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

 
Date: June 7th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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


159/13:07:16 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 214 3

164/10:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 214 7

172/07:16:24 783 1 0 1 1 1 1
N/A 0 2 -0 0 220 2
000/00:02:49 566 0 4 0 0 215 8

Coasting Arc #1 (Orbit 3684)
---------------------------------------

Vector Time (GMT): 2018/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907993
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         411434
34                 A    =         6785482
28  meter
 Y    =       -6072012
19  meter          E    =           
0007129
 Z    =       -2999609
47                 I    =           52
00906
 XDOT =       5081
668360                 Wp   =          129
76628
 YDOT =       2809
892868  meter/sec      RA   =           71
23568  deg
 ZDOT =      -5003
259067                 TA   =           84
35567
                                          MA   =           84
27438
                                          Ha   =            221
694  n
mi
                                          Hp   =            214
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1349850
20                 X    =          493873
21
 Y    =      -19921299
82  feet           Y    =        -6066950
02  meter
 Z    =       -9841238
43                 Z    =        -2997411
19
 XDOT =      16672
140288                 XDOT =        5074
172918
 YDOT =       9218
808623  feet/sec       YDOT =        2866
678135  meter/sec
 ZDOT =     -16414
891952                 ZDOT =       -4978
591991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18757476
96                 X    =        -5717278
98
 Y    =       -6859215
48  feet           Y    =        -2090688
88  meter
 Z    =       -9830487
13                 Z    =        -2996332
48
 XDOT =      12991
203812                 XDOT =        3959
718922
 YDOT =     -12216
298285  feet/sec       YDOT =       -3723
527717  meter/sec
 ZDOT =     -16304
898058                 ZDOT =       -4969
732928


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   18157
52607057  
00016717  00000-0  10270-3 0  9001
2 25544  51
6411  71
8659 0003216 157
6093 202
5200 15
54141383 36857


Satellite: ISS
Catalog Number: 25544
Epoch time:      18157
52607057   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:        71
8659  deg
Eccentricity:     
0003216     
Arg of perigee:   157
6093  deg
Mean anomaly:     202
5200  deg
Mean motion:   15
54141383  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3685
Checksum:              292


Coasting Arc #2 (Orbit 3700)
---------------------------------------

Vector Time (GMT): 2018/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907993
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1372159
28                 A    =         6781703
81  meter
 Y    =        5109916
10  meter          E    =           
0012191
 Z    =        4236942
55                 I    =           51
98471
 XDOT =      -5079
221389                 Wp   =          118
47725
 YDOT =      -4420
860079  meter/sec      RA   =           66
27599  deg
 ZDOT =       3673
134294                 TA   =          294
02649
                                          MA   =          294
15404
                                          Ha   =            221
651  n
mi
                                          Hp   =            214
211

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4501834
91                 X    =        -1449778
69
 Y    =       16764816
59  feet           Y    =         5094137
31  meter
 Z    =       13900730
14                 Z    =         4230088
95
 XDOT =     -16664
112167                 XDOT =       -5047
250842
 YDOT =     -14504
134119  feet/sec       YDOT =       -4477
480986  meter/sec
 ZDOT =      12050
965533                 ZDOT =        3648
538372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14999840
39                 X    =         4571951
35
 Y    =        8786571
75  feet           Y    =         2678147
07  meter
 Z    =       13869276
71                 Z    =         4227355
54
 XDOT =     -17710
078652                 XDOT =       -5398
031973
 YDOT =      11313
283086  feet/sec       YDOT =        3448
288685  meter/sec
 ZDOT =      11941
540737                 ZDOT =        3639
781617


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   18158
55489335  
00016717  00000-0  10270-3 0  9013
2 25544  51
6409  66
7373 0003245 162
2935 197
8331 15
54143414 37016


Satellite: ISS
Catalog Number: 25544
Epoch time:      18158
55489335   =   yrday
fracday
Element set:     901
Inclination:       51
6409  deg
RA of node:        66
7373  deg
Eccentricity:     
0003245     
Arg of perigee:   162
2935  deg
Mean anomaly:     197
8331  deg
Mean motion:   15
54143414  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3701
Checksum:              313


