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

 
Date: May 31st 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16903 7526 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 8
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 1265)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4196636
32                 A    =         6786018
02  meter
 Y    =         -22481
40  meter          E    =           
0008778
 Z    =        5331724
80                 I    =           52
00405
 XDOT =       -545
565885                 Wp   =           11
75749
 YDOT =      -7632
099925  meter/sec      RA   =           83
25987  deg
 ZDOT =       -453
109550                 TA   =           82
59434
                                          MA   =           82
49460
                                          Ha   =            227
155  n
mi
                                          Hp   =            218
980

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13768491
88                 X    =        -4221971
96
 Y    =         -73757
86  feet           Y    =          -69553
33  meter
 Z    =       17492535
43                 Z    =         5311277
27
 XDOT =      -1789
914321                 XDOT =        -457
980031
 YDOT =     -25039
697917  feet/sec       YDOT =       -7637
711055  meter/sec
 ZDOT =      -1486
579888                 ZDOT =        -455
547798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5311248
60                 X    =        -1618868
57
 Y    =       12829828
32  feet           Y    =         3910531
67  meter
 Z    =       17399762
88                 Z    =         5303447
73
 XDOT =     -22922
071270                 XDOT =       -6986
647323
 YDOT =      -7421
204734  feet/sec       YDOT =       -2261
983203  meter/sec
 ZDOT =      -1496
847536                 ZDOT =        -456
239129


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
54756649  
00016717  00000-0  10270-3 0  9000
2 25544  51
6414  83
8844 0007714 354
5725   5
5342 15
51179348 12666


Satellite: ISS
Catalog Number: 25544
Epoch time:      19151
54756649   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:        83
8844  deg
Eccentricity:     
0007714     
Arg of perigee:   354
5725  deg
Mean anomaly:       5
5342  deg
Mean motion:   15
51179348  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1266
Checksum:              320


Coasting Arc #2 (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    =        4292971
67                 A    =         6786543
43  meter
 Y    =         552700
44  meter          E    =           
0014766
 Z    =       -5237872
94                 I    =           52
00127
 XDOT =        554
357405                 Wp   =           68
32621
 YDOT =       7530
094632  meter/sec      RA   =           78
31597  deg
 ZDOT =       1257
064003                 TA   =          213
65570
                                          MA   =          213
74956
                                          Ha   =            227
283  n
mi
                                          Hp   =            218
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14084552
72                 X    =         4311915
23
 Y    =        1813321
64  feet           Y    =          600814
02  meter
 Z    =      -17184622
49                 Z    =        -5216972
87
 XDOT =       1818
757890                 XDOT =         464
006322
 YDOT =      24705
034882  feet/sec       YDOT =        7535
788503  meter/sec
 ZDOT =       4124
225732                 ZDOT =        1259
538397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6825153
56                 X    =         2080306
81
 Y    =      -12582855
77  feet           Y    =        -3835254
44  meter
 Z    =      -17089851
68                 Z    =        -5208986
79
 XDOT =      22763
059507                 XDOT =        6938
180538
 YDOT =       6767
905965  feet/sec       YDOT =        2062
857738  meter/sec
 ZDOT =       4134
646099                 ZDOT =        1260
240131


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
51394715  
00016717  00000-0  10270-3 0  9011
2 25544  51
6421  79
0881 0007775 359
2821    
8317 15
51156663 12810


Satellite: ISS
Catalog Number: 25544
Epoch time:      19152
51394715   =   yrday
fracday
Element set:     901
Inclination:       51
6421  deg
RA of node:        79
0881  deg
Eccentricity:     
0007775     
Arg of perigee:   359
2821  deg
Mean anomaly:        
8317  deg
Mean motion:   15
51156663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1281
Checksum:              305


