[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: August 25th 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 3

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 2

236/05:30:52 000 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 221 9

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 1

Coasting Arc #1 (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    =        5953041
03                 A    =         6799187
29  meter
 Y    =        2844792
76  meter          E    =           
0011021
 Z    =       -1611961
62                 I    =           51
88955
 XDOT =       -833
906153                 Wp   =          356
07489
 YDOT =       4998
715409  meter/sec      RA   =           36
59038  deg
 ZDOT =       5750
471305                 TA   =          346
36909
                                          MA   =          346
39882
                                          Ha   =            226
597  n
mi
                                          Hp   =            222
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19530974
51                 X    =         5928617
28
 Y    =        9333309
58  feet           Y    =         2911227
25  meter
 Z    =       -5288588
00                 Z    =        -1583103
52
 XDOT =      -2735
912574                 XDOT =        -917
673716
 YDOT =      16399
984938  feet/sec       YDOT =        4988
921869  meter/sec
 ZDOT =      18866
375672                 ZDOT =        5746
216928

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11848023
51                 X    =        -3611277
56
 Y    =      -18153873
79  feet           Y    =        -5533300
73  meter
 Z    =       -5157518
95                 Z    =        -1572011
77
 XDOT =       9658
171194                 XDOT =        2943
810580
 YDOT =     -11649
637636  feet/sec       YDOT =       -3550
809551  meter/sec
 ZDOT =      18846
504157                 ZDOT =        5744
414467


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
50307464  
00016717  00000-0  10270-3 0  9004
2 25544  51
6408  37
2388 0007281 309
5568  50
4939 15
50385689 25389


Satellite: ISS
Catalog Number: 25544
Epoch time:      19233
50307464   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:        37
2388  deg
Eccentricity:     
0007281     
Arg of perigee:   309
5568  deg
Mean anomaly:      50
4939  deg
Mean motion:   15
50385689  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2538
Checksum:              327


Coasting Arc #2 (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    =        4342360
43                 A    =         6798412
97  meter
 Y    =        4797767
34  meter          E    =           
0012692
 Z    =        2056614
35                 I    =           51
87092
 XDOT =      -4871
001186                 Wp   =           35
98844
 YDOT =       2019
960360  meter/sec      RA   =           33
40679  deg
 ZDOT =       5565
027715                 TA   =          346
65835
                                          MA   =          346
69188
                                          Ha   =            226
780  n
mi
                                          Hp   =            222
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14246589
35                 X    =         4278397
83
 Y    =       15740706
50  feet           Y    =         4845969
07  meter
 Z    =        6747422
42                 Z    =         2077552
40
 XDOT =     -15980
975021                 XDOT =       -4920
258669
 YDOT =       6627
166536  feet/sec       YDOT =        1965
214084  meter/sec
 ZDOT =      18257
964945                 ZDOT =        5541
246622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19362226
76                 X    =         5901606
72
 Y    =        8634284
27  feet           Y    =         2631729
85  meter
 Z    =        6842234
17                 Z    =         2085512
98
 XDOT =     -11405
287288                 XDOT =       -3476
331565
 YDOT =      11174
593843  feet/sec       YDOT =        3406
016203  meter/sec
 ZDOT =      18149
515577                 ZDOT =        5531
972348


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
21210678  
00016717  00000-0  10270-3 0  9014
2 25544  51
6423  33
7287 0007647 314
5140  45
5385 15
50380337 25490


Satellite: ISS
Catalog Number: 25544
Epoch time:      19234
21210678   =   yrday
fracday
Element set:     901
Inclination:       51
6423  deg
RA of node:        33
7287  deg
Eccentricity:     
0007647     
Arg of perigee:   314
5140  deg
Mean anomaly:      45
5385  deg
Mean motion:   15
50380337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2549
Checksum:              298


Coasting Arc #3 (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    =       -4359085
70                 A    =         6797541
32  meter
 Y    =       -4586337
30  meter          E    =           
0002556
 Z    =       -2486759
69                 I    =           51
84069
 XDOT =       5128
128121                 Wp   =          332
65932
 YDOT =      -1982
425214  meter/sec      RA   =           28
46713  deg
 ZDOT =      -5328
609280                 TA   =          235
06334
                                          MA   =          235
08735
                                          Ha   =            226
945  n
mi
                                          Hp   =            222
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14301462
27                 X    =        -4295396
71
 Y    =      -15047038
40  feet           Y    =        -4634727
57  meter
 Z    =       -8158660
40                 Z    =        -2507779
74
 XDOT =      16824
567326                 XDOT =        5175
798399
 YDOT =      -6504
019731  feet/sec       YDOT =       -1924
812345  meter/sec
 ZDOT =     -17482
313910                 ZDOT =       -5303
583032

