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

 
Date: November 26th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


333/00:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 8
000/00:00:00 000 0 0 0 0 221 6

333/10:24:30 000 0 0 0 0 0 0
N/A 0 0 0 0 227 8
000/00:00:00 000 0 0 0 0 221 6

336/14:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 221 0

338/17:51:47 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 220 6

339/18:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 220 5

340/09:34:11 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 220 4

341/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 220 3

342/14:24:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 220 1

342/21:54:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 220 1

Coasting Arc #1 (Orbit 27)
---------------------------------------

Vector Time (GMT): 2019/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3942168
65                 A    =         6794565
12  meter
 Y    =       -3892077
16  meter          E    =           
0007521
 Z    =        3925587
31                 I    =           51
25904
 XDOT =       2105
923879                 Wp   =           63
25405
 YDOT =       6182
171954  meter/sec      RA   =          280
71758  deg
 ZDOT =       4011
931515                 TA   =          344
58512
                                          MA   =          344
60801
                                          Ha   =            227
273  n
mi
                                          Hp   =            222
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12933624
17                 X    =         3966329
20
 Y    =      -12769282
04  feet           Y    =        -3847858
23  meter
 Z    =       12879223
47                 Z    =         3944795
78
 XDOT =       6909
199077                 XDOT =        2017
148297
 YDOT =      20282
716383  feet/sec       YDOT =        6205
225229  meter/sec
 ZDOT =      13162
504970                 ZDOT =        4021
946360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5619882
30                 X    =         1712940
12
 Y    =       17218571
51  feet           Y    =         5248220
60  meter
 Z    =       12967085
76                 Z    =         3952367
74
 XDOT =     -19926
895077                 XDOT =       -6073
717619
 YDOT =      -3449
157571  feet/sec       YDOT =       -1051
303228  meter/sec
 ZDOT =      13207
630115                 ZDOT =        4025
685659


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   19329
55589821  
00016717  00000-0  10270-3 0  9004
2 25544  51
6410 281
2508 0006716 322
2570  37
8108 15
50066407   287


Satellite: ISS
Catalog Number: 25544
Epoch time:      19329
55589821   =   yrday
fracday
Element set:     900
Inclination:       51
6410  deg
RA of node:       281
2508  deg
Eccentricity:     
0006716     
Arg of perigee:   322
2570  deg
Mean anomaly:      37
8108  deg
Mean motion:   15
50066407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              28
Checksum:              295


Coasting Arc #2 (Orbit 42)
---------------------------------------

Vector Time (GMT): 2019/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3743917
68                 A    =         6793816
49  meter
 Y    =        3859745
46  meter          E    =           
0009103
 Z    =       -4161174
16                 I    =           51
25224
 XDOT =      -2352
410628                 Wp   =           23
36575
 YDOT =      -6274
416472  meter/sec      RA   =          275
73575  deg
 ZDOT =      -3697
975850                 TA   =          208
32831
                                          MA   =          208
37784
                                          Ha   =            227
638  n
mi
                                          Hp   =            221
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12283194
49                 X    =        -3766587
08
 Y    =       12663206
88  feet           Y    =         3817751
97  meter
 Z    =      -13652146
21                 Z    =        -4179415
84
 XDOT =      -7717
882639                 XDOT =       -2264
110309
 YDOT =     -20585
355878  feet/sec       YDOT =       -6300
228720  meter/sec
 ZDOT =     -12132
466700                 ZDOT =       -3709
189373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6104645
61                 X    =        -1860695
98
 Y    =      -16482761
19  feet           Y    =        -5023945
61  meter
 Z    =      -13735598
16                 Z    =        -4186610
32
 XDOT =      20656
723814                 XDOT =        6296
169418
 YDOT =       2516
675307  feet/sec       YDOT =         767
082634  meter/sec
 ZDOT =     -12183
057275                 ZDOT =       -3713
395857


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   19330
52297621  
00016717  00000-0  10270-3 0  9018
2 25544  51
6419 276
4591 0006840 327
1971  32
8754 15
50055045   436


Satellite: ISS
Catalog Number: 25544
Epoch time:      19330
52297621   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       276
4591  deg
Eccentricity:     
0006840     
Arg of perigee:   327
1971  deg
Mean anomaly:      32
8754  deg
Mean motion:   15
50055045  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              43
Checksum:              298


Coasting Arc #3 (Orbit 58)
---------------------------------------

Vector Time (GMT): 2019/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3557917
74                 A    =         6792973
99  meter
 Y    =       -3785576
14  meter          E    =           
0006137
 Z    =        4370237
02                 I    =           51
24768
 XDOT =       2624
396986                 Wp   =           62
94832
 YDOT =       6362
419211  meter/sec      RA   =          270
75426  deg
 ZDOT =       3373
723454                 TA   =          352
68630
                                          MA   =          352
69525
                                          Ha   =            227
582  n
mi
                                          Hp   =            221
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11672958
46                 X    =         3578756
12
 Y    =      -12419869
24  feet           Y    =        -3745672
99  meter
 Z    =       14338047
96                 Z    =         4387570
57
 XDOT =       8610
226332                 XDOT =        2536
667514
 YDOT =      20874
078776  feet/sec       YDOT =        6391
276153  meter/sec
 ZDOT =      11068
646504                 ZDOT =        3386
259702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6423990
94                 X    =         1958032
44
 Y    =       15715055
23  feet           Y    =         4789948
83  meter
 Z    =       14417354
47                 Z    =         4394409
64
 XDOT =     -21384
184865                 XDOT =       -6517
899547
 YDOT =      -1467
949171  feet/sec       YDOT =        -447
430907  meter/sec
 ZDOT =      11125
271437                 ZDOT =        3390
982734


