731318
61                 Z    =         -832505
91
 XDOT =      -2501
173019                 XDOT =        -762
357536
 YDOT =     -14070
080279  feet/sec       YDOT =       -4288
560469  meter/sec
 ZDOT =      19474
344574                 ZDOT =        5935
780226


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   19183
50161281  
00016717  00000-0  10270-3 0  9047
2 25544  51
6432 285
2952 0008105 109
7501 250
4525 15
51239221 17623


Satellite: ISS
Catalog Number: 25544
Epoch time:      19183
50161281   =   yrday
fracday
Element set:     904
Inclination:       51
6432  deg
RA of node:       285
2952  deg
Eccentricity:     
0008105     
Arg of perigee:   109
7501  deg
Mean anomaly:     250
4525  deg
Mean motion:   15
51239221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1762
Checksum:              284


Coasting Arc #6 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2019/184/00:03:33
561
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3892444
11                 A    =         6786943
31  meter
 Y    =       -1913364
06  meter          E    =           
0020924
 Z    =       -5238637
86                 I    =           51
24752
 XDOT =       2299
916977                 Wp   =          101
30463
 YDOT =      -7233
714140  meter/sec      RA   =          281
97997  deg
 ZDOT =        932
311370                 TA   =          177
69371
                                          MA   =          177
68405
                                          Ha   =            228
389  n
mi
                                          Hp   =            217
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12770485
91                 X    =        -3845312
91
 Y    =       -6277441
14  feet           Y    =        -1956627
53  meter
 Z    =      -17187132
08                 Z    =        -5257431
61
 XDOT =       7545
659373                 XDOT =        2376
106903
 YDOT =     -23732
657938  feet/sec       YDOT =       -7207
569036  meter/sec
 ZDOT =       3058
764337                 ZDOT =         943
667007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3811422
47                 X    =         1161721
57
 Y    =      -13602761
80  feet           Y    =        -4146121
80  meter
 Z    =      -17272145
70                 Z    =        -5264550
01
 XDOT =      23726
861622                 XDOT =        7231
947422
 YDOT =       2694
433281  feet/sec       YDOT =         821
263264  meter/sec
 ZDOT =       3111
027456                 ZDOT =         948
241168


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   19184
01698455  
00016717  00000-0  10270-3 0  9053
2 25544  51
6425 282
7396 0006663 110
3342 249
8525 15
50945969 17700


Satellite: ISS
Catalog Number: 25544
Epoch time:      19184
01698455   =   yrday
fracday
Element set:     905
Inclination:       51
6425  deg
RA of node:       282
7396  deg
Eccentricity:     
0006663     
Arg of perigee:   110
3342  deg
Mean anomaly:     249
8525  deg
Mean motion:   15
50945969  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1770
Checksum:              337


Coasting Arc #7 (Orbit 1776)
---------------------------------------

Vector Time (GMT): 2019/184/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3323538
31                 A    =         6794690
25  meter
 Y    =       -5116171
91  meter          E    =           
0019209
 Z    =        2976297
53                 I    =           51
27087
 XDOT =       3154
514406                 Wp   =           94
40195
 YDOT =       4940
642930  meter/sec      RA   =          279
97635  deg
 ZDOT =       4941
159219                 TA   =          299
79489
                                          MA   =          299
98577
                                          Ha   =            228
310  n
mi
                                          Hp   =            217
267

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10903997
10                 X    =         3366044
79
 Y    =      -16785340
92  feet           Y    =        -5078768
69  meter
 Z    =        9764755
68                 Z    =         2992544
08
 XDOT =      10349
456711                 XDOT =        3075
031177
 YDOT =      16209
458432  feet/sec       YDOT =        4975
473540  meter/sec
 ZDOT =      16211
152293                 ZDOT =        4956
290390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11430269
77                 X    =        -3483946
23
 Y    =      -16387158
15  feet           Y    =        -4994805
80  meter
 Z    =        9838966
25                 Z    =         2998916
91
 XDOT =      17686
188160                 XDOT =        5390
750151
 YDOT =      -2505
259703  feet/sec       YDOT =        -763
603157  meter/sec
 ZDOT =      16279
242388                 ZDOT =        4961
913080


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   19184
46802082  
00016717  00000-0  10270-3 0  9066
2 25544  51
6423 280
4975 0006860 117
0903 243
0949 15
50984011 17776