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19257047
19                 X    =        -5869547
98
 Y    =       -7651728
24  feet           Y    =        -2332246
77  meter
 Z    =       -8253854
60                 Z    =        -2515774
88
 XDOT =      12070
956940                 XDOT =        3679
227675
 YDOT =     -11628
605693  feet/sec       YDOT =       -3544
399015  meter/sec
 ZDOT =     -17368
205034                 ZDOT =       -5293
828894


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
17896763  
00016717  00000-0  10270-3 0  9026
2 25544  51
6433  28
9367 0007704 317
7620  42
2936 15
50392030 25644


Satellite: ISS
Catalog Number: 25544
Epoch time:      19235
17896763   =   yrday
fracday
Element set:     902
Inclination:       51
6433  deg
RA of node:        28
9367  deg
Eccentricity:     
0007704     
Arg of perigee:   317
7620  deg
Mean anomaly:      42
2936  deg
Mean motion:   15
50392030  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2564
Checksum:              314


Coasting Arc #4 (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    =        4363966
29                 A    =         6790625
56  meter
 Y    =       -2066831
57  meter          E    =           
0005663
 Z    =       -4778377
02                 I    =           51
80233
 XDOT =       5250
508104                 Wp   =           70
51231
 YDOT =       4885
460271  meter/sec      RA   =           25
79538  deg
 ZDOT =       2686
436801                 TA   =          225
97412
                                          MA   =          226
02079
                                          Ha   =            226
894  n
mi
                                          Hp   =            222
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14317474
72                 X    =         4409964
50
 Y    =       -6780943
48  feet           Y    =        -2017773
40  meter
 Z    =      -15677089
96                 Z    =        -4757066
86
 XDOT =      17226
076457                 XDOT =        5182
438070
 YDOT =      16028
412962  feet/sec       YDOT =        4943
794525  meter/sec
 ZDOT =       8813
769033                 ZDOT =        2711
776437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7490342
46                 X    =        -2283056
38
 Y    =       14067846
85  feet           Y    =         4287879
72  meter
 Z    =      -15579887
07                 Z    =        -4748749
58
 XDOT =     -22320
752501                 XDOT =       -6803
365362
 YDOT =      -2012
520337  feet/sec       YDOT =        -613
416199  meter/sec
 ZDOT =       8928
585297                 ZDOT =        2721
432799


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
69462492  
00016717  00000-0  10270-3 0  9032
2 25544  51
6438  26
3787 0007418 316
9241  43
1337 15
50416771 25722


Satellite: ISS
Catalog Number: 25544
Epoch time:      19235
69462492   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:        26
3787  deg
Eccentricity:     
0007418     
Arg of perigee:   316
9241  deg
Mean anomaly:      43
1337  deg
Mean motion:   15
50416771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2572
Checksum:              318


Coasting Arc #5 (Orbit 2580)
---------------------------------------

Vector Time (GMT): 2019/236/05:30:52
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3547364
70                 A    =         6789381
93  meter
 Y    =        2818121
52  meter          E    =           
0009333
 Z    =        5059617
84                 I    =           51
78299
 XDOT =      -6093
649066                 Wp   =          358
33046
 YDOT =      -4231
338407  meter/sec      RA   =           23
10073  deg
 ZDOT =      -1906
544052                 TA   =          110
18950
                                          MA   =          110
08909
                                          Ha   =            227
119  n
mi
                                          Hp   =            221
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11638335
63                 X    =        -3603190
83
 Y    =        9245805
52  feet           Y    =         2778140
17  meter
 Z    =       16599796
05                 Z    =         5042250
58
 XDOT =     -19992
286963                 XDOT =       -6036
619230
 YDOT =     -13882
343855  feet/sec       YDOT =       -4299
162975  meter/sec
 ZDOT =      -6255
065788                 ZDOT =       -1936
006163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         584459
43                 X    =          178143
23
 Y    =       14940609
45  feet           Y    =         4553897
76  meter
 Z    =       16520460
08                 Z    =         5035436
23
 XDOT =     -21862
677275                 XDOT =       -6663
744034
 YDOT =       7952
345805  feet/sec       YDOT =        2423
875001  meter/sec
 ZDOT =      -6388
706287                 ZDOT =       -1947
277676


