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

 
Date: April 16th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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


107/20:46:03 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 217 3

109/09:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 217 4

114/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 217 2

116/09:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 6

118/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 217 5

118/11:34:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 5

Coasting Arc #1 (Orbit 550)
---------------------------------------

Vector Time (GMT): 2019/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4504904
34                 A    =         6783274
33  meter
 Y    =        -970680
27  meter          E    =           
0012014
 Z    =       -4988516
96                 I    =           51
34118
 XDOT =       3630
615139                 Wp   =           80
36078
 YDOT =      -6428
139667  meter/sec      RA   =          312
16540  deg
 ZDOT =      -2030
057927                 TA   =          169
80268
                                          MA   =          169
77829
                                          Ha   =            223
344  n
mi
                                          Hp   =            217
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14779869
87                 X    =        -4469483
71
 Y    =       -3184646
57  feet           Y    =        -1020859
49  meter
 Z    =      -16366525
44                 Z    =        -5010313
96
 XDOT =      11911
466990                 XDOT =        3712
087462
 YDOT =     -21089
697071  feet/sec       YDOT =       -6387
084159  meter/sec
 ZDOT =      -6660
295037                 ZDOT =       -2012
223565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14773616
65                 X    =        -4502998
36
 Y    =        2663697
49  feet           Y    =          811895
00  meter
 Z    =      -16464952
13                 Z    =        -5018517
41
 XDOT =       3180
520827                 XDOT =         969
422748
 YDOT =     -22981
313413  feet/sec       YDOT =       -7004
704328  meter/sec
 ZDOT =      -6578
959301                 ZDOT =       -2005
266795


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   19105
51960560  
00016717  00000-0  10270-3 0  9005
2 25544  51
6391 312
7326 0001421 200
2218 159
8878 15
52554164  5519


Satellite: ISS
Catalog Number: 25544
Epoch time:      19105
51960560   =   yrday
fracday
Element set:     900
Inclination:       51
6391  deg
RA of node:       312
7326  deg
Eccentricity:     
0001421     
Arg of perigee:   200
2218  deg
Mean anomaly:     159
8878  deg
Mean motion:   15
52554164  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             551
Checksum:              288


Coasting Arc #2 (Orbit 566)
---------------------------------------

Vector Time (GMT): 2019/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3850028
26                 A    =         6782174
08  meter
 Y    =        1884935
14  meter          E    =           
0003470
 Z    =        5254014
11                 I    =           51
31601
 XDOT =      -4134
944038                 Wp   =          139
74709
 YDOT =       6416
430593  meter/sec      RA   =          307
16139  deg
 ZDOT =        725
162582                 TA   =          303
27760
                                          MA   =          303
31084
                                          Ha   =            223
255  n
mi
                                          Hp   =            217
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12631326
32                 X    =         3803143
14
 Y    =        6184170
42  feet           Y    =         1927727
08  meter
 Z    =       17237579
11                 Z    =         5272602
11
 XDOT =     -13566
089363                 XDOT =       -4209
909511
 YDOT =      21051
281472  feet/sec       YDOT =        6369
771648  meter/sec
 ZDOT =       2379
142330                 ZDOT =         704
894020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13943423
03                 X    =         4249955
34
 Y    =         691836
00  feet           Y    =          210871
61  meter
 Z    =       17321397
72                 Z    =         5279562
03
 XDOT =      -4028
479619                 XDOT =       -1227
880588
 YDOT =      23701
407622  feet/sec       YDOT =        7224
189043  meter/sec
 ZDOT =       2286
823129                 ZDOT =         697
023690


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   19106
54948450  
00016717  00000-0  10270-3 0  9014
2 25544  51
6394 307
6103 0001380 201
3746 158
7348 15
52527373  5679


Satellite: ISS
Catalog Number: 25544
Epoch time:      19106
54948450   =   yrday
fracday
Element set:     901
Inclination:       51
6394  deg
RA of node:       307
6103  deg
Eccentricity:     
0001380     
Arg of perigee:   201
3746  deg
Mean anomaly:     158
7348  deg
Mean motion:   15
52527373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             567
Checksum:              307


Coasting Arc #3 (Orbit 581)
---------------------------------------

Vector Time (GMT): 2019/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3198335
28                 A    =         6782069
45  meter
 Y    =       -2848539
19  meter          E    =           
0014311
 Z    =       -5271085
45                 I    =           51
29458
 XDOT =       4474
854726                 Wp   =          100
12094
 YDOT =      -6179
976831  meter/sec      RA   =          302
15352  deg
 ZDOT =        623
488533                 TA   =          175
87561
                                          MA   =          175
86380
                                          Ha   =            223
341  n
mi
                                          Hp   =            217
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10493225
99                 X    =        -3140640
26
 Y    =       -9345601
01  feet           Y    =        -2883983
05  meter
 Z    =      -17293587
42                 Z    =        -5286481
48
 XDOT =      14681
281909                 XDOT =        4540
599826
 YDOT =     -20275
514538  feet/sec       YDOT =       -6129
568218  meter/sec
 ZDOT =       2045
566054                 ZDOT =         645
385997

