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

 
Date: May 30th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14730 1961 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 1234)
---------------------------------------

Vector Time (GMT): 2019/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965102
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4162228
57                 A    =         6786388
69  meter
 Y    =        1103738
75  meter          E    =           
0005486
 Z    =        5242906
37                 I    =           52
00566
 XDOT =       -513
718113                 Wp   =           17
82321
 YDOT =      -7555
951762  meter/sec      RA   =           93
14639  deg
 ZDOT =       1187
604847                 TA   =           60
86716
                                          MA   =           60
81226
                                          Ha   =            226
919  n
mi
                                          Hp   =            219
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13655605
54                 X    =        -4199728
90
 Y    =        3621190
12  feet           Y    =         1056983
72  meter
 Z    =       17201136
38                 Z    =         5222596
64
 XDOT =      -1685
426880                 XDOT =        -434
955901
 YDOT =     -24789
867986  feet/sec       YDOT =       -7561
256221  meter/sec
 ZDOT =       3896
341363                 ZDOT =        1185
300101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2331149
47                 X    =         -710534
36
 Y    =       14047049
74  feet           Y    =         4281540
76  meter
 Z    =       17108881
00                 Z    =         5214786
93
 XDOT =     -22294
335384                 XDOT =       -6795
313425
 YDOT =      -8414
517571  feet/sec       YDOT =       -2564
744956  meter/sec
 ZDOT =       3886
631604                 ZDOT =        1184
645313


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   19149
55037642  
00016717  00000-0  10270-3 0  9003
2 25544  51
6403  93
7954 0007624 347
8071  12
2894 15
51185904 12353


Satellite: ISS
Catalog Number: 25544
Epoch time:      19149
55037642   =   yrday
fracday
Element set:     900
Inclination:       51
6403  deg
RA of node:        93
7954  deg
Eccentricity:     
0007624     
Arg of perigee:   347
8071  deg
Mean anomaly:      12
2894  deg
Mean motion:   15
51185904  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1235
Checksum:              310


Coasting Arc #2 (Orbit 1249)
---------------------------------------

Vector Time (GMT): 2019/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965102
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4159351
97                 A    =         6786086
35  meter
 Y    =        -562214
54  meter          E    =           
0016002
 Z    =       -5344655
11                 I    =           52
00509
 XDOT =        535
040278                 Wp   =           58
77296
 YDOT =       7625
096168  meter/sec      RA   =           88
20294  deg
 ZDOT =       -378
494985                 TA   =          207
58651
                                          MA   =          207
67152
                                          Ha   =            227
002  n
mi
                                          Hp   =            219
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13646167
88                 X    =         4191291
37
 Y    =       -1844535
89  feet           Y    =         -515522
71  meter
 Z    =      -17534957
70                 Z    =        -5324372
75
 XDOT =       1755
381490                 XDOT =         451
573052
 YDOT =      25016
719712  feet/sec       YDOT =        7630
612701  meter/sec
 ZDOT =      -1241
781447                 ZDOT =        -376
098002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3719618
97                 X    =         1133739
86
 Y    =      -13379291
25  feet           Y    =        -4078007
97  meter
 Z    =      -17442876
83                 Z    =        -5316588
86
 XDOT =      22716
476840                 XDOT =        6923
982141
 YDOT =       7952
296394  feet/sec       YDOT =        2423
859941  meter/sec
 ZDOT =      -1231
679251                 ZDOT =        -375
415836


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   19150
51675975  
00016717  00000-0  10270-3 0  9019
2 25544  51
6404  88
9994 0007611 351
9784   8
1244 15
51152049 12501


Satellite: ISS
Catalog Number: 25544
Epoch time:      19150
51675975   =   yrday
fracday
Element set:     901
Inclination:       51
6404  deg
RA of node:        88
9994  deg
Eccentricity:     
0007611     
Arg of perigee:   351
9784  deg
Mean anomaly:       8
1244  deg
Mean motion:   15
51152049  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1250
Checksum:              314