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
27473932  
00016717  00000-0  10270-3 0  9049
2 25544  51
6449  23
5060 0007896 320
8831  39
1748 15
50437349 25811


Satellite: ISS
Catalog Number: 25544
Epoch time:      19236
27473932   =   yrday
fracday
Element set:     904
Inclination:       51
6449  deg
RA of node:        23
5060  deg
Eccentricity:     
0007896     
Arg of perigee:   320
8831  deg
Mean anomaly:      39
1748  deg
Mean motion:   15
50437349  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2581
Checksum:              324


Coasting Arc #6 (Orbit 2595)
---------------------------------------

Vector Time (GMT): 2019/237/05:30:52
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3770752
72                 A    =         6790167
27  meter
 Y    =       -2824074
24  meter          E    =           
0007344
 Z    =       -4894708
39                 I    =           51
75366
 XDOT =       6085
992300                 Wp   =           65
98752
 YDOT =       3982
822382  meter/sec      RA   =           18
14997  deg
 ZDOT =       2396
292369                 TA   =          227
46197
                                          MA   =          227
52400
                                          Ha   =            227
338  n
mi
                                          Hp   =            221
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12371235
94                 X    =         3825827
71
 Y    =       -9265335
45  feet           Y    =        -2781598
95  meter
 Z    =      -16058754
56                 Z    =        -4876257
91
 XDOT =      19967
166337                 XDOT =        6029
363125
 YDOT =      13067
002564  feet/sec       YDOT =        4050
563528  meter/sec
 ZDOT =       7861
851603                 ZDOT =        2425
718228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -439318
85                 X    =         -133904
39
 Y    =      -15537059
42  feet           Y    =        -4735695
71  meter
 Z    =      -15974489
07                 Z    =        -4869024
27
 XDOT =      20989
656700                 XDOT =        6397
647362
 YDOT =      -8794
425028  feet/sec       YDOT =       -2680
540749  meter/sec
 ZDOT =       7995
343900                 ZDOT =        2436
980821


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
24159795  
00016717  00000-0  10270-3 0  9056
2 25544  51
6444  18
7132 0007878 325
2106  34
8529 15
50407099 25960


Satellite: ISS
Catalog Number: 25544
Epoch time:      19237
24159795   =   yrday
fracday
Element set:     905
Inclination:       51
6444  deg
RA of node:        18
7132  deg
Eccentricity:     
0007878     
Arg of perigee:   325
2106  deg
Mean anomaly:      34
8529  deg
Mean motion:   15
50407099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2596
Checksum:              330


Coasting Arc #7 (Orbit 2611)
---------------------------------------

Vector Time (GMT): 2019/238/05:30:52
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4021052
66                 A    =         6790955
31  meter
 Y    =        2846746
47  meter          E    =           
0010848
 Z    =        4675893
24                 I    =           51
72394
 XDOT =      -6023
493724                 Wp   =           17
29457
 YDOT =      -3750
564886  meter/sec      RA   =           13
19795  deg
 ZDOT =      -2884
699483                 TA   =          101
43441
                                          MA   =          101
31255
                                          Ha   =            227
446  n
mi
                                          Hp   =            221
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13192430
00                 X    =        -4075299
62
 Y    =        9339719
38  feet           Y    =         2801476
76  meter
 Z    =       15340857
07                 Z    =         4656229
00
 XDOT =     -19762
118517                 XDOT =       -5967
094022
 YDOT =     -12305
002908  feet/sec       YDOT =       -3817
608386  meter/sec
 ZDOT =      -9464
237148                 ZDOT =       -2913
822207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         311766
61                 X    =           95026
46
 Y    =       16245621
19  feet           Y    =         4951665
34  meter
 Z    =       15251067
40                 Z    =         4648525
34
 XDOT =     -20030
506024                 XDOT =       -6105
298236
 YDOT =       9429
942974  feet/sec       YDOT =        2874
246618  meter/sec
 ZDOT =      -9596
368099                 ZDOT =       -2924
972996


