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

 
Date: March 3rd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


060/17:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 224 7
000/00:00:00 000 0 0 0 0 215 5

061/07:49:02 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 6

062/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 5

066/23:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 224 6
000/00:00:00 000 0 0 0 0 215 4

067/07:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 4

073/19:14:11 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 5

074/01:07:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 6

Coasting Arc #1 (Orbit 3851)
---------------------------------------

Vector Time (GMT): 2019/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6574664
94                 A    =         6792362
74  meter
 Y    =         704505
14  meter          E    =           
0010044
 Z    =       -1544823
40                 I    =           51
68144
 XDOT =      -1849
303897                 Wp   =          123
84922
 YDOT =       4708
889880  meter/sec      RA   =          175
47650  deg
 ZDOT =      -5755
401867                 TA   =           73
00686
                                          MA   =           72
89682
                                          Ha   =            224
432  n
mi
                                          Hp   =            215
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21570423
03                 X    =         6573802
07
 Y    =        2311368
58  feet           Y    =          778022
74  meter
 Z    =       -5068318
25                 Z    =        -1512888
93
 XDOT =      -6067
270002                 XDOT =       -1873
866620
 YDOT =      15449
113779  feet/sec       YDOT =        4688
072054  meter/sec
 ZDOT =     -18882
552056                 ZDOT =       -5764
444792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19186463
37                 X    =         5848034
04
 Y    =       10195431
01  feet           Y    =         3107567
37  meter
 Z    =       -4924046
50                 Z    =        -1500849
37
 XDOT =     -10526
183405                 XDOT =       -3208
380702
 YDOT =      10722
107270  feet/sec       YDOT =        3268
098296  meter/sec
 ZDOT =     -18923
770558                 ZDOT =       -5767
965266


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   19060
52930245  
00016717  00000-0  10270-3 0  9003
2 25544  51
6392 176
5055 0003485  72
8865 287
2669 15
52756296 38529


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
52930245   =   yrday
fracday
Element set:     900
Inclination:       51
6392  deg
RA of node:       176
5055  deg
Eccentricity:     
0003485     
Arg of perigee:    72
8865  deg
Mean anomaly:     287
2669  deg
Mean motion:   15
52756296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3852
Checksum:              336


Coasting Arc #2 (Orbit 3855)
---------------------------------------

Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6115400
64                 A    =         6790719
51  meter
 Y    =       -1429405
78  meter          E    =           
0017607
 Z    =        2561088
56                 I    =           51
68243
 XDOT =       3272
690354                 Wp   =           74
52926
 YDOT =      -4509
855029  meter/sec      RA   =          174
35607  deg
 ZDOT =       5271
919142                 TA   =          314
24012
                                          MA   =          314
38454
                                          Ha   =            224
658  n
mi
                                          Hp   =            215
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20063650
41                 X    =        -6111402
20
 Y    =       -4689651
51  feet           Y    =        -1497769
98  meter
 Z    =        8402521
52                 Z    =         2531392
65
 XDOT =      10737
173079                 XDOT =        3297
270081
 YDOT =     -14796
112299  feet/sec       YDOT =       -4473
119819  meter/sec
 ZDOT =      17296
322644                 ZDOT =        5287
876235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14062715
08                 X    =        -4286315
56
 Y    =       15133360
80  feet           Y    =         4612648
37  meter
 Z    =        8268415
96                 Z    =         2520213
18
 XDOT =      -6462
156015                 XDOT =       -1969
665153
 YDOT =     -15541
377855  feet/sec       YDOT =       -4737
011970  meter/sec
 ZDOT =      17368
776204                 ZDOT =        5294
002987


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   19060
78674004  
00016717  00000-0  10270-3 0  9010
2 25544  51
6385 175
2278 0003955  68
6659 291
4914 15
52727639 38563


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
78674004   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:       175
2278  deg
Eccentricity:     
0003955     
Arg of perigee:    68
6659  deg
Mean anomaly:     291
4914  deg
Mean motion:   15
52727639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3856
Checksum:              347


Coasting Arc #3 (Orbit 3864)
---------------------------------------

Vector Time (GMT): 2019/061/07:49:02
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4346269
57                 A    =         6787384
60  meter
 Y    =       -3638097
87  meter          E    =           
0015028
 Z    =        3723182
34                 I    =           51
68957
 XDOT =       5823
381087                 Wp   =           81
18903
 YDOT =       2544
376627  meter/sec      RA   =          171
33163  deg
 ZDOT =      -4294
655384                 TA   =           54
40840
                                          MA   =           54
26845
                                          Ha   =            224
338  n
mi
                                          Hp   =            215
595

