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

 
Date: August 17th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15269 8125 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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


234/03:38:33 000 0 0 0 0 0 0
N/A 0 0 0 0 226 8
000/00:00:00 000 0 0 0 0 222 2

235/16:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 9
000/00:00:00 000 0 0 0 0 222 1

236/05:30:59 000 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 221 8

239/14:44:31 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 221 3

240/02:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 7
000/00:00:00 000 0 0 0 0 221 0

Coasting Arc #1 (Orbit 2460)
---------------------------------------

Vector Time (GMT): 2019/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4888376
46                 A    =         6794719
59  meter
 Y    =       -3017904
56  meter          E    =           
0005930
 Z    =        3627353
22                 I    =           51
98264
 XDOT =        543
526542                 Wp   =           54
17519
 YDOT =      -6221
374722  meter/sec      RA   =           61
26809  deg
 ZDOT =      -4435
165703                 TA   =           83
16279
                                          MA   =           83
09532
                                          Ha   =            225
685  n
mi
                                          Hp   =            223
436

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16037980
52                 X    =        -4871885
35
 Y    =       -9901261
68  feet           Y    =        -3072477
60  meter
 Z    =       11900765
15                 Z    =         3603647
91
 XDOT =       1783
223563                 XDOT =         634
598447
 YDOT =     -20411
334391  feet/sec       YDOT =       -6214
787438  meter/sec
 ZDOT =     -14551
068578                 ZDOT =       -4432
304284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7129489
04                 X    =         2173068
26
 Y    =       17520639
12  feet           Y    =         5340290
80  meter
 Z    =       11793116
79                 Z    =         3594542
00
 XDOT =     -12321
930878                 XDOT =       -3755
724532
 YDOT =      14817
993658  feet/sec       YDOT =        4516
524467  meter/sec
 ZDOT =     -14537
449491                 ZDOT =       -4431
014605


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   19228
53983921  
00016717  00000-0  10270-3 0  9009
2 25544  51
6410  61
8441 0007683 291
4190  68
6140 15
50406753 24617


Satellite: ISS
Catalog Number: 25544
Epoch time:      19228
53983921   =   yrday
fracday
Element set:     900
Inclination:       51
6410  deg
RA of node:        61
8441  deg
Eccentricity:     
0007683     
Arg of perigee:   291
4190  deg
Mean anomaly:      68
6140  deg
Mean motion:   15
50406753  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2461
Checksum:              300


Coasting Arc #2 (Orbit 2475)
---------------------------------------

Vector Time (GMT): 2019/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5109647
87                 A    =         6795814
01  meter
 Y    =        3053687
55  meter          E    =           
0004359
 Z    =       -3272560
96                 I    =           51
96758
 XDOT =       -510
635713                 Wp   =          329
60551
 YDOT =       5970
425171  meter/sec      RA   =           56
33323  deg
 ZDOT =       4774
710404                 TA   =          352
68650
                                          MA   =          352
69286
                                          Ha   =            225
982  n
mi
                                          Hp   =            223
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16763936
57                 X    =         5091016
87
 Y    =       10018659
93  feet           Y    =         3110722
98  meter
 Z    =      -10736748
57                 Z    =        -3247786
01
 XDOT =      -1675
314019                 XDOT =        -600
553218
 YDOT =      19588
009091  feet/sec       YDOT =        5964
212225  meter/sec
 ZDOT =      15665
060382                 ZDOT =        4772
011459

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7947899
49                 X    =        -2422519
77
 Y    =      -17906347
50  feet           Y    =        -5457854
72  meter
 Z    =      -10624241
10                 Z    =        -3238268
69
 XDOT =      11470
170537                 XDOT =        3496
107980
 YDOT =     -14376
210831  feet/sec       YDOT =       -4381
869061  meter/sec
 ZDOT =      15652
198916                 ZDOT =        4770
790230


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   19229
50670526  
00016717  00000-0  10270-3 0  9012
2 25544  51
6395  57
0502 0007405 294
6717  65
3662 15
50381757 24761


Satellite: ISS
Catalog Number: 25544
Epoch time:      19229
50670526   =   yrday
fracday
Element set:     901
Inclination:       51
6395  deg
RA of node:        57
0502  deg
Eccentricity:     
0007405     
Arg of perigee:   294
6717  deg
Mean anomaly:      65
3662  deg
Mean motion:   15
50381757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2476
Checksum:              317