Coasting Arc #3 (Orbit 1265)
---------------------------------------

Vector Time (GMT): 2019/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965102
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4196692
31                 A    =         6786014
14  meter
 Y    =         -23346
64  meter          E    =           
0008760
 Z    =        5331660
43                 I    =           52
00401
 XDOT =       -544
933776                 Wp   =           11
86898
 YDOT =      -7632
111824  meter/sec      RA   =           83
26006  deg
 ZDOT =       -453
881049                 TA   =           82
49008
                                          MA   =           82
39056
                                          Ha   =            227
148  n
mi
                                          Hp   =            218
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13768675
54                 X    =        -4222017
95
 Y    =         -76596
60  feet           Y    =          -70419
15  meter
 Z    =       17492324
24                 Z    =         5311212
65
 XDOT =      -1787
840473                 XDOT =        -457
344089
 YDOT =     -25039
736956  feet/sec       YDOT =       -7637
715864  meter/sec
 ZDOT =      -1489
111054                 ZDOT =        -456
316218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5313945
95                 X    =        -1619690
72
 Y    =       12828924
98  feet           Y    =         3910256
33  meter
 Z    =       17399550
66                 Z    =         5303383
04
 XDOT =     -22921
383839                 XDOT =       -6986
437794
 YDOT =      -7422
958797  feet/sec       YDOT =       -2262
517841  meter/sec
 ZDOT =      -1499
364727                 ZDOT =        -457
006369


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   19151
54756514  
00016717  00000-0  10270-3 0  9023
2 25544  51
6414  83
8845 0007691 354
6496   5
4572 15
51180753 12663


Satellite: ISS
Catalog Number: 25544
Epoch time:      19151
54756514   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:        83
8845  deg
Eccentricity:     
0007691     
Arg of perigee:   354
6496  deg
Mean anomaly:       5
4572  deg
Mean motion:   15
51180753  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1266
Checksum:              320


Coasting Arc #4 (Orbit 1280)
---------------------------------------

Vector Time (GMT): 2019/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965102
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4293095
57                 A    =         6786538
72  meter
 Y    =         554335
73  meter          E    =           
0014764
 Z    =       -5237602
68                 I    =           52
00123
 XDOT =        553
169574                 Wp   =           68
43275
 YDOT =       7529
938777  meter/sec      RA   =           78
31614  deg
 ZDOT =       1258
482087                 TA   =          213
56307
                                          MA   =          213
65669
                                          Ha   =            227
274  n
mi
                                          Hp   =            218
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14084959
22                 X    =         4312019
52
 Y    =        1818686
79  feet           Y    =          602450
60  meter
 Z    =      -17183735
82                 Z    =        -5216702
06
 XDOT =       1814
860808                 XDOT =         462
813434
 YDOT =      24704
523547  feet/sec       YDOT =        7535
619337  meter/sec
 ZDOT =       4128
878237                 ZDOT =        1260
950698

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6830300
43                 X    =         2081875
57
 Y    =      -12581288
71  feet           Y    =        -3834776
80  meter
 Z    =      -17088962
67                 Z    =        -5208715
82
 XDOT =      22761
276603                 XDOT =        6937
637109
 YDOT =       6771
008108  feet/sec       YDOT =        2063
803271  meter/sec
 ZDOT =       4139
272385                 ZDOT =        1261
650223


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   19152
51394471  
00016717  00000-0  10270-3 0  9032
2 25544  51
6421  79
0882 0007751 359
3573    
7567 15
51158684 12811


Satellite: ISS
Catalog Number: 25544
Epoch time:      19152
51394471   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:        79
0882  deg
Eccentricity:     
0007751     
Arg of perigee:   359
3573  deg
Mean anomaly:        
7567  deg
Mean motion:   15
51158684  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1281
Checksum:              317