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14259414
61                 X    =         4368544
04
 Y    =      -11936016
65  feet           Y    =        -3589370
09  meter
 Z    =       12215165
15                 Z    =         3744348
72
 XDOT =      19105
580993                 XDOT =        5815
356933
 YDOT =       8347
692345  feet/sec       YDOT =        2609
452631  meter/sec
 ZDOT =     -14090
076718                 ZDOT =       -4266
387847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13394840
56                 X    =         4082747
40
 Y    =       12807208
60  feet           Y    =         3903637
18  meter
 Z    =       12311105
23                 Z    =         3752424
87
 XDOT =      -5293
105353                 XDOT =       -1613
338512
 YDOT =      19010
986803  feet/sec       YDOT =        5794
548777  meter/sec
 ZDOT =     -13962
497793                 ZDOT =       -4255
769327


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   19061
36597037  
00016717  00000-0  10270-3 0  9026
2 25544  51
6365 172
3432 0003502  70
6740 289
4790 15
52746658 38654


Satellite: ISS
Catalog Number: 25544
Epoch time:      19061
36597037   =   yrday
fracday
Element set:     902
Inclination:       51
6365  deg
RA of node:       172
3432  deg
Eccentricity:     
0003502     
Arg of perigee:    70
6740  deg
Mean anomaly:     289
4790  deg
Mean motion:   15
52746658  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3865
Checksum:              324


Coasting Arc #4 (Orbit 3879)
---------------------------------------

Vector Time (GMT): 2019/062/07:49:02
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5144765
39                 A    =         6790030
41  meter
 Y    =        3478269
52  meter          E    =           
0008418
 Z    =       -2747513
84                 I    =           51
73189
 XDOT =      -4790
316119                 Wp   =           67
39088
 YDOT =      -3024
184096  meter/sec      RA   =          166
36438  deg
 ZDOT =       5157
190934                 TA   =          261
59016
                                          MA   =          261
68560
                                          Ha   =            224
473  n
mi
                                          Hp   =            215
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16879151
54                 X    =        -5169932
43
 Y    =       11411645
39  feet           Y    =         3420596
24  meter
 Z    =       -9014153
01                 Z    =        -2772565
96
 XDOT =     -15716
260234                 XDOT =       -4781
192998
 YDOT =      -9921
863833  feet/sec       YDOT =       -3077
701381  meter/sec
 ZDOT =      16919
917763                 ZDOT =        5133
944295

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13423129
14                 X    =        -4091369
76
 Y    =      -15260793
14  feet           Y    =        -4651489
75  meter
 Z    =       -9127659
00                 Z    =        -2782110
46
 XDOT =       6752
228778                 XDOT =        2058
079331
 YDOT =     -15965
862608  feet/sec       YDOT =       -4866
394923  meter/sec
 ZDOT =      16815
052900                 ZDOT =        5125
228124


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   19062
33135564  
00016717  00000-0  10270-3 0  9038
2 25544  51
6371 167
5404 0003765  76
6326 283
5245 15
52760026 38805


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
33135564   =   yrday
fracday
Element set:     903
Inclination:       51
6371  deg
RA of node:       167
5404  deg
Eccentricity:     
0003765     
Arg of perigee:    76
6326  deg
Mean anomaly:     283
5245  deg
Mean motion:   15
52760026  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3880
Checksum:              307


Coasting Arc #5 (Orbit 3881)
---------------------------------------

Vector Time (GMT): 2019/062/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6326912
83                 A    =         6792990
58  meter
 Y    =        2306480
87  meter          E    =           
0013099
 Z    =        -855749
51                 I    =           51
74883
 XDOT =      -2339
846732                 Wp   =           49
55559
 YDOT =      -4238
851372  meter/sec      RA   =          165
72028  deg
 ZDOT =       5942
670892                 TA   =          301
20703
                                          MA   =          301
33535
                                          Ha   =            224
456  n
mi
                                          Hp   =            215
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20757588
04                 X    =        -6348077
67
 Y    =        7567194
46  feet           Y    =         2235610
51  meter
 Z    =       -2807577
13                 Z    =         -886534
13
 XDOT =      -7676
662505                 XDOT =       -2321
138314
 YDOT =     -13906
992691  feet/sec       YDOT =       -4264
912134  meter/sec
 ZDOT =      19496
951747                 ZDOT =        5931
350811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21333112
21                 X    =        -6502332
60
 Y    =       -5677711
61  feet           Y    =        -1730566
50  meter
 Z    =       -2946913
10                 Z    =         -898219
11
 XDOT =       1152
891393                 XDOT =         351
401297
 YDOT =     -14314
496463  feet/sec       YDOT =       -4363
058522  meter/sec
 ZDOT =      19446
090005                 ZDOT =        5927
168234


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   19062
46007331  
00016717  00000-0  10270-3 0  9043
2 25544  51
6401 166
9005 0003666  77
2253 282
9308 15
52751228 38824


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
46007331   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       166
9005  deg
Eccentricity:     
0003666     
Arg of perigee:    77
2253  deg
Mean anomaly:     282
9308  deg
Mean motion:   15
52751228  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3882
Checksum:              301