Satellite: ISS
Catalog Number: 25544
Epoch time:      19184
46802082   =   yrday
fracday
Element set:     906
Inclination:       51
6423  deg
RA of node:       280
4975  deg
Eccentricity:     
0006860     
Arg of perigee:   117
0903  deg
Mean anomaly:     243
0949  deg
Mean motion:   15
50984011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1777
Checksum:              316


Coasting Arc #8 (Orbit 1791)
---------------------------------------

Vector Time (GMT): 2019/185/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3258532
85                 A    =         6793282
13  meter
 Y    =        4812267
70  meter          E    =           
0011552
 Z    =       -3524410
81                 I    =           51
26096
 XDOT =      -3126
404991                 Wp   =          104
41001
 YDOT =      -5376
051487  meter/sec      RA   =          274
99081  deg
 ZDOT =      -4465
136186                 TA   =          117
25576
                                          MA   =          117
13803
                                          Ha   =            228
371  n
mi
                                          Hp   =            217
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10690724
58                 X    =        -3294983
50
 Y    =       15788279
85  feet           Y    =         4775625
32  meter
 Z    =      -11563027
59                 Z    =        -3540326
94
 XDOT =     -10257
234224                 XDOT =       -3044
367316
 YDOT =     -17637
964195  feet/sec       YDOT =       -5410
553640  meter/sec
 ZDOT =     -14649
396937                 ZDOT =       -4480
124538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10862929
04                 X    =         3311020
77
 Y    =       15616410
69  feet           Y    =         4759881
98  meter
 Z    =      -11635698
06                 Z    =        -3546560
77
 XDOT =     -18983
643520                 XDOT =       -5786
214545
 YDOT =       2276
649797  feet/sec       YDOT =         693
922858  meter/sec
 ZDOT =     -14716
814202                 ZDOT =       -4485
684969


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   19185
43453122  
00016717  00000-0  10270-3 0  9072
2 25544  51
6421 275
7030 0006907 119
2862 240
8980 15
50947367 17923


Satellite: ISS
Catalog Number: 25544
Epoch time:      19185
43453122   =   yrday
fracday
Element set:     907
Inclination:       51
6421  deg
RA of node:       275
7030  deg
Eccentricity:     
0006907     
Arg of perigee:   119
2862  deg
Mean anomaly:     240
8980  deg
Mean motion:   15
50947367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1792
Checksum:              319


Coasting Arc #9 (Orbit 1807)
---------------------------------------

Vector Time (GMT): 2019/186/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3183034
33                 A    =         6791756
67  meter
 Y    =       -4492998
29  meter          E    =           
0017472
 Z    =        3966173
88                 I    =           51
25397
 XDOT =       3171
574442                 Wp   =          109
39338
 YDOT =       5753
794030  meter/sec      RA   =          270
00377  deg
 ZDOT =       3952
732347                 TA   =          299
14388
                                          MA   =          299
31864
                                          Ha   =            228
238  n
mi
                                          Hp   =            217
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10443026
03                 X    =         3213774
68
 Y    =      -14740808
03  feet           Y    =        -4457232
10  meter
 Z    =       13012381
49                 Z    =         3981709
53
 XDOT =      10405
427958                 XDOT =        3087
798361
 YDOT =      18877
277000  feet/sec       YDOT =        5788
791769  meter/sec
 ZDOT =      12968
281977                 ZDOT =        3967
935775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10236564
20                 X    =        -3120104
77
 Y    =      -14822642
76  feet           Y    =        -4517941
51  meter
 Z    =       13083283
26                 Z    =         3987784
74
 XDOT =      20203
410171                 XDOT =        6157
999420
 YDOT =      -2388
054198  feet/sec       YDOT =        -727
878920  meter/sec
 ZDOT =      13036
658978                 ZDOT =        3973
573657


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   19186
46547169  
00016717  00000-0  10270-3 0  9082
2 25544  51
6416 270
5890 0006882 123
3323 236
8488 15
50986513 18086


Satellite: ISS
Catalog Number: 25544
Epoch time:      19186
46547169   =   yrday
fracday
Element set:     908
Inclination:       51
6416  deg
RA of node:       270
5890  deg
Eccentricity:     
0006882     
Arg of perigee:   123
3323  deg
Mean anomaly:     236
8488  deg
Mean motion:   15
50986513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1808
Checksum:              342


