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

 
Date: April 30th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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


121/07:59:48 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 3

124/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 217 4

128/05:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 2

131/09:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 3

Coasting Arc #1 (Orbit 768)
---------------------------------------

Vector Time (GMT): 2019/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2620752
51                 A    =         6782819
88  meter
 Y    =       -3698289
71  meter          E    =           
0004916
 Z    =        5044077
66                 I    =           51
28197
 XDOT =       4690
504802                 Wp   =          138
67176
 YDOT =       5790
838209  meter/sec      RA   =          242
18392  deg
 ZDOT =       1804
126076                 TA   =          293
75036
                                          MA   =          293
80192
                                          Ha   =            222
800  n
mi
                                          Hp   =            217
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8598269
39                 X    =         2637411
63
 Y    =      -12133496
41  feet           Y    =        -3668889
40  meter
 Z    =       16548811
23                 Z    =         5056848
87
 XDOT =      15388
795281                 XDOT =        4616
637913
 YDOT =      18998
813022  feet/sec       YDOT =        5842
877728  meter/sec
 ZDOT =       5919
048806                 ZDOT =        1826
731394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -335102
44                 X    =         -102139
22
 Y    =      -14802520
97  feet           Y    =        -4511808
39  meter
 Z    =       16606872
19                 Z    =         5061774
64
 XDOT =      22535
280818                 XDOT =        6868
753593
 YDOT =       6261
531068  feet/sec       YDOT =        1908
514670  meter/sec
 ZDOT =       6020
776856                 ZDOT =        1835
132786


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   19119
55146691  
00016717  00000-0  10270-3 0  9005
2 25544  51
6399 242
9409 0001396 246
2119 113
8887 15
52634111  7696


Satellite: ISS
Catalog Number: 25544
Epoch time:      19119
55146691   =   yrday
fracday
Element set:     900
Inclination:       51
6399  deg
RA of node:       242
9409  deg
Eccentricity:     
0001396     
Arg of perigee:   246
2119  deg
Mean anomaly:     113
8887  deg
Mean motion:   15
52634111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             769
Checksum:              325


Coasting Arc #2 (Orbit 783)
---------------------------------------

Vector Time (GMT): 2019/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3275074
57                 A    =         6781833
55  meter
 Y    =        2733444
51  meter          E    =           
0013566
 Z    =       -5283959
45                 I    =           51
29600
 XDOT =      -4446
963627                 Wp   =           87
61426
 YDOT =      -6215
230920  meter/sec      RA   =          237
17716  deg
 ZDOT =       -459
379437                 TA   =          177
97881
                                          MA   =          177
97332
                                          Ha   =            222
950  n
mi
                                          Hp   =            217
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10744995
31                 X    =        -3279730
59
 Y    =        8967993
79  feet           Y    =         2696794
18  meter
 Z    =      -17335824
98                 Z    =        -5299880
01
 XDOT =     -14589
775680                 XDOT =       -4374
901213
 YDOT =     -20391
177559  feet/sec       YDOT =       -6264
557065  meter/sec
 ZDOT =      -1507
150384                 ZDOT =        -480
806110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3031126
09                 X    =         -923887
23
 Y    =       13571401
67  feet           Y    =         4136563
23  meter
 Z    =      -17408044
00                 Z    =        -5305971
81
 XDOT =     -22959
181114                 XDOT =       -6997
958404
 YDOT =      -7182
730862  feet/sec       YDOT =       -2189
296367  meter/sec
 ZDOT =      -1603
532563                 ZDOT =        -488
756725


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   19120
51694566  
00016717  00000-0  10270-3 0  9013
2 25544  51
6408 238
1398 0001207 253
2980 106
8040 15
52619378  7844


Satellite: ISS
Catalog Number: 25544
Epoch time:      19120
51694566   =   yrday
fracday
Element set:     901
Inclination:       51
6408  deg
RA of node:       238
1398  deg
Eccentricity:     
0001207     
Arg of perigee:   253
2980  deg
Mean anomaly:     106
8040  deg
Mean motion:   15
52619378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             784
Checksum:              311