Coasting Arc #6 (Orbit 3897)
---------------------------------------

Vector Time (GMT): 2019/063/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6500781
83                 A    =         6793229
57  meter
 Y    =       -1906538
39  meter          E    =           
0013641
 Z    =        -433651
57                 I    =           51
78126
 XDOT =        977
226863                 Wp   =          125
61870
 YDOT =       4665
587066  meter/sec      RA   =          160
76546  deg
 ZDOT =      -6003
002915                 TA   =           59
04511
                                          MA   =           58
91113
                                          Ha   =            224
475  n
mi
                                          Hp   =            215
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21328024
36                 X    =         6523724
52
 Y    =       -6255047
22  feet           Y    =        -1833713
86  meter
 Z    =       -1422741
37                 Z    =         -402018
06
 XDOT =       3206
124879                 XDOT =         954
140895
 YDOT =      15307
044180  feet/sec       YDOT =        4676
385484  meter/sec
 ZDOT =     -19694
891455                 ZDOT =       -5998
312511

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21191300
47                 X    =         6459108
38
 Y    =        6732450
63  feet           Y    =         2052050
95  meter
 Z    =       -1279579
89                 Z    =         -390015
95
 XDOT =      -5291
553836                 XDOT =       -1612
865609
 YDOT =      13013
861410  feet/sec       YDOT =        3966
624958  meter/sec
 ZDOT =     -19674
027754                 ZDOT =       -5996
643659


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   19063
48981407  
00016717  00000-0  10270-3 0  9052
2 25544  51
6397 161
7781 0003584  82
4070 277
7488 15
52764977 38989


Satellite: ISS
Catalog Number: 25544
Epoch time:      19063
48981407   =   yrday
fracday
Element set:     905
Inclination:       51
6397  deg
RA of node:       161
7781  deg
Eccentricity:     
0003584     
Arg of perigee:    82
4070  deg
Mean anomaly:     277
7488  deg
Mean motion:   15
52764977  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3898
Checksum:              365


Coasting Arc #7 (Orbit 3913)
---------------------------------------

Vector Time (GMT): 2019/064/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6416986
92                 A    =         6792190
58  meter
 Y    =        1459101
01  meter          E    =           
0017370
 Z    =        1650425
13                 I    =           51
81021
 XDOT =        327
470701                 Wp   =           67
97025
 YDOT =      -5087
707441  meter/sec      RA   =          155
81168  deg
 ZDOT =       5729
284318                 TA   =          310
05917
                                          MA   =          310
21139
                                          Ha   =            224
502  n
mi
                                          Hp   =            215
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21053106
68                 X    =        -6440842
75
 Y    =        4787076
80  feet           Y    =         1387208
56  meter
 Z    =        5414780
61                 Z    =         1619196
41
 XDOT =       1074
378941                 XDOT =         356
509475
 YDOT =     -16691
953548  feet/sec       YDOT =       -5083
882472  meter/sec
 ZDOT =      18796
864560                 ZDOT =        5730
946071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20296861
31                 X    =        -6186483
33
 Y    =       -7463057
52  feet           Y    =        -2274739
93  meter
 Z    =        5273466
39                 Z    =         1607352
56
 XDOT =       9336
628155                 XDOT =        2845
804262
 YDOT =     -12005
031384  feet/sec       YDOT =       -3659
133566  meter/sec
 ZDOT =      18804
751831                 ZDOT =        5731
688358


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   19064
51955171  
00016717  00000-0  10270-3 0  9067
2 25544  51
6411 156
6558 0003657  84
5870 275
5699 15
52770773 39143


Satellite: ISS
Catalog Number: 25544
Epoch time:      19064
51955171   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:       156
6558  deg
Eccentricity:     
0003657     
Arg of perigee:    84
5870  deg
Mean anomaly:     275
5699  deg
Mean motion:   15
52770773  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3914
Checksum:              344


Coasting Arc #8 (Orbit 3928)
---------------------------------------

Vector Time (GMT): 2019/065/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6115001
86                 A    =         6790010
33  meter
 Y    =        -867899
89  meter          E    =           
0008040
 Z    =       -2824342
98                 I    =           51
83254
 XDOT =      -1577
227457                 Wp   =          106
90474
 YDOT =       5481
233431  meter/sec      RA   =          150
85679  deg
 ZDOT =      -5113
512731                 TA   =          105
03018
                                          MA   =          104
94119
                                          Ha   =            224
508  n
mi
                                          Hp   =            215
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20062342
06                 X    =         6137971
31
 Y    =       -2847440
58  feet           Y    =         -799389
56  meter
 Z    =       -9266217
13                 Z    =        -2794583
28
 XDOT =      -5174
630763                 XDOT =       -1613
564811
 YDOT =      17983
049313  feet/sec       YDOT =        5463
391999  meter/sec
 ZDOT =     -16776
616571                 ZDOT =       -5121
263056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18576321
30                 X    =         5662062
73
 Y    =        8246386
26  feet           Y    =         2513498
53  meter
 Z    =       -9131575
30                 Z    =        -2783304
15
 XDOT =     -13219
066648                 XDOT =       -4029
171514
 YDOT =      11214
107006  feet/sec       YDOT =        3418
059815  meter/sec
 ZDOT =     -16812
068155                 ZDOT =       -5124
318374