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   19331
55452076  
00016717  00000-0  10270-3 0  9020
2 25544  51
6421 271
3490 0006839 330
1554  29
9206 15
50076795   591


Satellite: ISS
Catalog Number: 25544
Epoch time:      19331
55452076   =   yrday
fracday
Element set:     902
Inclination:       51
6421  deg
RA of node:       271
3490  deg
Eccentricity:     
0006839     
Arg of perigee:   330
1554  deg
Mean anomaly:      29
9206  deg
Mean motion:   15
50076795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              59
Checksum:              305


Coasting Arc #4 (Orbit 73)
---------------------------------------

Vector Time (GMT): 2019/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3402638
66                 A    =         6792305
23  meter
 Y    =        3712787
01  meter          E    =           
0011726
 Z    =       -4568401
01                 I    =           51
24560
 XDOT =      -2909
361521                 Wp   =           33
90348
 YDOT =      -6397
926285  meter/sec      RA   =          265
77200  deg
 ZDOT =      -3026
934594                 TA   =          205
58849
                                          MA   =          205
64657
                                          Ha   =            227
942  n
mi
                                          Hp   =            221
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11163512
66                 X    =        -3421712
15
 Y    =       12181059
73  feet           Y    =         3674630
24  meter
 Z    =      -14988192
28                 Z    =        -4584975
85
 XDOT =      -9545
149348                 XDOT =       -2822
898432
 YDOT =     -20990
571800  feet/sec       YDOT =       -6429
976985  meter/sec
 ZDOT =      -9930
887777                 ZDOT =       -3040
858212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6682108
41                 X    =        -2036706
64
 Y    =      -15035705
35  feet           Y    =        -4582882
99  meter
 Z    =      -15064034
35                 Z    =        -4591517
67
 XDOT =      21934
384161                 XDOT =        6685
600292
 YDOT =        283
573287  feet/sec       YDOT =          86
433138  meter/sec
 ZDOT =      -9993
849986                 ZDOT =       -3046
125476


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   19332
52159477  
00016717  00000-0  10270-3 0  9038
2 25544  51
6417 266
5582 0006919 335
4642  24
6179 15
50061431   748


Satellite: ISS
Catalog Number: 25544
Epoch time:      19332
52159477   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:       266
5582  deg
Eccentricity:     
0006919     
Arg of perigee:   335
4642  deg
Mean anomaly:      24
6179  deg
Mean motion:   15
50061431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              74
Checksum:              310


Coasting Arc #5 (Orbit 81)
---------------------------------------

Vector Time (GMT): 2019/333/00:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4190530
88                 A    =         6789250
59  meter
 Y    =         770968
85  meter          E    =           
0013539
 Z    =       -5296378
56                 I    =           51
23846
 XDOT =      -1094
802907                 Wp   =           62
20761
 YDOT =      -7570
720418  meter/sec      RA   =          263
15530  deg
 ZDOT =       -230
076303                 TA   =          205
54929
                                          MA   =          205
61627
                                          Ha   =            227
755  n
mi
                                          Hp   =            221
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13748460
90                 X    =        -4173113
45
 Y    =        2529425
35  feet           Y    =          724205
45  meter
 Z    =      -17376570
08                 Z    =        -5316692
44
 XDOT =      -3591
873054                 XDOT =       -1008
945943
 YDOT =     -24838
321580  feet/sec       YDOT =       -7582
483190  meter/sec
 ZDOT =       -754
843514                 ZDOT =        -235
186966

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1273699
99                 X    =         -388223
76
 Y    =       13804605
95  feet           Y    =         4207643
89  meter
 Z    =      -17469227
24                 Z    =        -5324620
46
 XDOT =     -23871
029667                 XDOT =       -7275
889843
 YDOT =      -3210
170081  feet/sec       YDOT =        -978
459841  meter/sec
 ZDOT =       -777
552420                 ZDOT =        -236
997978


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   19333
03736567  
00016717  00000-0  10270-3 0  9047
2 25544  51
6433 264
0008 0006494 334
1913  25
8912 15
50058777   823


Satellite: ISS
Catalog Number: 25544
Epoch time:      19333
03736567   =   yrday
fracday
Element set:     904
Inclination:       51
6433  deg
RA of node:       264
0008  deg
Eccentricity:     
0006494     
Arg of perigee:   334
1913  deg
Mean anomaly:      25
8912  deg
Mean motion:   15
50058777  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              82
Checksum:              304


Coasting Arc #6 (Orbit 88)
---------------------------------------

Vector Time (GMT): 2019/333/10:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2729972
98                 A    =         6793465
16  meter
 Y    =       -4548489
87  meter          E    =           
0007709
 Z    =        4235525
44                 I    =           51
25231
 XDOT =       3789
964469                 Wp   =           63
44413
 YDOT =       5615
843995  meter/sec      RA   =          261
12412  deg
 ZDOT =       3586
316178                 TA   =          349
68794
                                          MA   =          349
70374
                                          Ha   =            227
823  n
mi
                                          Hp   =            221
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8956604
27                 X    =         2760058
58
 Y    =      -14922867
02  feet           Y    =        -4517793
71  meter
 Z    =       13896080
85                 Z    =         4248859
25
 XDOT =      12434
266629                 XDOT =        3709
464278
 YDOT =      18424
685022  feet/sec       YDOT =        5657
775483  meter/sec
 ZDOT =      11766
129194                 ZDOT =        3604
531805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3769732
82                 X    =         1149014
56
 Y    =       16941048
97  feet           Y    =         5163631
73  meter
 Z    =       13957211
66                 Z    =         4254158
11
 XDOT =     -20388
249788                 XDOT =       -6214
338535
 YDOT =      -5229
562876  feet/sec       YDOT =       -1593
970765  meter/sec
 ZDOT =      11848
734750                 ZDOT =        3611
494352