Coasting Arc #3 (Orbit 2491)
---------------------------------------

Vector Time (GMT): 2019/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5334924
28                 A    =         6796753
78  meter
 Y    =       -3066697
18  meter          E    =           
0006606
 Z    =        2882551
60                 I    =           51
95149
 XDOT =        530
429582                 Wp   =           77
20675
 YDOT =      -5708
263007  meter/sec      RA   =           51
39926  deg
 ZDOT =      -5080
001503                 TA   =           70
19963
                                          MA   =           70
12842
                                          Ha   =            226
034  n
mi
                                          Hp   =            223
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17503032
43                 X    =        -5314236
71
 Y    =      -10061342
46  feet           Y    =        -3126240
29  meter
 Z    =        9457190
28                 Z    =         2856687
29
 XDOT =       1740
254535                 XDOT =         618
897038
 YDOT =     -18727
897004  feet/sec       YDOT =       -5701
836883  meter/sec
 ZDOT =     -16666
671598                 ZDOT =       -5077
209862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8833872
17                 X    =         2692564
24
 Y    =       18214205
22  feet           Y    =         5551689
75  meter
 Z    =        9339734
19                 Z    =         2846750
98
 XDOT =     -10762
793108                 XDOT =       -3280
499339
 YDOT =      13778
460397  feet/sec       YDOT =        4199
674729  meter/sec
 ZDOT =     -16653
407330                 ZDOT =       -5075
958554


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   19230
53802581  
00016717  00000-0  10270-3 0  9026
2 25544  51
6395  51
9380 0007612 298
5027  61
5357 15
50405907 24926


Satellite: ISS
Catalog Number: 25544
Epoch time:      19230
53802581   =   yrday
fracday
Element set:     902
Inclination:       51
6395  deg
RA of node:        51
9380  deg
Eccentricity:     
0007612     
Arg of perigee:   298
5027  deg
Mean anomaly:      61
5357  deg
Mean motion:   15
50405907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2492
Checksum:              306


Coasting Arc #4 (Orbit 2506)
---------------------------------------

Vector Time (GMT): 2019/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5553418
25                 A    =         6797725
26  meter
 Y    =        3023371
02  meter          E    =           
0007802
 Z    =       -2481347
10                 I    =           51
93247
 XDOT =       -585
980913                 Wp   =          343
33757
 YDOT =       5460
434382  meter/sec      RA   =           46
46380  deg
 ZDOT =       5344
860368                 TA   =          349
01643
                                          MA   =          349
03345
                                          Ha   =            226
280  n
mi
                                          Hp   =            222
896

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18219876
16                 X    =         5531250
17
 Y    =        9919196
25  feet           Y    =         3085349
21  meter
 Z    =       -8140902
56                 Z    =        -2454424
95
 XDOT =      -1922
509557                 XDOT =        -672
959570
 YDOT =      17914
810963  feet/sec       YDOT =        5453
395406  meter/sec
 ZDOT =      17535
631130                 ZDOT =        5341
802466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9815402
26                 X    =        -2991734
61
 Y    =      -18329974
38  feet           Y    =        -5586976
19  meter
 Z    =       -8018637
92                 Z    =        -2444080
84
 XDOT =      10214
771389                 XDOT =        3113
462319
 YDOT =     -13130
122290  feet/sec       YDOT =       -4002
061274  meter/sec
 ZDOT =      17521
172672                 ZDOT =        5340
453430


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   19231
50489143  
00016717  00000-0  10270-3 0  9030
2 25544  51
6392  47
1447 0007317 301
5013  58
5422 15
50379548 25073


Satellite: ISS
Catalog Number: 25544
Epoch time:      19231
50489143   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:        47
1447  deg
Eccentricity:     
0007317     
Arg of perigee:   301
5013  deg
Mean anomaly:      58
5422  deg
Mean motion:   15
50379548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2507
Checksum:              297


