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

 
Date: December 3rd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19912 1579 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


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 0 220 9

338/17:51:57 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 220 5

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 4

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 3

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 2

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 0

343/10:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 219 8

346/03:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 2
000/00:00:00 000 0 0 0 0 219 4

Coasting Arc #1 (Orbit 135)
---------------------------------------

Vector Time (GMT): 2019/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3055330
02                 A    =         6789896
31  meter
 Y    =        3247907
15  meter          E    =           
0015602
 Z    =       -5133261
22                 I    =           51
26980
 XDOT =      -4128
381262                 Wp   =           51
54804
 YDOT =      -6264
509010  meter/sec      RA   =          245
84212  deg
 ZDOT =      -1500
040033                 TA   =          203
85987
                                          MA   =          203
93227
                                          Ha   =            228
423  n
mi
                                          Hp   =            220
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10024048
61                 X    =        -3066487
40
 Y    =       10655863
35  feet           Y    =         3213678
37  meter
 Z    =      -16841408
19                 Z    =        -5148129
70
 XDOT =     -13544
557945                 XDOT =       -4050
736490
 YDOT =     -20552
851082  feet/sec       YDOT =       -6310
241209  meter/sec
 ZDOT =      -4921
391186                 ZDOT =       -1519
906195

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6656574
64                 X    =        -2028923
95
 Y    =      -12939213
14  feet           Y    =        -3943872
16  meter
 Z    =      -16909428
78                 Z    =        -5153993
89
 XDOT =      22976
293845                 XDOT =        7003
174364
 YDOT =      -5243
527566  feet/sec       YDOT =       -1598
227202  meter/sec
 ZDOT =      -5011
546388                 ZDOT =       -1527
519339


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
51877323  
00016717  00000-0  10270-3 0  9005
2 25544  51
6422 246
7557 0007099 350
6795   9
4222 15
50098184  1368


Satellite: ISS
Catalog Number: 25544
Epoch time:      19336
51877323   =   yrday
fracday
Element set:     900
Inclination:       51
6422  deg
RA of node:       246
7557  deg
Eccentricity:     
0007099     
Arg of perigee:   350
6795  deg
Mean anomaly:       9
4222  deg
Mean motion:   15
50098184  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             136
Checksum:              317


Coasting Arc #2 (Orbit 137)
---------------------------------------

Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4731127
46                 A    =         6791494
43  meter
 Y    =        1247542
64  meter          E    =           
0011962
 Z    =        4709966
47                 I    =           51
27726
 XDOT =        858
778128                 Wp   =           27
54887
 YDOT =       7105
846460  meter/sec      RA   =          245
29086  deg
 ZDOT =      -2731
568810                 TA   =           89
71406
                                          MA   =           89
57699
                                          Ha   =            228
281  n
mi
                                          Hp   =            220
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15522071
72                 X    =         4693947
00
 Y    =        4092987
67  feet           Y    =         1300241
14  meter
 Z    =       15452645
90                 Z    =         4732858
37
 XDOT =       2817
513543                 XDOT =         792
523129
 YDOT =      23313
144554  feet/sec       YDOT =        7115
079713  meter/sec
 ZDOT =      -8961
839928                 ZDOT =       -2727
557463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         801667
45                 X    =          244348
24
 Y    =       15931426
34  feet           Y    =         4855898
75  meter
 Z    =       15556944
03                 Z    =         4741756
54
 XDOT =     -20163
332253                 XDOT =       -6145
783671
 YDOT =       9790
464411  feet/sec       YDOT =        2984
133552  meter/sec
 ZDOT =      -8944
035129                 ZDOT =       -2726
141907


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
64771099  
00016717  00000-0  10270-3 0  9013
2 25544  51
6425 246
1175 0007199 349
1124  10
9870 15
50128825  1385


Satellite: ISS
Catalog Number: 25544
Epoch time:      19336
64771099   =   yrday
fracday
Element set:     901
Inclination:       51
6425  deg
RA of node:       246
1175  deg
Eccentricity:     
0007199     
Arg of perigee:   349
1124  deg
Mean anomaly:      10
9870  deg
Mean motion:   15
50128825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             138
Checksum:              312


Coasting Arc #3 (Orbit 152)
---------------------------------------

Vector Time (GMT): 2019/337/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4899233
89                 A    =         6792247
15  meter
 Y    =       -1243982
88  meter          E    =           
0009157
 Z    =       -4542439
56                 I    =           51
29434
 XDOT =      -1097
575080                 Wp   =           66
65089
 YDOT =      -6919
935219  meter/sec      RA   =          240
31030  deg
 ZDOT =       3087
400163                 TA   =          234
41944
                                          MA   =          234
50482
                                          Ha   =            228
417  n
mi
                                          Hp   =            220
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16073602
00                 X    =        -4862894
48
 Y    =       -4081308
66  feet           Y    =        -1298566
04  meter
 Z    =      -14903016
94                 Z    =        -4566150
11
 XDOT =      -3600
968110                 XDOT =       -1035
109692
 YDOT =     -22703
199539  feet/sec       YDOT =       -6931
860047  meter/sec
 ZDOT =      10129
265626                 ZDOT =        3082
219732