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13314726
10                 X    =        -4058328
52
 Y    =       -4214839
65  feet           Y    =        -1284683
13  meter
 Z    =      -17362874
51                 Z    =        -5292204
15
 XDOT =       4655
153255                 XDOT =        1418
890712
 YDOT =     -23556
457868  feet/sec       YDOT =       -7180
008358  meter/sec
 ZDOT =       2145
204543                 ZDOT =         653
858345


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   19107
51499308  
00016717  00000-0  10270-3 0  9026
2 25544  51
6373 302
8072 0001383 201
4279 158
6815 15
52560650  5823


Satellite: ISS
Catalog Number: 25544
Epoch time:      19107
51499308   =   yrday
fracday
Element set:     902
Inclination:       51
6373  deg
RA of node:       302
8072  deg
Eccentricity:     
0001383     
Arg of perigee:   201
4279  deg
Mean anomaly:     158
6815  deg
Mean motion:   15
52560650  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             582
Checksum:              303


Coasting Arc #4 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2019/107/20:46:03
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1905911
08                 A    =         6792368
24  meter
 Y    =        6235475
06  meter          E    =           
0014059
 Z    =        1877051
06                 I    =           51
32536
 XDOT =      -5242
081495                 Wp   =          119
17907
 YDOT =         90
018805  meter/sec      RA   =          300
31828  deg
 ZDOT =      -5596
658854                 TA   =           40
06720
                                          MA   =           39
96359
                                          Ha   =            223
298  n
mi
                                          Hp   =            217
290

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6252989
10                 X    =        -1984614
02
 Y    =       20457595
34  feet           Y    =         6213721
93  meter
 Z    =        6158304
00                 Z    =         1867601
13
 XDOT =     -17198
430102                 XDOT =       -5215
512852
 YDOT =        295
337288  feet/sec       YDOT =          31
546277  meter/sec
 ZDOT =     -18361
741646                 ZDOT =       -5622
058576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13981611
98                 X    =         4261595
33
 Y    =      -16206787
59  feet           Y    =        -4939828
86  meter
 Z    =        6114928
49                 Z    =         1863830
20
 XDOT =      14573
295977                 XDOT =        4441
940614
 YDOT =       5569
829319  feet/sec       YDOT =        1697
683976  meter/sec
 ZDOT =     -18476
557721                 ZDOT =       -5631
654793


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   19107
90119682  
00016717  00000-0  10270-3 0  9034
2 25544  51
6400 300
8877 0001446 201
9114 158
1977 15
52579617  5881


Satellite: ISS
Catalog Number: 25544
Epoch time:      19107
90119682   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:       300
8877  deg
Eccentricity:     
0001446     
Arg of perigee:   201
9114  deg
Mean anomaly:     158
1977  deg
Mean motion:   15
52579617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             588
Checksum:              319


Coasting Arc #5 (Orbit 602)
---------------------------------------

Vector Time (GMT): 2019/108/20:46:03
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2343879
87                 A    =         6793791
93  meter
 Y    =       -6329711
40  meter          E    =           
0009114
 Z    =        -736382
78                 I    =           51
31287
 XDOT =       4741
803120                 Wp   =           41
81453
 YDOT =       1072
297697  meter/sec      RA   =          295
33145  deg
 ZDOT =       5925
023999                 TA   =          310
19882
                                          MA   =          310
27856
                                          Ha   =            223
357  n
mi
                                          Hp   =            217
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7689894
57                 X    =         2418063
28
 Y    =      -20766769
68  feet           Y    =        -6303085
76  meter
 Z    =       -2415953
99                 Z    =         -724816
30
 XDOT =      15557
096850                 XDOT =        4700
679136
 YDOT =       3518
037063  feet/sec       YDOT =        1125
094359  meter/sec
 ZDOT =      19439
055116                 ZDOT =        5947
958214

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15122435
15                 X    =        -4609318
23
 Y    =       16185121
36  feet           Y    =         4933224
99  meter
 Z    =       -2363014
39                 Z    =         -720246
78
 XDOT =     -11693
555928                 XDOT =       -3564
195847
 YDOT =      -8096
651558  feet/sec       YDOT =       -2467
859395  meter/sec
 ZDOT =      19542
600771                 ZDOT =        5956
584715


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   19108
86670624  
00016717  00000-0  10270-3 0  9049
2 25544  51
6391 296
0859 0001405 207
5952 152
5126 15
52517857  6033


