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

 
Date: October 14th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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


291/16:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 216 4

295/18:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 216 2

300/09:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 215 5

Coasting Arc #1 (Orbit 1674)
---------------------------------------

Vector Time (GMT): 2018/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4414771
51                 A    =         6787497
63  meter
 Y    =        4488538
90  meter          E    =           
0004094
 Z    =       -2529857
62                 I    =           51
81952
 XDOT =      -5134
728058                 Wp   =            1
40016
 YDOT =      -2062
349840  meter/sec      RA   =          152
94583  deg
 ZDOT =       5305
541451                 TA   =          330
28408
                                          MA   =          330
30732
                                          Ha   =            220
084  n
mi
                                          Hp   =            216
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14484158
51                 X    =        -4452346
50
 Y    =       14726177
49  feet           Y    =         4438959
61  meter
 Z    =       -8300057
80                 Z    =        -2551395
06
 XDOT =     -16846
220662                 XDOT =       -5137
056759
 YDOT =      -6766
239631  feet/sec       YDOT =       -2119
782635  meter/sec
 ZDOT =      17406
632057                 ZDOT =        5280
592638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8477916
63                 X    =         2584068
99
 Y    =      -18792361
16  feet           Y    =        -5727911
68  meter
 Z    =       -8397273
51                 Z    =        -2559488
97
 XDOT =      16883
367423                 XDOT =        5146
050390
 YDOT =       -105
303274  feet/sec       YDOT =         -32
096438  meter/sec
 ZDOT =      17294
690476                 ZDOT =        5271
421657


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   18285
50514150  
00016717  00000-0  10270-3 0  9002
2 25544  51
6399 154
0925 0004050 282
0263  78
0435 15
53802565 16759


Satellite: ISS
Catalog Number: 25544
Epoch time:      18285
50514150   =   yrday
fracday
Element set:     900
Inclination:       51
6399  deg
RA of node:       154
0925  deg
Eccentricity:     
0004050     
Arg of perigee:   282
0263  deg
Mean anomaly:      78
0435  deg
Mean motion:   15
53802565  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1675
Checksum:              295


Coasting Arc #2 (Orbit 1690)
---------------------------------------

Vector Time (GMT): 2018/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5235042
87                 A    =         6789857
79  meter
 Y    =       -4198240
22  meter          E    =           
0010005
 Z    =         999154
61                 I    =           51
85604
 XDOT =       3687
368073                 Wp   =          131
47098
 YDOT =       3180
733195  meter/sec      RA   =          147
98724  deg
 ZDOT =      -5923
223298                 TA   =           37
73626
                                          MA   =           37
66613
                                          Ha   =            220
234  n
mi
                                          Hp   =            216
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17175337
50                 X    =         5276746
21
 Y    =      -13773754
01  feet           Y    =        -4139465
12  meter
 Z    =        3278066
32                 Z    =         1024686
63
 XDOT =      12097
664281                 XDOT =        3680
298661
 YDOT =      10435
476362  feet/sec       YDOT =        3221
928117  meter/sec
 ZDOT =     -19433
147303                 ZDOT =       -5905
328287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11037966
03                 X    =        -3364372
04
 Y    =       19029018
10  feet           Y    =         5800044
72  meter
 Z    =        3393230
43                 Z    =         1034256
64
 XDOT =     -13777
394860                 XDOT =       -4199
349953
 YDOT =      -4522
701319  feet/sec       YDOT =       -1378
519362  meter/sec
 ZDOT =     -19353
007549                 ZDOT =       -5898
796701


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   18286
53418432  
00016717  00000-0  10270-3 0  9013
2 25544  51
6397 148
9646 0003866 284
7913  75
2811 15
53791057 16912


Satellite: ISS
Catalog Number: 25544
Epoch time:      18286
53418432   =   yrday
fracday
Element set:     901
Inclination:       51
6397  deg
RA of node:       148
9646  deg
Eccentricity:     
0003866     
Arg of perigee:   284
7913  deg
Mean anomaly:      75
2811  deg
Mean motion:   15
53791057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1691
Checksum:              339