Coasting Arc #5 (Orbit 2522)
---------------------------------------

Vector Time (GMT): 2019/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5764312
39                 A    =         6798450
93  meter
 Y    =       -2961411
69  meter          E    =           
0006842
 Z    =        2047401
68                 I    =           51
91215
 XDOT =        695
322700                 Wp   =           95
60217
 YDOT =      -5213
601220  meter/sec      RA   =           41
52815  deg
 ZDOT =      -5568
109097                 TA   =           61
89332
                                          MA   =           61
82418
                                          Ha   =            226
359  n
mi
                                          Hp   =            222
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18911786
06                 X    =        -5740713
68
 Y    =       -9715917
62  feet           Y    =        -3025740
27  meter
 Z    =        6717197
11                 Z    =         2019458
46
 XDOT =       2281
242455                 XDOT =         780
617582
 YDOT =     -17104
990880  feet/sec       YDOT =       -5205
348922  meter/sec
 ZDOT =     -18268
074465                 ZDOT =       -5564
524153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10814369
50                 X    =         3296219
82
 Y    =       18351918
74  feet           Y    =         5593664
83  meter
 Z    =        6590290
97                 Z    =         2008720
69
 XDOT =      -9847
141632                 XDOT =       -3001
408769
 YDOT =      12375
252723  feet/sec       YDOT =        3771
977030  meter/sec
 ZDOT =     -18251
234860                 ZDOT =       -5562
976385


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   19232
53620979  
00016717  00000-0  10270-3 0  9049
2 25544  51
6399  42
0323 0007548 305
9095  54
1355 15
50412154 25237


Satellite: ISS
Catalog Number: 25544
Epoch time:      19232
53620979   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:        42
0323  deg
Eccentricity:     
0007548     
Arg of perigee:   305
9095  deg
Mean anomaly:      54
1355  deg
Mean motion:   15
50412154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2523
Checksum:              300


Coasting Arc #6 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2019/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5952874
14                 A    =         6799184
97  meter
 Y    =        2845929
14  meter          E    =           
0010979
 Z    =       -1610742
10                 I    =           51
88925
 XDOT =       -835
635693                 Wp   =          356
55655
 YDOT =       4997
904689  meter/sec      RA   =           36
59099  deg
 ZDOT =       5750
862356                 TA   =          345
90117
                                          MA   =          345
93179
                                          Ha   =            226
583  n
mi
                                          Hp   =            222
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19530426
96                 X    =         5928431
76
 Y    =        9337037
86  feet           Y    =         2912361
66  meter
 Z    =       -5284586
95                 Z    =        -1581884
85
 XDOT =      -2741
586920                 XDOT =        -919
395962
 YDOT =      16397
325095  feet/sec       YDOT =        4988
091848  meter/sec
 ZDOT =      18867
658649                 ZDOT =        5746
599595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11845592
13                 X    =        -3610536
48
 Y    =      -18156758
29  feet           Y    =        -5534179
93  meter
 Z    =       -5153521
91                 Z    =        -1570793
48
 XDOT =       9661
428549                 XDOT =        2944
803422
 YDOT =     -11644
585756  feet/sec       YDOT =       -3549
269739  meter/sec
 ZDOT =      18847
749057                 ZDOT =        5744
793912


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   19233
50307224  
00016717  00000-0  10270-3 0  9053
2 25544  51
6405  37
2393 0007183 309
7788  50
2729 15
50387018 25382


Satellite: ISS
Catalog Number: 25544
Epoch time:      19233
50307224   =   yrday
fracday
Element set:     905
Inclination:       51
6405  deg
RA of node:        37
2393  deg
Eccentricity:     
0007183     
Arg of perigee:   309
7788  deg
Mean anomaly:      50
2729  deg
Mean motion:   15
50387018  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2538
Checksum:              309


Coasting Arc #7 (Orbit 2548)
---------------------------------------

Vector Time (GMT): 2019/234/03:38:33
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4341039
45                 A    =         6798406
20  meter
 Y    =        4798344
78  meter          E    =           
0012708
 Z    =        2058050
66                 I    =           51
87061
 XDOT =      -4872
523498                 Wp   =           36
45323
 YDOT =       2018
292435  meter/sec      RA   =           33
40737  deg
 ZDOT =       5564
297154                 TA   =          346
21035
                                          MA   =          346
24503
                                          Ha   =            226
765  n
mi
                                          Hp   =            222
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14242255
41                 X    =         4277063
51
 Y    =       15742600
97  feet           Y    =         4846531
66  meter
 Z    =        6752134
72                 Z    =         2078982
26
 XDOT =     -15985
969482                 XDOT =       -4921
758667
 YDOT =       6621
694342  feet/sec       YDOT =        1963
529261  meter/sec
 ZDOT =      18255
568090                 ZDOT =        5540
508720

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19359003
84                 X    =         5900624
37
 Y    =        8637785
87  feet           Y    =         2632797
13  meter
 Z    =        6846917
07                 Z    =         2086940
32
 XDOT =     -11411
800946                 XDOT =       -3478
316928
 YDOT =      11171
843943  feet/sec       YDOT =        3405
178034  meter/sec
 ZDOT =      18147
085482                 ZDOT =        5531
231655


