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

 
Date: November 6th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 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


311/22:43:23 807 1 0 1 5 1 5
N/A 0 7 -0 0 225 8
000/00:06:43 614 0 8 -0 0 223 7

312/03:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 9
000/00:00:00 000 0 0 0 0 223 6

317/14:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 3
000/00:00:00 000 0 0 0 0 223 6

Coasting Arc #1 (Orbit 3732)
---------------------------------------

Vector Time (GMT): 2019/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6417669
54                 A    =         6798565
36  meter
 Y    =          87241
45  meter          E    =           
0011385
 Z    =        2219845
18                 I    =           51
75953
 XDOT =      -1964
276837                 Wp   =          135
13262
 YDOT =      -4994
005168  meter/sec      RA   =           15
03806  deg
 ZDOT =      -5473
300744                 TA   =           20
27455
                                          MA   =           20
22938
                                          Ha   =            226
370  n
mi
                                          Hp   =            222
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21055346
27                 X    =        -6428951
04
 Y    =         286225
24  feet           Y    =           15411
48  meter
 Z    =        7282956
63                 Z    =         2188642
74
 XDOT =      -6444
477811                 XDOT =       -1881
699826
 YDOT =     -16384
531392  feet/sec       YDOT =       -5015
509432  meter/sec
 ZDOT =     -17957
023437                 ZDOT =       -5482
641977

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14845416
31                 X    =         4524882
89
 Y    =      -15002529
15  feet           Y    =        -4572770
89  meter
 Z    =        7140638
77                 Z    =         2176466
70
 XDOT =      14903
752418                 XDOT =        4542
663737
 YDOT =       6166
047896  feet/sec       YDOT =        1879
411399  meter/sec
 ZDOT =     -17999
128320                 ZDOT =       -5486
134312


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   19310
53656490  
00016717  00000-0  10270-3 0  9009
2 25544  51
6434  15
4762 0006228 235
3385 124
7179 15
50271819 37333


Satellite: ISS
Catalog Number: 25544
Epoch time:      19310
53656490   =   yrday
fracday
Element set:     900
Inclination:       51
6434  deg
RA of node:        15
4762  deg
Eccentricity:     
0006228     
Arg of perigee:   235
3385  deg
Mean anomaly:     124
7179  deg
Mean motion:   15
50271819  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3733
Checksum:              306


Coasting Arc #2 (Orbit 3747)
---------------------------------------

Vector Time (GMT): 2019/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6540190
44                 A    =         6799318
37  meter
 Y    =        -300633
82  meter          E    =           
0002797
 Z    =       -1827686
45                 I    =           51
72917
 XDOT =       1801
408434                 Wp   =          342
93072
 YDOT =       4847
433717  meter/sec      RA   =           10
09105  deg
 ZDOT =       5649
220113                 TA   =          357
04114
                                          MA   =          357
04279
                                          Ha   =            226
108  n
mi
                                          Hp   =            222
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21457317
72                 X    =         6551944
16
 Y    =        -986331
42  feet           Y    =         -227431
10  meter
 Z    =       -5996346
62                 Z    =        -1795887
60
 XDOT =       5910
132656                 XDOT =        1719
627928
 YDOT =      15903
653928  feet/sec       YDOT =        4867
121176  meter/sec
 ZDOT =      18534
186723                 ZDOT =        5657
772099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14361392
04                 X    =        -4377352
29
 Y    =       16026796
87  feet           Y    =         4884967
69  meter
 Z    =       -5851299
60                 Z    =        -1783476
12
 XDOT =     -14231
173925                 XDOT =       -4337
661812
 YDOT =      -5972
067397  feet/sec       YDOT =       -1820
286143  meter/sec
 ZDOT =      18572
702073                 ZDOT =        5660
959592


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   19311
50350625  
00016717  00000-0  10270-3 0  9019
2 25544  51
6434  10
6841 0006241 240
0806 119
9726 15
50237390 37480


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
50350625   =   yrday
fracday
Element set:     901
Inclination:       51
6434  deg
RA of node:        10
6841  deg
Eccentricity:     
0006241     
Arg of perigee:   240
0806  deg
Mean anomaly:     119
9726  deg
Mean motion:   15
50237390  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3748
Checksum:              283


