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

 
Date: May 17th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15478 5032 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


137/14:37:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 213 4

138/21:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 4

140/09:04:46 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 4

142/00:19:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 5

144/09:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 6

146/20:57:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

148/06:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 8

Coasting Arc #1 (Orbit 3358)
---------------------------------------

Vector Time (GMT): 2018/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6754335
36                 A    =         6789498
94  meter
 Y    =          39260
89  meter          E    =           
0016425
 Z    =         619984
16                 I    =           51
68211
 XDOT =        530
876263                 Wp   =           60
12587
 YDOT =      -4778
523106  meter/sec      RA   =          175
50724  deg
 ZDOT =       5975
575213                 TA   =          306
56434
                                          MA   =          306
71541
                                          Ha   =            222
623  n
mi
                                          Hp   =            213
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22159892
91                 X    =        -6757284
00
 Y    =         128808
69  feet           Y    =          -36287
28  meter
 Z    =        2034068
76                 Z    =          587166
11
 XDOT =       1741
720024                 XDOT =         555
244782
 YDOT =     -15677
569245  feet/sec       YDOT =       -4772
450781  meter/sec
 ZDOT =      19604
905555                 ZDOT =        5978
212825

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13154403
58                 X    =        -4009462
21
 Y    =       17849763
33  feet           Y    =         5440607
86  meter
 Z    =        1887457
77                 Z    =          575297
13
 XDOT =     -10299
597319                 XDOT =       -3139
317263
 YDOT =      -9705
999921  feet/sec       YDOT =       -2958
388776  meter/sec
 ZDOT =      19617
250105                 ZDOT =        5979
337832


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   18136
56320018  
00016717  00000-0  10270-3 0  9001
2 25544  51
6384 176
3617 0003998  88
6223 271
5387 15
54023084 33593


Satellite: ISS
Catalog Number: 25544
Epoch time:      18136
56320018   =   yrday
fracday
Element set:     900
Inclination:       51
6384  deg
RA of node:       176
3617  deg
Eccentricity:     
0003998     
Arg of perigee:    88
6223  deg
Mean anomaly:     271
5387  deg
Mean motion:   15
54023084  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3359
Checksum:              318


Coasting Arc #2 (Orbit 3373)
---------------------------------------

Vector Time (GMT): 2018/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6347951
17                 A    =         6787358
34  meter
 Y    =         763915
92  meter          E    =           
0009370
 Z    =       -2276024
17                 I    =           51
70860
 XDOT =      -2517
709081                 Wp   =          120
48951
 YDOT =       4774
400427  meter/sec      RA   =          170
53934  deg
 ZDOT =      -5440
884706                 TA   =           84
80576
                                          MA   =           84
69884
                                          Ha   =            222
576  n
mi
                                          Hp   =            213
342

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20826611
47                 X    =         6349992
96
 Y    =        2506285
84  feet           Y    =          834914
75  meter
 Z    =       -7467270
91                 Z    =        -2245182
49
 XDOT =      -8260
200398                 XDOT =       -2544
481245
 YDOT =      15664
043395  feet/sec       YDOT =        4746
096580  meter/sec
 ZDOT =     -17850
671607                 ZDOT =       -5453
179557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14226313
24                 X    =         4336180
28
 Y    =      -15481566
52  feet           Y    =        -4718781
48  meter
 Z    =       -7329560
57                 Z    =        -2234050
06
 XDOT =       6829
340825                 XDOT =        2081
583083
 YDOT =      14719
331873  feet/sec       YDOT =        4486
452355  meter/sec
 ZDOT =     -17906
170386                 ZDOT =       -5457
800734


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   18137
52776996  
00016717  00000-0  10270-3 0  9019
2 25544  51
6388 171
5536 0003983  94
2653 265
8955 15
54077042 33745


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
52776996   =   yrday
fracday
Element set:     901
Inclination:       51
6388  deg
RA of node:       171
5536  deg
Eccentricity:     
0003983     
Arg of perigee:    94
2653  deg
Mean anomaly:     265
8955  deg
Mean motion:   15
54077042  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3374
Checksum:              348


Coasting Arc #3 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2018/137/14:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         146473
03                 A    =         6777713
30  meter
 Y    =       -4254702
70  meter          E    =           
0006724
 Z    =        5268257
07                 I    =           51
67636
 XDOT =       7599
958445                 Wp   =           80
05190
 YDOT =       -713
670683  meter/sec      RA   =          169
96890  deg
 ZDOT =       -785
680509                 TA   =           17
45857
                                          MA   =           17
43547
                                          Ha   =            222
514  n
mi
                                          Hp   =            213
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         480554
55                 X    =          168448
59
 Y    =      -13958998
37  feet           Y    =        -4252942
46  meter
 Z    =       17284307
99                 Z    =         5269021
50
 XDOT =      24934
246866                 XDOT =        7611
190539
 YDOT =      -2341
439249  feet/sec       YDOT =        -628
619826  meter/sec
 ZDOT =      -2577
691960                 ZDOT =        -748
734777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13951710
56                 X    =        -4252481
38
 Y    =         546647
01  feet           Y    =          166618
01  meter
 Z    =       17288227
79                 Z    =         5269451
83
 XDOT =      -3927
222767                 XDOT =       -1197
017499
 YDOT =     -23727
027287  feet/sec       YDOT =       -7231
997917  meter/sec
 ZDOT =      -2412
530461                 ZDOT =        -735
339285