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
27291114  
00016717  00000-0  10270-3 0  9063
2 25544  51
6438  13
6013 0007988 328
7983  31
2693 15
50440746 26126


Satellite: ISS
Catalog Number: 25544
Epoch time:      19238
27291114   =   yrday
fracday
Element set:     906
Inclination:       51
6438  deg
RA of node:        13
6013  deg
Eccentricity:     
0007988     
Arg of perigee:   328
7983  deg
Mean anomaly:      31
2693  deg
Mean motion:   15
50440746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2612
Checksum:              313


Coasting Arc #8 (Orbit 2626)
---------------------------------------

Vector Time (GMT): 2019/239/05:30:52
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4227486
74                 A    =         6791963
96  meter
 Y    =       -2929499
96  meter          E    =           
0006071
 Z    =       -4437670
04                 I    =           51
69414
 XDOT =       5930
494184                 Wp   =           50
01549
 YDOT =       3519
547874  meter/sec      RA   =            8
24391  deg
 ZDOT =       3333
028500                 TA   =          253
63001
                                          MA   =          253
69676
                                          Ha   =            227
629  n
mi
                                          Hp   =            221
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13869707
16                 X    =         4281486
49
 Y    =       -9611220
36  feet           Y    =        -2881923
18  meter
 Z    =      -14559284
90                 Z    =        -4417003
71
 XDOT =      19457
001917                 XDOT =        5874
507054
 YDOT =      11547
073078  feet/sec       YDOT =        3585
553701  meter/sec
 ZDOT =      10935
132874                 ZDOT =        3361
700317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -452765
36                 X    =         -138002
88
 Y    =      -16949274
97  feet           Y    =        -5166139
01  meter
 Z    =      -14464929
71                 Z    =        -4408910
58
 XDOT =      19006
318272                 XDOT =        5793
125809
 YDOT =      -9931
808366  feet/sec       YDOT =       -3027
215190  meter/sec
 ZDOT =      11065
232368                 ZDOT =        3372
682826


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
23976875  
00016717  00000-0  10270-3 0  9075
2 25544  51
6437   8
8083 0007955 331
9401  28
1320 15
50406913 26279


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
23976875   =   yrday
fracday
Element set:     907
Inclination:       51
6437  deg
RA of node:         8
8083  deg
Eccentricity:     
0007955     
Arg of perigee:   331
9401  deg
Mean anomaly:      28
1320  deg
Mean motion:   15
50406913  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2627
Checksum:              318


Coasting Arc #9 (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    =        2855484
30                 A    =         6789770
12  meter
 Y    =       -3640020
19  meter          E    =           
0008978
 Z    =       -4975769
71                 I    =           51
67453
 XDOT =       6914
132200                 Wp   =           68
33132
 YDOT =       2484
131249  meter/sec      RA   =            6
34315  deg
 ZDOT =       2156
970845                 TA   =          222
67773
                                          MA   =          222
74750
                                          Ha   =            227
472  n
mi
                                          Hp   =            221
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9368386
82                 X    =         2920144
97
 Y    =      -11942323
44  feet           Y    =        -3607726
51  meter
 Z    =      -16324703
76                 Z    =        -4961742
09
 XDOT =      22684
160760                 XDOT =        6875
362861
 YDOT =       8150
036905  feet/sec       YDOT =        2561
233123  meter/sec
 ZDOT =       7076
676000                 ZDOT =        2190
462458

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5871375
48                 X    =        -1789595
24
 Y    =       14071435
59  feet           Y    =         4288973
57  meter
 Z    =      -16260484
74                 Z    =        -4956195
75
 XDOT =     -22973
463043                 XDOT =       -7002
311535
 YDOT =      -1256
644095  feet/sec       YDOT =        -383
025120  meter/sec
 ZDOT =       7228
816749                 ZDOT =        2203
343345


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
62651089  
00016717  00000-0  10270-3 0  9086
2 25544  51
6440   6
8886 0007518 332
4665  27
6087 15
50420552 26331


Satellite: ISS
Catalog Number: 25544
Epoch time:      19239
62651089   =   yrday
fracday
Element set:     908
Inclination:       51
6440  deg
RA of node:         6
8886  deg
Eccentricity:     
0007518     
Arg of perigee:   332
4665  deg
Mean anomaly:      27
6087  deg
Mean motion:   15
50420552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2633
Checksum:              321


