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

 
Date: October 29th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 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


306/13:59:44 828 0 0 0 0 0 0
N/A 0 0 0 0 227 0
000/00:00:00 000 0 0 0 0 222 0

308/07:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 3

308/09:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 2

311/22:40:58 115 1 0 1 3 1 3
N/A 0 6 -0 0 225 9
000/00:05:52 230 0 6 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 5

Coasting Arc #1 (Orbit 3592)
---------------------------------------

Vector Time (GMT): 2019/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4719838
52                 A    =         6790821
10  meter
 Y    =         510086
60  meter          E    =           
0013262
 Z    =       -4867263
46                 I    =           51
96483
 XDOT =       1839
360723                 Wp   =          138
31541
 YDOT =       6990
595420  meter/sec      RA   =           59
49341  deg
 ZDOT =       2510
561326                 TA   =          156
33207
                                          MA   =          156
27101
                                          Ha   =            227
831  n
mi
                                          Hp   =            221
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15485034
51                 X    =         4737426
94
 Y    =        1673512
48  feet           Y    =          562965
35  meter
 Z    =      -15968712
14                 Z    =        -4844292
89
 XDOT =       6034
648042                 XDOT =        1748
857883
 YDOT =      22935
024343  feet/sec       YDOT =        7010
658504  meter/sec
 ZDOT =       8236
749757                 ZDOT =        2519
276446

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13644728
80                 X    =        -4158913
34
 Y    =        7729347
47  feet           Y    =         2355905
11  meter
 Z    =      -15863961
32                 Z    =        -4835335
41
 XDOT =     -17663
125083                 XDOT =       -5383
720525
 YDOT =     -14156
611311  feet/sec       YDOT =       -4314
935127  meter/sec
 ZDOT =       8275
908157                 ZDOT =        2522
496806


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   19301
51168225  
00016717  00000-0  10270-3 0  9001
2 25544  51
6430  60
1970 0006754 198
9844 161
1056 15
50238400 35937


Satellite: ISS
Catalog Number: 25544
Epoch time:      19301
51168225   =   yrday
fracday
Element set:     900
Inclination:       51
6430  deg
RA of node:        60
1970  deg
Eccentricity:     
0006754     
Arg of perigee:   198
9844  deg
Mean anomaly:     161
1056  deg
Mean motion:   15
50238400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3593
Checksum:              292


Coasting Arc #2 (Orbit 3608)
---------------------------------------

Vector Time (GMT): 2019/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4891114
70                 A    =         6791664
77  meter
 Y    =        -565009
02  meter          E    =           
0005706
 Z    =        4672456
54                 I    =           51
94945
 XDOT =      -2016
196301                 Wp   =          118
56200
 YDOT =      -6789
543741  meter/sec      RA   =           54
55797  deg
 ZDOT =      -2931
508283                 TA   =             
49383
                                          MA   =             
49327
                                          Ha   =            227
922  n
mi
                                          Hp   =            221
346

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16046964
22                 X    =        -4907129
95
 Y    =       -1853704
12  feet           Y    =         -619794
43  meter
 Z    =       15329581
84                 Z    =         4648657
75
 XDOT =      -6614
817261                 XDOT =       -1925
883745
 YDOT =     -22275
405973  feet/sec       YDOT =       -6811
585323  meter/sec
 ZDOT =      -9617
809327                 ZDOT =       -2941
083089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14064741
29                 X    =         4286933
15
 Y    =       -8151055
24  feet           Y    =        -2484441
64  meter
 Z    =       15221061
39                 Z    =         4639379
51
 XDOT =      17954
766629                 XDOT =        5472
612868
 YDOT =      12940
343338  feet/sec       YDOT =        3944
216650  meter/sec
 ZDOT =      -9660
886175                 ZDOT =       -2944
638106


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   19302
54310737  
00016717  00000-0  10270-3 0  9013
2 25544  51
6430  55
0859 0006740 201
9648 158
1215 15
50203702 36096


Satellite: ISS
Catalog Number: 25544
Epoch time:      19302
54310737   =   yrday
fracday
Element set:     901
Inclination:       51
6430  deg
RA of node:        55
0859  deg
Eccentricity:     
0006740     
Arg of perigee:   201
9648  deg
Mean anomaly:     158
1215  deg
Mean motion:   15
50203702  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3609
Checksum:              283


