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

 
Date: July 13th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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


196/12:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 215 8

196/17:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 215 9

197/12:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 215 7

199/15:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 215 5

201/19:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 2
000/00:00:00 000 0 0 0 0 215 3

203/18:49:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 215 1

206/03:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 214 8

207/15:56:37 575 -1 2 1 2 1 2
N/A 0 2 0 0 221 8
000/00:03:15 150 -0 4 0 0 215 4

Coasting Arc #1 (Orbit 259)
---------------------------------------

Vector Time (GMT): 2018/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959643
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3063702
65                 A    =         6789798
53  meter
 Y    =       -6029537
91  meter          E    =           
0011391
 Z    =        -515645
36                 I    =           51
30690
 XDOT =       4082
996155                 Wp   =           21
03151
 YDOT =      -2579
774250  meter/sec      RA   =          246
56519  deg
 ZDOT =       5958
140715                 TA   =          333
37899
                                          MA   =          333
43744
                                          Ha   =            220
473  n
mi
                                          Hp   =            216
121

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10051517
87                 X    =        -2993546
31
 Y    =      -19781948
51  feet           Y    =        -6063406
00  meter
 Z    =       -1691749
88                 Z    =         -530358
01
 XDOT =      13395
656675                 XDOT =        4082
599490
 YDOT =      -8463
826278  feet/sec       YDOT =       -2534
118491  meter/sec
 ZDOT =      19547
705757                 ZDOT =        5977
972770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15029213
26                 X    =        -4580904
20
 Y    =       16317380
18  feet           Y    =         4973537
48  meter
 Z    =       -1756806
45                 Z    =         -535474
61
 XDOT =     -11372
965989                 XDOT =       -3466
480034
 YDOT =      -8378
442145  feet/sec       YDOT =       -2553
749166  meter/sec
 ZDOT =      19636
790984                 ZDOT =        5985
293892


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   18194
50103487  
00016717  00000-0  10270-3 0  9008
2 25544  51
6380 247
5599 0003986 307
3687  52
7102 15
53925203  2606


Satellite: ISS
Catalog Number: 25544
Epoch time:      18194
50103487   =   yrday
fracday
Element set:     900
Inclination:       51
6380  deg
RA of node:       247
5599  deg
Eccentricity:     
0003986     
Arg of perigee:   307
3687  deg
Mean anomaly:      52
7102  deg
Mean motion:   15
53925203  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             260
Checksum:              308


Coasting Arc #2 (Orbit 275)
---------------------------------------

Vector Time (GMT): 2018/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959643
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2341847
59                 A    =         6789198
85  meter
 Y    =        6264446
58  meter          E    =           
0005592
 Z    =       -1152497
80                 I    =           51
32014
 XDOT =      -4904
910798                 Wp   =          149
10864
 YDOT =        762
171319  meter/sec      RA   =          241
57284  deg
 ZDOT =      -5841
202501                 TA   =           43
45602
                                          MA   =           43
41196
                                          Ha   =            220
555  n
mi
                                          Hp   =            215
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7683227
01                 X    =         2277220
88
 Y    =       20552646
25  feet           Y    =         6290273
53  meter
 Z    =       -3781160
77                 Z    =        -1141278
35
 XDOT =     -16092
227026                 XDOT =       -4884
696226
 YDOT =       2500
562069  feet/sec       YDOT =         707
434986  meter/sec
 ZDOT =     -19164
050199                 ZDOT =       -5864
979132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16315310
04                 X    =         4972906
50
 Y    =      -14684181
11  feet           Y    =        -4475738
40  meter
 Z    =       -3731742
92                 Z    =        -1137435
24
 XDOT =       7088
307766                 XDOT =        2160
516207
 YDOT =      12758
316515  feet/sec       YDOT =        3888
734874  meter/sec
 ZDOT =     -19270
561294                 ZDOT =       -5873
667082


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   18195
52997410  
00016717  00000-0  10270-3 0  9019
2 25544  51
6386 242
4313 0003867 311
8306  48
2516 15
53983566  2768


Satellite: ISS
Catalog Number: 25544
Epoch time:      18195
52997410   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:       242
4313  deg
Eccentricity:     
0003867     
Arg of perigee:   311
8306  deg
Mean anomaly:      48
2516  deg
Mean motion:   15
53983566  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             276
Checksum:              321