Coasting Arc #3 (Orbit 3754)
---------------------------------------

Vector Time (GMT): 2019/311/22:46:45
614
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6028796
20                 A    =         6798129
65  meter
 Y    =       -1404666
02  meter          E    =           
0002214
 Z    =       -2807147
43                 I    =           51
70978
 XDOT =       3440
933972                 Wp   =          285
46220
 YDOT =       4548
561809  meter/sec      RA   =            7
86246  deg
 ZDOT =       5111
114168                 TA   =           42
78947
                                          MA   =           42
77224
                                          Ha   =            225
845  n
mi
                                          Hp   =            223
672

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19779515
10                 X    =         6057691
31
 Y    =       -4608484
31  feet           Y    =        -1337086
25  meter
 Z    =       -9209801
28                 Z    =        -2777791
08
 XDOT =      11289
153451                 XDOT =        3364
987510
 YDOT =      14923
103049  feet/sec       YDOT =        4586
616224  meter/sec
 ZDOT =      16768
747269                 ZDOT =        5127
644668

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15438353
90                 X    =         4705610
27
 Y    =      -13288155
93  feet           Y    =        -4050229
93  meter
 Z    =       -9075787
89                 Z    =        -2766300
15
 XDOT =      15855
096865                 XDOT =        4832
633524
 YDOT =       6910
117136  feet/sec       YDOT =        2106
203703  meter/sec
 ZDOT =      16843
674553                 ZDOT =        5133
952004


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   19311
95474502  
00016717  00000-0  10270-3 0  9020
2 25544  51
6452   8
4495 0006481 253
1292 106
9148 15
49999498 37554


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
95474502   =   yrday
fracday
Element set:     902
Inclination:       51
6452  deg
RA of node:         8
4495  deg
Eccentricity:     
0006481     
Arg of perigee:   253
1292  deg
Mean anomaly:     106
9148  deg
Mean motion:   15
49999498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3755
Checksum:              338


Coasting Arc #4 (Orbit 3757)
---------------------------------------

Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1867498
85                 A    =         6790820
59  meter
 Y    =       -4209122
76  meter          E    =           
0006173
 Z    =       -4996755
79                 I    =           51
67536
 XDOT =       7325
098313                 Wp   =           76
09440
 YDOT =       -766
082240  meter/sec      RA   =            7
01130  deg
 ZDOT =      -2093
099563                 TA   =          173
51659
                                          MA   =          173
50860
                                          Ha   =            225
852  n
mi
                                          Hp   =            223
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6126964
72                 X    =        -1796020
52
 Y    =      -13809457
87  feet           Y    =        -4229606
89  meter
 Z    =      -16393555
74                 Z    =        -5005653
86
 XDOT =      24032
474779                 XDOT =        7343
287745
 YDOT =      -2513
393176  feet/sec       YDOT =        -684
066157  meter/sec
 ZDOT =      -6867
124550                 ZDOT =       -2057
472150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13548884
36                 X    =        -4129699
95
 Y    =        6584100
93  feet           Y    =         2006833
96  meter
 Z    =      -16433710
49                 Z    =        -5008994
96
 XDOT =      -3030
748727                 XDOT =        -923
772212
 YDOT =     -22965
220700  feet/sec       YDOT =       -6999
799269  meter/sec
 ZDOT =      -6704
580094                 ZDOT =       -2043
556013


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   19312
14816645  
00016717  00000-0  10270-3 0  9031
2 25544  51
6410   7
4887 0006507 253
3699 106
6737 15
49986728 37580


Satellite: ISS
Catalog Number: 25544
Epoch time:      19312
14816645   =   yrday
fracday
Element set:     903
Inclination:       51
6410  deg
RA of node:         7
4887  deg
Eccentricity:     
0006507     
Arg of perigee:   253
3699  deg
Mean anomaly:     106
6737  deg
Mean motion:   15
49986728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3758
Checksum:              345


