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

 
Date: June 27th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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


179/14:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 216 1

180/09:42:42 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 216 0

183/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 216 2

187/05:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 216 1

Coasting Arc #1 (Orbit 3980)
---------------------------------------

Vector Time (GMT): 2018/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6279606
03                 A    =         6787024
57  meter
 Y    =        -531973
99  meter          E    =           
0010501
 Z    =        2509307
87                 I    =           51
50162
 XDOT =      -1670
803411                 Wp   =           86
69247
 YDOT =       5297
509573  meter/sec      RA   =          336
69427  deg
 ZDOT =       5285
756110                 TA   =          301
51536
                                          MA   =          301
61790
                                          Ha   =            220
614  n
mi
                                          Hp   =            215
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20602381
98                 X    =         6272899
07
 Y    =       -1745321
50  feet           Y    =         -461788
99  meter
 Z    =        8232637
38                 Z    =         2539795
73
 XDOT =      -5481
638487                 XDOT =       -1755
592909
 YDOT =      17380
280750  feet/sec       YDOT =        5278
350619  meter/sec
 ZDOT =      17341
719522                 ZDOT =        5277
434760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2711645
03                 X    =         -826509
41
 Y    =      -20442250
30  feet           Y    =        -6230797
89  meter
 Z    =        8369109
43                 Z    =         2550904
55
 XDOT =      16135
569233                 XDOT =        4918
121502
 YDOT =       4968
281361  feet/sec       YDOT =        1514
332159  meter/sec
 ZDOT =      17303
619849                 ZDOT =        5274
143330


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   18176
55918965  
00016717  00000-0  10270-3 0  9008
2 25544  51
6377 336
9772 0003910 225
4028 134
6805 15
53973338 39819


Satellite: ISS
Catalog Number: 25544
Epoch time:      18176
55918965   =   yrday
fracday
Element set:     900
Inclination:       51
6377  deg
RA of node:       336
9772  deg
Eccentricity:     
0003910     
Arg of perigee:   225
4028  deg
Mean anomaly:     134
6805  deg
Mean motion:   15
53973338  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3981
Checksum:              341


Coasting Arc #2 (Orbit 3995)
---------------------------------------

Vector Time (GMT): 2018/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5573165
88                 A    =         6783395
83  meter
 Y    =        -473767
83  meter          E    =           
0003355
 Z    =       -3840143
94                 I    =           51
45994
 XDOT =       3319
296946                 Wp   =          103
20496
 YDOT =      -5531
116006  meter/sec      RA   =          331
70415  deg
 ZDOT =      -4138
682958                 TA   =          123
15024
                                          MA   =          123
11804
                                          Ha   =            220
455  n
mi
                                          Hp   =            215
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18284664
95                 X    =        -5548800
48
 Y    =       -1554356
41  feet           Y    =         -535953
96  meter
 Z    =      -12598897
45                 Z    =        -3867157
35
 XDOT =      10890
081843                 XDOT =        3401
004240
 YDOT =     -18146
706056  feet/sec       YDOT =       -5493
539816  meter/sec
 ZDOT =     -13578
356163                 ZDOT =       -4122
361406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -381275
63                 X    =         -116212
81
 Y    =       18263136
06  feet           Y    =         5566603
87  meter
 Z    =      -12719658
14                 Z    =        -3876951
80
 XDOT =     -17484
780237                 XDOT =       -5329
361016
 YDOT =      -9761
798209  feet/sec       YDOT =       -2975
396094  meter/sec
 ZDOT =     -13504
434995                 ZDOT =       -4116
151786


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   18177
52382121  
00016717  00000-0  10270-3 0  9016
2 25544  51
6380 332
1703 0003810 229
4612 130
6209 15
53978055 39968


Satellite: ISS
Catalog Number: 25544
Epoch time:      18177
52382121   =   yrday
fracday
Element set:     901
Inclination:       51
6380  deg
RA of node:       332
1703  deg
Eccentricity:     
0003810     
Arg of perigee:   229
4612  deg
Mean anomaly:     130
6209  deg
Mean motion:   15
53978055  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3996
Checksum:              298


