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

 
Date: November 3rd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


307/06:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 214 8

311/16:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 214 2

319/09:49:40 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 5

320/04:47:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 5

320/18:14:08 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 4

Coasting Arc #1 (Orbit 2001)
---------------------------------------

Vector Time (GMT): 2018/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5274969
93                 A    =         6788716
98  meter
 Y    =       -3860706
48  meter          E    =           
0013025
 Z    =        1816970
63                 I    =           51
94612
 XDOT =       1616
692038                 Wp   =           97
28968
 YDOT =      -4895
400354  meter/sec      RA   =           48
76738  deg
 ZDOT =      -5675
083838                 TA   =           62
82736
                                          MA   =           62
69464
                                          Ha   =            222
010  n
mi
                                          Hp   =            214
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17306331
79                 X    =        -5240232
38
 Y    =      -12666359
84  feet           Y    =        -3919500
57  meter
 Z    =        5961189
74                 Z    =         1791430
85
 XDOT =       5304
107737                 XDOT =        1698
880513
 YDOT =     -16061
024784  feet/sec       YDOT =       -4876
862028  meter/sec
 ZDOT =     -18619
041464                 ZDOT =       -5667
030626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21405742
89                 X    =         6524470
43
 Y    =       -1758065
71  feet           Y    =         -535858
43  meter
 Z    =        5846789
82                 Z    =         1782101
54
 XDOT =       6267
276917                 XDOT =        1910
266004
 YDOT =      14141
305778  feet/sec       YDOT =        4310
270001  meter/sec
 ZDOT =     -18582
152749                 ZDOT =       -5663
840158


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   18306
53569403  
00016717  00000-0  10270-3 0  9000
2 25544  51
6414  49
2918 0004090   3
3209 356
7970 15
53876756 20020


Satellite: ISS
Catalog Number: 25544
Epoch time:      18306
53569403   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:        49
2918  deg
Eccentricity:     
0004090     
Arg of perigee:     3
3209  deg
Mean anomaly:     356
7970  deg
Mean motion:   15
53876756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2002
Checksum:              304


Coasting Arc #2 (Orbit 2013)
---------------------------------------

Vector Time (GMT): 2018/307/06:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          57215
45                 A    =         6781446
60  meter
 Y    =        5060042
78  meter          E    =           
0008622
 Z    =        4506443
17                 I    =           51
90181
 XDOT =      -6371
415127                 Wp   =           81
22781
 YDOT =      -2804
830181  meter/sec      RA   =           45
06742  deg
 ZDOT =       3226
316237                 TA   =          336
45427
                                          MA   =          336
49371
                                          Ha   =            222
178  n
mi
                                          Hp   =            214
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         187714
73                 X    =          -21261
85
 Y    =       16601190
22  feet           Y    =         5060244
01  meter
 Z    =       14784918
52                 Z    =         4506530
26
 XDOT =     -20903
592935                 XDOT =       -6355
249160
 YDOT =      -9202
198756  feet/sec       YDOT =       -2875
989237  meter/sec
 ZDOT =      10585
027024                 ZDOT =        3195
405066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12115937
27                 X    =         3692937
68
 Y    =      -11351093
92  feet           Y    =        -3459813
43  meter
 Z    =       14784630
54                 Z    =         4506355
39
 XDOT =       6680
689898                 XDOT =        2036
274281
 YDOT =      20753
989453  feet/sec       YDOT =        6325
815985  meter/sec
 ZDOT =      10446
325400                 ZDOT =        3184
039982


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   18307
30743718  
00016717  00000-0  10270-3 0  9010
2 25544  51
6381  45
4471 0004632   3
6602 356
4584 15
53873060 20143


Satellite: ISS
Catalog Number: 25544
Epoch time:      18307
30743718   =   yrday
fracday
Element set:     901
Inclination:       51
6381  deg
RA of node:        45
4471  deg
Eccentricity:     
0004632     
Arg of perigee:     3
6602  deg
Mean anomaly:     356
4584  deg
Mean motion:   15
53873060  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2014
Checksum:              287