Coasting Arc #3 (Orbit 291)
---------------------------------------

Vector Time (GMT): 2018/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959643
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1422196
59                 A    =         6786806
20  meter
 Y    =       -6059841
76  meter          E    =           
0012096
 Z    =        2687289
77                 I    =           51
32772
 XDOT =       5593
274297                 Wp   =           62
11958
 YDOT =        980
202191  meter/sec      RA   =          236
57761  deg
 ZDOT =       5158
232181                 TA   =          328
39018
                                          MA   =          328
46277
                                          Ha   =            220
760  n
mi
                                          Hp   =            215
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4665999
31                 X    =        -1367381
21
 Y    =      -19881370
60  feet           Y    =        -6075439
51  meter
 Z    =        8816567
48                 Z    =         2680513
93
 XDOT =      18350
637458                 XDOT =        5556
842316
 YDOT =       3215
886452  feet/sec       YDOT =        1042
545839  meter/sec
 ZDOT =      16923
333927                 ZDOT =        5185
313353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16577133
31                 X    =        -5052710
23
 Y    =       11948211
63  feet           Y    =         3641814
91  meter
 Z    =        8786990
29                 Z    =         2678274
64
 XDOT =      -3108
967406                 XDOT =        -947
613265
 YDOT =     -16877
971333  feet/sec       YDOT =       -5144
405662  meter/sec
 ZDOT =      17044
428736                 ZDOT =        5195
141879


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   18196
55891191  
00016717  00000-0  10270-3 0  9023
2 25544  51
6379 237
3029 0003881 318
5652  41
5206 15
53950708  2923


Satellite: ISS
Catalog Number: 25544
Epoch time:      18196
55891191   =   yrday
fracday
Element set:     902
Inclination:       51
6379  deg
RA of node:       237
3029  deg
Eccentricity:     
0003881     
Arg of perigee:   318
5652  deg
Mean anomaly:      41
5206  deg
Mean motion:   15
53950708  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             292
Checksum:              320


Coasting Arc #4 (Orbit 291)
---------------------------------------

Vector Time (GMT): 2018/196/12:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4463948
26                 A    =         6789086
73  meter
 Y    =        4962137
68  meter          E    =           
0010042
 Z    =        1218196
95                 I    =           51
33671
 XDOT =      -2904
786852                 Wp   =          115
51245
 YDOT =       4051
448710  meter/sec      RA   =          236
42227  deg
 ZDOT =      -5825
286196                 TA   =           51
19375
                                          MA   =           51
10412
                                          Ha   =            220
682  n
mi
                                          Hp   =            215
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14645499
53                 X    =         4402211
28
 Y    =       16279979
26  feet           Y    =         5011711
32  meter
 Z    =        3996709
17                 Z    =         1239731
30
 XDOT =      -9530
140592                 XDOT =       -2921
579867
 YDOT =      13292
154560  feet/sec       YDOT =        4018
872045  meter/sec
 ZDOT =     -19111
831351                 ZDOT =       -5839
436714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6356722
53                 X    =         1937529
03
 Y    =      -20936707
67  feet           Y    =        -6381508
50  meter
 Z    =        4092482
89                 Z    =         1247388
78
 XDOT =      14712
482856                 XDOT =        4484
364774
 YDOT =        697
777444  feet/sec       YDOT =         212
682565  meter/sec
 ZDOT =     -19175
672004                 ZDOT =       -5844
744827


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   18196
55891067  
00016717  00000-0  10270-3 0  9036
2 25544  51
6383 237
3033 0003907 317
1089  42
9758 15
53985161  2929


Satellite: ISS
Catalog Number: 25544
Epoch time:      18196
55891067   =   yrday
fracday
Element set:     903
Inclination:       51
6383  deg
RA of node:       237
3033  deg
Eccentricity:     
0003907     
Arg of perigee:   317
1089  deg
Mean anomaly:      42
9758  deg
Mean motion:   15
53985161  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             292
Checksum:              329


Coasting Arc #5 (Orbit 294)
---------------------------------------

Vector Time (GMT): 2018/196/17:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4852092
03                 A    =         6780197
69  meter
 Y    =         385456
25  meter          E    =           
0007749
 Z    =        4719544
31                 I    =           51
30795
 XDOT =       2091
948303                 Wp   =           31
36188
 YDOT =       6864
020780  meter/sec      RA   =          235
49218  deg
 ZDOT =      -2702
792057                 TA   =           85
52889
                                          MA   =           85
44037
                                          Ha   =            220
624  n
mi
                                          Hp   =            215
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15918937
11                 X    =         4824496
61
 Y    =        1264620
25  feet           Y    =          439560
97  meter
 Z    =       15484069
24                 Z    =         4743046
56
 XDOT =       6863
347450                 XDOT =        2028
165894
 YDOT =      22519
753215  feet/sec       YDOT =        6887
058008  meter/sec
 ZDOT =      -8867
428007                 ZDOT =       -2692
784614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15844062
43                 X    =        -4829270
23
 Y    =         842675
03  feet           Y    =          256847
35  meter
 Z    =       15589220
89                 Z    =         4751594
53
 XDOT =      -9785
684350                 XDOT =       -2982
676590
 YDOT =     -20246
881665  feet/sec       YDOT =       -6171
249532  meter/sec
 ZDOT =      -8823
480654                 ZDOT =       -2689
396903


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   18196
75183685  
00016717  00000-0  10270-3 0  9049
2 25544  51
6360 236
3419 0004123 318
1034  41
9803 15
53975765  2955