Coasting Arc #10 (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    =        -662154
23                 A    =         6788171
35  meter
 Y    =        4169858
54  meter          E    =           
0008025
 Z    =        5316495
35                 I    =           51
65323
 XDOT =      -7614
531322                 Wp   =          353
73397
 YDOT =       -786
580705  meter/sec      RA   =            3
98083  deg
 ZDOT =       -323
686131                 TA   =           99
39925
                                          MA   =           99
30851
                                          Ha   =            227
678  n
mi
                                          Hp   =            221
053

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2172422
02                 X    =         -734557
70
 Y    =       13680638
26  feet           Y    =         4162048
97  meter
 Z    =       17442570
06                 Z    =         5313103
11
 XDOT =     -24982
058142                 XDOT =       -7603
597367
 YDOT =      -2580
645357  feet/sec       YDOT =        -871
670614  meter/sec
 ZDOT =      -1061
962373                 ZDOT =        -360
647460

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -89720
68                 X    =          -27346
86
 Y    =       13871728
27  feet           Y    =         4228102
78  meter
 Z    =       17426693
20                 Z    =         5311656
09
 XDOT =     -24055
867856                 XDOT =       -7332
228522
 YDOT =       1421
673841  feet/sec       YDOT =         433
326187  meter/sec
 ZDOT =      -1230
069146                 ZDOT =        -374
925076


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
14216674  
00016717  00000-0  10270-3 0  9093
2 25544  51
6437   4
3349 0007953 335
5524  24
5248 15
50435038 26414


Satellite: ISS
Catalog Number: 25544
Epoch time:      19240
14216674   =   yrday
fracday
Element set:     909
Inclination:       51
6437  deg
RA of node:         4
3349  deg
Eccentricity:     
0007953     
Arg of perigee:   335
5524  deg
Mean anomaly:      24
5248  deg
Mean motion:   15
50435038  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2641
Checksum:              301


Coasting Arc #11 (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    =         884450
42                 A    =         6788460
95  meter
 Y    =       -4192920
34  meter          E    =           
0013010
 Z    =       -5274350
80                 I    =           51
62142
 XDOT =       7588
011460                 Wp   =           63
23938
 YDOT =        542
418841  meter/sec      RA   =          359
02057  deg
 ZDOT =        848
561669                 TA   =          214
84759
                                          MA   =          214
93284
                                          Ha   =            227
854  n
mi
                                          Hp   =            220
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2901740
23                 X    =          956890
48
 Y    =      -13756300
32  feet           Y    =        -4182624
83  meter
 Z    =      -17304300
52                 Z    =        -5269878
55
 XDOT =      24895
050721                 XDOT =        7577
260267
 YDOT =       1779
589372  feet/sec       YDOT =         627
213226  meter/sec
 ZDOT =       2783
994977                 ZDOT =         885
394509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         554859
40                 X    =          169121
14
 Y    =      -14073629
16  feet           Y    =        -4289642
17  meter
 Z    =      -17283512
51                 Z    =        -5268014
61
 XDOT =      23775
334298                 XDOT =        7246
721894
 YDOT =      -2657
753503  feet/sec       YDOT =        -810
083268  meter/sec
 ZDOT =       2951
534660                 ZDOT =         899
627764


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
10902117  
00016717  00000-0  10270-3 0  9106
2 25544  51
6446 359
5423 0007953 340
5154  19
5691 15
50412096 26568


Satellite: ISS
Catalog Number: 25544
Epoch time:      19241
10902117   =   yrday
fracday
Element set:     910
Inclination:       51
6446  deg
RA of node:       359
5423  deg
Eccentricity:     
0007953     
Arg of perigee:   340
5154  deg
Mean anomaly:      19
5691  deg
Mean motion:   15
50412096  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2656
Checksum:              298


