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

 
Date: November 11th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 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


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 3809)
---------------------------------------

Vector Time (GMT): 2019/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6612352
48                 A    =         6801362
03  meter
 Y    =       -1500575
73  meter          E    =           
0008091
 Z    =        -458931
19                 I    =           51
60004
 XDOT =       1449
107127                 Wp   =            7
83322
 YDOT =       4562
232768  meter/sec      RA   =          350
28927  deg
 ZDOT =       5982
030275                 TA   =          347
22357
                                          MA   =          347
24406
                                          Ha   =            225
252  n
mi
                                          Hp   =            223
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21694069
81                 X    =         6630870
20
 Y    =       -4923148
73  feet           Y    =        -1426528
19  meter
 Z    =       -1505679
74                 Z    =         -426764
98
 XDOT =       4754
288475                 XDOT =        1368
924999
 YDOT =      14967
955276  feet/sec       YDOT =        4577
989306  meter/sec
 ZDOT =      19626
083579                 ZDOT =        5988
875000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10368487
97                 X    =        -3160315
13
 Y    =       19692257
63  feet           Y    =         6002200
12  meter
 Z    =       -1358887
97                 Z    =         -414189
05
 XDOT =     -12942
925635                 XDOT =       -3945
003733
 YDOT =      -5463
433878  feet/sec       YDOT =       -1665
254646  meter/sec
 ZDOT =      19656
824114                 ZDOT =        5991
399990


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
50080136  
00016717  00000-0  10270-3 0  9009
2 25544  51
6432 350
8820 0006364 267
3689  92
6733 15
49972798 38102


Satellite: ISS
Catalog Number: 25544
Epoch time:      19315
50080136   =   yrday
fracday
Element set:     900
Inclination:       51
6432  deg
RA of node:       350
8820  deg
Eccentricity:     
0006364     
Arg of perigee:   267
3689  deg
Mean anomaly:      92
6733  deg
Mean motion:   15
49972798  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3810
Checksum:              325


Coasting Arc #2 (Orbit 3825)
---------------------------------------

Vector Time (GMT): 2019/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6550473
00                 A    =         6801335
26  meter
 Y    =        1805324
81  meter          E    =           
0008759
 Z    =         110873
67                 I    =           51
56773
 XDOT =      -1361
713601                 Wp   =          163
08418
 YDOT =      -4565
501582  meter/sec      RA   =          345
33357  deg
 ZDOT =      -6000
589812                 TA   =           15
72237
                                          MA   =           15
69519
                                          Ha   =            225
148  n
mi
                                          Hp   =            223
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21491053
14                 X    =        -6570712
39
 Y    =        5922981
65  feet           Y    =         1731959
62  meter
 Z    =         363758
76                 Z    =           79003
88
 XDOT =      -4467
564307                 XDOT =       -1281
411230
 YDOT =     -14978
679732  feet/sec       YDOT =       -4580
280019  meter/sec
 ZDOT =     -19686
974450                 ZDOT =       -6007
009816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9123263
93                 X    =         2780770
85
 Y    =      -20342020
52  feet           Y    =        -6200247
85  meter
 Z    =         218296
87                 Z    =           66536
89
 XDOT =      12825
792422                 XDOT =        3909
301530
 YDOT =       5534
174455  feet/sec       YDOT =        1686
816374  meter/sec
 ZDOT =     -19715
774735                 ZDOT =       -6009
368139


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
53237707  
00016717  00000-0  10270-3 0  9012
2 25544  51
6433 345
7717 0006330 270
5076  89
5349 15
50006661 38264


Satellite: ISS
Catalog Number: 25544
Epoch time:      19316
53237707   =   yrday
fracday
Element set:     901
Inclination:       51
6433  deg
RA of node:       345
7717  deg
Eccentricity:     
0006330     
Arg of perigee:   270
5076  deg
Mean anomaly:      89
5349  deg
Mean motion:   15
50006661  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3826
Checksum:              310