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   19234
21210372  
00016717  00000-0  10270-3 0  9060
2 25544  51
6420  33
7292 0007551 314
7548  45
2988 15
50381808 25491


Satellite: ISS
Catalog Number: 25544
Epoch time:      19234
21210372   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:        33
7292  deg
Eccentricity:     
0007551     
Arg of perigee:   314
7548  deg
Mean anomaly:      45
2988  deg
Mean motion:   15
50381808  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2549
Checksum:              305


Coasting Arc #8 (Orbit 2563)
---------------------------------------

Vector Time (GMT): 2019/235/03:38:33
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4357062
85                 A    =         6797532
14  meter
 Y    =       -4587146
56  meter          E    =           
0002479
 Z    =       -2488791
84                 I    =           51
84038
 XDOT =       5130
236979                 Wp   =          334
01725
 YDOT =      -1980
220371  meter/sec      RA   =           28
46767  deg
 ZDOT =      -5327
403110                 TA   =          233
73018
                                          MA   =          233
75309
                                          Ha   =            226
929  n
mi
                                          Hp   =            222
019

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14294825
63                 X    =        -4293355
09
 Y    =      -15049693
43  feet           Y    =        -4635514
09  meter
 Z    =       -8165327
55                 Z    =        -2509802
02
 XDOT =      16831
486150                 XDOT =        5177
876586
 YDOT =      -6496
785994  feet/sec       YDOT =       -1922
584091  meter/sec
 ZDOT =     -17478
356661                 ZDOT =       -5302
366693

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19252104
61                 X    =        -5868041
49
 Y    =       -7656949
66  feet           Y    =        -2333838
26  meter
 Z    =       -8260476
73                 Z    =        -2517793
31
 XDOT =      12079
873109                 XDOT =        3681
945324
 YDOT =     -11625
305826  feet/sec       YDOT =       -3543
393216  meter/sec
 ZDOT =     -17364
201729                 ZDOT =       -5292
608687


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   19235
17896357  
00016717  00000-0  10270-3 0  9070
2 25544  51
6430  28
9372 0007609 317
9985  42
0582 15
50393707 25644


Satellite: ISS
Catalog Number: 25544
Epoch time:      19235
17896357   =   yrday
fracday
Element set:     907
Inclination:       51
6430  deg
RA of node:        28
9372  deg
Eccentricity:     
0007609     
Arg of perigee:   317
9985  deg
Mean anomaly:      42
0582  deg
Mean motion:   15
50393707  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2564
Checksum:              338


Coasting Arc #9 (Orbit 2571)
---------------------------------------

Vector Time (GMT): 2019/235/16:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937174
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4366236
38                 A    =         6790625
09  meter
 Y    =       -2064786
22  meter          E    =           
0005720
 Z    =       -4777274
99                 I    =           51
80204
 XDOT =       5248
089663                 Wp   =           71
26210
 YDOT =       4886
570675  meter/sec      RA   =           25
79586  deg
 ZDOT =       2688
942840                 TA   =          225
25142
                                          MA   =          225
29799
                                          Ha   =            226
877  n
mi
                                          Hp   =            222
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14324922
50                 X    =         4412206
19
 Y    =       -6774233
02  feet           Y    =        -2015702
83  meter
 Z    =      -15673474
39                 Z    =        -4755953
88
 XDOT =      17218
141938                 XDOT =        5179
995219
 YDOT =      16032
056021  feet/sec       YDOT =        4944
877748  meter/sec
 ZDOT =       8821
990945                 ZDOT =        2714
270669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7500306
09                 X    =        -2286093
30
 Y    =       14066917
17  feet           Y    =         4287596
35  meter
 Z    =      -15576221
84                 Z    =        -4747632
42
 XDOT =     -22316
603000                 XDOT =       -6802
100594
 YDOT =      -2019
496083  feet/sec       YDOT =        -615
542406  meter/sec
 ZDOT =       8936
753359                 ZDOT =        2723
922424


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   19235
69462009  
00016717  00000-0  10270-3 0  9081
2 25544  51
6435  26
3791 0007322 317
1331  42
9247 15
50418530 25723


Satellite: ISS
Catalog Number: 25544
Epoch time:      19235
69462009   =   yrday
fracday
Element set:     908
Inclination:       51
6435  deg
RA of node:        26
3791  deg
Eccentricity:     
0007322     
Arg of perigee:   317
1331  deg
Mean anomaly:      42
9247  deg
Mean motion:   15
50418530  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2572
Checksum:              298