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   18137
65637892  
00016717  00000-0  10270-3 0  9025
2 25544  51
6352 170
9128 0003860  93
5508 266
6086 15
54063280 33766


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
65637892   =   yrday
fracday
Element set:     902
Inclination:       51
6352  deg
RA of node:       170
9128  deg
Eccentricity:     
0003860     
Arg of perigee:    93
5508  deg
Mean anomaly:     266
6086  deg
Mean motion:   15
54063280  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              325


Coasting Arc #4 (Orbit 3390)
---------------------------------------

Vector Time (GMT): 2018/138/14:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1871517
17                 A    =         6779788
69  meter
 Y    =        4424094
34  meter          E    =           
0015286
 Z    =       -4798830
63                 I    =           51
71575
 XDOT =      -7192
203500                 Wp   =          105
64595
 YDOT =       -207
799746  meter/sec      RA   =          164
97641  deg
 ZDOT =       2616
267782                 TA   =          190
14591
                                          MA   =          190
17680
                                          Ha   =            222
551  n
mi
                                          Hp   =            213
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6140148
18                 X    =        -1897539
09
 Y    =       14514745
20  feet           Y    =         4403020
82  meter
 Z    =      -15744194
99                 Z    =        -4807984
58
 XDOT =     -23596
468175                 XDOT =       -7202
053860
 YDOT =       -681
757698  feet/sec       YDOT =        -288
283303  meter/sec
 ZDOT =       8583
555715                 ZDOT =        2581
306251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14961971
44                 X    =         4560408
90
 Y    =        4817905
89  feet           Y    =         1468497
71  meter
 Z    =      -15785630
09                 Z    =        -4811460
05
 XDOT =       1623
963256                 XDOT =         494
984000
 YDOT =      22537
240596  feet/sec       YDOT =        6869
350934  meter/sec
 ZDOT =       8427
341720                 ZDOT =        2568
653756


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   18138
62094793  
00016717  00000-0  10270-3 0  9031
2 25544  51
6355 166
1050 0003906  96
3630 263
7967 15
54044157 33913


Satellite: ISS
Catalog Number: 25544
Epoch time:      18138
62094793   =   yrday
fracday
Element set:     903
Inclination:       51
6355  deg
RA of node:       166
1050  deg
Eccentricity:     
0003906     
Arg of perigee:    96
3630  deg
Mean anomaly:     263
7967  deg
Mean motion:   15
54044157  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3391
Checksum:              318


Coasting Arc #5 (Orbit 3394)
---------------------------------------

Vector Time (GMT): 2018/138/21:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5870065
44                 A    =         6788331
47  meter
 Y    =        3017372
99  meter          E    =           
0010330
 Z    =       -1578529
67                 I    =           51
75728
 XDOT =      -3446
790631                 Wp   =           56
04977
 YDOT =      -3713
473591  meter/sec      RA   =          163
66047  deg
 ZDOT =       5751
806668                 TA   =          286
72295
                                          MA   =          286
83629
                                          Ha   =            222
374  n
mi
                                          Hp   =            213
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19258744
88                 X    =        -5895702
52
 Y    =        9899517
68  feet           Y    =         2951586
72  meter
 Z    =       -5178903
11                 Z    =        -1607106
57
 XDOT =     -11308
368212                 XDOT =       -3432
948860
 YDOT =     -12183
312305  feet/sec       YDOT =       -3751
941263  meter/sec
 ZDOT =      18870
756784                 ZDOT =        5735
096389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17070618
13                 X    =         5203124
40
 Y    =      -13272179
51  feet           Y    =        -4045360
32  meter
 Z    =       -5306975
57                 Z    =        -1617566
15
 XDOT =      12514
188883                 XDOT =        3814
324772
 YDOT =       8621
494663  feet/sec       YDOT =        2627
831573  meter/sec
 ZDOT =      18796
520088                 ZDOT =        5729
179323


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   18138
87816585  
00016717  00000-0  10270-3 0  9040
2 25544  51
6396 164
8239 0003685  96
6163 263
5409 15
54088133 33955


Satellite: ISS
Catalog Number: 25544
Epoch time:      18138
87816585   =   yrday
fracday
Element set:     904
Inclination:       51
6396  deg
RA of node:       164
8239  deg
Eccentricity:     
0003685     
Arg of perigee:    96
6163  deg
Mean anomaly:     263
5409  deg
Mean motion:   15
54088133  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3395
Checksum:              349


