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

 
Date: March 25th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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


087/06:36:30 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 216 6

090/20:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 2
000/00:00:00 000 0 0 0 0 216 7

094/11:01:35 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 216 9

094/14:24:50 000 0 0 0 0 0 0
N/A 0 0 0 0 224 0
000/00:00:00 000 0 0 0 0 216 9

097/20:12:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 216 9

Coasting Arc #1 (Orbit 224)
---------------------------------------

Vector Time (GMT): 2019/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4541754
57                 A    =         6793413
21  meter
 Y    =       -4833571
21  meter          E    =           
0015898
 Z    =        1434553
63                 I    =           51
97770
 XDOT =       2654
114481                 Wp   =          118
20257
 YDOT =      -4232
791722  meter/sec      RA   =           56
51944  deg
 ZDOT =      -5817
480433                 TA   =           46
23111
                                          MA   =           46
09966
                                          Ha   =            224
405  n
mi
                                          Hp   =            216
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14900769
58                 X    =        -4494334
93
 Y    =      -15858173
26  feet           Y    =        -4884095
04  meter
 Z    =        4706540
78                 Z    =         1412606
96
 XDOT =       8707
724674                 XDOT =        2729
507662
 YDOT =     -13887
111949  feet/sec       YDOT =       -4202
690428  meter/sec
 ZDOT =     -19086
221894                 ZDOT =       -5804
404286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15415972
06                 X    =        -4698788
28
 Y    =      -15387744
62  feet           Y    =        -4690184
56  meter
 Z    =        4607736
96                 Z    =         1404438
23
 XDOT =       7278
775470                 XDOT =        2218
570763
 YDOT =     -13031
229690  feet/sec       YDOT =       -3971
918810  meter/sec
 ZDOT =     -19026
582768                 ZDOT =       -5799
302428


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   19084
53496800  
00016717  00000-0  10270-3 0  9004
2 25544  51
6387  57
0811 0002084 112
5331 247
6042 15
52439279  2255


Satellite: ISS
Catalog Number: 25544
Epoch time:      19084
53496800   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:        57
0811  deg
Eccentricity:     
0002084     
Arg of perigee:   112
5331  deg
Mean anomaly:     247
6042  deg
Mean motion:   15
52439279  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             225
Checksum:              293


Coasting Arc #2 (Orbit 239)
---------------------------------------

Vector Time (GMT): 2019/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4404817
89                 A    =         6794159
76  meter
 Y    =        5157153
54  meter          E    =           
0012237
 Z    =        -314710
76                 I    =           51
96183
 XDOT =      -3418
562267                 Wp   =           52
83059
 YDOT =       3277
372064  meter/sec      RA   =           51
57924  deg
 ZDOT =       6026
643492                 TA   =          303
79545
                                          MA   =          303
91192
                                          Ha   =            224
378  n
mi
                                          Hp   =            216
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14451502
28                 X    =         4348350
46
 Y    =       16919795
07  feet           Y    =         5206095
55  meter
 Z    =       -1032515
63                 Z    =         -293451
25
 XDOT =     -11215
755470                 XDOT =       -3484
230797
 YDOT =      10752
533018  feet/sec       YDOT =        3238
776478  meter/sec
 ZDOT =      19772
452403                 ZDOT =        6009
877709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15256222
06                 X    =         4650096
48
 Y    =       16203747
55  feet           Y    =         4938902
25  meter
 Z    =        -936870
12                 Z    =         -285558
01
 XDOT =      -9635
164625                 XDOT =       -2936
798178
 YDOT =      10175
410114  feet/sec       YDOT =        3101
465003  meter/sec
 ZDOT =      19696
211782                 ZDOT =        6003
405351


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   19085
50055288  
00016717  00000-0  10270-3 0  9014
2 25544  51
6394  52
2806 0002183 118
8369 241
3002 15
52455349  2404