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1265042
90                 X    =         -385585
08
 Y    =      -16437317
24  feet           Y    =        -5010094
29  meter
 Z    =      -15011060
72                 Z    =        -4575371
31
 XDOT =      19121
985764                 XDOT =        5828
381261
 YDOT =     -10675
467732  feet/sec       YDOT =       -3253
882565  meter/sec
 ZDOT =      10106
097395                 ZDOT =        3080
338486


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
61476291  
00016717  00000-0  10270-3 0  9028
2 25544  51
6423 241
3259 0007158 352
4252   7
6789 15
50097064  1536


Satellite: ISS
Catalog Number: 25544
Epoch time:      19337
61476291   =   yrday
fracday
Element set:     902
Inclination:       51
6423  deg
RA of node:       241
3259  deg
Eccentricity:     
0007158     
Arg of perigee:   352
4252  deg
Mean anomaly:       7
6789  deg
Mean motion:   15
50097064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             153
Checksum:              308


Coasting Arc #4 (Orbit 168)
---------------------------------------

Vector Time (GMT): 2019/338/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5083330
65                 A    =         6792948
73  meter
 Y    =        1262498
99  meter          E    =           
0013400
 Z    =        4324427
44                 I    =           51
31516
 XDOT =       1283
387498                 Wp   =           39
59982
 YDOT =       6716
894583  meter/sec      RA   =          235
33099  deg
 ZDOT =      -3453
504352                 TA   =           85
75145
                                          MA   =           85
59834
                                          Ha   =            228
518  n
mi
                                          Hp   =            220
565

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16677593
99                 X    =         5047829
45
 Y    =        4142057
07  feet           Y    =         1319145
61  meter
 Z    =       14187754
06                 Z    =         4349034
33
 XDOT =       4210
588905                 XDOT =        1224
957126
 YDOT =      22037
055717  feet/sec       YDOT =        6730
919847  meter/sec
 ZDOT =     -11330
394857                 ZDOT =       -3447
411589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1695916
52                 X    =          516915
36
 Y    =       17006703
60  feet           Y    =         5183643
26  meter
 Z    =       14299896
61                 Z    =         4358608
49
 XDOT =     -18056
639311                 XDOT =       -5503
663662
 YDOT =      11348
651779  feet/sec       YDOT =        3459
069062  meter/sec
 ZDOT =     -11303
034527                 ZDOT =       -3445
164924


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
64627974  
00016717  00000-0  10270-3 0  9039
2 25544  51
6429 236
2146 0007345 355
4999   4
6084 15
50135452  1695


Satellite: ISS
Catalog Number: 25544
Epoch time:      19338
64627974   =   yrday
fracday
Element set:     903
Inclination:       51
6429  deg
RA of node:       236
2146  deg
Eccentricity:     
0007345     
Arg of perigee:   355
4999  deg
Mean anomaly:       4
6084  deg
Mean motion:   15
50135452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             169
Checksum:              328


Coasting Arc #5 (Orbit 170)
---------------------------------------

Vector Time (GMT): 2019/338/17:51:57
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3383732
68                 A    =         6800709
37  meter
 Y    =        5847723
50  meter          E    =           
0006478
 Z    =        -777811
61                 I    =           51
34013
 XDOT =      -4505
318857                 Wp   =           97
56286
 YDOT =       1826
072231  meter/sec      RA   =          234
66005  deg
 ZDOT =      -5914
228546                 TA   =           90
85935
                                          MA   =           90
78512
                                          Ha   =            228
613  n
mi
                                          Hp   =            220
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11101485
17                 X    =         3321868
44
 Y    =       19185444
55  feet           Y    =         5885216
93  meter
 Z    =       -2551875
37                 Z    =         -761524
51
 XDOT =     -14781
229845                 XDOT =       -4496
675503
 YDOT =       5991
050628  feet/sec       YDOT =        1775
739276  meter/sec
 ZDOT =     -19403
636961                 ZDOT =       -5936
092699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4019072
27                 X    =         1225013
23
 Y    =       21806950
10  feet           Y    =         6646758
39  meter
 Z    =       -2477964
70                 Z    =         -755283
64
 XDOT =     -14220
661078                 XDOT =       -4334
457496
 YDOT =        421
333076  feet/sec       YDOT =         128
422322  meter/sec
 ZDOT =     -19503
467525                 ZDOT =       -5944
656902


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
77522043  
00016717  00000-0  10270-3 0  9045
2 25544  51
6393 235
5715 0007138 358
2132   1
8992 15
50136929  1719


Satellite: ISS
Catalog Number: 25544
Epoch time:      19338
77522043   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:       235
5715  deg
Eccentricity:     
0007138     
Arg of perigee:   358
2132  deg
Mean anomaly:       1
8992  deg
Mean motion:   15
50136929  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             171
Checksum:              308