Coasting Arc #3 (Orbit 1706)
---------------------------------------

Vector Time (GMT): 2018/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5670516
58                 A    =         6790040
49  meter
 Y    =        3672855
56  meter          E    =           
0011401
 Z    =         605884
56                 I    =           51
88330
 XDOT =      -2129
330314                 Wp   =           34
36811
 YDOT =      -4283
907092  meter/sec      RA   =          143
03375  deg
 ZDOT =       5994
690500                 TA   =          332
15082
                                          MA   =          332
21180
                                          Ha   =            220
208  n
mi
                                          Hp   =            216
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18604057
01                 X    =        -5714109
14
 Y    =       12050051
05  feet           Y    =         3609200
19  meter
 Z    =        1987810
25                 Z    =          578232
66
 XDOT =      -6985
991845                 XDOT =       -2110
387784
 YDOT =     -14054
813295  feet/sec       YDOT =       -4307
612620  meter/sec
 ZDOT =      19667
619750                 ZDOT =        5984
392924

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12713642
84                 X    =         3875118
34
 Y    =      -18170251
38  feet           Y    =        -5538292
62  meter
 Z    =        1863144
49                 Z    =          567886
44
 XDOT =      10557
069776                 XDOT =        3217
794868
 YDOT =       9415
107753  feet/sec       YDOT =        2869
724843  meter/sec
 ZDOT =      19621
735915                 ZDOT =        5980
705107


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   18287
56322227  
00016717  00000-0  10270-3 0  9024
2 25544  51
6385 143
8366 0003987 288
6492  71
4227 15
53837897 17071


Satellite: ISS
Catalog Number: 25544
Epoch time:      18287
56322227   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       143
8366  deg
Eccentricity:     
0003987     
Arg of perigee:   288
6492  deg
Mean anomaly:      71
4227  deg
Mean motion:   15
53837897  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1707
Checksum:              349


Coasting Arc #4 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2018/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5751345
84                 A    =         6788322
36  meter
 Y    =       -2870710
42  meter          E    =           
0003213
 Z    =       -2176392
01                 I    =           51
90324
 XDOT =        562
108182                 Wp   =          174
20556
 YDOT =       5299
759573  meter/sec      RA   =          138
08080  deg
 ZDOT =      -5508
892698                 TA   =           29
84291
                                          MA   =           29
82459
                                          Ha   =            220
279  n
mi
                                          Hp   =            216
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18869244
90                 X    =         5793591
40
 Y    =       -9418341
26  feet           Y    =        -2806158
73  meter
 Z    =       -7140393
74                 Z    =        -2148350
85
 XDOT =       1844
186950                 XDOT =         529
562721
 YDOT =      17387
662642  feet/sec       YDOT =        5305
863306  meter/sec
 ZDOT =     -18073
794941                 ZDOT =       -5506
241350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13706682
95                 X    =        -4177796
96
 Y    =       16083188
16  feet           Y    =         4902155
75  meter
 Z    =       -7014034
42                 Z    =        -2137877
69
 XDOT =      -7453
101990                 XDOT =       -2271
705486
 YDOT =     -14223
426444  feet/sec       YDOT =       -4335
300380  meter/sec
 ZDOT =     -18062
389956                 ZDOT =       -5505
416459


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   18288
52794544  
00016717  00000-0  10270-3 0  9037
2 25544  51
6387 139
0299 0004154 291
5955  68
4755 15
53807828 17229


Satellite: ISS
Catalog Number: 25544
Epoch time:      18288
52794544   =   yrday
fracday
Element set:     903
Inclination:       51
6387  deg
RA of node:       139
0299  deg
Eccentricity:     
0004154     
Arg of perigee:   291
5955  deg
Mean anomaly:      68
4755  deg
Mean motion:   15
53807828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1722
Checksum:              350


Coasting Arc #5 (Orbit 1737)
---------------------------------------

Vector Time (GMT): 2018/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5494907
79                 A    =         6785030
92  meter
 Y    =        1818955
78  meter          E    =           
0008664
 Z    =        3531503
59                 I    =           51
91604
 XDOT =        883
475592                 Wp   =           79
84298
 YDOT =      -6130
124368  meter/sec      RA   =          133
12112  deg
 ZDOT =       4524
153608                 TA   =          321
58755
                                          MA   =          321
64921
                                          Ha   =            220
516  n
mi
                                          Hp   =            216
535