Coasting Arc #3 (Orbit 2028)
---------------------------------------

Vector Time (GMT): 2018/308/06:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1300534
05                 A    =         6778755
40  meter
 Y    =       -4207317
12  meter          E    =           
0015867
 Z    =       -5167312
31                 I    =           51
86877
 XDOT =       6435
788580                 Wp   =           62
93420
 YDOT =       3859
139060  meter/sec      RA   =           40
09101  deg
 ZDOT =      -1518
946007                 TA   =          192
43767
                                          MA   =          192
47687
                                          Ha   =            222
182  n
mi
                                          Hp   =            214
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4266844
00                 X    =         1372585
32
 Y    =      -13803533
85  feet           Y    =        -4192371
04  meter
 Z    =      -16953124
38                 Z    =        -5160819
43
 XDOT =      21114
791929                 XDOT =        6399
534659
 YDOT =      12661
217387  feet/sec       YDOT =        3930
905732  meter/sec
 ZDOT =      -4983
418659                 ZDOT =       -1487
770872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12993843
51                 X    =        -3960523
50
 Y    =        6396284
37  feet           Y    =         1949587
48  meter
 Z    =      -16923342
09                 Z    =        -5158234
67
 XDOT =      -5037
047065                 XDOT =       -1535
291945
 YDOT =     -23077
998783  feet/sec       YDOT =       -7034
174029  meter/sec
 ZDOT =      -4843
685011                 ZDOT =       -1476
355191


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   18308
27211439  
00016717  00000-0  10270-3 0  9028
2 25544  51
6380  40
6395 0004508   9
0636 351
0597 15
53897954 20292


Satellite: ISS
Catalog Number: 25544
Epoch time:      18308
27211439   =   yrday
fracday
Element set:     902
Inclination:       51
6380  deg
RA of node:        40
6395  deg
Eccentricity:     
0004508     
Arg of perigee:     9
0636  deg
Mean anomaly:     351
0597  deg
Mean motion:   15
53897954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2029
Checksum:              314


Coasting Arc #4 (Orbit 2044)
---------------------------------------

Vector Time (GMT): 2018/309/06:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2712211
71                 A    =         6778156
08  meter
 Y    =        3202907
09  meter          E    =           
0006276
 Z    =        5319716
42                 I    =           51
84098
 XDOT =      -6115
811604                 Wp   =           33
70942
 YDOT =      -4618
522850  meter/sec      RA   =           35
10808  deg
 ZDOT =       -332
082230                 TA   =           59
47763
                                          MA   =           59
41569
                                          Ha   =            222
436  n
mi
                                          Hp   =            214
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8898332
37                 X    =        -2773666
88
 Y    =       10508225
37  feet           Y    =         3172233
90  meter
 Z    =       17453137
87                 Z    =         5306391
72
 XDOT =     -20064
998700                 XDOT =       -6062
098334
 YDOT =     -15152
634021  feet/sec       YDOT =       -4686
613791  meter/sec
 ZDOT =      -1089
508628                 ZDOT =        -361
660693

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13809084
43                 X    =         4209008
94
 Y    =       -1008169
02  feet           Y    =         -307289
92  meter
 Z    =       17392754
91                 Z    =         5301311
70
 XDOT =       3306
010919                 XDOT =        1007
672128
 YDOT =      23902
445092  feet/sec       YDOT =        7285
465264  meter/sec
 ZDOT =      -1221
939213                 ZDOT =        -372
447072


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   18309
30110030  
00016717  00000-0  10270-3 0  9039
2 25544  51
6386  35
5111 0004563  13
0944 347
0326 15
53866144 20455


Satellite: ISS
Catalog Number: 25544
Epoch time:      18309
30110030   =   yrday
fracday
Element set:     903
Inclination:       51
6386  deg
RA of node:        35
5111  deg
Eccentricity:     
0004563     
Arg of perigee:    13
0944  deg
Mean anomaly:     347
0326  deg
Mean motion:   15
53866144  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2045
Checksum:              268