Coasting Arc #12 (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    =       -1143067
30                 A    =         6788795
53  meter
 Y    =        4244186
06  meter          E    =           
0010390
 Z    =        5174756
63                 I    =           51
58905
 XDOT =      -7528
057471                 Wp   =            7
32368
 YDOT =       -322
844404  meter/sec      RA   =          354
05878  deg
 ZDOT =      -1387
720872                 TA   =           96
10039
                                          MA   =           95
98200
                                          Ha   =            227
966  n
mi
                                          Hp   =            220
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3750220
81                 X    =        -1215577
65
 Y    =       13924494
94  feet           Y    =         4230998
28  meter
 Z    =       16977548
00                 Z    =         5169027
85
 XDOT =     -24698
351284                 XDOT =       -7517
147194
 YDOT =      -1059
200799  feet/sec       YDOT =        -406
967504  meter/sec
 ZDOT =      -4552
890001                 ZDOT =       -1424
262102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1110736
78                 X    =         -338552
57
 Y    =       14409066
23  feet           Y    =         4391883
39  meter
 Z    =       16951044
97                 Z    =         5166678
51
 XDOT =     -23358
779765                 XDOT =       -7119
756072
 YDOT =       3791
154145  feet/sec       YDOT =        1155
543783  meter/sec
 ZDOT =      -4719
114409                 ZDOT =       -1438
386072


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
14032978  
00016717  00000-0  10270-3 0  9111
2 25544  51
6442 354
4309 0008024 343
2658  16
8227 15
50441897 26724


Satellite: ISS
Catalog Number: 25544
Epoch time:      19242
14032978   =   yrday
fracday
Element set:     911
Inclination:       51
6442  deg
RA of node:       354
4309  deg
Eccentricity:     
0008024     
Arg of perigee:   343
2658  deg
Mean anomaly:      16
8227  deg
Mean motion:   15
50441897  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2672
Checksum:              309


Coasting Arc #13 (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    =        1343588
65                 A    =         6789428
72  meter
 Y    =       -4342159
43  meter          E    =           
0011564
 Z    =       -5051301
22                 I    =           51
55852
 XDOT =       7417
078323                 Wp   =           66
10484
 YDOT =        101
659455  meter/sec      RA   =          349
09503  deg
 ZDOT =       1893
486152                 TA   =          222
25846
                                          MA   =          222
34763
                                          Ha   =            228
085  n
mi
                                          Hp   =            220
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4408099
25                 X    =         1416580
08
 Y    =      -14245929
88  feet           Y    =        -4326726
71  meter
 Z    =      -16572510
57                 Z    =        -5044597
09
 XDOT =      24334
246468                 XDOT =        7406
192939
 YDOT =        333
528396  feet/sec       YDOT =         184
541721  meter/sec
 ZDOT =       6212
224908                 ZDOT =        1929
488486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1436023
82                 X    =          437700
06
 Y    =      -14877509
99  feet           Y    =        -4534665
05  meter
 Z    =      -16541568
72                 Z    =        -5041870
15
 XDOT =      22738
292929                 XDOT =        6930
631685
 YDOT =      -4865
101573  feet/sec       YDOT =       -1482
882959  meter/sec
 ZDOT =       6376
005843                 ZDOT =        1943
406581


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
10718231  
00016717  00000-0  10270-3 0  9122
2 25544  51
6449 349
6387 0008031 346
5325  13
5610 15
50415328 26874


Satellite: ISS
Catalog Number: 25544
Epoch time:      19243
10718231   =   yrday
fracday
Element set:     912
Inclination:       51
6449  deg
RA of node:       349
6387  deg
Eccentricity:     
0008031     
Arg of perigee:   346
5325  deg
Mean anomaly:      13
5610  deg
Mean motion:   15
50415328  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2687
Checksum:              300


Coasting Arc #14 (Orbit 2702)
---------------------------------------

Vector Time (GMT): 2019/244/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1574164
11                 A    =         6790080
89  meter
 Y    =        4467190
92  meter          E    =           
0012493
 Z    =        4865771
18                 I    =           51
52886
 XDOT =      -7272
186276                 Wp   =           21
53970
 YDOT =         76
786545  meter/sec      RA   =          344
12898  deg
 ZDOT =      -2409
830807                 TA   =           92
21952
                                          MA   =           92
07646
                                          Ha   =            228
217  n
mi
                                          Hp   =            220
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5164580
40                 X    =        -1647635
48
 Y    =       14656138
18  feet           Y    =         4449177
11  meter
 Z    =       15963816
19                 Z    =         4857945
74
 XDOT =     -23858
878859                 XDOT =       -7260
798957
 YDOT =        251
924359  feet/sec       YDOT =          -4
472700  meter/sec
 ZDOT =      -7906
269051                 ZDOT =       -2445
128304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1819983
53                 X    =         -554730
98
 Y    =       15469729
30  feet           Y    =         4715173
49  meter
 Z    =       15927769
45                 Z    =         4854784
13
 XDOT =     -22003
139607                 XDOT =       -6706
556952
 YDOT =       5762
260695  feet/sec       YDOT =        1756
337060  meter/sec
 ZDOT =      -8066
845441                 ZDOT =       -2458
774491