Satellite: ISS
Catalog Number: 25544
Epoch time:      19108
86670624   =   yrday
fracday
Element set:     904
Inclination:       51
6391  deg
RA of node:       296
0859  deg
Eccentricity:     
0001405     
Arg of perigee:   207
5952  deg
Mean anomaly:     152
5126  deg
Mean motion:   15
52517857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             603
Checksum:              316


Coasting Arc #6 (Orbit 611)
---------------------------------------

Vector Time (GMT): 2019/109/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4333691
84                 A    =         6782366
27  meter
 Y    =         440841
87  meter          E    =           
0003964
 Z    =        5196956
16                 I    =           51
26900
 XDOT =      -2082
465100                 Wp   =          141
63407
 YDOT =       7294
762645  meter/sec      RA   =          292
69792  deg
 ZDOT =       1114
241409                 TA   =          297
60981
                                          MA   =          297
65006
                                          Ha   =            223
105  n
mi
                                          Hp   =            217
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14218149
07                 X    =         4303195
84
 Y    =        1446331
59  feet           Y    =          489134
07  meter
 Z    =       17050381
11                 Z    =         5217933
81
 XDOT =      -6832
234580                 XDOT =       -2169
294880
 YDOT =      23932
948312  feet/sec       YDOT =        7270
989639  meter/sec
 ZDOT =       3655
647666                 ZDOT =        1103
914059

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13554781
06                 X    =         4131497
27
 Y    =        4156312
53  feet           Y    =         1266844
06  meter
 Z    =       17145148
31                 Z    =         5225841
21
 XDOT =     -11066
662078                 XDOT =       -3373
118601
 YDOT =      21159
682331  feet/sec       YDOT =        6449
471174  meter/sec
 ZDOT =       3608
213993                 ZDOT =        1099
783625


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   19109
44601107  
00016717  00000-0  10270-3 0  9055
2 25544  51
6404 293
2062 0001266 216
1146 143
9920 15
52543857  6124


Satellite: ISS
Catalog Number: 25544
Epoch time:      19109
44601107   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       293
2062  deg
Eccentricity:     
0001266     
Arg of perigee:   216
1146  deg
Mean anomaly:     143
9920  deg
Mean motion:   15
52543857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             612
Checksum:              283


Coasting Arc #7 (Orbit 626)
---------------------------------------

Vector Time (GMT): 2019/110/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3965631
15                 A    =         6781905
18  meter
 Y    =       -1543649
90  meter          E    =           
0014021
 Z    =       -5292824
81                 I    =           51
25513
 XDOT =       2502
426032                 Wp   =           95
63126
 YDOT =      -7231
409485  meter/sec      RA   =          287
68636  deg
 ZDOT =        233
287989                 TA   =          176
61262
                                          MA   =          176
60312
                                          Ha   =            223
154  n
mi
                                          Hp   =            217
257

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13010600
89                 X    =        -3922364
85
 Y    =       -5064468
17  feet           Y    =        -1587754
67  meter
 Z    =      -17364910
80                 Z    =        -5311983
53
 XDOT =       8210
059160                 XDOT =        2581
970520
 YDOT =     -23725
096734  feet/sec       YDOT =       -7202
980834  meter/sec
 ZDOT =        765
380540                 ZDOT =         245
637543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11792934
20                 X    =        -3594486
34
 Y    =       -7269252
45  feet           Y    =        -2215668
15  meter
 Z    =      -17451342
99                 Z    =        -5319169
34
 XDOT =      11747
001508                 XDOT =        3580
486060
 YDOT =     -21036
820011  feet/sec       YDOT =       -6412
022739  meter/sec
 ZDOT =        821
937330                 ZDOT =         250
526498


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   19110
41151650  
00016717  00000-0  10270-3 0  9068
2 25544  51
6397 288
4025 0001259 223
8226 136
2826 15
52575113  6272


Satellite: ISS
Catalog Number: 25544
Epoch time:      19110
41151650   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       288
4025  deg
Eccentricity:     
0001259     
Arg of perigee:   223
8226  deg
Mean anomaly:     136
2826  deg
Mean motion:   15
52575113  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             627
Checksum:              294


Coasting Arc #8 (Orbit 642)
---------------------------------------

Vector Time (GMT): 2019/111/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3605210
14                 A    =         6782734
46  meter
 Y    =        2635514
73  meter          E    =           
0003639
 Z    =        5102878
71                 I    =           51
24860
 XDOT =      -2851
859060                 Wp   =           57
74342
 YDOT =       6942
867316  meter/sec      RA   =          282
67690  deg
 ZDOT =      -1568
239274                 TA   =           47
47561
                                          MA   =           47
44488
                                          Ha   =            223
008  n
mi
                                          Hp   =            217
457

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11828117
26                 X    =         3550683
75
 Y    =        8646701
86  feet           Y    =         2675525
91  meter
 Z    =       16741728
06                 Z    =         5120259
29
 XDOT =      -9356
492980                 XDOT =       -2921
666456
 YDOT =      22778
436076  feet/sec       YDOT =        6910
585491  meter/sec
 ZDOT =      -5145
141976                 ZDOT =       -1582
262424