Coasting Arc #3 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2018/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907993
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2430796
19                 A    =         6778391
46  meter
 Y    =       -3809916
94  meter          E    =           
0013350
 Z    =       -5063513
88                 I    =           51
96112
 XDOT =       4811
045256                 Wp   =           89
17751
 YDOT =       5635
957829  meter/sec      RA   =           61
30498  deg
 ZDOT =      -1935
252631                 TA   =          162
13255
                                          MA   =          162
08557
                                          Ha   =            221
481  n
mi
                                          Hp   =            214
305

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7975053
11                 X    =         2497815
12
 Y    =      -12499727
48  feet           Y    =        -3782358
94  meter
 Z    =      -16612578
36                 Z    =        -5051543
38
 XDOT =      15784
269213                 XDOT =        4757
065367
 YDOT =      18490
675293  feet/sec       YDOT =        5689
456597  meter/sec
 ZDOT =      -6349
254038                 ZDOT =       -1912
012702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10163841
47                 X    =        -3097938
88
 Y    =      -10878314
64  feet           Y    =        -3315710
30  meter
 Z    =      -16558412
25                 Z    =        -5047004
05
 XDOT =      20986
296755                 XDOT =        6396
623251
 YDOT =     -10121
551389  feet/sec       YDOT =       -3085
048863  meter/sec
 ZDOT =      -6246
096207                 ZDOT =       -1903
810124


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   18159
51940548  
00016717  00000-0  10270-3 0  9029
2 25544  51
6423  61
9291 0003139 166
2584 193
8654 15
54183840 37161


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
51940548   =   yrday
fracday
Element set:     902
Inclination:       51
6423  deg
RA of node:        61
9291  deg
Eccentricity:     
0003139     
Arg of perigee:   166
2584  deg
Mean anomaly:     193
8654  deg
Mean motion:   15
54183840  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              324


Coasting Arc #4 (Orbit 3716)
---------------------------------------

Vector Time (GMT): 2018/159/13:07:16
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4586604
78                 A    =         6786821
99  meter
 Y    =       -4356322
99  meter          E    =           
0015628
 Z    =        2435400
01                 I    =           51
98812
 XDOT =       1980
257388                 Wp   =          116
06959
 YDOT =      -5102
576400  meter/sec      RA   =           61
03807  deg
 ZDOT =      -5377
836949                 TA   =           36
79967
                                          MA   =           36
69250
                                          Ha   =            221
615  n
mi
                                          Hp   =            214
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15047915
96                 X    =        -4549380
27
 Y    =      -14292398
26  feet           Y    =        -4407405
64  meter
 Z    =        7990157
51                 Z    =         2413209
75
 XDOT =       6496
907441                 XDOT =        2063
291502
 YDOT =     -16740
736221  feet/sec       YDOT =       -5079
967066  meter/sec
 ZDOT =     -17643
822011                 ZDOT =       -5368
016233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13534250
78                 X    =        -4125239
64
 Y    =       15783006
38  feet           Y    =         4810660
35  meter
 Z    =        7891502
07                 Z    =         2405329
83
 XDOT =     -15895
341967                 XDOT =       -4844
900232
 YDOT =      -4797
877924  feet/sec       YDOT =       -1462
393191  meter/sec
 ZDOT =     -17599
079378                 ZDOT =       -5364
199394


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   18159
58370677  
00016717  00000-0  10270-3 0  9037
2 25544  51
6423  61
6093 0003221 166
2288 193
8953 15
54147770 37176


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
58370677   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:        61
6093  deg
Eccentricity:     
0003221     
Arg of perigee:   166
2288  deg
Mean anomaly:     193
8953  deg
Mean motion:   15
54147770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3717
Checksum:              327