Coasting Arc #3 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2019/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5097167
88                 A    =         6792401
75  meter
 Y    =         603611
01  meter          E    =           
0010675
 Z    =       -4458723
19                 I    =           51
93301
 XDOT =       2143
462735                 Wp   =          149
05576
 YDOT =       6548
061062  meter/sec      RA   =           49
62228  deg
 ZDOT =       3331
484868                 TA   =          154
53829
                                          MA   =          154
48566
                                          Ha   =            227
540  n
mi
                                          Hp   =            221
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16722991
73                 X    =         5111697
88
 Y    =        1980351
09  feet           Y    =          660692
46  meter
 Z    =      -14628356
93                 Z    =        -4433927
08
 XDOT =       7032
358055                 XDOT =        2053
898164
 YDOT =      21483
139967  feet/sec       YDOT =        6571
529929  meter/sec
 ZDOT =      10930
068464                 ZDOT =        3341
679864

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14531470
17                 X    =        -4429192
11
 Y    =        8701247
25  feet           Y    =         2652140
16  meter
 Z    =      -14515293
32                 Z    =        -4424261
40
 XDOT =     -17992
205660                 XDOT =       -5484
024285
 YDOT =     -11708
250749  feet/sec       YDOT =       -3568
674828  meter/sec
 ZDOT =      10975
977480                 ZDOT =        3345
477936


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   19303
51006382  
00016717  00000-0  10270-3 0  9020
2 25544  51
6441  50
2949 0006739 206
9439 153
1362 15
50244524 36248


Satellite: ISS
Catalog Number: 25544
Epoch time:      19303
51006382   =   yrday
fracday
Element set:     902
Inclination:       51
6441  deg
RA of node:        50
2949  deg
Eccentricity:     
0006739     
Arg of perigee:   206
9439  deg
Mean anomaly:     153
1362  deg
Mean motion:   15
50244524  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3624
Checksum:              292


Coasting Arc #4 (Orbit 3639)
---------------------------------------

Vector Time (GMT): 2019/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5294282
73                 A    =         6793358
42  meter
 Y    =        -599646
24  meter          E    =           
0007404
 Z    =        4206451
20                 I    =           51
91378
 XDOT =      -2241
397630                 Wp   =          114
77451
 YDOT =      -6316
778686  meter/sec      RA   =           44
68499  deg
 ZDOT =      -3719
423289                 TA   =           13
29438
                                          MA   =           13
27488
                                          Ha   =            227
581  n
mi
                                          Hp   =            221
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17369694
00                 X    =        -5307616
91
 Y    =       -1967343
29  feet           Y    =         -658925
34  meter
 Z    =       13800692
92                 Z    =         4180700
55
 XDOT =      -7353
666766                 XDOT =       -2152
527674
 YDOT =     -20724
339521  feet/sec       YDOT =       -6341
346547  meter/sec
 ZDOT =     -12202
832314                 ZDOT =       -3730
095776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14872530
82                 X    =         4533147
39
 Y    =       -9360106
70  feet           Y    =        -2852960
52  meter
 Z    =       13683276
79                 Z    =         4170662
77
 XDOT =      17931
933169                 XDOT =        5465
653230
 YDOT =      10573
077754  feet/sec       YDOT =        3222
674099  meter/sec
 ZDOT =     -12250
925337                 ZDOT =       -3734
082043


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   19304
54148262  
00016717  00000-0  10270-3 0  9039
2 25544  51
6444  45
1836 0006590 209
8141 150
2635 15
50221938 36409


Satellite: ISS
Catalog Number: 25544
Epoch time:      19304
54148262   =   yrday
fracday
Element set:     903
Inclination:       51
6444  deg
RA of node:        45
1836  deg
Eccentricity:     
0006590     
Arg of perigee:   209
8141  deg
Mean anomaly:     150
2635  deg
Mean motion:   15
50221938  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3640
Checksum:              292


Coasting Arc #5 (Orbit 3654)
---------------------------------------

Vector Time (GMT): 2019/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5513687
89                 A    =         6794231
35  meter
 Y    =         569437
70  meter          E    =           
0007515
 Z    =       -3936724
52                 I    =           51
89221
 XDOT =       2287
956355                 Wp   =          160
68422
 YDOT =       6061
113821  meter/sec      RA   =           39
74740  deg
 ZDOT =       4076
508307                 TA   =          151
93311
                                          MA   =          151
89257
                                          Ha   =            227
196  n
mi
                                          Hp   =            222
014

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18089527
20                 X    =         5526033
27
 Y    =        1868233
91  feet           Y    =          631164
83  meter
 Z    =      -12915762
85                 Z    =        -3909910
57
 XDOT =       7506
418488                 XDOT =        2200
207381
 YDOT =      19885
544031  feet/sec       YDOT =        6086
208566  meter/sec
 ZDOT =      13374
371085                 ZDOT =        4087
409666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15196257
21                 X    =        -4631819
20
 Y    =       10145859
26  feet           Y    =         3092457
90  meter
 Z    =      -12793495
57                 Z    =        -3899457
45
 XDOT =     -17649
443772                 XDOT =       -5379
550462
 YDOT =      -9488
948746  feet/sec       YDOT =       -2892
231578  meter/sec
 ZDOT =      13423
520098                 ZDOT =        4091
488926