Coasting Arc #6 (Orbit 3410)
---------------------------------------

Vector Time (GMT): 2018/139/21:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6355725
62                 A    =         6789577
67  meter
 Y    =       -2366962
82  meter          E    =           
0015212
 Z    =        -131459
40                 I    =           51
79276
 XDOT =       1555
093059                 Wp   =          127
81078
 YDOT =       4483
417124  meter/sec      RA   =          158
69976  deg
 ZDOT =      -6024
502979                 TA   =           53
60244
                                          MA   =           53
46222
                                          Ha   =            222
518  n
mi
                                          Hp   =            213
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20852118
19                 X    =         6382359
84
 Y    =       -7765626
06  feet           Y    =        -2295739
79  meter
 Z    =        -431297
25                 Z    =         -100520
93
 XDOT =       5102
011349                 XDOT =        1534
106659
 YDOT =      14709
373765  feet/sec       YDOT =        4500
690562  meter/sec
 ZDOT =     -19765
429722                 ZDOT =       -6016
999327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18866076
20                 X    =        -5750380
03
 Y    =       11802003
20  feet           Y    =         3597250
58  meter
 Z    =        -292724
32                 Z    =          -89222
37
 XDOT =      -7223
692752                 XDOT =       -2201
781551
 YDOT =     -11978
803407  feet/sec       YDOT =       -3651
139278  meter/sec
 ZDOT =     -19732
426185                 ZDOT =       -6014
443501


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   18139
90703452  
00016717  00000-0  10270-3 0  9054
2 25544  51
6402 159
6954 0003761 101
7764 258
3810 15
54042039 34111


Satellite: ISS
Catalog Number: 25544
Epoch time:      18139
90703452   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       159
6954  deg
Eccentricity:     
0003761     
Arg of perigee:   101
7764  deg
Mean anomaly:     258
3810  deg
Mean motion:   15
54042039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3411
Checksum:              299


Coasting Arc #7 (Orbit 3418)
---------------------------------------

Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1530636
70                 A    =         6780133
50  meter
 Y    =       -4681113
91  meter          E    =           
0011140
 Z    =        4651733
84                 I    =           51
77631
 XDOT =       7068
716332                 Wp   =           76
87975
 YDOT =       -603
601745  meter/sec      RA   =          156
17073  deg
 ZDOT =      -2924
996700                 TA   =           42
18821
                                          MA   =           42
10253
                                          Ha   =            222
299  n
mi
                                          Hp   =            213
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5021773
94                 X    =         1560272
71
 Y    =      -15357985
28  feet           Y    =        -4663832
04  meter
 Z    =       15261593
97                 Z    =         4659240
67
 XDOT =      23191
326548                 XDOT =        7089
148735
 YDOT =      -1980
320686  feet/sec       YDOT =        -524
439952  meter/sec
 ZDOT =      -9596
445865                 ZDOT =       -2890
609674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1257998
12                 X    =          383437
83
 Y    =      -16076716
54  feet           Y    =        -4900183
20  meter
 Z    =       15295711
88                 Z    =         4662132
98
 XDOT =      21003
464872                 XDOT =        6401
856093
 YDOT =      -7366
437124  feet/sec       YDOT =       -2245
290035  meter/sec
 ZDOT =      -9442
657327                 ZDOT =       -2878
121953


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   18140
42146430  
00016717  00000-0  10270-3 0  9061
2 25544  51
6390 157
1285 0003635 104
9329 255
2226 15
54114473 34196


Satellite: ISS
Catalog Number: 25544
Epoch time:      18140
42146430   =   yrday
fracday
Element set:     906
Inclination:       51
6390  deg
RA of node:       157
1285  deg
Eccentricity:     
0003635     
Arg of perigee:   104
9329  deg
Mean anomaly:     255
2226  deg
Mean motion:   15
54114473  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3419
Checksum:              291


Coasting Arc #8 (Orbit 3433)
---------------------------------------

Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3001272
95                 A    =         6783772
52  meter
 Y    =        4897951
83  meter          E    =           
0009388
 Z    =       -3618513
98                 I    =           51
81731
 XDOT =      -6226
021489                 Wp   =          103
31269
 YDOT =       -549
839051  meter/sec      RA   =          151
19410  deg
 ZDOT =       4427
293083                 TA   =          213
99431
                                          MA   =          214
05449
                                          Ha   =            222
419  n
mi
                                          Hp   =            213
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9846696
03                 X    =        -3038243
28
 Y    =       16069395
76  feet           Y    =         4864183
11  meter
 Z    =      -11871765
02                 Z    =        -3633182
54
 XDOT =     -20426
579689                 XDOT =       -6240
915783
 YDOT =      -1803
933893  feet/sec       YDOT =        -619
546347  meter/sec
 ZDOT =      14525
239775                 ZDOT =        4397
012978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5503254
90                 X    =        -1677392
09
 Y    =       17981146
38  feet           Y    =         5480653
42  meter
 Z    =      -11937933
99                 Z    =        -3638682
28
 XDOT =     -19021
706537                 XDOT =       -5797
816153
 YDOT =       3715
596493  feet/sec       YDOT =        1132
513811  meter/sec
 ZDOT =      14389
929146                 ZDOT =        4386
050404