Coasting Arc #3 (Orbit 4011)
---------------------------------------

Vector Time (GMT): 2018/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4550966
75                 A    =         6779919
68  meter
 Y    =        1567466
14  meter          E    =           
0006697
 Z    =        4774515
20                 I    =           51
42051
 XDOT =      -4637
251182                 Wp   =          151
45350
 YDOT =       5526
151530  meter/sec      RA   =          326
70072  deg
 ZDOT =       2598
619819                 TA   =          272
81715
                                          MA   =          272
89380
                                          Ha   =            220
250  n
mi
                                          Hp   =            216
042

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14930993
26                 X    =         4509908
68
 Y    =        5142605
44  feet           Y    =         1618127
81  meter
 Z    =       15664419
96                 Z    =         4796522
69
 XDOT =     -15214
078681                 XDOT =       -4711
324158
 YDOT =      18130
418406  feet/sec       YDOT =        5473
879988  meter/sec
 ZDOT =       8525
655574                 ZDOT =        2575
914746

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3918561
95                 X    =         1194377
68
 Y    =      -15196712
46  feet           Y    =        -4631957
96  meter
 Z    =       15762607
83                 Z    =         4804442
87
 XDOT =      18206
973312                 XDOT =        5549
485466
 YDOT =      13456
253274  feet/sec       YDOT =        4101
465998  meter/sec
 ZDOT =       8423
186804                 ZDOT =        2567
387338


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   18178
55275710  
00016717  00000-0  10270-3 0  9026
2 25544  51
6386 327
0414 0004003 234
5209 125
5570 15
53997615 40127


Satellite: ISS
Catalog Number: 25544
Epoch time:      18178
55275710   =   yrday
fracday
Element set:     902
Inclination:       51
6386  deg
RA of node:       327
0414  deg
Eccentricity:     
0004003     
Arg of perigee:   234
5209  deg
Mean anomaly:     125
5570  deg
Mean motion:   15
53997615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4012
Checksum:              297


Coasting Arc #4 (Orbit 4026)
---------------------------------------

Vector Time (GMT): 2018/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3304636
12                 A    =         6777924
83  meter
 Y    =       -2738522
00  meter          E    =           
0011353
 Z    =       -5255752
68                 I    =           51
38783
 XDOT =       5566
277966                 Wp   =           92
38702
 YDOT =      -5202
715280  meter/sec      RA   =          321
68922  deg
 ZDOT =       -790
942937                 TA   =          170
03082
                                          MA   =          170
00828
                                          Ha   =            220
292  n
mi
                                          Hp   =            215
890

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10841982
02                 X    =        -3248238
11
 Y    =       -8984652
24  feet           Y    =        -2775160
50  meter
 Z    =      -17243283
06                 Z    =        -5271668
83
 XDOT =      18262
066817                 XDOT =        5627
884418
 YDOT =     -17069
275854  feet/sec       YDOT =       -5140
124729  meter/sec
 ZDOT =      -2594
957141                 ZDOT =        -763
755299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7884300
66                 X    =        -2403134
84
 Y    =       11561374
06  feet           Y    =         3523906
81  meter
 Z    =      -17314034
58                 Z    =        -5277317
74
 XDOT =     -17945
852054                 XDOT =       -5469
895706
 YDOT =     -15931
438481  feet/sec       YDOT =       -4855
902449  meter/sec
 ZDOT =      -2472
497908                 ZDOT =        -753
617362


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   18179
51738186  
00016717  00000-0  10270-3 0  9035
2 25544  51
6397 322
2347 0003760 237
4251 122
6539 15
53997155 40277


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
51738186   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       322
2347  deg
Eccentricity:     
0003760     
Arg of perigee:   237
4251  deg
Mean anomaly:     122
6539  deg
Mean motion:   15
53997155  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4027
Checksum:              326


Coasting Arc #5 (Orbit 4028)
---------------------------------------

Vector Time (GMT): 2018/179/14:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2050754
86                 A    =         6777856
48  meter
 Y    =        3745783
61  meter          E    =           
0000863
 Z    =        5263838
35                 I    =           51
38710
 XDOT =      -6270
140267                 Wp   =          226
82708
 YDOT =       4364
366172  meter/sec      RA   =          321
18212  deg
 ZDOT =       -663
558157                 TA   =          229
52733
                                          MA   =          229
53486
                                          Ha   =            220
123  n
mi
                                          Hp   =            216
082