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   19065
48492770  
00016717  00000-0  10270-3 0  9076
2 25544  51
6409 151
8537 0003631  87
8243 272
3324 15
52766373 39293


Satellite: ISS
Catalog Number: 25544
Epoch time:      19065
48492770   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       151
8537  deg
Eccentricity:     
0003631     
Arg of perigee:    87
8243  deg
Mean anomaly:     272
3324  deg
Mean motion:   15
52766373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3929
Checksum:              333


Coasting Arc #9 (Orbit 3944)
---------------------------------------

Vector Time (GMT): 2019/066/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5615112
75                 A    =         6787212
98  meter
 Y    =         201569
26  meter          E    =           
0015220
 Z    =        3795538
83                 I    =           51
85184
 XDOT =       2662
716218                 Wp   =           95
48360
 YDOT =      -5817
367151  meter/sec      RA   =          145
89882  deg
 ZDOT =       4232
173715                 TA   =          309
89747
                                          MA   =          310
03118
                                          Ha   =            224
542  n
mi
                                          Hp   =            215
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18422285
94                 X    =        -5635385
76
 Y    =         661316
47  feet           Y    =          138664
26  meter
 Z    =       12452555
20                 Z    =         3768213
89
 XDOT =       8735
945596                 XDOT =        2707
012540
 YDOT =     -19085
850232  feet/sec       YDOT =       -5787
342591  meter/sec
 ZDOT =      13885
084368                 ZDOT =        4245
216299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16201969
99                 X    =        -4938360
45
 Y    =       -8965319
71  feet           Y    =        -2732629
45  meter
 Z    =       12328961
87                 Z    =         3757867
58
 XDOT =      16585
529693                 XDOT =        5055
269450
 YDOT =     -10723
982448  feet/sec       YDOT =       -3268
669850  meter/sec
 ZDOT =      13944
501559                 ZDOT =        4250
284075


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   19066
51465873  
00016717  00000-0  10270-3 0  9086
2 25544  51
6408 146
7315 0003649  91
2222 268
9348 15
52799222 39458


Satellite: ISS
Catalog Number: 25544
Epoch time:      19066
51465873   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       146
7315  deg
Eccentricity:     
0003649     
Arg of perigee:    91
2222  deg
Mean anomaly:     268
9348  deg
Mean motion:   15
52799222  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3945
Checksum:              338


Coasting Arc #10 (Orbit 3952)
---------------------------------------

Vector Time (GMT): 2019/066/23:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 935961
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4276221
71                 A    =         6782829
80  meter
 Y    =       -1691595
53  meter          E    =           
0009617
 Z    =        4979121
99                 I    =           51
85073
 XDOT =       4739
971142                 Wp   =          109
33532
 YDOT =      -5635
997165  meter/sec      RA   =          143
31917  deg
 ZDOT =       2149
587112                 TA   =          319
75542
                                          MA   =          319
82658
                                          Ha   =            224
617  n
mi
                                          Hp   =            215
410

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14029598
79                 X    =        -4281173
47
 Y    =       -5549854
11  feet           Y    =        -1739442
29  meter
 Z    =       16335702
06                 Z    =         4958338
18
 XDOT =      15551
086425                 XDOT =        4792
200819
 YDOT =     -18490
804348  feet/sec       YDOT =       -5582
699186  meter/sec
 ZDOT =       7052
451155                 ZDOT =        2172
739365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10730798
53                 X    =         3270747
39
 Y    =       10748890
65  feet           Y    =         3276261
87  meter
 Z    =       16241828
63                 Z    =         4950509
37
 XDOT =     -20829
467254                 XDOT =       -6348
821619
 YDOT =       9946
801291  feet/sec       YDOT =        3031
785033  meter/sec
 ZDOT =       7157
583295                 ZDOT =        2181
631388


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   19067
02952560  
00016717  00000-0  10270-3 0  9098
2 25544  51
6402 144
1734 0003747  85
7755 274
3825 15
52787936 39536


Satellite: ISS
Catalog Number: 25544
Epoch time:      19067
02952560   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:       144
1734  deg
Eccentricity:     
0003747     
Arg of perigee:    85
7755  deg
Mean anomaly:     274
3825  deg
Mean motion:   15
52787936  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3953
Checksum:              338