Coasting Arc #5 (Orbit 3773)
---------------------------------------

Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1818002
05                 A    =         6790502
57  meter
 Y    =        4103368
58  meter          E    =           
0004821
 Z    =        5098800
58                 I    =           51
64008
 XDOT =      -7377
287163                 Wp   =          204
96111
 YDOT =       1108
656762  meter/sec      RA   =            2
05740  deg
 ZDOT =       1734
522381                 TA   =          228
23147
                                          MA   =          228
27268
                                          Ha   =            225
653  n
mi
                                          Hp   =            223
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5964573
64                 X    =         1747214
19
 Y    =       13462495
33  feet           Y    =         4123303
06  meter
 Z    =       16728348
38                 Z    =         5107459
93
 XDOT =     -24203
698042                 XDOT =       -7397
561715
 YDOT =       3637
325334  feet/sec       YDOT =        1026
045398  meter/sec
 ZDOT =       5690
690227                 ZDOT =        1698
636249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13096942
09                 X    =         3991947
95
 Y    =       -6631461
94  feet           Y    =        -2021269
60  meter
 Z    =       16767420
17                 Z    =         5110709
67
 XDOT =       4570
308831                 XDOT =        1393
030132
 YDOT =      23031
289934  feet/sec       YDOT =        7019
937172  meter/sec
 ZDOT =       5526
946664                 ZDOT =        1684
613343


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   19313
17975342  
00016717  00000-0  10270-3 0  9046
2 25544  51
6405   2
3784 0006448 257
5006 102
5423 15
49944748 37747


Satellite: ISS
Catalog Number: 25544
Epoch time:      19313
17975342   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:         2
3784  deg
Eccentricity:     
0006448     
Arg of perigee:   257
5006  deg
Mean anomaly:     102
5423  deg
Mean motion:   15
49944748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3774
Checksum:              317


Coasting Arc #6 (Orbit 3788)
---------------------------------------

Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1748569
71                 A    =         6789994
74  meter
 Y    =       -4026841
61  meter          E    =           
0007529
 Z    =       -5186561
95                 I    =           51
60468
 XDOT =       7391
970292                 Wp   =           79
93864
 YDOT =      -1455
448791  meter/sec      RA   =          357
10082  deg
 ZDOT =      -1362
483754                 TA   =          176
93935
                                          MA   =          176
93475
                                          Ha   =            225
507  n
mi
                                          Hp   =            223
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5736777
28                 X    =        -1678216
37
 Y    =      -13211422
60  feet           Y    =        -4046002
04  meter
 Z    =      -17016279
37                 Z    =        -5194885
14
 XDOT =      24251
871038                 XDOT =        7414
314509
 YDOT =      -4775
094460  feet/sec       YDOT =       -1372
661639  meter/sec
 ZDOT =      -4470
091057                 ZDOT =       -1326
521146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12748027
72                 X    =        -3885598
85
 Y    =        6607650
13  feet           Y    =         2014011
76  meter
 Z    =      -17053821
08                 Z    =        -5198004
66
 XDOT =      -6121
342000                 XDOT =       -1865
785042
 YDOT =     -22919
781925  feet/sec       YDOT =       -6985
949531  meter/sec
 ZDOT =      -4305
978618                 ZDOT =       -1312
462283


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   19314
14686260  
00016717  00000-0  10270-3 0  9053
2 25544  51
6398 357
5875 0006419 259
5209 100
5218 15
49991847 37897


Satellite: ISS
Catalog Number: 25544
Epoch time:      19314
14686260   =   yrday
fracday
Element set:     905
Inclination:       51
6398  deg
RA of node:       357
5875  deg
Eccentricity:     
0006419     
Arg of perigee:   259
5209  deg
Mean anomaly:     100
5218  deg
Mean motion:   15
49991847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3789
Checksum:              354