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10179433
41                 X    =         3102691
30
 Y    =       10412563
74  feet           Y    =         3173749
43  meter
 Z    =       16820015
49                 Z    =         5126740
72
 XDOT =     -12090
301410                 XDOT =       -3685
123870
 YDOT =      20248
783364  feet/sec       YDOT =        6171
829169  meter/sec
 ZDOT =      -5209
225149                 ZDOT =       -1587
771825


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   19111
44138945  
00016717  00000-0  10270-3 0  9075
2 25544  51
6395 283
2810 0001285 226
8339 133
2705 15
52566417  6430


Satellite: ISS
Catalog Number: 25544
Epoch time:      19111
44138945   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:       283
2810  deg
Eccentricity:     
0001285     
Arg of perigee:   226
8339  deg
Mean anomaly:     133
2705  deg
Mean motion:   15
52566417  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             643
Checksum:              309


Coasting Arc #9 (Orbit 657)
---------------------------------------

Vector Time (GMT): 2019/112/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3287668
57                 A    =         6784566
60  meter
 Y    =       -3674618
42  meter          E    =           
0010056
 Z    =       -4670258
46                 I    =           51
24762
 XDOT =       3141
492981                 Wp   =          116
02579
 YDOT =      -6389
909708  meter/sec      RA   =          277
66825  deg
 ZDOT =       2816
594378                 TA   =          182
11475
                                          MA   =          182
11901
                                          Ha   =            223
095  n
mi
                                          Hp   =            217
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10786314
20                 X    =        -3223647
73
 Y    =      -12055834
70  feet           Y    =        -3711025
42  meter
 Z    =      -15322370
28                 Z    =        -4686073
50
 XDOT =      10306
735501                 XDOT =        3199
031629
 YDOT =     -20964
270696  feet/sec       YDOT =       -6354
457644  meter/sec
 ZDOT =       9240
795205                 ZDOT =        2831
994494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8847369
11                 X    =        -2696678
10
 Y    =      -13462075
40  feet           Y    =        -4103240
58  meter
 Z    =      -15393483
72                 Z    =        -4691933
84
 XDOT =      12158
479948                 XDOT =        3705
904688
 YDOT =     -18635
989692  feet/sec       YDOT =       -5680
249658  meter/sec
 ZDOT =       9311
039156                 ZDOT =        2838
004735


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   19112
40689544  
00016717  00000-0  10270-3 0  9089
2 25544  51
6386 278
4784 0001362 230
1476 129
9556 15
52569423  6584


Satellite: ISS
Catalog Number: 25544
Epoch time:      19112
40689544   =   yrday
fracday
Element set:     908
Inclination:       51
6386  deg
RA of node:       278
4784  deg
Eccentricity:     
0001362     
Arg of perigee:   230
1476  deg
Mean anomaly:     129
9556  deg
Mean motion:   15
52569423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             658
Checksum:              337


Coasting Arc #10 (Orbit 673)
---------------------------------------

Vector Time (GMT): 2019/113/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2983070
84                 A    =         6787032
34  meter
 Y    =        4611376
53  meter          E    =           
0009550
 Z    =        3980384
66                 I    =           51
25369
 XDOT =      -3423
551401                 Wp   =           81
41670
 YDOT =       5620
391236  meter/sec      RA   =          272
66396  deg
 ZDOT =      -3936
086209                 TA   =           49
78282
                                          MA   =           49
69930
                                          Ha   =            222
905  n
mi
                                          Hp   =            217
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9786977
81                 X    =         2911948
68
 Y    =       15129188
10  feet           Y    =         4644337
55  meter
 Z    =       13059004
78                 Z    =         3994702
84
 XDOT =     -11232
124019                 XDOT =       -3467
026222
 YDOT =      18439
603794  feet/sec       YDOT =        5581
863707  meter/sec
 ZDOT =     -12913
668664                 ZDOT =       -3952
822184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7713764
06                 X    =         2351155
29
 Y    =       16232452
54  feet           Y    =         4947651
54  meter
 Z    =       13123269
46                 Z    =         3999972
53
 XDOT =     -12198
001723                 XDOT =       -3717
950925
 YDOT =      16323
477329  feet/sec       YDOT =        4975
395890  meter/sec
 ZDOT =     -12989
868060                 ZDOT =       -3959
311785


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   19113
43676570  
00016717  00000-0  10270-3 0  9099
2 25544  51
6396 273
3560 0001397 241
5443 118
5568 15
52588670  6749


Satellite: ISS
Catalog Number: 25544
Epoch time:      19113
43676570   =   yrday
fracday
Element set:     909
Inclination:       51
6396  deg
RA of node:       273
3560  deg
Eccentricity:     
0001397     
Arg of perigee:   241
5443  deg
Mean anomaly:     118
5568  deg
Mean motion:   15
52588670  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             674
Checksum:              332