Coasting Arc #11 (Orbit 3957)
---------------------------------------

Vector Time (GMT): 2019/067/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5924207
86                 A    =         6790840
34  meter
 Y    =        2269572
02  meter          E    =           
0017324
 Z    =        2401788
56                 I    =           51
88374
 XDOT =        103
166612                 Wp   =           78
17688
 YDOT =      -5460
373434  meter/sec      RA   =          141
75912  deg
 ZDOT =       5384
944525                 TA   =          308
56857
                                          MA   =          308
72366
                                          Ha   =            224
513  n
mi
                                          Hp   =            215
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19436377
49                 X    =        -5960812
97
 Y    =        7446102
42  feet           Y    =         2203119
02  meter
 Z    =        7879883
71                 Z    =         2372922
14
 XDOT =        338
473138                 XDOT =         138
061641
 YDOT =     -17914
611003  feet/sec       YDOT =       -5459
023954  meter/sec
 ZDOT =      17667
140831                 ZDOT =        5385
531114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7383403
47                 X    =        -2250461
38
 Y    =      -19512706
77  feet           Y    =        -5947473
02  meter
 Z    =        7749155
21                 Z    =         2361942
51
 XDOT =      16489
737255                 XDOT =        5026
071915
 YDOT =        816
722543  feet/sec       YDOT =         248
937031  meter/sec
 ZDOT =      17670
203045                 ZDOT =        5385
877888


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   19067
35131539  
00016717  00000-0  10270-3 0  9101
2 25544  51
6380 142
5675 0003731  94
6506 265
5072 15
52798721 39588


Satellite: ISS
Catalog Number: 25544
Epoch time:      19067
35131539   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       142
5675  deg
Eccentricity:     
0003731     
Arg of perigee:    94
6506  deg
Mean anomaly:     265
5072  deg
Mean motion:   15
52798721  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3958
Checksum:              323


Coasting Arc #12 (Orbit 3972)
---------------------------------------

Vector Time (GMT): 2019/068/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5625011
79                 A    =         6788215
86  meter
 Y    =       -1535003
20  meter          E    =           
0008699
 Z    =       -3483230
86                 I    =           51
90070
 XDOT =      -1181
063454                 Wp   =           92
04588
 YDOT =       6028
234831  meter/sec      RA   =          136
80537  deg
 ZDOT =      -4573
979824                 TA   =          128
62405
                                          MA   =          128
54614
                                          Ha   =            224
527  n
mi
                                          Hp   =            215
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18454763
09                 X    =         5658678
03
 Y    =       -5036099
75  feet           Y    =        -1471912
58  meter
 Z    =      -11427922
77                 Z    =        -3455824
94
 XDOT =      -3874
880098                 XDOT =       -1226
167436
 YDOT =      19777
673330  feet/sec       YDOT =        6014
774588  meter/sec
 ZDOT =     -15006
495485                 ZDOT =       -4579
827241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5295052
35                 X    =         1613931
95
 Y    =       18458698
18  feet           Y    =         5626211
21  meter
 Z    =      -11303843
70                 Z    =        -3445411
56
 XDOT =     -18481
406738                 XDOT =       -5633
132774
 YDOT =      -3884
049191  feet/sec       YDOT =       -1183
858194  meter/sec
 ZDOT =     -15033
404027                 ZDOT =       -4582
181547


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   19068
31668537  
00016717  00000-0  10270-3 0  9112
2 25544  51
6384 137
7644 0003783  95
7003 264
4580 15
52784843 39734


Satellite: ISS
Catalog Number: 25544
Epoch time:      19068
31668537   =   yrday
fracday
Element set:     911
Inclination:       51
6384  deg
RA of node:       137
7644  deg
Eccentricity:     
0003783     
Arg of perigee:    95
7003  deg
Mean anomaly:     264
4580  deg
Mean motion:   15
52784843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3973
Checksum:              340


Coasting Arc #13 (Orbit 3988)
---------------------------------------

Vector Time (GMT): 2019/069/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5173436
76                 A    =         6785359
44  meter
 Y    =         694602
57  meter          E    =           
0013567
 Z    =        4326211
31                 I    =           51
91489
 XDOT =       2091
869239                 Wp   =          105
52809
 YDOT =      -6481
583473  meter/sec      RA   =          131
84810  deg
 ZDOT =       3529
465207                 TA   =          308
63919
                                          MA   =          308
76055
                                          Ha   =            224
572  n
mi
                                          Hp   =            215
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16973217
72                 X    =        -5201833
73
 Y    =        2278879
81  feet           Y    =          636591
31  meter
 Z    =       14193606
66                 Z    =         4301011
77
 XDOT =       6863
088055                 XDOT =        2147
048570
 YDOT =     -21265
037640  feet/sec       YDOT =       -6457
881791  meter/sec
 ZDOT =      11579
610259                 ZDOT =        3539
761445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2810503
08                 X    =         -856641
34
 Y    =      -16988492
77  feet           Y    =        -5178092
60  meter
 Z    =       14079562
09                 Z    =         4291450
52
 XDOT =      20226
537599                 XDOT =        6165
048660
 YDOT =       6324
556709  feet/sec       YDOT =        1927
724885  meter/sec
 ZDOT =      11626
690626                 ZDOT =        3543
815303