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6728198
37                 X    =         1983147
30
 Y    =       12289316
32  feet           Y    =         3768337
67  meter
 Z    =       17269810
84                 Z    =         5273636
55
 XDOT =     -20571
326334                 XDOT =       -6315
254607
 YDOT =      14318
786652  feet/sec       YDOT =        4293
997002  meter/sec
 ZDOT =      -2177
028074                 ZDOT =        -694
124967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4849806
70                 X    =         1478221
08
 Y    =      -13087420
84  feet           Y    =        -3989045
87  meter
 Z    =       17313032
84                 Z    =         5277012
41
 XDOT =      23378
565993                 XDOT =        7125
786915
 YDOT =       5604
452347  feet/sec       YDOT =        1708
237075  meter/sec
 ZDOT =      -2314
466144                 ZDOT =        -705
449281


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   18179
64599685  
00016717  00000-0  10270-3 0  9049
2 25544  51
6417 321
5937 0003900 239
7696 120
3071 15
54010044 40293


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
64599685   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:       321
5937  deg
Eccentricity:     
0003900     
Arg of perigee:   239
7696  deg
Mean anomaly:     120
3071  deg
Mean motion:   15
54010044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4029
Checksum:              316


Coasting Arc #6 (Orbit 4040)
---------------------------------------

Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1328769
47                 A    =         6778792
83  meter
 Y    =       -4302402
19  meter          E    =           
0010768
 Z    =       -5076764
89                 I    =           51
36550
 XDOT =       6313
508473                 Wp   =          115
68341
 YDOT =      -3981
960339  meter/sec      RA   =          317
14457  deg
 ZDOT =       1720
400072                 TA   =          171
03571
                                          MA   =          171
01647
                                          Ha   =            220
228  n
mi
                                          Hp   =            216
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4359479
88                 X    =        -1255900
06
 Y    =      -14115492
76  feet           Y    =        -4316853
15  meter
 Z    =      -16656052
80                 Z    =        -5083043
24
 XDOT =      20713
610476                 XDOT =        6349
209900
 YDOT =     -13064
174339  feet/sec       YDOT =       -3911
158993  meter/sec
 ZDOT =       5644
357191                 ZDOT =        1751
154694

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14470453
00                 X    =        -4410594
07
 Y    =       -2818675
25  feet           Y    =         -859132
22  meter
 Z    =      -16683445
54                 Z    =        -5085114
20
 XDOT =      -2129
762445                 XDOT =        -649
151593
 YDOT =     -23326
027702  feet/sec       YDOT =       -7109
773244  meter/sec
 ZDOT =       5782
567233                 ZDOT =        1762
526492


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   18180
41769420  
00016717  00000-0  10270-3 0  9053
2 25544  51
6376 317
7476 0003645 242
3951 117
6832 15
53988752 40419


Satellite: ISS
Catalog Number: 25544
Epoch time:      18180
41769420   =   yrday
fracday
Element set:     905
Inclination:       51
6376  deg
RA of node:       317
7476  deg
Eccentricity:     
0003645     
Arg of perigee:   242
3951  deg
Mean anomaly:     117
6832  deg
Mean motion:   15
53988752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4041
Checksum:              326


Coasting Arc #7 (Orbit 4056)
---------------------------------------

Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -21889
76                 A    =         6781792
80  meter
 Y    =        5203688
85  meter          E    =           
0005872
 Z    =        4345042
19                 I    =           51
35126
 XDOT =      -6252
042908                 Wp   =           74
47614
 YDOT =       2834
166432  meter/sec      RA   =          312
13264  deg
 ZDOT =      -3420
327754                 TA   =           50
37222
                                          MA   =           50
32041
                                          Ha   =            220
120  n
mi
                                          Hp   =            216
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -71816
78                 X    =         -101182
88
 Y    =       17072469
97  feet           Y    =         5203000
05  meter
 Z    =       14255387
77                 Z    =         4344744
06
 XDOT =     -20511
951799                 XDOT =       -6266
656724
 YDOT =       9298
446299  feet/sec       YDOT =        2764
170581  meter/sec
 ZDOT =     -11221
547750                 ZDOT =       -3450
732724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15166319
00                 X    =         4622694
03
 Y    =        7843386
39  feet           Y    =         2390664
17  meter
 Z    =       14253228
64                 Z    =         4344384
09
 XDOT =       -339
167541                 XDOT =        -103
378267
 YDOT =      21328
181310  feet/sec       YDOT =        6500
829663  meter/sec
 ZDOT =     -11358
002813                 ZDOT =       -3461
919258