Coasting Arc #5 (Orbit 2059)
---------------------------------------

Vector Time (GMT): 2018/310/06:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4052958
16                 A    =         6779560
14  meter
 Y    =       -2183412
52  meter          E    =           
0013419
 Z    =       -4988050
05                 I    =           51
81825
 XDOT =       5346
489083                 Wp   =           85
94132
 YDOT =       5048
340926  meter/sec      RA   =           30
12501  deg
 ZDOT =       2140
283009                 TA   =          204
85241
                                          MA   =          204
91710
                                          Ha   =            222
382  n
mi
                                          Hp   =            214
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13297106
81                 X    =         4101302
40
 Y    =       -7163426
91  feet           Y    =        -2137819
40  meter
 Z    =      -16364993
60                 Z    =        -4968244
17
 XDOT =      17540
974682                 XDOT =        5279
243125
 YDOT =      16562
798315  feet/sec       YDOT =        5107
753165  meter/sec
 ZDOT =       7021
925883                 ZDOT =        2166
091551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14604311
65                 X    =        -4451394
19
 Y    =       -4214236
60  feet           Y    =        -1284499
32  meter
 Z    =      -16275596
50                 Z    =        -4960801
81
 XDOT =      -1293
866693                 XDOT =        -394
370568
 YDOT =     -23005
867170  feet/sec       YDOT =       -7012
188313  meter/sec
 ZDOT =       7137
320794                 ZDOT =        2175
455378


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   18310
26577003  
00016717  00000-0  10270-3 0  9044
2 25544  51
6386  30
7038 0004503  18
8417 341
2902 15
53908069 20608


Satellite: ISS
Catalog Number: 25544
Epoch time:      18310
26577003   =   yrday
fracday
Element set:     904
Inclination:       51
6386  deg
RA of node:        30
7038  deg
Eccentricity:     
0004503     
Arg of perigee:    18
8417  deg
Mean anomaly:     341
2902  deg
Mean motion:   15
53908069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2060
Checksum:              286


Coasting Arc #6 (Orbit 2075)
---------------------------------------

Vector Time (GMT): 2018/311/06:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5231461
40                 A    =         6782825
59  meter
 Y    =        1155630
40  meter          E    =           
0013494
 Z    =        4154191
31                 I    =           51
79906
 XDOT =      -4159
159489                 Wp   =           60
31626
 YDOT =      -5227
846264  meter/sec      RA   =           25
14656  deg
 ZDOT =      -3767
712613                 TA   =           68
44628
                                          MA   =           68
30252
                                          Ha   =            222
498  n
mi
                                          Hp   =            214
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17163587
26                 X    =        -5264174
60
 Y    =        3791438
32  feet           Y    =         1096945
73  meter
 Z    =       13629236
60                 Z    =         4128698
50
 XDOT =     -13645
536382                 XDOT =       -4082
089057
 YDOT =     -17151
726587  feet/sec       YDOT =       -5273
926015  meter/sec
 ZDOT =     -12361
261854                 ZDOT =       -3787
729645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15168541
81                 X    =         4623371
54
 Y    =        9055163
95  feet           Y    =         2760013
97  meter
 Z    =       13514405
94                 Z    =         4119190
93
 XDOT =      -1206
856754                 XDOT =        -367
849939
 YDOT =      20681
051779  feet/sec       YDOT =        6303
584582  meter/sec
 ZDOT =     -12450
564201                 ZDOT =       -3794
931968


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   18311
29474890  
00016717  00000-0  10270-3 0  9059
2 25544  51
6380  25
5763 0004429  21
1935 338
9400 15
53890469 20765


Satellite: ISS
Catalog Number: 25544
Epoch time:      18311
29474890   =   yrday
fracday
Element set:     905
Inclination:       51
6380  deg
RA of node:        25
5763  deg
Eccentricity:     
0004429     
Arg of perigee:    21
1935  deg
Mean anomaly:     338
9400  deg
Mean motion:   15
53890469  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2076
Checksum:              318


