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

 
Date: September 6th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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


249/00:50:06 532 0 3 0 7 0 7
N/A 0 2 -0 1 223 1
000/00:00:13 064 0 5 -0 0 213 7

249/22:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 7

253/11:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 9

253/22:49:12 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 214 0

257/11:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 214 2

257/13:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 214 1

Coasting Arc #1 (Orbit 1099)
---------------------------------------

Vector Time (GMT): 2018/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5371262
39                 A    =         6783142
69  meter
 Y    =       -1223321
15  meter          E    =           
0010748
 Z    =       -3965676
48                 I    =           51
49887
 XDOT =       4099
565445                 Wp   =           99
03822
 YDOT =      -5092
853297  meter/sec      RA   =          337
89584  deg
 ZDOT =      -3992
497164                 TA   =          129
25343
                                          MA   =          129
15801
                                          Ha   =            223
035  n
mi
                                          Hp   =            213
287

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17622251
93                 X    =        -5337920
67
 Y    =       -4013520
82  feet           Y    =        -1283199
96  meter
 Z    =      -13010749
60                 Z    =        -3991686
99
 XDOT =      13450
017865                 XDOT =        4175
603737
 YDOT =     -16708
836277  feet/sec       YDOT =       -5046
584022  meter/sec
 ZDOT =     -13098
743975                 ZDOT =       -3972
398304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15698776
54                 X    =         4784987
09
 Y    =        8783790
34  feet           Y    =         2677299
30  meter
 Z    =      -13127267
81                 Z    =        -4001191
23
 XDOT =     -17049
074256                 XDOT =       -5196
557833
 YDOT =      11083
852487  feet/sec       YDOT =        3378
358238  meter/sec
 ZDOT =     -13007
848241                 ZDOT =       -3964
792144


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   18248
52349744  
00016717  00000-0  10270-3 0  9008
2 25544  51
6418 338
3524 0005561 134
0975 226
0636 15
53924252 11006


Satellite: ISS
Catalog Number: 25544
Epoch time:      18248
52349744   =   yrday
fracday
Element set:     900
Inclination:       51
6418  deg
RA of node:       338
3524  deg
Eccentricity:     
0005561     
Arg of perigee:   134
0975  deg
Mean anomaly:     226
0636  deg
Mean motion:   15
53924252  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1100
Checksum:              298


Coasting Arc #2 (Orbit 1107)
---------------------------------------

Vector Time (GMT): 2018/249/00:50:13
064
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5326088
94                 A    =         6789116
87  meter
 Y    =       -3884123
15  meter          E    =           
0009367
 Z    =       -1622532
51                 I    =           51
50249
 XDOT =       4024
552091                 Wp   =           68
38073
 YDOT =       3144
890096  meter/sec      RA   =          335
18781  deg
 ZDOT =       5712
426714                 TA   =          273
83792
                                          MA   =          273
94501
                                          Ha   =            223
066  n
mi
                                          Hp   =            213
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17474045
07                 X    =         5377007
76
 Y    =      -12743186
19  feet           Y    =        -3824278
46  meter
 Z    =       -5323269
40                 Z    =        -1596536
74
 XDOT =      13203
911061                 XDOT =        3961
338284
 YDOT =      10317
880894  feet/sec       YDOT =        3189
542102  meter/sec
 ZDOT =      18741
557460                 ZDOT =        5731
822781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18203638
42                 X    =         5548468
99
 Y    =      -11729977
20  feet           Y    =        -3575297
05  meter
 Z    =       -5206095
01                 Z    =        -1586817
76
 XDOT =      11617
370858                 XDOT =        3540
974638
 YDOT =       9717
042999  feet/sec       YDOT =        2961
754706  meter/sec
 ZDOT =      18828
128389                 ZDOT =        5738
813533


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   18249
03797799  
00016717  00000-0  10270-3 0  9013
2 25544  51
6429 335
7915 0004833 127
7511 232
4080 15
53832130 11084


Satellite: ISS
Catalog Number: 25544
Epoch time:      18249
03797799   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:       335
7915  deg
Eccentricity:     
0004833     
Arg of perigee:   127
7511  deg
Mean anomaly:     232
4080  deg
Mean motion:   15
53832130  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1108
Checksum:              311