Satellite: ISS
Catalog Number: 25544
Epoch time:      18196
75183685   =   yrday
fracday
Element set:     904
Inclination:       51
6360  deg
RA of node:       236
3419  deg
Eccentricity:     
0004123     
Arg of perigee:   318
1034  deg
Mean anomaly:      41
9803  deg
Mean motion:   15
53975765  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             295
Checksum:              318


Coasting Arc #6 (Orbit 307)
---------------------------------------

Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -786352
67                 A    =         6784208
23  meter
 Y    =       -5661265
44  meter          E    =           
0009821
 Z    =        3644450
44                 I    =           51
33812
 XDOT =       6011
378694                 Wp   =           77
24046
 YDOT =       1965
115414  meter/sec      RA   =          231
41889  deg
 ZDOT =       4341
881048                 TA   =          326
27334
                                          MA   =          326
33578
                                          Ha   =            220
874  n
mi
                                          Hp   =            215
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2579897
22                 X    =         -740690
85
 Y    =      -18573705
51  feet           Y    =        -5669803
93  meter
 Z    =       11956858
41                 Z    =         3640741
19
 XDOT =      19722
371042                 XDOT =        5967
867336
 YDOT =       6447
229048  feet/sec       YDOT =        2032
095203  meter/sec
 ZDOT =      14245
016561                 ZDOT =        4370
976088

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13759804
77                 X    =        -4193988
49
 Y    =       12754865
32  feet           Y    =         3887682
95  meter
 Z    =       11940940
17                 Z    =         3639598
57
 XDOT =      -4935
533984                 XDOT =       -1504
350758
 YDOT =     -18806
018218  feet/sec       YDOT =       -5732
074353  meter/sec
 ZDOT =      14375
021154                 ZDOT =        4381
506448


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   18197
58784794  
00016717  00000-0  10270-3 0  9050
2 25544  51
6372 232
1747 0003841 323
5337  36
5554 15
53956749  3087


Satellite: ISS
Catalog Number: 25544
Epoch time:      18197
58784794   =   yrday
fracday
Element set:     905
Inclination:       51
6372  deg
RA of node:       232
1747  deg
Eccentricity:     
0003841     
Arg of perigee:   323
5337  deg
Mean anomaly:      36
5554  deg
Mean motion:   15
53956749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             308
Checksum:              341


Coasting Arc #7 (Orbit 322)
---------------------------------------

Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -475575
88                 A    =         6780551
26  meter
 Y    =        4909046
25  meter          E    =           
0010166
 Z    =       -4662857
22                 I    =           51
34882
 XDOT =      -6293
444653                 Wp   =           49
01472
 YDOT =      -3313
006592  meter/sec      RA   =          226
41133  deg
 ZDOT =      -2843
570104                 TA   =          192
58940
                                          MA   =          192
61481
                                          Ha   =            220
882  n
mi
                                          Hp   =            215
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1560288
34                 X    =         -507785
55
 Y    =       16105794
78  feet           Y    =         4903548
20  meter
 Z    =      -15298087
98                 Z    =        -4665245
31
 XDOT =     -20647
784295                 XDOT =       -6242
117644
 YDOT =     -10869
444199  feet/sec       YDOT =       -3383
097088  meter/sec
 ZDOT =      -9329
298241                 ZDOT =       -2874
016463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13934242
54                 X    =         4247157
13
 Y    =       -8205055
17  feet           Y    =        -2500900
82  meter
 Z    =      -15309362
35                 Z    =        -4666293
64
 XDOT =       2573
403548                 XDOT =         784
373401
 YDOT =      22046
024064  feet/sec       YDOT =        6719
628135  meter/sec
 ZDOT =      -9465
208015                 ZDOT =       -2884
995403


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   18198
55247318  
00016717  00000-0  10270-3 0  9065
2 25544  51
6385 227
3676 0003921 324
0961  35
9927 15
53978992  3234


Satellite: ISS
Catalog Number: 25544
Epoch time:      18198
55247318   =   yrday
fracday
Element set:     906
Inclination:       51
6385  deg
RA of node:       227
3676  deg
Eccentricity:     
0003921     
Arg of perigee:   324
0961  deg
Mean anomaly:      35
9927  deg
Mean motion:   15
53978992  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             323
Checksum:              343


Coasting Arc #8 (Orbit 338)
---------------------------------------

Vector Time (GMT): 2018/199/12:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1844015
70                 A    =         6778178
98  meter
 Y    =       -3924418
95  meter          E    =           
0001802
 Z    =        5208558
31                 I    =           51
36392
 XDOT =       6227
141808                 Wp   =           42
40242
 YDOT =       4347
097063  meter/sec      RA   =          221
39574  deg
 ZDOT =       1071
804844                 TA   =           37
29793
                                          MA   =           37
28542
                                          Ha   =            220
941  n
mi
                                          Hp   =            215
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6049920
27                 X    =         1862462
50
 Y    =      -12875390
27  feet           Y    =        -3903695
03  meter
 Z    =       17088445
91                 Z    =         5217560
38
 XDOT =      20430
255274                 XDOT =        6172
862369
 YDOT =      14262
129473  feet/sec       YDOT =        4416
429713  meter/sec
 ZDOT =       3516
420091                 ZDOT =        1101
922117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13872275
99                 X    =        -4228269
72
 Y    =        2922730
49  feet           Y    =          890848
25  meter
 Z    =       17129208
93                 Z    =         5220982
88
 XDOT =       -526
512571                 XDOT =        -160
481032
 YDOT =     -23874
032114  feet/sec       YDOT =       -7276
804988  meter/sec
 ZDOT =       3650
753588                 ZDOT =        1112
749693