Coasting Arc #6 (Orbit 186)
---------------------------------------

Vector Time (GMT): 2019/339/17:51:57
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3602960
69                 A    =         6800579
51  meter
 Y    =       -5642641
79  meter          E    =           
0018382
 Z    =        1129802
19                 I    =           51
35892
 XDOT =       4627
879168                 Wp   =           39
84837
 YDOT =      -1775
662382  meter/sec      RA   =          229
68707  deg
 ZDOT =       5850
979278                 TA   =          332
45255
                                          MA   =          332
54986
                                          Ha   =            228
666  n
mi
                                          Hp   =            220
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11820737
18                 X    =        -3545083
24
 Y    =      -18512604
30  feet           Y    =        -5682609
09  meter
 Z    =        3706700
09                 Z    =         1112440
47
 XDOT =      15183
330604                 XDOT =        4618
970160
 YDOT =      -5825
663984  feet/sec       YDOT =       -1723
960317  meter/sec
 ZDOT =      19196
126239                 ZDOT =        5873
438216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5297747
54                 X    =        -1614753
45
 Y    =      -21329756
06  feet           Y    =        -6501309
65  meter
 Z    =        3627857
28                 Z    =         1105770
90
 XDOT =      14570
172808                 XDOT =        4440
988672
 YDOT =       -314
143576  feet/sec       YDOT =         -95
750962  meter/sec
 ZDOT =      19298
671394                 ZDOT =        5882
235041


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
80673852  
00016717  00000-0  10270-3 0  9056
2 25544  51
6388 230
4603 0006784   2
5867 357
5318 15
50092054  1873


Satellite: ISS
Catalog Number: 25544
Epoch time:      19339
80673852   =   yrday
fracday
Element set:     905
Inclination:       51
6388  deg
RA of node:       230
4603  deg
Eccentricity:     
0006784     
Arg of perigee:     2
5867  deg
Mean anomaly:     357
5318  deg
Mean motion:   15
50092054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             187
Checksum:              323


Coasting Arc #7 (Orbit 186)
---------------------------------------

Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -349473
81                 A    =         6792622
96  meter
 Y    =        5107682
17  meter          E    =           
0013568
 Z    =       -4477749
86                 I    =           51
33445
 XDOT =      -6143
273981                 Wp   =           42
58236
 YDOT =      -3237
938305  meter/sec      RA   =          229
49969  deg
 ZDOT =      -3209
933109                 TA   =          194
89298
                                          MA   =          194
93298
                                          Ha   =            228
690  n
mi
                                          Hp   =            220
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1146567
62                 X    =         -384812
83
 Y    =       16757487
44  feet           Y    =         5103576
77  meter
 Z    =      -14690780
37                 Z    =        -4479533
02
 XDOT =     -20155
098363                 XDOT =       -6091
017635
 YDOT =     -10623
157169  feet/sec       YDOT =       -3306
344368  meter/sec
 ZDOT =     -10531
276604                 ZDOT =       -3239
648334

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2246460
20                 X    =         -684721
07
 Y    =       16638305
62  feet           Y    =         5071355
55  meter
 Z    =      -14699225
59                 Z    =        -4480323
96
 XDOT =     -18056
419327                 XDOT =       -5503
596611
 YDOT =     -11873
176266  feet/sec       YDOT =       -3618
944126  meter/sec
 ZDOT =     -10666
612275                 ZDOT =       -3251
183421


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
80673873  
00016717  00000-0  10270-3 0  9060
2 25544  51
6399 230
4608 0006772   3
0230 357
0960 15
50099615  1875


Satellite: ISS
Catalog Number: 25544
Epoch time:      19339
80673873   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       230
4608  deg
Eccentricity:     
0006772     
Arg of perigee:     3
0230  deg
Mean anomaly:     357
0960  deg
Mean motion:   15
50099615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             187
Checksum:              319


Coasting Arc #8 (Orbit 196)
---------------------------------------

Vector Time (GMT): 2019/340/09:34:11
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         925173
85                 A    =         6791040
74  meter
 Y    =       -4656137
18  meter          E    =           
0007411
 Z    =        4849183
67                 I    =           51
34419
 XDOT =       6234
017404                 Wp   =           61
45623
 YDOT =       3753
187048  meter/sec      RA   =          226
44517  deg
 ZDOT =       2415
045632                 TA   =            4
75840
                                          MA   =            4
75136
                                          Ha   =            228
714  n
mi
                                          Hp   =            220
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3035347
29                 X    =          953616
50
 Y    =      -15276040
62  feet           Y    =        -4645632
48  meter
 Z    =       15909395
26                 Z    =         4853746
68
 XDOT =      20452
813004                 XDOT =        6179
853781
 YDOT =      12313
605800  feet/sec       YDOT =        3822
597251  meter/sec
 ZDOT =       7923
378058                 ZDOT =        2445
197111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6985298
10                 X    =         2129118
86
 Y    =       13896214
00  feet           Y    =         4235566
03  meter
 Z    =       15930488
21                 Z    =         4855612
81
 XDOT =     -22664
718910                 XDOT =       -6908
206324
 YDOT =       2154
802407  feet/sec       YDOT =         656
783774  meter/sec
 ZDOT =       8060
683529                 ZDOT =        2456
896340


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
45143540  
00016717  00000-0  10270-3 0  9077
2 25544  51
6411 227
2707 0007127   3
4747 356
6452 15
50118305  1976