Coasting Arc #10 (Orbit 1822)
---------------------------------------

Vector Time (GMT): 2019/187/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3182695
37                 A    =         6790387
58  meter
 Y    =        4095585
53  meter          E    =           
0013956
 Z    =       -4394027
31                 I    =           51
25018
 XDOT =      -3224
411383                 Wp   =           93
91936
 YDOT =      -6082
257993  meter/sec      RA   =          265
01477  deg
 ZDOT =      -3343
807113                 TA   =          142
05820
                                          MA   =          141
95979
                                          Ha   =            228
285  n
mi
                                          Hp   =            217
444

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10441913
95                 X    =        -3206913
52
 Y    =       13436960
39  feet           Y    =         4059859
54  meter
 Z    =      -14416100
10                 Z    =        -4409545
65
 XDOT =     -10578
777504                 XDOT =       -3139
916155
 YDOT =     -19954
914676  feet/sec       YDOT =       -6117
842759  meter/sec
 ZDOT =     -10970
495776                 ZDOT =       -3359
265335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9262817
00                 X    =         2823306
62
 Y    =       14203525
06  feet           Y    =         4329234
44  meter
 Z    =      -14486873
75                 Z    =        -4415599
12
 XDOT =     -21270
178449                 XDOT =       -6483
150391
 YDOT =       2644
938581  feet/sec       YDOT =         806
177280  meter/sec
 ZDOT =     -11040
019629                 ZDOT =       -3364
997983


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   19187
43198014  
00016717  00000-0  10270-3 0  9092
2 25544  51
6417 265
7945 0006847 126
9818 233
1961 15
50942713 18230


Satellite: ISS
Catalog Number: 25544
Epoch time:      19187
43198014   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:       265
7945  deg
Eccentricity:     
0006847     
Arg of perigee:   126
9818  deg
Mean anomaly:     233
1961  deg
Mean motion:   15
50942713  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1823
Checksum:              336


Coasting Arc #11 (Orbit 1827)
---------------------------------------

Vector Time (GMT): 2019/187/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4200122
04                 A    =         6786600
81  meter
 Y    =        -632999
18  meter          E    =           
0008974
 Z    =        5286150
91                 I    =           51
23587
 XDOT =        972
414829                 Wp   =          116
88193
 YDOT =       7606
767313  meter/sec      RA   =          263
51953  deg
 ZDOT =        134
083291                 TA   =          331
80910
                                          MA   =          331
85765
                                          Ha   =            228
140  n
mi
                                          Hp   =            217
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13779927
95                 X    =         4181211
57
 Y    =       -2076768
95  feet           Y    =         -586136
83  meter
 Z    =       17343014
79                 Z    =         5306507
13
 XDOT =       3190
337367                 XDOT =         886
630217
 YDOT =      24956
585671  feet/sec       YDOT =        7617
161870  meter/sec
 ZDOT =        439
905810                 ZDOT =         138
599377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13740671
87                 X    =        -4188156
79
 Y    =        1476610
88  feet           Y    =          450071
00  meter
 Z    =       17435397
97                 Z    =         5314309
30
 XDOT =      -1986
112912                 XDOT =        -605
367216
 YDOT =     -24070
064428  feet/sec       YDOT =       -7336
555638  meter/sec
 ZDOT =        459
665040                 ZDOT =         140
105904


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   19187
75414772  
00016717  00000-0  10270-3 0  9101
2 25544  51
6390 264
1989 0006736 124
1670 236
0120 15
50956323 18280


Satellite: ISS
Catalog Number: 25544
Epoch time:      19187
75414772   =   yrday
fracday
Element set:     910
Inclination:       51
6390  deg
RA of node:       264
1989  deg
Eccentricity:     
0006736     
Arg of perigee:   124
1670  deg
Mean anomaly:     236
0120  deg
Mean motion:   15
50956323  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              315


Coasting Arc #12 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2019/188/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4290194
03                 A    =         6786798
92  meter
 Y    =         151218
88  meter          E    =           
0020688
 Z    =       -5274516
30                 I    =           51
24152
 XDOT =      -1028
148372                 Wp   =          104
75648
 YDOT =      -7553
465760  meter/sec      RA   =          258
52556  deg
 ZDOT =        616
592462                 TA   =          171
19601
                                          MA   =          171
15967
                                          Ha   =            228
292  n
mi
                                          Hp   =            217
399