Coasting Arc #7 (Orbit 3804)
---------------------------------------

Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1678595
86                 A    =         6789834
35  meter
 Y    =        3971823
48  meter          E    =           
0004214
 Z    =        5248177
23                 I    =           51
57062
 XDOT =      -7376
395695                 Wp   =          233
36440
 YDOT =       1809
469236  meter/sec      RA   =          352
14123  deg
 ZDOT =        987
978795                 TA   =          207
14680
                                          MA   =          207
16884
                                          Ha   =            225
288  n
mi
                                          Hp   =            223
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5507204
25                 X    =         1608563
57
 Y    =       13030916
93  feet           Y    =         3990203
12  meter
 Z    =       17218429
24                 Z    =         5256161
37
 XDOT =     -24200
773278                 XDOT =       -7400
880659
 YDOT =       5936
578857  feet/sec       YDOT =        1726
844260  meter/sec
 ZDOT =       3241
400247                 ZDOT =         952
086568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12474245
67                 X    =         3802150
08
 Y    =       -6579238
67  feet           Y    =        -2005351
95  meter
 Z    =       17254425
92                 Z    =         5259149
02
 XDOT =       7683
534597                 XDOT =        2341
941345
 YDOT =      22655
508716  feet/sec       YDOT =        6905
399057  meter/sec
 ZDOT =       3077
586374                 ZDOT =         938
048327


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   19315
17844541  
00016717  00000-0  10270-3 0  9066
2 25544  51
6400 352
4765 0006426 264
1473  95
8945 15
49950964 38053


Satellite: ISS
Catalog Number: 25544
Epoch time:      19315
17844541   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       352
4765  deg
Eccentricity:     
0006426     
Arg of perigee:   264
1473  deg
Mean anomaly:      95
8945  deg
Mean motion:   15
49950964  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3805
Checksum:              333


Coasting Arc #8 (Orbit 3819)
---------------------------------------

Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1601198
68                 A    =         6789487
21  meter
 Y    =       -3948193
21  meter          E    =           
0008407
 Z    =       -5293638
58                 I    =           51
53771
 XDOT =       7320
259712                 Wp   =           84
36809
 YDOT =      -2158
303746  meter/sec      RA   =          347
17970  deg
 ZDOT =       -604
481900                 TA   =          179
84459
                                          MA   =          179
84433
                                          Ha   =            225
224  n
mi
                                          Hp   =            223
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5253276
51                 X    =        -1531215
51
 Y    =      -12953389
81  feet           Y    =        -3965707
51  meter
 Z    =      -17367580
63                 Z    =        -5301246
95
 XDOT =      24016
600104                 XDOT =        7346
786755
 YDOT =      -7081
049036  feet/sec       YDOT =       -2076
295095  meter/sec
 ZDOT =      -1983
208334                 ZDOT =        -568
857397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12310252
38                 X    =        -3752164
92
 Y    =        6530922
39  feet           Y    =         1990625
14  meter
 Z    =      -17401862
49                 Z    =        -5304087
69
 XDOT =      -9207
427928                 XDOT =       -2806
424032
 YDOT =     -22206
075794  feet/sec       YDOT =       -6768
411902  meter/sec
 ZDOT =      -1820
590990                 ZDOT =        -554
916134


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   19316
14554916  
00016717  00000-0  10270-3 0  9079
2 25544  51
6407 347
6856 0006277 266
9013  93
1419 15
50005374 38203


Satellite: ISS
Catalog Number: 25544
Epoch time:      19316
14554916   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       347
6856  deg
Eccentricity:     
0006277     
Arg of perigee:   266
9013  deg
Mean anomaly:      93
1419  deg
Mean motion:   15
50005374  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3820
Checksum:              316


Coasting Arc #9 (Orbit 3835)
---------------------------------------

Vector Time (GMT): 2019/317/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1526925
65                 A    =         6789535
84  meter
 Y    =        3947271
50  meter          E    =           
0003795
 Z    =        5312278
50                 I    =           51
50367
 XDOT =      -7235
101029                 Wp   =          265
51467
 YDOT =       2503
782339  meter/sec      RA   =          342
21505  deg
 ZDOT =        219
026362                 TA   =          182
39048
                                          MA   =          182
39229
                                          Ha   =            225
230  n
mi
                                          Hp   =            223
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5009598
60                 X    =         1456867
77
 Y    =       12950365
81  feet           Y    =         3963954
68  meter
 Z    =       17428735
25                 Z    =         5319525
98
 XDOT =     -23737
208101                 XDOT =       -7263
625259
 YDOT =       8214
508985  feet/sec       YDOT =        2422
714831  meter/sec
 ZDOT =        718
590427                 ZDOT =         183
810751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12224141
40                 X    =         3725918
30
 Y    =       -6499217
38  feet           Y    =        -1980961
46  meter
 Z    =       17461368
95                 Z    =         5322225
26
 XDOT =      10693
285484                 XDOT =        3259
313415
 YDOT =      21612
639274  feet/sec       YDOT =        6587
532451  meter/sec
 ZDOT =        557
810858                 ZDOT =         170
020750