Coasting Arc #3 (Orbit 1122)
---------------------------------------

Vector Time (GMT): 2018/249/22:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3043605
47                 A    =         6778452
58  meter
 Y    =        3062480
86  meter          E    =           
0008321
 Z    =        5220372
19                 I    =           51
43832
 XDOT =      -6193
094733                 Wp   =          126
56078
 YDOT =       4414
400171  meter/sec      RA   =          330
62680  deg
 ZDOT =       1015
071561                 TA   =          313
66410
                                          MA   =          313
73305
                                          Ha   =            222
857  n
mi
                                          Hp   =            213
684

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9985582
25                 X    =         2983776
28
 Y    =       10047509
38  feet           Y    =         3096182
25  meter
 Z    =       17127205
34                 Z    =         5235011
33
 XDOT =     -20318
552274                 XDOT =       -6246
928114
 YDOT =      14482
940195  feet/sec       YDOT =        4344
843735  meter/sec
 ZDOT =       3330
287275                 ZDOT =         984
857136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3070219
96                 X    =          935803
04
 Y    =       13747685
60  feet           Y    =         4190294
57  meter
 Z    =       17192450
39                 Z    =         5240258
88
 XDOT =     -23919
283359                 XDOT =       -7290
597568
 YDOT =       1322
846166  feet/sec       YDOT =         403
203511  meter/sec
 ZDOT =       3194
123192                 ZDOT =         973
568749


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   18250
00269998  
00016717  00000-0  10270-3 0  9028
2 25544  51
6412 330
9847 0004786 130
9899 229
1668 15
53856009 11232


Satellite: ISS
Catalog Number: 25544
Epoch time:      18250
00269998   =   yrday
fracday
Element set:     902
Inclination:       51
6412  deg
RA of node:       330
9847  deg
Eccentricity:     
0004786     
Arg of perigee:   130
9899  deg
Mean anomaly:     229
1668  deg
Mean motion:   15
53856009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1123
Checksum:              334


Coasting Arc #4 (Orbit 1137)
---------------------------------------

Vector Time (GMT): 2018/250/22:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1609533
93                 A    =         6778479
92  meter
 Y    =       -3983769
92  meter          E    =           
0018587
 Z    =       -5258929
15                 I    =           51
41004
 XDOT =       6623
786839                 Wp   =          105
10046
 YDOT =      -3749
135594  meter/sec      RA   =          325
61515  deg
 ZDOT =        810
465964                 TA   =          172
69869
                                          MA   =          172
67159
                                          Ha   =            222
993  n
mi
                                          Hp   =            213
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5280623
12                 X    =        -1539321
96
 Y    =      -13070111
29  feet           Y    =        -4001376
61  meter
 Z    =      -17253704
57                 Z    =        -5266576
80
 XDOT =      21731
584116                 XDOT =        6661
281663
 YDOT =     -12300
313627  feet/sec       YDOT =       -3674
854118  meter/sec
 ZDOT =       2659
009069                 ZDOT =         842
732860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2283831
84                 X    =          696111
94
 Y    =      -13868339
61  feet           Y    =        -4227069
91  meter
 Z    =      -17287463
08                 Z    =        -5269218
75
 XDOT =      23936
689697                 XDOT =        7295
903020
 YDOT =        436
692269  feet/sec       YDOT =         133
103804  meter/sec
 ZDOT =       2804
273337                 ZDOT =         854
742513


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   18250
96742245  
00016717  00000-0  10270-3 0  9035
2 25544  51
6416 326
1779 0004822 133
2525 226
9031 15
53827481 11387


Satellite: ISS
Catalog Number: 25544
Epoch time:      18250
96742245   =   yrday
fracday
Element set:     903
Inclination:       51
6416  deg
RA of node:       326
1779  deg
Eccentricity:     
0004822     
Arg of perigee:   133
2525  deg
Mean anomaly:     226
9031  deg
Mean motion:   15
53827481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1138
Checksum:              306


Coasting Arc #5 (Orbit 1153)
---------------------------------------

Vector Time (GMT): 2018/251/22:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         186272
91                 A    =         6780417
91  meter
 Y    =        4791856
70  meter          E    =           
0009712
 Z    =        4785135
18                 I    =           51
38977
 XDOT =      -6660
331912                 Wp   =           88
90063
 YDOT =       2822
170942  meter/sec      RA   =          320
60515  deg
 ZDOT =      -2562
174840                 TA   =           26
41912
                                          MA   =           26
36963
                                          Ha   =            222
855  n
mi
                                          Hp   =            213
838