Coasting Arc #3 (Orbit 796)
---------------------------------------

Vector Time (GMT): 2019/121/07:59:48
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1417518
46                 A    =         6783806
68  meter
 Y    =        4553722
20  meter          E    =           
0010721
 Z    =       -4834518
74                 I    =           51
31491
 XDOT =      -5768
428052                 Wp   =           71
21862
 YDOT =      -4398
106143  meter/sec      RA   =          233
03013  deg
 ZDOT =      -2452
402848                 TA   =          174
56371
                                          MA   =          174
55207
                                          Ha   =            223
016  n
mi
                                          Hp   =            217
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4650651
12                 X    =        -1444850
49
 Y    =       14940033
45  feet           Y    =         4537717
58  meter
 Z    =      -15861281
97                 Z    =        -4841471
07
 XDOT =     -18925
288884                 XDOT =       -5706
905927
 YDOT =     -14429
482096  feet/sec       YDOT =       -4462
268809  meter/sec
 ZDOT =      -8045
941103                 ZDOT =       -2480
274456

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9803597
73                 X    =        -2988136
59
 Y    =       12153706
35  feet           Y    =         3704449
70  meter
 Z    =      -15893090
15                 Z    =        -4844213
88
 XDOT =     -11215
070948                 XDOT =       -3418
353625
 YDOT =     -19727
611758  feet/sec       YDOT =       -6012
976064  meter/sec
 ZDOT =      -8171
630957                 ZDOT =       -2490
713116


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   19121
35369116  
00016717  00000-0  10270-3 0  9027
2 25544  51
6375 233
9781 0000952 267
0602  93
0441 15
52619842  7978


Satellite: ISS
Catalog Number: 25544
Epoch time:      19121
35369116   =   yrday
fracday
Element set:     902
Inclination:       51
6375  deg
RA of node:       233
9781  deg
Eccentricity:     
0000952     
Arg of perigee:   267
0602  deg
Mean anomaly:      93
0441  deg
Mean motion:   15
52619842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             797
Checksum:              309


Coasting Arc #4 (Orbit 812)
---------------------------------------

Vector Time (GMT): 2019/122/07:59:48
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2215588
05                 A    =         6782332
01  meter
 Y    =       -3753400
31  meter          E    =           
0003196
 Z    =        5194842
70                 I    =           51
32976
 XDOT =       5718
378575                 Wp   =          134
06095
 YDOT =       4976
022615  meter/sec      RA   =          228
02595  deg
 ZDOT =       1153
796427                 TA   =          304
81171
                                          MA   =          304
84178
                                          Ha   =            222
972  n
mi
                                          Hp   =            217
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7268989
68                 X    =         2232160
98
 Y    =      -12314305
48  feet           Y    =        -3728531
30  meter
 Z    =       17043447
19                 Z    =         5205645
66
 XDOT =      18761
084564                 XDOT =        5656
705693
 YDOT =      16325
533513  feet/sec       YDOT =        5039
624714  meter/sec
 ZDOT =       3785
421350                 ZDOT =        1181
424659

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11089878
78                 X    =         3380195
05
 Y    =       -8934033
69  feet           Y    =        -2723093
47  meter
 Z    =       17092602
29                 Z    =         5209825
18
 XDOT =      10994
097359                 XDOT =        3351
000875
 YDOT =      21144
065585  feet/sec       YDOT =        6444
711190  meter/sec
 ZDOT =       3909
980370                 ZDOT =        1191
762017


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   19122
38353126  
00016717  00000-0  10270-3 0  9036
2 25544  51
6367 228
8555 0001019 271
9291  88
1745 15
52579839  8136


Satellite: ISS
Catalog Number: 25544
Epoch time:      19122
38353126   =   yrday
fracday
Element set:     903
Inclination:       51
6367  deg
RA of node:       228
8555  deg
Eccentricity:     
0001019     
Arg of perigee:   271
9291  deg
Mean anomaly:      88
1745  deg
Mean motion:   15
52579839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             813
Checksum:              326


Coasting Arc #5 (Orbit 827)
---------------------------------------

Vector Time (GMT): 2019/123/07:59:48
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3068804
47                 A    =         6781744
77  meter
 Y    =        2933539
61  meter          E    =           
0013847
 Z    =       -5300594
85                 I    =           51
35342
 XDOT =      -5477
287207                 Wp   =           91
74112
 YDOT =      -5344
797888  meter/sec      RA   =          223
02233  deg
 ZDOT =        213
169772                 TA   =          180
30154
                                          MA   =          180
30238
                                          Ha   =            222
992  n
mi
                                          Hp   =            217
263