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   18181
44661943  
00016717  00000-0  10270-3 0  9069
2 25544  51
6371 312
6198 0003776 246
6820 113
3935 15
53966319 40575


Satellite: ISS
Catalog Number: 25544
Epoch time:      18181
44661943   =   yrday
fracday
Element set:     906
Inclination:       51
6371  deg
RA of node:       312
6198  deg
Eccentricity:     
0003776     
Arg of perigee:   246
6820  deg
Mean anomaly:     113
3935  deg
Mean motion:   15
53966319  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4057
Checksum:              328


Coasting Arc #8 (Orbit 4071)
---------------------------------------

Vector Time (GMT): 2018/182/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1230181
34                 A    =         6785382
93  meter
 Y    =       -5859028
28  meter          E    =           
0001087
 Z    =       -3195034
87                 I    =           51
34424
 XDOT =       5833
882698                 Wp   =          109
81869
 YDOT =      -1378
383845  meter/sec      RA   =          307
12770  deg
 ZDOT =       4774
849673                 TA   =          213
10206
                                          MA   =          213
10887
                                          Ha   =            220
044  n
mi
                                          Hp   =            216
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4036028
03                 X    =         1311126
76
 Y    =      -19222533
74  feet           Y    =        -5844818
52  meter
 Z    =      -10482397
85                 Z    =        -3188863
35
 XDOT =      19140
035097                 XDOT =        5825
669189
 YDOT =      -4522
256708  feet/sec       YDOT =       -1313
191920  meter/sec
 ZDOT =      15665
517300                 ZDOT =        4803
168145

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15519839
43                 X    =        -4730447
06
 Y    =      -12063459
30  feet           Y    =        -3676942
40  meter
 Z    =      -10453876
02                 Z    =        -3186341
41
 XDOT =       3335
761664                 XDOT =        1016
740155
 YDOT =     -17974
038800  feet/sec       YDOT =       -5478
487026  meter/sec
 ZDOT =      15792
404128                 ZDOT =        4813
524778


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   18182
41123175  
00016717  00000-0  10270-3 0  9078
2 25544  51
6390 307
8119 0003666 250
1660 109
9097 15
54005430 40721


Satellite: ISS
Catalog Number: 25544
Epoch time:      18182
41123175   =   yrday
fracday
Element set:     907
Inclination:       51
6390  deg
RA of node:       307
8119  deg
Eccentricity:     
0003666     
Arg of perigee:   250
1660  deg
Mean anomaly:     109
9097  deg
Mean motion:   15
54005430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4072
Checksum:              293


Coasting Arc #9 (Orbit 4087)
---------------------------------------

Vector Time (GMT): 2018/183/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2256078
49                 A    =         6788459
06  meter
 Y    =        6163223
71  meter          E    =           
0011384
 Z    =        1708954
06                 I    =           51
33408
 XDOT =      -5159
040978                 Wp   =          127
61903
 YDOT =       -311
798757  meter/sec      RA   =          302
13130  deg
 ZDOT =      -5667
101547                 TA   =           33
55326
                                          MA   =           33
48121
                                          Ha   =            219
935  n
mi
                                          Hp   =            216
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7401832
33                 X    =        -2333130
76
 Y    =       20220550
22  feet           Y    =         6137563
65  meter
 Z    =        5606804
66                 Z    =         1697808
56
 XDOT =     -16925
987461                 XDOT =       -5127
643514
 YDOT =      -1022
961801  feet/sec       YDOT =        -369
314475  meter/sec
 ZDOT =     -18592
852843                 ZDOT =       -5692
085824

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15231451
15                 X    =         4642546
31
 Y    =       15239021
29  feet           Y    =         4644853
69  meter
 Z    =        5556001
92                 Z    =         1693469
39
 XDOT =      -6870
873424                 XDOT =       -2094
242220
 YDOT =      13710
061943  feet/sec       YDOT =        4178
826880  meter/sec
 ZDOT =     -18704
560888                 ZDOT =       -5701
150159


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   18183
44014635  
00016717  00000-0  10270-3 0  9083
2 25544  51
6376 302
6837 0003688 255
4590 104
6154 15
54010291 40883