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   19305
50843338  
00016717  00000-0  10270-3 0  9043
2 25544  51
6442  40
3926 0006559 214
9757 145
0963 15
50246505 36558


Satellite: ISS
Catalog Number: 25544
Epoch time:      19305
50843338   =   yrday
fracday
Element set:     904
Inclination:       51
6442  deg
RA of node:        40
3926  deg
Eccentricity:     
0006559     
Arg of perigee:   214
9757  deg
Mean anomaly:     145
0963  deg
Mean motion:   15
50246505  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3655
Checksum:              315


Coasting Arc #6 (Orbit 3670)
---------------------------------------

Vector Time (GMT): 2019/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5714281
60                 A    =         6795204
45  meter
 Y    =        -500405
91  meter          E    =           
0009159
 Z    =        3631957
33                 I    =           51
86854
 XDOT =      -2301
436733                 Wp   =          118
82198
 YDOT =      -5825
247914  meter/sec      RA   =           34
80840  deg
 ZDOT =      -4419
399236                 TA   =           18
32760
                                          MA   =           18
29462
                                          Ha   =            227
226  n
mi
                                          Hp   =            222
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18747643
06                 X    =        -5725903
52
 Y    =       -1641751
67  feet           Y    =         -564372
15  meter
 Z    =       11915870
51                 Z    =         3604170
82
 XDOT =      -7550
645450                 XDOT =       -2214
658755
 YDOT =     -19111
705755  feet/sec       YDOT =       -5850
498837  meter/sec
 ZDOT =     -14499
341325                 ZDOT =       -4430
368366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15366892
47                 X    =         4683828
83
 Y    =      -11001440
43  feet           Y    =        -3353239
04  meter
 Z    =       11789162
95                 Z    =         3593336
87
 XDOT =      17291
081224                 XDOT =        5270
321557
 YDOT =       8547
122072  feet/sec       YDOT =        2605
162808  meter/sec
 ZDOT =     -14548
812795                 ZDOT =       -4434
478140


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   19306
53984715  
00016717  00000-0  10270-3 0  9053
2 25544  51
6438  35
2817 0006503 217
9030 142
1664 15
50239076 36710


Satellite: ISS
Catalog Number: 25544
Epoch time:      19306
53984715   =   yrday
fracday
Element set:     905
Inclination:       51
6438  deg
RA of node:        35
2817  deg
Eccentricity:     
0006503     
Arg of perigee:   217
9030  deg
Mean anomaly:     142
1664  deg
Mean motion:   15
50239076  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3671
Checksum:              307


Coasting Arc #7 (Orbit 3671)
---------------------------------------

Vector Time (GMT): 2019/306/13:59:44
828
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -576500
87                 A    =         6791348
02  meter
 Y    =       -4872269
08  meter          E    =           
0006237
 Z    =       -4700440
91                 I    =           51
85230
 XDOT =       6827
150215                 Wp   =          103
08986
 YDOT =       1952
767428  meter/sec      RA   =           34
44490  deg
 ZDOT =      -2866
066099                 TA   =          138
51391
                                          MA   =          138
46655
                                          Ha   =            227
047  n
mi
                                          Hp   =            222
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1891407
06                 X    =         -499142
42
 Y    =      -15985134
78  feet           Y    =        -4878283
22  meter
 Z    =      -15421394
07                 Z    =        -4703053
66
 XDOT =      22398
786794                 XDOT =        6818
728360
 YDOT =       6406
717284  feet/sec       YDOT =        2029
066453  meter/sec
 ZDOT =      -9403
104000                 ZDOT =       -2832
922246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15672069
63                 X    =         4776846
82
 Y    =        3624237
55  feet           Y    =         1104667
60  meter
 Z    =      -15432837
90                 Z    =        -4703928
99
 XDOT =     -13239
170623                 XDOT =       -4035
299206
 YDOT =      17915
648498  feet/sec       YDOT =        5460
689662  meter/sec
 ZDOT =      -9252
099212                 ZDOT =       -2820
039840


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   19306
60431011  
00016717  00000-0  10270-3 0  9068
2 25544  51
6425  34
9632 0006447 219
1409 140
9276 15
50232024 36720