Satellite: ISS
Catalog Number: 25544
Epoch time:      19085
50055288   =   yrday
fracday
Element set:     901
Inclination:       51
6394  deg
RA of node:        52
2806  deg
Eccentricity:     
0002183     
Arg of perigee:   118
8369  deg
Mean anomaly:     241
3002  deg
Mean motion:   15
52455349  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             240
Checksum:              292


Coasting Arc #3 (Orbit 255)
---------------------------------------

Vector Time (GMT): 2019/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4108070
67                 A    =         6793901
28  meter
 Y    =       -5335473
52  meter          E    =           
0011904
 Z    =        -864296
27                 I    =           51
93992
 XDOT =       4236
920431                 Wp   =          136
54920
 YDOT =      -2306
524823  meter/sec      RA   =           46
63758  deg
 ZDOT =      -5956
803757                 TA   =           52
75575
                                          MA   =           52
64722
                                          Ha   =            224
320  n
mi
                                          Hp   =            216
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13477922
14                 X    =        -4043904
31
 Y    =      -17504834
37  feet           Y    =        -5381054
10  meter
 Z    =       -2835617
67                 Z    =         -884095
57
 XDOT =      13900
657581                 XDOT =        4291
332524
 YDOT =      -7567
338657  feet/sec       YDOT =       -2258
840679  meter/sec
 ZDOT =     -19543
319414                 ZDOT =       -5936
090166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14573613
87                 X    =        -4442037
51
 Y    =      -16588269
89  feet           Y    =        -5056104
66  meter
 Z    =       -2924623
03                 Z    =         -891425
10
 XDOT =      12297
051521                 XDOT =        3748
141304
 YDOT =      -7406
497104  feet/sec       YDOT =       -2257
500317  meter/sec
 ZDOT =     -19449
316451                 ZDOT =       -5928
151654


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   19086
53050777  
00016717  00000-0  10270-3 0  9027
2 25544  51
6400  47
1588 0002017 116
9830 243
1528 15
52440774  2566


Satellite: ISS
Catalog Number: 25544
Epoch time:      19086
53050777   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:        47
1588  deg
Eccentricity:     
0002017     
Arg of perigee:   116
9830  deg
Mean anomaly:     243
1528  deg
Mean motion:   15
52440774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             256
Checksum:              297


Coasting Arc #4 (Orbit 267)
---------------------------------------

Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3280199
52                 A    =         6791942
79  meter
 Y    =       -5486196
06  meter          E    =           
0008010
 Z    =       -2291651
68                 I    =           51
91720
 XDOT =       5308
893968                 Wp   =          131
66515
 YDOT =       -904
622611  meter/sec      RA   =           42
80849  deg
 ZDOT =      -5450
780275                 TA   =           73
72356
                                          MA   =           73
63547
                                          Ha   =            224
338  n
mi
                                          Hp   =            216
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10761809
44                 X    =        -3207476
01
 Y    =      -17999330
91  feet           Y    =        -5522471
04  meter
 Z    =       -7518542
25                 Z    =        -2307408
67
 XDOT =      17417
631128                 XDOT =        5345
091887
 YDOT =      -2967
921953  feet/sec       YDOT =        -845
052728  meter/sec
 ZDOT =     -17883
137386                 ZDOT =       -5424
903819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14967419
25                 X    =         4562069
39
 Y    =      -14652675
69  feet           Y    =        -4466135
55  meter
 Z    =       -7589228
50                 Z    =        -2313196
85
 XDOT =       5951
148115                 XDOT =        1813
909945
 YDOT =      15251
310434  feet/sec       YDOT =        4648
599420  meter/sec
 ZDOT =     -17765
927489                 ZDOT =       -5415
054699


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   19087
30297294  
00016717  00000-0  10270-3 0  9031
2 25544  51
6418  43
3181 0002228 123
7957 236
3407 15
52450731  2689


Satellite: ISS
Catalog Number: 25544
Epoch time:      19087
30297294   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:        43
3181  deg
Eccentricity:     
0002228     
Arg of perigee:   123
7957  deg
Mean anomaly:     236
3407  deg
Mean motion:   15
52450731  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             268
Checksum:              304