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         611131
61                 X    =          109431
85
 Y    =       15721314
62  feet           Y    =         4793510
52  meter
 Z    =       15699262
40                 Z    =         4785852
94
 XDOT =     -21851
482652                 XDOT =       -6678
949675
 YDOT =       9259
091018  feet/sec       YDOT =        2747
586159  meter/sec
 ZDOT =      -8406
085433                 ZDOT =       -2594
573463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7405383
17                 X    =        -2257160
79
 Y    =       13878500
65  feet           Y    =         4230167
00  meter
 Z    =       15701833
48                 Z    =         4785918
85
 XDOT =     -22495
839759                 XDOT =       -6856
731958
 YDOT =      -2310
753351  feet/sec       YDOT =        -704
317621  meter/sec
 ZDOT =      -8551
798182                 ZDOT =       -2606
588086


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   18251
99645502  
00016717  00000-0  10270-3 0  9048
2 25544  51
6413 321
0516 0004710 137
3003 222
8516 15
53845481 11540


Satellite: ISS
Catalog Number: 25544
Epoch time:      18251
99645502   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       321
0516  deg
Eccentricity:     
0004710     
Arg of perigee:   137
3003  deg
Mean anomaly:     222
8516  deg
Mean motion:   15
53845481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1154
Checksum:              282


Coasting Arc #6 (Orbit 1168)
---------------------------------------

Vector Time (GMT): 2018/252/22:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1117905
58                 A    =         6783763
97  meter
 Y    =       -5449702
10  meter          E    =           
0010648
 Z    =       -3894354
87                 I    =           51
37673
 XDOT =       6286
677252                 Wp   =          119
70603
 YDOT =      -1612
138541  meter/sec      RA   =          315
59885  deg
 ZDOT =       4063
861724                 TA   =          193
06847
                                          MA   =          193
09608
                                          Ha   =            222
855  n
mi
                                          Hp   =            213
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3667669
22                 X    =         1197679
12
 Y    =      -17879600
07  feet           Y    =        -5436755
30  meter
 Z    =      -12776754
84                 Z    =        -3888730
17
 XDOT =      20625
581536                 XDOT =        6284
497486
 YDOT =      -5289
168440  feet/sec       YDOT =       -1541
848290  meter/sec
 ZDOT =      13332
879673                 ZDOT =        4094
394809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11937234
89                 X    =         3638469
19
 Y    =      -13831011
23  feet           Y    =        -4215692
22  meter
 Z    =      -12750800
44                 Z    =        -3886443
97
 XDOT =      19522
002189                 XDOT =        5950
306267
 YDOT =       4440
727003  feet/sec       YDOT =        1353
533590  meter/sec
 ZDOT =      13470
047563                 ZDOT =        4105
670497


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   18252
96116989  
00016717  00000-0  10270-3 0  9059
2 25544  51
6420 316
2441 0004733 139
9959 220
1543 15
53844836 11694


Satellite: ISS
Catalog Number: 25544
Epoch time:      18252
96116989   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       316
2441  deg
Eccentricity:     
0004733     
Arg of perigee:   139
9959  deg
Mean anomaly:     220
1543  deg
Mean motion:   15
53844836  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1169
Checksum:              327


Coasting Arc #7 (Orbit 1176)
---------------------------------------

Vector Time (GMT): 2018/253/11:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2896038
10                 A    =         6778286
46  meter
 Y    =       -3107156
51  meter          E    =           
0018131
 Z    =       -5297812
20                 I    =           51
34494
 XDOT =       5372
444905                 Wp   =          104
44071
 YDOT =      -5446
978754  meter/sec      RA   =          313
08298  deg
 ZDOT =        254
106632                 TA   =          168
01715
                                          MA   =          167
97396
                                          Ha   =            222
847  n
mi
                                          Hp   =            213
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9501437
34                 X    =        -2835343
98
 Y    =      -10194083
04  feet           Y    =        -3139203
28  meter
 Z    =      -17381273
63                 Z    =        -5311732
27
 XDOT =      17626
131578                 XDOT =        5431
720935
 YDOT =     -17870
665202  feet/sec       YDOT =       -5386
568886  meter/sec
 ZDOT =        833
683177                 ZDOT =         280
348528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4008318
64                 X    =         1221735
52
 Y    =       13265369
74  feet           Y    =         4043284
70  meter
 Z    =      -17443298
46                 Z    =        -5316717
37
 XDOT =     -22677
154426                 XDOT =       -6911
996669
 YDOT =       8120
096020  feet/sec       YDOT =        2475
005267  meter/sec
 ZDOT =        952
103774                 ZDOT =         290
201230