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10068256
13                 X    =        -3075632
28
 Y    =        9624473
77  feet           Y    =         2899183
88  meter
 Z    =      -17390403
05                 Z    =        -5315518
80
 XDOT =     -17970
102386                 XDOT =       -5418
148549
 YDOT =     -17535
426141  feet/sec       YDOT =       -5405
718083  meter/sec
 ZDOT =        699
375892                 ZDOT =         186
706380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12642748
21                 X    =        -3853509
65
 Y    =        5639228
99  feet           Y    =         1718837
00  meter
 Z    =      -17458133
04                 Z    =        -5321238
95
 XDOT =     -10481
519332                 XDOT =       -3194
767093
 YDOT =     -21703
650535  feet/sec       YDOT =       -6615
272683  meter/sec
 ZDOT =        580
098602                 ZDOT =         176
814054


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   19123
34900192  
00016717  00000-0  10270-3 0  9045
2 25544  51
6388 224
0543 0000998 271
2567  88
8470 15
52626573  8284


Satellite: ISS
Catalog Number: 25544
Epoch time:      19123
34900192   =   yrday
fracday
Element set:     904
Inclination:       51
6388  deg
RA of node:       224
0543  deg
Eccentricity:     
0000998     
Arg of perigee:   271
2567  deg
Mean anomaly:      88
8470  deg
Mean motion:   15
52626573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             828
Checksum:              323


Coasting Arc #6 (Orbit 843)
---------------------------------------

Vector Time (GMT): 2019/124/07:59:48
000
Vector Time (MET): N/A
Weight (LBS)     : 944482
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3919625
36                 A    =         6782629
09  meter
 Y    =       -2118949
17  meter          E    =           
0004159
 Z    =        5111798
34                 I    =           51
38074
 XDOT =       5054
777938                 Wp   =           47
03189
 YDOT =       5546
943587  meter/sec      RA   =          218
01903  deg
 ZDOT =      -1572
982331                 TA   =           58
21061
                                          MA   =           58
17011
                                          Ha   =            222
959  n
mi
                                          Hp   =            217
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12859663
26                 X    =         3918197
97
 Y    =       -6951932
97  feet           Y    =        -2075125
22  meter
 Z    =       16770991
93                 Z    =         5130835
29
 XDOT =      16583
917118                 XDOT =        5000
015577
 YDOT =      18198
633816  feet/sec       YDOT =        5603
163477  meter/sec
 ZDOT =      -5160
703187                 ZDOT =       -1548
560573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14316090
27                 X    =         4363544
31
 Y    =       -2418380
04  feet           Y    =         -737122
23  meter
 Z    =       16857267
83                 Z    =         5138095
24
 XDOT =       9605
732643                 XDOT =        2927
827310
 YDOT =      21575
760108  feet/sec       YDOT =        6576
291681  meter/sec
 ZDOT =      -5050
661425                 ZDOT =       -1539
441602


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   19124
37883620  
00016717  00000-0  10270-3 0  9056
2 25544  51
6383 218
9311 0000906 276
4802  83
6246 15
52585828  8441


Satellite: ISS
Catalog Number: 25544
Epoch time:      19124
37883620   =   yrday
fracday
Element set:     905
Inclination:       51
6383  deg
RA of node:       218
9311  deg
Eccentricity:     
0000906     
Arg of perigee:   276
4802  deg
Mean anomaly:      83
6246  deg
Mean motion:   15
52585828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             844
Checksum:              321


Coasting Arc #7 (Orbit 845)
---------------------------------------

Vector Time (GMT): 2019/124/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2104385
95                 A    =         6781724
92  meter
 Y    =       -3698957
47  meter          E    =           
0001721
 Z    =        5279108
81                 I    =           51
38494
 XDOT =       6314
787728                 Wp   =          125
41251
 YDOT =       4319
306930  meter/sec      RA   =          217
41285  deg
 ZDOT =        508
115571                 TA   =          319
71590
                                          MA   =          319
72865
                                          Ha   =            222
784  n
mi
                                          Hp   =            217
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6904153
37                 X    =         2119948
85
 Y    =      -12135687
24  feet           Y    =        -3675337
82  meter
 Z    =       17319910
79                 Z    =         5289369
08
 XDOT =      20717
807507                 XDOT =        6263
550486
 YDOT =      14170
954495  feet/sec       YDOT =        4389
636815  meter/sec
 ZDOT =       1667
045835                 ZDOT =         538
666670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         743126
93                 X    =          226505
09
 Y    =      -13884171
80  feet           Y    =        -4231895
56  meter
 Z    =       17366608
31                 Z    =         5293342
21
 XDOT =      23820
348214                 XDOT =        7260
442135
 YDOT =       3537
047419  feet/sec       YDOT =        1078
092053  meter/sec
 ZDOT =       1804
910042                 ZDOT =         550
136581