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   19317
17712723  
00016717  00000-0  10270-3 0  9086
2 25544  51
6393 342
5744 0006220 270
8834  89
1604 15
49956428 38361


Satellite: ISS
Catalog Number: 25544
Epoch time:      19317
17712723   =   yrday
fracday
Element set:     908
Inclination:       51
6393  deg
RA of node:       342
5744  deg
Eccentricity:     
0006220     
Arg of perigee:   270
8834  deg
Mean anomaly:      89
1604  deg
Mean motion:   15
49956428  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3836
Checksum:              331


Coasting Arc #10 (Orbit 3842)
---------------------------------------

Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2093549
43                 A    =         6792829
37  meter
 Y    =       -4612182
70  meter          E    =           
0003813
 Z    =       -4530073
28                 I    =           51
49955
 XDOT =       6984
087360                 Wp   =          135
17851
 YDOT =         86
402123  meter/sec      RA   =          339
76519  deg
 ZDOT =       3138
661306                 TA   =          166
41044
                                          MA   =          166
40017
                                          Ha   =            225
326  n
mi
                                          Hp   =            223
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6868600
49                 X    =         2166973
82
 Y    =      -15131833
00  feet           Y    =        -4588360
34  meter
 Z    =      -14862445
14                 Z    =        -4519725
24
 XDOT =      22913
672441                 XDOT =        6967
355796
 YDOT =        283
471533  feet/sec       YDOT =         164
409381  meter/sec
 ZDOT =      10297
445230                 ZDOT =        3172
547737

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15586008
43                 X    =         4750615
37
 Y    =        5885591
71  feet           Y    =         1793928
35  meter
 Z    =      -14814805
76                 Z    =        -4515552
80
 XDOT =       1754
792164                 XDOT =         534
860652
 YDOT =      21670
350802  feet/sec       YDOT =        6605
122925  meter/sec
 ZDOT =      10451
898045                 ZDOT =        3185
738524


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   19317
62843943  
00016717  00000-0  10270-3 0  9096
2 25544  51
6397 340
3427 0006363 275
5946  84
4479 15
49976566 38434


Satellite: ISS
Catalog Number: 25544
Epoch time:      19317
62843943   =   yrday
fracday
Element set:     909
Inclination:       51
6397  deg
RA of node:       340
3427  deg
Eccentricity:     
0006363     
Arg of perigee:   275
5946  deg
Mean anomaly:      84
4479  deg
Mean motion:   15
49976566  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3843
Checksum:              364


Coasting Arc #11 (Orbit 3858)
---------------------------------------

Vector Time (GMT): 2019/318/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2086665
58                 A    =         6793459
29  meter
 Y    =        4796559
10  meter          E    =           
0004939
 Z    =        4334732
95                 I    =           51
47110
 XDOT =      -6829
684495                 Wp   =           35
35428
 YDOT =        165
091666  meter/sec      RA   =          334
79965  deg
 ZDOT =      -3464
443203                 TA   =           89
99447
                                          MA   =           89
93787
                                          Ha   =            225
456  n
mi
                                          Hp   =            223
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6846015
70                 X    =        -2161203
30
 Y    =       15736742
44  feet           Y    =         4772807
42  meter
 Z    =       14221564
81                 Z    =         4324415
78
 XDOT =     -22407
101362                 XDOT =       -6814
194211
 YDOT =        541
639325  feet/sec       YDOT =          88
804196  meter/sec
 ZDOT =     -11366
283476                 ZDOT =       -3497
582499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16285134
64                 X    =        -4963709
04
 Y    =       -5536841
07  feet           Y    =        -1687629
16  meter
 Z    =       14174049
52                 Z    =         4320250
29
 XDOT =      -2898
347433                 XDOT =        -883
416298
 YDOT =     -21009
126391  feet/sec       YDOT =       -6403
581724  meter/sec
 ZDOT =     -11517
350967                 ZDOT =       -3510
488575