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   19244
13848690  
00016717  00000-0  10270-3 0  9130
2 25544  51
6452 344
5268 0008172 350
0897  10
0091 15
50454867 27035


Satellite: ISS
Catalog Number: 25544
Epoch time:      19244
13848690   =   yrday
fracday
Element set:     913
Inclination:       51
6452  deg
RA of node:       344
5268  deg
Eccentricity:     
0008172     
Arg of perigee:   350
0897  deg
Mean anomaly:      10
0091  deg
Mean motion:   15
50454867  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2703
Checksum:              309


Coasting Arc #15 (Orbit 2717)
---------------------------------------

Vector Time (GMT): 2019/245/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1729480
20                 A    =         6791006
23  meter
 Y    =       -4628353
16  meter          E    =           
0010081
 Z    =       -4664387
97                 I    =           51
49892
 XDOT =       7089
724901                 Wp   =           62
36968
 YDOT =       -245
673548  meter/sec      RA   =          339
16157  deg
 ZDOT =       2881
895518                 TA   =          236
32831
                                          MA   =          236
42450
                                          Ha   =            228
372  n
mi
                                          Hp   =            220
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5674147
64                 X    =         1803764
12
 Y    =      -15184885
69  feet           Y    =        -4608597
93  meter
 Z    =      -15303110
13                 Z    =        -4655806
05
 XDOT =      23260
252301                 XDOT =        7077
946606
 YDOT =       -806
015578  feet/sec       YDOT =        -166
456865  meter/sec
 ZDOT =       9455
037790                 ZDOT =        2916
305951

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1915156
92                 X    =          583739
83
 Y    =      -16134315
46  feet           Y    =        -4917739
35  meter
 Z    =      -15263614
35                 Z    =        -4652349
66
 XDOT =      21129
038240                 XDOT =        6440
130856
 YDOT =      -6555
710628  feet/sec       YDOT =       -1998
180599  meter/sec
 ZDOT =       9611
580078                 ZDOT =        2929
609608


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   19245
10533589  
00016717  00000-0  10270-3 0  9147
2 25544  51
6443 339
7344 0008163 354
1495   5
9559 15
50418285 27187


Satellite: ISS
Catalog Number: 25544
Epoch time:      19245
10533589   =   yrday
fracday
Element set:     914
Inclination:       51
6443  deg
RA of node:       339
7344  deg
Eccentricity:     
0008163     
Arg of perigee:   354
1495  deg
Mean anomaly:       5
9559  deg
Mean motion:   15
50418285  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2718
Checksum:              328


Coasting Arc #16 (Orbit 2733)
---------------------------------------

Vector Time (GMT): 2019/246/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1906944
42                 A    =         6791913
66  meter
 Y    =        4811543
94  meter          E    =           
0014221
 Z    =        4397373
58                 I    =           51
47096
 XDOT =      -6877
607035                 Wp   =           36
59389
 YDOT =        357
132809  meter/sec      RA   =          334
19259  deg
 ZDOT =      -3356
470413                 TA   =           87
54557
                                          MA   =           87
38277
                                          Ha   =            228
466  n
mi
                                          Hp   =            219
887

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6256379
32                 X    =        -1981966
73
 Y    =       15785905
31  feet           Y    =         4789799
98  meter
 Z    =       14427078
69                 Z    =         4387927
82
 XDOT =     -22564
327543                 XDOT =       -6864
785599
 YDOT =       1171
695569  feet/sec       YDOT =         280
294013  meter/sec
 ZDOT =     -11012
042038                 ZDOT =       -3389
848072

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2037913
51                 X    =         -621156
04
 Y    =       16894833
90  feet           Y    =         5149545
37  meter
 Z    =       14383642
93                 Z    =         4384134
37
 XDOT =     -20182
833557                 XDOT =       -6151
727668
 YDOT =       7117
094088  feet/sec       YDOT =        2169
290278  meter/sec
 ZDOT =     -11163
883991                 ZDOT =       -3402
751840


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   19246
13663859  
00016717  00000-0  10270-3 0  9156
2 25544  51
6438 334
6225 0008258 357
4503   2
6605 15
50456933 27340