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   19333
48866445  
00016717  00000-0  10270-3 0  9056
2 25544  51
6410 261
7674 0006815 336
9411  23
1433 15
50083660   896


Satellite: ISS
Catalog Number: 25544
Epoch time:      19333
48866445   =   yrday
fracday
Element set:     905
Inclination:       51
6410  deg
RA of node:       261
7674  deg
Eccentricity:     
0006815     
Arg of perigee:   336
9411  deg
Mean anomaly:      23
1433  deg
Mean motion:   15
50083660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              89
Checksum:              306


Coasting Arc #7 (Orbit 103)
---------------------------------------

Vector Time (GMT): 2019/334/10:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2579836
41                 A    =         6792763
92  meter
 Y    =        4448449
40  meter          E    =           
0011827
 Z    =       -4449442
73                 I    =           51
25650
 XDOT =      -4066
724521                 Wp   =           33
57010
 YDOT =      -5610
602498  meter/sec      RA   =          256
14191  deg
 ZDOT =      -3245
906520                 TA   =          203
45572
                                          MA   =          203
50971
                                          Ha   =            228
163  n
mi
                                          Hp   =            221
282

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8464030
23                 X    =        -2607775
48
 Y    =       14594650
26  feet           Y    =         4419444
17  meter
 Z    =      -14597909
23                 Z    =        -4462042
01
 XDOT =     -13342
272052                 XDOT =       -3987
915977
 YDOT =     -18407
488512  feet/sec       YDOT =       -5655
638442  meter/sec
 ZDOT =     -10649
299606                 ZDOT =       -3265
470539

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4187877
72                 X    =        -1276465
13
 Y    =      -16291572
75  feet           Y    =        -4965671
37  meter
 Z    =      -14655678
60                 Z    =        -4467050
84
 XDOT =      21161
522598                 XDOT =        6450
032088
 YDOT =       4236
291511  feet/sec       YDOT =        1291
221653  meter/sec
 ZDOT =     -10738
074342                 ZDOT =       -3272
965059


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   19334
45573389  
00016717  00000-0  10270-3 0  9067
2 25544  51
6414 256
9759 0006965 341
7469  18
3431 15
50067174  1047


Satellite: ISS
Catalog Number: 25544
Epoch time:      19334
45573389   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       256
9759  deg
Eccentricity:     
0006965     
Arg of perigee:   341
7469  deg
Mean anomaly:      18
3431  deg
Mean motion:   15
50067174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             104
Checksum:              328


Coasting Arc #8 (Orbit 119)
---------------------------------------

Vector Time (GMT): 2019/335/10:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2455118
34                 A    =         6791949
48  meter
 Y    =       -4311445
64  meter          E    =           
0006433
 Z    =        4631963
06                 I    =           51
26294
 XDOT =       4364
565485                 Wp   =           60
35254
 YDOT =       5596
866019  meter/sec      RA   =          251
16069  deg
 ZDOT =       2896
278229                 TA   =             
67648
                                          MA   =             
67561
                                          Ha   =            228
109  n
mi
                                          Hp   =            221
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8054850
18                 X    =         2480648
13
 Y    =      -14145162
87  feet           Y    =        -4283848
53  meter
 Z    =       15196729
21                 Z    =         4643950
69
 XDOT =      14319
440568                 XDOT =        4287
586759
 YDOT =      18362
421321  feet/sec       YDOT =        5645
242945  meter/sec
 ZDOT =       9502
225161                 ZDOT =        2917
293362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4439449
82                 X    =         1353144
31
 Y    =       15607176
07  feet           Y    =         4757067
26  meter
 Z    =       15251693
78                 Z    =         4648716
27
 XDOT =     -21937
402534                 XDOT =       -6686
520292
 YDOT =      -3138
685650  feet/sec       YDOT =        -956
671386  meter/sec
 ZDOT =       9597
640118                 ZDOT =        2925
360708


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   19335
48726909  
00016717  00000-0  10270-3 0  9070
2 25544  51
6412 251
8657 0006964 344
6956  15
3983 15
50093575  1209


Satellite: ISS
Catalog Number: 25544
Epoch time:      19335
48726909   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       251
8657  deg
Eccentricity:     
0006964     
Arg of perigee:   344
6956  deg
Mean anomaly:      15
3983  deg
Mean motion:   15
50093575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             120
Checksum:              333