Coasting Arc #3 (Orbit 3841)
---------------------------------------

Vector Time (GMT): 2019/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6455442
81                 A    =         6801357
88  meter
 Y    =       -2109381
59  meter          E    =           
0009480
 Z    =         228121
92                 I    =           51
53481
 XDOT =       1287
947667                 Wp   =           18
64040
 YDOT =       4596
312902  meter/sec      RA   =          340
37552  deg
 ZDOT =       5993
993133                 TA   =          343
81696
                                          MA   =          343
84721
                                          Ha   =            225
305  n
mi
                                          Hp   =            223
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21179274
31                 X    =         6477442
62
 Y    =       -6920543
27  feet           Y    =        -2037069
28  meter
 Z    =         748431
49                 Z    =          259534
27
 XDOT =       4225
550089                 XDOT =        1207
338299
 YDOT =      15079
766739  feet/sec       YDOT =        4610
264587  meter/sec
 ZDOT =      19665
331801                 ZDOT =        6000
054153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7793102
32                 X    =        -2375337
59
 Y    =       20868347
36  feet           Y    =         6360672
27  meter
 Z    =         891831
87                 Z    =          271830
35
 XDOT =     -12820
140959                 XDOT =       -3907
578964
 YDOT =      -5636
239363  feet/sec       YDOT =       -1717
925758  meter/sec
 ZDOT =      19692
490096                 ZDOT =        6002
270981


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
56395313  
00016717  00000-0  10270-3 0  9025
2 25544  51
6426 340
6614 0006282 275
4802  84
5631 15
49989463 38428


Satellite: ISS
Catalog Number: 25544
Epoch time:      19317
56395313   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:       340
6614  deg
Eccentricity:     
0006282     
Arg of perigee:   275
4802  deg
Mean anomaly:      84
5631  deg
Mean motion:   15
49989463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3842
Checksum:              327


Coasting Arc #4 (Orbit 3842)
---------------------------------------

Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2101465
26                 A    =         6792841
26  meter
 Y    =       -4612075
60  meter          E    =           
0003748
 Z    =       -4526474
92                 I    =           51
49960
 XDOT =       6981
075738                 Wp   =          134
88743
 YDOT =         93
039020  meter/sec      RA   =          339
76470  deg
 ZDOT =       3145
255771                 TA   =          166
77514
                                          MA   =          166
76531
                                          Ha   =            225
340  n
mi
                                          Hp   =            223
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6894571
07                 X    =         2174870
38
 Y    =      -15131481
63  feet           Y    =        -4588164
83  meter
 Z    =      -14850639
49                 Z    =        -4516088
47
 XDOT =      22903
791792                 XDOT =        6964
238149
 YDOT =        305
246130  feet/sec       YDOT =         171
012007  meter/sec
 ZDOT =      10319
080615                 ZDOT =        3179
127315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15587480
81                 X    =         4751064
15
 Y    =        5911442
48  feet           Y    =         1801807
67  meter
 Z    =      -14802825
06                 Z    =        -4511901
08
 XDOT =       1734
249173                 XDOT =         528
599148
 YDOT =      21661
775648  feet/sec       YDOT =        6602
509218  meter/sec
 ZDOT =      10473
464894                 ZDOT =        3192
312100


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
62842611  
00016717  00000-0  10270-3 0  9031
2 25544  51
6397 340
3424 0006379 276
0674  83
9750 15
49977217 38432


Satellite: ISS
Catalog Number: 25544
Epoch time:      19317
62842611   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       340
3424  deg
Eccentricity:     
0006379     
Arg of perigee:   276
0674  deg
Mean anomaly:      83
9750  deg
Mean motion:   15
49977217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3843
Checksum:              337