Coasting Arc #5 (Orbit 283)
---------------------------------------

Vector Time (GMT): 2019/088/06:36:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2672617
26                 A    =         6789745
85  meter
 Y    =        5315944
51  meter          E    =           
0014597
 Z    =        3258983
52                 I    =           51
88329
 XDOT =      -6001
019917                 Wp   =           92
51230
 YDOT =         78
911931  meter/sec      RA   =           37
85813  deg
 ZDOT =       4773
536447                 TA   =          305
12038
                                          MA   =          305
25711
                                          Ha   =            224
396  n
mi
                                          Hp   =            216
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8768429
32                 X    =         2597144
00
 Y    =       17440762
82  feet           Y    =         5345409
77  meter
 Z    =       10692203
16                 Z    =         3271782
39
 XDOT =     -19688
385556                 XDOT =       -6024
643352
 YDOT =        258
897412  feet/sec       YDOT =          11
672513  meter/sec
 ZDOT =      15661
208815                 ZDOT =        4744
328571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14681413
53                 X    =        -4474894
84
 Y    =       12817676
60  feet           Y    =         3906827
83  meter
 Z    =       10749513
12                 Z    =         3276451
60
 XDOT =      -4313
023045                 XDOT =       -1314
609424
 YDOT =     -18015
644236  feet/sec       YDOT =       -5491
168363  meter/sec
 ZDOT =      15529
020000                 ZDOT =        4733
245296


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   19088
33292610  
00016717  00000-0  10270-3 0  9043
2 25544  51
6407  38
1967 0002289 123
5309 236
6062 15
52424371  2846


Satellite: ISS
Catalog Number: 25544
Epoch time:      19088
33292610   =   yrday
fracday
Element set:     904
Inclination:       51
6407  deg
RA of node:        38
1967  deg
Eccentricity:     
0002289     
Arg of perigee:   123
5309  deg
Mean anomaly:     236
6062  deg
Mean motion:   15
52424371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             284
Checksum:              303


Coasting Arc #6 (Orbit 298)
---------------------------------------

Vector Time (GMT): 2019/089/06:36:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1888499
29                 A    =         6787011
22  meter
 Y    =       -5067003
96  meter          E    =           
0008819
 Z    =       -4109901
46                 I    =           51
84943
 XDOT =       6587
487554                 Wp   =           82
54275
 YDOT =        661
426660  meter/sec      RA   =           32
90180  deg
 ZDOT =      -3848
365453                 TA   =          147
76347
                                          MA   =          147
70954
                                          Ha   =            224
282  n
mi
                                          Hp   =            216
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6195863
81                 X    =        -1811734
81
 Y    =      -16624028
75  feet           Y    =        -5087693
54  meter
 Z    =      -13483928
66                 Z    =        -4118888
21
 XDOT =      21612
491974                 XDOT =        6598
294764
 YDOT =       2170
034974  feet/sec       YDOT =         735
152724  meter/sec
 ZDOT =     -12625
870910                 ZDOT =       -3816
339980

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14369429
68                 X    =         4379802
17
 Y    =      -10352973
11  feet           Y    =        -3155586
21  meter
 Z    =      -13524009
41                 Z    =        -4122118
07
 XDOT =       2992
874430                 XDOT =         912
228126
 YDOT =      20432
372990  feet/sec       YDOT =        6227
787287  meter/sec
 ZDOT =     -12481
022926                 ZDOT =       -3804
215788


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   19089
29850224  
00016717  00000-0  10270-3 0  9051
2 25544  51
6425  33
3959 0002160 129
2726 230
8617 15
52457293  2995


Satellite: ISS
Catalog Number: 25544
Epoch time:      19089
29850224   =   yrday
fracday
Element set:     905
Inclination:       51
6425  deg
RA of node:        33
3959  deg
Eccentricity:     
0002160     
Arg of perigee:   129
2726  deg
Mean anomaly:     230
8617  deg
Mean motion:   15
52457293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             299
Checksum:              320