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14075439
73                 X    =        -4265945
89
 Y    =         496124
95  feet           Y    =          103379
02  meter
 Z    =      -17304843
50                 Z    =        -5295297
21
 XDOT =      -3373
190197                 XDOT =        -946
601955
 YDOT =     -24781
711810  feet/sec       YDOT =       -7564
507341  meter/sec
 ZDOT =       2022
941149                 ZDOT =         611
795507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13967001
25                 X    =         4257141
98
 Y    =        -124829
35  feet           Y    =          -38047
99  meter
 Z    =      -17399110
49                 Z    =        -5303248
88
 XDOT =       2719
623884                 XDOT =         828
941360
 YDOT =      23844
142297  feet/sec       YDOT =        7267
694572  meter/sec
 ZDOT =       2001
878866                 ZDOT =         610
172678


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   19188
72065282  
00016717  00000-0  10270-3 0  9118
2 25544  51
6393 259
4040 0006748 126
6955 233
4817 15
50936056 18436


Satellite: ISS
Catalog Number: 25544
Epoch time:      19188
72065282   =   yrday
fracday
Element set:     911
Inclination:       51
6393  deg
RA of node:       259
4040  deg
Eccentricity:     
0006748     
Arg of perigee:   126
6955  deg
Mean anomaly:     233
4817  deg
Mean motion:   15
50936056  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              328


Coasting Arc #13 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2019/189/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4400212
81                 A    =         6787193
80  meter
 Y    =         301965
07  meter          E    =           
0008804
 Z    =        5150911
59                 I    =           51
24953
 XDOT =       1074
340684                 Wp   =          101
85856
 YDOT =       7472
605530  meter/sec      RA   =          253
53220  deg
 ZDOT =      -1355
644039                 TA   =            1
24111
                                          MA   =            1
23893
                                          Ha   =            228
018  n
mi
                                          Hp   =            217
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14436393
75                 X    =         4371489
16
 Y    =         990699
06  feet           Y    =          351010
29  meter
 Z    =       16899316
24                 Z    =         5172216
19
 XDOT =       3524
739778                 XDOT =         997
284908
 YDOT =      24516
422343  feet/sec       YDOT =        7484
188834  meter/sec
 ZDOT =      -4447
651045                 ZDOT =       -1350
611855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14312607
85                 X    =        -4362482
87
 Y    =       -1125052
07  feet           Y    =         -342915
87  meter
 Z    =       16995921
65                 Z    =         5180356
92
 XDOT =      -3408
343274                 XDOT =       -1038
863030
 YDOT =     -23504
445960  feet/sec       YDOT =       -7164
155129  meter/sec
 ZDOT =      -4425
493450                 ZDOT =       -1348
890404


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   19189
75158989  
00016717  00000-0  10270-3 0  9120
2 25544  51
6380 254
2890 0006608 130
3981 229
7748 15
50956978 18597


Satellite: ISS
Catalog Number: 25544
Epoch time:      19189
75158989   =   yrday
fracday
Element set:     912
Inclination:       51
6380  deg
RA of node:       254
2890  deg
Eccentricity:     
0006608     
Arg of perigee:   130
3981  deg
Mean anomaly:     229
7748  deg
Mean motion:   15
50956978  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              371


Coasting Arc #14 (Orbit 1873)
---------------------------------------

Vector Time (GMT): 2019/190/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4577658
30                 A    =         6788089
60  meter
 Y    =        -735182
23  meter          E    =           
0018715
 Z    =       -4975415
13                 I    =           51
26285
 XDOT =      -1080
237713                 Wp   =          115
03195
 YDOT =      -7283
962015  meter/sec      RA   =          248
54055  deg
 ZDOT =       2068
560048                 TA   =          175
26353
                                          MA   =          175
24580
                                          Ha   =            228
169  n
mi
                                          Hp   =            217
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15018563
98                 X    =        -4544929
45
 Y    =       -2412015
19  feet           Y    =         -786189
37  meter
 Z    =      -16323540
46                 Z    =        -4997572
08
 XDOT =      -3544
086986                 XDOT =       -1008
753914
 YDOT =     -23897
513171  feet/sec       YDOT =       -7295
642486  meter/sec
 ZDOT =       6786
614331                 ZDOT =        2063
485660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14927074
64                 X    =         4549772
35
 Y    =        2295294
39  feet           Y    =          699605
73  meter
 Z    =      -16423980
05                 Z    =        -5006029
12
 XDOT =       3945
629179                 XDOT =        1202
627774
 YDOT =      22779
466526  feet/sec       YDOT =        6943
181397  meter/sec
 ZDOT =       6764
230981                 ZDOT =        2061
737603