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   19124
50756214  
00016717  00000-0  10270-3 0  9060
2 25544  51
6416 218
2918 0001201 275
2243  84
8772 15
52660260  8462


Satellite: ISS
Catalog Number: 25544
Epoch time:      19124
50756214   =   yrday
fracday
Element set:     906
Inclination:       51
6416  deg
RA of node:       218
2918  deg
Eccentricity:     
0001201     
Arg of perigee:   275
2243  deg
Mean anomaly:      84
8772  deg
Mean motion:   15
52660260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             846
Checksum:              296


Coasting Arc #8 (Orbit 860)
---------------------------------------

Vector Time (GMT): 2019/125/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3074503
87                 A    =         6781911
60  meter
 Y    =        3012587
55  meter          E    =           
0013406
 Z    =       -5252560
47                 I    =           51
41209
 XDOT =      -6025
783471                 Wp   =           96
29456
 YDOT =      -4643
214934  meter/sec      RA   =          212
41381  deg
 ZDOT =        864
463910                 TA   =          182
00827
                                          MA   =          182
01366
                                          Ha   =            222
936  n
mi
                                          Hp   =            217
274

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10086954
96                 X    =        -3082448
42
 Y    =        9883817
41  feet           Y    =         2978162
06  meter
 Z    =      -17232809
95                 Z    =        -5267514
76
 XDOT =     -19769
630811                 XDOT =       -5977
613043
 YDOT =     -15233
644798  feet/sec       YDOT =       -4710
330157  meter/sec
 ZDOT =       2836
167684                 ZDOT =         835
309124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4364267
08                 X    =        -1330228
61
 Y    =       13343365
43  feet           Y    =         4067057
78  meter
 Z    =      -17300694
13                 Z    =        -5273251
57
 XDOT =     -23585
705925                 XDOT =       -7188
923166
 YDOT =      -4209
485881  feet/sec       YDOT =       -1283
051296  meter/sec
 ZDOT =       2704
627804                 ZDOT =         824
370555


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   19125
47302961  
00016717  00000-0  10270-3 0  9074
2 25544  51
6412 213
4915 0001111 282
2163  77
8864 15
52642556  8610


Satellite: ISS
Catalog Number: 25544
Epoch time:      19125
47302961   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       213
4915  deg
Eccentricity:     
0001111     
Arg of perigee:   282
2163  deg
Mean anomaly:      77
8864  deg
Mean motion:   15
52642556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             861
Checksum:              298


Coasting Arc #9 (Orbit 876)
---------------------------------------

Vector Time (GMT): 2019/126/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4020207
03                 A    =         6783213
59  meter
 Y    =       -2343631
93  meter          E    =           
0005631
 Z    =        4932917
89                 I    =           51
44528
 XDOT =       5525
678354                 Wp   =           48
64334
 YDOT =       4840
101638  meter/sec      RA   =          207
41626  deg
 ZDOT =      -2198
474578                 TA   =           62
89416
                                          MA   =           62
83673
                                          Ha   =            222
798  n
mi
                                          Hp   =            217
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13189655
60                 X    =         4022153
53
 Y    =       -7689081
12  feet           Y    =        -2298664
56  meter
 Z    =       16184113
82                 Z    =         4952451
54
 XDOT =      18128
865992                 XDOT =        5481
823465
 YDOT =      15879
598550  feet/sec       YDOT =        4901
648562  meter/sec
 ZDOT =      -7212
843103                 ZDOT =       -2171
738584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7911167
34                 X    =         2411323
80
 Y    =      -12947123
73  feet           Y    =        -3946283
31  meter
 Z    =       16272674
70                 Z    =         4959911
25
 XDOT =      22572
197361                 XDOT =        6880
005756
 YDOT =       4856
843357  feet/sec       YDOT =        1480
365855  meter/sec
 ZDOT =      -7092
243714                 ZDOT =       -2161
715884


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   19126
50285859  
00016717  00000-0  10270-3 0  9086
2 25544  51
6412 208
3691 0001169 287
9094  72
1930 15
52647323  8778