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   18253
47568256  
00016717  00000-0  10270-3 0  9065
2 25544  51
6406 313
6785 0004866 146
1469 213
9995 15
53820106 11777


Satellite: ISS
Catalog Number: 25544
Epoch time:      18253
47568256   =   yrday
fracday
Element set:     906
Inclination:       51
6406  deg
RA of node:       313
6785  deg
Eccentricity:     
0004866     
Arg of perigee:   146
1469  deg
Mean anomaly:     213
9995  deg
Mean motion:   15
53820106  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1177
Checksum:              336


Coasting Arc #8 (Orbit 1184)
---------------------------------------

Vector Time (GMT): 2018/253/22:49:12
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1273965
86                 A    =         6785233
25  meter
 Y    =        5702342
89  meter          E    =           
0015717
 Z    =        3432577
46                 I    =           51
35731
 XDOT =      -6010
145349                 Wp   =          103
57727
 YDOT =       1410
043195  meter/sec      RA   =          310
60809  deg
 ZDOT =      -4559
050742                 TA   =           35
99225
                                          MA   =           35
88650
                                          Ha   =            222
858  n
mi
                                          Hp   =            213
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4179678
02                 X    =        -1354309
93
 Y    =       18708474
05  feet           Y    =         5687647
70  meter
 Z    =       11261737
08                 Z    =         3426193
18
 XDOT =     -19718
324636                 XDOT =       -6003
320793
 YDOT =       4626
125968  feet/sec       YDOT =        1342
871189  meter/sec
 ZDOT =     -14957
515559                 ZDOT =       -4588
229400

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12706527
74                 X    =        -3872949
65
 Y    =       14376431
10  feet           Y    =         4381936
20  meter
 Z    =       11232355
65                 Z    =         3423622
00
 XDOT =     -18384
658379                 XDOT =       -5603
643874
 YDOT =      -4424
505294  feet/sec       YDOT =       -1348
589214  meter/sec
 ZDOT =     -15088
569434                 ZDOT =       -4598
995963


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   18253
99019790  
00016717  00000-0  10270-3 0  9077
2 25544  51
6407 311
1177 0004790 143
2819 216
8662 15
53826470 11851


Satellite: ISS
Catalog Number: 25544
Epoch time:      18253
99019790   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       311
1177  deg
Eccentricity:     
0004790     
Arg of perigee:   143
2819  deg
Mean anomaly:     216
8662  deg
Mean motion:   15
53826470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1185
Checksum:              322


Coasting Arc #9 (Orbit 1199)
---------------------------------------

Vector Time (GMT): 2018/254/22:49:12
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2288454
67                 A    =         6788314
57  meter
 Y    =       -6045832
19  meter          E    =           
0006751
 Z    =       -2075410
31                 I    =           51
34778
 XDOT =       5324
518597                 Wp   =           81
15769
 YDOT =        130
470314  meter/sec      RA   =          305
61104  deg
 ZDOT =       5507
424965                 TA   =          255
79924
                                          MA   =          255
87425
                                          Ha   =            222
682  n
mi
                                          Hp   =            214
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7508053
39                 X    =         2365972
02
 Y    =      -19835407
45  feet           Y    =        -6019807
92  meter
 Z    =       -6809088
94                 Z    =        -2064104
80
 XDOT =      17468
893036                 XDOT =        5295
911737
 YDOT =        428
052210  feet/sec       YDOT =         189
853472  meter/sec
 ZDOT =      18068
979545                 ZDOT =        5533
220137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15901938
71                 X    =         4846910
92
 Y    =      -14058487
73  feet           Y    =        -4285027
06  meter
 Z    =       -6757604
20                 Z    =        -2059717
76
 XDOT =      14139
107919                 XDOT =        4309
600094
 YDOT =       7278
241108  feet/sec       YDOT =        2218
407890  meter/sec
 ZDOT =      18184
649143                 ZDOT =        5542
681059


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   18254
95490793  
00016717  00000-0  10270-3 0  9081
2 25544  51
6413 306
3102 0004632 148
9208 211
2220 15
53857108 12000


Satellite: ISS
Catalog Number: 25544
Epoch time:      18254
95490793   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       306
3102  deg
Eccentricity:     
0004632     
Arg of perigee:   148
9208  deg
Mean anomaly:     211
2220  deg
Mean motion:   15
53857108  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1200
Checksum:              285