Coasting Arc #5 (Orbit 3858)
---------------------------------------

Vector Time (GMT): 2019/318/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2094614
11                 A    =         6793474
57  meter
 Y    =        4796780
99  meter          E    =           
0004983
 Z    =        4330701
47                 I    =           51
47115
 XDOT =      -6826
566550                 Wp   =           35
15325
 YDOT =        158
049381  meter/sec      RA   =          334
79917  deg
 ZDOT =      -3470
851217                 TA   =           90
27100
                                          MA   =           90
21389
                                          Ha   =            225
480  n
mi
                                          Hp   =            223
625

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6872093
52                 X    =        -2169134
13
 Y    =       15737470
45  feet           Y    =         4772940
53  meter
 Z    =       14208338
16                 Z    =         4320345
73
 XDOT =     -22396
871884                 XDOT =       -6810
966622
 YDOT =        518
534714  feet/sec       YDOT =          81
797391  meter/sec
 ZDOT =     -11387
307141                 ZDOT =       -3503
975100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16288135
16                 X    =        -4964623
60
 Y    =       -5562665
44  feet           Y    =        -1695500
43  meter
 Z    =       14160647
05                 Z    =         4316165
22
 XDOT =      -2876
305118                 XDOT =        -876
697800
 YDOT =     -21000
599959  feet/sec       YDOT =       -6400
982868  meter/sec
 ZDOT =     -11538
303664                 ZDOT =       -3516
874957


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
65999985  
00016717  00000-0  10270-3 0  9043
2 25544  51
6399 335
2316 0006495 279
9380  80
1037 15
50008655 38599


Satellite: ISS
Catalog Number: 25544
Epoch time:      19318
65999985   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       335
2316  deg
Eccentricity:     
0006495     
Arg of perigee:   279
9380  deg
Mean anomaly:      80
1037  deg
Mean motion:   15
50008655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3859
Checksum:              356


Coasting Arc #6 (Orbit 3873)
---------------------------------------

Vector Time (GMT): 2019/319/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2053600
79                 A    =         6794271
87  meter
 Y    =       -4995110
38  meter          E    =           
0001105
 Z    =       -4123574
47                 I    =           51
44476
 XDOT =       6651
220114                 Wp   =          135
52300
 YDOT =       -383
926122  meter/sec      RA   =          329
83194  deg
 ZDOT =       3777
320170                 TA   =          173
57951
                                          MA   =          173
57809
                                          Ha   =            225
763  n
mi
                                          Hp   =            223
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6737535
40                 X    =         2129335
42
 Y    =      -16388157
42  feet           Y    =        -4971721
73  meter
 Z    =      -13528787
63                 Z    =        -4113415
13
 XDOT =      21821
588302                 XDOT =        6636
670414
 YDOT =      -1259
600137  feet/sec       YDOT =        -309
629183  meter/sec
 ZDOT =      12392
782709                 ZDOT =        3809
594667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17013912
68                 X    =         5185840
58
 Y    =        5075165
26  feet           Y    =         1546910
37  meter
 Z    =      -13481975
17                 Z    =        -4109306
03
 XDOT =       3898
042599                 XDOT =        1188
123384
 YDOT =      20245
440527  feet/sec       YDOT =        6170
810273  meter/sec
 ZDOT =      12539
927370                 ZDOT =        3822
169862


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
62709836  
00016717  00000-0  10270-3 0  9056
2 25544  51
6408 330
4404 0006446 284
4317  75
6118 15
49987373 38749


Satellite: ISS
Catalog Number: 25544
Epoch time:      19319
62709836   =   yrday
fracday
Element set:     905
Inclination:       51
6408  deg
RA of node:       330
4404  deg
Eccentricity:     
0006446     
Arg of perigee:   284
4317  deg
Mean anomaly:      75
6118  deg
Mean motion:   15
49987373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3874
Checksum:              339