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   18199
58140543  
00016717  00000-0  10270-3 0  9072
2 25544  51
6378 222
2385 0003988 330
0797  30
0127 15
53983307  3395


Satellite: ISS
Catalog Number: 25544
Epoch time:      18199
58140543   =   yrday
fracday
Element set:     907
Inclination:       51
6378  deg
RA of node:       222
2385  deg
Eccentricity:     
0003988     
Arg of perigee:   330
0797  deg
Mean anomaly:      30
0127  deg
Mean motion:   15
53983307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             339
Checksum:              321


Coasting Arc #9 (Orbit 339)
---------------------------------------

Vector Time (GMT): 2018/199/15:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5105991
18                 A    =         6781273
50  meter
 Y    =         294980
63  meter          E    =           
0006846
 Z    =       -4458612
22                 I    =           51
37535
 XDOT =      -3181
580001                 Wp   =           87
95640
 YDOT =      -6172
127159  meter/sec      RA   =          220
84287  deg
 ZDOT =       3239
747788                 TA   =          214
78598
                                          MA   =          214
83076
                                          Ha   =            221
020  n
mi
                                          Hp   =            215
460

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16751939
55                 X    =        -5087252
95
 Y    =         967784
23  feet           Y    =          237986
92  meter
 Z    =      -14627992
84                 Z    =        -4483369
49
 XDOT =     -10438
254595                 XDOT =       -3128
061889
 YDOT =     -20249
761020  feet/sec       YDOT =       -6207
406715  meter/sec
 ZDOT =      10629
093794                 ZDOT =        3224
422644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16291966
09                 X    =         4965791
26
 Y    =        3588836
72  feet           Y    =         1093877
43  meter
 Z    =      -14738872
12                 Z    =        -4492408
22
 XDOT =       4881
423790                 XDOT =        1487
857971
 YDOT =      21152
670527  feet/sec       YDOT =        6447
333976  meter/sec
 ZDOT =      10561
199494                 ZDOT =        3219
053606


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   18199
64571456  
00016717  00000-0  10270-3 0  9081
2 25544  51
6364 221
9186 0004172 330
0993  29
9921 15
53958745  3408


Satellite: ISS
Catalog Number: 25544
Epoch time:      18199
64571456   =   yrday
fracday
Element set:     908
Inclination:       51
6364  deg
RA of node:       221
9186  deg
Eccentricity:     
0004172     
Arg of perigee:   330
0993  deg
Mean anomaly:      29
9921  deg
Mean motion:   15
53958745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             340
Checksum:              333


Coasting Arc #10 (Orbit 355)
---------------------------------------

Vector Time (GMT): 2018/200/15:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5830815
17                 A    =         6784913
91  meter
 Y    =         925756
69  meter          E    =           
0011195
 Z    =        3338254
01                 I    =           51
41301
 XDOT =       1745
597780                 Wp   =           71
17405
 YDOT =       5839
889272  meter/sec      RA   =          215
84045  deg
 ZDOT =      -4652
120517                 TA   =           69
79895
                                          MA   =           69
67860
                                          Ha   =            221
098  n
mi
                                          Hp   =            215
435

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19129971
04                 X    =         5803814
44
 Y    =        3037259
48  feet           Y    =          990809
73  meter
 Z    =       10952276
95                 Z    =         3366512
28
 XDOT =       5727
026837                 XDOT =        1702
762113
 YDOT =      19159
741707  feet/sec       YDOT =        5859
170511  meter/sec
 ZDOT =     -15262
862588                 ZDOT =       -4643
744797

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17654159
68                 X    =        -5380987
87
 Y    =       -7792696
55  feet           Y    =        -2375213
91  meter
 Z    =       11078701
81                 Z    =         3376788
31
 XDOT =      -1323
400497                 XDOT =        -403
372472
 YDOT =     -18723
815485  feet/sec       YDOT =       -5707
018960  meter/sec
 ZDOT =     -15226
032116                 ZDOT =       -4640
894589


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   18200
67464610  
00016717  00000-0  10270-3 0  9091
2 25544  51
6360 216
7903 0004272 333
4686  26
6247 15
53985256  3569


Satellite: ISS
Catalog Number: 25544
Epoch time:      18200
67464610   =   yrday
fracday
Element set:     909
Inclination:       51
6360  deg
RA of node:       216
7903  deg
Eccentricity:     
0004272     
Arg of perigee:   333
4686  deg
Mean anomaly:      26
6247  deg
Mean motion:   15
53985256  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             356
Checksum:              314