Satellite: ISS
Catalog Number: 25544
Epoch time:      19340
45143540   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       227
2707  deg
Eccentricity:     
0007127     
Arg of perigee:     3
4747  deg
Mean anomaly:     356
6452  deg
Mean motion:   15
50118305  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             197
Checksum:              287


Coasting Arc #9 (Orbit 211)
---------------------------------------

Vector Time (GMT): 2019/341/09:34:11
000
Vector Time (MET): N/A
Weight (LBS)     : 920317
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -919003
79                 A    =         6790507
47  meter
 Y    =        4519554
75  meter          E    =           
0016829
 Z    =       -4998729
45                 I    =           51
36710
 XDOT =      -6463
690772                 Wp   =           51
66675
 YDOT =      -3556
272655  meter/sec      RA   =          221
46922  deg
 ZDOT =      -2021
462472                 TA   =          198
52934
                                          MA   =          198
59070
                                          Ha   =            228
949  n
mi
                                          Hp   =            220
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3015104
29                 X    =         -945193
10
 Y    =       14827935
52  feet           Y    =         4509131
68  meter
 Z    =      -16400030
99                 Z    =        -5003257
01
 XDOT =     -21206
334555                 XDOT =       -6413
623831
 YDOT =     -11667
561205  feet/sec       YDOT =       -3628
274145  meter/sec
 ZDOT =      -6632
094725                 ZDOT =       -2052
739684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6962616
89                 X    =        -2122205
63
 Y    =      -13408725
55  feet           Y    =        -4086979
55  meter
 Z    =      -16420949
66                 Z    =        -5005105
46
 XDOT =      22844
843326                 XDOT =        6963
108246
 YDOT =      -3543
596860  feet/sec       YDOT =       -1080
088323  meter/sec
 ZDOT =      -6774
565461                 ZDOT =       -2064
887553


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
41848208  
00016717  00000-0  10270-3 0  9088
2 25544  51
6420 222
4793 0007264   7
6972 352
4288 15
50108743  2120


Satellite: ISS
Catalog Number: 25544
Epoch time:      19341
41848208   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:       222
4793  deg
Eccentricity:     
0007264     
Arg of perigee:     7
6972  deg
Mean anomaly:     352
4288  deg
Mean motion:   15
50108743  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             212
Checksum:              302


Coasting Arc #10 (Orbit 212)
---------------------------------------

Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942917
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1834093
33                 A    =         6795571
23  meter
 Y    =        5454239
89  meter          E    =           
0009990
 Z    =       -3627553
53                 I    =           51
38646
 XDOT =      -6228
111924                 Wp   =           38
25376
 YDOT =       -812
381084  meter/sec      RA   =          221
18284  deg
 ZDOT =      -4369
203248                 TA   =          184
78490
                                          MA   =          184
79445
                                          Ha   =            228
921  n
mi
                                          Hp   =            220
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6017366
57                 X    =         1790586
99
 Y    =       17894487
84  feet           Y    =         5474506
99  meter
 Z    =      -11901422
35                 Z    =        -3618749
40
 XDOT =     -20433
438072                 XDOT =       -6197
341317
 YDOT =      -2665
292271  feet/sec       YDOT =        -881
855907  meter/sec
 ZDOT =     -14334
656324                 ZDOT =       -4399
382791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18547604
92                 X    =        -5653309
98
 Y    =       -3654386
65  feet           Y    =        -1113857
05  meter
 Z    =      -11861579
14                 Z    =        -3615409
32
 XDOT =      12200
223760                 XDOT =        3718
628202
 YDOT =     -14933
857709  feet/sec       YDOT =       -4551
839830  meter/sec
 ZDOT =     -14472
281450                 ZDOT =       -4411
151386


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
48295118  
00016717  00000-0  10270-3 0  9092
2 25544  51
6431 222
1607 0007203   6
5755 353
5489 15
50096908  2138


Satellite: ISS
Catalog Number: 25544
Epoch time:      19341
48295118   =   yrday
fracday
Element set:     909
Inclination:       51
6431  deg
RA of node:       222
1607  deg
Eccentricity:     
0007203     
Arg of perigee:     6
5755  deg
Mean anomaly:     353
5489  deg
Mean motion:   15
50096908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             213
Checksum:              304


Coasting Arc #11 (Orbit 228)
---------------------------------------

Vector Time (GMT): 2019/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942917
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1899290
91                 A    =         6794771
16  meter
 Y    =       -5231097
90  meter          E    =           
0013723
 Z    =        3883022
28                 I    =           51
40992
 XDOT =       6455
996808                 Wp   =           66
59458
 YDOT =        690
205666  meter/sec      RA   =          216
21092  deg
 ZDOT =       4081
486093                 TA   =          340
46622
                                          MA   =          340
51875
                                          Ha   =            229
106  n
mi
                                          Hp   =            220
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6231269
40                 X    =        -1859515
95
 Y    =      -17162394
67  feet           Y    =        -5252115
02  meter
 Z    =       12739574
40                 Z    =         3873892
29
 XDOT =      21181
091891                 XDOT =        6427
973006
 YDOT =       2264
454285  feet/sec       YDOT =         762
244174  meter/sec
 ZDOT =      13390
702406                 ZDOT =        4112
779380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18073609
97                 X    =         5508836
32
 Y    =        2788018
55  feet           Y    =          849788
05  meter
 Z    =       12698221
94                 Z    =         3870418
05
 XDOT =     -11996
005587                 XDOT =       -3656
382503
 YDOT =      16034
295250  feet/sec       YDOT =        4887
253192  meter/sec
 ZDOT =      13533
431378                 ZDOT =        4124
989884