Coasting Arc #5 (Orbit 1296)
---------------------------------------

Vector Time (GMT): 2019/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965102
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4426994
12                 A    =         6787407
36  meter
 Y    =       -1107762
81  meter          E    =           
0012386
 Z    =        5023066
06                 I    =           51
99635
 XDOT =       -514
828241                 Wp   =           26
17539
 YDOT =      -7363
000733  meter/sec      RA   =           73
37418  deg
 ZDOT =      -2064
785016                 TA   =           83
88737
                                          MA   =           83
74626
                                          Ha   =            227
425  n
mi
                                          Hp   =            218
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14524258
94                 X    =        -4438677
42
 Y    =       -3634392
42  feet           Y    =        -1157334
62  meter
 Z    =       16479875
51                 Z    =         5001532
50
 XDOT =      -1689
069031                 XDOT =        -422
425071
 YDOT =     -24156
826552  feet/sec       YDOT =       -7368
240941  meter/sec
 ZDOT =      -6774
229055                 ZDOT =       -2067
062545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8466933
32                 X    =        -2580721
28
 Y    =       12477211
14  feet           Y    =         3803053
95  meter
 Z    =       16382290
60                 Z    =         4993322
17
 XDOT =     -22327
014128                 XDOT =       -6805
273906
 YDOT =      -6188
764552  feet/sec       YDOT =       -1886
335436  meter/sec
 ZDOT =      -6783
752573                 ZDOT =       -2067
687784


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   19153
54474821  
00016717  00000-0  10270-3 0  9045
2 25544  51
6420  73
9739 0007789   3
1060 357
0138 15
51168188 12979


Satellite: ISS
Catalog Number: 25544
Epoch time:      19153
54474821   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:        73
9739  deg
Eccentricity:     
0007789     
Arg of perigee:     3
1060  deg
Mean anomaly:     357
0138  deg
Mean motion:   15
51168188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1297
Checksum:              318


Coasting Arc #6 (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    =        4605429
84                 A    =         6788581
19  meter
 Y    =        1570659
58  meter          E    =           
0011796
 Z    =       -4741307
96                 I    =           51
99059
 XDOT =        453
076024                 Wp   =           69
24615
 YDOT =       7109
906217  meter/sec      RA   =           68
43175  deg
 ZDOT =       2805
086982                 TA   =          228
41190
                                          MA   =          228
51306
                                          Ha   =            227
473  n
mi
                                          Hp   =            218
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15109677
94                 X    =         4610554
92
 Y    =        5153082
61  feet           Y    =         1622190
17  meter
 Z    =      -15555472
31                 Z    =        -4718923
51
 XDOT =       1486
469894                 XDOT =         359
911622
 YDOT =      23326
463966  feet/sec       YDOT =        7114
451449  meter/sec
 ZDOT =       9203
041278                 ZDOT =        2807
062785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9875837
59                 X    =         3010155
30
 Y    =      -12667621
49  feet           Y    =        -3861091
03  meter
 Z    =      -15454078
58                 Z    =        -4710403
15
 XDOT =      21570
800251                 XDOT =        6574
779917
 YDOT =       5618
531290  feet/sec       YDOT =        1712
528337  meter/sec
 ZDOT =       9211
203889                 ZDOT =        2807
574945


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
51112617  
00016717  00000-0  10270-3 0  9056
2 25544  51
6429  69
1782 0007752   6
4610 353
6639 15
51169541 13120


Satellite: ISS
Catalog Number: 25544
Epoch time:      19154
51112617   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:        69
1782  deg
Eccentricity:     
0007752     
Arg of perigee:     6
4610  deg
Mean anomaly:     353
6639  deg
Mean motion:   15
51169541  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1312
Checksum:              300


Coasting Arc #7 (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    =       -2191113
00                 A    =         6797886
30  meter
 Y    =       -6412975
03  meter          E    =           
0007924
 Z    =        -534997
41                 I    =           52
01889
 XDOT =       4624
376252                 Wp   =           93
97200
 YDOT =      -1085
400224  meter/sec      RA   =           67
60261  deg
 ZDOT =      -6005
850538                 TA   =           91
75821
                                          MA   =           91
66745
                                          Ha   =            227
379  n
mi
                                          Hp   =            218
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7188690
95                 X    =        -2116639
68
 Y    =      -21039944
31  feet           Y    =        -6437061
09  meter
 Z    =       -1755240
86                 Z    =         -545461
35
 XDOT =      15171
838098                 XDOT =        4665
343252
 YDOT =      -3561
024357  feet/sec       YDOT =       -1033
457134  meter/sec
 ZDOT =     -19704
234050                 ZDOT =       -5983
287453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10392928
15                 X    =        -3167764
50
 Y    =       19651393
41  feet           Y    =         5989744
71  meter
 Z    =       -1801995
10                 Z    =         -549248
11
 XDOT =     -11654
074919                 XDOT =       -3552
162035
 YDOT =      -7938
287288  feet/sec       YDOT =       -2419
589965  meter/sec
 ZDOT =     -19601
728611                 ZDOT =       -5974
606881