Coasting Arc #11 (Orbit 370)
---------------------------------------

Vector Time (GMT): 2018/201/15:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6213173
88                 A    =         6788146
62  meter
 Y    =       -1935647
66  meter          E    =           
0009586
 Z    =       -1912923
80                 I    =           51
45138
 XDOT =        -84
172840                 Wp   =           17
09725
 YDOT =      -5243
493812  meter/sec      RA   =          210
84974  deg
 ZDOT =       5595
294420                 TA   =          321
76585
                                          MA   =          321
83379
                                          Ha   =            221
169  n
mi
                                          Hp   =            215
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20384428
74                 X    =        -6181775
26
 Y    =       -6350550
07  feet           Y    =        -2004951
97  meter
 Z    =       -6275996
73                 Z    =        -1943028
88
 XDOT =       -276
157613                 XDOT =         -52
711166
 YDOT =     -17203
063687  feet/sec       YDOT =       -5244
259558  meter/sec
 ZDOT =      18357
265159                 ZDOT =        5594
961599

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18245331
29                 X    =         5561176
98
 Y    =       11011574
17  feet           Y    =         3356327
81  meter
 Z    =       -6410590
98                 Z    =        -1953948
13
 XDOT =      -2905
932546                 XDOT =        -885
728240
 YDOT =      15471
266866  feet/sec       YDOT =        4715
642141  meter/sec
 ZDOT =      18356
373799                 ZDOT =        5595
022734


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   18201
63926863  
00016717  00000-0  10270-3 0  9103
2 25544  51
6363 211
9829 0004215 337
1207  22
9757 15
53977442  3713


Satellite: ISS
Catalog Number: 25544
Epoch time:      18201
63926863   =   yrday
fracday
Element set:     910
Inclination:       51
6363  deg
RA of node:       211
9829  deg
Eccentricity:     
0004215     
Arg of perigee:   337
1207  deg
Mean anomaly:      22
9757  deg
Mean motion:   15
53977442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             371
Checksum:              310


Coasting Arc #12 (Orbit 373)
---------------------------------------

Vector Time (GMT): 2018/201/19:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1675810
71                 A    =         6777798
25  meter
 Y    =        3905409
30  meter          E    =           
0013884
 Z    =       -5291556
43                 I    =           51
42563
 XDOT =      -6791
104009                 Wp   =           69
60651
 YDOT =      -3513
106866  meter/sec      RA   =          209
97353  deg
 ZDOT =       -438
318543                 TA   =          196
17313
                                          MA   =          196
21749
                                          Ha   =            221
204  n
mi
                                          Hp   =            215
286

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5498066
63                 X    =        -1693654
13
 Y    =       12813022
64  feet           Y    =         3886569
83  meter
 Z    =      -17360749
44                 Z    =        -5299739
94
 XDOT =     -22280
524964                 XDOT =       -6749
185650
 YDOT =     -11525
941160  feet/sec       YDOT =       -3588
815270  meter/sec
 ZDOT =      -1438
052963                 ZDOT =        -471
205557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6601912
16                 X    =        -2012262
83
 Y    =      -12228152
88  feet           Y    =        -3727141
00  meter
 Z    =      -17397842
97                 Z    =        -5302862
54
 XDOT =      22053
931454                 XDOT =        6722
038307
 YDOT =      -9634
089899  feet/sec       YDOT =       -2936
470601  meter/sec
 ZDOT =      -1584
928483                 ZDOT =        -483
086202


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   18201
83219273  
00016717  00000-0  10270-3 0  9116
2 25544  51
6399 211
0227 0004331 336
3398  23
7554 15
54003758  3744


Satellite: ISS
Catalog Number: 25544
Epoch time:      18201
83219273   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       211
0227  deg
Eccentricity:     
0004331     
Arg of perigee:   336
3398  deg
Mean anomaly:      23
7554  deg
Mean motion:   15
54003758  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             374
Checksum:              294


Coasting Arc #13 (Orbit 389)
---------------------------------------

Vector Time (GMT): 2018/202/19:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3213459
67                 A    =         6778288
40  meter
 Y    =       -3024800
12  meter          E    =           
0007031
 Z    =        5144417
32                 I    =           51
45699
 XDOT =       6262
318274                 Wp   =           17
86185
 YDOT =       4184
283377  meter/sec      RA   =          204
96132  deg
 ZDOT =      -1444
405439                 TA   =           86
11269
                                          MA   =           86
03231
                                          Ha   =            221
159  n
mi
                                          Hp   =            215
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10542846
68                 X    =         3222056
30
 Y    =       -9923884
91  feet           Y    =        -2988817
36  meter
 Z    =       16878009
56                 Z    =         5160047
70
 XDOT =      20545
663630                 XDOT =        6222
079147
 YDOT =      13727
963834  feet/sec       YDOT =        4254
088074  meter/sec
 ZDOT =      -4738
862989                 ZDOT =       -1414
082870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1432224
56                 X    =          436542
05
 Y    =       14324950
56  feet           Y    =         4366244
93  meter
 Z    =       16948358
01                 Z    =         5165859
52
 XDOT =     -22422
185323                 XDOT =       -6834
282087
 YDOT =       7715
790870  feet/sec       YDOT =        2351
773057  meter/sec
 ZDOT =      -4603
528238                 ZDOT =       -1403
155407