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   18141
38602568  
00016717  00000-0  10270-3 0  9077
2 25544  51
6381 152
3212 0003949 108
5350 251
6232 15
54110973 34340


Satellite: ISS
Catalog Number: 25544
Epoch time:      18141
38602568   =   yrday
fracday
Element set:     907
Inclination:       51
6381  deg
RA of node:       152
3212  deg
Eccentricity:     
0003949     
Arg of perigee:   108
5350  deg
Mean anomaly:     251
6232  deg
Mean motion:   15
54110973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3434
Checksum:              291


Coasting Arc #9 (Orbit 3443)
---------------------------------------

Vector Time (GMT): 2018/142/00:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2044966
31                 A    =         6777481
27  meter
 Y    =        3669717
89  meter          E    =           
0018518
 Z    =       -5334368
85                 I    =           51
81164
 XDOT =      -6568
541256                 Wp   =           95
27836
 YDOT =       3926
407165  meter/sec      RA   =          148
05931  deg
 ZDOT =        181
916282                 TA   =          176
46087
                                          MA   =          176
44775
                                          Ha   =            222
409  n
mi
                                          Hp   =            213
457

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6709207
04                 X    =         2029690
11
 Y    =       12039756
87  feet           Y    =         3692501
06  meter
 Z    =      -17501210
12                 Z    =        -5324471
95
 XDOT =     -21550
332204                 XDOT =       -6612
842882
 YDOT =      12881
913271  feet/sec       YDOT =        3852
705495  meter/sec
 ZDOT =        596
838197                 ZDOT =         149
901209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13819257
72                 X    =        -4212109
75
 Y    =         727191
12  feet           Y    =          221647
85  meter
 Z    =      -17457401
57                 Z    =        -5321016
00
 XDOT =      -1841
706948                 XDOT =        -561
352278
 YDOT =     -24030
680240  feet/sec       YDOT =       -7324
551337  meter/sec
 ZDOT =        453
220539                 ZDOT =         138
141620


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   18142
02906365  
00016717  00000-0  10270-3 0  9082
2 25544  51
6357 149
1135 0003818 109
8296 250
3269 15
54089779 34445


Satellite: ISS
Catalog Number: 25544
Epoch time:      18142
02906365   =   yrday
fracday
Element set:     908
Inclination:       51
6357  deg
RA of node:       149
1135  deg
Eccentricity:     
0003818     
Arg of perigee:   109
8296  deg
Mean anomaly:     250
3269  deg
Mean motion:   15
54089779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3444
Checksum:              331


Coasting Arc #10 (Orbit 3459)
---------------------------------------

Vector Time (GMT): 2018/143/00:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -491426
57                 A    =         6778900
29  meter
 Y    =       -4544230
66  meter          E    =           
0008659
 Z    =        4999436
43                 I    =           51
84414
 XDOT =       6740
252745                 Wp   =           78
33599
 YDOT =      -3021
872137  meter/sec      RA   =          143
07356  deg
 ZDOT =      -2079
436859                 TA   =           31
84828
                                          MA   =           31
79595
                                          Ha   =            222
453  n
mi
                                          Hp   =            213
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1612291
90                 X    =         -464859
92
 Y    =      -14908893
23  feet           Y    =        -4549577
84  meter
 Z    =       16402350
49                 Z    =         4997113
53
 XDOT =      22113
690107                 XDOT =        6783
644038
 YDOT =      -9914
278666  feet/sec       YDOT =       -2946
255266  meter/sec
 ZDOT =      -6822
299405                 ZDOT =       -2046
589701

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14191746
75                 X    =         4325644
41
 Y    =        4877652
70  feet           Y    =         1486708
54  meter
 Z    =       16392513
91                 Z    =         4996438
24
 XDOT =       -256
854645                 XDOT =         -78
289296
 YDOT =      23232
804864  feet/sec       YDOT =        7081
358923  meter/sec
 ZDOT =      -6675
052103                 ZDOT =       -2034
555881


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   18143
05792176  
00016717  00000-0  10270-3 0  9090
2 25544  51
6361 143
9843 0003780 113
4318 246
7233 15
54065601 34608


Satellite: ISS
Catalog Number: 25544
Epoch time:      18143
05792176   =   yrday
fracday
Element set:     909
Inclination:       51
6361  deg
RA of node:       143
9843  deg
Eccentricity:     
0003780     
Arg of perigee:   113
4318  deg
Mean anomaly:     246
7233  deg
Mean motion:   15
54065601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3460
Checksum:              302