Coasting Arc #9 (Orbit 134)
---------------------------------------

Vector Time (GMT): 2019/336/10:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2360797
30                 A    =         6791368
26  meter
 Y    =        4193315
67  meter          E    =           
0014225
 Z    =       -4804878
88                 I    =           51
27215
 XDOT =      -4653
462342                 Wp   =           42
59997
 YDOT =      -5522
360945  meter/sec      RA   =          246
17928  deg
 ZDOT =      -2527
218340                 TA   =          202
31912
                                          MA   =          202
38108
                                          Ha   =            228
432  n
mi
                                          Hp   =            220
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7745397
97                 X    =        -2384173
24
 Y    =       13757597
34  feet           Y    =         4166785
31  meter
 Z    =      -15764038
32                 Z    =        -4816403
16
 XDOT =     -15267
264903                 XDOT =       -4579
087989
 YDOT =     -18117
982102  feet/sec       YDOT =       -5573
983162  meter/sec
 ZDOT =      -8291
398753                 ZDOT =       -2549
643036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4644264
73                 X    =        -1415571
89
 Y    =      -15034122
38  feet           Y    =        -4582400
50  meter
 Z    =      -15816875
42                 Z    =        -4820983
63
 XDOT =      22509
258549                 XDOT =        6860
822006
 YDOT =       1896
969990  feet/sec       YDOT =         578
196453  meter/sec
 ZDOT =      -8393
269776                 ZDOT =       -2558
268628


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   19336
45433472  
00016717  00000-0  10270-3 0  9089
2 25544  51
6407 247
0746 0007060 349
7022  10
3983 15
50072664  1354


Satellite: ISS
Catalog Number: 25544
Epoch time:      19336
45433472   =   yrday
fracday
Element set:     908
Inclination:       51
6407  deg
RA of node:       247
0746  deg
Eccentricity:     
0007060     
Arg of perigee:   349
7022  deg
Mean anomaly:      10
3983  deg
Mean motion:   15
50072664  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             135
Checksum:              297


Coasting Arc #10 (Orbit 137)
---------------------------------------

Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4728629
20                 A    =         6791516
08  meter
 Y    =        1226799
08  meter          E    =           
0011853
 Z    =        4717988
01                 I    =           51
27720
 XDOT =        876
243823                 Wp   =           27
16802
 YDOT =       7110
385329  meter/sec      RA   =          245
29158  deg
 ZDOT =      -2714
033416                 TA   =           89
90565
                                          MA   =           89
76982
                                          Ha   =            228
276  n
mi
                                          Hp   =            220
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15513875
33                 X    =         4691641
92
 Y    =        4024931
38  feet           Y    =         1279470
72  meter
 Z    =       15478963
28                 Z    =         4740868
25
 XDOT =       2874
815693                 XDOT =         809
851594
 YDOT =      23328
035857  feet/sec       YDOT =        7119
813127  meter/sec
 ZDOT =      -8904
309108                 ZDOT =       -2709
937560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         863928
49                 X    =          263325
40
 Y    =       15902701
33  feet           Y    =         4847143
37  meter
 Z    =       15583209
64                 Z    =         4749762
30
 XDOT =     -20162
260270                 XDOT =       -6145
456930
 YDOT =       9844
667848  feet/sec       YDOT =        3000
654760  meter/sec
 ZDOT =      -8886
119274                 ZDOT =       -2708
489155


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   19336
64774505  
00016717  00000-0  10270-3 0  9096
2 25544  51
6424 246
1177 0007151 348
4769  11
6216 15
50110499  1381


Satellite: ISS
Catalog Number: 25544
Epoch time:      19336
64774505   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       246
1177  deg
Eccentricity:     
0007151     
Arg of perigee:   348
4769  deg
Mean anomaly:      11
6216  deg
Mean motion:   15
50110499  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             138
Checksum:              311


Coasting Arc #11 (Orbit 152)
---------------------------------------

Vector Time (GMT): 2019/337/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4894906
74                 A    =         6792253
38  meter
 Y    =       -1216991
65  meter          E    =           
0009127
 Z    =       -4554478
97                 I    =           51
29422
 XDOT =      -1121
810206                 Wp   =           67
06410
 YDOT =      -6926
045482  meter/sec      RA   =          240
31117  deg
 ZDOT =       3064
766614                 TA   =          233
75386
                                          MA   =          233
83824
                                          Ha   =            228
413  n
mi
                                          Hp   =            220
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16059405
33                 X    =        -4858811
00
 Y    =       -3992754
77  feet           Y    =        -1271527
79  meter
 Z    =      -14942516
31                 Z    =        -4578169
09
 XDOT =      -3680
479680                 XDOT =       -1059
164749
 YDOT =     -22723
246331  feet/sec       YDOT =       -6938
240315  meter/sec
 ZDOT =      10055
008576                 ZDOT =        3059
468895

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1344255
00                 X    =         -409728
92
 Y    =      -16395174
72  feet           Y    =        -4997249
26  meter
 Z    =      -15050468
70                 Z    =        -4587382
86
 XDOT =      19118
667482                 XDOT =        5827
369848
 YDOT =     -10750
953133  feet/sec       YDOT =       -3276
890515  meter/sec
 ZDOT =      10031
305887                 ZDOT =        3057
542034


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   19337
61480827  
00016717  00000-0  10270-3 0  9107
2 25544  51
6423 241
3262 0007111 351
7919   8
3114 15
50079165  1533


Satellite: ISS
Catalog Number: 25544
Epoch time:      19337
61480827   =   yrday
fracday
Element set:     910
Inclination:       51
6423  deg
RA of node:       241
3262  deg
Eccentricity:     
0007111     
Arg of perigee:   351
7919  deg
Mean anomaly:       8
3114  deg
Mean motion:   15
50079165  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             153
Checksum:              284