Coasting Arc #11 (Orbit 688)
---------------------------------------

Vector Time (GMT): 2019/114/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2716035
60                 A    =         6789742
32  meter
 Y    =       -5392155
85  meter          E    =           
0003343
 Z    =       -3108631
50                 I    =           51
26020
 XDOT =       3695
983423                 Wp   =           83
59248
 YDOT =      -4648
646558  meter/sec      RA   =          267
66436  deg
 ZDOT =       4839
086720                 TA   =          240
47134
                                          MA   =          240
50467
                                          Ha   =            223
077  n
mi
                                          Hp   =            217
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8910877
96                 X    =        -2640436
99
 Y    =      -17690800
03  feet           Y    =        -5422105
67  meter
 Z    =      -10198922
24                 Z    =        -3121641
64
 XDOT =      12125
929866                 XDOT =        3724
185429
 YDOT =     -15251
465085  feet/sec       YDOT =       -4607
157949  meter/sec
 ZDOT =      15876
268766                 ZDOT =        4857
108922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6860762
45                 X    =        -2091160
39
 Y    =      -18550086
79  feet           Y    =        -5654066
45  meter
 Z    =      -10257211
39                 Z    =        -3126398
03
 XDOT =      12257
658721                 XDOT =        3736
134378
 YDOT =     -13348
748426  feet/sec       YDOT =       -4068
698520  meter/sec
 ZDOT =      15958
182357                 ZDOT =        4864
053982


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   19114
40227001  
00016717  00000-0  10270-3 0  9100
2 25544  51
6377 268
5536 0001291 235
2444 124
8587 15
52564658  6898


Satellite: ISS
Catalog Number: 25544
Epoch time:      19114
40227001   =   yrday
fracday
Element set:     910
Inclination:       51
6377  deg
RA of node:       268
5536  deg
Eccentricity:     
0001291     
Arg of perigee:   235
2444  deg
Mean anomaly:     124
8587  deg
Mean motion:   15
52564658  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             689
Checksum:              312


Coasting Arc #12 (Orbit 689)
---------------------------------------

Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4035163
10                 A    =         6782654
00  meter
 Y    =        1889192
49  meter          E    =           
0012730
 Z    =       -5125356
84                 I    =           51
23650
 XDOT =      -1535
397810                 Wp   =           81
80365
 YDOT =      -7348
972015  meter/sec      RA   =          267
43993  deg
 ZDOT =      -1501
434162                 TA   =          173
63813
                                          MA   =          173
62195
                                          Ha   =            223
176  n
mi
                                          Hp   =            217
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13238724
07                 X    =        -4031092
35
 Y    =        6198138
10  feet           Y    =         1844091
40  meter
 Z    =      -16815475
20                 Z    =        -5144948
36
 XDOT =      -5037
394390                 XDOT =       -1445
812210
 YDOT =     -24110
800574  feet/sec       YDOT =       -7365
640956  meter/sec
 ZDOT =      -4925
965100                 ZDOT =       -1508
675252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11466821
20                 X    =        -3495087
10
 Y    =        8899461
33  feet           Y    =         2712555
81  meter
 Z    =      -16904216
54                 Z    =        -5152405
20
 XDOT =      -9471
776512                 XDOT =       -2886
997481
 YDOT =     -21612
884994  feet/sec       YDOT =       -6587
607346  meter/sec
 ZDOT =      -4957
988615                 ZDOT =       -1511
194930


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   19114
46663809  
00016717  00000-0  10270-3 0  9117
2 25544  51
6376 268
2326 0001205 221
7639 138
3421 15
52570205  6906


Satellite: ISS
Catalog Number: 25544
Epoch time:      19114
46663809   =   yrday
fracday
Element set:     911
Inclination:       51
6376  deg
RA of node:       268
2326  deg
Eccentricity:     
0001205     
Arg of perigee:   221
7639  deg
Mean anomaly:     138
3421  deg
Mean motion:   15
52570205  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             690
Checksum:              297


Coasting Arc #13 (Orbit 705)
---------------------------------------

Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4181854
77                 A    =         6782039
32  meter
 Y    =        -748657
74  meter          E    =           
0001968
 Z    =        5285227
13                 I    =           51
23553
 XDOT =       1143
414951                 Wp   =          127
58040
 YDOT =       7579
931928  meter/sec      RA   =          262
42874  deg
 ZDOT =        167
771890                 TA   =          320
80442
                                          MA   =          320
81867
                                          Ha   =            223
078  n
mi
                                          Hp   =            217
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13719995
96                 X    =         4164242
84
 Y    =       -2456226
19  feet           Y    =         -701991
94  meter
 Z    =       17339984
01                 Z    =         5305498
31
 XDOT =       3751
361389                 XDOT =        1057
754070
 YDOT =      24868
543070  feet/sec       YDOT =        7592
239429  meter/sec
 ZDOT =        550
432710                 ZDOT =         173
118355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12651825
14                 X    =         3856276
30
 Y    =       -5569004
49  feet           Y    =        -1697432
57  meter
 Z    =       17431692
15                 Z    =         5313179
77
 XDOT =       9054
648865                 XDOT =        2759
856974
 YDOT =      22379
453744  feet/sec       YDOT =        6821
257501  meter/sec
 ZDOT =        573
887781                 ZDOT =         174
920996