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
51446445  
00016717  00000-0  10270-3 0  9100
2 25544  51
6434 217
0494 0007335  11
3700 348
7615 15
50086538  2290


Satellite: ISS
Catalog Number: 25544
Epoch time:      19342
51446445   =   yrday
fracday
Element set:     910
Inclination:       51
6434  deg
RA of node:       217
0494  deg
Eccentricity:     
0007335     
Arg of perigee:    11
3700  deg
Mean anomaly:     348
7615  deg
Mean motion:   15
50086538  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             229
Checksum:              294


Coasting Arc #12 (Orbit 235)
---------------------------------------

Vector Time (GMT): 2019/342/21:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 942917
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -221950
37                 A    =         6791193
40  meter
 Y    =       -4778496
05  meter          E    =           
0008434
 Z    =        4812422
71                 I    =           51
41044
 XDOT =       6894
276083                 Wp   =           68
71993
 YDOT =       2217
245993  meter/sec      RA   =          213
94317  deg
 ZDOT =       2519
012534                 TA   =          356
42316
                                          MA   =          356
42919
                                          Ha   =            228
870  n
mi
                                          Hp   =            220
020

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -728183
62                 X    =         -191875
79
 Y    =      -15677480
47  feet           Y    =        -4780810
32  meter
 Z    =       15788788
41                 Z    =         4811417
17
 XDOT =      22619
016020                 XDOT =        6856
733633
 YDOT =       7274
429110  feet/sec       YDOT =        2294
132527  meter/sec
 ZDOT =       8264
476817                 ZDOT =        2552
411894

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11692686
36                 X    =        -3563930
80
 Y    =      -10475254
12  feet           Y    =        -3192857
45  meter
 Z    =       15784474
06                 Z    =         4811107
69
 XDOT =      20316
558488                 XDOT =        6192
487027
 YDOT =      -9992
307838  feet/sec       YDOT =       -3045
655429  meter/sec
 ZDOT =       8416
735367                 ZDOT =        2565
420940


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
96574824  
00016717  00000-0  10270-3 0  9113
2 25544  51
6431 214
8106 0006834  12
4679 347
6639 15
50127731  2365


Satellite: ISS
Catalog Number: 25544
Epoch time:      19342
96574824   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:       214
8106  deg
Eccentricity:     
0006834     
Arg of perigee:    12
4679  deg
Mean anomaly:     347
6639  deg
Mean motion:   15
50127731  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             236
Checksum:              312


Coasting Arc #13 (Orbit 243)
---------------------------------------

Vector Time (GMT): 2019/343/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6043964
34                 A    =         6797276
58  meter
 Y    =         899907
08  meter          E    =           
0015944
 Z    =        2971059
90                 I    =           51
44479
 XDOT =       1617
201039                 Wp   =           70
23411
 YDOT =       5608
502941  meter/sec      RA   =          211
26892  deg
 ZDOT =      -4961
537346                 TA   =           75
76812
                                          MA   =           75
59107
                                          Ha   =            229
145  n
mi
                                          Hp   =            219
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19829279
33                 X    =         6019020
12
 Y    =        2952451
05  feet           Y    =          967355
19  meter
 Z    =        9747571
85                 Z    =         3000359
21
 XDOT =       5305
777688                 XDOT =        1578
465720
 YDOT =      18400
600199  feet/sec       YDOT =        5626
371533  meter/sec
 ZDOT =     -16278
009665                 ZDOT =       -4953
774986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13372363
65                 X    =        -4075896
44
 Y    =       14848368
68  feet           Y    =         4525782
77  meter
 Z    =        9881208
48                 Z    =         3011792
34
 XDOT =     -17248
780877                 XDOT =       -5257
428411
 YDOT =      -4666
629582  feet/sec       YDOT =       -1422
388697  meter/sec
 ZDOT =     -16242
910353                 ZDOT =       -4950
839076


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
48150674  
00016717  00000-0  10270-3 0  9125
2 25544  51
6424 212
2589 0007323  15
5885 344
5490 15
50088510  2442


Satellite: ISS
Catalog Number: 25544
Epoch time:      19343
48150674   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:       212
2589  deg
Eccentricity:     
0007323     
Arg of perigee:    15
5885  deg
Mean anomaly:     344
5490  deg
Mean motion:   15
50088510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             244
Checksum:              301