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
44014635   =   yrday
fracday
Element set:     908
Inclination:       51
6376  deg
RA of node:       302
6837  deg
Eccentricity:     
0003688     
Arg of perigee:   255
4590  deg
Mean anomaly:     104
6154  deg
Mean motion:   15
54010291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4088
Checksum:              310


Coasting Arc #10 (Orbit 4088)
---------------------------------------

Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1688818
69                 A    =         6787599
98  meter
 Y    =       -6174164
24  meter          E    =           
0003517
 Z    =       -2252118
11                 I    =           51
33245
 XDOT =       5399
805973                 Wp   =            8
21566
 YDOT =       -497
627034  meter/sec      RA   =          301
65066  deg
 ZDOT =       5417
915091                 TA   =          326
62857
                                          MA   =          326
65074
                                          Ha   =            219
957  n
mi
                                          Hp   =            216
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5540743
74                 X    =         1768673
83
 Y    =      -20256444
36  feet           Y    =        -6154831
94  meter
 Z    =       -7388838
95                 Z    =        -2243721
31
 XDOT =      17715
898862                 XDOT =        5378
652235
 YDOT =      -1632
634625  feet/sec       YDOT =        -437
361601  meter/sec
 ZDOT =      17775
311977                 ZDOT =        5444
093690

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20905602
96                 X    =        -6372027
78
 Y    =       -2132303
16  feet           Y    =         -649926
00  meter
 Z    =       -7350331
15                 Z    =        -2240380
94
 XDOT =      -4699
234669                 XDOT =       -1432
326727
 YDOT =     -15554
578934  feet/sec       YDOT =       -4741
035659  meter/sec
 ZDOT =      17892
486574                 ZDOT =        5453
629908


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   18183
50445358  
00016717  00000-0  10270-3 0  9091
2 25544  51
6407 302
3640 0003727 256
1047 103
9691 15
53990362 40890


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
50445358   =   yrday
fracday
Element set:     909
Inclination:       51
6407  deg
RA of node:       302
3640  deg
Eccentricity:     
0003727     
Arg of perigee:   256
1047  deg
Mean anomaly:     103
9691  deg
Mean motion:   15
53990362  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4089
Checksum:              315


Coasting Arc #11 (Orbit 4104)
---------------------------------------

Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2568149
08                 A    =         6789523
81  meter
 Y    =        6245930
01  meter          E    =           
0011130
 Z    =         633525
76                 I    =           51
32181
 XDOT =      -4666
069710                 Wp   =          143
57248
 YDOT =      -1311
088390  meter/sec      RA   =          296
65788  deg
 ZDOT =      -5943
976439                 TA   =           29
55615
                                          MA   =           29
49329
                                          Ha   =            219
868  n
mi
                                          Hp   =            216
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8425685
97                 X    =        -2640879
22
 Y    =       20491896
36  feet           Y    =         6216804
47  meter
 Z    =        2078496
59                 Z    =          620874
74
 XDOT =     -15308
627657                 XDOT =       -4622
189624
 YDOT =      -4301
471097  feet/sec       YDOT =       -1363
021636  meter/sec
 ZDOT =     -19501
235035                 ZDOT =       -5966
535872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21693816
60                 X    =         6612275
30
 Y    =        4530360
89  feet           Y    =         1380854
00  meter
 Z    =        2020965
11                 Z    =          615990
17
 XDOT =      -1110
400373                 XDOT =        -338
450034
 YDOT =      14129
295543  feet/sec       YDOT =        4306
609282  meter/sec
 ZDOT =     -19601
945110                 ZDOT =       -5974
672870


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   18184
53336460  
00016717  00000-0  10270-3 0  9100
2 25544  51
6399 297
2363 0003795 257
4132 102
6596 15
54006778 41057


Satellite: ISS
Catalog Number: 25544
Epoch time:      18184
53336460   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       297
2363  deg
Eccentricity:     
0003795     
Arg of perigee:   257
4132  deg
Mean anomaly:     102
6596  deg
Mean motion:   15
54006778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4105
Checksum:              321


