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

 
Date: June 5th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 20352 94 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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


154/16:09:12 500 -0 0 -0 0 0 0
N/A 0 0 -0 0 227 4
000/00:00:25 000 0 0 0 0 218 6

155/08:40:30 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 218 3

157/09:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 7
000/00:00:00 000 0 0 0 0 218 1

161/12:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 0
000/00:00:00 000 0 0 0 0 217 6

Coasting Arc #1 (Orbit 1311)
---------------------------------------

Vector Time (GMT): 2019/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965102
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4605290
39                 A    =         6788583
83  meter
 Y    =        1568618
71  meter          E    =           
0011806
 Z    =       -4742129
59                 I    =           51
99076
 XDOT =        454
765099                 Wp   =           69
22977
 YDOT =       7110
470982  meter/sec      RA   =           68
43173  deg
 ZDOT =       2803
362861                 TA   =          228
40970
                                          MA   =          228
51094
                                          Ha   =            227
479  n
mi
                                          Hp   =            218
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15109220
43                 X    =         4610442
30
 Y    =        5146386
85  feet           Y    =         1620147
89  meter
 Z    =      -15558167
95                 Z    =        -4719745
75
 XDOT =       1492
011481                 XDOT =         361
602632
 YDOT =      23328
316871  feet/sec       YDOT =        7115
035114  meter/sec
 ZDOT =       9197
384714                 ZDOT =        2805
346874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9869370
59                 X    =         3008184
16
 Y    =      -12669412
22  feet           Y    =        -3861636
84  meter
 Z    =      -15456776
77                 Z    =        -4711225
56
 XDOT =      21574
256642                 XDOT =        6575
833424
 YDOT =       5614
345039  feet/sec       YDOT =        1711
252368  meter/sec
 ZDOT =       9205
584513                 ZDOT =        2805
862160


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   19154
51112949  
00016717  00000-0  10270-3 0  9009
2 25544  51
6430  69
1783 0007760   6
4780 353
6470 15
51167537 13126


Satellite: ISS
Catalog Number: 25544
Epoch time:      19154
51112949   =   yrday
fracday
Element set:     900
Inclination:       51
6430  deg
RA of node:        69
1783  deg
Eccentricity:     
0007760     
Arg of perigee:     6
4780  deg
Mean anomaly:     353
6470  deg
Mean motion:   15
51167537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1312
Checksum:              299


Coasting Arc #2 (Orbit 1314)
---------------------------------------

Vector Time (GMT): 2019/154/16:09:25
000
Vector Time (MET): N/A
Weight (LBS)     : 945426
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2192535
23                 A    =         6797893
18  meter
 Y    =       -6412651
36  meter          E    =           
0007931
 Z    =        -533164
88                 I    =           52
01907
 XDOT =       4623
501100                 Wp   =           93
92866
 YDOT =      -1087
885882  meter/sec      RA   =           67
60257  deg
 ZDOT =      -6006
066239                 TA   =           91
78184
                                          MA   =           91
69099
                                          Ha   =            227
385  n
mi
                                          Hp   =            218
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7193357
04                 X    =        -2118074
32
 Y    =      -21038882
40  feet           Y    =        -6436753
39  meter
 Z    =       -1749228
60                 Z    =         -543635
76
 XDOT =      15168
966862                 XDOT =        4664
497008
 YDOT =      -3569
179402  feet/sec       YDOT =       -1035
952416  meter/sec
 ZDOT =     -19704
941730                 ZDOT =       -5983
507336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10388927
66                 X    =        -3166545
15
 Y    =       19654090
50  feet           Y    =         5990566
78  meter
 Z    =       -1796014
37                 Z    =         -547425
18
 XDOT =     -11657
848427                 XDOT =       -3553
312201
 YDOT =      -7930
900492  feet/sec       YDOT =       -2417
338470  meter/sec
 ZDOT =     -19602
454983                 ZDOT =       -5974
828279


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   19154
70440364  
00016717  00000-0  10270-3 0  9016
2 25544  51
6425  68
2193 0007660   5
5344 354
5890 15
51141091 13156


Satellite: ISS
Catalog Number: 25544
Epoch time:      19154
70440364   =   yrday
fracday
Element set:     901
Inclination:       51
6425  deg
RA of node:        68
2193  deg
Eccentricity:     
0007660     
Arg of perigee:     5
5344  deg
Mean anomaly:     354
5890  deg
Mean motion:   15
51141091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1315
Checksum:              286