Satellite: ISS
Catalog Number: 25544
Epoch time:      19306
60431011   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:        34
9632  deg
Eccentricity:     
0006447     
Arg of perigee:   219
1409  deg
Mean anomaly:     140
9276  deg
Mean motion:   15
50232024  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3672
Checksum:              282


Coasting Arc #8 (Orbit 3687)
---------------------------------------

Vector Time (GMT): 2019/307/13:59:44
828
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         512604
51                 A    =         6790541
65  meter
 Y    =        4697419
88  meter          E    =           
0008264
 Z    =        4878513
38                 I    =           51
82207
 XDOT =      -7039
699654                 Wp   =          168
92780
 YDOT =      -1776
841917  meter/sec      RA   =           29
50080  deg
 ZDOT =       2441
981526                 TA   =          257
10126
                                          MA   =          257
19358
                                          Ha   =            226
774  n
mi
                                          Hp   =            222
214

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1681773
34                 X    =          436341
10
 Y    =       15411482
53  feet           Y    =         4702725
64  meter
 Z    =       16005621
32                 Z    =         4880818
34
 XDOT =     -23096
127474                 XDOT =       -7031
169223
 YDOT =      -5829
533850  feet/sec       YDOT =       -1855
517176  meter/sec
 ZDOT =       8011
750415                 ZDOT =        2407
805550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15120379
33                 X    =        -4608691
62
 Y    =       -3375561
04  feet           Y    =        -1028871
00  meter
 Z    =       16015673
12                 Z    =         4881577
17
 XDOT =      12597
241584                 XDOT =        3839
639235
 YDOT =     -19020
347986  feet/sec       YDOT =       -5797
402066  meter/sec
 ZDOT =       7856
026880                 ZDOT =        2394
516993


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   19307
63571845  
00016717  00000-0  10270-3 0  9073
2 25544  51
6429  29
8515 0006373 223
9232 136
1413 15
50260854 36881


Satellite: ISS
Catalog Number: 25544
Epoch time:      19307
63571845   =   yrday
fracday
Element set:     907
Inclination:       51
6429  deg
RA of node:        29
8515  deg
Eccentricity:     
0006373     
Arg of perigee:   223
9232  deg
Mean anomaly:     136
1413  deg
Mean motion:   15
50260854  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3688
Checksum:              318


Coasting Arc #9 (Orbit 3698)
---------------------------------------

Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1158259
04                 A    =         6791027
81  meter
 Y    =        4719323
67  meter          E    =           
0008391
 Z    =        4745444
77                 I    =           51
80125
 XDOT =      -7072
694935                 Wp   =          163
79894
 YDOT =      -1040
111129  meter/sec      RA   =           25
99675  deg
 ZDOT =       2751
645176                 TA   =          258
95384
                                          MA   =          259
04822
                                          Ha   =            226
695  n
mi
                                          Hp   =            222
250

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3800062
46                 X    =         1082349
11
 Y    =       15483345
36  feet           Y    =         4731851
61  meter
 Z    =       15569044
53                 Z    =         4750886
93
 XDOT =     -23204
379708                 XDOT =       -7073
904569
 YDOT =      -3412
438088  feet/sec       YDOT =       -1119
209809  meter/sec
 ZDOT =       9027
707269                 ZDOT =        2717
285324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5243670
82                 X    =         1598270
86
 Y    =      -15030613
51  feet           Y    =        -4581331
00  meter
 Z    =       15593401
80                 Z    =         4752868
87
 XDOT =      16650
887263                 XDOT =        5075
190438
 YDOT =      15042
854104  feet/sec       YDOT =        4585
061931  meter/sec
 ZDOT =       8871
077857                 ZDOT =        2703
904531


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   19308
34481070  
00016717  00000-0  10270-3 0  9083
2 25544  51
6413  26
3338 0006391 225
2984 134
7647 15
50273826 36996


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
34481070   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:        26
3338  deg
Eccentricity:     
0006391     
Arg of perigee:   225
2984  deg
Mean anomaly:     134
7647  deg
Mean motion:   15
50273826  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3699
Checksum:              323


Coasting Arc #10 (Orbit 3699)
---------------------------------------

Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4634572
13                 A    =         6798033
25  meter
 Y    =       -4332078
10  meter          E    =           
0008190
 Z    =       -2428590
67                 I    =           51
82412
 XDOT =       4961
844002                 Wp   =          182
87057
 YDOT =      -2304
157942  meter/sec      RA   =           25
55094  deg
 ZDOT =      -5365
944511                 TA   =           24
18068
                                          MA   =           24
14226
                                          Ha   =            226
709  n
mi
                                          Hp   =            222
225