Coasting Arc #7 (Orbit 314)
---------------------------------------

Vector Time (GMT): 2019/090/06:36:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1007397
11                 A    =         6784698
14  meter
 Y    =        4749350
32  meter          E    =           
0009890
 Z    =        4734063
69                 I    =           51
81129
 XDOT =      -7039
389362                 Wp   =          119
68928
 YDOT =      -1271
665269  meter/sec      RA   =           27
93848  deg
 ZDOT =       2764
625566                 TA   =          302
96274
                                          MA   =          303
05779
                                          Ha   =            224
306  n
mi
                                          Hp   =            216
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3305108
62                 X    =          931218
40
 Y    =       15581858
01  feet           Y    =         4760190
17  meter
 Z    =       15531705
03                 Z    =         4738771
81
 XDOT =     -23095
109457                 XDOT =       -7038
074960
 YDOT =      -4172
130148  feet/sec       YDOT =       -1350
377078  meter/sec
 ZDOT =       9070
293852                 ZDOT =        2730
434448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14019948
40                 X    =        -4273280
27
 Y    =        7517582
57  feet           Y    =         2291359
17  meter
 Z    =       15552456
47                 Z    =         4740388
73
 XDOT =      -2066
177637                 XDOT =        -629
770944
 YDOT =     -22360
033449  feet/sec       YDOT =       -6815
338195  meter/sec
 ZDOT =       8915
725819                 ZDOT =        2717
513230


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   19090
32844957  
00016717  00000-0  10270-3 0  9064
2 25544  51
6408  28
2743 0002210 129
2828 230
8520 15
52447281  3157


Satellite: ISS
Catalog Number: 25544
Epoch time:      19090
32844957   =   yrday
fracday
Element set:     906
Inclination:       51
6408  deg
RA of node:        28
2743  deg
Eccentricity:     
0002210     
Arg of perigee:   129
2828  deg
Mean anomaly:     230
8520  deg
Mean motion:   15
52447281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             315
Checksum:              295


Coasting Arc #8 (Orbit 323)
---------------------------------------

Vector Time (GMT): 2019/090/20:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3540834
86                 A    =         6789077
94  meter
 Y    =        4649794
19  meter          E    =           
0013803
 Z    =        3444516
51                 I    =           51
80622
 XDOT =      -6025
684438                 Wp   =           97
57050
 YDOT =       1171
261799  meter/sec      RA   =           25
08591  deg
 ZDOT =       4595
545384                 TA   =          302
67340
                                          MA   =          302
80646
                                          Ha   =            224
158  n
mi
                                          Hp   =            216
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11616912
28                 X    =         3471844
97
 Y    =       15255230
29  feet           Y    =         4689004
84  meter
 Z    =       11300907
17                 Z    =         3461548
44
 XDOT =     -19769
305900                 XDOT =       -6060
656404
 YDOT =       3842
722437  feet/sec       YDOT =        1103
683236  meter/sec
 ZDOT =      15077
248634                 ZDOT =        4566
190074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2863369
21                 X    =          872754
94
 Y    =      -18914025
65  feet           Y    =        -5764995
02  meter
 Z    =       11377431
84                 Z    =         3467841
22
 XDOT =      15245
912551                 XDOT =        4646
954145
 YDOT =      11331
925490  feet/sec       YDOT =        3453
970889  meter/sec
 ZDOT =      14944
283186                 ZDOT =        4555
017515


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   19090
90779416  
00016717  00000-0  10270-3 0  9076
2 25544  51
6380  25
3904 0002199 141
3621 218
7688 15
52465867  3245