Coasting Arc #3 (Orbit 1325)
---------------------------------------

Vector Time (GMT): 2019/155/08:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2631340
36                 A    =         6787081
55  meter
 Y    =        3661601
89  meter          E    =           
0007295
 Z    =        5066540
01                 I    =           51
97347
 XDOT =      -4514
244039                 Wp   =           52
08600
 YDOT =      -5895
056347  meter/sec      RA   =           64
21316  deg
 ZDOT =       1918
358212                 TA   =           19
41233
                                          MA   =           19
38457
                                          Ha   =            227
518  n
mi
                                          Hp   =            218
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8633006
43                 X    =        -2696700
53
 Y    =       12013129
57  feet           Y    =         3631810
05  meter
 Z    =       16622506
60                 Z    =         5053599
73
 XDOT =     -14810
511939                 XDOT =       -4457
306733
 YDOT =     -19340
736045  feet/sec       YDOT =       -5945
219770  meter/sec
 ZDOT =       6293
826156                 ZDOT =        1896
566733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3671903
24                 X    =        -1119196
11
 Y    =       14398744
45  feet           Y    =         4388737
31  meter
 Z    =       16563365
98                 Z    =         5048513
95
 XDOT =     -19910
035578                 XDOT =       -6068
578844
 YDOT =     -12194
981179  feet/sec       YDOT =       -3717
030263  meter/sec
 ZDOT =       6195
620926                 ZDOT =        1888
425258


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   19155
41308011  
00016717  00000-0  10270-3 0  9028
2 25544  51
6416  64
7019 0007705   8
6055 351
5227 15
51192646 13262


Satellite: ISS
Catalog Number: 25544
Epoch time:      19155
41308011   =   yrday
fracday
Element set:     902
Inclination:       51
6416  deg
RA of node:        64
7019  deg
Eccentricity:     
0007705     
Arg of perigee:     8
6055  deg
Mean anomaly:     351
5227  deg
Mean motion:   15
51192646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1326
Checksum:              284


Coasting Arc #4 (Orbit 1340)
---------------------------------------

Vector Time (GMT): 2019/156/08:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2889729
74                 A    =         6786419
78  meter
 Y    =       -3193687
00  meter          E    =           
0018564
 Z    =       -5259756
78                 I    =           51
95530
 XDOT =       4595
074965                 Wp   =           58
23227
 YDOT =       6013
508088  meter/sec      RA   =           59
26710  deg
 ZDOT =      -1120
214008                 TA   =          201
01446
                                          MA   =          201
09085
                                          Ha   =            227
616  n
mi
                                          Hp   =            218
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9480740
61                 X    =         2950776
77
 Y    =      -10477975
73  feet           Y    =        -3161029
71  meter
 Z    =      -17256419
87                 Z    =        -5245571
81
 XDOT =      15075
705265                 XDOT =        4532
930086
 YDOT =      19729
357244  feet/sec       YDOT =        6064
546168  meter/sec
 ZDOT =      -3675
242808                 ZDOT =       -1098
042577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4802595
90                 X    =         1463831
23
 Y    =      -13373024
83  feet           Y    =        -4076097
97  meter
 Z    =      -17191676
01                 Z    =        -5240022
85
 XDOT =      20574
708816                 XDOT =        6271
171247
 YDOT =      12013
091946  feet/sec       YDOT =        3661
590425  meter/sec
 ZDOT =      -3575
336255                 ZDOT =       -1089
762490


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   19156
37945690  
00016717  00000-0  10270-3 0  9035
2 25544  51
6416  59
9056 0007827  12
9966 347
1386 15
51158190 13413


Satellite: ISS
Catalog Number: 25544
Epoch time:      19156
37945690   =   yrday
fracday
Element set:     903
Inclination:       51
6416  deg
RA of node:        59
9056  deg
Eccentricity:     
0007827     
Arg of perigee:    12
9966  deg
Mean anomaly:     347
1386  deg
Mean motion:   15
51158190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1341
Checksum:              332