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15205289
14                 X    =        -4573988
24
 Y    =      -14212854
64  feet           Y    =        -4383566
37  meter
 Z    =       -7967817
17                 Z    =        -2450956
87
 XDOT =      16279
015753                 XDOT =        5013
306064
 YDOT =      -7559
573299  feet/sec       YDOT =       -2248
383268  meter/sec
 ZDOT =     -17604
804825                 ZDOT =       -5341
716502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15135225
25                 X    =         4613216
66
 Y    =       14230310
22  feet           Y    =         4337398
55  meter
 Z    =       -8069410
94                 Z    =        -2459556
46
 XDOT =     -15368
248595                 XDOT =       -4684
242172
 YDOT =       6438
579093  feet/sec       YDOT =        1962
478907  meter/sec
 ZDOT =     -17494
061031                 ZDOT =       -5332
189802


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   19308
40927396  
00016717  00000-0  10270-3 0  9097
2 25544  51
6436  26
0148 0006423 224
7883 135
2750 15
50263229 37005


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
40927396   =   yrday
fracday
Element set:     909
Inclination:       51
6436  deg
RA of node:        26
0148  deg
Eccentricity:     
0006423     
Arg of perigee:   224
7883  deg
Mean anomaly:     135
2750  deg
Mean motion:   15
50263229  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              306


Coasting Arc #11 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4648137
00                 A    =         6797161
18  meter
 Y    =        4095857
65  meter          E    =           
0008635
 Z    =        2791913
41                 I    =           51
79099
 XDOT =      -5174
723188                 Wp   =          103
01321
 YDOT =       2366
655034  meter/sec      RA   =           20
60820  deg
 ZDOT =       5127
928397                 TA   =          288
51259
                                          MA   =          288
60640
                                          Ha   =            226
573  n
mi
                                          Hp   =            222
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15249793
30                 X    =         4588428
75
 Y    =       13437853
17  feet           Y    =         4147502
54  meter
 Z    =        9159820
89                 Z    =         2814347
57
 XDOT =     -16977
438281                 XDOT =       -5225
712128
 YDOT =       7764
616254  feet/sec       YDOT =        2308
502508  meter/sec
 ZDOT =      16823
912064                 ZDOT =        5102
667410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15401754
51                 X    =        -4694454
78
 Y    =      -13192442
54  feet           Y    =        -4021056
49  meter
 Z    =        9261740
12                 Z    =         2822978
39
 XDOT =      16001
520479                 XDOT =        4877
263442
 YDOT =      -6916
345035  feet/sec       YDOT =       -2108
101967  meter/sec
 ZDOT =      16708
455796                 ZDOT =        5092
737327


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   19309
44067621  
00016717  00000-0  10270-3 0  9100
2 25544  51
6438  20
9037 0006411 228
2373 131
8230 15
50286397 37160


Satellite: ISS
Catalog Number: 25544
Epoch time:      19309
44067621   =   yrday
fracday
Element set:     910
Inclination:       51
6438  deg
RA of node:        20
9037  deg
Eccentricity:     
0006411     
Arg of perigee:   228
2373  deg
Mean anomaly:     131
8230  deg
Mean motion:   15
50286397  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              294


Coasting Arc #12 (Orbit 3730)
---------------------------------------

Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4602388
01                 A    =         6796299
29  meter
 Y    =       -3873947
34  meter          E    =           
0004868
 Z    =       -3156126
32                 I    =           51
75630
 XDOT =       5394
920497                 Wp   =          186
69498
 YDOT =      -2459
278784  meter/sec      RA   =           15
66321  deg
 ZDOT =      -4852
435338                 TA   =           29
57130
                                          MA   =           29
54378
                                          Ha   =            226
387  n
mi
                                          Hp   =            222
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15099698
18                 X    =        -4543395
43
 Y    =      -12709800
97  feet           Y    =        -3925084
66  meter
 Z    =      -10354745
14                 Z    =        -3178339
97
 XDOT =      17699
870397                 XDOT =        5445
590644
 YDOT =      -8068
499949  feet/sec       YDOT =       -2398
665697  meter/sec
 ZDOT =     -15920
063445                 ZDOT =       -4826
105410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15444105
56                 X    =         4707363
37
 Y    =       12203245
39  feet           Y    =         3719549
20  meter
 Z    =      -10455672
06                 Z    =        -3186888
84
 XDOT =     -16638
664544                 XDOT =       -5071
464953
 YDOT =       7531
358897  feet/sec       YDOT =        2295
558192  meter/sec
 ZDOT =     -15799
730230                 ZDOT =       -4815
757774