Coasting Arc #3 (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    =       -4426832
13                 A    =         6787412
00  meter
 Y    =       -1105263
84  meter          E    =           
0012401
 Z    =        5023780
58                 I    =           51
99638
 XDOT =       -516
766133                 Wp   =           26
06938
 YDOT =      -7363
460694  meter/sec      RA   =           73
37403  deg
 ZDOT =      -2062
603074                 TA   =           83
97149
                                          MA   =           83
83018
                                          Ha   =            227
435  n
mi
                                          Hp   =            218
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14523727
47                 X    =        -4438546
85
 Y    =       -3626193
71  feet           Y    =        -1154834
02  meter
 Z    =       16482219
75                 Z    =         5002247
74
 XDOT =      -1695
426947                 XDOT =        -424
368275
 YDOT =     -24158
335609  feet/sec       YDOT =       -7368
722603  meter/sec
 ZDOT =      -6767
070452                 ZDOT =       -2064
890030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8459061
38                 X    =        -2578321
91
 Y    =       12479560
62  feet           Y    =         3803770
08  meter
 Z    =       16384637
79                 Z    =         4994037
60
 XDOT =     -22330
472196                 XDOT =       -6806
327925
 YDOT =      -6183
848805  feet/sec       YDOT =       -1884
837116  meter/sec
 ZDOT =      -6776
636692                 ZDOT =       -2065
518864


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
54475221  
00016717  00000-0  10270-3 0  9028
2 25544  51
6420  73
9738 0007814   3
0344 357
0853 15
51165592 12971


Satellite: ISS
Catalog Number: 25544
Epoch time:      19153
54475221   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:        73
9738  deg
Eccentricity:     
0007814     
Arg of perigee:     3
0344  deg
Mean anomaly:     357
0853  deg
Mean motion:   15
51165592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1297
Checksum:              303


Coasting Arc #4 (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    =        4605197
11                 A    =         6788585
22  meter
 Y    =        1567012
90  meter          E    =           
0011808
 Z    =       -4742741
88                 I    =           51
99061
 XDOT =        456
073621                 Wp   =           69
13154
 YDOT =       7110
925251  meter/sec      RA   =           68
43163  deg
 ZDOT =       2802
019559                 TA   =          228
49348
                                          MA   =          228
59487
                                          Ha   =            227
485  n
mi
                                          Hp   =            218
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15108914
41                 X    =         4610369
96
 Y    =        5141118
45  feet           Y    =         1618541
15  meter
 Z    =      -15560176
78                 Z    =        -4720358
44
 XDOT =       1496
304530                 XDOT =         362
912501
 YDOT =      23329
807255  feet/sec       YDOT =        7115
504023  meter/sec
 ZDOT =       9192
977557                 ZDOT =        2804
009932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9864299
71                 X    =         3006638
55
 Y    =      -12670871
45  feet           Y    =        -3862081
62  meter
 Z    =      -15458787
24                 Z    =        -4711838
35
 XDOT =      21576
980981                 XDOT =        6576
663803
 YDOT =       5611
124345  feet/sec       YDOT =        1710
270700  meter/sec
 ZDOT =       9201
206162                 ZDOT =        2804
527638


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
51113205  
00016717  00000-0  10270-3 0  9038
2 25544  51
6429  69
1781 0007778   6
3955 353
7294 15
51166211 13127


Satellite: ISS
Catalog Number: 25544
Epoch time:      19154
51113205   =   yrday
fracday
Element set:     903
Inclination:       51
6429  deg
RA of node:        69
1781  deg
Eccentricity:     
0007778     
Arg of perigee:     6
3955  deg
Mean anomaly:     353
7294  deg
Mean motion:   15
51166211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1312
Checksum:              299


Coasting Arc #5 (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    =       -2193644
16                 A    =         6797897
83  meter
 Y    =       -6412406
31  meter          E    =           
0007925
 Z    =        -531747
58                 I    =           52
01893
 XDOT =       4622
846993                 Wp   =           93
79563
 YDOT =      -1089
814066  meter/sec      RA   =           67
60245  deg
 ZDOT =      -6006
201118                 TA   =           91
89963
                                          MA   =           91
80886
                                          Ha   =            227
391  n
mi
                                          Hp   =            218
574

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7196995
29                 X    =        -2119192
80
 Y    =      -21038078
46  feet           Y    =        -6436520
80  meter
 Z    =       -1744578
67                 Z    =         -542223
87
 XDOT =      15166
820842                 XDOT =        4663
865166
 YDOT =      -3575
505465  feet/sec       YDOT =       -1037
887791  meter/sec
 ZDOT =     -19705
384244                 ZDOT =       -5983
645338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10385826
09                 X    =        -3165599
79
 Y    =       19656209
78  feet           Y    =         5991212
74  meter
 Z    =       -1791389
02                 Z    =         -546015
37
 XDOT =     -11660
828882                 XDOT =       -3554
220643
 YDOT =      -7925
228889  feet/sec       YDOT =       -2415
609765  meter/sec
 ZDOT =     -19602
911453                 ZDOT =       -5974
967411