Coasting Arc #5 (Orbit 1356)
---------------------------------------

Vector Time (GMT): 2019/157/08:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3203488
48                 A    =         6785960
23  meter
 Y    =        2700052
06  meter          E    =           
0008442
 Z    =        5333960
87                 I    =           51
93584
 XDOT =      -4653
552767                 Wp   =           33
04454
 YDOT =      -6087
327658  meter/sec      RA   =           54
32066  deg
 ZDOT =        293
233239                 TA   =           54
21062
                                          MA   =           54
13218
                                          Ha   =            227
794  n
mi
                                          Hp   =            217
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10510132
80                 X    =        -3259352
53
 Y    =        8858438
53  feet           Y    =         2663915
08  meter
 Z    =       17499871
61                 Z    =         5318264
34
 XDOT =     -15267
561572                 XDOT =       -4586
561034
 YDOT =     -19971
547433  feet/sec       YDOT =       -6138
992422  meter/sec
 ZDOT =        962
051308                 ZDOT =         270
789640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6167119
42                 X    =        -1879738
00
 Y    =       12385500
85  feet           Y    =         3775100
66  meter
 Z    =       17428319
99                 Z    =         5312151
93
 XDOT =     -21112
652715                 XDOT =       -6435
136548
 YDOT =     -11693
155419  feet/sec       YDOT =       -3564
073772  meter/sec
 ZDOT =        860
925464                 ZDOT =         262
410081


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   19157
41025683  
00016717  00000-0  10270-3 0  9043
2 25544  51
6413  54
7910 0007883  16
2719 343
8684 15
51181268 13570


Satellite: ISS
Catalog Number: 25544
Epoch time:      19157
41025683   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:        54
7910  deg
Eccentricity:     
0007883     
Arg of perigee:    16
2719  deg
Mean anomaly:     343
8684  deg
Mean motion:   15
51181268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              317


Coasting Arc #6 (Orbit 1356)
---------------------------------------

Vector Time (GMT): 2019/157/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3986383
69                 A    =         6786331
62  meter
 Y    =       -1547041
43  meter          E    =           
0017426
 Z    =       -5283080
17                 I    =           51
93646
 XDOT =       3813
481280                 Wp   =           70
75479
 YDOT =       6563
918447  meter/sec      RA   =           54
14013  deg
 ZDOT =        963
551265                 TA   =          208
40056
                                          MA   =          208
49564
                                          Ha   =            227
743  n
mi
                                          Hp   =            218
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13078686
64                 X    =         4029049
11
 Y    =       -5075595
24  feet           Y    =        -1502223
38  meter
 Z    =      -17332940
18                 Z    =        -5263612
48
 XDOT =      12511
421523                 XDOT =        3735
117855
 YDOT =      21535
165510  feet/sec       YDOT =        6606
125132  meter/sec
 ZDOT =       3161
257430                 ZDOT =         981
886576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7665421
99                 X    =         2336420
62
 Y    =      -11879229
39  feet           Y    =        -3620789
12  meter
 Z    =      -17244411
89                 Z    =        -5256096
74
 XDOT =      21917
915828                 XDOT =        6680
580744
 YDOT =       9473
626065  feet/sec       YDOT =        2887
561224  meter/sec
 ZDOT =       3243
682953                 ZDOT =         988
674564


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   19157
41025743  
00016717  00000-0  10270-3 0  9051
2 25544  51
6417  54
7908 0007887  16
6924 343
4485 15
51161153 13573


Satellite: ISS
Catalog Number: 25544
Epoch time:      19157
41025743   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:        54
7908  deg
Eccentricity:     
0007887     
Arg of perigee:    16
6924  deg
Mean anomaly:     343
4485  deg
Mean motion:   15
51161153  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              318


Coasting Arc #7 (Orbit 1372)
---------------------------------------

Vector Time (GMT): 2019/158/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4339668
58                 A    =         6787062
73  meter
 Y    =        1088881
70  meter          E    =           
0012691
 Z    =        5100209
01                 I    =           51
91899
 XDOT =      -3729
400915                 Wp   =           33
93663
 YDOT =      -6456
546700  meter/sec      RA   =           49
19261  deg
 ZDOT =      -1782
425738                 TA   =           73
31298
                                          MA   =           73
17372
                                          Ha   =            227
891  n
mi
                                          Hp   =            217
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14237757
79                 X    =        -4376296
08
 Y    =        3572446
51  feet           Y    =         1040146
84  meter
 Z    =       16732969
20                 Z    =         5079039
85
 XDOT =     -12235
567308                 XDOT =       -3648
266802
 YDOT =     -21182
895998  feet/sec       YDOT =       -6497
797526  meter/sec
 ZDOT =      -5847
853471                 ZDOT =       -1800
345699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9287984
46                 X    =        -2830977
66
 Y    =       11507369
28  feet           Y    =         3507446
16  meter
 Z    =       16636771
81                 Z    =         5070888
05
 XDOT =     -21667
443536                 XDOT =       -6604
236790
 YDOT =      -8858
419762  feet/sec       YDOT =       -2700
046344  meter/sec
 ZDOT =      -5928
400260                 ZDOT =       -1806
976399