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18027912
71                 X    =        -5531993
87
 Y    =        5967702
69  feet           Y    =         1757300
67  meter
 Z    =       11586297
86                 Z    =         3504720
75
 XDOT =       2898
541968                 XDOT =         929
982452
 YDOT =     -20111
956587  feet/sec       YDOT =       -6119
984536  meter/sec
 ZDOT =      14843
023648                 ZDOT =        4528
558455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14094496
52                 X    =         4296002
54
 Y    =      -12835292
05  feet           Y    =        -3912197
02  meter
 Z    =       11465681
66                 Z    =         3494739
77
 XDOT =       4712
409541                 XDOT =        1436
342428
 YDOT =      18475
592397  feet/sec       YDOT =        5631
360563  meter/sec
 ZDOT =      14863
437117                 ZDOT =        4530
375633


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   18289
55697895  
00016717  00000-0  10270-3 0  9043
2 25544  51
6384 133
9010 0004169 297
2983  62
7745 15
53825669 17386


Satellite: ISS
Catalog Number: 25544
Epoch time:      18289
55697895   =   yrday
fracday
Element set:     904
Inclination:       51
6384  deg
RA of node:       133
9010  deg
Eccentricity:     
0004169     
Arg of perigee:   297
2983  deg
Mean anomaly:      62
7745  deg
Mean motion:   15
53825669  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1738
Checksum:              363


Coasting Arc #6 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2018/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4982507
83                 A    =         6781460
40  meter
 Y    =        -538506
54  meter          E    =           
0007906
 Z    =       -4576450
86                 I    =           51
92430
 XDOT =      -2138
362092                 Wp   =           46
63720
 YDOT =       6666
250946  meter/sec      RA   =          128
15517  deg
 ZDOT =      -3110
589778                 TA   =          192
30170
                                          MA   =          192
32102
                                          Ha   =            220
476  n
mi
                                          Hp   =            216
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16346810
47                 X    =         5010389
49
 Y    =       -1766753
74  feet           Y    =         -482632
98  meter
 Z    =      -15014602
57                 Z    =        -4552179
55
 XDOT =      -7015
623660                 XDOT =       -2197
637263
 YDOT =      21870
902053  feet/sec       YDOT =        6642
006737  meter/sec
 ZDOT =     -10205
347040                 ZDOT =       -3121
121567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14148959
92                 X    =        -4312602
98
 Y    =        8568201
64  feet           Y    =         2611587
86  meter
 Z    =      -14905394
18                 Z    =        -4543164
15
 XDOT =      -2346
167025                 XDOT =        -715
111709
 YDOT =     -21722
273895  feet/sec       YDOT =       -6620
949083  meter/sec
 ZDOT =     -10253
379374                 ZDOT =       -3125
230033


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   18290
52169564  
00016717  00000-0  10270-3 0  9050
2 25544  51
6367 129
0940 0004044 300
6166  59
4588 15
53830449 17536


Satellite: ISS
Catalog Number: 25544
Epoch time:      18290
52169564   =   yrday
fracday
Element set:     905
Inclination:       51
6367  deg
RA of node:       129
0940  deg
Eccentricity:     
0004044     
Arg of perigee:   300
6166  deg
Mean anomaly:      59
4588  deg
Mean motion:   15
53830449  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1753
Checksum:              320


Coasting Arc #7 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2018/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4271207
63                 A    =         6778994
87  meter
 Y    =        -891412
79  meter          E    =           
0000511
 Z    =        5187902
28                 I    =           51
93588
 XDOT =       3150
737649                 Wp   =          132
69173
 YDOT =      -6845
940015  meter/sec      RA   =          123
18227  deg
 ZDOT =       1417
275229                 TA   =          303
72901
                                          MA   =          303
73389
                                          Ha   =            220
766  n
mi
                                          Hp   =            216
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14013148
38                 X    =        -4286122
51
 Y    =       -2924582
63  feet           Y    =         -939259
51  meter
 Z    =       17020676
78                 Z    =         5167117
84
 XDOT =      10337
065778                 XDOT =        3220
172238
 YDOT =     -22460
433121  feet/sec       YDOT =       -6810
317971  meter/sec
 ZDOT =       4649
853112                 ZDOT =        1432
749589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13974937
20                 X    =         4259560
86
 Y    =       -3576741
99  feet           Y    =        -1090190
96  meter
 Z    =       16927285
55                 Z    =         5159436
64
 XDOT =        342
964401                 XDOT =         104
535549
 YDOT =      23685
238226  feet/sec       YDOT =        7219
260611  meter/sec
 ZDOT =       4720
147418                 ZDOT =        1438
700933


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   18291
55072585  
00016717  00000-0  10270-3 0  9061
2 25544  51
6371 123
9662 0004054 304
2835  55
7933 15
53798462 17697