Satellite: ISS
Catalog Number: 25544
Epoch time:      19126
50285859   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       208
3691  deg
Eccentricity:     
0001169     
Arg of perigee:   287
9094  deg
Mean anomaly:      72
1930  deg
Mean motion:   15
52647323  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             877
Checksum:              328


Coasting Arc #10 (Orbit 891)
---------------------------------------

Vector Time (GMT): 2019/127/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4895885
03                 A    =         6785415
07  meter
 Y    =        1743009
51  meter          E    =           
0007836
 Z    =       -4370826
61                 I    =           51
48251
 XDOT =      -4788
466848                 Wp   =          110
64652
 YDOT =      -4910
418088  meter/sec      RA   =          202
42554  deg
 ZDOT =       3407
764095                 TA   =          194
00194
                                          MA   =          194
02368
                                          Ha   =            222
909  n
mi
                                          Hp   =            217
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16062614
94                 X    =        -4893780
56
 Y    =        5718535
15  feet           Y    =         1688272
41  meter
 Z    =      -14339982
30                 Z    =        -4394604
16
 XDOT =     -15710
193071                 XDOT =       -4749
754588
 YDOT =     -16110
295563  feet/sec       YDOT =       -4963
749891  meter/sec
 ZDOT =      11180
328395                 ZDOT =        3384
596733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11166712
67                 X    =        -3403614
02
 Y    =       12763714
06  feet           Y    =         3890380
05  meter
 Z    =      -14447714
94                 Z    =        -4403663
51
 XDOT =     -20697
905511                 XDOT =       -6308
721600
 YDOT =      -5579
320901  feet/sec       YDOT =       -1700
577011  meter/sec
 ZDOT =      11075
864158                 ZDOT =        3375
923395


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   19127
46832091  
00016717  00000-0  10270-3 0  9099
2 25544  51
6408 203
5681 0001153 292
9007  67
2023 15
52656579  8920


Satellite: ISS
Catalog Number: 25544
Epoch time:      19127
46832091   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       203
5681  deg
Eccentricity:     
0001153     
Arg of perigee:   292
9007  deg
Mean anomaly:      67
2023  deg
Mean motion:   15
52656579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             892
Checksum:              313


Coasting Arc #11 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2019/128/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5279984
10                 A    =         6786873
71  meter
 Y    =        1560710
90  meter          E    =           
0006022
 Z    =       -3974571
16                 I    =           51
50744
 XDOT =      -4420
423492                 Wp   =          104
99844
 YDOT =      -4824
628065  meter/sec      RA   =          198
56671  deg
 ZDOT =       3981
296975                 TA   =          206
59960
                                          MA   =          206
63051
                                          Ha   =            223
037  n
mi
                                          Hp   =            217
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17322782
47                 X    =        -5277737
44
 Y    =        5120442
58  feet           Y    =         1501679
35  meter
 Z    =      -13039931
61                 Z    =        -4000214
13
 XDOT =     -14502
701746                 XDOT =       -4385
483810
 YDOT =     -15828
832235  feet/sec       YDOT =       -4873
865338  meter/sec
 ZDOT =      13061
997950                 ZDOT =        3959
908312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14713617
59                 X    =        -4484710
64
 Y    =      -10332660
36  feet           Y    =        -3149394
88  meter
 Z    =      -13156106
12                 Z    =        -4009981
15
 XDOT =       2596
544664                 XDOT =         791
426814
 YDOT =     -20191
300353  feet/sec       YDOT =       -6154
308348  meter/sec
 ZDOT =      12965
562985                 ZDOT =        3951
903598


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   19128
24069042  
00016717  00000-0  10270-3 0  9106
2 25544  51
6370 199
7243 0000996 306
9156  53
1904 15
52635407  9046


Satellite: ISS
Catalog Number: 25544
Epoch time:      19128
24069042   =   yrday
fracday
Element set:     910
Inclination:       51
6370  deg
RA of node:       199
7243  deg
Eccentricity:     
0000996     
Arg of perigee:   306
9156  deg
Mean anomaly:      53
1904  deg
Mean motion:   15
52635407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             904
Checksum:              306