Satellite: ISS
Catalog Number: 25544
Epoch time:      19246
13663859   =   yrday
fracday
Element set:     915
Inclination:       51
6438  deg
RA of node:       334
6225  deg
Eccentricity:     
0008258     
Arg of perigee:   357
4503  deg
Mean anomaly:       2
6605  deg
Mean motion:   15
50456933  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2734
Checksum:              320


Coasting Arc #17 (Orbit 2748)
---------------------------------------

Vector Time (GMT): 2019/247/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1996845
02                 A    =         6792990
57  meter
 Y    =       -5015887
98  meter          E    =           
0009158
 Z    =       -4124876
54                 I    =           51
44456
 XDOT =       6646
101127                 Wp   =           50
31580
 YDOT =       -452
652863  meter/sec      RA   =          329
22168  deg
 ZDOT =       3779
128588                 TA   =          258
75573
                                          MA   =          258
85867
                                          Ha   =            228
573  n
mi
                                          Hp   =            219
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6551328
80                 X    =         2072822
08
 Y    =      -16456325
40  feet           Y    =        -4993133
26  meter
 Z    =      -13533059
52                 Z    =        -4114991
81
 XDOT =      21804
793725                 XDOT =        6632
311957
 YDOT =      -1485
081573  feet/sec       YDOT =        -378
408378  meter/sec
 ZDOT =      12398
715841                 ZDOT =        3811
379397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1839568
94                 X    =          560700
61
 Y    =      -17651473
47  feet           Y    =        -5380169
11  meter
 Z    =      -13487613
77                 Z    =        -4111024
68
 XDOT =      19179
142428                 XDOT =        5845
802612
 YDOT =      -7558
767035  feet/sec       YDOT =       -2303
912192  meter/sec
 ZDOT =      12545
431242                 ZDOT =        3823
847443


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   19247
10348520  
00016717  00000-0  10270-3 0  9160
2 25544  51
6436 329
8295 0008203    
5066 359
6091 15
50422045 27498


Satellite: ISS
Catalog Number: 25544
Epoch time:      19247
10348520   =   yrday
fracday
Element set:     916
Inclination:       51
6436  deg
RA of node:       329
8295  deg
Eccentricity:     
0008203     
Arg of perigee:      
5066  deg
Mean anomaly:     359
6091  deg
Mean motion:   15
50422045  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2749
Checksum:              302


Coasting Arc #18 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2019/248/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933315
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2105122
52                 A    =         6794029
89  meter
 Y    =        5234262
73  meter          E    =           
0015478
 Z    =        3783359
70                 I    =           51
42051
 XDOT =      -6391
879367                 Wp   =           50
89969
 YDOT =        477
417308  meter/sec      RA   =          324
24910  deg
 ZDOT =      -4195
893591                 TA   =           83
66482
                                          MA   =           83
48856
                                          Ha   =            228
699  n
mi
                                          Hp   =            219
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6906569
95                 X    =        -2181874
57
 Y    =       17172777
99  feet           Y    =         5210292
76  meter
 Z    =       12412597
43                 Z    =         3772947
19
 XDOT =     -20970
732830                 XDOT =       -6376
361599
 YDOT =       1566
329752  feet/sec       YDOT =         406
025425  meter/sec
 ZDOT =     -13766
055087                 ZDOT =       -4226
905282

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1658495
92                 X    =         -505509
56
 Y    =       18467275
47  feet           Y    =         5628825
56  meter
 Z    =       12364736
76                 Z    =         3768771
77
 XDOT =     -18158
817141                 XDOT =       -5534
807465
 YDOT =       7727
357544  feet/sec       YDOT =        2355
298580  meter/sec
 ZDOT =     -13907
129731                 ZDOT =       -4238
893142


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   19248
13478393  
00016717  00000-0  10270-3 0  9177
2 25544  51
6439 324
7165 0008405   4
1981 355
9238 15
50458189 27659


Satellite: ISS
Catalog Number: 25544
Epoch time:      19248
13478393   =   yrday
fracday
Element set:     917
Inclination:       51
6439  deg
RA of node:       324
7165  deg
Eccentricity:     
0008405     
Arg of perigee:     4
1981  deg
Mean anomaly:     355
9238  deg
Mean motion:   15
50458189  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              340
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