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
70440006  
00016717  00000-0  10270-3 0  9064
2 25544  51
6424  68
2192 0007652   5
5142 354
6092 15
51143163 13158


Satellite: ISS
Catalog Number: 25544
Epoch time:      19154
70440006   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:        68
2192  deg
Eccentricity:     
0007652     
Arg of perigee:     5
5142  deg
Mean anomaly:     354
6092  deg
Mean motion:   15
51143163  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1315
Checksum:              276


Coasting Arc #8 (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    =       -2633113
78                 A    =         6787071
80  meter
 Y    =        3659309
01  meter          E    =           
0007284
 Z    =        5067272
47                 I    =           51
97328
 XDOT =      -4512
938304                 Wp   =           52
06972
 YDOT =      -5896
874795  meter/sec      RA   =           64
21314  deg
 ZDOT =       1915
826917                 TA   =           19
45388
                                          MA   =           19
42609
                                          Ha   =            227
511  n
mi
                                          Hp   =            218
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8638824
73                 X    =        -2698451
74
 Y    =       12005607
00  feet           Y    =         3629497
46  meter
 Z    =       16624909
69                 Z    =         5054323
63
 XDOT =     -14806
228033                 XDOT =       -4455
968465
 YDOT =     -19346
702084  feet/sec       YDOT =       -5947
023435  meter/sec
 ZDOT =       6285
521381                 ZDOT =        1894
041860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3680109
00                 X    =        -1121697
22
 Y    =       14393918
36  feet           Y    =         4387266
31  meter
 Z    =       16565730
49                 Z    =         5049234
65
 XDOT =     -19908
566857                 XDOT =       -6068
131178
 YDOT =     -12201
532444  feet/sec       YDOT =       -3719
027089  meter/sec
 ZDOT =       6187
345500                 ZDOT =        1885
902908


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
41307553  
00016717  00000-0  10270-3 0  9073
2 25544  51
6415  64
7018 0007698   8
5858 351
5423 15
51194927 13263


Satellite: ISS
Catalog Number: 25544
Epoch time:      19155
41307553   =   yrday
fracday
Element set:     907
Inclination:       51
6415  deg
RA of node:        64
7018  deg
Eccentricity:     
0007698     
Arg of perigee:     8
5858  deg
Mean anomaly:     351
5423  deg
Mean motion:   15
51194927  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1326
Checksum:              320


Coasting Arc #9 (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    =        2892182
40                 A    =         6786409
48  meter
 Y    =       -3190490
81  meter          E    =           
0018557
 Z    =       -5260329
51                 I    =           51
95511
 XDOT =       4593
140945                 Wp   =           58
26764
 YDOT =       6015
658640  meter/sec      RA   =           59
26703  deg
 ZDOT =      -1116
666211                 TA   =          201
01343
                                          MA   =          201
08978
                                          Ha   =            227
608  n
mi
                                          Hp   =            218
267

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9488787
39                 X    =         2953196
29
 Y    =      -10467489
53  feet           Y    =        -3157806
27  meter
 Z    =      -17258298
91                 Z    =        -5246132
71
 XDOT =      15069
360057                 XDOT =        4530
954929
 YDOT =      19736
412862  feet/sec       YDOT =        6066
674862  meter/sec
 ZDOT =      -3663
603053                 ZDOT =       -1094
504274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4814080
63                 X    =         1467331
78
 Y    =      -13366466
65  feet           Y    =        -4074099
03  meter
 Z    =      -17193501
73                 Z    =        -5240579
33
 XDOT =      20571
988847                 XDOT =        6270
342200
 YDOT =      12021
244567  feet/sec       YDOT =        3664
075344  meter/sec
 ZDOT =      -3563
739836                 ZDOT =       -1086
227902


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
37945073  
00016717  00000-0  10270-3 0  9085
2 25544  51
6414  59
9054 0007818  12
9744 347
1606 15
51160852 13416


Satellite: ISS
Catalog Number: 25544
Epoch time:      19156
37945073   =   yrday
fracday
Element set:     908
Inclination:       51
6414  deg
RA of node:        59
9054  deg
Eccentricity:     
0007818     
Arg of perigee:    12
9744  deg
Mean anomaly:     347
1606  deg
Mean motion:   15
51160852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1341
Checksum:              315