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
40761586  
00016717  00000-0  10270-3 0  9110
2 25544  51
6438  16
1125 0006429 232
1818 127
8751 15
50263487 37317


Satellite: ISS
Catalog Number: 25544
Epoch time:      19310
40761586   =   yrday
fracday
Element set:     911
Inclination:       51
6438  deg
RA of node:        16
1125  deg
Eccentricity:     
0006429     
Arg of perigee:   232
1818  deg
Mean anomaly:     127
8751  deg
Mean motion:   15
50263487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3731
Checksum:              301


Coasting Arc #13 (Orbit 3746)
---------------------------------------

Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4542867
64                 A    =         6795276
22  meter
 Y    =        3658132
20  meter          E    =           
0007921
 Z    =        3484493
11                 I    =           51
72162
 XDOT =      -5589
129634                 Wp   =          119
39523
 YDOT =       2596
316549  meter/sec      RA   =           10
71466  deg
 ZDOT =       4549
472027                 TA   =          281
39710
                                          MA   =          281
48606
                                          Ha   =            226
202  n
mi
                                          Hp   =            222
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14904421
38                 X    =         4484697
71
 Y    =       12001746
07  feet           Y    =         3708608
57  meter
 Z    =       11432064
00                 Z    =         3506419
65
 XDOT =     -18337
039483                 XDOT =       -5639
846154
 YDOT =       8518
098913  feet/sec       YDOT =        2533
531457  meter/sec
 ZDOT =      14926
089328                 ZDOT =        4522
198485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15413715
82                 X    =        -4698100
58
 Y    =      -11238913
57  feet           Y    =        -3425620
86  meter
 Z    =       11531693
67                 Z    =         3514860
23
 XDOT =      17164
427380                 XDOT =        5231
717465
 YDOT =      -8314
588459  feet/sec       YDOT =       -2534
286562  meter/sec
 ZDOT =      14801
448501                 ZDOT =        4511
481503


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
43901238  
00016717  00000-0  10270-3 0  9125
2 25544  51
6447  11
0011 0006403 236
2504 123
8037 15
50298392 37477


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
43901238   =   yrday
fracday
Element set:     912
Inclination:       51
6447  deg
RA of node:        11
0011  deg
Eccentricity:     
0006403     
Arg of perigee:   236
2504  deg
Mean anomaly:     123
8037  deg
Mean motion:   15
50298392  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3747
Checksum:              276


Coasting Arc #14 (Orbit 3754)
---------------------------------------

Vector Time (GMT): 2019/311/22:43:54
230
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5344444
14                 A    =         6795842
35  meter
 Y    =       -2141012
05  meter          E    =           
0002893
 Z    =       -3612342
51                 I    =           51
70250
 XDOT =       4660
383104                 Wp   =          199
31778
 YDOT =       4168
356217  meter/sec      RA   =            7
86956  deg
 ZDOT =       4420
779291                 TA   =          118
05593
                                          MA   =          118
02668
                                          Ha   =            225
910  n
mi
                                          Hp   =            223
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17534265
57                 X    =         5385535
41
 Y    =       -7024317
74  feet           Y    =        -2081017
02  meter
 Z    =      -11851517
42                 Z    =        -3586280
91
 XDOT =      15289
970814                 XDOT =        4591
950901
 YDOT =      13675
709372  feet/sec       YDOT =        4220
089374  meter/sec
 ZDOT =      14503
869066                 ZDOT =        4443
251779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12523261
27                 X    =         3817090
04
 Y    =      -14239641
79  feet           Y    =        -4340242
82  meter
 Z    =      -11732455
10                 Z    =        -3576052
32
 XDOT =      18699
707679                 XDOT =        5699
670901
 YDOT =       4401
435540  feet/sec       YDOT =        1341
557553  meter/sec
 ZDOT =      14605
931512                 ZDOT =        4451
887925


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
95471110  
00016717  00000-0  10270-3 0  9134
2 25544  51
6451   8
4494 0006565 251
0987 108
9453 15
50042014 37559


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
95471110   =   yrday
fracday
Element set:     913
Inclination:       51
6451  deg
RA of node:         8
4494  deg
Eccentricity:     
0006565     
Arg of perigee:   251
0987  deg
Mean anomaly:     108
9453  deg
Mean motion:   15
50042014  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3755
Checksum:              297