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
70440637  
00016717  00000-0  10270-3 0  9042
2 25544  51
6424  68
2191 0007679   5
4567 354
6667 15
51139717 13154


Satellite: ISS
Catalog Number: 25544
Epoch time:      19154
70440637   =   yrday
fracday
Element set:     904
Inclination:       51
6424  deg
RA of node:        68
2191  deg
Eccentricity:     
0007679     
Arg of perigee:     5
4567  deg
Mean anomaly:     354
6667  deg
Mean motion:   15
51139717  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1315
Checksum:              320


Coasting Arc #6 (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    =       -2630047
99                 A    =         6787088
59  meter
 Y    =        3663309
59  meter          E    =           
0007304
 Z    =        5065982
70                 I    =           51
97334
 XDOT =      -4515
229205                 Wp   =           51
95306
 YDOT =      -5893
691722  meter/sec      RA   =           64
21306  deg
 ZDOT =       1920
226948                 TA   =           19
52664
                                          MA   =           19
49868
                                          Ha   =            227
525  n
mi
                                          Hp   =            218
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8628766
37                 X    =        -2695424
65
 Y    =       12018732
24  feet           Y    =         3633532
10  meter
 Z    =       16620678
16                 Z    =         5053048
66
 XDOT =     -14813
744111                 XDOT =       -4458
316163
 YDOT =     -19336
258931  feet/sec       YDOT =       -5943
866299  meter/sec
 ZDOT =       6299
957178                 ZDOT =        1898
430625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3665878
18                 X    =        -1117359
67
 Y    =       14402373
30  feet           Y    =         4389843
38  meter
 Z    =       16561565
65                 Z    =         5047965
21
 XDOT =     -19911
152752                 XDOT =       -6068
919359
 YDOT =     -12190
049025  feet/sec       YDOT =       -3715
526943  meter/sec
 ZDOT =       6201
729809                 ZDOT =        1890
287246


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
41308353  
00016717  00000-0  10270-3 0  9050
2 25544  51
6415  64
7017 0007725   8
5277 351
6004 15
51191040 13267


Satellite: ISS
Catalog Number: 25544
Epoch time:      19155
41308353   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:        64
7017  deg
Eccentricity:     
0007725     
Arg of perigee:     8
5277  deg
Mean anomaly:     351
6004  deg
Mean motion:   15
51191040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1326
Checksum:              281


Coasting Arc #7 (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    =        2887918
63                 A    =         6786427
50  meter
 Y    =       -3196079
08  meter          E    =           
0018570
 Z    =       -5259307
13                 I    =           51
95517
 XDOT =       4596
527384                 Wp   =           58
14869
 YDOT =       6011
904818  meter/sec      RA   =           59
26701  deg
 ZDOT =      -1122
836029                 TA   =          201
07253
                                          MA   =          201
14914
                                          Ha   =            227
624  n
mi
                                          Hp   =            218
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9474798
65                 X    =         2948990
36
 Y    =      -10485823
77  feet           Y    =        -3163441
90  meter
 Z    =      -17254944
64                 Z    =        -5245130
90
 XDOT =      15080
470421                 XDOT =        4534
413062
 YDOT =      19724
097172  feet/sec       YDOT =        6062
959311  meter/sec
 ZDOT =      -3683
845240                 ZDOT =       -1100
657469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4794074
26                 X    =         1461233
84
 Y    =      -13377963
95  feet           Y    =        -4077603
41  meter
 Z    =      -17190240
16                 Z    =        -5239585
20
 XDOT =      20576
764504                 XDOT =        6271
797821
 YDOT =      12006
997887  feet/sec       YDOT =        3659
732956  meter/sec
 ZDOT =      -3583
906147                 ZDOT =       -1092
374594


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
37946145  
00016717  00000-0  10270-3 0  9064
2 25544  51
6415  59
9054 0007846  12
9212 347
2139 15
51156213 13416