Coasting Arc #7 (Orbit 2082)
---------------------------------------

Vector Time (GMT): 2018/311/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4212492
23                 A    =         6780324
12  meter
 Y    =        2307116
67  meter          E    =           
0011643
 Z    =        4782023
09                 I    =           51
77912
 XDOT =      -5536
558145                 Wp   =           46
35193
 YDOT =      -4603
103655  meter/sec      RA   =           22
92767  deg
 ZDOT =      -2644
497699                 TA   =           69
74044
                                          MA   =           69
61531
                                          Ha   =            222
556  n
mi
                                          Hp   =            214
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13820512
57                 X    =        -4261207
18
 Y    =        7569280
40  feet           Y    =         2259737
31  meter
 Z    =       15689052
15                 Z    =         4761441
34
 XDOT =     -18164
560843                 XDOT =       -5471
827521
 YDOT =     -15102
046113  feet/sec       YDOT =       -4664
655384  meter/sec
 ZDOT =      -8676
173553                 ZDOT =       -2671
235886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13291109
92                 X    =        -4051130
30
 Y    =       -8634432
17  feet           Y    =        -2631774
92  meter
 Z    =       15596150
45                 Z    =         4753706
66
 XDOT =       4019
781353                 XDOT =        1225
229356
 YDOT =     -22146
075419  feet/sec       YDOT =       -6750
123788  meter/sec
 ZDOT =      -8795
789069                 ZDOT =       -2680
956508


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   18311
74492428  
00016717  00000-0  10270-3 0  9067
2 25544  51
6395  23
3366 0004731  21
8460 338
2893 15
53927048 20833


Satellite: ISS
Catalog Number: 25544
Epoch time:      18311
74492428   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:        23
3366  deg
Eccentricity:     
0004731     
Arg of perigee:    21
8460  deg
Mean anomaly:     338
2893  deg
Mean motion:   15
53927048  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2083
Checksum:              314


Coasting Arc #8 (Orbit 2097)
---------------------------------------

Vector Time (GMT): 2018/312/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5394725
91                 A    =         6783804
75  meter
 Y    =       -1445869
60  meter          E    =           
0008663
 Z    =       -3855078
81                 I    =           51
75986
 XDOT =       4258
051155                 Wp   =           69
93976
 YDOT =       4824
977691  meter/sec      RA   =           17
94935  deg
 ZDOT =       4159
484840                 TA   =          243
73657
                                          MA   =          243
82562
                                          Ha   =            222
686  n
mi
                                          Hp   =            214
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17699231
97                 X    =         5429219
54
 Y    =       -4743666
66  feet           Y    =        -1385349
10  meter
 Z    =      -12647896
35                 Z    =        -3828788
60
 XDOT =      13969
984105                 XDOT =        4183
575284
 YDOT =      15829
979301  feet/sec       YDOT =        4872
177695  meter/sec
 ZDOT =      13646
603807                 ZDOT =        4179
988738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12873557
76                 X    =         3923860
40
 Y    =       13153669
06  feet           Y    =         4009238
33  meter
 Z    =      -12529444
07                 Z    =        -3818974
55
 XDOT =      -6004
357066                 XDOT =       -1830
128034
 YDOT =      18929
595072  feet/sec       YDOT =        5769
740578  meter/sec
 ZDOT =      13738
133680                 ZDOT =        4187
383146


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   18312
70958715  
00016717  00000-0  10270-3 0  9071
2 25544  51
6398  18
5301 0004917  26
6953 333
4452 15
53902672 20987


Satellite: ISS
Catalog Number: 25544
Epoch time:      18312
70958715   =   yrday
fracday
Element set:     907
Inclination:       51
6398  deg
RA of node:        18
5301  deg
Eccentricity:     
0004917     
Arg of perigee:    26
6953  deg
Mean anomaly:     333
4452  deg
Mean motion:   15
53902672  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2098
Checksum:              322