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   19318
66001332  
00016717  00000-0  10270-3 0  9101
2 25544  51
6398 335
2319 0006477 279
4698  80
5720 15
50008757 38594


Satellite: ISS
Catalog Number: 25544
Epoch time:      19318
66001332   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       335
2319  deg
Eccentricity:     
0006477     
Arg of perigee:   279
4698  deg
Mean anomaly:      80
5720  deg
Mean motion:   15
50008757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3859
Checksum:              329


Coasting Arc #12 (Orbit 3873)
---------------------------------------

Vector Time (GMT): 2019/319/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2046173
04                 A    =         6794254
18  meter
 Y    =       -4994679
77  meter          E    =           
0001172
 Z    =       -4127826
71                 I    =           51
44471
 XDOT =       6654
126839                 Wp   =          137
00986
 YDOT =       -391
017341  meter/sec      RA   =          329
83240  deg
 ZDOT =       3771
392500                 TA   =          172
02010
                                          MA   =          172
01824
                                          Ha   =            225
734  n
mi
                                          Hp   =            223
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6713166
13                 X    =         2121924
06
 Y    =      -16386744
64  feet           Y    =        -4971374
08  meter
 Z    =      -13542738
56                 Z    =        -4117703
41
 XDOT =      21831
124801                 XDOT =        6639
685013
 YDOT =      -1282
865292  feet/sec       YDOT =        -316
687293  meter/sec
 ZDOT =      12373
334975                 ZDOT =        3803
681379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17009966
83                 X    =         5184637
89
 Y    =        5051172
02  feet           Y    =         1539597
23  meter
 Z    =      -13496090
42                 Z    =        -4113608
36
 XDOT =       3920
443702                 XDOT =        1194
951240
 YDOT =      20252
906587  feet/sec       YDOT =        6173
085928  meter/sec
 ZDOT =      12520
545906                 ZDOT =        3816
262392


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   19319
62711147  
00016717  00000-0  10270-3 0  9111
2 25544  51
6407 330
4406 0006426 283
9604  76
0832 15
49988351 38746


Satellite: ISS
Catalog Number: 25544
Epoch time:      19319
62711147   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       330
4406  deg
Eccentricity:     
0006426     
Arg of perigee:   283
9604  deg
Mean anomaly:      76
0832  deg
Mean motion:   15
49988351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3874
Checksum:              321


Coasting Arc #13 (Orbit 3889)
---------------------------------------

Vector Time (GMT): 2019/320/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1990500
20                 A    =         6794961
09  meter
 Y    =        5199558
40  meter          E    =           
0006194
 Z    =        3894125
78                 I    =           51
41876
 XDOT =      -6463
684481                 Wp   =           52
65934
 YDOT =        579
278873  meter/sec      RA   =          324
86382  deg
 ZDOT =      -4069
257805                 TA   =           80
18636
                                          MA   =           80
11644
                                          Ha   =            225
947  n
mi
                                          Hp   =            223
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6530512
47                 X    =        -2067411
07
 Y    =       17058918
65  feet           Y    =         5176868
81  meter
 Z    =       12776003
21                 Z    =         3884270
20
 XDOT =     -21206
313914                 XDOT =       -6449
915202
 YDOT =       1900
521238  feet/sec       YDOT =         507
074776  meter/sec
 ZDOT =     -13350
583351                 ZDOT =       -4100
623030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17738584
44                 X    =        -5406720
54
 Y    =       -4489544
51  feet           Y    =        -1368413
17  meter
 Z    =       12730560
42                 Z    =         3880274
82
 XDOT =      -4784
770790                 XDOT =       -1458
398137
 YDOT =     -19433
571199  feet/sec       YDOT =       -5923
352501  meter/sec
 ZDOT =     -13493
601141                 ZDOT =       -4112
849628


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   19320
65868072  
00016717  00000-0  10270-3 0  9127
2 25544  51
6405 325
3301 0006499 288
5081  71
5363 15
50015968 38905