Coasting Arc #14 (Orbit 258)
---------------------------------------

Vector Time (GMT): 2019/344/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6206944
50                 A    =         6797920
38  meter
 Y    =        -691845
71  meter          E    =           
0011517
 Z    =       -2675711
60                 I    =           51
47621
 XDOT =      -1622
941675                 Wp   =           33
33762
 YDOT =      -5404
318952  meter/sec      RA   =          206
30276  deg
 ZDOT =       5182
215733                 TA   =          296
43931
                                          MA   =          296
55743
                                          Ha   =            229
115  n
mi
                                          Hp   =            219
685

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20363991
14                 X    =        -6185749
44
 Y    =       -2269835
00  feet           Y    =         -761137
31  meter
 Z    =       -8778581
36                 Z    =        -2705811
70
 XDOT =      -5324
611796                 XDOT =       -1587
561112
 YDOT =     -17730
705223  feet/sec       YDOT =       -5422
270638  meter/sec
 ZDOT =      17002
020121                 ZDOT =        5174
417239

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12830338
64                 X    =         3910687
22
 Y    =      -15899586
68  feet           Y    =        -4846194
02  meter
 Z    =       -8915903
24                 Z    =        -2717567
31
 XDOT =      16714
331606                 XDOT =        5094
528274
 YDOT =       4009
805058  feet/sec       YDOT =        1222
188582  meter/sec
 ZDOT =      16966
737036                 ZDOT =        5171
461449


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   19344
44854734  
00016717  00000-0  10270-3 0  9131
2 25544  51
6423 207
4676 0007336  17
4472 342
6930 15
50107925  2597


Satellite: ISS
Catalog Number: 25544
Epoch time:      19344
44854734   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:       207
4676  deg
Eccentricity:     
0007336     
Arg of perigee:    17
4472  deg
Mean anomaly:     342
6930  deg
Mean motion:   15
50107925  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             259
Checksum:              312


Coasting Arc #15 (Orbit 274)
---------------------------------------

Vector Time (GMT): 2019/345/10:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6367349
43                 A    =         6798733
75  meter
 Y    =         507345
57  meter          E    =           
0016162
 Z    =        2319604
08                 I    =           51
50912
 XDOT =       1561
470006                 Wp   =           80
25820
 YDOT =       5212
876779  meter/sec      RA   =          201
33968  deg
 ZDOT =      -5391
594112                 TA   =           73
88673
                                          MA   =           73
70887
                                          Ha   =            229
296  n
mi
                                          Hp   =            219
550

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20890254
04                 X    =         6349935
41
 Y    =        1664519
57  feet           Y    =          578452
07  meter
 Z    =        7610249
61                 Z    =         2350492
49
 XDOT =       5122
933092                 XDOT =        1529
251774
 YDOT =      17102
614104  feet/sec       YDOT =        5230
158859  meter/sec
 ZDOT =     -17688
957060                 ZDOT =       -5384
086485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12318349
04                 X    =        -3754632
79
 Y    =       16889830
87  feet           Y    =         5148020
45  meter
 Z    =        7751201
75                 Z    =         2362566
29
 XDOT =     -16086
127612                 XDOT =       -4903
051696
 YDOT =      -3578
340421  feet/sec       YDOT =       -1090
678160  meter/sec
 ZDOT =     -17654
983505                 ZDOT =       -5381
238972


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   19345
48005757  
00016717  00000-0  10270-3 0  9140
2 25544  51
6422 202
3571 0007338  21
8599 338
2863 15
50093296  2754


Satellite: ISS
Catalog Number: 25544
Epoch time:      19345
48005757   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       202
3571  deg
Eccentricity:     
0007338     
Arg of perigee:    21
8599  deg
Mean anomaly:     338
2863  deg
Mean motion:   15
50093296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             275
Checksum:              318


Coasting Arc #16 (Orbit 285)
---------------------------------------

Vector Time (GMT): 2019/346/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6412682
71                 A    =         6800901
29  meter
 Y    =       -2226889
02  meter          E    =           
0019195
 Z    =         175276
71                 I    =           51
53475
 XDOT =       1719
986948                 Wp   =           39
85852
 YDOT =      -4453
160253  meter/sec      RA   =          197
97485  deg
 ZDOT =       5999
899453                 TA   =          322
03062
                                          MA   =          322
16579
                                          Ha   =            229
230  n
mi
                                          Hp   =            219
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21038985
26                 X    =        -6388155
79
 Y    =       -7306066
32  feet           Y    =        -2298463
05  meter
 Z    =         575054
82                 Z    =          144185
18
 XDOT =       5643
001798                 XDOT =        1740
511147
 YDOT =     -14610
105818  feet/sec       YDOT =       -4433
812297  meter/sec
 ZDOT =      19684
709492                 ZDOT =        6008
303775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5948347
09                 X    =         1813056
19
 Y    =       21465732
02  feet           Y    =         6542755
12  meter
 Z    =         433255
06                 Z    =          132056
14
 XDOT =     -13586
135352                 XDOT =       -4141
054055
 YDOT =       3335
967164  feet/sec       YDOT =        1016
802792  meter/sec
 ZDOT =      19723
322030                 ZDOT =        6011
668555


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   19346
18921579  
00016717  00000-0  10270-3 0  9158
2 25544  51
6387 198
8420 0007151  26
7415 333
4103 15
50155742  2861