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   18202
86111918  
00016717  00000-0  10270-3 0  9128
2 25544  51
6401 205
8943 0004428 339
3897  20
7077 15
54030722  3904


Satellite: ISS
Catalog Number: 25544
Epoch time:      18202
86111918   =   yrday
fracday
Element set:     912
Inclination:       51
6401  deg
RA of node:       205
8943  deg
Eccentricity:     
0004428     
Arg of perigee:   339
3897  deg
Mean anomaly:      20
7077  deg
Mean motion:   15
54030722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             390
Checksum:              296


Coasting Arc #14 (Orbit 404)
---------------------------------------

Vector Time (GMT): 2018/203/18:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5001728
22                 A    =         6781992
00  meter
 Y    =       -1751496
47  meter          E    =           
0011038
 Z    =        4229337
63                 I    =           51
49743
 XDOT =       4754
333925                 Wp   =           50
23530
 YDOT =       4806
581157  meter/sec      RA   =          200
11069  deg
 ZDOT =      -3618
838735                 TA   =           76
91370
                                          MA   =           76
79052
                                          Ha   =            221
381  n
mi
                                          Hp   =            215
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16409869
50                 X    =         5000398
49
 Y    =       -5746379
50  feet           Y    =        -1695571
53  meter
 Z    =       13875779
63                 Z    =         4253630
69
 XDOT =      15598
208416                 XDOT =        4717
810322
 YDOT =      15769
623220  feet/sec       YDOT =        4859
543534  meter/sec
 ZDOT =     -11872
830496                 ZDOT =       -3595
832267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8323117
02                 X    =        -2536886
07
 Y    =       15165525
64  feet           Y    =         4622452
21  meter
 Z    =       13984795
67                 Z    =         4262565
72
 XDOT =     -21092
023809                 XDOT =       -6428
848857
 YDOT =       -682
096947  feet/sec       YDOT =        -207
903149  meter/sec
 ZDOT =     -11770
316986                 ZDOT =       -3587
592617


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   18203
82573981  
00016717  00000-0  10270-3 0  9138
2 25544  51
6389 201
0869 0004422 345
6267  14
4759 15
54002293  4055


Satellite: ISS
Catalog Number: 25544
Epoch time:      18203
82573981   =   yrday
fracday
Element set:     913
Inclination:       51
6389  deg
RA of node:       201
0869  deg
Eccentricity:     
0004422     
Arg of perigee:   345
6267  deg
Mean anomaly:      14
4759  deg
Mean motion:   15
54002293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             405
Checksum:              307


Coasting Arc #15 (Orbit 419)
---------------------------------------

Vector Time (GMT): 2018/204/18:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5998178
78                 A    =         6785671
98  meter
 Y    =         883399
51  meter          E    =           
0006507
 Z    =       -3043438
65                 I    =           51
54150
 XDOT =      -3216
840838                 Wp   =           31
17363
 YDOT =      -4918
849515  meter/sec      RA   =          195
11868  deg
 ZDOT =       4922
332499                 TA   =          293
87247
                                          MA   =          293
94064
                                          Ha   =            221
424  n
mi
                                          Hp   =            215
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19679064
24                 X    =        -5992828
14
 Y    =        2898292
36  feet           Y    =          816353
97  meter
 Z    =       -9985034
93                 Z    =        -3072562
33
 XDOT =     -10553
939756                 XDOT =       -3185
507665
 YDOT =     -16137
957727  feet/sec       YDOT =       -4954
647776  meter/sec
 ZDOT =      16149
384839                 ZDOT =        4906
781948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12413432
44                 X    =         3783614
21
 Y    =      -15457933
69  feet           Y    =        -4711578
19  meter
 Z    =      -10115610
31                 Z    =        -3083238
02
 XDOT =      17661
317704                 XDOT =        5383
169636
 YDOT =       3681
531799  feet/sec       YDOT =        1122
130892  meter/sec
 ZDOT =      16080
268785                 ZDOT =        4901
265926


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   18204
79035758  
00016717  00000-0  10270-3 0  9141
2 25544  51
6393 196
2790 0004445 346
8776  13
2260 15
53998878  4204


Satellite: ISS
Catalog Number: 25544
Epoch time:      18204
79035758   =   yrday
fracday
Element set:     914
Inclination:       51
6393  deg
RA of node:       196
2790  deg
Eccentricity:     
0004445     
Arg of perigee:   346
8776  deg
Mean anomaly:      13
2260  deg
Mean motion:   15
53998878  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             420
Checksum:              339