Coasting Arc #5 (Orbit 3731)
---------------------------------------

Vector Time (GMT): 2018/160/13:07:16
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4263818
30                 A    =         6788884
42  meter
 Y    =        5218278
79  meter          E    =           
0008574
 Z    =        -802069
52                 I    =           51
97854
 XDOT =      -3236
114907                 Wp   =           55
07894
 YDOT =       3554
311786  meter/sec      RA   =           56
08785  deg
 ZDOT =       5970
999036                 TA   =          296
29248
                                          MA   =          296
38054
                                          Ha   =            221
363  n
mi
                                          Hp   =            214
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13988905
20                 X    =         4209045
26
 Y    =       17120337
22  feet           Y    =         5265653
56  meter
 Z    =       -2631461
67                 Z    =         -781489
69
 XDOT =     -10617
174891                 XDOT =       -3304
623941
 YDOT =      11661
127907  feet/sec       YDOT =        3517
739698  meter/sec
 ZDOT =      19589
891851                 ZDOT =        5955
112885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16155376
91                 X    =         4924158
88
 Y    =      -15108652
72  feet           Y    =        -4605117
35  meter
 Z    =       -2540160
54                 Z    =         -774240
93
 XDOT =      11246
799864                 XDOT =        3428
024599
 YDOT =       8772
926956  feet/sec       YDOT =        2673
988136  meter/sec
 ZDOT =      19518
232749                 ZDOT =        5949
157342


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   18160
54821138  
00016717  00000-0  10270-3 0  9049
2 25544  51
6422  56
8006 0003110 172
0513 188
0690 15
54192261 37324


Satellite: ISS
Catalog Number: 25544
Epoch time:      18160
54821138   =   yrday
fracday
Element set:     904
Inclination:       51
6422  deg
RA of node:        56
8006  deg
Eccentricity:     
0003110     
Arg of perigee:   172
0513  deg
Mean anomaly:     188
0690  deg
Mean motion:   15
54192261  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3732
Checksum:              277


Coasting Arc #6 (Orbit 3747)
---------------------------------------

Vector Time (GMT): 2018/161/13:07:16
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3605726
83                 A    =         6788878
77  meter
 Y    =       -5664758
72  meter          E    =           
0012581
 Z    =        -953884
08                 I    =           51
95879
 XDOT =       4477
224600                 Wp   =          149
79963
 YDOT =      -1856
378222  meter/sec      RA   =           51
14092  deg
 ZDOT =      -5944
294464                 TA   =           40
48726
                                          MA   =           40
39372
                                          Ha   =            221
356  n
mi
                                          Hp   =            214
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11829812
44                 X    =        -3537480
44
 Y    =      -18585166
39  feet           Y    =        -5704698
74  meter
 Z    =       -3129540
96                 Z    =         -971234
55
 XDOT =      14689
057088                 XDOT =        4526
524985
 YDOT =      -6090
479731  feet/sec       YDOT =       -1806
034494  meter/sec
 ZDOT =     -19502
278426                 ZDOT =       -5922
425844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17536433
67                 X    =        -5345104
98
 Y    =       13316906
98  feet           Y    =         4058993
25  meter
 Z    =       -3206303
38                 Z    =         -977281
27
 XDOT =      -6334
882638                 XDOT =       -1930
872228
 YDOT =     -12979
720445  feet/sec       YDOT =       -3956
218792  meter/sec
 ZDOT =     -19404
105402                 ZDOT =       -5914
371326


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   18161
57701190  
00016717  00000-0  10270-3 0  9059
2 25544  51
6421  51
6725 0003260 177
7293 182
3875 15
54144025 37481


Satellite: ISS
Catalog Number: 25544
Epoch time:      18161
57701190   =   yrday
fracday
Element set:     905
Inclination:       51
6421  deg
RA of node:        51
6725  deg
Eccentricity:     
0003260     
Arg of perigee:   177
7293  deg
Mean anomaly:     182
3875  deg
Mean motion:   15
54144025  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3748
Checksum:              304