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   19115
49650913  
00016717  00000-0  10270-3 0  9124
2 25544  51
6365 263
1104 0001213 225
9745 134
1307 15
52522020  7062


Satellite: ISS
Catalog Number: 25544
Epoch time:      19115
49650913   =   yrday
fracday
Element set:     912
Inclination:       51
6365  deg
RA of node:       263
1104  deg
Eccentricity:     
0001213     
Arg of perigee:   225
9745  deg
Mean anomaly:     134
1307  deg
Mean motion:   15
52522020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             706
Checksum:              270


Coasting Arc #14 (Orbit 720)
---------------------------------------

Vector Time (GMT): 2019/116/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4069506
71                 A    =         6782048
57  meter
 Y    =       -1236663
50  meter          E    =           
0001920
 Z    =        5281407
10                 I    =           51
24124
 XDOT =       1874
387528                 Wp   =          131
20572
 YDOT =       7428
957292  meter/sec      RA   =          257
60428  deg
 ZDOT =        293
927278                 TA   =          315
96882
                                          MA   =          315
98412
                                          Ha   =            223
007  n
mi
                                          Hp   =            217
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13351399
97                 X    =         4057378
77
 Y    =       -4057294
94  feet           Y    =        -1191223
34  meter
 Z    =       17327451
12                 Z    =         5301145
82
 XDOT =       6149
565380                 XDOT =        1789
747767
 YDOT =      24373
219461  feet/sec       YDOT =        7449
444749  meter/sec
 ZDOT =        964
328340                 ZDOT =         302
826946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13087021
15                 X    =         3988924
05
 Y    =       -4510764
73  feet           Y    =        -1374881
09  meter
 Z    =       17416801
22                 Z    =         5308641
01
 XDOT =       6652
078639                 XDOT =        2027
553569
 YDOT =      23192
286810  feet/sec       YDOT =        7069
009020  meter/sec
 ZDOT =       1003
879799                 ZDOT =         305
982563


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   19116
46201012  
00016717  00000-0  10270-3 0  9135
2 25544  51
6369 258
3091 0001212 237
9016 122
2018 15
52526036  7215


Satellite: ISS
Catalog Number: 25544
Epoch time:      19116
46201012   =   yrday
fracday
Element set:     913
Inclination:       51
6369  deg
RA of node:       258
3091  deg
Eccentricity:     
0001212     
Arg of perigee:   237
9016  deg
Mean anomaly:     122
2018  deg
Mean motion:   15
52526036  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             721
Checksum:              264


Coasting Arc #15 (Orbit 735)
---------------------------------------

Vector Time (GMT): 2019/117/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4351348
95                 A    =         6782245
94  meter
 Y    =         106084
95  meter          E    =           
0013480
 Z    =       -5213198
17                 I    =           51
25144
 XDOT =      -1446
104527                 Wp   =          101
45798
 YDOT =      -7443
668304  meter/sec      RA   =          252
59344  deg
 ZDOT =       1055
260209                 TA   =          178
72341
                                          MA   =          178
71996
                                          Ha   =            223
114  n
mi
                                          Hp   =            217
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14276079
24                 X    =        -4326888
95
 Y    =         348047
75  feet           Y    =           57561
93  meter
 Z    =      -17103668
53                 Z    =        -5234276
02
 XDOT =      -4744
437426                 XDOT =       -1367
885712
 YDOT =     -24421
483938  feet/sec       YDOT =       -7459
402317  meter/sec
 ZDOT =       3462
139794                 ZDOT =        1048
425478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14124248
80                 X    =        -4305071
04
 Y    =        1078845
37  feet           Y    =          328832
07  meter
 Z    =      -17198975
01                 Z    =        -5242247
58
 XDOT =      -5945
546865                 XDOT =       -1812
202684
 YDOT =     -23112
036207  feet/sec       YDOT =       -7044
548636  meter/sec
 ZDOT =       3431
904480                 ZDOT =        1046
044485


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   19117
42750897  
00016717  00000-0  10270-3 0  9143
2 25544  51
6377 253
5071 0001134 235
3751 124
7294 15
52575559  7363


Satellite: ISS
Catalog Number: 25544
Epoch time:      19117
42750897   =   yrday
fracday
Element set:     914
Inclination:       51
6377  deg
RA of node:       253
5071  deg
Eccentricity:     
0001134     
Arg of perigee:   235
3751  deg
Mean anomaly:     124
7294  deg
Mean motion:   15
52575559  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             736
Checksum:              320