Satellite: ISS
Catalog Number: 25544
Epoch time:      19156
37946145   =   yrday
fracday
Element set:     906
Inclination:       51
6415  deg
RA of node:        59
9054  deg
Eccentricity:     
0007846     
Arg of perigee:    12
9212  deg
Mean anomaly:     347
2139  deg
Mean motion:   15
51156213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1341
Checksum:              304


Coasting Arc #8 (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    =       -3201135
15                 A    =         6785967
53  meter
 Y    =        2703158
59  meter          E    =           
0008453
 Z    =        5333807
95                 I    =           51
93570
 XDOT =      -4655
641724                 Wp   =           32
97115
 YDOT =      -6085
558606  meter/sec      RA   =           54
32058  deg
 ZDOT =        296
702411                 TA   =           54
25111
                                          MA   =           54
17253
                                          Ha   =            227
802  n
mi
                                          Hp   =            217
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10502411
91                 X    =        -3257033
37
 Y    =        8868630
54  feet           Y    =         2667047
73  meter
 Z    =       17499369
93                 Z    =         5318122
78
 XDOT =     -15274
415105                 XDOT =       -4588
686469
 YDOT =     -19965
743457  feet/sec       YDOT =       -6137
246935  meter/sec
 ZDOT =        973
433106                 ZDOT =         274
248576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6155948
70                 X    =        -1876333
16
 Y    =       12391726
02  feet           Y    =         3776998
09  meter
 Z    =       17427869
44                 Z    =         5312014
61
 XDOT =     -21116
209036                 XDOT =       -6436
220514
 YDOT =     -11685
868473  feet/sec       YDOT =       -3561
852710  meter/sec
 ZDOT =        872
260602                 ZDOT =         265
865032


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
41026282  
00016717  00000-0  10270-3 0  9072
2 25544  51
6412  54
7908 0007904  16
1990 343
9412 15
51178987 13574


Satellite: ISS
Catalog Number: 25544
Epoch time:      19157
41026282   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:        54
7908  deg
Eccentricity:     
0007904     
Arg of perigee:    16
1990  deg
Mean anomaly:     343
9412  deg
Mean motion:   15
51178987  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              320


Coasting Arc #9 (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    =        3984409
15                 A    =         6786336
33  meter
 Y    =       -1550469
52  meter          E    =           
0017435
 Z    =       -5283571
40                 I    =           51
93632
 XDOT =       3816
108069                 Wp   =           70
66688
 YDOT =       6562
897067  meter/sec      RA   =           54
14005  deg
 ZDOT =        960
077278                 TA   =          208
45491
                                          MA   =          208
55021
                                          Ha   =            227
752  n
mi
                                          Hp   =            218
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13072208
48                 X    =         4027115
43
 Y    =       -5086842
25  feet           Y    =        -1505673
32  meter
 Z    =      -17334551
83                 Z    =        -5264113
21
 XDOT =      12520
039598                 XDOT =        3737
772745
 YDOT =      21531
814524  feet/sec       YDOT =        6605
133284  meter/sec
 ZDOT =       3149
859837                 ZDOT =         978
425418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7653567
77                 X    =         2332807
46
 Y    =      -11884501
95  feet           Y    =        -3622396
19  meter
 Z    =      -17246066
21                 Z    =        -5256600
98
 XDOT =      21922
578460                 XDOT =        6682
001915
 YDOT =       9466
657652  feet/sec       YDOT =        2885
437252  meter/sec
 ZDOT =       3232
343695                 ZDOT =         985
218358


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
41026342  
00016717  00000-0  10270-3 0  9080
2 25544  51
6415  54
7906 0007908  16
6199 343
5210 15
51158781 13577


Satellite: ISS
Catalog Number: 25544
Epoch time:      19157
41026342   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:        54
7906  deg
Eccentricity:     
0007908     
Arg of perigee:    16
6199  deg
Mean anomaly:     343
5210  deg
Mean motion:   15
51158781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              311