Coasting Arc #7 (Orbit 3763)
---------------------------------------

Vector Time (GMT): 2018/162/13:07:16
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2657277
59                 A    =         6786289
09  meter
 Y    =        5683355
56  meter          E    =           
0013131
 Z    =        2575209
86                 I    =           51
92934
 XDOT =      -5553
518515                 Wp   =           88
95503
 YDOT =        191
285601  meter/sec      RA   =           46
18732  deg
 ZDOT =       5285
363781                 TA   =          299
88321
                                          MA   =          300
01361
                                          Ha   =            221
130  n
mi
                                          Hp   =            214
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8718102
32                 X    =         2581018
07
 Y    =       18646179
67  feet           Y    =         5712644
33  meter
 Z    =        8448851
26                 Z    =         2587933
71
 XDOT =     -18220
205102                 XDOT =       -5580
918628
 YDOT =        627
577430  feet/sec       YDOT =         129
028420  meter/sec
 ZDOT =      17340
432352                 ZDOT =        5258
319818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17682107
00                 X    =         5389506
21
 Y    =      -10491824
09  feet           Y    =        -3197907
98  meter
 Z    =        8504888
66                 Z    =         2592290
06
 XDOT =       1703
025501                 XDOT =         519
082173
 YDOT =      16889
225488  feet/sec       YDOT =        5147
835929  meter/sec
 ZDOT =      17219
360814                 ZDOT =        5248
461176


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   18162
60580283  
00016717  00000-0  10270-3 0  9063
2 25544  51
6423  46
5431 0002966 182
7876 177
3261 15
54195268 37641


Satellite: ISS
Catalog Number: 25544
Epoch time:      18162
60580283   =   yrday
fracday
Element set:     906
Inclination:       51
6423  deg
RA of node:        46
5431  deg
Eccentricity:     
0002966     
Arg of perigee:   182
7876  deg
Mean anomaly:     177
3261  deg
Mean motion:   15
54195268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3764
Checksum:              328


Coasting Arc #8 (Orbit 3778)
---------------------------------------

Vector Time (GMT): 2018/163/13:07:16
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1380226
24                 A    =         6782455
33  meter
 Y    =       -5335926
37  meter          E    =           
0006176
 Z    =       -3957321
58                 I    =           51
89196
 XDOT =       6363
560301                 Wp   =           98
72775
 YDOT =       1352
612875  meter/sec      RA   =           41
22337  deg
 ZDOT =      -4049
588218                 TA   =          129
10873
                                          MA   =          129
05380
                                          Ha   =            221
053  n
mi
                                          Hp   =            214
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4528301
31                 X    =        -1301233
06
 Y    =      -17506320
11  feet           Y    =        -5350918
71  meter
 Z    =      -12983338
53                 Z    =        -3963835
30
 XDOT =      20877
822510                 XDOT =        6367
633058
 YDOT =       4437
706284  feet/sec       YDOT =        1423
797999  meter/sec
 ZDOT =     -13286
050584                 ZDOT =       -4018
665764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16863595
58                 X    =        -5140023
93
 Y    =        6469976
58  feet           Y    =         1972048
86  meter
 Z    =      -13011624
92                 Z    =        -3965943
28
 XDOT =       2412
508431                 XDOT =         735
332570
 YDOT =     -20111
865295  feet/sec       YDOT =       -6130
096542  meter/sec
 ZDOT =     -13147
871980                 ZDOT =       -4007
471380


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   18163
57028776  
00016717  00000-0  10270-3 0  9075
2 25544  51
6412  41
7343 0002983 187
3113 172
7997 15
54199865 37790


Satellite: ISS
Catalog Number: 25544
Epoch time:      18163
57028776   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:        41
7343  deg
Eccentricity:     
0002983     
Arg of perigee:   187
3113  deg
Mean anomaly:     172
7997  deg
Mean motion:   15
54199865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3779
Checksum:              349


Coasting Arc #9 (Orbit 3792)
---------------------------------------

Vector Time (GMT): 2018/164/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3081491
60                 A    =         6777216
01  meter
 Y    =       -2901217
17  meter          E    =           
0014780
 Z    =       -5305810
41                 I    =           51
85238
 XDOT =       5798
802104                 Wp   =          106
67595
 YDOT =       4958
901379  meter/sec      RA   =           36
67746  deg
 ZDOT =        653
657655                 TA   =          169
57046
                                          MA   =          169
53977
                                          Ha   =            220
997  n
mi
                                          Hp   =            214
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10109880
58                 X    =         3139477
83
 Y    =       -9518429
05  feet           Y    =        -2866432
66  meter
 Z    =      -17407514
47                 Z    =        -5290701
13
 XDOT =      19024
941286                 XDOT =        5739
744180
 YDOT =      16269
361480  feet/sec       YDOT =        5023
417250  meter/sec
 ZDOT =       2144
546112                 ZDOT =         681
683895