Coasting Arc #16 (Orbit 751)
---------------------------------------

Vector Time (GMT): 2019/118/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4624512
75                 A    =         6783820
67  meter
 Y    =         985301
74  meter          E    =           
0005629
 Z    =        4861338
95                 I    =           51
26603
 XDOT =        940
270106                 Wp   =           59
50534
 YDOT =       7236
076410  meter/sec      RA   =          247
58490  deg
 ZDOT =      -2356
228109                 TA   =           53
71957
                                          MA   =           53
66759
                                          Ha   =            223
011  n
mi
                                          Hp   =            217
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15172285
92                 X    =         4589537
38
 Y    =        3232617
27  feet           Y    =         1036820
74  meter
 Z    =       15949274
77                 Z    =         4883718
20
 XDOT =       3084
875675                 XDOT =         870
729634
 YDOT =      23740
408168  feet/sec       YDOT =        7246
202335  meter/sec
 ZDOT =      -7730
407182                 ZDOT =       -2351
829543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15252041
76                 X    =         4648822
33
 Y    =        2188166
56  feet           Y    =          666953
17  meter
 Z    =       16050376
62                 Z    =         4892154
79
 XDOT =       4924
179339                 XDOT =        1500
889863
 YDOT =      22355
212040  feet/sec       YDOT =        6813
868630  meter/sec
 ZDOT =      -7711
148365                 ZDOT =       -2350
358022


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   19118
45737554  
00016717  00000-0  10270-3 0  9153
2 25544  51
6364 248
3847 0001151 237
0016 123
1025 15
52536058  7528


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
45737554   =   yrday
fracday
Element set:     915
Inclination:       51
6364  deg
RA of node:       248
3847  deg
Eccentricity:     
0001151     
Arg of perigee:   237
0016  deg
Mean anomaly:     123
1025  deg
Mean motion:   15
52536058  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             752
Checksum:              295


Coasting Arc #17 (Orbit 752)
---------------------------------------

Vector Time (GMT): 2019/118/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2218750
89                 A    =         6793720
90  meter
 Y    =       -6394658
66  meter          E    =           
0011675
 Z    =         513188
50                 I    =           51
30217
 XDOT =       4691
191283                 Wp   =           50
16097
 YDOT =      -1143
173016  meter/sec      RA   =          247
38265  deg
 ZDOT =       5954
452614                 TA   =          315
39791
                                          MA   =          315
49180
                                          Ha   =            223
064  n
mi
                                          Hp   =            217
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7279366
43                 X    =        -2149571
88
 Y    =      -20979851
25  feet           Y    =        -6419083
48  meter
 Z    =        1683689
31                 Z    =          502578
66
 XDOT =      15391
047517                 XDOT =        4674
702414
 YDOT =      -3750
567639  feet/sec       YDOT =       -1090
805004  meter/sec
 ZDOT =      19535
605689                 ZDOT =        5977
200676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14099748
36                 X    =        -4297603
30
 Y    =      -17160939
74  feet           Y    =        -5230654
43  meter
 Z    =        1636272
34                 Z    =          498735
81
 XDOT =      11768
326240                 XDOT =        3586
985838
 YDOT =      -7769
829326  feet/sec       YDOT =       -2368
243979  meter/sec
 ZDOT =      19638
560206                 ZDOT =        5985
833151


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   19118
52174085  
00016717  00000-0  10270-3 0  9166
2 25544  51
6385 248
0645 0001268 234
4474 125
6559 15
52583363  7533


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
52174085   =   yrday
fracday
Element set:     916
Inclination:       51
6385  deg
RA of node:       248
0645  deg
Eccentricity:     
0001268     
Arg of perigee:   234
4474  deg
Mean anomaly:     125
6559  deg
Mean motion:   15
52583363  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             753
Checksum:              323


Coasting Arc #18 (Orbit 752)
---------------------------------------

Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4532029
11                 A    =         6788870
17  meter
 Y    =        3710351
91  meter          E    =           
0011266
 Z    =        3422152
53                 I    =           51
28590
 XDOT =      -1450
964139                 Wp   =           93
30560
 YDOT =       5990
983181  meter/sec      RA   =          247
23269  deg
 ZDOT =      -4561
581259                 TA   =           46
41365
                                          MA   =           46
32019
                                          Ha   =            223
013  n
mi
                                          Hp   =            217
509