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   19158
44105704  
00016717  00000-0  10270-3 0  9062
2 25544  51
6420  49
6761 0007873  19
9151 340
2306 15
51170424 13736


Satellite: ISS
Catalog Number: 25544
Epoch time:      19158
44105704   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:        49
6761  deg
Eccentricity:     
0007873     
Arg of perigee:    19
9151  deg
Mean anomaly:     340
2306  deg
Mean motion:   15
51170424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1373
Checksum:              292


Coasting Arc #8 (Orbit 1387)
---------------------------------------

Vector Time (GMT): 2019/159/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4702315
89                 A    =         6788130
49  meter
 Y    =        -730165
73  meter          E    =           
0014542
 Z    =       -4851437
85                 I    =           51
90068
 XDOT =       3583
104813                 Wp   =           74
88949
 YDOT =       6269
141246  meter/sec      RA   =           44
24337  deg
 ZDOT =       2539
462970                 TA   =          219
99180
                                          MA   =          220
09899
                                          Ha   =            227
911  n
mi
                                          Hp   =            217
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15427545
58                 X    =         4733696
76
 Y    =       -2395556
85  feet           Y    =         -677404
98  meter
 Z    =      -15916790
86                 Z    =        -4828519
80
 XDOT =      11755
593219                 XDOT =        3500
399968
 YDOT =      20568
048707  feet/sec       YDOT =        6308
747238  meter/sec
 ZDOT =       8331
571423                 ZDOT =        2556
668259

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10746823
18                 X    =         3275631
70
 Y    =      -11469802
91  feet           Y    =        -3495995
93  meter
 Z    =      -15812700
57                 Z    =        -4819711
13
 XDOT =      21060
799318                 XDOT =        6419
331632
 YDOT =       8186
127207  feet/sec       YDOT =        2495
131573  meter/sec
 ZDOT =       8408
891303                 ZDOT =        2563
030069


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   19159
40742940  
00016717  00000-0  10270-3 0  9079
2 25544  51
6427  44
8795 0007935  23
6417 336
5097 15
51175940 13882


Satellite: ISS
Catalog Number: 25544
Epoch time:      19159
40742940   =   yrday
fracday
Element set:     907
Inclination:       51
6427  deg
RA of node:        44
8795  deg
Eccentricity:     
0007935     
Arg of perigee:    23
6417  deg
Mean anomaly:     336
5097  deg
Mean motion:   15
51175940  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1388
Checksum:              335


Coasting Arc #9 (Orbit 1403)
---------------------------------------

Vector Time (GMT): 2019/160/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5088286
23                 A    =         6789618
48  meter
 Y    =         373226
97  meter          E    =           
0016081
 Z    =        4475060
16                 I    =           51
88068
 XDOT =      -3346
656363                 Wp   =           49
74716
 YDOT =      -6065
791185  meter/sec      RA   =           39
29523  deg
 ZDOT =      -3281
460444                 TA   =           73
30565
                                          MA   =           73
12920
                                          Ha   =            228
085  n
mi
                                          Hp   =            217
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16693852
48                 X    =        -5113818
82
 Y    =        1224497
95  feet           Y    =          316182
90  meter
 Z    =       14681955
91                 Z    =         4450281
35
 XDOT =     -10979
843711                 XDOT =       -3262
638808
 YDOT =     -19900
889715  feet/sec       YDOT =       -6102
745681  meter/sec
 ZDOT =     -10765
946338                 ZDOT =       -3297
513809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12262769
55                 X    =        -3737692
16
 Y    =       11536854
52  feet           Y    =         3516433
26  meter
 Z    =       14569468
27                 Z    =         4440773
93
 XDOT =     -20171
622966                 XDOT =       -6148
310680
 YDOT =      -7679
138191  feet/sec       YDOT =       -2340
601321  meter/sec
 ZDOT =     -10838
056519                 ZDOT =       -3303
439627


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   19160
43822581  
00016717  00000-0  10270-3 0  9085
2 25544  51
6425  39
7645 0007995  27
7234 332
4342 15
51166025 14046