Coasting Arc #7 (Orbit 3889)
---------------------------------------

Vector Time (GMT): 2019/320/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1997326
91                 A    =         6794980
58  meter
 Y    =        5200207
61  meter          E    =           
0006228
 Z    =        3889827
98                 I    =           51
41882
 XDOT =      -6460
975749                 Wp   =           52
41229
 YDOT =        572
342677  meter/sec      RA   =          324
86337  deg
 ZDOT =      -4074
476880                 TA   =           80
50194
                                          MA   =           80
43155
                                          Ha   =            225
977  n
mi
                                          Hp   =            223
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6552909
82                 X    =        -2074223
66
 Y    =       17061048
58  feet           Y    =         5177441
75  meter
 Z    =       12761902
83                 Z    =         3879939
28
 XDOT =     -21197
426998                 XDOT =       -6447
103757
 YDOT =       1877
764687  feet/sec       YDOT =         500
169445  meter/sec
 ZDOT =     -13367
706298                 ZDOT =       -4105
828697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17743413
93                 X    =        -5408192
57
 Y    =       -4511420
78  feet           Y    =        -1375081
05  meter
 Z    =       12716308
99                 Z    =         3875930
98
 XDOT =      -4762
681397                 XDOT =       -1451
665290
 YDOT =     -19427
055530  feet/sec       YDOT =       -5921
366526  meter/sec
 ZDOT =     -13510
662282                 ZDOT =       -4118
049864


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
65866855  
00016717  00000-0  10270-3 0  9067
2 25544  51
6405 325
3298 0006521 288
9754  71
0690 15
50014194 38905


Satellite: ISS
Catalog Number: 25544
Epoch time:      19320
65866855   =   yrday
fracday
Element set:     906
Inclination:       51
6405  deg
RA of node:       325
3298  deg
Eccentricity:     
0006521     
Arg of perigee:   288
9754  deg
Mean anomaly:      71
0690  deg
Mean motion:   15
50014194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3890
Checksum:              326


Coasting Arc #8 (Orbit 3904)
---------------------------------------

Vector Time (GMT): 2019/321/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1898045
42                 A    =         6795806
63  meter
 Y    =       -5408157
90  meter          E    =           
0001813
 Z    =       -3649192
17                 I    =           51
39456
 XDOT =       6262
860660                 Wp   =          337
52274
 YDOT =       -735
536805  meter/sec      RA   =          319
89349  deg
 ZDOT =       4348
486715                 TA   =          339
06356
                                          MA   =          339
07098
                                          Ha   =            226
197  n
mi
                                          Hp   =            223
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6227183
14                 X    =         1976105
93
 Y    =      -17743300
18  feet           Y    =        -5386495
81  meter
 Z    =      -11972415
25                 Z    =        -3639782
96
 XDOT =      20547
443111                 XDOT =        6249
497364
 YDOT =      -2413
178493  feet/sec       YDOT =        -665
576198  meter/sec
 ZDOT =      14266
688697                 ZDOT =        4378
877227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18448018
72                 X    =         5622956
10
 Y    =        3782978
83  feet           Y    =         1153051
95  meter
 Z    =      -11928994
71                 Z    =        -3635957
59
 XDOT =       5504
413256                 XDOT =        1677
745160
 YDOT =      18572
315949  feet/sec       YDOT =        5660
841901  meter/sec
 ZDOT =      14405
277281                 ZDOT =        4390
728515


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
62576530  
00016717  00000-0  10270-3 0  9074
2 25544  51
6404 320
5390 0006564 292
3692  67
6753 15
49990430 39053


Satellite: ISS
Catalog Number: 25544
Epoch time:      19321
62576530   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       320
5390  deg
Eccentricity:     
0006564     
Arg of perigee:   292
3692  deg
Mean anomaly:      67
6753  deg
Mean motion:   15
49990430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3905
Checksum:              321