Coasting Arc #10 (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    =       -4337249
27                 A    =         6787065
43  meter
 Y    =        1093115
54  meter          E    =           
0012700
 Z    =        5101371
28                 I    =           51
91883
 XDOT =      -3733
022776                 Wp   =           33
84806
 YDOT =      -6455
621931  meter/sec      RA   =           49
19254  deg
 ZDOT =      -1778
158118                 TA   =           73
35927
                                          MA   =           73
21987
                                          Ha   =            227
901  n
mi
                                          Hp   =            217
883

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14229820
44                 X    =        -4373929
95
 Y    =        3586337
06  feet           Y    =         1044407
43  meter
 Z    =       16736782
41                 Z    =         5080213
74
 XDOT =     -12247
450052                 XDOT =       -3651
919464
 YDOT =     -21179
861977  feet/sec       YDOT =       -6496
913432  meter/sec
 ZDOT =      -5833
852093                 ZDOT =       -1796
095748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9273294
41                 X    =        -2826500
14
 Y    =       11513674
09  feet           Y    =         3509367
86  meter
 Z    =       16640637
26                 Z    =         5072066
24
 XDOT =     -21674
704007                 XDOT =       -6606
449781
 YDOT =      -8849
844997  feet/sec       YDOT =       -2697
432755  meter/sec
 ZDOT =      -5914
479172                 ZDOT =       -1802
733252


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
44106472  
00016717  00000-0  10270-3 0  9098
2 25544  51
6419  49
6758 0007894  19
8453 340
3004 15
51167772 13735


Satellite: ISS
Catalog Number: 25544
Epoch time:      19158
44106472   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:        49
6758  deg
Eccentricity:     
0007894     
Arg of perigee:    19
8453  deg
Mean anomaly:     340
3004  deg
Mean motion:   15
51167772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1373
Checksum:              327


Coasting Arc #11 (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    =        4699383
35                 A    =         6788131
01  meter
 Y    =        -735327
25  meter          E    =           
0014562
 Z    =       -4853510
78                 I    =           51
90052
 XDOT =       3587
992045                 Wp   =           74
81175
 YDOT =       6268
378718  meter/sec      RA   =           44
24330  deg
 ZDOT =       2534
412977                 TA   =          220
01657
                                          MA   =          220
12396
                                          Ha   =            227
922  n
mi
                                          Hp   =            217
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15417924
39                 X    =         4730832
22
 Y    =       -2412490
99  feet           Y    =         -682598
92  meter
 Z    =      -15923591
81                 Z    =        -4830606
81
 XDOT =      11771
627445                 XDOT =        3505
319893
 YDOT =      20565
546975  feet/sec       YDOT =        6308
039546  meter/sec
 ZDOT =       8315
003205                 ZDOT =        2551
642086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10728839
64                 X    =         3270150
32
 Y    =      -11477223
14  feet           Y    =        -3498257
61  meter
 Z    =      -15819564
80                 Z    =        -4821803
35
 XDOT =      21071
420411                 XDOT =        6422
568941
 YDOT =       8175
508212  feet/sec       YDOT =        2491
894903  meter/sec
 ZDOT =       8392
431270                 ZDOT =        2558
013051


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
40743889  
00016717  00000-0  10270-3 0  9106
2 25544  51
6426  44
8793 0007957  23
5753 336
5761 15
51172858 13888


Satellite: ISS
Catalog Number: 25544
Epoch time:      19159
40743889   =   yrday
fracday
Element set:     910
Inclination:       51
6426  deg
RA of node:        44
8793  deg
Eccentricity:     
0007957     
Arg of perigee:    23
5753  deg
Mean anomaly:     336
5761  deg
Mean motion:   15
51172858  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1388
Checksum:              348


Coasting Arc #12 (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    =       -5084982
78                 A    =         6789615
99  meter
 Y    =         379265
05  meter          E    =           
0016089
 Z    =        4478314
76                 I    =           51
88050
 XDOT =      -3353
095809                 Wp   =           49
63054
 YDOT =      -6065
301600  meter/sec      RA   =           39
29516  deg
 ZDOT =      -3275
768665                 TA   =           73
35803
                                          MA   =           73
18145
                                          Ha   =            228
097  n
mi
                                          Hp   =            217
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16683014
37                 X    =        -5110598
94
 Y    =        1244307
91  feet           Y    =          322257
45  meter
 Z    =       14692633
72                 Z    =         4453551
79
 XDOT =     -11000
970501                 XDOT =       -3269
110897
 YDOT =     -19899
283463  feet/sec       YDOT =       -6102
328289  meter/sec
 ZDOT =     -10747
272522                 ZDOT =       -3291
853390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12241923
53                 X    =        -3731338
29
 Y    =       11545446
26  feet           Y    =         3519052
02  meter
 Z    =       14580217
25                 Z    =         4444050
22
 XDOT =     -20186
480313                 XDOT =       -6152
839200
 YDOT =      -7666
013585  feet/sec       YDOT =       -2336
600941  meter/sec
 ZDOT =     -10819
525067                 ZDOT =       -3297
791240