Coasting Arc #10 (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    =       -3206706
32                 A    =         6785950
92  meter
 Y    =        2695863
44  meter          E    =           
0008439
 Z    =        5334144
50                 I    =           51
93565
 XDOT =      -4650
740385                 Wp   =           32
99924
 YDOT =      -6089
696280  meter/sec      RA   =           54
32054  deg
 ZDOT =        288
529427                 TA   =           54
30064
                                          MA   =           54
22214
                                          Ha   =            227
785  n
mi
                                          Hp   =            217
985

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10520690
01                 X    =        -3262524
18
 Y    =        8844696
34  feet           Y    =         2659690
74  meter
 Z    =       17500474
09                 Z    =         5318432
46
 XDOT =     -15258
334596                 XDOT =       -4583
699525
 YDOT =     -19979
318504  feet/sec       YDOT =       -6141
329319  meter/sec
 ZDOT =        946
618855                 ZDOT =         266
099609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6182315
30                 X    =        -1884369
70
 Y    =       12377166
15  feet           Y    =         3772560
24  meter
 Z    =       17428852
54                 Z    =         5312314
26
 XDOT =     -21107
843521                 XDOT =       -6433
670705
 YDOT =     -11702
915526  feet/sec       YDOT =       -3567
048652  meter/sec
 ZDOT =        845
555828                 ZDOT =         257
725416


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
41024875  
00016717  00000-0  10270-3 0  9090
2 25544  51
6412  54
7909 0007875  16
2499 343
8903 15
51184206 13572


Satellite: ISS
Catalog Number: 25544
Epoch time:      19157
41024875   =   yrday
fracday
Element set:     909
Inclination:       51
6412  deg
RA of node:        54
7909  deg
Eccentricity:     
0007875     
Arg of perigee:    16
2499  deg
Mean anomaly:     343
8903  deg
Mean motion:   15
51184206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              326


Coasting Arc #11 (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    =        3989050
89                 A    =         6786325
75  meter
 Y    =       -1542467
33  meter          E    =           
0017409
 Z    =       -5282383
33                 I    =           51
93629
 XDOT =       3809
966541                 Wp   =           70
79116
 YDOT =       6565
288739  meter/sec      RA   =           54
14001  deg
 ZDOT =        968
228104                 TA   =          208
40928
                                          MA   =          208
50430
                                          Ha   =            227
735  n
mi
                                          Hp   =            218
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13087437
30                 X    =         4031661
58
 Y    =       -5060588
37  feet           Y    =        -1497619
76  meter
 Z    =      -17330653
98                 Z    =        -5262902
82
 XDOT =      12499
890228                 XDOT =        3731
565337
 YDOT =      21539
661216  feet/sec       YDOT =        6607
455907  meter/sec
 ZDOT =       3176
601392                 ZDOT =         986
546251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7681324
65                 X    =         2341267
75
 Y    =      -11872256
67  feet           Y    =        -3618663
83  meter
 Z    =      -17242068
03                 Z    =        -5255382
34
 XDOT =      21911
677617                 XDOT =        6678
679338
 YDOT =       9482
957082  feet/sec       YDOT =        2890
405319  meter/sec
 ZDOT =       3258
948858                 ZDOT =         993
327612


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
41024934  
00016717  00000-0  10270-3 0  9108
2 25544  51
6415  54
7907 0007878  16
6686 343
4723 15
51164212 13579


Satellite: ISS
Catalog Number: 25544
Epoch time:      19157
41024934   =   yrday
fracday
Element set:     910
Inclination:       51
6415  deg
RA of node:        54
7907  deg
Eccentricity:     
0007878     
Arg of perigee:    16
6686  deg
Mean anomaly:     343
4723  deg
Mean motion:   15
51164212  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              311