Satellite: ISS
Catalog Number: 25544
Epoch time:      18291
55072585   =   yrday
fracday
Element set:     906
Inclination:       51
6371  deg
RA of node:       123
9662  deg
Eccentricity:     
0004054     
Arg of perigee:   304
2835  deg
Mean anomaly:      55
7933  deg
Mean motion:   15
53798462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1769
Checksum:              332


Coasting Arc #8 (Orbit 1770)
---------------------------------------

Vector Time (GMT): 2018/291/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         490379
71                 A    =         6782851
89  meter
 Y    =        5330664
70  meter          E    =           
0004061
 Z    =       -4169367
13                 I    =           51
95374
 XDOT =      -5691
879636                 Wp   =          100
74067
 YDOT =       3474
630244  meter/sec      RA   =          122
29918  deg
 ZDOT =       3775
348554                 TA   =          207
97415
                                          MA   =          207
99599
                                          Ha   =            220
508  n
mi
                                          Hp   =            216
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1608857
30                 X    =          450987
08
 Y    =       17489057
41  feet           Y    =         5335927
98  meter
 Z    =      -13679026
01                 Z    =        -4167080
98
 XDOT =     -18674
145789                 XDOT =       -5748
649733
 YDOT =      11399
705525  feet/sec       YDOT =        3410
662481  meter/sec
 ZDOT =      12386
314155                 ZDOT =        3747
561010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17546120
74                 X    =        -5348057
60
 Y    =         924964
91  feet           Y    =          281929
30  meter
 Z    =      -13669286
39                 Z    =        -4166398
49
 XDOT =     -10492
732098                 XDOT =       -3198
184744
 YDOT =     -17962
365530  feet/sec       YDOT =       -5474
929014  meter/sec
 ZDOT =      12260
978849                 ZDOT =        3737
146353


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   18291
67935436  
00016717  00000-0  10270-3 0  9078
2 25544  51
6386 123
3227 0003781 299
2799  60
7975 15
53826946 17716


Satellite: ISS
Catalog Number: 25544
Epoch time:      18291
67935436   =   yrday
fracday
Element set:     907
Inclination:       51
6386  deg
RA of node:       123
3227  deg
Eccentricity:     
0003781     
Arg of perigee:   299
2799  deg
Mean anomaly:      60
7975  deg
Mean motion:   15
53826946  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1771
Checksum:              358


Coasting Arc #9 (Orbit 1786)
---------------------------------------

Vector Time (GMT): 2018/292/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         535537
53                 A    =         6786476
86  meter
 Y    =       -6078254
43  meter          E    =           
0010010
 Z    =        2962296
71                 I    =           51
98314
 XDOT =       5444
234179                 Wp   =           88
46326
 YDOT =      -1976
561125  meter/sec      RA   =          117
33961  deg
 ZDOT =      -5025
009333                 TA   =           57
87083
                                          MA   =           57
77373
                                          Ha   =            220
597  n
mi
                                          Hp   =            216
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1757012
89                 X    =          589077
02
 Y    =      -19941779
64  feet           Y    =        -6071966
12  meter
 Z    =        9718821
24                 Z    =         2965028
66
 XDOT =      17861
660693                 XDOT =        5490
341130
 YDOT =      -6484
780594  feet/sec       YDOT =       -1915
422466  meter/sec
 ZDOT =     -16486
251093                 ZDOT =       -4998
450713

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19888064
83                 X    =         6061882
16
 Y    =        2230542
12  feet           Y    =          679869
24  meter
 Z    =        9731737
51                 Z    =         2966233
59
 XDOT =       6160
640769                 XDOT =        1877
763306
 YDOT =      16689
388122  feet/sec       YDOT =        5086
925500  meter/sec
 ZDOT =     -16366
584034                 ZDOT =       -4988
534814


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   18292
70837935  
00016717  00000-0  10270-3 0  9089
2 25544  51
6391 118
1947 0003681 303
5226  56
5575 15
53827417 17876


Satellite: ISS
Catalog Number: 25544
Epoch time:      18292
70837935   =   yrday
fracday
Element set:     908
Inclination:       51
6391  deg
RA of node:       118
1947  deg
Eccentricity:     
0003681     
Arg of perigee:   303
5226  deg
Mean anomaly:      56
5575  deg
Mean motion:   15
53827417  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1787
Checksum:              339