Coasting Arc #11 (Orbit 3474)
---------------------------------------

Vector Time (GMT): 2018/144/00:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -956631
44                 A    =         6782004
06  meter
 Y    =        5264694
55  meter          E    =           
0011788
 Z    =       -4179440
23                 I    =           51
88042
 XDOT =      -6425
088269                 Wp   =          112
52514
 YDOT =       1808
837006  meter/sec      RA   =          138
09598  deg
 ZDOT =       3753
210734                 TA   =          195
99120
                                          MA   =          196
02845
                                          Ha   =            222
414  n
mi
                                          Hp   =            213
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3138554
60                 X    =         -995129
95
 Y    =       17272619
93  feet           Y    =         5253781
77  meter
 Z    =      -13712074
24                 Z    =        -4184180
52
 XDOT =     -21079
685922                 XDOT =       -6463
068895
 YDOT =       5934
504612  feet/sec       YDOT =        1736
774717  meter/sec
 ZDOT =      12313
683509                 ZDOT =        3721
907499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14440983
69                 X    =        -4401611
83
 Y    =       -9952508
32  feet           Y    =        -3033524
54  meter
 Z    =      -13733916
87                 Z    =        -4186097
86
 XDOT =       2673
614132                 XDOT =         814
917587
 YDOT =     -20659
828351  feet/sec       YDOT =       -6297
115682  meter/sec
 ZDOT =      12173
471824                 ZDOT =        3710
474212


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   18144
02247281  
00016717  00000-0  10270-3 0  9102
2 25544  51
6359 139
1756 0003987 117
0849 243
0711 15
54097960 34753


Satellite: ISS
Catalog Number: 25544
Epoch time:      18144
02247281   =   yrday
fracday
Element set:     910
Inclination:       51
6359  deg
RA of node:       139
1756  deg
Eccentricity:     
0003987     
Arg of perigee:   117
0849  deg
Mean anomaly:     243
0711  deg
Mean motion:   15
54097960  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3475
Checksum:              319


Coasting Arc #12 (Orbit 3480)
---------------------------------------

Vector Time (GMT): 2018/144/09:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4275458
87                 A    =         6778664
00  meter
 Y    =        1424087
72  meter          E    =           
0016131
 Z    =       -5078094
82                 I    =           51
88137
 XDOT =      -4245
209254                 Wp   =           85
29528
 YDOT =       6090
944326  meter/sec      RA   =          136
27297  deg
 ZDOT =      -1869
910697                 TA   =          166
64037
                                          MA   =          166
59761
                                          Ha   =            222
405  n
mi
                                          Hp   =            213
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14027096
03                 X    =         4283883
48
 Y    =        4672203
81  feet           Y    =         1471946
17  meter
 Z    =      -16660416
08                 Z    =        -5057305
43
 XDOT =     -13927
851884                 XDOT =       -4303
921233
 YDOT =      19983
413143  feet/sec       YDOT =        6043
143273  meter/sec
 ZDOT =      -6134
877615                 ZDOT =       -1890
674962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14871271
02                 X    =         4532763
41
 Y    =        -719561
40  feet           Y    =         -219322
31  meter
 Z    =      -16567616
15                 Z    =        -5049809
40
 XDOT =      -5833
652849                 XDOT =       -1778
097388
 YDOT =      22553
303622  feet/sec       YDOT =        6874
246944  meter/sec
 ZDOT =      -6228
487859                 ZDOT =       -1898
443099


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   18144
40829230  
00016717  00000-0  10270-3 0  9115
2 25544  51
6392 137
2557 0003883 117
0076 243
1474 15
54089317 34816


Satellite: ISS
Catalog Number: 25544
Epoch time:      18144
40829230   =   yrday
fracday
Element set:     911
Inclination:       51
6392  deg
RA of node:       137
2557  deg
Eccentricity:     
0003883     
Arg of perigee:   117
0076  deg
Mean anomaly:     243
1474  deg
Mean motion:   15
54089317  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3481
Checksum:              305


Coasting Arc #13 (Orbit 3496)
---------------------------------------

Vector Time (GMT): 2018/145/09:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3116200
79                 A    =         6777397
83  meter
 Y    =       -2785390
60  meter          E    =           
0006178
 Z    =        5330106
87                 I    =           51
89927
 XDOT =       5083
411203                 Wp   =          108
27848
 YDOT =      -5748
059918  meter/sec      RA   =          131
29134  deg
 ZDOT =        -33
688412                 TA   =          342
03026
                                          MA   =          342
05209
                                          Ha   =            222
502  n
mi
                                          Hp   =            213
396

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10223755
88                 X    =        -3110713
34
 Y    =       -9138420
61  feet           Y    =        -2820207
68  meter
 Z    =       17487227
26                 Z    =         5314982
46
 XDOT =      16677
858277                 XDOT =        5147
473414
 YDOT =     -18858
464298  feet/sec       YDOT =       -5690
855516  meter/sec
 ZDOT =       -110
526285                 ZDOT =          -8
839351