Coasting Arc #12 (Orbit 168)
---------------------------------------

Vector Time (GMT): 2019/338/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5076954
62                 A    =         6792938
49  meter
 Y    =        1229383
16  meter          E    =           
0013282
 Z    =        4341462
81                 I    =           51
31499
 XDOT =       1315
116585                 Wp   =           39
10245
 YDOT =       6724
661221  meter/sec      RA   =          235
33199  deg
 ZDOT =      -3426
273242                 TA   =           85
92948
                                          MA   =           85
77767
                                          Ha   =            228
512  n
mi
                                          Hp   =            220
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16656675
26                 X    =         5041741
46
 Y    =        4033409
31  feet           Y    =         1285960
08  meter
 Z    =       14243644
38                 Z    =         4366039
42
 XDOT =       4314
686960                 XDOT =        1256
464732
 YDOT =      22062
536814  feet/sec       YDOT =        6739
040062  meter/sec
 ZDOT =     -11241
053945                 ZDOT =       -3420
026888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1791000
21                 X    =          545896
87
 Y    =       16949992
05  feet           Y    =         5166357
58  meter
 Z    =       14355650
96                 Z    =         4375602
41
 XDOT =     -18049
840171                 XDOT =       -5501
591284
 YDOT =      11447
739687  feet/sec       YDOT =        3489
271056  meter/sec
 ZDOT =     -11212
993640                 ZDOT =       -3417
720461


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   19338
64633703  
00016717  00000-0  10270-3 0  9115
2 25544  51
6428 236
2150 0007297 354
8608   5
2467 15
50117549  1694


Satellite: ISS
Catalog Number: 25544
Epoch time:      19338
64633703   =   yrday
fracday
Element set:     911
Inclination:       51
6428  deg
RA of node:       236
2150  deg
Eccentricity:     
0007297     
Arg of perigee:   354
8608  deg
Mean anomaly:       5
2467  deg
Mean motion:   15
50117549  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             169
Checksum:              313


Coasting Arc #13 (Orbit 170)
---------------------------------------

Vector Time (GMT): 2019/338/17:51:47
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3451097
11                 A    =         6800811
89  meter
 Y    =        5819401
70  meter          E    =           
0006636
 Z    =        -688553
29                 I    =           51
34035
 XDOT =      -4440
003622                 Wp   =           98
74602
 YDOT =       1937
566054  meter/sec      RA   =          234
66071  deg
 ZDOT =      -5928
301626                 TA   =           88
70390
                                          MA   =           88
62787
                                          Ha   =            228
606  n
mi
                                          Hp   =            220
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11322497
09                 X    =         3389111
00
 Y    =       19092525
28  feet           Y    =         5857647
77  meter
 Z    =       -2259033
09                 Z    =         -671939
25
 XDOT =     -14566
941016                 XDOT =       -4432
543519
 YDOT =       6356
844008  feet/sec       YDOT =        1887
956884  meter/sec
 ZDOT =     -19449
808484                 ZDOT =       -5949
851368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4240692
20                 X    =         1292562
98
 Y    =       21796214
90  feet           Y    =         6643486
30  meter
 Z    =       -2183629
60                 Z    =         -665570
30
 XDOT =     -14143
179163                 XDOT =       -4310
841009
 YDOT =        810
353244  feet/sec       YDOT =         246
995669  meter/sec
 ZDOT =     -19548
212162                 ZDOT =       -5958
295067


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   19338
77527915  
00016717  00000-0  10270-3 0  9127
2 25544  51
6393 235
5718 0007095 357
5190   2
5924 15
50120265  1719


Satellite: ISS
Catalog Number: 25544
Epoch time:      19338
77527915   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:       235
5718  deg
Eccentricity:     
0007095     
Arg of perigee:   357
5190  deg
Mean anomaly:       2
5924  deg
Mean motion:   15
50120265  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             171
Checksum:              310


Coasting Arc #14 (Orbit 186)
---------------------------------------

Vector Time (GMT): 2019/339/17:51:47
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3676568
18                 A    =         6800714
37  meter
 Y    =       -5613362
55  meter          E    =           
0018293
 Z    =        1035800
39                 I    =           51
35926
 XDOT =       4553
387111                 Wp   =           38
90607
 YDOT =      -1890
724233  meter/sec      RA   =          229
68785  deg
 ZDOT =       5873
139294                 TA   =          332
35698
                                          MA   =          332
45412
                                          Ha   =            228
658  n
mi
                                          Hp   =            220
541

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12062231
56                 X    =        -3618556
06
 Y    =      -18416543
80  feet           Y    =        -5654152
23  meter
 Z    =        3398295
24                 Z    =         1018081
44
 XDOT =      14938
934092                 XDOT =        4545
662653
 YDOT =      -6203
163495  feet/sec       YDOT =       -1839
848569  meter/sec
 ZDOT =      19268
829704                 ZDOT =        5895
239246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5539752
42                 X    =        -1688516
54
 Y    =      -21319430
84  feet           Y    =        -6498162
52  meter
 Z    =        3317821
29                 Z    =         1011271
93
 XDOT =      14460
562144                 XDOT =        4407
579341
 YDOT =       -720
830940  feet/sec       YDOT =        -219
709271  meter/sec
 ZDOT =      19369
744532                 ZDOT =        5903
898133


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   19339
80680907  
00016717  00000-0  10270-3 0  9134
2 25544  51
6388 230
4607 0006732   1
9281 358
1894 15
50074785  1870