Coasting Arc #10 (Orbit 1801)
---------------------------------------

Vector Time (GMT): 2018/293/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1396921
21                 A    =         6789211
57  meter
 Y    =        6466735
62  meter          E    =           
0009186
 Z    =       -1500004
84                 I    =           52
00672
 XDOT =      -5008
076515                 Wp   =           13
71620
 YDOT =        260
148431  meter/sec      RA   =          112
39019  deg
 ZDOT =       5801
369096                 TA   =          329
98934
                                          MA   =          330
04196
                                          Ha   =            220
739  n
mi
                                          Hp   =            216
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4583074
85                 X    =        -1461843
90
 Y    =       21216324
22  feet           Y    =         6450751
15  meter
 Z    =       -4921275
71                 Z    =        -1506948
91
 XDOT =     -16430
697227                 XDOT =       -5038
793721
 YDOT =        853
505350  feet/sec       YDOT =         203
973371  meter/sec
 ZDOT =      19033
363175                 ZDOT =        5776
966649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21170246
88                 X    =        -6452691
25
 Y    =       -4758412
89  feet           Y    =        -1450364
25  meter
 Z    =       -4953190
59                 Z    =        -1509732
49
 XDOT =      -1039
183561                 XDOT =        -316
743149
 YDOT =     -15020
803910  feet/sec       YDOT =       -4578
341032  meter/sec
 ZDOT =      18923
565362                 ZDOT =        5767
902722


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   18293
67308696  
00016717  00000-0  10270-3 0  9094
2 25544  51
6392 113
3880 0003756 309
6300  50
4521 15
53835882 18020


Satellite: ISS
Catalog Number: 25544
Epoch time:      18293
67308696   =   yrday
fracday
Element set:     909
Inclination:       51
6392  deg
RA of node:       113
3880  deg
Eccentricity:     
0003756     
Arg of perigee:   309
6300  deg
Mean anomaly:      50
4521  deg
Mean motion:   15
53835882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1802
Checksum:              318


Coasting Arc #11 (Orbit 1817)
---------------------------------------

Vector Time (GMT): 2018/294/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2128535
31                 A    =         6790117
46  meter
 Y    =       -6442430
17  meter          E    =           
0008144
 Z    =        -126906
38                 I    =           52
02105
 XDOT =       4446
152964                 Wp   =          137
34869
 YDOT =       1583
415725  meter/sec      RA   =          107
44653  deg
 ZDOT =      -6041
226282                 TA   =           44
01077
                                          MA   =           43
94596
                                          Ha   =            220
751  n
mi
                                          Hp   =            216
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6983383
57                 X    =         2201034
62
 Y    =      -21136581
92  feet           Y    =        -6418222
05  meter
 Z    =        -416359
52                 Z    =         -116389
85
 XDOT =      14587
116023                 XDOT =        4457
461893
 YDOT =       5194
933482  feet/sec       YDOT =        1633
198378  meter/sec
 ZDOT =     -19820
296202                 ZDOT =       -6019
600739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21187583
69                 X    =         6457975
51
 Y    =        6829839
09  feet           Y    =         2081734
95  meter
 Z    =        -368363
44                 Z    =         -112277
18
 XDOT =      -4586
718096                 XDOT =       -1398
031676
 YDOT =      13211
560520  feet/sec       YDOT =        4026
883647  meter/sec
 ZDOT =     -19723
182044                 ZDOT =       -6011
625887


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   18294
70210625  
00016717  00000-0  10270-3 0  9105
2 25544  51
6387 108
2604 0003754 311
6712  48
4119 15
53854833 18183


Satellite: ISS
Catalog Number: 25544
Epoch time:      18294
70210625   =   yrday
fracday
Element set:     910
Inclination:       51
6387  deg
RA of node:       108
2604  deg
Eccentricity:     
0003754     
Arg of perigee:   311
6712  deg
Mean anomaly:      48
4119  deg
Mean motion:   15
53854833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1818
Checksum:              302