Coasting Arc #12 (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    =       -4342938
98                 A    =         6787059
94  meter
 Y    =        1083241
52  meter          E    =           
0012693
 Z    =        5098627
43                 I    =           51
91883
 XDOT =      -3724
561492                 Wp   =           33
96394
 YDOT =      -6457
759754  meter/sec      RA   =           49
19245  deg
 ZDOT =      -1788
129301                 TA   =           73
34243
                                          MA   =           73
20313
                                          Ha   =            227
882  n
mi
                                          Hp   =            217
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14248487
46                 X    =        -4379495
49
 Y    =        3553942
00  feet           Y    =         1034470
49  meter
 Z    =       16727780
29                 Z    =         5077442
56
 XDOT =     -12219
689933                 XDOT =       -3643
386469
 YDOT =     -21186
875834  feet/sec       YDOT =       -6498
956233  meter/sec
 ZDOT =      -5866
565948                 ZDOT =       -1806
025655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9307677
69                 X    =        -2836980
16
 Y    =       11499063
80  feet           Y    =         3504914
64  meter
 Z    =       16631512
26                 Z    =         5069284
94
 XDOT =     -21657
688895                 XDOT =       -6601
263575
 YDOT =      -8869
813280  feet/sec       YDOT =       -2703
519088  meter/sec
 ZDOT =      -5947
005461                 ZDOT =       -1812
647264


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
44104679  
00016717  00000-0  10270-3 0  9118
2 25544  51
6419  49
6759 0007864  19
8905 340
2551 15
51173731 13733


Satellite: ISS
Catalog Number: 25544
Epoch time:      19158
44104679   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:        49
6759  deg
Eccentricity:     
0007864     
Arg of perigee:    19
8905  deg
Mean anomaly:     340
2551  deg
Mean motion:   15
51173731  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1373
Checksum:              325


Coasting Arc #13 (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    =        4706180
07                 A    =         6788130
70  meter
 Y    =        -723416
93  meter          E    =           
0014514
 Z    =       -4848671
45                 I    =           51
90054
 XDOT =       3576
685564                 Wp   =           74
89538
 YDOT =       6270
140958  meter/sec      RA   =           44
24316  deg
 ZDOT =       2546
107808                 TA   =          220
05564
                                          MA   =          220
16276
                                          Ha   =            227
901  n
mi
                                          Hp   =            217
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15440223
33                 X    =         4737471
74
 Y    =       -2373415
11  feet           Y    =         -670613
47  meter
 Z    =      -15907714
73                 Z    =        -4825734
84
 XDOT =      11734
532690                 XDOT =        3493
937740
 YDOT =      20571
328601  feet/sec       YDOT =        6309
674924  meter/sec
 ZDOT =       8353
372074                 ZDOT =        2563
281811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10770413
07                 X    =         3282821
90
 Y    =      -11460160
38  feet           Y    =        -3493056
88  meter
 Z    =      -15803541
05                 Z    =        -4816919
31
 XDOT =      21046
837285                 XDOT =        6415
076004
 YDOT =       8200
072625  feet/sec       YDOT =        2499
382136  meter/sec
 ZDOT =       8430
549856                 ZDOT =        2569
631596


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
40741691  
00016717  00000-0  10270-3 0  9127
2 25544  51
6426  44
8793 0007925  23
6131 336
5382 15
51179707 13883


Satellite: ISS
Catalog Number: 25544
Epoch time:      19159
40741691   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:        44
8793  deg
Eccentricity:     
0007925     
Arg of perigee:    23
6131  deg
Mean anomaly:     336
5382  deg
Mean motion:   15
51179707  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1388
Checksum:              324


Coasting Arc #14 (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    =       -5092615
63                 A    =         6789622
86  meter
 Y    =         365394
74  meter          E    =           
0016082
 Z    =        4470788
22                 I    =           51
88055
 XDOT =      -3338
267668                 Wp   =           49
82315
 YDOT =      -6066
403534  meter/sec      RA   =           39
29497  deg
 ZDOT =      -3288
855773                 TA   =           73
31353
                                          MA   =           73
13706
                                          Ha   =            228
074  n
mi
                                          Hp   =            217
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16708056
53                 X    =        -5118039
56
 Y    =        1198801
63  feet           Y    =          308302
86  meter
 Z    =       14667940
35                 Z    =         4445988
64
 XDOT =     -10952
321746                 XDOT =       -3254
207967
 YDOT =     -19902
898734  feet/sec       YDOT =       -6103
263985  meter/sec
 ZDOT =     -10790
209228                 ZDOT =       -3304
868287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12289921
87                 X    =        -3745968
19
 Y    =       11525800
84  feet           Y    =         3513064
10  meter
 Z    =       14555359
42                 Z    =         4436473
55
 XDOT =     -20152
205831                 XDOT =       -6142
392337
 YDOT =      -7696
170902  feet/sec       YDOT =       -2345
792891  meter/sec
 ZDOT =     -10862
133958                 ZDOT =       -3310
778430