Satellite: ISS
Catalog Number: 25544
Epoch time:      19346
18921579   =   yrday
fracday
Element set:     915
Inclination:       51
6387  deg
RA of node:       198
8420  deg
Eccentricity:     
0007151     
Arg of perigee:    26
7415  deg
Mean anomaly:     333
4103  deg
Mean motion:   15
50155742  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             286
Checksum:              313


Coasting Arc #17 (Orbit 300)
---------------------------------------

Vector Time (GMT): 2019/347/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6483280
91                 A    =         6800906
12  meter
 Y    =        1969754
13  meter          E    =           
0010925
 Z    =        -578430
10                 I    =           51
56577
 XDOT =      -1867
504392                 Wp   =           98
93894
 YDOT =       4424
668460  meter/sec      RA   =          193
01549  deg
 ZDOT =      -5962
453509                 TA   =           87
29477
                                          MA   =           87
16972
                                          Ha   =            229
504  n
mi
                                          Hp   =            219
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21270606
67                 X    =         6463582
41
 Y    =        6462447
92  feet           Y    =         2042144
70  meter
 Z    =       -1897736
56                 Z    =         -546984
07
 XDOT =      -6126
982913                 XDOT =       -1887
881055
 YDOT =      14516
628806  feet/sec       YDOT =        4403
671730  meter/sec
 ZDOT =     -19561
855345                 ZDOT =       -5971
573989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7142644
60                 X    =        -2177078
07
 Y    =      -21064389
01  feet           Y    =        -6420425
77  meter
 Z    =       -1754277
25                 Z    =         -534703
71
 XDOT =      13754
689801                 XDOT =        4192
429451
 YDOT =      -3060
427033  feet/sec       YDOT =        -932
818160  meter/sec
 ZDOT =     -19603
741204                 ZDOT =       -5975
220319


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   19347
15625527  
00016717  00000-0  10270-3 0  9161
2 25544  51
6379 194
0494 0007506  28
6664 331
4898 15
50110653  3011


Satellite: ISS
Catalog Number: 25544
Epoch time:      19347
15625527   =   yrday
fracday
Element set:     916
Inclination:       51
6379  deg
RA of node:       194
0494  deg
Eccentricity:     
0007506     
Arg of perigee:    28
6664  deg
Mean anomaly:     331
4898  deg
Mean motion:   15
50110653  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             301
Checksum:              316


Coasting Arc #18 (Orbit 316)
---------------------------------------

Vector Time (GMT): 2019/348/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6516217
79                 A    =         6800600
14  meter
 Y    =       -1666064
43  meter          E    =           
0020291
 Z    =         928514
58                 I    =           51
59728
 XDOT =       1991
600466                 Wp   =           47
43134
 YDOT =      -4454
049020  meter/sec      RA   =          188
05969  deg
 ZDOT =       5915
829348                 TA   =          322
61863
                                          MA   =          322
75963
                                          Ha   =            229
413  n
mi
                                          Hp   =            219
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21378667
29                 X    =        -6501613
29
 Y    =       -5466090
64  feet           Y    =        -1738851
87  meter
 Z    =        3046307
66                 Z    =          896896
39
 XDOT =       6534
122263                 XDOT =        2012
523077
 YDOT =     -14613
021720  feet/sec       YDOT =       -4431
661498  meter/sec
 ZDOT =      19408
888937                 ZDOT =        5925
553915

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8372870
34                 X    =         2552050
88
 Y    =       20437193
78  feet           Y    =         6229256
67  meter
 Z    =        2902017
39                 Z    =          884534
90
 XDOT =     -14057
338999                 XDOT =       -4284
676927
 YDOT =       2963
052927  feet/sec       YDOT =         903
138532  meter/sec
 ZDOT =      19453
540269                 ZDOT =        5929
439074


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   19348
18775976  
00016717  00000-0  10270-3 0  9170
2 25544  51
6373 188
9392 0007226  32
9653 327
1947 15
50148821  3171


Satellite: ISS
Catalog Number: 25544
Epoch time:      19348
18775976   =   yrday
fracday
Element set:     917
Inclination:       51
6373  deg
RA of node:       188
9392  deg
Eccentricity:     
0007226     
Arg of perigee:    32
9653  deg
Mean anomaly:     327
1947  deg
Mean motion:   15
50148821  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             317
Checksum:              345


Coasting Arc #19 (Orbit 331)
---------------------------------------

Vector Time (GMT): 2019/349/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6521526
54                 A    =         6800326
82  meter
 Y    =        1404257
35  meter          E    =           
0009820
 Z    =       -1324963
95                 I    =           51
63037
 XDOT =      -2141
404810                 Wp   =           95
89143
 YDOT =       4494
413247  meter/sec      RA   =          183
10448  deg
 ZDOT =      -5814
865837                 TA   =           98
49587
                                          MA   =           98
38457
                                          Ha   =            229
613  n
mi
                                          Hp   =            219
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21396084
44                 X    =         6511774
94
 Y    =        4607143
55  feet           Y    =         1477131
34  meter
 Z    =       -4346994
59                 Z    =        -1293308
41
 XDOT =      -7025
606331                 XDOT =       -2163
258215
 YDOT =      14745
450285  feet/sec       YDOT =        4470
345229  meter/sec
 ZDOT =     -19077
643823                 ZDOT =       -5825
320345