Coasting Arc #9 (Orbit 3920)
---------------------------------------

Vector Time (GMT): 2019/322/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1785722
72                 A    =         6796516
87  meter
 Y    =        5616969
84  meter          E    =           
0007113
 Z    =        3381523
50                 I    =           51
37351
 XDOT =      -6056
682513                 Wp   =           67
00502
 YDOT =        856
298673  meter/sec      RA   =          314
92225  deg
 ZDOT =      -4610
313272                 TA   =           73
42706
                                          MA   =           73
34895
                                          Ha   =            226
362  n
mi
                                          Hp   =            223
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5858670
34                 X    =        -1864826
31
 Y    =       18428378
73  feet           Y    =         5596558
06  meter
 Z    =       11094237
20                 Z    =         3372657
35
 XDOT =     -19871
005620                 XDOT =       -6043
413187
 YDOT =       2809
378848  feet/sec       YDOT =         788
643127  meter/sec
 ZDOT =     -15125
699710                 ZDOT =       -4639
702363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19128651
11                 X    =        -5830412
86
 Y    =       -2988461
79  feet           Y    =         -910883
15  meter
 Z    =       11053282
88                 Z    =         3369040
62
 XDOT =      -6073
281810                 XDOT =       -1851
136296
 YDOT =     -17694
160309  feet/sec       YDOT =       -5393
180062  meter/sec
 ZDOT =     -15259
732742                 ZDOT =       -4651
166540


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
65733379  
00016717  00000-0  10270-3 0  9085
2 25544  51
6416 315
4287 0006606 296
4091  63
6381 15
50018677 39216


Satellite: ISS
Catalog Number: 25544
Epoch time:      19322
65733379   =   yrday
fracday
Element set:     908
Inclination:       51
6416  deg
RA of node:       315
4287  deg
Eccentricity:     
0006606     
Arg of perigee:   296
4091  deg
Mean anomaly:      63
6381  deg
Mean motion:   15
50018677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3921
Checksum:              325


Coasting Arc #10 (Orbit 3935)
---------------------------------------

Vector Time (GMT): 2019/323/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1628035
42                 A    =         6797299
58  meter
 Y    =       -5816954
78  meter          E    =           
0004794
 Z    =       -3110279
16                 I    =           51
35316
 XDOT =       5854
936710                 Wp   =          342
71585
 YDOT =       -952
371176  meter/sec      RA   =          309
94951  deg
 ZDOT =       4848
407451                 TA   =          341
40036
                                          MA   =          341
41788
                                          Ha   =            226
577  n
mi
                                          Hp   =            223
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5341323
56                 X    =         1708069
44
 Y    =      -19084497
31  feet           Y    =        -5798301
26  meter
 Z    =      -10204327
96                 Z    =        -3102176
65
 XDOT =      19209
109941                 XDOT =        5841
600179
 YDOT =      -3124
577348  feet/sec       YDOT =        -886
971986  meter/sec
 ZDOT =      15906
848593                 ZDOT =        4876
816338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19732963
82                 X    =         6014607
37
 Y    =        2030124
76  feet           Y    =          618782
03  meter
 Z    =      -10166848
91                 Z    =        -3098855
55
 XDOT =       6525
990886                 XDOT =        1989
122022
 YDOT =      16834
957789  feet/sec       YDOT =        5131
295134  meter/sec
 ZDOT =      16036
418821                 ZDOT =        4887
900457


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
62442667  
00016717  00000-0  10270-3 0  9091
2 25544  51
6416 310
6377 0006659 300
3842  59
6650 15
50001189 39360


Satellite: ISS
Catalog Number: 25544
Epoch time:      19323
62442667   =   yrday
fracday
Element set:     909
Inclination:       51
6416  deg
RA of node:       310
6377  deg
Eccentricity:     
0006659     
Arg of perigee:   300
3842  deg
Mean anomaly:      59
6650  deg
Mean motion:   15
50001189  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3936
Checksum:              315