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14868861
90                 X    =         4473579
11
 Y    =       12173070
57  feet           Y    =         3760705
43  meter
 Z    =       11227534
55                 Z    =         3444025
51
 XDOT =      -4760
381032                 XDOT =       -1495
691494
 YDOT =      19655
456629  feet/sec       YDOT =        5974
507379  meter/sec
 ZDOT =     -14965
817778                 ZDOT =       -4568
738175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18833988
98                 X    =         5740599
84
 Y    =        3510597
43  feet           Y    =         1070030
10  meter
 Z    =       11326111
34                 Z    =         3452198
74
 XDOT =       5672
749474                 XDOT =        1729
054040
 YDOT =      18086
094113  feet/sec       YDOT =        5512
641486  meter/sec
 ZDOT =     -14998
697722                 ZDOT =       -4571
603066


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   19118
52174180  
00016717  00000-0  10270-3 0  9173
2 25544  51
6383 248
0645 0001317 234
6294 125
4735 15
52552037  7536


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
52174180   =   yrday
fracday
Element set:     917
Inclination:       51
6383  deg
RA of node:       248
0645  deg
Eccentricity:     
0001317     
Arg of perigee:   234
6294  deg
Mean anomaly:     125
4735  deg
Mean motion:   15
52552037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             753
Checksum:              303


Coasting Arc #19 (Orbit 767)
---------------------------------------

Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4536904
52                 A    =         6791288
57  meter
 Y    =       -4424082
27  meter          E    =           
0004149
 Z    =       -2439903
85                 I    =           51
30919
 XDOT =       2121
726841                 Wp   =           43
60699
 YDOT =      -5099
845512  meter/sec      RA   =          242
23956  deg
 ZDOT =       5310
239785                 TA   =          288
98324
                                          MA   =          289
02819
                                          Ha   =            223
005  n
mi
                                          Hp   =            217
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14884857
36                 X    =        -4475244
23
 Y    =      -14514705
61  feet           Y    =        -4474472
38  meter
 Z    =       -8004933
90                 Z    =        -2461792
70
 XDOT =       6961
046065                 XDOT =        2152
802768
 YDOT =     -16731
776615  feet/sec       YDOT =       -5075
945045  meter/sec
 ZDOT =      17422
046539                 ZDOT =        5320
621933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20090606
91                 X    =        -6123616
99
 Y    =       -5197578
39  feet           Y    =        -1584221
89  meter
 Z    =       -8103537
32                 Z    =        -2469958
18
 XDOT =      -2779
289310                 XDOT =        -847
127382
 YDOT =     -16451
279529  feet/sec       YDOT =       -5014
350000  meter/sec
 ZDOT =      17469
422951                 ZDOT =        5324
680116


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
48723930  
00016717  00000-0  10270-3 0  9183
2 25544  51
6395 243
2629 0001316 244
7669 115
3347 15
52566552  7685


Satellite: ISS
Catalog Number: 25544
Epoch time:      19119
48723930   =   yrday
fracday
Element set:     918
Inclination:       51
6395  deg
RA of node:       243
2629  deg
Eccentricity:     
0001316     
Arg of perigee:   244
7669  deg
Mean anomaly:     115
3347  deg
Mean motion:   15
52566552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             768
Checksum:              332


Coasting Arc #20 (Orbit 782)
---------------------------------------

Vector Time (GMT): 2019/120/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4435726
67                 A    =         6793104
21  meter
 Y    =        4967834
82  meter          E    =           
0013038
 Z    =        1303792
31                 I    =           51
33235
 XDOT =      -2880
560823                 Wp   =          125
12174
 YDOT =       4103
489317  meter/sec      RA   =          237
25156  deg
 ZDOT =      -5801
491302                 TA   =           40
63382
                                          MA   =           40
53660
                                          Ha   =            222
982  n
mi
                                          Hp   =            217
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14552909
01                 X    =         4373512
11
 Y    =       16298670
68  feet           Y    =         5017090
39  meter
 Z    =        4277533
81                 Z    =         1325188
34
 XDOT =      -9450
658867                 XDOT =       -2898
052500
 YDOT =      13462
891459  feet/sec       YDOT =        4071
178943  meter/sec
 ZDOT =     -19033
764113                 ZDOT =       -5815
526655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20828615
00                 X    =         6348561
85
 Y    =        6539808
51  feet           Y    =         1993333
63  meter
 Z    =        4373879
74                 Z    =         1333158
55
 XDOT =       -619
751377                 XDOT =        -188
900220
 YDOT =      14819
107646  feet/sec       YDOT =        4516
864010  meter/sec
 ZDOT =     -19097
570632                 ZDOT =       -5820
939529


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
51710197  
00016717  00000-0  10270-3 0  9191
2 25544  51
6401 238
1407 0001314 247
5168 112
5845 15
52573309  7830


Satellite: ISS
Catalog Number: 25544
Epoch time:      19120
51710197   =   yrday
fracday
Element set:     919
Inclination:       51
6401  deg
RA of node:       238
1407  deg
Eccentricity:     
0001314     
Arg of perigee:   247
5168  deg
Mean anomaly:     112
5845  deg
Mean motion:   15
52573309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             783
Checksum:              295
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