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
43823744  
00016717  00000-0  10270-3 0  9111
2 25544  51
6424  39
7643 0008017  27
6594 332
4982 15
51162662 14040


Satellite: ISS
Catalog Number: 25544
Epoch time:      19160
43823744   =   yrday
fracday
Element set:     911
Inclination:       51
6424  deg
RA of node:        39
7643  deg
Eccentricity:     
0008017     
Arg of perigee:    27
6594  deg
Mean anomaly:     332
4982  deg
Mean motion:   15
51162662  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1404
Checksum:              305


Coasting Arc #13 (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    =        5446859
23                 A    =         6791081
84  meter
 Y    =        -138543
47  meter          E    =           
0011738
 Z    =       -4059264
98                 I    =           51
85977
 XDOT =       3060
645280                 Wp   =           65
94685
 YDOT =       5821
322936  meter/sec      RA   =           34
34637  deg
 ZDOT =       3921
794952                 TA   =          244
62329
                                          MA   =          244
74487
                                          Ha   =            228
082  n
mi
                                          Hp   =            217
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17870273
08                 X    =         5467721
24
 Y    =        -454538
96  feet           Y    =          -77515
82  meter
 Z    =      -13317798
49                 Z    =        -4032755
60
 XDOT =      10041
487138                 XDOT =        2976
272266
 YDOT =      19098
828529  feet/sec       YDOT =        5855
077062  meter/sec
 ZDOT =      12866
781340                 ZDOT =        3936
458039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13451462
84                 X    =         4100005
87
 Y    =      -11908037
34  feet           Y    =        -3629569
78  meter
 Z    =      -13197492
81                 Z    =        -4022595
81
 XDOT =      19043
841400                 XDOT =        5804
562859
 YDOT =       7229
051748  feet/sec       YDOT =        2203
414973  meter/sec
 ZDOT =      12932
604301                 ZDOT =        3941
857791


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
40461048  
00016717  00000-0  10270-3 0  9125
2 25544  51
6430  34
9683 0007977  30
8563 329
3056 15
51179568 14190


Satellite: ISS
Catalog Number: 25544
Epoch time:      19161
40461048   =   yrday
fracday
Element set:     912
Inclination:       51
6430  deg
RA of node:        34
9683  deg
Eccentricity:     
0007977     
Arg of perigee:    30
8563  deg
Mean anomaly:     329
3056  deg
Mean motion:   15
51179568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1419
Checksum:              319


Coasting Arc #14 (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    =        3399479
02                 A    =         6786438
52  meter
 Y    =       -2681099
62  meter          E    =           
0018442
 Z    =       -5240570
19                 I    =           51
84066
 XDOT =       5717
775748                 Wp   =           75
21739
 YDOT =       4943
303945  meter/sec      RA   =           33
75008  deg
 ZDOT =       1188
091167                 TA   =          206
12594
                                          MA   =          206
21912
                                          Ha   =            227
996  n
mi
                                          Hp   =            217
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11153146
40                 X    =         3454662
90
 Y    =       -8796258
59  feet           Y    =        -2642775
19  meter
 Z    =      -17193471
74                 Z    =        -5223923
07
 XDOT =      18759
106784                 XDOT =        5656
302283
 YDOT =      16218
188796  feet/sec       YDOT =        5006
900282  meter/sec
 ZDOT =       3897
936900                 ZDOT =        1215
717098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7716078
77                 X    =        -2351860
81
 Y    =      -12034616
48  feet           Y    =        -3668151
10  meter
 Z    =      -17117606
29                 Z    =        -5217446
40
 XDOT =      17005
974399                 XDOT =        5183
420997
 YDOT =     -16587
384083  feet/sec       YDOT =       -5055
834669  meter/sec
 ZDOT =       4022
685926                 ZDOT =        1226
114670