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   19069
34640922  
00016717  00000-0  10270-3 0  9125
2 25544  51
6384 132
6415 0003758 100
0199 260
1377 15
52809154 39899


Satellite: ISS
Catalog Number: 25544
Epoch time:      19069
34640922   =   yrday
fracday
Element set:     912
Inclination:       51
6384  deg
RA of node:       132
6415  deg
Eccentricity:     
0003758     
Arg of perigee:   100
0199  deg
Mean anomaly:     260
1377  deg
Mean motion:   15
52809154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3989
Checksum:              318


Coasting Arc #14 (Orbit 4003)
---------------------------------------

Vector Time (GMT): 2019/070/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4632935
87                 A    =         6782984
48  meter
 Y    =         298647
61  meter          E    =           
0015570
 Z    =       -4959389
94                 I    =           51
92784
 XDOT =      -2846
178014                 Wp   =           80
56169
 YDOT =       6737
448356  meter/sec      RA   =          126
88724  deg
 ZDOT =      -2256
656083                 TA   =          167
46372
                                          MA   =          167
42495
                                          Ha   =            224
482  n
mi
                                          Hp   =            215
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15199920
84                 X    =         4653341
89
 Y    =         979814
99  feet           Y    =          350569
93  meter
 Z    =      -16270964
37                 Z    =        -4936835
40
 XDOT =      -9337
854377                 XDOT =       -2910
344979
 YDOT =      22104
489356  feet/sec       YDOT =        6705
261394  meter/sec
 ZDOT =      -7403
727306                 ZDOT =       -2270
638249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -237489
82                 X    =          -72386
90
 Y    =       15337874
98  feet           Y    =         4674984
29  meter
 Z    =      -16168954
89                 Z    =        -4928297
45
 XDOT =     -21408
731480                 XDOT =       -6525
381355
 YDOT =      -8191
284311  feet/sec       YDOT =       -2496
703458  meter/sec
 ZDOT =      -7467
519416                 ZDOT =       -2276
099918


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   19070
31177553  
00016717  00000-0  10270-3 0  9130
2 25544  51
6381 127
8394 0003775 102
8826 257
2748 15
52785958 40047


Satellite: ISS
Catalog Number: 25544
Epoch time:      19070
31177553   =   yrday
fracday
Element set:     913
Inclination:       51
6381  deg
RA of node:       127
8394  deg
Eccentricity:     
0003775     
Arg of perigee:   102
8826  deg
Mean anomaly:     257
2748  deg
Mean motion:   15
52785958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4004
Checksum:              331


Coasting Arc #15 (Orbit 4019)
---------------------------------------

Vector Time (GMT): 2019/071/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4028957
12                 A    =         6781417
24  meter
 Y    =       -1350157
65  meter          E    =           
0007008
 Z    =        5279908
78                 I    =           51
94316
 XDOT =       3432
012860                 Wp   =          113
47035
 YDOT =      -6804
688450  meter/sec      RA   =          121
92251  deg
 ZDOT =        875
172462                 TA   =          328
17773
                                          MA   =          328
22005
                                          Ha   =            224
511  n
mi
                                          Hp   =            215
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13218363
26                 X    =        -4039206
66
 Y    =       -4429651
07  feet           Y    =        -1395269
13  meter
 Z    =       17322535
36                 Z    =         5260312
86
 XDOT =      11259
884712                 XDOT =        3503
598644
 YDOT =     -22325
093339  feet/sec       YDOT =       -6765
908948  meter/sec
 ZDOT =       2871
300728                 ZDOT =         892
018307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3545340
97                 X    =         1080619
93
 Y    =      -13595488
28  feet           Y    =        -4143904
83  meter
 Z    =       17233990
33                 Z    =         5252920
25
 XDOT =      22022
000342                 XDOT =        6712
305704
 YDOT =       9495
006794  feet/sec       YDOT =        2894
078071  meter/sec
 ZDOT =       2948
074597                 ZDOT =         898
573137


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   19071
34149522  
00016717  00000-0  10270-3 0  9140
2 25544  51
6392 122
7156 0003652 106
3809 253
7745 15
52822537 40204


Satellite: ISS
Catalog Number: 25544
Epoch time:      19071
34149522   =   yrday
fracday
Element set:     914
Inclination:       51
6392  deg
RA of node:       122
7156  deg
Eccentricity:     
0003652     
Arg of perigee:   106
3809  deg
Mean anomaly:     253
7745  deg
Mean motion:   15
52822537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4020
Checksum:              298