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4267598
09                 X    =        -1300763
90
 Y    =      -13302783
83  feet           Y    =        -4054688
51  meter
 Z    =      -17339414
23                 Z    =        -5285053
46
 XDOT =      21839
583658                 XDOT =        6656
705099
 YDOT =      -9975
243640  feet/sec       YDOT =       -3040
454261  meter/sec
 ZDOT =       2269
167787                 ZDOT =         691
642342


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   18164
47046994  
00016717  00000-0  10270-3 0  9088
2 25544  51
6421  37
2474 0003002 188
3818 171
7285 15
54231601 37931


Satellite: ISS
Catalog Number: 25544
Epoch time:      18164
47046994   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:        37
2474  deg
Eccentricity:     
0003002     
Arg of perigee:   188
3818  deg
Mean anomaly:     171
7285  deg
Mean motion:   15
54231601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3793
Checksum:              313


Coasting Arc #10 (Orbit 3808)
---------------------------------------

Vector Time (GMT): 2018/165/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4439032
43                 A    =         6779148
40  meter
 Y    =        1714951
79  meter          E    =           
0005701
 Z    =        4823562
73                 I    =           51
83250
 XDOT =      -4854
793127                 Wp   =           82
28497
 YDOT =      -5360
954198  meter/sec      RA   =           31
69313  deg
 ZDOT =      -2558
429896                 TA   =           32
83130
                                          MA   =           32
79589
                                          Ha   =            220
921  n
mi
                                          Hp   =            214
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14563754
68                 X    =        -4481309
96
 Y    =        5626482
25  feet           Y    =         1665074
19  meter
 Z    =       15825337
03                 Z    =         4801897
01
 XDOT =     -15927
798972                 XDOT =       -4782
057115
 YDOT =     -17588
432407  feet/sec       YDOT =       -5414
836672  meter/sec
 ZDOT =      -8393
798873                 ZDOT =       -2581
837198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -874919
89                 X    =         -266675
58
 Y    =       15686409
15  feet           Y    =         4781217
51  meter
 Z    =       15728084
06                 Z    =         4793920
02
 XDOT =     -21403
563632                 XDOT =       -6523
806195
 YDOT =       7337
472536  feet/sec       YDOT =        2236
461629  meter/sec
 ZDOT =      -8497
674691                 ZDOT =       -2590
091246


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   18165
49924108  
00016717  00000-0  10270-3 0  9094
2 25544  51
6425  32
1187 0002962 195
9938 164
1121 15
54272280 38092


Satellite: ISS
Catalog Number: 25544
Epoch time:      18165
49924108   =   yrday
fracday
Element set:     909
Inclination:       51
6425  deg
RA of node:        32
1187  deg
Eccentricity:     
0002962     
Arg of perigee:   195
9938  deg
Mean anomaly:     164
1121  deg
Mean motion:   15
54272280  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3809
Checksum:              320


Coasting Arc #11 (Orbit 3823)
---------------------------------------

Vector Time (GMT): 2018/166/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5567845
96                 A    =         6782899
44  meter
 Y    =        -577442
75  meter          E    =           
0006460
 Z    =       -3838316
89                 I    =           51
81566
 XDOT =       3444
511428                 Wp   =          129
82686
 YDOT =       5415
932924  meter/sec      RA   =           26
71397  deg
 ZDOT =       4182
447183                 TA   =          184
16292
                                          MA   =          184
16829
                                          Ha   =            220
775  n
mi
                                          Hp   =            214
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18267211
15                 X    =         5592533
72
 Y    =       -1894497
20  feet           Y    =         -515040
52  meter
 Z    =      -12592903
17                 Z    =        -3811210
45
 XDOT =      11300
890513                 XDOT =        3363
376928
 YDOT =      17768
808806  feet/sec       YDOT =        5453
997410  meter/sec
 ZDOT =      13721
939576                 ZDOT =        4198
983300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5485791
98                 X    =         1672069
39
 Y    =      -17613331
42  feet           Y    =        -5368543
42  meter
 Z    =      -12471486
51                 Z    =        -3801309
09
 XDOT =      19464
407032                 XDOT =        5932
751263
 YDOT =      -3704
058719  feet/sec       YDOT =       -1128
997098  meter/sec
 ZDOT =      13795
048687                 ZDOT =        4204
730840