Satellite: ISS
Catalog Number: 25544
Epoch time:      19339
80680907   =   yrday
fracday
Element set:     913
Inclination:       51
6388  deg
RA of node:       230
4607  deg
Eccentricity:     
0006732     
Arg of perigee:     1
9281  deg
Mean anomaly:     358
1894  deg
Mean motion:   15
50074785  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             187
Checksum:              328


Coasting Arc #15 (Orbit 186)
---------------------------------------

Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -312111
28                 A    =         6792749
33  meter
 Y    =        5127267
80  meter          E    =           
0013380
 Z    =       -4458090
18                 I    =           51
33474
 XDOT =      -6145
815128                 Wp   =           42
22149
 YDOT =      -3198
617570  meter/sec      RA   =          229
50088  deg
 ZDOT =      -3244
463478                 TA   =          194
86104
                                          MA   =          194
90040
                                          Ha   =            228
686  n
mi
                                          Hp   =            220
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1023987
13                 X    =         -347767
59
 Y    =       16821744
74  feet           Y    =         5123578
44  meter
 Z    =      -14626280
13                 Z    =        -4459692
62
 XDOT =     -20163
435458                 XDOT =       -6093
830558
 YDOT =     -10494
152132  feet/sec       YDOT =       -3267
053568  meter/sec
 ZDOT =     -10644
565218                 ZDOT =       -3274
191705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2129242
39                 X    =         -648993
08
 Y    =       16711162
38  feet           Y    =         5093562
29  meter
 Z    =      -14633902
24                 Z    =        -4460413
40
 XDOT =     -18067
910948                 XDOT =       -5507
099257
 YDOT =     -11753
601192  feet/sec       YDOT =       -3582
497643  meter/sec
 ZDOT =     -10779
962589                 ZDOT =       -3285
732597


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   19339
80680929  
00016717  00000-0  10270-3 0  9149
2 25544  51
6399 230
4612 0006722   2
3585 357
7596 15
50081936  1879


Satellite: ISS
Catalog Number: 25544
Epoch time:      19339
80680929   =   yrday
fracday
Element set:     914
Inclination:       51
6399  deg
RA of node:       230
4612  deg
Eccentricity:     
0006722     
Arg of perigee:     2
3585  deg
Mean anomaly:     357
7596  deg
Mean motion:   15
50081936  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             187
Checksum:              332


Coasting Arc #16 (Orbit 196)
---------------------------------------

Vector Time (GMT): 2019/340/09:34:11
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         883502
14                 A    =         6791161
28  meter
 Y    =       -4681186
21  meter          E    =           
0007415
 Z    =        4832966
87                 I    =           51
34446
 XDOT =       6241
588992                 Wp   =           61
96691
 YDOT =       3713
462480  meter/sec      RA   =          226
44657  deg
 ZDOT =       2456
362079                 TA   =            3
81409
                                          MA   =            3
80844
                                          Ha   =            228
712  n
mi
                                          Hp   =            220
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2898629
08                 X    =          912306
77
 Y    =      -15358222
47  feet           Y    =        -4671145
48  meter
 Z    =       15856190
53                 Z    =         4837328
33
 XDOT =      20477
654173                 XDOT =        6187
668324
 YDOT =      12183
275853  feet/sec       YDOT =        3782
958710  meter/sec
 ZDOT =       8058
930707                 ZDOT =        2486
550926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7143495
55                 X    =         2177337
44
 Y    =       13878303
62  feet           Y    =         4230106
94  meter
 Z    =       15876365
65                 Z    =         4839116
25
 XDOT =     -22605
592906                 XDOT =       -6890
184718
 YDOT =       2261
181951  feet/sec       YDOT =         689
208259  meter/sec
 ZDOT =       8196
409006                 ZDOT =        2498
265465


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   19340
45151328  
00016717  00000-0  10270-3 0  9159
2 25544  51
6411 227
2712 0007079   2
8581 357
2608 15
50100334  1970


Satellite: ISS
Catalog Number: 25544
Epoch time:      19340
45151328   =   yrday
fracday
Element set:     915
Inclination:       51
6411  deg
RA of node:       227
2712  deg
Eccentricity:     
0007079     
Arg of perigee:     2
8581  deg
Mean anomaly:     357
2608  deg
Mean motion:   15
50100334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             197
Checksum:              283


Coasting Arc #17 (Orbit 211)
---------------------------------------

Vector Time (GMT): 2019/341/09:34:11
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -869499
17                 A    =         6790624
99  meter
 Y    =        4546616
43  meter          E    =           
0016670
 Z    =       -4983046
02                 I    =           51
36736
 XDOT =      -6472
336443                 Wp   =           51
23254
 YDOT =      -3512
479720  meter/sec      RA   =          221
47084  deg
 ZDOT =      -2069
956497                 TA   =          198
46924
                                          MA   =          198
52983
                                          Ha   =            228
945  n
mi
                                          Hp   =            220
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2852687
55                 X    =         -896070
95
 Y    =       14916720
58  feet           Y    =         4536744
82  meter
 Z    =      -16348576
19                 Z    =        -4987334
03
 XDOT =     -21234
699617                 XDOT =       -6422
523005
 YDOT =     -11523
883597  feet/sec       YDOT =       -3584
579306  meter/sec
 ZDOT =      -6791
195856                 ZDOT =       -2101
276319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7144709
64                 X    =        -2177707
50
 Y    =      -13377249
65  feet           Y    =        -4077385
69  meter
 Z    =      -16368403
67                 Z    =        -4989089
44
 XDOT =      22779
007023                 XDOT =        6943
041341
 YDOT =      -3659
714025  feet/sec       YDOT =       -1115
480835  meter/sec
 ZDOT =      -6933
863535                 ZDOT =       -2113
441606