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9419836
12                 X    =        -2871166
05
 Y    =      -19786872
33  feet           Y    =        -6031038
69  meter
 Z    =       -4202491
40                 Z    =        -1280919
38
 XDOT =      14447
120411                 XDOT =        4403
482301
 YDOT =      -2843
225487  feet/sec       YDOT =        -866
615129  meter/sec
 ZDOT =     -19125
636140                 ZDOT =       -5829
493895


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   19349
15479740  
00016717  00000-0  10270-3 0  9189
2 25544  51
6383 184
1466 0007483  35
1564 325
0079 15
50113115  3321


Satellite: ISS
Catalog Number: 25544
Epoch time:      19349
15479740   =   yrday
fracday
Element set:     918
Inclination:       51
6383  deg
RA of node:       184
1466  deg
Eccentricity:     
0007483     
Arg of perigee:    35
1564  deg
Mean anomaly:     325
0079  deg
Mean motion:   15
50113115  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             332
Checksum:              304


Coasting Arc #20 (Orbit 347)
---------------------------------------

Vector Time (GMT): 2019/350/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6487082
01                 A    =         6799836
68  meter
 Y    =       -1108454
00  meter          E    =           
0020803
 Z    =        1665416
66                 I    =           51
66306
 XDOT =       2260
906138                 Wp   =           55
42240
 YDOT =      -4591
725027  meter/sec      RA   =          178
15255  deg
 ZDOT =       5711
243400                 TA   =          322
80365
                                          MA   =          322
94759
                                          Ha   =            229
601  n
mi
                                          Hp   =            219
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21283077
48                 X    =        -6482294
44
 Y    =       -3636660
11  feet           Y    =        -1180970
59  meter
 Z    =        5463965
42                 Z    =         1633916
55
 XDOT =       7417
671055                 XDOT =        2284
342264
 YDOT =     -15064
714656  feet/sec       YDOT =       -4566
311689  meter/sec
 ZDOT =      18737
675198                 ZDOT =        5722
282276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10451782
84                 X    =         3185703
41
 Y    =       18934256
12  feet           Y    =         5771161
27  meter
 Z    =        5320129
90                 Z    =         1621575
59
 XDOT =     -14941
734416                 XDOT =       -4554
240650
 YDOT =       2931
602168  feet/sec       YDOT =         893
552341  meter/sec
 ZDOT =      18788
346791                 ZDOT =        5726
688102


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   19350
18629873  
00016717  00000-0  10270-3 0  9199
2 25544  51
6389 179
0360 0007348  39
1090 321
0590 15
50143187  3484


Satellite: ISS
Catalog Number: 25544
Epoch time:      19350
18629873   =   yrday
fracday
Element set:     919
Inclination:       51
6389  deg
RA of node:       179
0360  deg
Eccentricity:     
0007348     
Arg of perigee:    39
1090  deg
Mean anomaly:     321
0590  deg
Mean motion:   15
50143187  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             348
Checksum:              317


Coasting Arc #21 (Orbit 362)
---------------------------------------

Vector Time (GMT): 2019/351/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959319
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6428809
00                 A    =         6799312
73  meter
 Y    =         862736
53  meter          E    =           
0009377
 Z    =       -2047931
13                 I    =           51
69483
 XDOT =      -2391
091976                 Wp   =           87
06182
 YDOT =       4698
582826  meter/sec      RA   =          173
20187  deg
 ZDOT =      -5548
192067                 TA   =          115
49952
                                          MA   =          115
40250
                                          Ha   =            229
748  n
mi
                                          Hp   =            218
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21091893
05                 X    =         6428631
46
 Y    =        2830500
42  feet           Y    =          934627
24  meter
 Z    =       -6718934
15                 Z    =        -2016702
98
 XDOT =      -7844
789948                 XDOT =       -2416
505379
 YDOT =      15415
297986  feet/sec       YDOT =        4671
702447  meter/sec
 ZDOT =     -18202
729877                 ZDOT =       -5559
868219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11281107
80                 X    =        -3438481
66
 Y    =      -18097308
88  feet           Y    =        -5516059
75  meter
 Z    =       -6576304
36                 Z    =        -2004457
57
 XDOT =      15481
453861                 XDOT =        4718
747137
 YDOT =      -3042
623194  feet/sec       YDOT =        -927
391550  meter/sec
 ZDOT =     -18256
323250                 ZDOT =       -5564
527327


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   19351
15333299  
00016717  00000-0  10270-3 0  9203
2 25544  51
6392 174
2439 0007595  41
4621 318
7105 15
50117553  3632


Satellite: ISS
Catalog Number: 25544
Epoch time:      19351
15333299   =   yrday
fracday
Element set:     920
Inclination:       51
6392  deg
RA of node:       174
2439  deg
Eccentricity:     
0007595     
Arg of perigee:    41
4621  deg
Mean anomaly:     318
7105  deg
Mean motion:   15
50117553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             363
Checksum:              299
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