Coasting Arc #10 (Orbit 1215)
---------------------------------------

Vector Time (GMT): 2018/255/22:49:12
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3105715
63                 A    =         6790172
22  meter
 Y    =        6008469
28  meter          E    =           
0017385
 Z    =         484549
18                 I    =           51
33527
 XDOT =      -4469
047427                 Wp   =          135
67367
 YDOT =      -1819
504182  meter/sec      RA   =          300
62009  deg
 ZDOT =      -5964
763888                 TA   =           39
07552
                                          MA   =           38
95007
                                          Ha   =            222
706  n
mi
                                          Hp   =            214
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10189355
74                 X    =        -3175026
87
 Y    =       19712825
74  feet           Y    =         5973351
53  meter
 Z    =        1589728
29                 Z    =          469293
66
 XDOT =     -14662
229092                 XDOT =       -4419
395285
 YDOT =      -5969
501909  feet/sec       YDOT =       -1869
203178  meter/sec
 ZDOT =     -19569
435328                 ZDOT =       -5986
352262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17967108
85                 X    =        -5476374
78
 Y    =       13031371
55  feet           Y    =         3971962
05  meter
 Z    =        1520545
98                 Z    =          463462
41
 XDOT =      -9351
409997                 XDOT =       -2850
309767
 YDOT =     -10551
604962  feet/sec       YDOT =       -3216
129192  meter/sec
 ZDOT =     -19666
017877                 ZDOT =       -5994
202249


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   18255
98393092  
00016717  00000-0  10270-3 0  9090
2 25544  51
6414 301
1827 0004746 152
4069 207
7336 15
53808883 12160


Satellite: ISS
Catalog Number: 25544
Epoch time:      18255
98393092   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       301
1827  deg
Eccentricity:     
0004746     
Arg of perigee:   152
4069  deg
Mean anomaly:     207
7336  deg
Mean motion:   15
53808883  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1216
Checksum:              324


Coasting Arc #11 (Orbit 1231)
---------------------------------------

Vector Time (GMT): 2018/256/22:49:12
000
Vector Time (MET): N/A
Weight (LBS)     : 909595
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3670770
01                 A    =         6789583
72  meter
 Y    =       -5597947
77  meter          E    =           
0013770
 Z    =        1109473
69                 I    =           51
31707
 XDOT =       3524
796835                 Wp   =           76
00758
 YDOT =       3482
342241  meter/sec      RA   =          295
62861  deg
 ZDOT =       5850
476931                 TA   =          296
08309
                                          MA   =          296
22475
                                          Ha   =            222
530  n
mi
                                          Hp   =            214
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12043208
69                 X    =         3727705
72
 Y    =      -18365970
38  feet           Y    =        -5556580
23  meter
 Z    =        3640005
53                 Z    =         1127443
90
 XDOT =      11564
294079                 XDOT =        3457
175651
 YDOT =      11425
007354  feet/sec       YDOT =        3521
381390  meter/sec
 ZDOT =      19194
478120                 ZDOT =        5867
434717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18795027
31                 X    =         5728724
32
 Y    =      -11335619
35  feet           Y    =        -3455096
78  meter
 Z    =        3721298
99                 Z    =         1134251
93
 XDOT =       4522
351931                 XDOT =        1378
412869
 YDOT =      13885
399912  feet/sec       YDOT =        4232
269893  meter/sec
 ZDOT =      19270
084697                 ZDOT =        5873
521816


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   18257
01294917  
00016717  00000-0  10270-3 0  9104
2 25544  51
6406 296
0545 0004491 155
7173 204
4191 15
53854047 12323


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
01294917   =   yrday
fracday
Element set:     910
Inclination:       51
6406  deg
RA of node:       296
0545  deg
Eccentricity:     
0004491     
Arg of perigee:   155
7173  deg
Mean anomaly:     204
4191  deg
Mean motion:   15
53854047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1232
Checksum:              301