Coasting Arc #12 (Orbit 919)
---------------------------------------

Vector Time (GMT): 2019/129/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5967495
84                 A    =         6789659
77  meter
 Y    =       -1051108
36  meter          E    =           
0012056
 Z    =        3051984
21                 I    =           51
54709
 XDOT =       3370
732142                 Wp   =           93
29816
 YDOT =       4827
552671  meter/sec      RA   =          193
58679  deg
 ZDOT =      -4912
018786                 TA   =           51
64262
                                          MA   =           51
53435
                                          Ha   =            222
976  n
mi
                                          Hp   =            217
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19578398
42                 X    =         5963981
12
 Y    =       -3448518
24  feet           Y    =         -984395
60  meter
 Z    =       10013071
56                 Z    =         3080963
73
 XDOT =      11058
832487                 XDOT =        3340
358655
 YDOT =      15838
427398  feet/sec       YDOT =        4865
077214  meter/sec
 ZDOT =     -16115
547199                 ZDOT =       -4895
718157

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15040130
44                 X    =         4584231
76
 Y    =       12897853
05  feet           Y    =         3931265
61  meter
 Z    =       10144329
83                 Z    =         3091991
73
 XDOT =      -4221
666263                 XDOT =       -1286
763877
 YDOT =      17581
222006  feet/sec       YDOT =        5358
756467  meter/sec
 ZDOT =     -16042
125408                 ZDOT =       -4889
639824


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   19129
27051420  
00016717  00000-0  10270-3 0  9112
2 25544  51
6356 194
6022 0001100 305
7560  54
3489 15
52624283  9202


Satellite: ISS
Catalog Number: 25544
Epoch time:      19129
27051420   =   yrday
fracday
Element set:     911
Inclination:       51
6356  deg
RA of node:       194
6022  deg
Eccentricity:     
0001100     
Arg of perigee:   305
7560  deg
Mean anomaly:      54
3489  deg
Mean motion:   15
52624283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             920
Checksum:              278


Coasting Arc #13 (Orbit 934)
---------------------------------------

Vector Time (GMT): 2019/130/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6459783
91                 A    =         6791891
73  meter
 Y    =         621127
05  meter          E    =           
0006722
 Z    =       -1994729
58                 I    =           51
58955
 XDOT =      -2176
111369                 Wp   =           32
24504
 YDOT =      -4795
035591  meter/sec      RA   =          188
61353  deg
 ZDOT =       5568
305484                 TA   =          305
73336
                                          MA   =          305
79587
                                          Ha   =            223
024  n
mi
                                          Hp   =            217
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21193516
77                 X    =        -6456560
09
 Y    =        2037818
41  feet           Y    =          548907
44  meter
 Z    =       -6544388
38                 Z    =        -2026101
08
 XDOT =      -7139
472997                 XDOT =       -2149
378070
 YDOT =     -15731
744066  feet/sec       YDOT =       -4819
221444  meter/sec
 ZDOT =      18268
718779                 ZDOT =        5557
799165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15245553
22                 X    =        -4646844
62
 Y    =      -14799025
72  feet           Y    =        -4510743
04  meter
 Z    =       -6686465
53                 Z    =        -2038034
69
 XDOT =       6207
711766                 XDOT =        1892
110546
 YDOT =     -14607
179434  feet/sec       YDOT =       -4452
268292  meter/sec
 ZDOT =      18221
512001                 ZDOT =        5553
916858


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   19130
23597313  
00016717  00000-0  10270-3 0  9127
2 25544  51
6378 189
7998 0001024 311
6130  48
4934 15
52642062  9357


Satellite: ISS
Catalog Number: 25544
Epoch time:      19130
23597313   =   yrday
fracday
Element set:     912
Inclination:       51
6378  deg
RA of node:       189
7998  deg
Eccentricity:     
0001024     
Arg of perigee:   311
6130  deg
Mean anomaly:      48
4934  deg
Mean motion:   15
52642062  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             935
Checksum:              308


Coasting Arc #14 (Orbit 950)
---------------------------------------

Vector Time (GMT): 2019/131/05:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6737281
52                 A    =         6793312
09  meter
 Y    =        -204443
12  meter          E    =           
0012271
 Z    =         798758
93                 I    =           51
62693
 XDOT =        855
966295                 Wp   =          125
08666
 YDOT =       4768
731906  meter/sec      RA   =          183
64611  deg
 ZDOT =      -5941
520428                 TA   =           46
28033
                                          MA   =           46
17877
                                          Ha   =            223
073  n
mi
                                          Hp   =            217
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22103942
01                 X    =         6735187
00
 Y    =        -670745
14  feet           Y    =         -129113
90  meter
 Z    =        2620600
16                 Z    =          831481
10
 XDOT =       2808
288369                 XDOT =         831
438035
 YDOT =      15645
445885  feet/sec       YDOT =        4778
167246  meter/sec
 ZDOT =     -19493
177257                 ZDOT =       -5937
421649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15090226
91                 X    =         4599501
16
 Y    =       16140649
86  feet           Y    =         4919670
08  meter
 Z    =        2768785
00                 Z    =          843925
67
 XDOT =      -8628
616063                 XDOT =       -2630
002176
 YDOT =      11438
578829  feet/sec       YDOT =        3486
478827  meter/sec
 ZDOT =     -19474
971331                 ZDOT =       -5935
971262