Coasting Arc #15 (Orbit 3757)
---------------------------------------

Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1842350
57                 A    =         6790655
76  meter
 Y    =       -4211593
01  meter          E    =           
0006148
 Z    =       -5003724
43                 I    =           51
67517
 XDOT =       7333
246798                 Wp   =           78
79163
 YDOT =       -747
948261  meter/sec      RA   =            7
01099  deg
 ZDOT =      -2071
525349                 TA   =          171
04057
                                          MA   =          171
02960
                                          Ha   =            225
911  n
mi
                                          Hp   =            223
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6044457
25                 X    =        -1770812
63
 Y    =      -13817562
37  feet           Y    =        -4231795
59  meter
 Z    =      -16416418
75                 Z    =        -5012500
20
 XDOT =      24059
208654                 XDOT =        7351
128048
 YDOT =      -2453
898495  feet/sec       YDOT =        -665
842778  meter/sec
 ZDOT =      -6796
343010                 ZDOT =       -2035
859103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13560413
58                 X    =        -4133214
06
 Y    =        6501848
60  feet           Y    =         1981763
45  meter
 Z    =      -16456015
50                 Z    =        -5015793
53
 XDOT =      -2978
388545                 XDOT =        -907
812828
 YDOT =     -22993
081976  feet/sec       YDOT =       -7008
291386  meter/sec
 ZDOT =      -6633
623283                 ZDOT =       -2021
928377


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
14812674  
00016717  00000-0  10270-3 0  9141
2 25544  51
6410   7
4885 0006606 251
1617 108
8817 15
50033027 37584


Satellite: ISS
Catalog Number: 25544
Epoch time:      19312
14812674   =   yrday
fracday
Element set:     914
Inclination:       51
6410  deg
RA of node:         7
4885  deg
Eccentricity:     
0006606     
Arg of perigee:   251
1617  deg
Mean anomaly:     108
8817  deg
Mean motion:   15
50033027  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3758
Checksum:              299


Coasting Arc #16 (Orbit 3773)
---------------------------------------

Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1774301
49                 A    =         6790325
41  meter
 Y    =        4109802
48  meter          E    =           
0005071
 Z    =        5108898
33                 I    =           51
63985
 XDOT =      -7390
812000                 Wp   =          205
02045
 YDOT =       1077
738083  meter/sec      RA   =            2
05661  deg
 ZDOT =       1695
953784                 TA   =          228
55481
                                          MA   =          228
59838
                                          Ha   =            225
715  n
mi
                                          Hp   =            223
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5821199
13                 X    =         1703395
89
 Y    =       13483603
93  feet           Y    =         4129247
62  meter
 Z    =       16761477
45                 Z    =         5117345
10
 XDOT =     -24248
070865                 XDOT =       -7410
552456
 YDOT =       3535
886098  feet/sec       YDOT =         994
978460  meter/sec
 ZDOT =       5564
152835                 ZDOT =        1660
003250

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13126442
38                 X    =         4000939
64
 Y    =       -6489353
24  feet           Y    =        -1977954
87  meter
 Z    =       16799579
33                 Z    =         5120511
78
 XDOT =       4481
953083                 XDOT =        1366
099300
 YDOT =      23078
534225  feet/sec       YDOT =        7034
337232  meter/sec
 ZDOT =       5400
118727                 ZDOT =        1645
956188


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
17968285  
00016717  00000-0  10270-3 0  9156
2 25544  51
6405   2
3780 0006545 255
2519 104
7906 15
49990827 37744


Satellite: ISS
Catalog Number: 25544
Epoch time:      19313
17968285   =   yrday
fracday
Element set:     915
Inclination:       51
6405  deg
RA of node:         2
3780  deg
Eccentricity:     
0006545     
Arg of perigee:   255
2519  deg
Mean anomaly:     104
7906  deg
Mean motion:   15
49990827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3774
Checksum:              334


Coasting Arc #17 (Orbit 3788)
---------------------------------------

Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1684971
87                 A    =         6789810
95  meter
 Y    =       -4039027
34  meter          E    =           
0007517
 Z    =       -5197856
39                 I    =           51
60443
 XDOT =       7410
749829                 Wp   =           82
65250
 YDOT =      -1411
754961  meter/sec      RA   =          357
09950  deg
 ZDOT =      -1305
989997                 TA   =          174
78058
                                          MA   =          174
77274
                                          Ha   =            225
552  n
mi
                                          Hp   =            223
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5528122
95                 X    =        -1614432
13
 Y    =      -13251402
04  feet           Y    =        -4057475
53  meter
 Z    =      -17053334
63                 Z    =        -5205870
18
 XDOT =      24313
483692                 XDOT =        7432
329631
 YDOT =      -4631
741997  feet/sec       YDOT =       -1328
762076  meter/sec
 ZDOT =      -4284
744086                 ZDOT =       -1269
938020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12803737
71                 X    =        -3902579
25
 Y    =        6402384
39  feet           Y    =         1951446
76  meter
 Z    =      -17089464
47                 Z    =        -5208868
77
 XDOT =      -5997
937313                 XDOT =       -1828
171293
 YDOT =     -22986
778747  feet/sec       YDOT =       -7006
370162  meter/sec
 ZDOT =      -4120
228599                 ZDOT =       -1255
845677