Satellite: ISS
Catalog Number: 25544
Epoch time:      19090
90779416   =   yrday
fracday
Element set:     907
Inclination:       51
6380  deg
RA of node:        25
3904  deg
Eccentricity:     
0002199     
Arg of perigee:   141
3621  deg
Mean anomaly:     218
7688  deg
Mean motion:   15
52465867  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             324
Checksum:              325


Coasting Arc #9 (Orbit 338)
---------------------------------------

Vector Time (GMT): 2019/091/20:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2688811
49                 A    =         6786427
67  meter
 Y    =       -4557597
41  meter          E    =           
0009246
 Z    =       -4257759
86                 I    =           51
76878
 XDOT =       6719
260874                 Wp   =           82
19739
 YDOT =       -580
996194  meter/sec      RA   =           20
12370  deg
 ZDOT =      -3626
883353                 TA   =          150
74735
                                          MA   =          150
69554
                                          Ha   =            224
182  n
mi
                                          Hp   =            216
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8821560
02                 X    =        -2616965
61
 Y    =      -14952747
41  feet           Y    =        -4587264
29  meter
 Z    =      -13969028
41                 Z    =        -4270646
06
 XDOT =      22044
819139                 XDOT =        6742
875620
 YDOT =      -1906
155491  feet/sec       YDOT =        -505
725035  meter/sec
 ZDOT =     -11899
223599                 ZDOT =       -3594
186512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4323395
34                 X    =        -1317770
90
 Y    =       16765902
66  feet           Y    =         5110247
13  meter
 Z    =      -14026799
05                 Z    =        -4275368
35
 XDOT =     -15837
010486                 XDOT =       -4827
120796
 YDOT =     -13900
144951  feet/sec       YDOT =       -4236
764181  meter/sec
 ZDOT =     -11751
218394                 ZDOT =       -3581
771367


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   19091
87336756  
00016717  00000-0  10270-3 0  9080
2 25544  51
6399  20
5897 0002187 140
2414 219
8898 15
52471235  3395


Satellite: ISS
Catalog Number: 25544
Epoch time:      19091
87336756   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:        20
5897  deg
Eccentricity:     
0002187     
Arg of perigee:   140
2414  deg
Mean anomaly:     219
8898  deg
Mean motion:   15
52471235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             339
Checksum:              339


Coasting Arc #10 (Orbit 354)
---------------------------------------

Vector Time (GMT): 2019/092/20:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1733433
42                 A    =         6784170
01  meter
 Y    =        4423890
58  meter          E    =           
0009021
 Z    =        4838227
18                 I    =           51
72963
 XDOT =      -7246
344866                 Wp   =          125
84882
 YDOT =         87
336712  meter/sec      RA   =           15
15343  deg
 ZDOT =       2507
917576                 TA   =          299
48869
                                          MA   =          299
57864
                                          Ha   =            224
074  n
mi
                                          Hp   =            216
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5687117
52                 X    =         1660334
06
 Y    =       14514076
71  feet           Y    =         4442866
85  meter
 Z    =       15873448
75                 Z    =         4846469
49
 XDOT =     -23774
097331                 XDOT =       -7258
964954
 YDOT =        286
537770  feet/sec       YDOT =           6
232719  meter/sec
 ZDOT =       8228
076037                 ZDOT =        2472
687029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6004709
54                 X    =         1830235
47
 Y    =      -14344911
50  feet           Y    =        -4372329
02  meter
 Z    =       15910219
39                 Z    =         4849434
87
 XDOT =      16367
007813                 XDOT =        4988
663981
 YDOT =      15830
902402  feet/sec       YDOT =        4825
259052  meter/sec
 ZDOT =       8068
679113                 ZDOT =        2459
333394


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   19092
90330781  
00016717  00000-0  10270-3 0  9098
2 25544  51
6399  15
4675 0002144 147
3129 212
8156 15
52476547  3555


Satellite: ISS
Catalog Number: 25544
Epoch time:      19092
90330781   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:        15
4675  deg
Eccentricity:     
0002144     
Arg of perigee:   147
3129  deg
Mean anomaly:     212
8156  deg
Mean motion:   15
52476547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             355
Checksum:              317