Coasting Arc #9 (Orbit 2113)
---------------------------------------

Vector Time (GMT): 2018/313/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6268936
01                 A    =         6787254
16  meter
 Y    =         595262
49  meter          E    =           
0015613
 Z    =        2520503
84                 I    =           51
73861
 XDOT =      -2607
125419                 Wp   =           86
32582
 YDOT =      -4890
367110  meter/sec      RA   =           12
97706  deg
 ZDOT =      -5300
148144                 TA   =           65
42809
                                          MA   =           65
26546
                                          Ha   =            222
642  n
mi
                                          Hp   =            213
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20567375
37                 X    =        -6287370
08
 Y    =        1952960
94  feet           Y    =          525055
74  meter
 Z    =        8269369
56                 Z    =         2490005
97
 XDOT =      -8553
561085                 XDOT =       -2526
500200
 YDOT =     -16044
511517  feet/sec       YDOT =       -4919
070809  meter/sec
 ZDOT =     -17388
937480                 ZDOT =       -5312
617329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12129248
41                 X    =        -3696994
92
 Y    =      -16791766
62  feet           Y    =        -5118130
47  meter
 Z    =        8132119
37                 Z    =         2478669
98
 XDOT =       8337
406114                 XDOT =        2541
241384
 YDOT =     -14517
837392  feet/sec       YDOT =       -4425
036837  meter/sec
 ZDOT =     -17444
311143                 ZDOT =       -5317
026036


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   18313
73855622  
00016717  00000-0  10270-3 0  9089
2 25544  51
6384  13
4017 0004993  28
0153 332
1267 15
53947658 21144


Satellite: ISS
Catalog Number: 25544
Epoch time:      18313
73855622   =   yrday
fracday
Element set:     908
Inclination:       51
6384  deg
RA of node:        13
4017  deg
Eccentricity:     
0004993     
Arg of perigee:    28
0153  deg
Mean anomaly:     332
1267  deg
Mean motion:   15
53947658  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2114
Checksum:              307


Coasting Arc #10 (Orbit 2128)
---------------------------------------

Vector Time (GMT): 2018/314/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6708691
16                 A    =         6789469
65  meter
 Y    =         157572
68  meter          E    =           
0014750
 Z    =        -986832
13                 I    =           51
71324
 XDOT =        748
678391                 Wp   =           36
95384
 YDOT =       4822
197540  meter/sec      RA   =            8
01163  deg
 ZDOT =       5917
051925                 TA   =          312
36407
                                          MA   =          312
48886
                                          Ha   =            222
698  n
mi
                                          Hp   =            213
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22010141
60                 X    =         6711224
15
 Y    =         516970
73  feet           Y    =          232608
13  meter
 Z    =       -3237638
23                 Z    =         -954236
72
 XDOT =       2456
293934                 XDOT =         665
957006
 YDOT =      15820
858070  feet/sec       YDOT =        4830
106971  meter/sec
 ZDOT =      19412
900015                 ZDOT =        5920
488142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11042680
24                 X    =         3365808
94
 Y    =       19070930
77  feet           Y    =         5812819
70  meter
 Z    =       -3091068
73                 Z    =         -942157
75
 XDOT =     -10899
242656                 XDOT =       -3322
089162
 YDOT =       9427
930556  feet/sec       YDOT =        2873
633234  meter/sec
 ZDOT =      19427
652425                 ZDOT =        5921
548459


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   18314
70321373  
00016717  00000-0  10270-3 0  9099
2 25544  51
6381   8
5952 0004856  34
4467 325
6999 15
53950215 21299


Satellite: ISS
Catalog Number: 25544
Epoch time:      18314
70321373   =   yrday
fracday
Element set:     909
Inclination:       51
6381  deg
RA of node:         8
5952  deg
Eccentricity:     
0004856     
Arg of perigee:    34
4467  deg
Mean anomaly:     325
6999  deg
Mean motion:   15
53950215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2129
Checksum:              322


Coasting Arc #11 (Orbit 2144)
---------------------------------------

Vector Time (GMT): 2018/315/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6692332
57                 A    =         6789637
09  meter
 Y    =        -901671
47  meter          E    =           
0010428
 Z    =        -689406
30                 I    =           51
68189
 XDOT =       1233
425019                 Wp   =          111
56876
 YDOT =      -4653
575397  meter/sec      RA   =            3
04573  deg
 ZDOT =      -5963
231309                 TA   =           75
86905
                                          MA   =           75
75319
                                          Ha   =            222
729  n
mi
                                          Hp   =            213
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21956471
67                 X    =        -6678403
60
 Y    =       -2958239
74  feet           Y    =         -976431
86  meter
 Z    =       -2261831
70                 Z    =         -721882
19
 XDOT =       4046
670009                 XDOT =        1314
337729
 YDOT =     -15267
635816  feet/sec       YDOT =       -4639
329649  meter/sec
 ZDOT =     -19564
407181                 ZDOT =       -5957
043364