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
43821069  
00016717  00000-0  10270-3 0  9131
2 25544  51
6423  39
7643 0007984  27
6936 332
4639 15
51170054 14044


Satellite: ISS
Catalog Number: 25544
Epoch time:      19160
43821069   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:        39
7643  deg
Eccentricity:     
0007984     
Arg of perigee:    27
6936  deg
Mean anomaly:     332
4639  deg
Mean motion:   15
51170054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1404
Checksum:              309


Coasting Arc #15 (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    =        5455190
20                 A    =         6791094
51  meter
 Y    =        -122630
61  meter          E    =           
0011688
 Z    =       -4048508
92                 I    =           51
85985
 XDOT =       3041
748706                 Wp   =           65
82225
 YDOT =       5821
781100  meter/sec      RA   =           34
34616  deg
 ZDOT =       3935
892548                 TA   =          244
92457
                                          MA   =          245
04592
                                          Ha   =            228
058  n
mi
                                          Hp   =            217
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17897605
64                 X    =         5475821
40
 Y    =        -402331
38  feet           Y    =          -61511
08  meter
 Z    =      -13282509
59                 Z    =        -4021959
63
 XDOT =       9979
490505                 XDOT =        2957
303496
 YDOT =      19100
331694  feet/sec       YDOT =        5855
323507  meter/sec
 ZDOT =      12913
033294                 ZDOT =        3950
463667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13505804
15                 X    =         4116569
11
 Y    =      -11885519
66  feet           Y    =        -3622706
39  meter
 Z    =      -13162024
76                 Z    =        -4011785
15
 XDOT =      18998
769068                 XDOT =        5790
824812
 YDOT =       7266
344973  feet/sec       YDOT =        2214
781948  meter/sec
 ZDOT =      12978
438887                 ZDOT =        3955
828173


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
40457884  
00016717  00000-0  10270-3 0  9140
2 25544  51
6430  34
9683 0007943  30
8805 329
2812 15
51187732 14193


Satellite: ISS
Catalog Number: 25544
Epoch time:      19161
40457884   =   yrday
fracday
Element set:     914
Inclination:       51
6430  deg
RA of node:        34
9683  deg
Eccentricity:     
0007943     
Arg of perigee:    30
8805  deg
Mean anomaly:     329
2812  deg
Mean motion:   15
51187732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1419
Checksum:              317


Coasting Arc #16 (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    =        3415406
50                 A    =         6786429
58  meter
 Y    =       -2667283
34  meter          E    =           
0018385
 Z    =       -5237202
53                 I    =           51
84066
 XDOT =       5705
771111                 Wp   =           75
36311
 YDOT =       4952
748896  meter/sec      RA   =           33
74973  deg
 ZDOT =       1206
631062                 TA   =          206
16042
                                          MA   =          206
25342
                                          Ha   =            227
972  n
mi
                                          Hp   =            217
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11205401
90                 X    =         3470418
34
 Y    =       -8750929
59  feet           Y    =        -2628781
76  meter
 Z    =      -17182423
01                 Z    =        -5220478
46
 XDOT =      18719
721494                 XDOT =        5644
102866
 YDOT =      16249
176169  feet/sec       YDOT =        5016
209899  meter/sec
 ZDOT =       3958
763328                 ZDOT =        1234
198207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7666111
47                 X    =        -2336630
78
 Y    =      -12082374
47  feet           Y    =        -3682707
74  meter
 Z    =      -17106210
07                 Z    =        -5213972
83
 XDOT =      17029
665008                 XDOT =        5190
641894
 YDOT =     -16548
535921  feet/sec       YDOT =       -5043
993749  meter/sec
 ZDOT =       4083
244451                 ZDOT =        1244
572909


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
53342622  
00016717  00000-0  10270-3 0  9158
2 25544  51
6427  34
3290 0007905  30
1351 330
0253 15
51192337 14213