Coasting Arc #11 (Orbit 3951)
---------------------------------------

Vector Time (GMT): 2019/324/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1460561
73                 A    =         6797990
21  meter
 Y    =        6012325
48  meter          E    =           
0007867
 Z    =        2811593
38                 I    =           51
33489
 XDOT =      -5653
098402                 Wp   =           79
18311
 YDOT =       1003
899015  meter/sec      RA   =          304
97609  deg
 ZDOT =      -5069
826418                 TA   =           68
82183
                                          MA   =           68
73779
                                          Ha   =            226
764  n
mi
                                          Hp   =            223
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4791869
18                 X    =        -1541342
04
 Y    =       19725477
28  feet           Y    =         5995540
67  meter
 Z    =        9224387
72                 Z    =         2804302
47
 XDOT =     -18546
910768                 XDOT =       -5639
277505
 YDOT =       3293
631940  feet/sec       YDOT =         940
759539  meter/sec
 ZDOT =     -16633
288773                 ZDOT =       -5097
253712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20288726
38                 X    =        -6184003
80
 Y    =       -1022819
72  feet           Y    =         -311755
45  meter
 Z    =        9190604
72                 Z    =         2801296
32
 XDOT =      -6805
288675                 XDOT =       -2074
251988
 YDOT =     -15994
972425  feet/sec       YDOT =       -4875
267595  meter/sec
 ZDOT =     -16758
384278                 ZDOT =       -5107
955528


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
65599159  
00016717  00000-0  10270-3 0  9106
2 25544  51
6414 305
5275 0006632 305
0724  54
9804 15
50020059 39524


Satellite: ISS
Catalog Number: 25544
Epoch time:      19324
65599159   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       305
5275  deg
Eccentricity:     
0006632     
Arg of perigee:   305
0724  deg
Mean anomaly:      54
9804  deg
Mean motion:   15
50020059  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3952
Checksum:              304


Coasting Arc #12 (Orbit 3966)
---------------------------------------

Vector Time (GMT): 2019/325/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1246652
78                 A    =         6798682
03  meter
 Y    =       -6186610
25  meter          E    =           
0007649
 Z    =       -2515318
77                 I    =           51
31828
 XDOT =       5468
053963                 Wp   =          350
38843
 YDOT =      -1037
394326  meter/sec      RA   =          300
00154  deg
 ZDOT =       5266
718959                 TA   =          341
29886
                                          MA   =          341
32695
                                          Ha   =            226
894  n
mi
                                          Hp   =            223
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4090068
17                 X    =         1327958
78
 Y    =      -20297277
71  feet           Y    =        -6172214
63  meter
 Z    =       -8252358
16                 Z    =        -2509065
57
 XDOT =      17939
809591                 XDOT =        5453
664890
 YDOT =      -3403
524690  feet/sec       YDOT =        -976
327254  meter/sec
 ZDOT =      17279
261676                 ZDOT =        5293
246082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20716368
28                 X    =         6314349
05
 Y    =        -137518
48  feet           Y    =          -41915
63  meter
 Z    =       -8223304
03                 Z    =        -2506463
07
 XDOT =       7001
414261                 XDOT =        2134
031067
 YDOT =      15224
468256  feet/sec       YDOT =        4640
417924  meter/sec
 ZDOT =      17400
251272                 ZDOT =        5303
596588


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   19325
62308272  
00016717  00000-0  10270-3 0  9119
2 25544  51
6408 300
7367 0006687 307
8743  52
1802 15
50007439 39678


Satellite: ISS
Catalog Number: 25544
Epoch time:      19325
62308272   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:       300
7367  deg
Eccentricity:     
0006687     
Arg of perigee:   307
8743  deg
Mean anomaly:      52
1802  deg
Mean motion:   15
50007439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3967
Checksum:              311