Coasting Arc #16 (Orbit 435)
---------------------------------------

Vector Time (GMT): 2018/205/18:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6611482
33                 A    =         6788748
09  meter
 Y    =         -45592
17  meter          E    =           
0011922
 Z    =        1524132
49                 I    =           51
58380
 XDOT =       1368
223614                 Wp   =          100
55442
 YDOT =       4879
503085  meter/sec      RA   =          190
13874  deg
 ZDOT =      -5753
042690                 TA   =           62
78533
                                          MA   =           62
66390
                                          Ha   =            221
645  n
mi
                                          Hp   =            214
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21691215
00                 X    =         6604097
45
 Y    =        -149580
60  feet           Y    =           28300
54  meter
 Z    =        5000434
69                 Z    =         1556230
41
 XDOT =       4488
922618                 XDOT =        1341
502844
 YDOT =      16008
868389  feet/sec       YDOT =        4894
654731  meter/sec
 ZDOT =     -18874
811976                 ZDOT =       -5746
460788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15524212
62                 X    =        -4731780
01
 Y    =       15102016
63  feet           Y    =         4603094
67  meter
 Z    =        5144263
38                 Z    =         1567971
48
 XDOT =     -13310
667911                 XDOT =       -4057
091579
 YDOT =      -7223
952126  feet/sec       YDOT =       -2201
860608  meter/sec
 ZDOT =     -18845
864127                 ZDOT =       -5744
219386


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   18205
81928206  
00016717  00000-0  10270-3 0  9155
2 25544  51
6395 191
1509 0004348 352
0047   8
1035 15
53970324  4366


Satellite: ISS
Catalog Number: 25544
Epoch time:      18205
81928206   =   yrday
fracday
Element set:     915
Inclination:       51
6395  deg
RA of node:       191
1509  deg
Eccentricity:     
0004348     
Arg of perigee:   352
0047  deg
Mean anomaly:       8
1035  deg
Mean motion:   15
53970324  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             436
Checksum:              295


Coasting Arc #17 (Orbit 440)
---------------------------------------

Vector Time (GMT): 2018/206/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -851597
98                 A    =         6777702
76  meter
 Y    =        4137177
86  meter          E    =           
0014810
 Z    =       -5312897
36                 I    =           51
55739
 XDOT =      -7545
735602                 Wp   =           76
30437
 YDOT =      -1288
784411  meter/sec      RA   =          188
44557  deg
 ZDOT =        209
835372                 TA   =          195
67756
                                          MA   =          195
72347
                                          Ha   =            221
531  n
mi
                                          Hp   =            214
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2793956
61                 X    =         -871990
87
 Y    =       13573418
18  feet           Y    =         4127541
26  meter
 Z    =      -17430765
60                 Z    =        -5317083
14
 XDOT =     -24756
350401                 XDOT =       -7531
782504
 YDOT =      -4228
295312  feet/sec       YDOT =       -1373
088043  meter/sec
 ZDOT =        688
436259                 ZDOT =         173
215083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5684303
36                 X    =        -1732575
67
 Y    =       12611988
70  feet           Y    =         3844134
16  meter
 Z    =      -17449982
82                 Z    =        -5318754
76
 XDOT =     -22238
263705                 XDOT =       -6778
222777
 YDOT =      -9315
028326  feet/sec       YDOT =       -2839
220634  meter/sec
 ZDOT =        524
483486                 ZDOT =         159
862566


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   18206
14081938  
00016717  00000-0  10270-3 0  9165
2 25544  51
6386 189
5435 0003977 352
8537   7
2558 15
54012831  4411


Satellite: ISS
Catalog Number: 25544
Epoch time:      18206
14081938   =   yrday
fracday
Element set:     916
Inclination:       51
6386  deg
RA of node:       189
5435  deg
Eccentricity:     
0003977     
Arg of perigee:   352
8537  deg
Mean anomaly:       7
2558  deg
Mean motion:   15
54012831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             441
Checksum:              320


Coasting Arc #18 (Orbit 456)
---------------------------------------

Vector Time (GMT): 2018/207/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944929
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2575054
02                 A    =         6779121
82  meter
 Y    =       -3803324
47  meter          E    =           
0008726
 Z    =        4984098
91                 I    =           51
59461
 XDOT =       7087
771864                 Wp   =           33
92288
 YDOT =       2071
969597  meter/sec      RA   =          183
44316  deg
 ZDOT =      -2071
982061                 TA   =           76
29200
                                          MA   =           76
19487
                                          Ha   =            221
599  n
mi
                                          Hp   =            214
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8448339
97                 X    =         2593182
77
 Y    =      -12478098
66  feet           Y    =        -3774427
59  meter
 Z    =       16352030
54                 Z    =         4996651
04
 XDOT =      23253
844698                 XDOT =        7074
140173
 YDOT =       6797
800514  feet/sec       YDOT =        2151
153953  meter/sec
 ZDOT =      -6797
841406                 ZDOT =       -2037
585617