Satellite: ISS
Catalog Number: 25544
Epoch time:      19160
43822581   =   yrday
fracday
Element set:     908
Inclination:       51
6425  deg
RA of node:        39
7645  deg
Eccentricity:     
0007995     
Arg of perigee:    27
7234  deg
Mean anomaly:     332
4342  deg
Mean motion:   15
51166025  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1404
Checksum:              305


Coasting Arc #10 (Orbit 1418)
---------------------------------------

Vector Time (GMT): 2019/161/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5450511
20                 A    =         6791086
88  meter
 Y    =        -131551
86  meter          E    =           
0011714
 Z    =       -4054572
19                 I    =           51
85996
 XDOT =       3052
366625                 Wp   =           65
94208
 YDOT =       5821
525501  meter/sec      RA   =           34
34644  deg
 ZDOT =       3927
974276                 TA   =          244
70542
                                          MA   =          244
82682
                                          Ha   =            228
070  n
mi
                                          Hp   =            217
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17882254
60                 X    =         5471271
96
 Y    =        -431600
58  feet           Y    =          -70483
93  meter
 Z    =      -13302402
20                 Z    =        -4028045
31
 XDOT =      10014
326199                 XDOT =        2967
961947
 YDOT =      19099
493115  feet/sec       YDOT =        5855
186872  meter/sec
 ZDOT =      12887
054710                 ZDOT =        3942
597071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13475318
18                 X    =         4107276
98
 Y    =      -11898126
52  feet           Y    =        -3626548
96  meter
 Z    =      -13182017
98                 Z    =        -4017879
08
 XDOT =      19024
102230                 XDOT =        5798
546360
 YDOT =       7245
391193  feet/sec       YDOT =        2208
395236  meter/sec
 ZDOT =      12952
694820                 ZDOT =        3947
981381


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   19161
40459663  
00016717  00000-0  10270-3 0  9091
2 25544  51
6432  34
9686 0007954  30
9157 329
2461 15
51183312 14191


Satellite: ISS
Catalog Number: 25544
Epoch time:      19161
40459663   =   yrday
fracday
Element set:     909
Inclination:       51
6432  deg
RA of node:        34
9686  deg
Eccentricity:     
0007954     
Arg of perigee:    30
9157  deg
Mean anomaly:     329
2461  deg
Mean motion:   15
51183312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1419
Checksum:              316


Coasting Arc #11 (Orbit 1420)
---------------------------------------

Vector Time (GMT): 2019/161/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3406466
45                 A    =         6786434
05  meter
 Y    =       -2675024
82  meter          E    =           
0018416
 Z    =       -5239113
14                 I    =           51
84082
 XDOT =       5712
509187                 Wp   =           75
31348
 YDOT =       4947
459699  meter/sec      RA   =           33
75009  deg
 ZDOT =       1196
216877                 TA   =          206
10885
                                          MA   =          206
20184
                                          Ha   =            227
984  n
mi
                                          Hp   =            217
553

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11176071
04                 X    =         3461574
81
 Y    =       -8776328
14  feet           Y    =        -2636622
67  meter
 Z    =      -17188691
41                 Z    =        -5222432
26
 XDOT =      18741
828042                 XDOT =        5650
950173
 YDOT =      16231
823159  feet/sec       YDOT =        5010
996663  meter/sec
 ZDOT =       3924
596053                 ZDOT =        1223
817018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7694113
64                 X    =        -2345165
84
 Y    =      -12055564
38  feet           Y    =        -3674536
02  meter
 Z    =      -17112673
51                 Z    =        -5215942
89
 XDOT =      17016
407732                 XDOT =        5186
601077
 YDOT =     -16570
340671  feet/sec       YDOT =       -5050
639836  meter/sec
 ZDOT =       4049
227545                 ZDOT =        1234
204556


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   19161
53344438  
00016717  00000-0  10270-3 0  9100
2 25544  51
6429  34
3293 0007916  30
1730 329
9876 15
51187896 14213


Satellite: ISS
Catalog Number: 25544
Epoch time:      19161
53344438   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:        34
3293  deg
Eccentricity:     
0007916     
Arg of perigee:    30
1730  deg
Mean anomaly:     329
9876  deg
Mean motion:   15
51187896  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1421
Checksum:              317