Coasting Arc #12 (Orbit 1239)
---------------------------------------

Vector Time (GMT): 2018/257/11:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943674
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1409499
29                 A    =         6782773
03  meter
 Y    =        5179209
39  meter          E    =           
0011993
 Z    =        4135143
48                 I    =           51
28532
 XDOT =      -5090
387107                 Wp   =           98
70364
 YDOT =       4367
870356  meter/sec      RA   =          292
91153  deg
 ZDOT =      -3728
099040                 TA   =           29
83844
                                          MA   =           29
77012
                                          Ha   =            222
473  n
mi
                                          Hp   =            214
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4624341
49                 X    =         1331392
70
 Y    =       16992156
78  feet           Y    =         5194534
99  meter
 Z    =       13566743
70                 Z    =         4141800
26
 XDOT =     -16700
745101                 XDOT =       -5120
742267
 YDOT =      14330
283320  feet/sec       YDOT =        4310
776094  meter/sec
 ZDOT =     -12231
296064                 ZDOT =       -3752
900598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -755892
78                 X    =         -230396
12
 Y    =      -17571378
69  feet           Y    =        -5355756
23  meter
 Z    =       13595945
63                 Z    =         4144044
23
 XDOT =      18040
954552                 XDOT =        5498
882948
 YDOT =     -10345
589734  feet/sec       YDOT =       -3153
335751  meter/sec
 ZDOT =     -12343
064528                 ZDOT =       -3762
166068


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   18257
52745811  
00016717  00000-0  10270-3 0  9115
2 25544  51
6390 293
4894 0004741 158
0468 202
0889 15
53874621 12401


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
52745811   =   yrday
fracday
Element set:     911
Inclination:       51
6390  deg
RA of node:       293
4894  deg
Eccentricity:     
0004741     
Arg of perigee:   158
0468  deg
Mean anomaly:     202
0889  deg
Mean motion:   15
53874621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1240
Checksum:              320


Coasting Arc #13 (Orbit 1240)
---------------------------------------

Vector Time (GMT): 2018/257/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943674
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3740567
12                 A    =         6778289
87  meter
 Y    =       -2045387
88  meter          E    =           
0017398
 Z    =       -5284442
42                 I    =           51
26843
 XDOT =       3218
498730                 Wp   =          107
37399
 YDOT =      -6934
454857  meter/sec      RA   =          292
48129  deg
 ZDOT =        401
840773                 TA   =          166
50754
                                          MA   =          166
46097
                                          Ha   =            222
615  n
mi
                                          Hp   =            214
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12272201
84                 X    =        -3691747
83
 Y    =       -6710590
17  feet           Y    =        -2086944
95  meter
 Z    =      -17337409
53                 Z    =        -5302494
17
 XDOT =      10559
379035                 XDOT =        3293
850580
 YDOT =     -22750
836145  feet/sec       YDOT =       -6898
042023  meter/sec
 ZDOT =       1318
375238                 ZDOT =         417
658777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13723353
66                 X    =         4182878
19
 Y    =        2122244
38  feet           Y    =          646860
09  meter
 Z    =      -17418104
68                 Z    =        -5309038
31
 XDOT =      -1928
979790                 XDOT =        -587
953040
 YDOT =      23990
567534  feet/sec       YDOT =        7312
324984  meter/sec
 ZDOT =       1390
178809                 ZDOT =         423
726501


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   18257
59177210  
00016717  00000-0  10270-3 0  9125
2 25544  51
6387 293
1693 0004767 157
4274 202
7088 15
53829894 12418


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
59177210   =   yrday
fracday
Element set:     912
Inclination:       51
6387  deg
RA of node:       293
1693  deg
Eccentricity:     
0004767     
Arg of perigee:   157
4274  deg
Mean anomaly:     202
7088  deg
Mean motion:   15
53829894  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1241
Checksum:              337


Coasting Arc #14 (Orbit 1256)
---------------------------------------

Vector Time (GMT): 2018/258/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943674
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3020615
18                 A    =         6779747
71  meter
 Y    =        3547747
48  meter          E    =           
0007068
 Z    =        4918452
35                 I    =           51
26136
 XDOT =      -3817
272820                 Wp   =           98
01588
 YDOT =       6286
035522  meter/sec      RA   =          287
45911  deg
 ZDOT =      -2188
131677                 TA   =           13
43840
                                          MA   =           13
41959
                                          Ha   =            222
381  n
mi
                                          Hp   =            214
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9910154
81                 X    =         2956827
41
 Y    =       11639591
48  feet           Y    =         3581169
75  meter
 Z    =       16136654
70                 Z    =         4932970
37
 XDOT =     -12523
860959                 XDOT =       -3876
652460
 YDOT =      20623
476123  feet/sec       YDOT =        6243
015978  meter/sec
 ZDOT =      -7178
909700                 ZDOT =       -2206
819389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13335876
57                 X    =        -4064775
18
 Y    =       -7331745
55  feet           Y    =        -2234716
04  meter
 Z    =       16201320
51                 Z    =         4938162
49
 XDOT =       3681
253492                 XDOT =        1122
046064
 YDOT =     -22758
936905  feet/sec       YDOT =       -6936
923969  meter/sec
 ZDOT =      -7263
490831                 ZDOT =       -2213
912005