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   18166
46371017  
00016717  00000-0  10270-3 0  9109
2 25544  51
6421  27
3095 0002913 199
3652 160
7391 15
54234926 38242


Satellite: ISS
Catalog Number: 25544
Epoch time:      18166
46371017   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        27
3095  deg
Eccentricity:     
0002913     
Arg of perigee:   199
3652  deg
Mean anomaly:     160
7391  deg
Mean motion:   15
54234926  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3824
Checksum:              305


Coasting Arc #12 (Orbit 3839)
---------------------------------------

Vector Time (GMT): 2018/167/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6316355
74                 A    =         6786614
12  meter
 Y    =        -472839
74  meter          E    =           
0013924
 Z    =        2415259
50                 I    =           51
79748
 XDOT =      -1670
093367                 Wp   =          117
77451
 YDOT =      -5217
489194  meter/sec      RA   =           21
74430  deg
 ZDOT =      -5371
752734                 TA   =           35
26379
                                          MA   =           35
17175
                                          Ha   =            220
829  n
mi
                                          Hp   =            214
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20722951
89                 X    =        -6322330
83
 Y    =       -1551311
47  feet           Y    =         -543507
39  meter
 Z    =        7924079
72                 Z    =         2384562
48
 XDOT =      -5479
308948                 XDOT =       -1585
532920
 YDOT =     -17117
746699  feet/sec       YDOT =       -5235
691624  meter/sec
 ZDOT =     -17623
860675                 ZDOT =       -5379
660896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9289097
43                 X    =        -2831316
90
 Y    =       18647177
95  feet           Y    =         5683659
84  meter
 Z    =        7786768
59                 Z    =         2373407
07
 XDOT =     -16516
217628                 XDOT =       -5034
143133
 YDOT =       -829
587367  feet/sec       YDOT =        -252
858229  meter/sec
 ZDOT =     -17658
384768                 ZDOT =       -5382
275677


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   18167
49247177  
00016717  00000-0  10270-3 0  9113
2 25544  51
6414  22
1803 0002839 199
8239 160
2804 15
54241329 38404


Satellite: ISS
Catalog Number: 25544
Epoch time:      18167
49247177   =   yrday
fracday
Element set:     911
Inclination:       51
6414  deg
RA of node:        22
1803  deg
Eccentricity:     
0002839     
Arg of perigee:   199
8239  deg
Mean anomaly:     160
2804  deg
Mean motion:   15
54241329  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3840
Checksum:              311


Coasting Arc #13 (Orbit 3854)
---------------------------------------

Vector Time (GMT): 2018/168/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6602756
53                 A    =         6788724
70  meter
 Y    =        1370759
34  meter          E    =           
0007684
 Z    =        -753965
21                 I    =           51
77374
 XDOT =       -322
147023                 Wp   =           44
56679
 YDOT =       4808
023422  meter/sec      RA   =           16
78055  deg
 ZDOT =       5962
296609                 TA   =          307
30190
                                          MA   =          307
37192
                                          Ha   =            220
598  n
mi
                                          Hp   =            214
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21662587
03                 X    =         6590599
92
 Y    =        4497241
92  feet           Y    =         1444528
05  meter
 Z    =       -2473639
13                 Z    =         -721920
96
 XDOT =      -1056
912804                 XDOT =        -404
849104
 YDOT =      15774
355059  feet/sec       YDOT =        4803
957677  meter/sec
 ZDOT =      19561
340582                 ZDOT =        5960
531572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12040570
90                 X    =         3669966
01
 Y    =      -18579704
00  feet           Y    =        -5663093
78  meter
 Z    =       -2330451
49                 Z    =         -710321
61
 XDOT =      12921
292242                 XDOT =        3938
409875
 YDOT =       5939
563385  feet/sec       YDOT =        1810
378920  meter/sec
 ZDOT =      19552
639586                 ZDOT =        5959
644546


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   18168
45692969  
00016717  00000-0  10270-3 0  9124
2 25544  51
6413  17
3713 0002934 207
2666 152
8334 15
54261314 38550