Coasting Arc #12 (Orbit 1436)
---------------------------------------

Vector Time (GMT): 2019/162/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3893551
49                 A    =         6787258
30  meter
 Y    =        2369062
13  meter          E    =           
0013595
 Z    =        5024501
52                 I    =           51
81636
 XDOT =      -5572
839280                 Wp   =           42
55287
 YDOT =      -4867
404243  meter/sec      RA   =           28
79527  deg
 ZDOT =      -2010
526634                 TA   =           67
00574
                                          MA   =           66
86239
                                          Ha   =            228
080  n
mi
                                          Hp   =            217
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12774119
07                 X    =        -3944159
92
 Y    =        7772513
54  feet           Y    =         2325238
26  meter
 Z    =       16484585
05                 Z    =         5005465
38
 XDOT =     -18283
593437                 XDOT =       -5508
230352
 YDOT =     -15969
174027  feet/sec       YDOT =       -4929
362195  meter/sec
 ZDOT =      -6596
215991                 ZDOT =       -2037
440989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6779104
62                 X    =         2066271
09
 Y    =       13434416
74  feet           Y    =         4094810
22  meter
 Z    =       16397921
10                 Z    =         4998086
35
 XDOT =     -16320
875834                 XDOT =       -4974
602954
 YDOT =      16487
360080  feet/sec       YDOT =        5025
347352  meter/sec
 ZDOT =      -6717
732452                 ZDOT =       -2047
564851


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   19162
56423772  
00016717  00000-0  10270-3 0  9114
2 25544  51
6437  29
2138 0007872  32
6782 327
4855 15
51208439 14372


Satellite: ISS
Catalog Number: 25544
Epoch time:      19162
56423772   =   yrday
fracday
Element set:     911
Inclination:       51
6437  deg
RA of node:        29
2138  deg
Eccentricity:     
0007872     
Arg of perigee:    32
6782  deg
Mean anomaly:     327
4855  deg
Mean motion:   15
51208439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1437
Checksum:              320


Coasting Arc #13 (Orbit 1451)
---------------------------------------

Vector Time (GMT): 2019/163/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4354755
96                 A    =         6788497
19  meter
 Y    =       -2162887
48  meter          E    =           
0015232
 Z    =       -4748891
87                 I    =           51
78962
 XDOT =       5345
312070                 Wp   =           78
98990
 YDOT =       4733
809976  meter/sec      RA   =           23
83880  deg
 ZDOT =       2755
995511                 TA   =          218
23241
                                          MA   =          218
34053
                                          Ha   =            228
126  n
mi
                                          Hp   =            217
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14287257
10                 X    =         4401685
94
 Y    =       -7096087
54  feet           Y    =        -2113926
66  meter
 Z    =      -15580353
89                 Z    =        -4727624
21
 XDOT =      17537
113091                 XDOT =        5278
592810
 YDOT =      15530
872625  feet/sec       YDOT =        4793
211665  meter/sec
 ZDOT =       9041
980024                 ZDOT =        2781
799624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6245988
81                 X    =        -1903777
39
 Y    =      -14780849
64  feet           Y    =        -4505202
97  meter
 Z    =      -15483594
84                 Z    =        -4719399
71
 XDOT =      15446
156303                 XDOT =        4707
988441
 YDOT =     -16085
272361  feet/sec       YDOT =       -4902
791016  meter/sec
 ZDOT =       9158
461648                 ZDOT =        2791
499110


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   19163
53060667  
00016717  00000-0  10270-3 0  9123
2 25544  51
6428  24
4169 0007935  36
8443 323
3252 15
51189196 14524


Satellite: ISS
Catalog Number: 25544
Epoch time:      19163
53060667   =   yrday
fracday
Element set:     912
Inclination:       51
6428  deg
RA of node:        24
4169  deg
Eccentricity:     
0007935     
Arg of perigee:    36
8443  deg
Mean anomaly:     323
3252  deg
Mean motion:   15
51189196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1452
Checksum:              311


Coasting Arc #14 (Orbit 1467)
---------------------------------------

Vector Time (GMT): 2019/164/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4829627
90                 A    =         6789966
58  meter
 Y    =        1964617
62  meter          E    =           
0017018
 Z    =        4342794
39                 I    =           51
76341
 XDOT =      -5029
029218                 Wp   =           57
33741
 YDOT =      -4621
048822  meter/sec      RA   =           18
88308  deg
 ZDOT =      -3483
391683                 TA   =           68
09455
                                          MA   =           67
91369
                                          Ha   =            228
214  n
mi
                                          Hp   =            217
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15845235
89                 X    =        -4872332
92
 Y    =        6445595
88  feet           Y    =         1910370
04  meter
 Z    =       14248013
09                 Z    =         4319230
19
 XDOT =     -16499
439692                 XDOT =       -4960
061044
 YDOT =     -15160
921332  feet/sec       YDOT =       -4676
900904  meter/sec
 ZDOT =     -11428
450403                 ZDOT =       -3507
654071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5785584
24                 X    =         1763446
08
 Y    =       16192160
54  feet           Y    =         4935370
53  meter
 Z    =       14140864
03                 Z    =         4310135
36
 XDOT =     -14643
469148                 XDOT =       -4463
329396
 YDOT =      15363
055992  feet/sec       YDOT =        4682
659466  meter/sec
 ZDOT =     -11537
938081                 ZDOT =       -3516
763527