Satellite: ISS
Catalog Number: 25544
Epoch time:      19320
65868072   =   yrday
fracday
Element set:     912
Inclination:       51
6405  deg
RA of node:       325
3301  deg
Eccentricity:     
0006499     
Arg of perigee:   288
5081  deg
Mean anomaly:      71
5363  deg
Mean motion:   15
50015968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3890
Checksum:              316


Coasting Arc #14 (Orbit 3904)
---------------------------------------

Vector Time (GMT): 2019/321/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1892296
58                 A    =         6795786
52  meter
 Y    =       -5407480
01  meter          E    =           
0001741
 Z    =       -3653220
81                 I    =           51
39452
 XDOT =       6265
075306                 Wp   =          336
97283
 YDOT =       -741
864310  meter/sec      RA   =          319
89391  deg
 ZDOT =       4344
156139                 TA   =          339
55374
                                          MA   =          339
56071
                                          Ha   =            226
165  n
mi
                                          Hp   =            223
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6208322
12                 X    =         1970369
51
 Y    =      -17741076
15  feet           Y    =        -5385882
14  meter
 Z    =      -11985632
59                 Z    =        -3643839
50
 XDOT =      20554
709009                 XDOT =        6251
803637
 YDOT =      -2433
938025  feet/sec       YDOT =        -671
878425  meter/sec
 ZDOT =      14252
480772                 ZDOT =        4374
557632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18443210
58                 X    =         5621490
59
 Y    =        3764698
04  feet           Y    =         1147479
96  meter
 Z    =      -11942339
26                 Z    =        -3640025
01
 XDOT =       5524
661690                 XDOT =        1683
916883
 YDOT =      18577
074291  feet/sec       YDOT =        5662
292244  meter/sec
 ZDOT =      14391
120028                 ZDOT =        4386
413384


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   19321
62577609  
00016717  00000-0  10270-3 0  9139
2 25544  51
6403 320
5393 0006541 291
9010  68
1436 15
49993057 39051


Satellite: ISS
Catalog Number: 25544
Epoch time:      19321
62577609   =   yrday
fracday
Element set:     913
Inclination:       51
6403  deg
RA of node:       320
5393  deg
Eccentricity:     
0006541     
Arg of perigee:   291
9010  deg
Mean anomaly:      68
1436  deg
Mean motion:   15
49993057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3905
Checksum:              314


Coasting Arc #15 (Orbit 3920)
---------------------------------------

Vector Time (GMT): 2019/322/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1781080
67                 A    =         6796496
62  meter
 Y    =        5616264
11  meter          E    =           
0007087
 Z    =        3385053
90                 I    =           51
37347
 XDOT =      -6058
456315                 Wp   =           67
31195
 YDOT =        861
735013  meter/sec      RA   =          314
92265  deg
 ZDOT =      -4607
031731                 TA   =           73
07034
                                          MA   =           72
99267
                                          Ha   =            226
330  n
mi
                                          Hp   =            223
430

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5843440
52                 X    =        -1860193
87
 Y    =       18426063
35  feet           Y    =         5595904
19  meter
 Z    =       11105819
87                 Z    =         3376210
28
 XDOT =     -19876
825182                 XDOT =       -6045
263588
 YDOT =       2827
214609  feet/sec       YDOT =         794
059202  meter/sec
 ZDOT =     -15114
933501                 ZDOT =       -4636
429624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19124003
17                 X    =        -5828996
17
 Y    =       -2973856
51  feet           Y    =         -906431
46  meter
 Z    =       11064968
29                 Z    =         3372602
33
 XDOT =      -6090
753592                 XDOT =       -1856
461695
 YDOT =     -17697
539260  feet/sec       YDOT =       -5394
209966  meter/sec
 ZDOT =     -15249
007180                 ZDOT =       -4647
897388


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   19322
65734255  
00016717  00000-0  10270-3 0  9146
2 25544  51
6415 315
4289 0006583 295
9403  64
1069 15
50022117 39215


Satellite: ISS
Catalog Number: 25544
Epoch time:      19322
65734255   =   yrday
fracday
Element set:     914
Inclination:       51
6415  deg
RA of node:       315
4289  deg
Eccentricity:     
0006583     
Arg of perigee:   295
9403  deg
Mean anomaly:      64
1069  deg
Mean motion:   15
50022117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3921
Checksum:              305