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   19190
71809403  
00016717  00000-0  10270-3 0  9133
2 25544  51
6381 249
4942 0006609 133
5132 226
6569 15
50934226 18742


Satellite: ISS
Catalog Number: 25544
Epoch time:      19190
71809403   =   yrday
fracday
Element set:     913
Inclination:       51
6381  deg
RA of node:       249
4942  deg
Eccentricity:     
0006609     
Arg of perigee:   133
5132  deg
Mean anomaly:     226
6569  deg
Mean motion:   15
50934226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1874
Checksum:              319


Coasting Arc #15 (Orbit 1889)
---------------------------------------

Vector Time (GMT): 2019/191/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4763956
99                 A    =         6789088
96  meter
 Y    =        1128987
48  meter          E    =           
0011408
 Z    =        4692942
68                 I    =           51
28011
 XDOT =       1048
045892                 Wp   =           96
47804
 YDOT =       7078
726997  meter/sec      RA   =          243
55034  deg
 ZDOT =      -2762
310025                 TA   =           21
03356
                                          MA   =           20
98668
                                          Ha   =            227
883  n
mi
                                          Hp   =            217
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15629780
17                 X    =         4728182
67
 Y    =        3704027
17  feet           Y    =         1182060
88  meter
 Z    =       15396793
57                 Z    =         4715997
32
 XDOT =       3438
470773                 XDOT =         982
229346
 YDOT =      23224
169939  feet/sec       YDOT =        7090
079264  meter/sec
 ZDOT =      -9062
696934                 ZDOT =       -2757
378160

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15614008
17                 X    =        -4759149
69
 Y    =       -3314237
45  feet           Y    =        -1010179
58  meter
 Z    =       15501279
83                 Z    =         4724790
09
 XDOT =      -4322
748977                 XDOT =       -1317
573888
 YDOT =     -21989
835103  feet/sec       YDOT =       -6702
501739  meter/sec
 ZDOT =      -9040
927556                 ZDOT =       -2755
674719


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   19191
74902971  
00016717  00000-0  10270-3 0  9142
2 25544  51
6384 244
3792 0006516 137
6747 222
4908 15
50963587 18907


Satellite: ISS
Catalog Number: 25544
Epoch time:      19191
74902971   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       244
3792  deg
Eccentricity:     
0006516     
Arg of perigee:   137
6747  deg
Mean anomaly:     222
4908  deg
Mean motion:   15
50963587  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1890
Checksum:              343


Coasting Arc #16 (Orbit 1904)
---------------------------------------

Vector Time (GMT): 2019/192/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5001149
69                 A    =         6790460
70  meter
 Y    =       -1475545
20  meter          E    =           
0014897
 Z    =       -4365668
23                 I    =           51
30086
 XDOT =       -961
010863                 Wp   =          123
10742
 YDOT =      -6787
661413  meter/sec      RA   =          238
56281  deg
 ZDOT =       3395
530888                 TA   =          181
55103
                                          MA   =          181
55565
                                          Ha   =            228
019  n
mi
                                          Hp   =            217
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16407971
41                 X    =        -4963072
11
 Y    =       -4841027
55  feet           Y    =        -1531258
13  meter
 Z    =      -14323058
48                 Z    =        -4389869
54
 XDOT =      -3152
922778                 XDOT =        -901
531402
 YDOT =     -22269
230357  feet/sec       YDOT =       -6798
075952  meter/sec
 ZDOT =      11140
193201                 ZDOT =        3391
006315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16501473
73                 X    =         5029649
19
 Y    =        4147864
79  feet           Y    =         1264269
19  meter
 Z    =      -14432728
78                 Z    =        -4399095
73
 XDOT =       4469
055814                 XDOT =        1362
168212
 YDOT =      20908
757696  feet/sec       YDOT =        6372
989346  meter/sec
 ZDOT =      11120
233996                 ZDOT =        3389
447322


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   19192
71553055  
00016717  00000-0  10270-3 0  9156
2 25544  51
6390 239
5843 0006473 140
0103 220
1526 15
50942135 19057