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   19341
41857082  
00016717  00000-0  10270-3 0  9167
2 25544  51
6420 222
4798 0007215   7
0775 353
0476 15
50091527  2123


Satellite: ISS
Catalog Number: 25544
Epoch time:      19341
41857082   =   yrday
fracday
Element set:     916
Inclination:       51
6420  deg
RA of node:       222
4798  deg
Eccentricity:     
0007215     
Arg of perigee:     7
0775  deg
Mean anomaly:     353
0476  deg
Mean motion:   15
50091527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             212
Checksum:              294


Coasting Arc #18 (Orbit 212)
---------------------------------------

Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938320
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1882078
40                 A    =         6795727
22  meter
 Y    =        5460332
56  meter          E    =           
0009751
 Z    =       -3593645
48                 I    =           51
38684
 XDOT =      -6209
961663                 Wp   =           38
04713
 YDOT =       -759
117347  meter/sec      RA   =          221
18410  deg
 ZDOT =      -4404
632648                 TA   =          184
49319
                                          MA   =          184
50195
                                          Ha   =            228
917  n
mi
                                          Hp   =            220
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6174797
89                 X    =         1838335
65
 Y    =       17914476
89  feet           Y    =         5481134
94  meter
 Z    =      -11790175
46                 Z    =        -3584608
83
 XDOT =     -20373
889969                 XDOT =       -6179
615916
 YDOT =      -2490
542477  feet/sec       YDOT =        -828
391574  meter/sec
 ZDOT =     -14450
894516                 ZDOT =       -4434
725053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18643180
17                 X    =        -5682441
31
 Y    =       -3528638
86  feet           Y    =        -1075529
12  meter
 Z    =      -11749271
89                 Z    =        -3581178
07
 XDOT =      12027
873417                 XDOT =        3666
095817
 YDOT =     -14961
895158  feet/sec       YDOT =       -4560
385644  meter/sec
 ZDOT =     -14588
125244                 ZDOT =       -4446
460574


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   19341
48304066  
00016717  00000-0  10270-3 0  9174
2 25544  51
6431 222
1613 0007153   5
9259 354
1975 15
50078915  2136


Satellite: ISS
Catalog Number: 25544
Epoch time:      19341
48304066   =   yrday
fracday
Element set:     917
Inclination:       51
6431  deg
RA of node:       222
1613  deg
Eccentricity:     
0007153     
Arg of perigee:     5
9259  deg
Mean anomaly:     354
1975  deg
Mean motion:   15
50078915  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             213
Checksum:              294


Coasting Arc #19 (Orbit 228)
---------------------------------------

Vector Time (GMT): 2019/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938320
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1955184
04                 A    =         6794938
70  meter
 Y    =       -5236950
83  meter          E    =           
0013789
 Z    =        3847473
28                 I    =           51
41035
 XDOT =       6434
579070                 Wp   =           66
30802
 YDOT =        632
383614  meter/sec      RA   =          216
21237  deg
 ZDOT =       4124
332492                 TA   =          340
19042
                                          MA   =          340
24392
                                          Ha   =            229
103  n
mi
                                          Hp   =            220
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6414645
79                 X    =        -1915166
79
 Y    =      -17181597
21  feet           Y    =        -5258591
63  meter
 Z    =       12622943
82                 Z    =         3838072
36
 XDOT =      21110
823721                 XDOT =        6406
995316
 YDOT =       2074
749390  feet/sec       YDOT =         704
185071  meter/sec
 ZDOT =      13531
274581                 ZDOT =        4155
522802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18178872
13                 X    =         5540920
22
 Y    =        2637599
97  feet           Y    =          803940
47  meter
 Z    =       12580355
67                 Z    =         3834492
41
 XDOT =     -11806
524294                 XDOT =       -3598
628605
 YDOT =      16056
221726  feet/sec       YDOT =        4893
936382  meter/sec
 ZDOT =      13673
537068                 ZDOT =        4167
694098


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   19342
51456541  
00016717  00000-0  10270-3 0  9186
2 25544  51
6434 217
0500 0007286  10
7364 349
3941 15
50069391  2299


Satellite: ISS
Catalog Number: 25544
Epoch time:      19342
51456541   =   yrday
fracday
Element set:     918
Inclination:       51
6434  deg
RA of node:       217
0500  deg
Eccentricity:     
0007286     
Arg of perigee:    10
7364  deg
Mean anomaly:     349
3941  deg
Mean motion:   15
50069391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             229
Checksum:              299


Coasting Arc #20 (Orbit 230)
---------------------------------------

Vector Time (GMT): 2019/342/14:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 952754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4873717
30                 A    =         6791968
08  meter
 Y    =       -1047419
64  meter          E    =           
0013678
 Z    =        4610760
04                 I    =           51
40248
 XDOT =       4057
011339                 Wp   =           39
41980
 YDOT =       5788
239966  meter/sec      RA   =          215
45725  deg
 ZDOT =      -2958
272603                 TA   =           80
26001
                                          MA   =           80
10556
                                          Ha   =            228
881  n
mi
                                          Hp   =            220
082