Coasting Arc #12 (Orbit 1833)
---------------------------------------

Vector Time (GMT): 2018/295/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2700830
75                 A    =         6788883
58  meter
 Y    =        5977315
18  meter          E    =           
0013347
 Z    =        1720365
15                 I    =           52
02712
 XDOT =      -3826
470692                 Wp   =           48
79951
 YDOT =      -3382
327776  meter/sec      RA   =          102
50265  deg
 ZDOT =       5724
300323                 TA   =          329
97436
                                          MA   =          330
05083
                                          Ha   =            220
944  n
mi
                                          Hp   =            216
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8860993
28                 X    =        -2775826
82
 Y    =       19610614
12  feet           Y    =         5946693
44  meter
 Z    =        5644242
63                 Z    =         1707062
49
 XDOT =     -12554
037705                 XDOT =       -3816
170366
 YDOT =     -11096
875907  feet/sec       YDOT =       -3425
059918  meter/sec
 ZDOT =      18780
512871                 ZDOT =        5705
737606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19823804
21                 X    =        -6042295
52
 Y    =       -8413643
87  feet           Y    =        -2564478
65  meter
 Z    =        5583748
43                 Z    =         1701926
52
 XDOT =      10167
013073                 XDOT =        3098
905585
 YDOT =     -11502
021167  feet/sec       YDOT =       -3505
816052  meter/sec
 ZDOT =      18697
373597                 ZDOT =        5698
959472


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   18295
73112202  
00016717  00000-0  10270-3 0  9112
2 25544  51
6400 103
1326 0003766 317
7986  42
2876 15
53860835 18346


Satellite: ISS
Catalog Number: 25544
Epoch time:      18295
73112202   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:       103
1326  deg
Eccentricity:     
0003766     
Arg of perigee:   317
7986  deg
Mean anomaly:      42
2876  deg
Mean motion:   15
53860835  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1834
Checksum:              302


Coasting Arc #13 (Orbit 1834)
---------------------------------------

Vector Time (GMT): 2018/295/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4045404
40                 A    =         6783083
08  meter
 Y    =       -3575708
44  meter          E    =           
0006786
 Z    =       -4113458
85                 I    =           52
00724
 XDOT =       1722
383309                 Wp   =           39
25375
 YDOT =       6389
705068  meter/sec      RA   =          102
00821  deg
 ZDOT =      -3858
855351                 TA   =          191
00876
                                          MA   =          191
02361
                                          Ha   =            220
912  n
mi
                                          Hp   =            216
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13272324
15                 X    =         4105069
73
 Y    =      -11731326
91  feet           Y    =        -3530136
68  meter
 Z    =      -13495599
91                 Z    =        -4093662
04
 XDOT =       5650
863875                 XDOT =        1669
548508
 YDOT =      20963
599304  feet/sec       YDOT =        6408
670189  meter/sec
 ZDOT =     -12660
286586                 ZDOT =       -3850
617344

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17486299
51                 X    =         5329824
09
 Y    =        3227116
37  feet           Y    =          983625
07  meter
 Z    =      -13406151
04                 Z    =        -4086194
84
 XDOT =     -12673
790128                 XDOT =       -3862
971231
 YDOT =      16208
554865  feet/sec       YDOT =        4940
367523  meter/sec
 ZDOT =     -12623
923130                 ZDOT =       -3847
771770


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   18295
79543513  
00016717  00000-0  10270-3 0  9122
2 25544  51
6389 102
8143 0003942 317
7159  42
3689 15
53846138 18357


Satellite: ISS
Catalog Number: 25544
Epoch time:      18295
79543513   =   yrday
fracday
Element set:     912
Inclination:       51
6389  deg
RA of node:       102
8143  deg
Eccentricity:     
0003942     
Arg of perigee:   317
7159  deg
Mean anomaly:      42
3689  deg
Mean motion:   15
53846138  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1835
Checksum:              333


Coasting Arc #14 (Orbit 1850)
---------------------------------------

Vector Time (GMT): 2018/296/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4148438
58                 A    =         6779802
51  meter
 Y    =        2065914
12  meter          E    =           
0003162
 Z    =        4945940
39                 I    =           52
00269
 XDOT =       -897
705552                 Wp   =           95
01958
 YDOT =      -7267
461099  meter/sec      RA   =           97
04317  deg
 ZDOT =       2281
135923                 TA   =          332
79842
                                          MA   =          332
81498
                                          Ha   =            221
161  n
mi
                                          Hp   =            215
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13610362
79                 X    =        -4195257
25
 Y    =        6777933
46  feet           Y    =         2019262
01  meter
 Z    =       16226838
56                 Z    =         4925674
34
 XDOT =      -2945
228189                 XDOT =        -827
452887
 YDOT =     -23843
376308  feet/sec       YDOT =       -7277
106877  meter/sec
 ZDOT =       7484
041743                 ZDOT =        2276
946289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13928557
80                 X    =        -4245424
42
 Y    =       -6335267
42  feet           Y    =        -1930989
51  meter
 Z    =       16135436
51                 Z    =         4918081
05
 XDOT =      16108
447067                 XDOT =        4909
854666
 YDOT =     -16387
524239  feet/sec       YDOT =       -4994
917388  meter/sec
 ZDOT =       7466
003832                 ZDOT =        2275
637968