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   19164
56139803  
00016717  00000-0  10270-3 0  9137
2 25544  51
6424  19
3017 0007962  39
8931 320
2804 15
51211691 14682


Satellite: ISS
Catalog Number: 25544
Epoch time:      19164
56139803   =   yrday
fracday
Element set:     913
Inclination:       51
6424  deg
RA of node:        19
3017  deg
Eccentricity:     
0007962     
Arg of perigee:    39
8931  deg
Mean anomaly:     320
2804  deg
Mean motion:   15
51211691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1468
Checksum:              303


Coasting Arc #15 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2019/165/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5242786
72                 A    =         6791596
05  meter
 Y    =       -1868244
22  meter          E    =           
0012210
 Z    =       -3898775
68                 I    =           51
73552
 XDOT =       4644
966309                 Wp   =           70
49831
 YDOT =       4490
724842  meter/sec      RA   =           13
92650  deg
 ZDOT =       4108
779409                 TA   =          242
55445
                                          MA   =          242
67868
                                          Ha   =            228
226  n
mi
                                          Hp   =            217
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17200743
84                 X    =         5282226
56
 Y    =       -6129410
18  feet           Y    =        -1809394
63  meter
 Z    =      -12791258
80                 Z    =        -3873212
43
 XDOT =      15239
390776                 XDOT =        4574
446175
 YDOT =      14733
349219  feet/sec       YDOT =        4542
273222  meter/sec
 ZDOT =      13480
247404                 ZDOT =        4131
172475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5714859
08                 X    =        -1741889
05
 Y    =      -17427991
07  feet           Y    =        -5312051
68  meter
 Z    =      -12675057
11                 Z    =        -3863357
41
 XDOT =      13821
697412                 XDOT =        4212
853371
 YDOT =     -14374
868329  feet/sec       YDOT =       -4381
459867  meter/sec
 ZDOT =      13581
259578                 ZDOT =        4139
567920


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   19165
52776656  
00016717  00000-0  10270-3 0  9148
2 25544  51
6411  14
5056 0007823  44
3106 315
8670 15
51185206 14839


Satellite: ISS
Catalog Number: 25544
Epoch time:      19165
52776656   =   yrday
fracday
Element set:     914
Inclination:       51
6411  deg
RA of node:        14
5056  deg
Eccentricity:     
0007823     
Arg of perigee:    44
3106  deg
Mean anomaly:     315
8670  deg
Mean motion:   15
51185206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1483
Checksum:              301


Coasting Arc #16 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2019/166/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5644160
86                 A    =         6793228
51  meter
 Y    =        1770566
91  meter          E    =           
0018989
 Z    =        3329807
93                 I    =           51
70935
 XDOT =      -4165
384948                 Wp   =           74
36857
 YDOT =      -4406
189735  meter/sec      RA   =            8
96899  deg
 ZDOT =      -4690
298639                 TA   =           66
95079
                                          MA   =           66
75067
                                          Ha   =            228
238  n
mi
                                          Hp   =            216
979

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18517588
12                 X    =        -5679714
83
 Y    =        5808946
54  feet           Y    =         1707250
61  meter
 Z    =       10924566
71                 Z    =         3302304
44
 XDOT =     -13665
961114                 XDOT =       -4093
021061
 YDOT =     -14456
003068  feet/sec       YDOT =       -4452
364607  meter/sec
 ZDOT =     -15388
118893                 ZDOT =       -4710
357636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5684437
18                 X    =         1732616
45
 Y    =       18629206
83  feet           Y    =         5678182
24  meter
 Z    =       10799579
35                 Z    =         3291711
79
 XDOT =     -13189
552211                 XDOT =       -4020
175514
 YDOT =      13050
201964  feet/sec       YDOT =        3977
701559  meter/sec
 ZDOT =     -15478
544708                 ZDOT =       -4717
860427