Coasting Arc #10 (Orbit 2580)
---------------------------------------

Vector Time (GMT): 2019/236/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3592755
33                 A    =         6789438
38  meter
 Y    =        2786377
73  meter          E    =           
0009322
 Z    =        5045121
88                 I    =           51
78289
 XDOT =      -6059
812228                 Wp   =          359
53716
 YDOT =      -4258
020488  meter/sec      RA   =           23
10047  deg
 ZDOT =      -1954
607393                 TA   =          109
46598
                                          MA   =          109
36524
                                          Ha   =            227
102  n
mi
                                          Hp   =            221
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11787255
00                 X    =        -3648152
70
 Y    =        9141659
23  feet           Y    =         2745891
19  meter
 Z    =       16552237
13                 Z    =         5027535
18
 XDOT =     -19881
273713                 XDOT =       -6002
253076
 YDOT =     -13969
883492  feet/sec       YDOT =       -4325
463708  meter/sec
 ZDOT =      -6412
753913                 ZDOT =       -1983
903853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         420554
62                 X    =          128185
05
 Y    =       14999510
74  feet           Y    =         4571850
87  meter
 Z    =       16471905
76                 Z    =         5020636
88
 XDOT =     -21859
420174                 XDOT =       -6662
751269
 YDOT =       7833
889714  feet/sec       YDOT =        2387
769585  meter/sec
 ZDOT =      -6545
637715                 ZDOT =       -1995
110375


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   19236
27473397  
00016717  00000-0  10270-3 0  9099
2 25544  51
6446  23
5064 0007802 321
1152  38
9437 15
50439476 25814


Satellite: ISS
Catalog Number: 25544
Epoch time:      19236
27473397   =   yrday
fracday
Element set:     909
Inclination:       51
6446  deg
RA of node:        23
5064  deg
Eccentricity:     
0007802     
Arg of perigee:   321
1152  deg
Mean anomaly:      38
9437  deg
Mean motion:   15
50439476  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2581
Checksum:              317


Coasting Arc #11 (Orbit 2595)
---------------------------------------

Vector Time (GMT): 2019/237/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3816881
33                 A    =         6790238
35  meter
 Y    =       -2793754
14  meter          E    =           
0007268
 Z    =       -4876360
16                 I    =           51
75360
 XDOT =       6049
376672                 Wp   =           66
36070
 YDOT =       4009
888861  meter/sec      RA   =           18
14970  deg
 ZDOT =       2443
428480                 TA   =          227
57955
                                          MA   =          227
64106
                                          Ha   =            227
320  n
mi
                                          Hp   =            221
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12522576
55                 X    =         3871524
72
 Y    =       -9165860
03  feet           Y    =        -2750765
42  meter
 Z    =      -15998556
95                 Z    =        -4857686
65
 XDOT =      19847
036327                 XDOT =        5992
218594
 YDOT =      13155
803351  feet/sec       YDOT =        4077
217588  meter/sec
 ZDOT =       8016
497637                 ZDOT =        2472
675192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -279252
12                 X    =          -85116
05
 Y    =      -15603566
43  feet           Y    =        -4755967
05  meter
 Z    =      -15913279
70                 Z    =        -4850367
65
 XDOT =      20983
687801                 XDOT =        6395
828042
 YDOT =      -8667
196409  feet/sec       YDOT =       -2641
761465  meter/sec
 ZDOT =       8149
171783                 ZDOT =        2483
867559


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   19237
24159132  
00016717  00000-0  10270-3 0  9107
2 25544  51
6441  18
7136 0007784 325
4345  34
6299 15
50408930 25961


Satellite: ISS
Catalog Number: 25544
Epoch time:      19237
24159132   =   yrday
fracday
Element set:     910
Inclination:       51
6441  deg
RA of node:        18
7136  deg
Eccentricity:     
0007784     
Arg of perigee:   325
4345  deg
Mean anomaly:      34
6299  deg
Mean motion:   15
50408930  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2596
Checksum:              312