Coasting Arc #16 (Orbit 4034)
---------------------------------------

Vector Time (GMT): 2019/072/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3424321
21                 A    =         6781291
00  meter
 Y    =        2460711
72  meter          E    =           
0018476
 Z    =       -5326802
25                 I    =           51
95982
 XDOT =      -3850
136960                 Wp   =           97
24546
 YDOT =       6589
109649  meter/sec      RA   =          116
95887  deg
 ZDOT =        568
205151                 TA   =          178
16757
                                          MA   =          178
16079
                                          Ha   =            224
438  n
mi
                                          Hp   =            215
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11234649
64                 X    =         3422424
92
 Y    =        8073201
17  feet           Y    =         2498993
92  meter
 Z    =      -17476385
32                 Z    =        -5310172
99
 XDOT =     -12631
682938                 XDOT =       -3926
292119
 YDOT =      21617
813810  feet/sec       YDOT =        6545
628954  meter/sec
 ZDOT =       1864
190128                 ZDOT =         549
317275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7105933
51                 X    =        -2165888
54
 Y    =       11979841
66  feet           Y    =         3651455
74  meter
 Z    =      -17401352
71                 Z    =        -5303932
31
 XDOT =     -21715
670934                 XDOT =       -6618
936501
 YDOT =     -10295
159824  feet/sec       YDOT =       -3137
964714  meter/sec
 ZDOT =       1778
172486                 ZDOT =         541
986974


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   19072
30685715  
00016717  00000-0  10270-3 0  9157
2 25544  51
6397 117
9138 0003852 107
8848 252
2724 15
52813204 40354


Satellite: ISS
Catalog Number: 25544
Epoch time:      19072
30685715   =   yrday
fracday
Element set:     915
Inclination:       51
6397  deg
RA of node:       117
9138  deg
Eccentricity:     
0003852     
Arg of perigee:   107
8848  deg
Mean anomaly:     252
2724  deg
Mean motion:   15
52813204  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4035
Checksum:              315


Coasting Arc #17 (Orbit 4050)
---------------------------------------

Vector Time (GMT): 2019/073/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2822127
70                 A    =         6782513
97  meter
 Y    =       -3541217
08  meter          E    =           
0008639
 Z    =        5042813
10                 I    =           51
97767
 XDOT =       4151
871819                 Wp   =           77
87575
 YDOT =      -6138
913299  meter/sec      RA   =          111
99611  deg
 ZDOT =      -1982
780423                 TA   =           31
30226
                                          MA   =           31
25085
                                          Ha   =            224
592  n
mi
                                          Hp   =            215
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9258949
14                 X    =        -2806814
12
 Y    =      -11618166
26  feet           Y    =        -3572690
20  meter
 Z    =       16544662
40                 Z    =         5029141
71
 XDOT =      13621
626704                 XDOT =        4229
841510
 YDOT =     -20140
791662  feet/sec       YDOT =       -6092
048312  meter/sec
 ZDOT =      -6505
185115                 ZDOT =       -1962
422599

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10623940
13                 X    =         3238176
95
 Y    =      -10482121
18  feet           Y    =        -3194950
53  meter
 Z    =       16483106
87                 Z    =         5024050
98
 XDOT =      20640
108371                 XDOT =        6291
105031
 YDOT =      10811
723708  feet/sec       YDOT =        3295
413386  meter/sec
 ZDOT =      -6412
532096                 ZDOT =       -1954
539783


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   19073
33657476  
00016717  00000-0  10270-3 0  9165
2 25544  51
6395 112
7905 0003892 111
0323 249
1245 15
52788789 40516


Satellite: ISS
Catalog Number: 25544
Epoch time:      19073
33657476   =   yrday
fracday
Element set:     916
Inclination:       51
6395  deg
RA of node:       112
7905  deg
Eccentricity:     
0003892     
Arg of perigee:   111
0323  deg
Mean anomaly:     249
1245  deg
Mean motion:   15
52788789  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4051
Checksum:              325


Coasting Arc #18 (Orbit 4058)
---------------------------------------

Vector Time (GMT): 2019/073/19:14:11
000
Vector Time (MET): N/A
Weight (LBS)     : 910513
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4238704
53                 A    =         6781418
20  meter
 Y    =        -384227
92  meter          E    =           
0006976
 Z    =        5274443
59                 I    =           51
97984
 XDOT =       1839
631220                 Wp   =          114
35839
 YDOT =      -7388
225616  meter/sec      RA   =          109
50000  deg
 ZDOT =        936
400592                 TA   =          326
70588
                                          MA   =          326
74974
                                          Ha   =            224
453  n
mi
                                          Hp   =            215
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13906510
92                 X    =        -4259713
10
 Y    =       -1260590
29  feet           Y    =         -431745
30  meter
 Z    =       17304604
97                 Z    =         5253802
69
 XDOT =       6035
535498                 XDOT =        1917
563243
 YDOT =     -24239
585353  feet/sec       YDOT =       -7367
217785  meter/sec
 ZDOT =       3072
180419                 ZDOT =         945
526395