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9259171
64                 X    =        -2822195
51
 Y    =      -20110300
71  feet           Y    =        -6129619
66  meter
 Z    =       -2407749
84                 Z    =         -733882
15
 XDOT =      13663
592156                 XDOT =        4164
662889
 YDOT =      -3980
155005  feet/sec       YDOT =       -1213
151246  meter/sec
 ZDOT =     -19535
899505                 ZDOT =       -5954
542169


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   18315
73217680  
00016717  00000-0  10270-3 0  9100
2 25544  51
6391   3
4662 0005040  35
8496 324
2994 15
53942239 21450


Satellite: ISS
Catalog Number: 25544
Epoch time:      18315
73217680   =   yrday
fracday
Element set:     910
Inclination:       51
6391  deg
RA of node:         3
4662  deg
Eccentricity:     
0005040     
Arg of perigee:    35
8496  deg
Mean anomaly:     324
2994  deg
Mean motion:   15
53942239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2145
Checksum:              304


Coasting Arc #12 (Orbit 2160)
---------------------------------------

Vector Time (GMT): 2018/316/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6194597
44                 A    =         6787539
34  meter
 Y    =        1576825
10  meter          E    =           
0018096
 Z    =        2254028
32                 I    =           51
64175
 XDOT =      -3115
873668                 Wp   =           63
52947
 YDOT =       4417
687275  meter/sec      RA   =          358
07660  deg
 ZDOT =       5446
796446                 TA   =          321
56415
                                          MA   =          321
69292
                                          Ha   =            222
615  n
mi
                                          Hp   =            213
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20323482
41                 X    =         6165555
48
 Y    =        5173310
69  feet           Y    =         1645934
89  meter
 Z    =        7395106
02                 Z    =         2284049
57
 XDOT =     -10222
682638                 XDOT =       -3191
500002
 YDOT =      14493
724656  feet/sec       YDOT =        4382
420273  meter/sec
 ZDOT =      17870
067080                 ZDOT =        5431
476907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6836475
41                 X    =         2083757
70
 Y    =       19775190
56  feet           Y    =         6027478
08  meter
 Z    =        7529881
54                 Z    =         2295107
89
 XDOT =     -16351
743774                 XDOT =       -4984
011502
 YDOT =      -1156
829007  feet/sec       YDOT =        -352
601481  meter/sec
 ZDOT =      17800
529570                 ZDOT =        5425
601413


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   18316
76113476  
00016717  00000-0  10270-3 0  9113
2 25544  51
6388 358
3390 0004849  39
6199 320
5307 15
53977435 21615


Satellite: ISS
Catalog Number: 25544
Epoch time:      18316
76113476   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:       358
3390  deg
Eccentricity:     
0004849     
Arg of perigee:    39
6199  deg
Mean anomaly:     320
5307  deg
Mean motion:   15
53977435  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2161
Checksum:              332


Coasting Arc #13 (Orbit 2175)
---------------------------------------

Vector Time (GMT): 2018/317/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5263761
09                 A    =         6784141
76  meter
 Y    =       -2269601
94  meter          E    =           
0010065
 Z    =       -3640647
94                 I    =           51
59703
 XDOT =       4782
088169                 Wp   =           61
43924
 YDOT =      -4074
903946  meter/sec      RA   =          353
09637  deg
 ZDOT =      -4378
282638                 TA   =          161
72822
                                          MA   =          161
69203
                                          Ha   =            222
819  n
mi
                                          Hp   =            213
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17269557
37                 X    =        -5220305
95
 Y    =       -7446200
58  feet           Y    =        -2328221
83  meter
 Z    =      -11944383
02                 Z    =        -3666112
39
 XDOT =      15689
265647                 XDOT =        4848
567155
 YDOT =     -13369
107435  feet/sec       YDOT =       -4021
055406  meter/sec
 ZDOT =     -14364
444352                 ZDOT =       -4354
891303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3558111
62                 X    =        -1084512
42
 Y    =      -18392464
27  feet           Y    =        -5606023
11  meter
 Z    =      -12058561
29                 Z    =        -3675449
48
 XDOT =      18605
852290                 XDOT =        5671
063778
 YDOT =       5739
332194  feet/sec       YDOT =        1749
348453  meter/sec
 ZDOT =     -14258
663609                 ZDOT =       -4346
040668