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   18258
62078851  
00016717  00000-0  10270-3 0  9132
2 25544  51
6381 288
0412 0004702 160
8068 199
3263 15
53860167 12573


Satellite: ISS
Catalog Number: 25544
Epoch time:      18258
62078851   =   yrday
fracday
Element set:     913
Inclination:       51
6381  deg
RA of node:       288
0412  deg
Eccentricity:     
0004702     
Arg of perigee:   160
8068  deg
Mean anomaly:     199
3263  deg
Mean motion:   15
53860167  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1257
Checksum:              319


Coasting Arc #15 (Orbit 1271)
---------------------------------------

Vector Time (GMT): 2018/259/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943674
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2299988
58                 A    =         6782977
85  meter
 Y    =       -4889066
85  meter          E    =           
0010915
 Z    =       -4112950
38                 I    =           51
26316
 XDOT =       4229
537183                 Wp   =          128
77548
 YDOT =      -5155
844558  meter/sec      RA   =          282
44348  deg
 ZDOT =       3763
639181                 TA   =          180
28207
                                          MA   =          180
28269
                                          Ha   =            222
478  n
mi
                                          Hp   =            214
375

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7545894
29                 X    =        -2225168
12
 Y    =      -16040245
57  feet           Y    =        -4914368
80  meter
 Z    =      -13493931
70                 Z    =        -4123940
97
 XDOT =      13876
434327                 XDOT =        4268
595081
 YDOT =     -16915
500520  feet/sec       YDOT =       -5108
328345  meter/sec
 ZDOT =      12347
897574                 ZDOT =        3784
280028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12939956
22                 X    =         3944098
65
 Y    =       12061139
85  feet           Y    =         3676235
43  meter
 Z    =      -13542622
71                 Z    =        -4127791
40
 XDOT =      -5543
230026                 XDOT =       -1689
576512
 YDOT =      19916
121437  feet/sec       YDOT =        6070
433814  meter/sec
 ZDOT =      12441
089643                 ZDOT =        3792
044123


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   18259
58548962  
00016717  00000-0  10270-3 0  9144
2 25544  51
6382 283
2346 0004600 162
4674 197
6639 15
53834565 12723


Satellite: ISS
Catalog Number: 25544
Epoch time:      18259
58548962   =   yrday
fracday
Element set:     914
Inclination:       51
6382  deg
RA of node:       283
2346  deg
Eccentricity:     
0004600     
Arg of perigee:   162
4674  deg
Mean anomaly:     197
6639  deg
Mean motion:   15
53834565  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1272
Checksum:              341


Coasting Arc #16 (Orbit 1287)
---------------------------------------

Vector Time (GMT): 2018/260/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943674
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1569145
14                 A    =         6786476
69  meter
 Y    =        5923657
03  meter          E    =           
0015413
 Z    =        2895690
55                 I    =           51
26782
 XDOT =      -4525
844661                 Wp   =          113
98435
 YDOT =       3653
197273  meter/sec      RA   =          277
43576  deg
 ZDOT =      -5005
784774                 TA   =           32
80717
                                          MA   =           32
71157
                                          Ha   =            222
205  n
mi
                                          Hp   =            214
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5148113
98                 X    =         1488722
79
 Y    =       19434570
30  feet           Y    =         5940754
78  meter
 Z    =        9500297
08                 Z    =         2903117
28
 XDOT =     -14848
571723                 XDOT =       -4542
043867
 YDOT =      11985
555356  feet/sec       YDOT =        3602
495300  meter/sec
 ZDOT =     -16423
178393                 ZDOT =       -5027
809318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12293896
02                 X    =        -3747179
51
 Y    =      -15888527
83  feet           Y    =        -4842823
28  meter
 Z    =        9532893
00                 Z    =         2905625
79
 XDOT =       7705
725893                 XDOT =        2348
705252
 YDOT =     -15904
963279  feet/sec       YDOT =       -4847
832807  meter/sec
 ZDOT =     -16522
387707                 ZDOT =       -5036
023773


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   18260
61450148  
00016717  00000-0  10270-3 0  9159
2 25544  51
6369 278
1066 0004441 167
8293 192
2968 15
53878244 12884