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13012320
26                 X    =        -3966155
22
 Y    =       -4589623
02  feet           Y    =        -1398917
10  meter
 Z    =       17419928
67                 Z    =         5309594
26
 XDOT =       8048
288044                 XDOT =        2453
118196
 YDOT =     -22789
927845  feet/sec       YDOT =       -6946
370007  meter/sec
 ZDOT =          1
329113                 ZDOT =            
405114


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   18145
43714245  
00016717  00000-0  10270-3 0  9129
2 25544  51
6379 132
1269 0003958 118
8921 241
2629 15
54109746 34973


Satellite: ISS
Catalog Number: 25544
Epoch time:      18145
43714245   =   yrday
fracday
Element set:     912
Inclination:       51
6379  deg
RA of node:       132
1269  deg
Eccentricity:     
0003958     
Arg of perigee:   118
8921  deg
Mean anomaly:     241
2629  deg
Mean motion:   15
54109746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3497
Checksum:              326


Coasting Arc #14 (Orbit 3511)
---------------------------------------

Vector Time (GMT): 2018/146/09:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1899316
22                 A    =         6778669
09  meter
 Y    =        4109598
73  meter          E    =           
0016575
 Z    =       -5060296
85                 I    =           51
92600
 XDOT =      -5517
096378                 Wp   =          108
49161
 YDOT =       4939
792644  meter/sec      RA   =          126
31110  deg
 ZDOT =       1941
052525                 TA   =          180
29680
                                          MA   =          180
29779
                                          Ha   =            222
301  n
mi
                                          Hp   =            213
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6231352
44                 X    =         1877801
02
 Y    =       13482935
47  feet           Y    =         4130718
21  meter
 Z    =      -16602023
79                 Z    =        -5051122
50
 XDOT =     -18100
709900                 XDOT =       -5581
353194
 YDOT =      16206
668778  feet/sec       YDOT =        4877
737269  meter/sec
 ZDOT =       6368
282562                 ZDOT =        1914
096228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11108994
93                 X    =         3386021
65
 Y    =        9927396
23  feet           Y    =         3025870
37  meter
 Z    =      -16561507
54                 Z    =        -5047947
50
 XDOT =      -9634
057080                 XDOT =       -2936
460598
 YDOT =      21202
033296  feet/sec       YDOT =        6462
379749  meter/sec
 ZDOT =       6247
082635                 ZDOT =        1904
110787


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   18146
40168526  
00016717  00000-0  10270-3 0  9133
2 25544  51
6396 127
3187 0003733 122
2717 237
8798 15
54091349 35125


Satellite: ISS
Catalog Number: 25544
Epoch time:      18146
40168526   =   yrday
fracday
Element set:     913
Inclination:       51
6396  deg
RA of node:       127
3187  deg
Eccentricity:     
0003733     
Arg of perigee:   122
2717  deg
Mean anomaly:     237
8798  deg
Mean motion:   15
54091349  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3512
Checksum:              322


Coasting Arc #15 (Orbit 3519)
---------------------------------------

Vector Time (GMT): 2018/146/20:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1058099
36                 A    =         6780380
19  meter
 Y    =       -4869115
73  meter          E    =           
0010742
 Z    =        4590065
22                 I    =           51
93994
 XDOT =       5682
437391                 Wp   =           81
83543
 YDOT =      -4140
390285  meter/sec      RA   =          123
89909  deg
 ZDOT =      -3074
574833                 TA   =           38
79140
                                          MA   =           38
71433
                                          Ha   =            222
160  n
mi
                                          Hp   =            213
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3471454
58                 X    =        -1025869
39
 Y    =      -15974789
14  feet           Y    =        -4880768
24  meter
 Z    =       15059269
09                 Z    =         4585003
20
 XDOT =      18643
167292                 XDOT =        5743
248929
 YDOT =     -13583
957628  feet/sec       YDOT =       -4076
505120  meter/sec
 ZDOT =     -10087
187772                 ZDOT =       -3046
823684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8302183
08                 X    =         2530505
40
 Y    =       14106076
77  feet           Y    =         4299532
20  meter
 Z    =       15037247
91                 Z    =         4583353
16
 XDOT =     -12607
235197                 XDOT =       -3842
685288
 YDOT =      18066
879741  feet/sec       YDOT =        5506
784945  meter/sec
 ZDOT =      -9962
523967                 ZDOT =       -3036
577305


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   18146
91610550  
00016717  00000-0  10270-3 0  9149
2 25544  51
6380 124
7535 0003402 123
8796 236
2681 15
54136171 35209


Satellite: ISS
Catalog Number: 25544
Epoch time:      18146
91610550   =   yrday
fracday
Element set:     914
Inclination:       51
6380  deg
RA of node:       124
7535  deg
Eccentricity:     
0003402     
Arg of perigee:   123
8796  deg
Mean anomaly:     236
2681  deg
Mean motion:   15
54136171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3520
Checksum:              292