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   19166
55855558  
00016717  00000-0  10270-3 0  9152
2 25544  51
6418   9
3890 0007870  46
5003 313
6802 15
51217804 14996


Satellite: ISS
Catalog Number: 25544
Epoch time:      19166
55855558   =   yrday
fracday
Element set:     915
Inclination:       51
6418  deg
RA of node:         9
3890  deg
Eccentricity:     
0007870     
Arg of perigee:    46
5003  deg
Mean anomaly:     313
6802  deg
Mean motion:   15
51217804  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1499
Checksum:              322


Coasting Arc #17 (Orbit 1513)
---------------------------------------

Vector Time (GMT): 2019/167/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5956839
82                 A    =         6794802
72  meter
 Y    =       -1761991
20  meter          E    =           
0012772
 Z    =       -2751179
33                 I    =           51
67925
 XDOT =       3650
974965                 Wp   =           53
25455
 YDOT =       4337
294828  meter/sec      RA   =            4
01124  deg
 ZDOT =       5151
294216                 TA   =          275
67110
                                          MA   =          275
81673
                                          Ha   =            228
373  n
mi
                                          Hp   =            216
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19543437
72                 X    =         5989463
94
 Y    =       -5780811
02  feet           Y    =        -1695194
73  meter
 Z    =       -9026178
90                 Z    =        -2722164
17
 XDOT =      11978
264321                 XDOT =        3577
180508
 YDOT =      14229
969908  feet/sec       YDOT =        4377
709043  meter/sec
 ZDOT =      16900
571575                 ZDOT =        5168
850923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5986388
52                 X    =        -1824651
22
 Y    =      -19541994
09  feet           Y    =        -5956399
80  meter
 Z    =       -8894338
58                 Z    =        -2710994
40
 XDOT =      12681
090825                 XDOT =        3865
196484
 YDOT =     -11576
341671  feet/sec       YDOT =       -3528
468941  meter/sec
 ZDOT =      16979
649396                 ZDOT =        5175
397136


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   19167
52492178  
00016717  00000-0  10270-3 0  9166
2 25544  51
6398   4
5925 0007911  52
1407 308
0459 15
51180131 15142


Satellite: ISS
Catalog Number: 25544
Epoch time:      19167
52492178   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:         4
5925  deg
Eccentricity:     
0007911     
Arg of perigee:    52
1407  deg
Mean anomaly:     308
0459  deg
Mean motion:   15
51180131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1514
Checksum:              302


Coasting Arc #18 (Orbit 1529)
---------------------------------------

Vector Time (GMT): 2019/168/12:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931378
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6233952
82                 A    =         6796058
09  meter
 Y    =        1733630
83  meter          E    =           
0019305
 Z    =        2060803
43                 I    =           51
65054
 XDOT =      -3050
287830                 Wp   =           90
90358
 YDOT =      -4331
904748  meter/sec      RA   =          359
05348  deg
 ZDOT =      -5538
360443                 TA   =           66
33084
                                          MA   =           66
12834
                                          Ha   =            228
272  n
mi
                                          Hp   =            216
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20452601
11                 X    =        -6262885
70
 Y    =        5687765
19  feet           Y    =         1663756
23  meter
 Z    =        6761166
13                 Z    =         2030451
26
 XDOT =     -10007
506005                 XDOT =       -2974
718235
 YDOT =     -14212
285917  feet/sec       YDOT =       -4365
591607  meter/sec
 ZDOT =     -18170
473894                 ZDOT =       -5552
994897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6253220
99                 X    =         1905981
76
 Y    =       20332301
47  feet           Y    =         6197285
49  meter
 Z    =        6623267
82                 Z    =         2018772
03
 XDOT =     -12451
913514                 XDOT =       -3795
343239
 YDOT =       9818
771200  feet/sec       YDOT =        2992
761462  meter/sec
 ZDOT =     -18236
293854                 ZDOT =       -5558
422367


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   19168
55570894  
00016717  00000-0  10270-3 0  9173
2 25544  51
6398 359
4764 0007853  54
0773 306
1106 15
51227416 15301


Satellite: ISS
Catalog Number: 25544
Epoch time:      19168
55570894   =   yrday
fracday
Element set:     917
Inclination:       51
6398  deg
RA of node:       359
4764  deg
Eccentricity:     
0007853     
Arg of perigee:    54
0773  deg
Mean anomaly:     306
1106  deg
Mean motion:   15
51227416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1530
Checksum:              328
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