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   18296
82444641  
00016717  00000-0  10270-3 0  9130
2 25544  51
6392  97
6862 0004029 322
7160  37
3712 15
53874051 18519


Satellite: ISS
Catalog Number: 25544
Epoch time:      18296
82444641   =   yrday
fracday
Element set:     913
Inclination:       51
6392  deg
RA of node:        97
6862  deg
Eccentricity:     
0004029     
Arg of perigee:   322
7160  deg
Mean anomaly:      37
3712  deg
Mean motion:   15
53874051  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1851
Checksum:              313


Coasting Arc #15 (Orbit 1865)
---------------------------------------

Vector Time (GMT): 2018/297/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4181950
05                 A    =         6778278
21  meter
 Y    =        -398626
13  meter          E    =           
0013236
 Z    =       -5330599
39                 I    =           51
99949
 XDOT =        103
946947                 Wp   =           70
90202
 YDOT =       7642
469001  meter/sec      RA   =           92
07269  deg
 ZDOT =       -486
735740                 TA   =          194
45303
                                          MA   =          194
49092
                                          Ha   =            221
192  n
mi
                                          Hp   =            216
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13720308
55                 X    =         4211990
75
 Y    =       -1307828
50  feet           Y    =         -351693
02  meter
 Z    =      -17488843
16                 Z    =        -5310211
37
 XDOT =        341
033292                 XDOT =          20
843376
 YDOT =      25073
717196  feet/sec       YDOT =        7643
166717  meter/sec
 ZDOT =      -1596
902035                 ZDOT =        -486
433116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9935795
87                 X    =         3028430
58
 Y    =        9717954
39  feet           Y    =         2962032
50  meter
 Z    =      -17397075
62                 Z    =        -5302628
65
 XDOT =     -18206
808951                 XDOT =       -5549
435368
 YDOT =      15737
996882  feet/sec       YDOT =        4796
941450  meter/sec
 ZDOT =      -1596
413738                 ZDOT =        -486
586907


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   18297
78914458  
00016717  00000-0  10270-3 0  9145
2 25544  51
6384  92
8795 0004024 326
7344  33
3555 15
53839316 18667


Satellite: ISS
Catalog Number: 25544
Epoch time:      18297
78914458   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:        92
8795  deg
Eccentricity:     
0004024     
Arg of perigee:   326
7344  deg
Mean anomaly:      33
3555  deg
Mean motion:   15
53839316  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1866
Checksum:              346


Coasting Arc #16 (Orbit 1881)
---------------------------------------

Vector Time (GMT): 2018/298/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4137577
31                 A    =         6778651
39  meter
 Y    =       -1322427
00  meter          E    =           
0006281
 Z    =        5203870
87                 I    =           52
00225
 XDOT =        683
375536                 Wp   =           14
48180
 YDOT =      -7515
769663  meter/sec      RA   =           87
10029  deg
 ZDOT =      -1360
313918                 TA   =           88
56336
                                          MA   =           88
49140
                                          Ha   =            221
323  n
mi
                                          Hp   =            215
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13574728
72                 X    =        -4147760
47
 Y    =       -4338671
25  feet           Y    =        -1368752
98  meter
 Z    =       17073067
15                 Z    =         5183746
67
 XDOT =       2242
045721                 XDOT =         773
976063
 YDOT =     -24658
036951  feet/sec       YDOT =       -7507
621160  meter/sec
 ZDOT =      -4462
972173                 ZDOT =       -1356
773847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5756245
82                 X    =        -1754503
73
 Y    =      -13154504
39  feet           Y    =        -4009492
94  meter
 Z    =       16982685
25                 Z    =         5176322
46
 XDOT =      19086
390814                 XDOT =        5817
531920
 YDOT =     -14118
745676  feet/sec       YDOT =       -4303
393682  meter/sec
 ZDOT =      -4446
164633                 ZDOT =       -1355
190980