Coasting Arc #12 (Orbit 4120)
---------------------------------------

Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3223651
07                 A    =         6789172
28  meter
 Y    =       -5878817
15  meter          E    =           
0010438
 Z    =        1030685
69                 I    =           51
30809
 XDOT =       3816
735922                 Wp   =           46
93829
 YDOT =       3127
512225  meter/sec      RA   =          291
66581  deg
 ZDOT =       5870
440128                 TA   =          324
28704
                                          MA   =          324
35681
                                          Ha   =            219
821  n
mi
                                          Hp   =            216
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10576283
05                 X    =         3284143
56
 Y    =      -19287457
86  feet           Y    =        -5842429
92  meter
 Z    =        3381514
73                 Z    =         1046491
30
 XDOT =      12522
099482                 XDOT =        3752
964340
 YDOT =      10260
866880  feet/sec       YDOT =        3169
836490  meter/sec
 ZDOT =      19259
974172                 ZDOT =        5888
825724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21012345
31                 X    =        -6404562
85
 Y    =       -6469619
87  feet           Y    =        -1971940
14  meter
 Z    =        3453085
44                 Z    =         1052500
44
 XDOT =       7095
437651                 XDOT =        2162
689396
 YDOT =     -12668
781144  feet/sec       YDOT =       -3861
444493  meter/sec
 ZDOT =      19341
747048                 ZDOT =        5895
364500


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   18185
56227058  
00016717  00000-0  10270-3 0  9117
2 25544  51
6411 292
1081 0003703 263
7767  96
2964 15
54021728 41213


Satellite: ISS
Catalog Number: 25544
Epoch time:      18185
56227058   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       292
1081  deg
Eccentricity:     
0003703     
Arg of perigee:   263
7767  deg
Mean anomaly:      96
2964  deg
Mean motion:   15
54021728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4121
Checksum:              304


Coasting Arc #13 (Orbit 4135)
---------------------------------------

Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3698767
45                 A    =         6786682
72  meter
 Y    =        5052586
33  meter          E    =           
0003152
 Z    =       -2612637
68                 I    =           51
28812
 XDOT =      -2910
172741                 Wp   =          174
19362
 YDOT =      -4818
956646  meter/sec      RA   =          286
66934  deg
 ZDOT =      -5203
029931                 TA   =           35
37607
                                          MA   =           35
35516
                                          Ha   =            219
769  n
mi
                                          Hp   =            216
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12135063
80                 X    =        -3742301
23
 Y    =       16576726
82  feet           Y    =         5010980
98  meter
 Z    =       -8571645
93                 Z    =        -2630710
18
 XDOT =      -9547
810829                 XDOT =       -2830
796157
 YDOT =     -15810
225215  feet/sec       YDOT =       -4851
055931  meter/sec
 ZDOT =     -17070
308171                 ZDOT =       -5216
974071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18805708
61                 X    =         5731979
98
 Y    =        8184610
88  feet           Y    =         2494669
40  meter
 Z    =       -8653220
68                 Z    =        -2637501
66
 XDOT =     -12784
958902                 XDOT =       -3896
855473
 YDOT =      11275
502998  feet/sec       YDOT =        3436
773314  meter/sec
 ZDOT =     -17131
974264                 ZDOT =       -5221
825756


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   18186
52686550  
00016717  00000-0  10270-3 0  9121
2 25544  51
6406 287
3008 0003728 267
4286  92
6439 15
54023823 41367


Satellite: ISS
Catalog Number: 25544
Epoch time:      18186
52686550   =   yrday
fracday
Element set:     912
Inclination:       51
6406  deg
RA of node:       287
3008  deg
Eccentricity:     
0003728     
Arg of perigee:   267
4286  deg
Mean anomaly:      92
6439  deg
Mean motion:   15
54023823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4136
Checksum:              322


Coasting Arc #14 (Orbit 4146)
---------------------------------------

Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2045004
52                 A    =         6783028
76  meter
 Y    =       -5142738
28  meter          E    =           
0002998
 Z    =       -3925116
82                 I    =           51
26596
 XDOT =       4411
852278                 Wp   =          118
97694
 YDOT =      -4814
675331  meter/sec      RA   =          282
98724  deg
 ZDOT =       4010
557196                 TA   =          193
15442
                                          MA   =          193
16224
                                          Ha   =            219
767  n
mi
                                          Hp   =            216
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6709332
40                 X    =        -1968278
96
 Y    =      -16872500
92  feet           Y    =        -5165177
59  meter
 Z    =      -12877679
87                 Z    =        -3934864
80
 XDOT =      14474
580966                 XDOT =        4445
882326
 YDOT =     -15796
178906  feet/sec       YDOT =       -4765
149033  meter/sec
 ZDOT =      13157
996049                 ZDOT =        4032
070575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7934169
24                 X    =        -2418334
78
 Y    =      -16298457
77  feet           Y    =        -4967769
93  meter
 Z    =      -12920537
92                 Z    =        -3938179
96
 XDOT =      11907
769931                 XDOT =        3629
488275
 YDOT =     -16302
201710  feet/sec       YDOT =       -4968
911081  meter/sec
 ZDOT =      13254
918487                 ZDOT =        4040
099155