Coasting Arc #16 (Orbit 3534)
---------------------------------------

Vector Time (GMT): 2018/147/20:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -76432
00                 A    =         6784135
55  meter
 Y    =        5811397
76  meter          E    =           
0008267
 Z    =       -3508834
24                 I    =           51
96824
 XDOT =      -5548
125633                 Wp   =          108
53846
 YDOT =       2673
211627  meter/sec      RA   =          118
93246  deg
 ZDOT =       4554
491413                 TA   =          210
45326
                                          MA   =          210
50130
                                          Ha   =            222
142  n
mi
                                          Hp   =            213
643

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -250761
15                 X    =         -124366
62
 Y    =       19066265
62  feet           Y    =         5810275
35  meter
 Z    =      -11511923
36                 Z    =        -3509321
42
 XDOT =     -18202
511920                 XDOT =       -5599
729542
 YDOT =       8770
379355  feet/sec       YDOT =        2610
879716  meter/sec
 ZDOT =      14942
557129                 ZDOT =        4527
415007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5998738
93                 X    =        -1828415
63
 Y    =      -18097869
58  feet           Y    =        -5516230
65  meter
 Z    =      -11514859
68                 Z    =        -3509729
23
 XDOT =      13162
500821                 XDOT =        4011
930250
 YDOT =     -13779
874748  feet/sec       YDOT =       -4200
105823  meter/sec
 ZDOT =      14821
081795                 ZDOT =        4517
465731


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   18147
88064513  
00016717  00000-0  10270-3 0  9159
2 25544  51
6363 119
9447 0003559 128
9234 231
2236 15
54120141 35351


Satellite: ISS
Catalog Number: 25544
Epoch time:      18147
88064513   =   yrday
fracday
Element set:     915
Inclination:       51
6363  deg
RA of node:       119
9447  deg
Eccentricity:     
0003559     
Arg of perigee:   128
9234  deg
Mean anomaly:     231
2236  deg
Mean motion:   15
54120141  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3535
Checksum:              304


Coasting Arc #17 (Orbit 3540)
---------------------------------------

Vector Time (GMT): 2018/148/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3817913
84                 A    =         6777474
23  meter
 Y    =        1719994
56  meter          E    =           
0017696
 Z    =       -5344167
48                 I    =           51
95340
 XDOT =      -3355
207647                 Wp   =           96
99737
 YDOT =       6878
609903  meter/sec      RA   =          117
09033  deg
 ZDOT =       -185
760442                 TA   =          171
25239
                                          MA   =          171
22151
                                          Ha   =            222
202  n
mi
                                          Hp   =            213
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12525964
06                 X    =         3824356
20
 Y    =        5643026
78  feet           Y    =         1762725
65  meter
 Z    =      -17533357
86                 Z    =        -5325605
26
 XDOT =     -11007
899105                 XDOT =       -3430
974438
 YDOT =      22567
617791  feet/sec       YDOT =        6840
666040  meter/sec
 ZDOT =       -609
450268                 ZDOT =        -202
242489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9047323
46                 X    =         2757624
19
 Y    =       10477913
96  feet           Y    =         3193668
18  meter
 Z    =      -17450542
17                 Z    =        -5318925
25
 XDOT =     -18784
819344                 XDOT =       -5725
612936
 YDOT =      15095
128610  feet/sec       YDOT =        4600
995200  meter/sec
 ZDOT =       -684
088233                 ZDOT =        -208
510093


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   18148
26646072  
00016717  00000-0  10270-3 0  9169
2 25544  51
6382 118
0219 0003704 132
6271 227
5194 15
54094285 35411


Satellite: ISS
Catalog Number: 25544
Epoch time:      18148
26646072   =   yrday
fracday
Element set:     916
Inclination:       51
6382  deg
RA of node:       118
0219  deg
Eccentricity:     
0003704     
Arg of perigee:   132
6271  deg
Mean anomaly:     227
5194  deg
Mean motion:   15
54094285  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              304


Coasting Arc #18 (Orbit 3556)
---------------------------------------

Vector Time (GMT): 2018/149/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2966938
07                 A    =         6778253
00  meter
 Y    =       -3313258
29  meter          E    =           
0006808
 Z    =        5109347
92                 I    =           51
97166
 XDOT =       4027
624212                 Wp   =           87
03200
 YDOT =      -6295
095237  meter/sec      RA   =          112
11323  deg
 ZDOT =      -1741
050088                 TA   =           19
72203
                                          MA   =           19
69572
                                          Ha   =            222
175  n
mi
                                          Hp   =            213
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9734048
78                 X    =        -2954486
69
 Y    =      -10870269
98  feet           Y    =        -3346367
62  meter
 Z    =       16762952
48                 Z    =         5094965
19
 XDOT =      13213
990197                 XDOT =        4106
175577
 YDOT =     -20653
199598  feet/sec       YDOT =       -6249
616156  meter/sec
 ZDOT =      -5712
106587                 ZDOT =       -1721
294945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4535117
64                 X    =        -1382303
86
 Y    =      -13945809
75  feet           Y    =        -4250682
81  meter
 Z    =       16699046
36                 Z    =         5089869
33
 XDOT =      19525
905577                 XDOT =        5951
496020
 YDOT =     -13091
920707  feet/sec       YDOT =       -3990
417432  meter/sec
 ZDOT =      -5622
877822                 ZDOT =       -1713
853160