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   18298
81814987  
00016717  00000-0  10270-3 0  9157
2 25544  51
6393  87
7518 0004113 330
7561  29
3361 15
53890981 18821


Satellite: ISS
Catalog Number: 25544
Epoch time:      18298
81814987   =   yrday
fracday
Element set:     915
Inclination:       51
6393  deg
RA of node:        87
7518  deg
Eccentricity:     
0004113     
Arg of perigee:   330
7561  deg
Mean anomaly:      29
3361  deg
Mean motion:   15
53890981  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1882
Checksum:              342


Coasting Arc #17 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2018/299/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4035920
98                 A    =         6781182
72  meter
 Y    =        2921547
17  meter          E    =           
0007909
 Z    =       -4606605
25                 I    =           52
00841
 XDOT =      -1471
395669                 Wp   =           86
75209
 YDOT =       6864
259058  meter/sec      RA   =           82
13189  deg
 ZDOT =       3069
222083                 TA   =          213
77301
                                          MA   =          213
82342
                                          Ha   =            221
510  n
mi
                                          Hp   =            215
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13241210
57                 X    =         4025328
60
 Y    =        9585128
50  feet           Y    =         2966620
33  meter
 Z    =      -15113534
29                 Z    =        -4587025
34
 XDOT =      -4827
413611                 XDOT =       -1562
953480
 YDOT =      22520
534967  feet/sec       YDOT =        6847
293017  meter/sec
 ZDOT =      10069
626256                 ZDOT =        3061
851823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1862269
52                 X    =          567619
75
 Y    =       16321173
32  feet           Y    =         4974693
63  meter
 Z    =      -15025795
09                 Z    =        -4579862
34
 XDOT =     -18781
010182                 XDOT =       -5724
451903
 YDOT =      11366
987744  feet/sec       YDOT =        3464
657864  meter/sec
 ZDOT =      10035
641614                 ZDOT =        3058
863564


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   18299
78284123  
00016717  00000-0  10270-3 0  9168
2 25544  51
6399  82
9446 0004183 338
6514  21
4463 15
53875216 18972


Satellite: ISS
Catalog Number: 25544
Epoch time:      18299
78284123   =   yrday
fracday
Element set:     916
Inclination:       51
6399  deg
RA of node:        82
9446  deg
Eccentricity:     
0004183     
Arg of perigee:   338
6514  deg
Mean anomaly:      21
4463  deg
Mean motion:   15
53875216  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1897
Checksum:              344


Coasting Arc #18 (Orbit 1906)
---------------------------------------

Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3396286
82                 A    =         6779512
28  meter
 Y    =       -3066303
49  meter          E    =           
0013009
 Z    =       -5014110
73                 I    =           51
99671
 XDOT =       2977
330594                 Wp   =           56
44719
 YDOT =       6735
992659  meter/sec      RA   =           79
02545  deg
 ZDOT =      -2099
533986                 TA   =          193
17511
                                          MA   =          193
20912
                                          Ha   =            221
478  n
mi
                                          Hp   =            215
543

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11142673
29                 X    =         3454679
27
 Y    =      -10060050
84  feet           Y    =        -3027997
39  meter
 Z    =      -16450494
54                 Z    =        -4997470
43
 XDOT =       9768
144993                 XDOT =        2911
984289
 YDOT =      22099
713447  feet/sec       YDOT =        6768
921851  meter/sec
 ZDOT =      -6888
234863                 ZDOT =       -2085
229482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11060898
31                 X    =        -3371361
80
 Y    =       10270840
83  feet           Y    =         3130552
28  meter
 Z    =      -16375253
24                 Z    =        -4991177
19
 XDOT =      -9478
208347                 XDOT =       -2888
957904
 YDOT =     -21104
388133  feet/sec       YDOT =       -6432
617503  meter/sec
 ZDOT =      -6824
699962                 ZDOT =       -2080
168548


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   18300
42596724  
00016717  00000-0  10270-3 0  9176
2 25544  51
6369  79
7377 0004050 341
1610  18
9392 15
53881952 19073


Satellite: ISS
Catalog Number: 25544
Epoch time:      18300
42596724   =   yrday
fracday
Element set:     917
Inclination:       51
6369  deg
RA of node:        79
7377  deg
Eccentricity:     
0004050     
Arg of perigee:   341
1610  deg
Mean anomaly:      18
9392  deg
Mean motion:   15
53881952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1907
Checksum:              323
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