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   18187
23423223  
00016717  00000-0  10270-3 0  9137
2 25544  51
6370 283
7761 0003776 276
6270  83
4453 15
54034982 41475


Satellite: ISS
Catalog Number: 25544
Epoch time:      18187
23423223   =   yrday
fracday
Element set:     913
Inclination:       51
6370  deg
RA of node:       283
7761  deg
Eccentricity:     
0003776     
Arg of perigee:   276
6270  deg
Mean anomaly:      83
4453  deg
Mean motion:   15
54034982  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4147
Checksum:              316


Coasting Arc #15 (Orbit 4162)
---------------------------------------

Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1249659
06                 A    =         6786594
14  meter
 Y    =        6135799
72  meter          E    =           
0009560
 Z    =        2605464
69                 I    =           51
27268
 XDOT =      -4658
518960                 Wp   =          103
18155
 YDOT =       3164
923264  meter/sec      RA   =          277
98035  deg
 ZDOT =      -5204
923911                 TA   =           47
31785
                                          MA   =           47
23735
                                          Ha   =            219
685  n
mi
                                          Hp   =            216
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4099931
31                 X    =         1168298
04
 Y    =       20130576
52  feet           Y    =         6149319
11  meter
 Z    =        8548112
50                 Z    =         2611338
07
 XDOT =     -15283
854855                 XDOT =       -4668
281048
 YDOT =      10383
606509  feet/sec       YDOT =        3112
774407  meter/sec
 ZDOT =     -17076
522017                 ZDOT =       -5227
576746

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5957428
20                 X    =         1815824
11
 Y    =       19650032
29  feet           Y    =         5989329
84  meter
 Z    =        8573508
94                 Z    =         2613205
53
 XDOT =     -12670
444076                 XDOT =       -3861
951354
 YDOT =      11356
456663  feet/sec       YDOT =        3461
447991  meter/sec
 ZDOT =     -17178
296695                 ZDOT =       -5235
944833


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   18188
26312658  
00016717  00000-0  10270-3 0  9141
2 25544  51
6379 278
6474 0004044 282
4015  77
6685 15
54073795 41634


Satellite: ISS
Catalog Number: 25544
Epoch time:      18188
26312658   =   yrday
fracday
Element set:     914
Inclination:       51
6379  deg
RA of node:       278
6474  deg
Eccentricity:     
0004044     
Arg of perigee:   282
4015  deg
Mean anomaly:      77
6685  deg
Mean motion:   15
54073795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4163
Checksum:              339


Coasting Arc #16 (Orbit 4177)
---------------------------------------

Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -486010
87                 A    =         6789123
03  meter
 Y    =       -6686138
58  meter          E    =           
0008764
 Z    =       -1038915
99                 I    =           51
27654
 XDOT =       4775
830753                 Wp   =           15
33324
 YDOT =      -1255
687336  meter/sec      RA   =          272
98068  deg
 ZDOT =       5866
720173                 TA   =          333
34621
                                          MA   =          333
39124
                                          Ha   =            219
836  n
mi
                                          Hp   =            216
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1594523
84                 X    =         -406162
00
 Y    =      -21936150
21  feet           Y    =        -6691126
92  meter
 Z    =       -3408517
03                 Z    =        -1041083
67
 XDOT =      15668
736067                 XDOT =        4761
019820
 YDOT =      -4119
709107  feet/sec       YDOT =       -1202
364165  meter/sec
 ZDOT =      19247
769596                 ZDOT =        5889
883390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4043345
79                 X    =        -1232411
80
 Y    =      -21617788
66  feet           Y    =        -6589101
98  meter
 Z    =       -3417272
14                 Z    =        -1041584
55
 XDOT =      13398
762839                 XDOT =        4083
942913
 YDOT =      -5554
934278  feet/sec       YDOT =       -1693
143968  meter/sec
 ZDOT =      19351
555009                 ZDOT =        5898
353967