Coasting Arc #13 (Orbit 3982)
---------------------------------------

Vector Time (GMT): 2019/326/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1028551
35                 A    =         6799278
24  meter
 Y    =        6351462
02  meter          E    =           
0008065
 Z    =        2190856
66                 I    =           51
30578
 XDOT =      -5290
384147                 Wp   =           90
42648
 YDOT =       1026
623801  meter/sec      RA   =          295
02577  deg
 ZDOT =      -5442
573832                 TA   =           65
18134
                                          MA   =           65
09748
                                          Ha   =            227
065  n
mi
                                          Hp   =            222
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3374512
31                 X    =        -1110140
95
 Y    =       20838129
99  feet           Y    =         6339503
79  meter
 Z    =        7187849
94                 Z    =         2185662
21
 XDOT =     -17356
903370                 XDOT =       -5275
033511
 YDOT =       3368
188325  feet/sec       YDOT =         967
548921  meter/sec
 ZDOT =     -17856
213358                 ZDOT =       -5468
235667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21076589
64                 X    =        -6424144
52
 Y    =        1319127
12  feet           Y    =          402069
95  meter
 Z    =        7163620
21                 Z    =         2183471
44
 XDOT =      -7036
505372                 XDOT =       -2144
726837
 YDOT =     -14511
060104  feet/sec       YDOT =       -4422
971120  meter/sec
 ZDOT =     -17973
252539                 ZDOT =       -5478
247374


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   19326
65464452  
00016717  00000-0  10270-3 0  9127
2 25544  51
6419 295
6260 0006722 311
8405  48
2171 15
50023445 39832


Satellite: ISS
Catalog Number: 25544
Epoch time:      19326
65464452   =   yrday
fracday
Element set:     912
Inclination:       51
6419  deg
RA of node:       295
6260  deg
Eccentricity:     
0006722     
Arg of perigee:   311
8405  deg
Mean anomaly:      48
2171  deg
Mean motion:   15
50023445  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3983
Checksum:              303


Coasting Arc #14 (Orbit 3997)
---------------------------------------

Vector Time (GMT): 2019/327/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         768822
73                 A    =         6799830
95  meter
 Y    =       -6484444
59  meter          E    =           
0010416
 Z    =       -1872904
30                 I    =           51
29419
 XDOT =       5139
562908                 Wp   =          358
71616
 YDOT =      -1004
049280  meter/sec      RA   =          290
04902  deg
 ZDOT =       5595
648908                 TA   =          340
59445
                                          MA   =          340
63408
                                          Ha   =            227
218  n
mi
                                          Hp   =            222
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2522384
27                 X    =          850374
25
 Y    =      -21274424
51  feet           Y    =        -6475391
04  meter
 Z    =       -6144699
15                 Z    =        -1868971
67
 XDOT =      16862
083033                 XDOT =        5123
227367
 YDOT =      -3294
124935  feet/sec       YDOT =        -946
666550  meter/sec
 ZDOT =      18358
428176                 ZDOT =        5620
575802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21267924
46                 X    =         6482463
38
 Y    =       -2620249
00  feet           Y    =         -798651
89  meter
 Z    =       -6126220
10                 Z    =        -1867271
89
 XDOT =       7025
048580                 XDOT =        2141
234807
 YDOT =      13906
210400  feet/sec       YDOT =        4238
612930  meter/sec
 ZDOT =      18472
111602                 ZDOT =        5630
299616


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   19327
62173105  
00016717  00000-0  10270-3 0  9138
2 25544  51
6416 290
8346 0006765 315
9977  44
0635 15
50018250 39980


Satellite: ISS
Catalog Number: 25544
Epoch time:      19327
62173105   =   yrday
fracday
Element set:     913
Inclination:       51
6416  deg
RA of node:       290
8346  deg
Eccentricity:     
0006765     
Arg of perigee:   315
9977  deg
Mean anomaly:      44
0635  deg
Mean motion:   15
50018250  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3998
Checksum:              322