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
53345855  
00016717  00000-0  10270-3 0  9137
2 25544  51
6427  34
3290 0007939  30
1176 330
0430 15
51184136 14210


Satellite: ISS
Catalog Number: 25544
Epoch time:      19161
53345855   =   yrday
fracday
Element set:     913
Inclination:       51
6427  deg
RA of node:        34
3290  deg
Eccentricity:     
0007939     
Arg of perigee:    30
1176  deg
Mean anomaly:     330
0430  deg
Mean motion:   15
51184136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1421
Checksum:              281


Coasting Arc #15 (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    =       -3885569
22                 A    =         6787258
15  meter
 Y    =        2376057
93  meter          E    =           
0013596
 Z    =        5027375
49                 I    =           51
81618
 XDOT =      -5579
952093                 Wp   =           42
46288
 YDOT =      -4863
053297  meter/sec      RA   =           28
79527  deg
 ZDOT =      -2001
309116                 TA   =           67
00285
                                          MA   =           66
85950
                                          Ha   =            228
094  n
mi
                                          Hp   =            217
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12747930
50                 X    =        -3936270
43
 Y    =        7795465
66  feet           Y    =         2332322
81  meter
 Z    =       16494014
09                 Z    =         5008377
90
 XDOT =     -18306
929439                 XDOT =       -5515
436064
 YDOT =     -15954
899268  feet/sec       YDOT =       -4925
091309  meter/sec
 ZDOT =      -6565
974790                 ZDOT =       -2028
258248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6803963
49                 X    =         2073848
07
 Y    =       13410098
74  feet           Y    =         4087398
10  meter
 Z    =       16407524
20                 Z    =         5001013
37
 XDOT =     -16310
189421                 XDOT =       -4971
345736
 YDOT =      16510
096157  feet/sec       YDOT =        5032
277309  meter/sec
 ZDOT =      -6687
649578                 ZDOT =       -2038
395591


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
56425450  
00016717  00000-0  10270-3 0  9142
2 25544  51
6436  29
2136 0007895  32
6327 327
5310 15
51204243 14375


Satellite: ISS
Catalog Number: 25544
Epoch time:      19162
56425450   =   yrday
fracday
Element set:     914
Inclination:       51
6436  deg
RA of node:        29
2136  deg
Eccentricity:     
0007895     
Arg of perigee:    32
6327  deg
Mean anomaly:     327
5310  deg
Mean motion:   15
51204243  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1437
Checksum:              291


Coasting Arc #16 (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    =        4345805
59                 A    =         6788491
36  meter
 Y    =       -2170833
23  meter          E    =           
0015273
 Z    =       -4753495
52                 I    =           51
78942
 XDOT =       5354
533295                 Wp   =           78
93912
 YDOT =       4729
209495  meter/sec      RA   =           23
83881  deg
 ZDOT =       2745
895058                 TA   =          218
17509
                                          MA   =          218
28336
                                          Ha   =            228
140  n
mi
                                          Hp   =            217
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14257892
36                 X    =         4392847
45
 Y    =       -7122156
25  feet           Y    =        -2121971
86  meter
 Z    =      -15595457
75                 Z    =        -4732271
07
 XDOT =      17567
366452                 XDOT =        5287
913856
 YDOT =      15515
779182  feet/sec       YDOT =        4788
714861  meter/sec
 ZDOT =       9008
842054                 ZDOT =        2771
744206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6273720
35                 X    =        -1912229
96
 Y    =      -14753156
71  feet           Y    =        -4496762
16  meter
 Z    =      -15498893
73                 Z    =        -4724062
81
 XDOT =      15434
882512                 XDOT =        4704
552190
 YDOT =     -16114
553606  feet/sec       YDOT =       -4911
715939  meter/sec
 ZDOT =       9125
528573                 ZDOT =        2781
461109


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
53062605  
00016717  00000-0  10270-3 0  9150
2 25544  51
6426  24
4167 0007958  36
7949 323
3747 15
51184877 14525