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10772066
36                 X    =         3283325
83
 Y    =      -10449077
77  feet           Y    =        -3184878
90  meter
 Z    =       16408706
76                 Z    =         5001373
82
 XDOT =      20591
460847                 XDOT =        6276
277266
 YDOT =      10749
300949  feet/sec       YDOT =        3276
386929  meter/sec
 ZDOT =      -6643
914896                 ZDOT =       -2025
065260


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   18207
16974139  
00016717  00000-0  10270-3 0  9173
2 25544  51
6384 184
4146 0003990 357
6861   2
4272 15
53987878  4578


Satellite: ISS
Catalog Number: 25544
Epoch time:      18207
16974139   =   yrday
fracday
Element set:     917
Inclination:       51
6384  deg
RA of node:       184
4146  deg
Eccentricity:     
0003990     
Arg of perigee:   357
6861  deg
Mean anomaly:       2
4272  deg
Mean motion:   15
53987878  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             457
Checksum:              345


Coasting Arc #19 (Orbit 464)
---------------------------------------

Vector Time (GMT): 2018/207/15:58:15
150
Vector Time (MET): N/A
Weight (LBS)     : 944798
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1630938
56                 A    =         6779154
81  meter
 Y    =        4106092
79  meter          E    =           
0014202
 Z    =       -5153981
63                 I    =           51
61052
 XDOT =      -7433
357814                 Wp   =           61
27710
 YDOT =       1078
654400  meter/sec      RA   =          180
78185  deg
 ZDOT =      -1489
332277                 TA   =          194
33520
                                          MA   =          194
37553
                                          Ha   =            221
829  n
mi
                                          Hp   =            215
444

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5350848
29                 X    =         1609936
73
 Y    =       13471433
03  feet           Y    =         4124214
15  meter
 Z    =      -16909388
53                 Z    =        -5146109
84
 XDOT =     -24387
656869                 XDOT =       -7437
632914
 YDOT =       3538
892390  feet/sec       YDOT =         995
505704  meter/sec
 ZDOT =      -4886
260751                 ZDOT =       -1525
450543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6156527
22                 X    =        -1876509
50
 Y    =      -13167571
29  feet           Y    =        -4013475
73  meter
 Z    =      -16874559
09                 Z    =        -5143365
61
 XDOT =      23177
354898                 XDOT =        7064
457773
 YDOT =      -4352
187275  feet/sec       YDOT =       -1326
546681  meter/sec
 ZDOT =      -5048
265915                 ZDOT =       -1538
711451


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   18207
68420268  
00016717  00000-0  10270-3 0  9180
2 25544  51
6386 181
8547 0004278 347
1382  12
9660 15
53781754  4659


Satellite: ISS
Catalog Number: 25544
Epoch time:      18207
68420268   =   yrday
fracday
Element set:     918
Inclination:       51
6386  deg
RA of node:       181
8547  deg
Eccentricity:     
0004278     
Arg of perigee:   347
1382  deg
Mean anomaly:      12
9660  deg
Mean motion:   15
53781754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             465
Checksum:              333


Coasting Arc #20 (Orbit 480)
---------------------------------------

Vector Time (GMT): 2018/208/15:58:15
150
Vector Time (MET): N/A
Weight (LBS)     : 944798
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          41690
67                 A    =         6778304
71  meter
 Y    =       -4214730
47  meter          E    =           
0004978
 Z    =        5307317
09                 I    =           51
64152
 XDOT =       7656
606606                 Wp   =           18
29593
 YDOT =       -319
118185  meter/sec      RA   =          175
78544  deg
 ZDOT =       -308
867103                 TA   =           74
67548
                                          MA   =           74
62048
                                          Ha   =            221
782  n
mi
                                          Hp   =            215
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         136780
40                 X    =           63038
25
 Y    =      -13827855
88  feet           Y    =        -4214145
36  meter
 Z    =       17412457
64                 Z    =         5307571
09
 XDOT =      25120
100415                 XDOT =        7661
106306
 YDOT =      -1046
975672  feet/sec       YDOT =        -233
471535  meter/sec
 ZDOT =      -1013
343513                 ZDOT =        -271
663846

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         935768
93                 X    =          285222
37
 Y    =       13794814
52  feet           Y    =         4204659
47  meter
 Z    =       17414058
03                 Z    =         5307804
89
 XDOT =     -23987
621074                 XDOT =       -7311
426903
 YDOT =       2715
297354  feet/sec       YDOT =         827
622634  meter/sec
 ZDOT =       -846
533738                 ZDOT =        -258
023483


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   18208
71327348  
00016717  00000-0  10270-3 0  9191
2 25544  51
6390 176
7277 0004319 347
7519  12
3528 15
53807291  4811


Satellite: ISS
Catalog Number: 25544
Epoch time:      18208
71327348   =   yrday
fracday
Element set:     919
Inclination:       51
6390  deg
RA of node:       176
7277  deg
Eccentricity:     
0004319     
Arg of perigee:   347
7519  deg
Mean anomaly:      12
3528  deg
Mean motion:   15
53807291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             481
Checksum:              326
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