Coasting Arc #11 (Orbit 369)
---------------------------------------

Vector Time (GMT): 2019/093/20:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -661210
52                 A    =         6782649
07  meter
 Y    =       -4303430
68  meter          E    =           
0015182
 Z    =       -5213945
37                 I    =           51
69253
 XDOT =       7543
687998                 Wp   =           88
11284
 YDOT =        351
652968  meter/sec      RA   =           10
17959  deg
 ZDOT =      -1249
562433                 TA   =          169
89521
                                          MA   =          169
86466
                                          Ha   =            224
154  n
mi
                                          Hp   =            216
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2169325
84                 X    =         -587712
74
 Y    =      -14118867
06  feet           Y    =        -4310414
43  meter
 Z    =      -17106119
97                 Z    =        -5216978
29
 XDOT =      24749
632541                 XDOT =        7545
264734
 YDOT =       1153
717086  feet/sec       YDOT =         436
020444  meter/sec
 ZDOT =      -4099
614280                 ZDOT =       -1212
914247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8077637
67                 X    =        -2462063
96
 Y    =       11762137
36  feet           Y    =         3585099
47  meter
 Z    =      -17119334
58                 Z    =        -5217973
18
 XDOT =     -16550
563235                 XDOT =       -5044
611674
 YDOT =     -17078
989521  feet/sec       YDOT =       -5205
676006  meter/sec
 ZDOT =      -3933
871703                 ZDOT =       -1199
044095


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   19093
86887551  
00016717  00000-0  10270-3 0  9108
2 25544  51
6404  10
6678 0002254 146
6071 213
5223 15
52475899  3701


Satellite: ISS
Catalog Number: 25544
Epoch time:      19093
86887551   =   yrday
fracday
Element set:     910
Inclination:       51
6404  deg
RA of node:        10
6678  deg
Eccentricity:     
0002254     
Arg of perigee:   146
6071  deg
Mean anomaly:     213
5223  deg
Mean motion:   15
52475899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             370
Checksum:              313


Coasting Arc #12 (Orbit 379)
---------------------------------------

Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2662528
43                 A    =         6784622
56  meter
 Y    =        4087354
18  meter          E    =           
0009363
 Z    =        4710905
03                 I    =           51
68042
 XDOT =      -7015
051605                 Wp   =          122
45430
 YDOT =       1341
414161  meter/sec      RA   =            7
17016  deg
 ZDOT =       2791
974463                 TA   =          299
84981
                                          MA   =          299
94283
                                          Ha   =            223
922  n
mi
                                          Hp   =            216
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8735329
48                 X    =         2593741
57
 Y    =       13409954
65  feet           Y    =         4116744
35  meter
 Z    =       15455725
17                 Z    =         4723671
10
 XDOT =     -23015
261170                 XDOT =       -7043
092200
 YDOT =       4400
965094  feet/sec       YDOT =        1262
810469  meter/sec
 ZDOT =       9160
021203                 ZDOT =        2757
829645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7914789
21                 X    =         2412427
75
 Y    =       13846138
40  feet           Y    =         4220302
99  meter
 Z    =       15512990
31                 Z    =         4728359
45
 XDOT =     -22265
863817                 XDOT =       -6786
635291
 YDOT =       2605
372474  feet/sec       YDOT =         794
117530  meter/sec
 ZDOT =       9005
413595                 ZDOT =        2744
850064


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   19094
51258494  
00016717  00000-0  10270-3 0  9110
2 25544  51
6414   7
4711 0001790 148
5925 211
5334 15
52490258  3805


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
51258494   =   yrday
fracday
Element set:     911
Inclination:       51
6414  deg
RA of node:         7
4711  deg
Eccentricity:     
0001790     
Arg of perigee:   148
5925  deg
Mean anomaly:     211
5334  deg
Mean motion:   15
52490258  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             380
Checksum:              299