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
14676307  
00016717  00000-0  10270-3 0  9166
2 25544  51
6398 357
5869 0006524 257
3010 102
7411 15
50038156 37899


Satellite: ISS
Catalog Number: 25544
Epoch time:      19314
14676307   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       357
5869  deg
Eccentricity:     
0006524     
Arg of perigee:   257
3010  deg
Mean anomaly:     102
7411  deg
Mean motion:   15
50038156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3789
Checksum:              319


Coasting Arc #18 (Orbit 3804)
---------------------------------------

Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1596724
11                 A    =         6789655
85  meter
 Y    =        3991525
82  meter          E    =           
0004416
 Z    =        5258664
03                 I    =           51
57038
 XDOT =      -7399
445589                 Wp   =          233
14363
 YDOT =       1753
448429  meter/sec      RA   =          352
13941  deg
 ZDOT =        913
752655                 TA   =          208
08452
                                          MA   =          208
10836
                                          Ha   =            225
308  n
mi
                                          Hp   =            223
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5238596
18                 X    =         1526426
66
 Y    =       13095557
16  feet           Y    =         4008988
43  meter
 Z    =       17252834
73                 Z    =         5266249
81
 XDOT =     -24276
396291                 XDOT =       -7422
941840
 YDOT =       5752
783561  feet/sec       YDOT =        1670
571222  meter/sec
 ZDOT =       2997
876165                 ZDOT =         877
750858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12563604
95                 X    =         3829386
79
 Y    =       -6317579
78  feet           Y    =        -1925598
32  meter
 Z    =       17287013
33                 Z    =         5269081
66
 XDOT =       7526
479960                 XDOT =        2294
071092
 YDOT =      22739
740589  feet/sec       YDOT =        6931
072932  meter/sec
 ZDOT =       2833
568454                 ZDOT =         863
671665


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
17831500  
00016717  00000-0  10270-3 0  9179
2 25544  51
6400 352
4757 0006526 261
8932  98
1478 15
49996866 38057


Satellite: ISS
Catalog Number: 25544
Epoch time:      19315
17831500   =   yrday
fracday
Element set:     917
Inclination:       51
6400  deg
RA of node:       352
4757  deg
Eccentricity:     
0006526     
Arg of perigee:   261
8932  deg
Mean anomaly:      98
1478  deg
Mean motion:   15
49996866  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3805
Checksum:              340


Coasting Arc #19 (Orbit 3819)
---------------------------------------

Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1500312
50                 A    =         6789320
65  meter
 Y    =       -3977278
93  meter          E    =           
0008356
 Z    =       -5301150
13                 I    =           51
53750
 XDOT =       7347
364020                 Wp   =           87
34693
 YDOT =      -2089
504033  meter/sec      RA   =          347
17734  deg
 ZDOT =       -512
059827                 TA   =          177
75480
                                          MA   =          177
75105
                                          Ha   =            225
188  n
mi
                                          Hp   =            223
393

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4922285
11                 X    =        -1429975
10
 Y    =      -13048815
38  feet           Y    =        -3993663
06  meter
 Z    =      -17392224
84                 Z    =        -5308267
57
 XDOT =      24105
525000                 XDOT =        7372
670762
 YDOT =      -6855
328192  feet/sec       YDOT =       -2007
199107  meter/sec
 ZDOT =      -1679
986309                 ZDOT =        -476
306619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12441557
68                 X    =        -3792186
78
 Y    =        6212291
42  feet           Y    =         1893506
43  meter
 Z    =      -17424265
73                 Z    =        -5310916
19
 XDOT =      -9015
860540                 XDOT =       -2748
034293
 YDOT =     -22307
701597  feet/sec       YDOT =       -6799
387447  meter/sec
 ZDOT =      -1516
789261                 ZDOT =        -462
317367


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
14538979  
00016717  00000-0  10270-3 0  9182
2 25544  51
6406 347
6846 0006382 264
6259  95
4164 15
50051620 38202


Satellite: ISS
Catalog Number: 25544
Epoch time:      19316
14538979   =   yrday
fracday
Element set:     918
Inclination:       51
6406  deg
RA of node:       347
6846  deg
Eccentricity:     
0006382     
Arg of perigee:   264
6259  deg
Mean anomaly:      95
4164  deg
Mean motion:   15
50051620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3820
Checksum:              328
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list