Coasting Arc #12 (Orbit 2611)
---------------------------------------

Vector Time (GMT): 2019/238/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4067326
04                 A    =         6791037
24  meter
 Y    =        2817685
16  meter          E    =           
0010837
 Z    =        4653404
42                 I    =           51
72393
 XDOT =      -5983
931774                 Wp   =           18
51582
 YDOT =      -3778
390850  meter/sec      RA   =           13
19769  deg
 ZDOT =      -2930
515168                 TA   =          100
71175
                                          MA   =          100
58971
                                          Ha   =            227
427  n
mi
                                          Hp   =            221
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13344245
54                 X    =        -4121135
35
 Y    =        9244373
89  feet           Y    =         2771900
44  meter
 Z    =       15267074
86                 Z    =         4633516
47
 XDOT =     -19632
322092                 XDOT =       -5927
001309
 YDOT =     -12396
295440  feet/sec       YDOT =       -3844
988971  meter/sec
 ZDOT =      -9614
551075                 ZDOT =       -2959
444428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         156444
90                 X    =           47684
41
 Y    =       16317697
75  feet           Y    =         4973634
27  meter
 Z    =       15176270
21                 Z    =         4625727
16
 XDOT =     -20023
077355                 XDOT =       -6103
033978
 YDOT =       9292
600598  feet/sec       YDOT =        2832
384662  meter/sec
 ZDOT =      -9745
798664                 ZDOT =       -2970
519433


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   19238
27290300  
00016717  00000-0  10270-3 0  9115
2 25544  51
6435  13
6016 0007896 329
0442  31
0242 15
50443200 26124


Satellite: ISS
Catalog Number: 25544
Epoch time:      19238
27290300   =   yrday
fracday
Element set:     911
Inclination:       51
6435  deg
RA of node:        13
6016  deg
Eccentricity:     
0007896     
Arg of perigee:   329
0442  deg
Mean anomaly:      31
0242  deg
Mean motion:   15
50443200  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2612
Checksum:              263


Coasting Arc #13 (Orbit 2626)
---------------------------------------

Vector Time (GMT): 2019/239/05:30:59
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4273966
75                 A    =         6792055
83  meter
 Y    =       -2901758
68  meter          E    =           
0006009
 Z    =       -4411333
52                 I    =           51
69416
 XDOT =       5888
030894                 Wp   =           49
70573
 YDOT =       3548
643572  meter/sec      RA   =            8
24367  deg
 ZDOT =       3377
225764                 TA   =          254
44764
                                          MA   =          254
51399
                                          Ha   =            227
608  n
mi
                                          Hp   =            221
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14022200
63                 X    =         4327524
90
 Y    =       -9520205
64  feet           Y    =        -2853664
59  meter
 Z    =      -14472878
99                 Z    =        -4390442
48
 XDOT =      19317
686661                 XDOT =        5831
506880
 YDOT =      11642
531405  feet/sec       YDOT =        3614
171542  meter/sec
 ZDOT =      11080
137020                 ZDOT =        3405
690010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -302379
37                 X    =          -92165
23
 Y    =      -17026937
24  feet           Y    =        -5189810
47  meter
 Z    =      -14377504
21                 Z    =        -4382263
28
 XDOT =      18999
297186                 XDOT =        5790
985782
 YDOT =      -9783
456260  feet/sec       YDOT =       -2981
997468  meter/sec
 ZDOT =      11209
288853                 ZDOT =        3416
591242


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   19239
23975904  
00016717  00000-0  10270-3 0  9123
2 25544  51
6434   8
8086 0007860 332
1558  27
9171 15
50409274 26274


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
23975904   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:         8
8086  deg
Eccentricity:     
0007860     
Arg of perigee:   332
1558  deg
Mean anomaly:      27
9171  deg
Mean motion:   15
50409274  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2627
Checksum:              321


Coasting Arc #14 (Orbit 2632)
---------------------------------------

Vector Time (GMT): 2019/239/14:44:31
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2861867
68                 A    =         6789770
78  meter
 Y    =       -3637779
16  meter          E    =           
0009003
 Z    =       -4973808
79                 I    =           51
67426
 XDOT =       6910
748019                 Wp   =           68
90146
 YDOT =       2488
376225  meter/sec      RA   =            6
34342  deg
 ZDOT =       2162
717620                 TA   =          222
16683
                                          MA   =          222
23611
                                          Ha   =            227
450  n
mi
                                          Hp   =            221
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9389329
66                 X    =         2926493
29
 Y    =      -11934971
01  feet           Y    =        -3605414
30  meter
 Z    =      -16318270
31                 Z    =        -4959750
25
 XDOT =      22673
057806                 XDOT =        6871
903549
 YDOT =       8163
963992  feet/sec       YDOT =        2565
439834  meter/sec
 ZDOT =       7095
530250                 ZDOT =        2196
192613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5893486
61                 X    =        -1796334
72
 Y    =       14070045
81  feet           Y    =         4288549
96  meter
 Z    =      -16253910
82                 Z    =        -4954192
02
 XDOT =     -22966
547522                 XDOT =       -7000
203685
 YDOT =      -1271
489738  feet/sec       YDOT =        -387
550072  meter/sec
 ZDOT =       7247
594915                 ZDOT =        2209
066930