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15989886
17                 X    =         4862670
77
 Y    =       -3436416
14  feet           Y    =         -992980
43  meter
 Z    =       15127165
49                 Z    =         4634408
19
 XDOT =      13310
404655                 XDOT =        4006
353895
 YDOT =      18990
288602  feet/sec       YDOT =        5833
325329  meter/sec
 ZDOT =      -9705
618775                 ZDOT =       -2938
687423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9203990
20                 X    =         2805376
21
 Y    =       13397549
25  feet           Y    =         4083573
01  meter
 Z    =       15235116
99                 Z    =         4643663
66
 XDOT =     -11521
473498                 XDOT =       -3511
745122
 YDOT =      18907
064191  feet/sec       YDOT =        5762
873165  meter/sec
 ZDOT =      -9616
596640                 ZDOT =       -2931
138656


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   19342
64350299  
00016717  00000-0  10270-3 0  9194
2 25544  51
6411 216
4093 0007212   9
1249 351
0031 15
50098624  2311


Satellite: ISS
Catalog Number: 25544
Epoch time:      19342
64350299   =   yrday
fracday
Element set:     919
Inclination:       51
6411  deg
RA of node:       216
4093  deg
Eccentricity:     
0007212     
Arg of perigee:     9
1249  deg
Mean anomaly:     351
0031  deg
Mean motion:   15
50098624  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             231
Checksum:              279


Coasting Arc #21 (Orbit 235)
---------------------------------------

Vector Time (GMT): 2019/342/21:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 952754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -284735
47                 A    =         6791339
80  meter
 Y    =       -4798544
67  meter          E    =           
0008487
 Z    =        4789278
29                 I    =           51
41079
 XDOT =       6891
209091                 Wp   =           69
13538
 YDOT =       2161
734938  meter/sec      RA   =          213
94498  deg
 ZDOT =       2574
882289                 TA   =          355
41676
                                          MA   =          355
42452
                                          Ha   =            228
868  n
mi
                                          Hp   =            220
082

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -934171
49                 X    =         -254319
61
 Y    =      -15743256
79  feet           Y    =        -4801559
13  meter
 Z    =       15712855
29                 Z    =         4787968
59
 XDOT =      22608
953710                 XDOT =        6854
016221
 YDOT =       7092
306226  feet/sec       YDOT =        2238
589124  meter/sec
 ZDOT =       8447
776540                 ZDOT =        2608
267596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11884325
93                 X    =        -3622342
54
 Y    =      -10376161
72  feet           Y    =        -3162654
09  meter
 Z    =       15707154
33                 Z    =         4787540
64
 XDOT =      20186
821159                 XDOT =        6152
943089
 YDOT =     -10098
887820  feet/sec       YDOT =       -3078
141008  meter/sec
 ZDOT =       8599
974137                 ZDOT =        2621
272117


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   19342
96585420  
00016717  00000-0  10270-3 0  9207
2 25544  51
6430 214
8112 0006784  11
8053 348
3255 15
50110518  2361


Satellite: ISS
Catalog Number: 25544
Epoch time:      19342
96585420   =   yrday
fracday
Element set:     920
Inclination:       51
6430  deg
RA of node:       214
8112  deg
Eccentricity:     
0006784     
Arg of perigee:    11
8053  deg
Mean anomaly:     348
3255  deg
Mean motion:   15
50110518  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             236
Checksum:              282


Coasting Arc #22 (Orbit 250)
---------------------------------------

Vector Time (GMT): 2019/343/21:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 952754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         268198
15                 A    =         6790889
39  meter
 Y    =        4658649
11  meter          E    =           
0016819
 Z    =       -4948886
34                 I    =           51
43564
 XDOT =      -7072
656370                 Wp   =           53
93757
 YDOT =      -1922
153156  meter/sec      RA   =          208
97504  deg
 ZDOT =      -2188
260504                 TA   =          194
57610
                                          MA   =          194
62466
                                          Ha   =            229
059  n
mi
                                          Hp   =            219
996

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         879915
20                 X    =          240123
18
 Y    =       15284281
87  feet           Y    =         4661491
86  meter
 Z    =      -16236503
74                 Z    =        -4947651
19
 XDOT =     -23204
253182                 XDOT =       -7040
007108
 YDOT =      -6306
276758  feet/sec       YDOT =       -2001
061803  meter/sec
 ZDOT =      -7179
332362                 ZDOT =       -2222
538301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11695244
11                 X    =         3564710
40
 Y    =        9888336
86  feet           Y    =         3013965
07  meter
 Z    =      -16231131
70                 Z    =        -4947248
94
 XDOT =     -19883
294035                 XDOT =       -6060
428022
 YDOT =      11451
557214  feet/sec       YDOT =        3490
434639  meter/sec
 ZDOT =      -7335
637121                 ZDOT =       -2235
902194


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   19343
93290816  
00016717  00000-0  10270-3 0  9218
2 25544  51
6415 210
0210 0006800  15
2656 344
8698 15
50061406  2517


Satellite: ISS
Catalog Number: 25544
Epoch time:      19343
93290816   =   yrday
fracday
Element set:     921
Inclination:       51
6415  deg
RA of node:       210
0210  deg
Eccentricity:     
0006800     
Arg of perigee:    15
2656  deg
Mean anomaly:     344
8698  deg
Mean motion:   15
50061406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             251
Checksum:              279
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