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   19131
26579279  
00016717  00000-0  10270-3 0  9133
2 25544  51
6373 184
6769 0001148 320
3880  39
7188 15
52656261  9516


Satellite: ISS
Catalog Number: 25544
Epoch time:      19131
26579279   =   yrday
fracday
Element set:     913
Inclination:       51
6373  deg
RA of node:       184
6769  deg
Eccentricity:     
0001148     
Arg of perigee:   320
3880  deg
Mean anomaly:      39
7188  deg
Mean motion:   15
52656261  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             951
Checksum:              333


Coasting Arc #15 (Orbit 952)
---------------------------------------

Vector Time (GMT): 2019/131/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -313217
30                 A    =         6781685
28  meter
 Y    =        4207745
89  meter          E    =           
0014024
 Z    =       -5321356
79                 I    =           51
59607
 XDOT =      -7641
515626                 Wp   =           87
13248
 YDOT =       -459
808875  meter/sec      RA   =          182
92681  deg
 ZDOT =         87
083077                 TA   =          183
69402
                                          MA   =          183
70438
                                          Ha   =            223
049  n
mi
                                          Hp   =            217
282

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1027615
82                 X    =         -334397
98
 Y    =       13804940
59  feet           Y    =         4204125
25  meter
 Z    =      -17458519
66                 Z    =        -5322929
41
 XDOT =     -25070
589325                 XDOT =       -7636
228982
 YDOT =      -1508
559301  feet/sec       YDOT =        -545
232099  meter/sec
 ZDOT =        285
705634                 ZDOT =          49
976179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         109872
01                 X    =           33488
99
 Y    =       13833318
94  feet           Y    =         4216395
61  meter
 Z    =      -17465952
67                 Z    =        -5323622
37
 XDOT =     -24106
180981                 XDOT =       -7347
563963
 YDOT =        336
427318  feet/sec       YDOT =         102
543046  meter/sec
 ZDOT =        117
711683                 ZDOT =          35
878521


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   19131
39451972  
00016717  00000-0  10270-3 0  9147
2 25544  51
6406 184
0391 0001241 316
0144  44
0909 15
52643407  9537


Satellite: ISS
Catalog Number: 25544
Epoch time:      19131
39451972   =   yrday
fracday
Element set:     914
Inclination:       51
6406  deg
RA of node:       184
0391  deg
Eccentricity:     
0001241     
Arg of perigee:   316
0144  deg
Mean anomaly:      44
0909  deg
Mean motion:   15
52643407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             953
Checksum:              288


Coasting Arc #16 (Orbit 968)
---------------------------------------

Vector Time (GMT): 2019/132/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1502951
11                 A    =         6782236
16  meter
 Y    =       -4139063
60  meter          E    =           
0004556
 Z    =        5156566
96                 I    =           51
63174
 XDOT =       7474
594130                 Wp   =           39
25273
 YDOT =        888
733392  meter/sec      RA   =          177
94113  deg
 ZDOT =      -1461
047728                 TA   =           64
83636
                                          MA   =           64
78912
                                          Ha   =            222
961  n
mi
                                          Hp   =            217
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4930941
95                 X    =         1524075
81
 Y    =      -13579604
99  feet           Y    =        -4122138
72  meter
 Z    =       16917870
61                 Z    =         5163918
83
 XDOT =      24522
946621                 XDOT =        7471
197503
 YDOT =       2915
791969  feet/sec       YDOT =         972
300625  meter/sec
 ZDOT =      -4793
463673                 ZDOT =       -1424
747091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3563357
97                 X    =         1086111
51
 Y    =      -13960098
20  feet           Y    =        -4255037
93  meter
 Z    =       16951470
28                 Z    =         5166808
14
 XDOT =      23699
901850                 XDOT =        7223
730084
 YDOT =        411
887414  feet/sec       YDOT =         125
543284  meter/sec
 ZDOT =      -4629
127691                 ZDOT =       -1410
958120