Coasting Arc #15 (Orbit 4013)
---------------------------------------

Vector Time (GMT): 2019/328/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -510795
57                 A    =         6800319
58  meter
 Y    =        6604383
15  meter          E    =           
0008026
 Z    =        1527256
25                 I    =           51
28597
 XDOT =      -5003
247200                 Wp   =           99
66528
 YDOT =        941
831272  meter/sec      RA   =          285
07240  deg
 ZDOT =      -5721
657623                 TA   =           63
60058
                                          MA   =           63
51822
                                          Ha   =            227
392  n
mi
                                          Hp   =            222
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1675838
48                 X    =         -592028
48
 Y    =       21667923
73  feet           Y    =         6598216
80  meter
 Z    =        5010683
25                 Z    =         1524577
95
 XDOT =     -16414
853018                 XDOT =       -4985
613875
 YDOT =       3089
997610  feet/sec       YDOT =         885
980290  meter/sec
 ZDOT =     -18771
842594                 ZDOT =       -5745
919235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21380580
44                 X    =        -6516800
92
 Y    =        3912272
61  feet           Y    =         1192460
69  meter
 Z    =        4997919
85                 Z    =         1523365
97
 XDOT =      -6882
770665                 XDOT =       -2097
868499
 YDOT =     -13389
087044  feet/sec       YDOT =       -4080
993731  meter/sec
 ZDOT =     -18882
486855                 ZDOT =       -5755
381993


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   19328
65328940  
00016717  00000-0  10270-3 0  9142
2 25544  51
6421 285
7242 0006710 319
8933  40
1722 15
50019711 40146


Satellite: ISS
Catalog Number: 25544
Epoch time:      19328
65328940   =   yrday
fracday
Element set:     914
Inclination:       51
6421  deg
RA of node:       285
7242  deg
Eccentricity:     
0006710     
Arg of perigee:   319
8933  deg
Mean anomaly:      40
1722  deg
Mean motion:   15
50019711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4014
Checksum:              292


Coasting Arc #16 (Orbit 4028)
---------------------------------------

Vector Time (GMT): 2019/329/14:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         216948
39                 A    =         6800683
87  meter
 Y    =       -6683114
40  meter          E    =           
0012757
 Z    =       -1194703
37                 I    =           51
27985
 XDOT =       4901
638493                 Wp   =            6
87394
 YDOT =       -879
159609  meter/sec      RA   =          280
09497  deg
 ZDOT =       5826
977140                 TA   =          340
09773
                                          MA   =          340
14745
                                          Ha   =            227
479  n
mi
                                          Hp   =            222
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         711772
92                 X    =          297468
14
 Y    =      -21926228
33  feet           Y    =        -6680238
03  meter
 Z    =       -3919630
48                 Z    =        -1193454
40
 XDOT =      16081
491118                 XDOT =        4882
800291
 YDOT =      -2884
381920  feet/sec       YDOT =        -824
451777  meter/sec
 ZDOT =      19117
379069                 ZDOT =        5850
742236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21292942
31                 X    =         6490088
82
 Y    =       -5284473
04  feet           Y    =        -1610707
38  meter
 Z    =       -3913382
82                 Z    =        -1192799
09
 XDOT =       6749
192462                 XDOT =        2057
153863
 YDOT =      13003
282711  feet/sec       YDOT =        3963
400570  meter/sec
 ZDOT =      19225
756171                 ZDOT =        5860
010481


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   19329
62037406  
00016717  00000-0  10270-3 0  9155
2 25544  51
6423 280
9330 0006812 322
8911  37
1768 15
50025009 40295


Satellite: ISS
Catalog Number: 25544
Epoch time:      19329
62037406   =   yrday
fracday
Element set:     915
Inclination:       51
6423  deg
RA of node:       280
9330  deg
Eccentricity:     
0006812     
Arg of perigee:   322
8911  deg
Mean anomaly:      37
1768  deg
Mean motion:   15
50025009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4029
Checksum:              294
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