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   18189
22771458  
00016717  00000-0  10270-3 0  9156
2 25544  51
6371 273
8385 0003778 283
9669  76
1064 15
54040511 41789


Satellite: ISS
Catalog Number: 25544
Epoch time:      18189
22771458   =   yrday
fracday
Element set:     915
Inclination:       51
6371  deg
RA of node:       273
8385  deg
Eccentricity:     
0003778     
Arg of perigee:   283
9669  deg
Mean anomaly:      76
1064  deg
Mean motion:   15
54040511  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4178
Checksum:              339


Coasting Arc #17 (Orbit 4193)
---------------------------------------

Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -287902
02                 A    =         6789263
49  meter
 Y    =        6747240
21  meter          E    =           
0007532
 Z    =        -654557
75                 I    =           51
27664
 XDOT =      -4789
915763                 Wp   =          153
02567
 YDOT =       -776
995495  meter/sec      RA   =          267
98608  deg
 ZDOT =      -5936
055072                 TA   =           34
07729
                                          MA   =           34
02895
                                          Ha   =            219
922  n
mi
                                          Hp   =            216
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -944560
43                 X    =         -360150
62
 Y    =       22136614
86  feet           Y    =         6743616
81  meter
 Z    =       -2147499
18                 Z    =         -656130
88
 XDOT =     -15714
946730                 XDOT =       -4752
036964
 YDOT =      -2549
197819  feet/sec       YDOT =        -830
347071  meter/sec
 ZDOT =     -19475
246299                 ZDOT =       -5959
230929

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1959751
48                 X    =          597332
25
 Y    =       22069140
66  feet           Y    =         6726674
07  meter
 Z    =       -2155474
27                 Z    =         -656988
56
 XDOT =     -14175
610321                 XDOT =       -4320
726026
 YDOT =       -642
741917  feet/sec       YDOT =        -195
907736  meter/sec
 ZDOT =     -19578
808047                 ZDOT =       -5967
620693


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   18190
25660264  
00016717  00000-0  10270-3 0  9164
2 25544  51
6370 268
7100 0003758 291
8007  68
2746 15
54087488 41949


Satellite: ISS
Catalog Number: 25544
Epoch time:      18190
25660264   =   yrday
fracday
Element set:     916
Inclination:       51
6370  deg
RA of node:       268
7100  deg
Eccentricity:     
0003758     
Arg of perigee:   291
8007  deg
Mean anomaly:      68
2746  deg
Mean motion:   15
54087488  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4194
Checksum:              327


Coasting Arc #18 (Orbit 4209)
---------------------------------------

Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1052435
50                 A    =         6787374
59  meter
 Y    =       -6305432
33  meter          E    =           
0011227
 Z    =        2262250
63                 I    =           51
27131
 XDOT =       4705
110470                 Wp   =           60
46817
 YDOT =       2730
708183  meter/sec      RA   =          262
98845  deg
 ZDOT =       5407
394313                 TA   =          324
84970
                                          MA   =          324
92372
                                          Ha   =            219
948  n
mi
                                          Hp   =            216
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3452872
37                 X    =         1111877
56
 Y    =      -20687113
94  feet           Y    =        -6293331
25  meter
 Z    =        7422082
13                 Z    =         2267506
42
 XDOT =      15436
714141                 XDOT =        4647
959024
 YDOT =       8959
016350  feet/sec       YDOT =        2783
003611  meter/sec
 ZDOT =      17740
794990                 ZDOT =        5430
111674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         320725
98                 X    =           97757
28
 Y    =      -20962196
48  feet           Y    =        -6389277
49  meter
 Z    =        7446460
07                 Z    =         2269681
03
 XDOT =      14942
490262                 XDOT =        4554
471032
 YDOT =       6583
951093  feet/sec       YDOT =        2006
788293  meter/sec
 ZDOT =      17842
045720                 ZDOT =        5438
255536


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   18191
28549031  
00016717  00000-0  10270-3 0  9177
2 25544  51
6361 263
5812 0003639 290
6620  69
4142 15
54050385 42106


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
28549031   =   yrday
fracday
Element set:     917
Inclination:       51
6361  deg
RA of node:       263
5812  deg
Eccentricity:     
0003639     
Arg of perigee:   290
6620  deg
Mean anomaly:      69
4142  deg
Mean motion:   15
54050385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4210
Checksum:              297
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