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   18317
72578388  
00016717  00000-0  10270-3 0  9128
2 25544  51
6387 353
5309 0005057  41
9631 318
1908 15
53946403 21767


Satellite: ISS
Catalog Number: 25544
Epoch time:      18317
72578388   =   yrday
fracday
Element set:     912
Inclination:       51
6387  deg
RA of node:       353
5309  deg
Eccentricity:     
0005057     
Arg of perigee:    41
9631  deg
Mean anomaly:     318
1908  deg
Mean motion:   15
53946403  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2176
Checksum:              329


Coasting Arc #14 (Orbit 2191)
---------------------------------------

Vector Time (GMT): 2018/318/16:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3973445
76                 A    =         6780483
26  meter
 Y    =        2927669
24  meter          E    =           
0010671
 Z    =        4640004
60                 I    =           51
55342
 XDOT =      -6093
160648                 Wp   =           90
01113
 YDOT =       3645
774135  meter/sec      RA   =          348
10564  deg
 ZDOT =       2911
707750                 TA   =          330
98362
                                          MA   =          331
04290
                                          Ha   =            222
615  n
mi
                                          Hp   =            213
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13036239
36                 X    =         3917873
44
 Y    =        9605214
04  feet           Y    =         2971792
17  meter
 Z    =       15223112
21                 Z    =         4659171
60
 XDOT =     -19990
684542                 XDOT =       -6147
619575
 YDOT =      11961
201230  feet/sec       YDOT =        3577
331575  meter/sec
 ZDOT =       9552
846949                 ZDOT =        2881
976772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -349368
81                 X    =         -106487
61
 Y    =       16107859
70  feet           Y    =         4909675
64  meter
 Z    =       15308873
76                 Z    =         4666144
72
 XDOT =     -20185
831972                 XDOT =       -6152
641585
 YDOT =      -9407
227289  feet/sec       YDOT =       -2867
322878  meter/sec
 ZDOT =       9418
629340                 ZDOT =        2870
798223


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   18318
75473612  
00016717  00000-0  10270-3 0  9137
2 25544  51
6397 348
4037 0004835  44
6188 315
5353 15
53988186 21926


Satellite: ISS
Catalog Number: 25544
Epoch time:      18318
75473612   =   yrday
fracday
Element set:     913
Inclination:       51
6397  deg
RA of node:       348
4037  deg
Eccentricity:     
0004835     
Arg of perigee:    44
6188  deg
Mean anomaly:     315
5353  deg
Mean motion:   15
53988186  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2192
Checksum:              337


Coasting Arc #15 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2018/319/09:49:40
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3782938
02                 A    =         6779888
58  meter
 Y    =        2915517
30  meter          E    =           
0009802
 Z    =        4803717
33                 I    =           51
52983
 XDOT =      -6163
982707                 Wp   =           91
85580
 YDOT =       3798
419846  meter/sec      RA   =          344
56912  deg
 ZDOT =       2543
976973                 TA   =          333
06930
                                          MA   =          333
12014
                                          Ha   =            222
675  n
mi
                                          Hp   =            213
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12411213
97                 X    =         3726720
52
 Y    =        9565345
48  feet           Y    =         2957506
28  meter
 Z    =       15760227
47                 Z    =         4821957
30
 XDOT =     -20223
040377                 XDOT =       -6218
357029
 YDOT =      12462
007369  feet/sec       YDOT =        3729
185812  meter/sec
 ZDOT =       8346
381144                 ZDOT =        2513
902150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14914818
85                 X    =        -4546036
78
 Y    =       -4528103
93  feet           Y    =        -1380166
08  meter
 Z    =       15841820
92                 Z    =         4828587
02
 XDOT =      14143
857067                 XDOT =        4311
047634
 YDOT =     -17807
443818  feet/sec       YDOT =       -5427
708876  meter/sec
 ZDOT =       8210
602838                 ZDOT =        2502
591745