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   18149
29529516  
00016717  00000-0  10270-3 0  9177
2 25544  51
6391 112
8932 0003629 135
9685 224
1757 15
54150280 35579


Satellite: ISS
Catalog Number: 25544
Epoch time:      18149
29529516   =   yrday
fracday
Element set:     917
Inclination:       51
6391  deg
RA of node:       112
8932  deg
Eccentricity:     
0003629     
Arg of perigee:   135
9685  deg
Mean anomaly:     224
1757  deg
Mean motion:   15
54150280  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3557
Checksum:              330


Coasting Arc #19 (Orbit 3571)
---------------------------------------

Vector Time (GMT): 2018/150/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2107982
78                 A    =         6781270
01  meter
 Y    =        4750090
39  meter          E    =           
0012224
 Z    =       -4369234
78                 I    =           51
99352
 XDOT =      -4443
642815                 Wp   =          117
78301
 YDOT =       5173
425668  meter/sec      RA   =          107
14244  deg
 ZDOT =       3482
389493                 TA   =          187
45895
                                          MA   =          187
47715
                                          Ha   =            222
113  n
mi
                                          Hp   =            213
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6915954
00                 X    =         2075933
00
 Y    =       15584286
07  feet           Y    =         4773484
69  meter
 Z    =      -14334759
77                 Z    =        -4359072
01
 XDOT =     -14578
880627                 XDOT =       -4518
079040
 YDOT =      16973
181327  feet/sec       YDOT =        5123
317131  meter/sec
 ZDOT =      11425
162380                 ZDOT =        3460
623436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         314006
22                 X    =           95709
10
 Y    =       17084639
52  feet           Y    =         5207398
12  meter
 Z    =      -14289934
30                 Z    =        -4355571
97
 XDOT =     -18904
900709                 XDOT =       -5762
213736
 YDOT =       9816
440679  feet/sec       YDOT =        2992
051119  meter/sec
 ZDOT =      11327
064422                 ZDOT =        3452
489236


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   18150
25982614  
00016717  00000-0  10270-3 0  9188
2 25544  51
6395 108
0850 0003724 134
6092 225
5365 15
54140353 35720


Satellite: ISS
Catalog Number: 25544
Epoch time:      18150
25982614   =   yrday
fracday
Element set:     918
Inclination:       51
6395  deg
RA of node:       108
0850  deg
Eccentricity:     
0003724     
Arg of perigee:   134
6092  deg
Mean anomaly:     225
5365  deg
Mean motion:   15
54140353  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3572
Checksum:              302


Coasting Arc #20 (Orbit 3587)
---------------------------------------

Vector Time (GMT): 2018/151/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1244430
59                 A    =         6785055
59  meter
 Y    =       -5872587
77  meter          E    =           
0015704
 Z    =        3144815
98                 I    =           52
01481
 XDOT =       4683
654545                 Wp   =          104
19434
 YDOT =      -3617
486911  meter/sec      RA   =          102
18264  deg
 ZDOT =      -4885
304277                 TA   =           39
73574
                                          MA   =           39
62081
                                          Ha   =            222
040  n
mi
                                          Hp   =            213
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4082777
53                 X    =        -1193945
22
 Y    =      -19267020
23  feet           Y    =        -5886222
01  meter
 Z    =       10317637
73                 Z    =         3138892
69
 XDOT =      15366
320686                 XDOT =        4747
488632
 YDOT =     -11868
395376  feet/sec       YDOT =       -3564
753447  meter/sec
 ZDOT =     -16027
901170                 ZDOT =       -4862
397954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3430820
61                 X    =         1045714
12
 Y    =      -19407372
12  feet           Y    =        -5915367
02  meter
 Z    =       10291946
67                 Z    =         3136985
35
 XDOT =      17393
316042                 XDOT =        5301
482730
 YDOT =      -5399
293223  feet/sec       YDOT =       -1645
704574  meter/sec
 ZDOT =     -15924
895263                 ZDOT =       -4853
908076


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   18151
28865430  
00016717  00000-0  10270-3 0  9199
2 25544  51
6392 102
9567 0003634 139
9033 220
2389 15
54162425 35887


Satellite: ISS
Catalog Number: 25544
Epoch time:      18151
28865430   =   yrday
fracday
Element set:     919
Inclination:       51
6392  deg
RA of node:       102
9567  deg
Eccentricity:     
0003634     
Arg of perigee:   139
9033  deg
Mean anomaly:     220
2389  deg
Mean motion:   15
54162425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3588
Checksum:              320
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