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   19239
62650051  
00016717  00000-0  10270-3 0  9130
2 25544  51
6437   6
8888 0007422 332
6898  27
3862 15
50423253 26332


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
62650051   =   yrday
fracday
Element set:     913
Inclination:       51
6437  deg
RA of node:         6
8888  deg
Eccentricity:     
0007422     
Arg of perigee:   332
6898  deg
Mean anomaly:      27
3862  deg
Mean motion:   15
50423253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2633
Checksum:              316


Coasting Arc #15 (Orbit 2640)
---------------------------------------

Vector Time (GMT): 2019/240/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -669566
16                 A    =         6788164
91  meter
 Y    =        4169082
01  meter          E    =           
0007959
 Z    =        5316110
76                 I    =           51
65292
 XDOT =      -7613
760044                 Wp   =          354
19841
 YDOT =       -791
805843  meter/sec      RA   =            3
98106  deg
 ZDOT =       -330
301412                 TA   =           98
99764
                                          MA   =           98
90756
                                          Ha   =            227
656  n
mi
                                          Hp   =            221
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2196739
37                 X    =         -741958
52
 Y    =       13678090
59  feet           Y    =         4161189
62  meter
 Z    =       17441308
28                 Z    =         5312682
54
 XDOT =     -24979
527703                 XDOT =       -7602
735584
 YDOT =      -2597
788200  feet/sec       YDOT =        -876
886622  meter/sec
 ZDOT =      -1083
666051                 ZDOT =        -367
258774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -114125
26                 X    =          -34785
38
 Y    =       13873070
26  feet           Y    =         4228511
81  meter
 Z    =       17425267
79                 Z    =         5311221
62
 XDOT =     -24055
847918                 XDOT =       -7332
222445
 YDOT =       1406
101762  feet/sec       YDOT =         428
579817  meter/sec
 ZDOT =      -1251
754225                 ZDOT =        -381
534688


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   19240
14215544  
00016717  00000-0  10270-3 0  9144
2 25544  51
6434   4
3351 0007859 335
7787  24
2994 15
50437833 26412


Satellite: ISS
Catalog Number: 25544
Epoch time:      19240
14215544   =   yrday
fracday
Element set:     914
Inclination:       51
6434  deg
RA of node:         4
3351  deg
Eccentricity:     
0007859     
Arg of perigee:   335
7787  deg
Mean anomaly:      24
2994  deg
Mean motion:   15
50437833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2641
Checksum:              310


Coasting Arc #16 (Orbit 2655)
---------------------------------------

Vector Time (GMT): 2019/241/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         893269
44                 A    =         6788456
99  meter
 Y    =       -4192337
32  meter          E    =           
0013018
 Z    =       -5273372
33                 I    =           51
62113
 XDOT =       7586
660424                 Wp   =           63
70054
 YDOT =        548
580025  meter/sec      RA   =          359
02073  deg
 ZDOT =        856
275308                 TA   =          214
46130
                                          MA   =          214
54578
                                          Ha   =            227
831  n
mi
                                          Hp   =            220
853

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2930674
01                 X    =          965697
56
 Y    =      -13754387
55  feet           Y    =        -4181943
26  meter
 Z    =      -17301090
32                 Z    =        -5268857
28
 XDOT =      24890
618190                 XDOT =        7575
802968
 YDOT =       1799
803233  feet/sec       YDOT =         633
358709  meter/sec
 ZDOT =       2809
302193                 ZDOT =         893
101327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         583657
41                 X    =          177898
78
 Y    =      -14076824
18  feet           Y    =        -4290616
01  meter
 Z    =      -17280107
58                 Z    =        -5266976
79
 XDOT =      23774
120770                 XDOT =        7246
352011
 YDOT =      -2639
143864  feet/sec       YDOT =        -804
411050  meter/sec
 ZDOT =       2976
810196                 ZDOT =         907
331748