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1139811
63                 X    =          347414
59
 Y    =       14032239
38  feet           Y    =         4277026
56  meter
 Z    =       17211233
96                 Z    =         5245984
11
 XDOT =     -23885
461651                 XDOT =       -7280
288711
 YDOT =      -1894
724375  feet/sec       YDOT =        -577
511989  meter/sec
 ZDOT =       3114
126923                 ZDOT =         949
185886


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   19073
85143134  
00016717  00000-0  10270-3 0  9174
2 25544  51
6388 110
2335 0003523 107
1229 253
0309 15
52832948 40590


Satellite: ISS
Catalog Number: 25544
Epoch time:      19073
85143134   =   yrday
fracday
Element set:     917
Inclination:       51
6388  deg
RA of node:       110
2335  deg
Eccentricity:     
0003523     
Arg of perigee:   107
1229  deg
Mean anomaly:     253
0309  deg
Mean motion:   15
52832948  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4059
Checksum:              298


Coasting Arc #19 (Orbit 4062)
---------------------------------------

Vector Time (GMT): 2019/074/01:07:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2877278
61                 A    =         6792739
70  meter
 Y    =        6053183
17  meter          E    =           
0015961
 Z    =        1066367
81                 I    =           52
01855
 XDOT =      -3906
420853                 Wp   =           66
58768
 YDOT =      -2911
099652  meter/sec      RA   =          108
28730  deg
 ZDOT =       5920
580171                 TA   =          304
91131
                                          MA   =          305
06119
                                          Ha   =            224
349  n
mi
                                          Hp   =            215
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9439890
45                 X    =        -2949932
96
 Y    =       19859524
83  feet           Y    =         6020601
24  meter
 Z    =        3498582
07                 Z    =         1052214
45
 XDOT =     -12816
341382                 XDOT =       -3902
336451
 YDOT =      -9550
851877  feet/sec       YDOT =       -2954
760876  meter/sec
 ZDOT =      19424
475628                 ZDOT =        5901
614442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6525724
84                 X    =         1989040
93
 Y    =      -21008924
54  feet           Y    =        -6403520
20  meter
 Z    =        3433997
63                 Z    =         1046682
48
 XDOT =      12646
654328                 XDOT =        3854
700239
 YDOT =       7124
150773  feet/sec       YDOT =        2171
441156  meter/sec
 ZDOT =      19338
906913                 ZDOT =        5894
498827


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   19074
10885969  
00016717  00000-0  10270-3 0  9183
2 25544  51
6374 108
9510 0003509 109
1972 250
9560 15
52797937 40633


Satellite: ISS
Catalog Number: 25544
Epoch time:      19074
10885969   =   yrday
fracday
Element set:     918
Inclination:       51
6374  deg
RA of node:       108
9510  deg
Eccentricity:     
0003509     
Arg of perigee:   109
1972  deg
Mean anomaly:     250
9560  deg
Mean motion:   15
52797937  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4063
Checksum:              340


Coasting Arc #20 (Orbit 4077)
---------------------------------------

Vector Time (GMT): 2019/075/01:07:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3165093
46                 A    =         6790955
79  meter
 Y    =       -5547226
36  meter          E    =           
0009201
 Z    =       -2304597
60                 I    =           52
02219
 XDOT =       3382
357260                 Wp   =          126
57934
 YDOT =       4187
188733  meter/sec      RA   =          103
34630  deg
 ZDOT =      -5453
784320                 TA   =           78
92655
                                          MA   =           78
82309
                                          Ha   =            224
344  n
mi
                                          Hp   =            215
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10384164
90                 X    =         3238083
21
 Y    =      -18199561
54  feet           Y    =        -5511424
06  meter
 Z    =       -7561015
76                 Z    =        -2289045
42
 XDOT =      11096
972638                 XDOT =        3361
774696
 YDOT =      13737
495842  feet/sec       YDOT =        4224
897287  meter/sec
 ZDOT =     -17892
993176                 ZDOT =       -5437
404467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7387874
41                 X    =        -2251824
12
 Y    =       19635201
91  feet           Y    =         5984809
54  meter
 Z    =       -7490129
38                 Z    =        -2282991
43
 XDOT =     -11838
099471                 XDOT =       -3608
252719
 YDOT =     -11225
818551  feet/sec       YDOT =       -3421
629494  meter/sec
 ZDOT =     -17819
240674                 ZDOT =       -5431
304557


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   19075
07421640  
00016717  00000-0  10270-3 0  9193
2 25544  51
6375 104
1475 0003513 110
7330 249
4198 15
52809413 40782


Satellite: ISS
Catalog Number: 25544
Epoch time:      19075
07421640   =   yrday
fracday
Element set:     919
Inclination:       51
6375  deg
RA of node:       104
1475  deg
Eccentricity:     
0003513     
Arg of perigee:   110
7330  deg
Mean anomaly:     249
4198  deg
Mean motion:   15
52809413  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4078
Checksum:              299
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