Satellite: ISS
Catalog Number: 25544
Epoch time:      18168
45692969   =   yrday
fracday
Element set:     912
Inclination:       51
6413  deg
RA of node:        17
3713  deg
Eccentricity:     
0002934     
Arg of perigee:   207
2666  deg
Mean anomaly:     152
8334  deg
Mean motion:   15
54261314  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3855
Checksum:              318


Coasting Arc #14 (Orbit 3870)
---------------------------------------

Vector Time (GMT): 2018/169/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6351083
64                 A    =         6788552
07  meter
 Y    =       -2150596
74  meter          E    =           
0010945
 Z    =       -1019950
21                 I    =           51
74141
 XDOT =       2387
812661                 Wp   =          156
21334
 YDOT =      -4263
083969  meter/sec      RA   =           11
81778  deg
 ZDOT =      -5911
574249                 TA   =           34
82777
                                          MA   =           34
75619
                                          Ha   =            220
490  n
mi
                                          Hp   =            215
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20836888
58                 X    =        -6321608
72
 Y    =       -7055763
60  feet           Y    =        -2221454
01  meter
 Z    =       -3346293
35                 Z    =        -1050729
93
 XDOT =       7834
031041                 XDOT =        2464
021182
 YDOT =     -13986
495960  feet/sec       YDOT =       -4235
954984  meter/sec
 ZDOT =     -19394
928638                 ZDOT =       -5899
790616

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13821178
53                 X    =        -4212695
22
 Y    =       17087901
02  feet           Y    =         5208392
23  meter
 Z    =       -3483685
95                 Z    =        -1061827
48
 XDOT =      -9123
594107                 XDOT =       -2780
871484
 YDOT =     -11302
077362  feet/sec       YDOT =       -3444
873180  meter/sec
 ZDOT =     -19341
483429                 ZDOT =       -5895
284149


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   18169
48567974  
00016717  00000-0  10270-3 0  9136
2 25544  51
6417  12
2415 0003015 212
4174 147
6794 15
54231185 38713


Satellite: ISS
Catalog Number: 25544
Epoch time:      18169
48567974   =   yrday
fracday
Element set:     913
Inclination:       51
6417  deg
RA of node:        12
2415  deg
Eccentricity:     
0003015     
Arg of perigee:   212
4174  deg
Mean anomaly:     147
6794  deg
Mean motion:   15
54231185  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3871
Checksum:              313


Coasting Arc #15 (Orbit 3886)
---------------------------------------

Vector Time (GMT): 2018/170/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5585948
86                 A    =         6785831
58  meter
 Y    =        2782345
90  meter          E    =           
0011493
 Z    =        2654452
11                 I    =           51
69895
 XDOT =      -4295
112161                 Wp   =           87
30166
 YDOT =       3631
207040  meter/sec      RA   =            6
84812  deg
 ZDOT =       5213
387787                 TA   =          302
61710
                                          MA   =          302
72798
                                          Ha   =            220
331  n
mi
                                          Hp   =            215
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18326603
86                 X    =         5541526
92
 Y    =        9128431
44  feet           Y    =         2844563
19  meter
 Z    =        8708832
37                 Z    =         2681478
88
 XDOT =     -14091
575330                 XDOT =       -4360
721774
 YDOT =      11913
408924  feet/sec       YDOT =        3582
808760  meter/sec
 ZDOT =      17104
290639                 ZDOT =        5192
364803

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14642824
95                 X    =         4463133
04
 Y    =      -14236125
20  feet           Y    =        -4339170
96  meter
 Z    =        8829317
49                 Z    =         2691175
97
 XDOT =       5525
976004                 XDOT =        1684
317486
 YDOT =      16271
331628  feet/sec       YDOT =        4959
501880  meter/sec
 ZDOT =      17009
608374                 ZDOT =        5184
528632


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   18170
51442299  
00016717  00000-0  10270-3 0  9145
2 25544  51
6403   7
1114 0002909 217
4865 142
6085 15
54276139 38873


Satellite: ISS
Catalog Number: 25544
Epoch time:      18170
51442299   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:         7
1114  deg
Eccentricity:     
0002909     
Arg of perigee:   217
4865  deg
Mean anomaly:     142
6085  deg
Mean motion:   15
54276139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3887
Checksum:              312