Satellite: ISS
Catalog Number: 25544
Epoch time:      18260
61450148   =   yrday
fracday
Element set:     915
Inclination:       51
6369  deg
RA of node:       278
1066  deg
Eccentricity:     
0004441     
Arg of perigee:   167
8293  deg
Mean anomaly:     192
2968  deg
Mean motion:   15
53878244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1288
Checksum:              337


Coasting Arc #17 (Orbit 1302)
---------------------------------------

Vector Time (GMT): 2018/261/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943674
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -871806
61                 A    =         6789173
55  meter
 Y    =       -6577974
14  meter          E    =           
0006357
 Z    =       -1435006
27                 I    =           51
27353
 XDOT =       4699
199078                 Wp   =           70
55463
 YDOT =      -1873
339937  meter/sec      RA   =          272
43723  deg
 ZDOT =       5755
366099                 TA   =          273
72485
                                          MA   =          273
79754
                                          Ha   =            222
286  n
mi
                                          Hp   =            214
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2860257
90                 X    =         -791214
59
 Y    =      -21581279
97  feet           Y    =        -6587272
74  meter
 Z    =       -4708025
81                 Z    =        -1439045
09
 XDOT =      15417
319811                 XDOT =        4691
841532
 YDOT =      -6146
128401  feet/sec       YDOT =       -1820
831058  meter/sec
 ZDOT =      18882
434709                 ZDOT =        5778
175381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11380242
32                 X    =         3468697
86
 Y    =       18554224
09  feet           Y    =         5655327
50  meter
 Z    =       -4725365
68                 Z    =        -1440291
46
 XDOT =     -10105
750914                 XDOT =       -3080
232878
 YDOT =      11014
286485  feet/sec       YDOT =        3357
154521  meter/sec
 ZDOT =      18984
949393                 ZDOT =        5786
612575


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   18261
57919989  
00016717  00000-0  10270-3 0  9169
2 25544  51
6367 273
3003 0004668 169
8102 190
3146 15
53877375 13031


Satellite: ISS
Catalog Number: 25544
Epoch time:      18261
57919989   =   yrday
fracday
Element set:     916
Inclination:       51
6367  deg
RA of node:       273
3003  deg
Eccentricity:     
0004668     
Arg of perigee:   169
8102  deg
Mean anomaly:     190
3146  deg
Mean motion:   15
53877375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1303
Checksum:              334


Coasting Arc #18 (Orbit 1318)
---------------------------------------

Vector Time (GMT): 2018/262/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943674
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         144745
05                 A    =         6790062
18  meter
 Y    =        6777168
89  meter          E    =           
0015424
 Z    =        -196886
93                 I    =           51
27682
 XDOT =      -4803
401421                 Wp   =          146
23102
 YDOT =        -64
236068  meter/sec      RA   =          267
44202  deg
 ZDOT =      -5981
112785                 TA   =           35
90161
                                          MA   =           35
79807
                                          Ha   =            222
104  n
mi
                                          Hp   =            214
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         474885
34                 X    =           69906
48
 Y    =       22234806
07  feet           Y    =         6778369
07  meter
 Z    =        -645954
51                 Z    =         -196366
00
 XDOT =     -15759
191015                 XDOT =       -4773
273115
 YDOT =       -210
748254  feet/sec       YDOT =        -117
782944  meter/sec
 ZDOT =     -19623
073441                 ZDOT =       -6004
372788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9845293
89                 X    =        -3000845
58
 Y    =      -19942023
82  feet           Y    =        -6078328
86  meter
 Z    =        -644397
83                 Z    =         -196412
46
 XDOT =      12795
042144                 XDOT =        3899
928846
 YDOT =      -5704
763159  feet/sec       YDOT =       -1738
811811  meter/sec
 ZDOT =     -19727
386272                 ZDOT =       -6012
907336


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   18262
60820749  
00016717  00000-0  10270-3 0  9170
2 25544  51
6375 268
1716 0004400 174
1202 186
0003 15
53871811 13197


Satellite: ISS
Catalog Number: 25544
Epoch time:      18262
60820749   =   yrday
fracday
Element set:     917
Inclination:       51
6375  deg
RA of node:       268
1716  deg
Eccentricity:     
0004400     
Arg of perigee:   174
1202  deg
Mean anomaly:     186
0003  deg
Mean motion:   15
53871811  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1319
Checksum:              291
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