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   19241
10900801  
00016717  00000-0  10270-3 0  9159
2 25544  51
6442 359
5425 0007860 340
7568  19
3285 15
50415084 26561


Satellite: ISS
Catalog Number: 25544
Epoch time:      19241
10900801   =   yrday
fracday
Element set:     915
Inclination:       51
6442  deg
RA of node:       359
5425  deg
Eccentricity:     
0007860     
Arg of perigee:   340
7568  deg
Mean anomaly:      19
3285  deg
Mean motion:   15
50415084  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2656
Checksum:              304


Coasting Arc #17 (Orbit 2671)
---------------------------------------

Vector Time (GMT): 2019/242/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1152975
82                 A    =         6788794
10  meter
 Y    =        4243741
43  meter          E    =           
0010333
 Z    =        5172856
65                 I    =           51
58877
 XDOT =      -7526
192283                 Wp   =            7
77759
 YDOT =       -330
009278  meter/sec      RA   =          354
05888  deg
 ZDOT =      -1396
434480                 TA   =           95
73164
                                          MA   =           95
61381
                                          Ha   =            227
942  n
mi
                                          Hp   =            220
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3782729
06                 X    =        -1225471
23
 Y    =       13923036
17  feet           Y    =         4230442
92  meter
 Z    =       16971314
46                 Z    =         5167079
77
 XDOT =     -24692
231901                 XDOT =       -7515
159700
 YDOT =      -1082
707605  feet/sec       YDOT =        -414
110837  meter/sec
 ZDOT =      -4581
477952                 ZDOT =       -1432
966352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1142875
70                 X    =         -348348
51
 Y    =       14413885
83  feet           Y    =         4393352
40  meter
 Z    =       16944592
65                 Z    =         5164711
84
 XDOT =     -23356
761325                 XDOT =       -7119
140852
 YDOT =       3769
213754  feet/sec       YDOT =        1148
856352  meter/sec
 ZDOT =      -4747
659046                 ZDOT =       -1447
086477


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   19242
14031446  
00016717  00000-0  10270-3 0  9165
2 25544  51
6438 354
4310 0007931 343
4956  16
5935 15
50445249 26728


Satellite: ISS
Catalog Number: 25544
Epoch time:      19242
14031446   =   yrday
fracday
Element set:     916
Inclination:       51
6438  deg
RA of node:       354
4310  deg
Eccentricity:     
0007931     
Arg of perigee:   343
4956  deg
Mean anomaly:      16
5935  deg
Mean motion:   15
50445249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2672
Checksum:              307


Coasting Arc #18 (Orbit 2686)
---------------------------------------

Vector Time (GMT): 2019/243/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1354983
62                 A    =         6789431
14  meter
 Y    =       -4342045
53  meter          E    =           
0011554
 Z    =       -5048397
98                 I    =           51
55826
 XDOT =       7414
415622                 Wp   =           66
58282
 YDOT =        110
104786  meter/sec      RA   =          349
09506  deg
 ZDOT =       1903
275162                 TA   =          221
87961
                                          MA   =          221
96805
                                          Ha   =            228
059  n
mi
                                          Hp   =            220
541

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4445484
33                 X    =         1427958
83
 Y    =      -14245556
19  feet           Y    =        -4326485
47  meter
 Z    =      -16562985
49                 Z    =        -5041638
54
 XDOT =      24325
510572                 XDOT =        7403
388448
 YDOT =        361
236176  feet/sec       YDOT =         192
956484  meter/sec
 ZDOT =       6244
341082                 ZDOT =        1939
264217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1472594
81                 X    =          448846
90
 Y    =      -14884959
11  feet           Y    =        -4536935
54  meter
 Z    =      -16531792
02                 Z    =        -5038890
21
 XDOT =      22734
798775                 XDOT =        6929
566667
 YDOT =      -4838
798376  feet/sec       YDOT =       -1474
865745  meter/sec
 ZDOT =       6408
060745                 ZDOT =        1953
176915


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   19243
10716478  
00016717  00000-0  10270-3 0  9178
2 25544  51
6445 349
6388 0007938 346
7565  13
3376 15
50418874 26870


Satellite: ISS
Catalog Number: 25544
Epoch time:      19243
10716478   =   yrday
fracday
Element set:     917
Inclination:       51
6445  deg
RA of node:       349
6388  deg
Eccentricity:     
0007938     
Arg of perigee:   346
7565  deg
Mean anomaly:      13
3376  deg
Mean motion:   15
50418874  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2687
Checksum:              352
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