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   19132
42433810  
00016717  00000-0  10270-3 0  9154
2 25544  51
6406 178
9167 0001284 319
6086  40
4971 15
52677419  9697


Satellite: ISS
Catalog Number: 25544
Epoch time:      19132
42433810   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:       178
9167  deg
Eccentricity:     
0001284     
Arg of perigee:   319
6086  deg
Mean anomaly:      40
4971  deg
Mean motion:   15
52677419  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             969
Checksum:              325


Coasting Arc #17 (Orbit 983)
---------------------------------------

Vector Time (GMT): 2019/133/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2624676
69                 A    =         6784024
01  meter
 Y    =        4097356
86  meter          E    =           
0010152
 Z    =       -4736788
25                 I    =           51
67045
 XDOT =      -7023
433610                 Wp   =          105
22335
 YDOT =      -1323
102220  meter/sec      RA   =          172
96145  deg
 ZDOT =       2749
544765                 TA   =          192
00448
                                          MA   =          192
02870
                                          Ha   =            223
077  n
mi
                                          Hp   =            217
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8611143
99                 X    =        -2647290
66
 Y    =       13442771
86  feet           Y    =         4067879
62  meter
 Z    =      -15540643
87                 Z    =        -4749592
77
 XDOT =     -23042
761189                 XDOT =       -7021
472116
 YDOT =      -4340
886550  feet/sec       YDOT =       -1401
632303  meter/sec
 ZDOT =       9020
816159                 ZDOT =        2715
432156

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7005236
32                 X    =        -2135196
03
 Y    =       14281850
06  feet           Y    =         4353107
90  meter
 Z    =      -15598940
70                 Z    =        -4754557
12
 XDOT =     -22394
907397                 XDOT =       -6825
967775
 YDOT =      -1308
896673  feet/sec       YDOT =        -398
951706  meter/sec
 ZDOT =       8866
400607                 ZDOT =        2702
478905


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   19133
38979370  
00016717  00000-0  10270-3 0  9167
2 25544  51
6401 174
1158 0001193 326
2286  33
8790 15
52669173  9845


Satellite: ISS
Catalog Number: 25544
Epoch time:      19133
38979370   =   yrday
fracday
Element set:     916
Inclination:       51
6401  deg
RA of node:       174
1158  deg
Eccentricity:     
0001193     
Arg of perigee:   326
2286  deg
Mean anomaly:      33
8790  deg
Mean motion:   15
52669173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             984
Checksum:              326


Coasting Arc #18 (Orbit 999)
---------------------------------------

Vector Time (GMT): 2019/134/09:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964623
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3650887
34                 A    =         6786556
41  meter
 Y    =       -4040652
55  meter          E    =           
0010352
 Z    =        4043979
00                 I    =           51
71266
 XDOT =       6343
473376                 Wp   =           70
56743
 YDOT =       1806
248357  meter/sec      RA   =          167
98700  deg
 ZDOT =      -3910
573482                 TA   =           60
00703
                                          MA   =           59
90433
                                          Ha   =            223
035  n
mi
                                          Hp   =            217
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11977976
85                 X    =         3676156
19
 Y    =      -13256734
09  feet           Y    =        -3999684
58  meter
 Z    =       13267647
65                 Z    =         4061775
05
 XDOT =      20811
920525                 XDOT =        6341
799459
 YDOT =       5926
011670  feet/sec       YDOT =        1877
176255  meter/sec
 ZDOT =     -12829
965491                 ZDOT =       -3879
763070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10137217
75                 X    =         3089823
97
 Y    =      -14638859
18  feet           Y    =        -4461924
28  meter
 Z    =       13348558
73                 Z    =         4068640
70
 XDOT =      20407
029358                 XDOT =        6220
062548
 YDOT =       2525
373577  feet/sec       YDOT =         769
733866  meter/sec
 ZDOT =     -12690
526038                 ZDOT =       -3868
072336


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   19134
41960954  
00016717  00000-0  10270-3 0  9171
2 25544  51
6409 168
9933 0001393 331
6386  28
4690 15
52671859 10001


Satellite: ISS
Catalog Number: 25544
Epoch time:      19134
41960954   =   yrday
fracday
Element set:     917
Inclination:       51
6409  deg
RA of node:       168
9933  deg
Eccentricity:     
0001393     
Arg of perigee:   331
6386  deg
Mean anomaly:      28
4690  deg
Mean motion:   15
52671859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1000
Checksum:              326
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