Satellite: ISS
Catalog Number: 25544
Epoch time:      19163
53062605   =   yrday
fracday
Element set:     915
Inclination:       51
6426  deg
RA of node:        24
4167  deg
Eccentricity:     
0007958     
Arg of perigee:    36
7949  deg
Mean anomaly:     323
3747  deg
Mean motion:   15
51184877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1452
Checksum:              329


Coasting Arc #17 (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    =       -4820004
04                 A    =         6789955
52  meter
 Y    =        1973481
81  meter          E    =           
0017019
 Z    =        4349451
78                 I    =           51
76319
 XDOT =      -5040
803872                 Wp   =           57
18939
 YDOT =      -4616
233053  meter/sec      RA   =           18
88309  deg
 ZDOT =      -3472
744431                 TA   =           68
11861
                                          MA   =           67
93772
                                          Ha   =            228
229  n
mi
                                          Hp   =            217
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15813661
54                 X    =        -4862841
23
 Y    =        6474677
85  feet           Y    =         1919341
10  meter
 Z    =       14269854
91                 Z    =         4325934
00
 XDOT =     -16538
070447                 XDOT =       -4971
940393
 YDOT =     -15145
121565  feet/sec       YDOT =       -4672
217394  meter/sec
 ZDOT =     -11393
518475                 ZDOT =       -3497
064271

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5815935
49                 X    =         1772697
14
 Y    =       16161956
14  feet           Y    =         4926164
23  meter
 Z    =       14162915
38                 Z    =         4316856
61
 XDOT =     -14631
481145                 XDOT =       -4459
675453
 YDOT =      15400
324124  feet/sec       YDOT =        4694
018793  meter/sec
 ZDOT =     -11503
267393                 ZDOT =       -3506
195901


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
56142038  
00016717  00000-0  10270-3 0  9164
2 25544  51
6422  19
3015 0007985  39
8497 320
3239 15
51207067 14685


Satellite: ISS
Catalog Number: 25544
Epoch time:      19164
56142038   =   yrday
fracday
Element set:     916
Inclination:       51
6422  deg
RA of node:        19
3015  deg
Eccentricity:     
0007985     
Arg of perigee:    39
8497  deg
Mean anomaly:     320
3239  deg
Mean motion:   15
51207067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1468
Checksum:              313


Coasting Arc #18 (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    =        5232627
29                 A    =         6791580
79  meter
 Y    =       -1878075
38  meter          E    =           
0012248
 Z    =       -3907740
05                 I    =           51
73528
 XDOT =       4659
482320                 Wp   =           70
60488
 YDOT =       4485
532168  meter/sec      RA   =           13
92649  deg
 ZDOT =       4097
925353                 TA   =          242
30674
                                          MA   =          242
43107
                                          Ha   =            228
241  n
mi
                                          Hp   =            217
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17167412
38                 X    =         5272221
36
 Y    =       -6161664
62  feet           Y    =        -1819338
53  meter
 Z    =      -12820669
46                 Z    =        -3882225
78
 XDOT =      15287
015484                 XDOT =        4589
071897
 YDOT =      14716
312887  feet/sec       YDOT =        4537
243491  meter/sec
 ZDOT =      13444
636986                 ZDOT =        4120
389199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5747899
19                 X    =        -1751959
67
 Y    =      -17395639
22  feet           Y    =        -5302190
83  meter
 Z    =      -12704688
71                 Z    =        -3872389
12
 XDOT =      13808
168042                 XDOT =        4208
729619
 YDOT =     -14420
715780  feet/sec       YDOT =       -4395
434170  meter/sec
 ZDOT =      13545
970904                 ZDOT =        4128
811931


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
52779187  
00016717  00000-0  10270-3 0  9173
2 25544  51
6410  14
5054 0007847  44
2677 315
9100 15
51180368 14837


Satellite: ISS
Catalog Number: 25544
Epoch time:      19165
52779187   =   yrday
fracday
Element set:     917
Inclination:       51
6410  deg
RA of node:        14
5054  deg
Eccentricity:     
0007847     
Arg of perigee:    44
2677  deg
Mean anomaly:     315
9100  deg
Mean motion:   15
51180368  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1483
Checksum:              314
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