Coasting Arc #16 (Orbit 3901)
---------------------------------------

Vector Time (GMT): 2018/171/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923225
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4331782
51                 A    =         6781956
18  meter
 Y    =       -3326808
88  meter          E    =           
0004844
 Z    =       -4024562
32                 I    =           51
65226
 XDOT =       5893
360583                 Wp   =           89
07196
 YDOT =      -2920
781725  meter/sec      RA   =            1
86776  deg
 ZDOT =      -3932
860825                 TA   =          140
07452
                                          MA   =          140
03888
                                          Ha   =            220
250  n
mi
                                          Hp   =            215
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14211884
88                 X    =        -4274710
17
 Y    =      -10914727
29  feet           Y    =        -3374930
38  meter
 Z    =      -13203944
62                 Z    =        -4045466
20
 XDOT =      19335
172515                 XDOT =        5944
687231
 YDOT =      -9582
617207  feet/sec       YDOT =       -2854
590757  meter/sec
 ZDOT =     -12903
086695                 ZDOT =       -3904
108661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14793189
71                 X    =        -4508964
22
 Y    =        9990305
77  feet           Y    =         3045045
20  meter
 Z    =      -13296932
95                 Z    =        -4052905
16
 XDOT =      -2284
241203                 XDOT =        -696
236719
 YDOT =     -20366
888150  feet/sec       YDOT =       -6207
827508  meter/sec
 ZDOT =     -12773
943955                 ZDOT =       -3893
498118


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   18171
47886654  
00016717  00000-0  10270-3 0  9159
2 25544  51
6395   2
3030 0002968 221
6761 138
4166 15
54269814 39027


Satellite: ISS
Catalog Number: 25544
Epoch time:      18171
47886654   =   yrday
fracday
Element set:     915
Inclination:       51
6395  deg
RA of node:         2
3030  deg
Eccentricity:     
0002968     
Arg of perigee:   221
6761  deg
Mean anomaly:     138
4166  deg
Mean motion:   15
54269814  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3902
Checksum:              320


Coasting Arc #17 (Orbit 3914)
---------------------------------------

Vector Time (GMT): 2018/172/07:17:49
566
Vector Time (MET): N/A
Weight (LBS)     : 923113
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3222782
91                 A    =         6780532
80  meter
 Y    =       -3792617
12  meter          E    =           
0008476
 Z    =       -4613318
80                 I    =           51
62030
 XDOT =       6737
432744                 Wp   =          127
04839
 YDOT =       2086
741611  meter/sec      RA   =          357
59113  deg
 ZDOT =       2989
942263                 TA   =          172
81738
                                          MA   =          172
80523
                                          Ha   =            220
224  n
mi
                                          Hp   =            215
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10573434
74                 X    =         3287362
50
 Y    =      -12442969
54  feet           Y    =        -3756216
23  meter
 Z    =      -15135560
37                 Z    =        -4597507
16
 XDOT =      22104
438136                 XDOT =        6699
073951
 YDOT =       6846
265128  feet/sec       YDOT =        2161
869479  meter/sec
 ZDOT =       9809
521860                 ZDOT =        3022
577347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6299331
02                 X    =         1920036
10
 Y    =      -15136016
45  feet           Y    =        -4613457
81  meter
 Z    =      -15064183
87                 Z    =        -4591563
24
 XDOT =      21972
298048                 XDOT =        6697
156445
 YDOT =       -767
411073  feet/sec       YDOT =        -233
906895  meter/sec
 ZDOT =       9955
200450                 ZDOT =        3034
345097


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   18172
31471444  
00016717  00000-0  10270-3 0  9161
2 25544  51
6424 358
1366 0003246 238
5566 121
5270 15
54084302 39154


Satellite: ISS
Catalog Number: 25544
Epoch time:      18172
31471444   =   yrday
fracday
Element set:     916
Inclination:       51
6424  deg
RA of node:       358
1366  deg
Eccentricity:     
0003246     
Arg of perigee:   238
5566  deg
Mean anomaly:     121
5270  deg
Mean motion:   15
54084302  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3915
Checksum:              299
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