Satellite: ISS
Catalog Number: 25544
Epoch time:      19192
71553055   =   yrday
fracday
Element set:     915
Inclination:       51
6390  deg
RA of node:       239
5843  deg
Eccentricity:     
0006473     
Arg of perigee:   140
0103  deg
Mean anomaly:     220
1526  deg
Mean motion:   15
50942135  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1905
Checksum:              287


Coasting Arc #17 (Orbit 1920)
---------------------------------------

Vector Time (GMT): 2019/193/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5228877
35                 A    =         6791846
74  meter
 Y    =        1776257
82  meter          E    =           
0014853
 Z    =        3938735
38                 I    =           51
32335
 XDOT =        813
597772                 Wp   =          102
49123
 YDOT =       6494
822953  meter/sec      RA   =          233
57803  deg
 ZDOT =      -3999
438923                 TA   =           29
45276
                                          MA   =           29
36915
                                          Ha   =            227
744  n
mi
                                          Hp   =            218
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17155109
41                 X    =         5189494
01
 Y    =        5827617
52  feet           Y    =         1834510
04  meter
 Z    =       12922360
18                 Z    =         3964039
78
 XDOT =       2669
284028                 XDOT =         760
337289
 YDOT =      21308
474255  feet/sec       YDOT =        6503
623934  meter/sec
 ZDOT =     -13121
518776                 ZDOT =       -3995
615241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17384242
58                 X    =        -5298717
14
 Y    =       -4803165
10  feet           Y    =        -1464004
72  meter
 Z    =       13037024
67                 Z    =         3973685
12
 XDOT =      -4369
968495                 XDOT =       -1331
966397
 YDOT =     -19838
221619  feet/sec       YDOT =       -6046
689950  meter/sec
 ZDOT =     -13104
703311                 ZDOT =       -3994
313569


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   19193
74646411  
00016717  00000-0  10270-3 0  9160
2 25544  51
6382 234
4697 0006368 144
0017 216
1564 15
50968590 19218


Satellite: ISS
Catalog Number: 25544
Epoch time:      19193
74646411   =   yrday
fracday
Element set:     916
Inclination:       51
6382  deg
RA of node:       234
4697  deg
Eccentricity:     
0006368     
Arg of perigee:   144
0017  deg
Mean anomaly:     216
1564  deg
Mean motion:   15
50968590  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1921
Checksum:              322


Coasting Arc #18 (Orbit 1929)
---------------------------------------

Vector Time (GMT): 2019/194/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5152000
27                 A    =         6797310
52  meter
 Y    =       -4089565
26  meter          E    =           
0008086
 Z    =       -1720044
73                 I    =           51
35711
 XDOT =       1918
067257                 Wp   =           88
88754
 YDOT =      -4786
598885  meter/sec      RA   =          230
50959  deg
 ZDOT =       5658
756867                 TA   =          252
21334
                                          MA   =          252
30159
                                          Ha   =            227
928  n
mi
                                          Hp   =            218
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16902888
01                 X    =        -5097531
70
 Y    =      -13417208
84  feet           Y    =        -4146873
73  meter
 Z    =       -5643191
36                 Z    =        -1744939
38
 XDOT =       6292
871578                 XDOT =        1943
962903
 YDOT =     -15704
064582  feet/sec       YDOT =       -4765
005763  meter/sec
 ZDOT =      18565
475284                 ZDOT =        5668
136243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21353546
65                 X    =        -6508561
02
 Y    =        2910552
68  feet           Y    =          887136
46  meter
 Z    =       -5755819
10                 Z    =        -1754373
66
 XDOT =      -6870
492361                 XDOT =       -2094
126072
 YDOT =     -13754
838721  feet/sec       YDOT =       -4192
474842  meter/sec
 ZDOT =      18608
422835                 ZDOT =        5671
847280


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   19194
32636392  
00016717  00000-0  10270-3 0  9173
2 25544  51
6416 231
5906 0006635 148
8926 211
2619 15
50938699 19309


Satellite: ISS
Catalog Number: 25544
Epoch time:      19194
32636392   =   yrday
fracday
Element set:     917
Inclination:       51
6416  deg
RA of node:       231
5906  deg
Eccentricity:     
0006635     
Arg of perigee:   148
8926  deg
Mean anomaly:     211
2619  deg
Mean motion:   15
50938699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1930
Checksum:              336
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