Coasting Arc #16 (Orbit 3935)
---------------------------------------

Vector Time (GMT): 2019/323/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1624898
32                 A    =         6797280
16  meter
 Y    =       -5816443
23  meter          E    =           
0004728
 Z    =       -3112916
56                 I    =           51
35313
 XDOT =       5856
050060                 Wp   =          342
44196
 YDOT =       -956
367600  meter/sec      RA   =          309
94988  deg
 ZDOT =       4846
224703                 TA   =          341
63920
                                          MA   =          341
65626
                                          Ha   =            226
544  n
mi
                                          Hp   =            223
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5331031
23                 X    =         1704939
66
 Y    =      -19082819
00  feet           Y    =        -5797824
75  meter
 Z    =      -10212980
83                 Z    =        -3104829
27
 XDOT =      19212
762664                 XDOT =        5842
768738
 YDOT =      -3137
688975  feet/sec       YDOT =        -890
955651  meter/sec
 ZDOT =      15899
687347                 ZDOT =        4874
639132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19729542
56                 X    =         6013564
57
 Y    =        2020335
10  feet           Y    =          615798
14  meter
 Z    =      -10175571
19                 Z    =        -3101514
10
 XDOT =       6538
831414                 XDOT =        1993
035815
 YDOT =      16836
586355  feet/sec       YDOT =        5131
791521  meter/sec
 ZDOT =      16029
283214                 ZDOT =        4885
725523


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   19323
62443301  
00016717  00000-0  10270-3 0  9154
2 25544  51
6415 310
6379 0006634 299
9153  60
1338 15
50005462 39360


Satellite: ISS
Catalog Number: 25544
Epoch time:      19323
62443301   =   yrday
fracday
Element set:     915
Inclination:       51
6415  deg
RA of node:       310
6379  deg
Eccentricity:     
0006634     
Arg of perigee:   299
9153  deg
Mean anomaly:      60
1338  deg
Mean motion:   15
50005462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3936
Checksum:              298


Coasting Arc #17 (Orbit 3951)
---------------------------------------

Vector Time (GMT): 2019/324/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932146
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1458920
62                 A    =         6797971
58  meter
 Y    =        6011980
08  meter          E    =           
0007848
 Z    =        2813066
47                 I    =           51
33487
 XDOT =      -5653
676771                 Wp   =           79
56296
 YDOT =       1006
094677  meter/sec      RA   =          304
97642  deg
 ZDOT =      -5068
812779                 TA   =           68
42297
                                          MA   =           68
33935
                                          Ha   =            226
730  n
mi
                                          Hp   =            223
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4786484
97                 X    =        -1539704
35
 Y    =       19724344
08  feet           Y    =         5995213
60  meter
 Z    =        9229220
70                 Z    =         2805783
52
 XDOT =     -18548
808304                 XDOT =       -5639
885307
 YDOT =       3300
835555  feet/sec       YDOT =         942
948568  meter/sec
 ZDOT =     -16629
963187                 ZDOT =       -5096
242954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20286598
60                 X    =        -6183355
25
 Y    =       -1017780
47  feet           Y    =         -310219
49  meter
 Z    =        9195474
02                 Z    =         2802780
48
 XDOT =      -6812
358462                 XDOT =       -2076
406859
 YDOT =     -15995
645719  feet/sec       YDOT =       -4875
472815  meter/sec
 ZDOT =     -16755
072025                 ZDOT =       -5106
945953


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   19324
65599479  
00016717  00000-0  10270-3 0  9167
2 25544  51
6413 305
5277 0006604 304
5998  55
4529 15
50025221 39527


Satellite: ISS
Catalog Number: 25544
Epoch time:      19324
65599479   =   yrday
fracday
Element set:     916
Inclination:       51
6413  deg
RA of node:       305
5277  deg
Eccentricity:     
0006604     
Arg of perigee:   304
5998  deg
Mean anomaly:      55
4529  deg
Mean motion:   15
50025221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3952
Checksum:              328
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