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   18319
46213940  
00016717  00000-0  10270-3 0  9143
2 25544  51
6413 344
8769 0004776  48
7498 311
4066 15
53966939 22031


Satellite: ISS
Catalog Number: 25544
Epoch time:      18319
46213940   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:       344
8769  deg
Eccentricity:     
0004776     
Arg of perigee:    48
7498  deg
Mean anomaly:     311
4066  deg
Mean motion:   15
53966939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              338


Coasting Arc #16 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2018/320/04:47:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5892263
44                 A    =         6789217
34  meter
 Y    =        3123335
99  meter          E    =           
0016159
 Z    =        1243650
00                 I    =           51
53424
 XDOT =      -3243
738607                 Wp   =          105
65170
 YDOT =      -3772
434778  meter/sec      RA   =          340
59314  deg
 ZDOT =      -5835
287932                 TA   =           60
80751
                                          MA   =           60
64596
                                          Ha   =            222
849  n
mi
                                          Hp   =            213
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19331572
95                 X    =        -5932792
60
 Y    =       10247165
33  feet           Y    =         3057217
97  meter
 Z    =        4080216
53                 Z    =         1214928
68
 XDOT =     -10642
187031                 XDOT =       -3172
967994
 YDOT =     -12376
754522  feet/sec       YDOT =       -3808
312708  meter/sec
 ZDOT =     -19144
645446                 ZDOT =       -5850
873267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19683118
97                 X    =         5999414
66
 Y    =        9608830
52  feet           Y    =         2928771
54  meter
 Z    =        3950630
42                 Z    =         1204152
15
 XDOT =      -3109
900225                 XDOT =        -947
897589
 YDOT =      14352
414573  feet/sec       YDOT =        4374
615962  meter/sec
 ZDOT =     -19214
178216                 ZDOT =       -5856
481520


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   18320
23385241  
00016717  00000-0  10270-3 0  9155
2 25544  51
6399 341
0280 0004739  54
7435 305
4160 15
53956360 22156


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
23385241   =   yrday
fracday
Element set:     915
Inclination:       51
6399  deg
RA of node:       341
0280  deg
Eccentricity:     
0004739     
Arg of perigee:    54
7435  deg
Mean anomaly:     305
4160  deg
Mean motion:   15
53956360  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              295


Coasting Arc #17 (Orbit 2223)
---------------------------------------

Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4181977
00                 A    =         6779991
94  meter
 Y    =        2389148
44  meter          E    =           
0010391
 Z    =        4763112
04                 I    =           51
48682
 XDOT =      -5598
285655                 Wp   =           92
28275
 YDOT =       4542
359626  meter/sec      RA   =          337
83132  deg
 ZDOT =       2631
461329                 TA   =          331
69945
                                          MA   =          331
75586
                                          Ha   =            222
735  n
mi
                                          Hp   =            213
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13720396
97                 X    =         4131813
06
 Y    =        7838413
51  feet           Y    =         2435633
67  meter
 Z    =       15627008
00                 Z    =         4783305
09
 XDOT =     -18367
078922                 XDOT =       -5661
445935
 YDOT =      14902
754678  feet/sec       YDOT =        4479
402527  meter/sec
 ZDOT =       8633
403311                 ZDOT =        2604
113075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7494232
92                 X    =         2284242
19
 Y    =       13809108
34  feet           Y    =         4209016
22  meter
 Z    =       15717455
21                 Z    =         4790680
35
 XDOT =     -22493
459970                 XDOT =       -6856
006599
 YDOT =       2501
502869  feet/sec       YDOT =         762
458075  meter/sec
 ZDOT =       8509
794024                 ZDOT =        2593
785219


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   18320
81263425  
00016717  00000-0  10270-3 0  9169
2 25544  51
6403 338
1486 0004973  51
9529 308
2071 15
53984520 22241


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
81263425   =   yrday
fracday
Element set:     916
Inclination:       51
6403  deg
RA of node:       338
1486  deg
Eccentricity:     
0004973     
Arg of perigee:    51
9529  deg
Mean anomaly:     308
2071  deg
Mean motion:   15
53984520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2224
Checksum:              304
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