Satellite: ISS
Catalog Number: 25544
Epoch time:      19161
53342622   =   yrday
fracday
Element set:     915
Inclination:       51
6427  deg
RA of node:        34
3290  deg
Eccentricity:     
0007905     
Arg of perigee:    30
1351  deg
Mean anomaly:     330
0253  deg
Mean motion:   15
51192337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1421
Checksum:              265


Coasting Arc #17 (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    =       -3903691
08                 A    =         6787259
89  meter
 Y    =        2360214
61  meter          E    =           
0013610
 Z    =        5020808
56                 I    =           51
81623
 XDOT =      -5563
804616                 Wp   =           42
59490
 YDOT =      -4872
879205  meter/sec      RA   =           28
79486  deg
 ZDOT =      -2022
217592                 TA   =           67
08183
                                          MA   =           66
93824
                                          Ha   =            228
068  n
mi
                                          Hp   =            217
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12807385
45                 X    =        -3954181
89
 Y    =        7743486
27  feet           Y    =         2316278
02  meter
 Z    =       16472469
03                 Z    =         5001723
45
 XDOT =     -18253
952153                 XDOT =       -5499
078350
 YDOT =     -15987
136499  feet/sec       YDOT =       -4934
735468  meter/sec
 ZDOT =      -6634
572153                 ZDOT =       -2049
087776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6747654
96                 X    =         2056685
23
 Y    =       13465315
72  feet           Y    =         4104228
23  meter
 Z    =       16385584
00                 Z    =         4994326
00
 XDOT =     -16334
280156                 XDOT =       -4978
688591
 YDOT =      16458
484780  feet/sec       YDOT =        5016
546161  meter/sec
 ZDOT =      -6755
887520                 ZDOT =       -2059
194516


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
56421647  
00016717  00000-0  10270-3 0  9168
2 25544  51
6436  29
2134 0007861  32
6313 327
5322 15
51213355 14378


Satellite: ISS
Catalog Number: 25544
Epoch time:      19162
56421647   =   yrday
fracday
Element set:     916
Inclination:       51
6436  deg
RA of node:        29
2134  deg
Eccentricity:     
0007861     
Arg of perigee:    32
6313  deg
Mean anomaly:     327
5322  deg
Mean motion:   15
51213355  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1437
Checksum:              290


Coasting Arc #18 (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    =        4365945
16                 A    =         6788505
85  meter
 Y    =       -2152974
94  meter          E    =           
0015184
 Z    =       -4743069
00                 I    =           51
78951
 XDOT =       5333
751308                 Wp   =           78
96703
 YDOT =       4739
537316  meter/sec      RA   =           23
83835  deg
 ZDOT =       2768
643875                 TA   =          218
39080
                                          MA   =          218
49895
                                          Ha   =            228
114  n
mi
                                          Hp   =            217
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14323967
06                 X    =         4412735
18
 Y    =       -7063566
08  feet           Y    =        -2103889
77  meter
 Z    =      -15561249
99                 Z    =        -4721747
33
 XDOT =      17499
184083                 XDOT =        5266
907424
 YDOT =      15549
663111  feet/sec       YDOT =        4798
809027  meter/sec
 ZDOT =       9083
477279                 ZDOT =        2794
391527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6211388
56                 X    =        -1893231
23
 Y    =      -14815472
07  feet           Y    =        -4515755
89  meter
 Z    =      -15464247
11                 Z    =        -4713502
52
 XDOT =      15460
165324                 XDOT =        4712
258391
 YDOT =     -16048
557961  feet/sec       YDOT =       -4891
600467  meter/sec
 ZDOT =       9199
702032                 ZDOT =        2804
069179


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
53058236  
00016717  00000-0  10270-3 0  9177
2 25544  51
6426  24
4165 0007924  36
8022 323
3672 15
51194193 14528


Satellite: ISS
Catalog Number: 25544
Epoch time:      19163
53058236   =   yrday
fracday
Element set:     917
Inclination:       51
6426  deg
RA of node:        24
4165  deg
Eccentricity:     
0007924     
Arg of perigee:    36
8022  deg
Mean anomaly:     323
3672  deg
Mean motion:   15
51194193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1452
Checksum:              299
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