Coasting Arc #13 (Orbit 381)
---------------------------------------

Vector Time (GMT): 2019/094/14:24:50
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4844613
39                 A    =         6787505
97  meter
 Y    =        2607491
19  meter          E    =           
0011834
 Z    =        3965331
57                 I    =           51
68675
 XDOT =      -5329
323870                 Wp   =           86
79318
 YDOT =      -3787
861616  meter/sec      RA   =            6
42349  deg
 ZDOT =      -4009
295105                 TA   =           45
03150
                                          MA   =           44
93561
                                          Ha   =            224
042  n
mi
                                          Hp   =            216
896

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15894400
89                 X    =        -4892672
47
 Y    =        8554761
11  feet           Y    =         2553047
05  meter
 Z    =       13009618
01                 Z    =         3941681
18
 XDOT =     -17484
658367                 XDOT =       -5267
095854
 YDOT =     -12427
367506  feet/sec       YDOT =       -3847
110352  meter/sec
 ZDOT =     -13153
855332                 ZDOT =       -4035
031472

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4354285
77                 X    =        -1327186
30
 Y    =       17596478
89  feet           Y    =         5363406
77  meter
 Z    =       12902333
29                 Z    =         3932631
19
 XDOT =     -19598
077471                 XDOT =       -5973
494013
 YDOT =       4906
915119  feet/sec       YDOT =        1495
627728  meter/sec
 ZDOT =     -13269
823251                 ZDOT =       -4044
642127


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   19094
64132621  
00016717  00000-0  10270-3 0  9128
2 25544  51
6430   6
8319 0001592 145
7392 214
3863 15
52503217  3827


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
64132621   =   yrday
fracday
Element set:     912
Inclination:       51
6430  deg
RA of node:         6
8319  deg
Eccentricity:     
0001592     
Arg of perigee:   145
7392  deg
Mean anomaly:     214
3863  deg
Mean motion:   15
52503217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             382
Checksum:              289


Coasting Arc #14 (Orbit 396)
---------------------------------------

Vector Time (GMT): 2019/095/14:24:50
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5574550
60                 A    =         6790164
16  meter
 Y    =       -2319461
98  meter          E    =           
0004970
 Z    =       -3110921
07                 I    =           51
66207
 XDOT =       4370
784250                 Wp   =           90
41385
 YDOT =       3970
352548  meter/sec      RA   =            1
45438  deg
 ZDOT =       4878
607569                 TA   =          233
85852
                                          MA   =          233
90452
                                          Ha   =            223
931  n
mi
                                          Hp   =            217
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18289208
00                 X    =         5615184
40
 Y    =       -7609783
40  feet           Y    =        -2256896
58  meter
 Z    =      -10206433
95                 Z    =        -3083742
88
 XDOT =      14339
843341                 XDOT =        4302
364064
 YDOT =      13026
091036  feet/sec       YDOT =        4018
847663  meter/sec
 ZDOT =      16005
930343                 ZDOT =        4899
672749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6324616
76                 X    =         1927743
19
 Y    =      -18838863
23  feet           Y    =        -5742085
51  meter
 Z    =      -10083237
66                 Z    =        -3073370
84
 XDOT =      17798
107259                 XDOT =        5424
863093
 YDOT =      -2630
547258  feet/sec       YDOT =        -801
790804  meter/sec
 ZDOT =      16100
736444                 ZDOT =        4907
504468


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   19095
60688965  
00016717  00000-0  10270-3 0  9133
2 25544  51
6429   2
0306 0001540 154
9556 205
1670 15
52467757  3974


Satellite: ISS
Catalog Number: 25544
Epoch time:      19095
60688965   =   yrday
fracday
Element set:     913
Inclination:       51
6429  deg
RA of node:         2
0306  deg
Eccentricity:     
0001540     
Arg of perigee:   154
9556  deg
Mean anomaly:     205
1670  deg
Mean motion:   15
52467757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             397
Checksum:              321


Coasting Arc #15 (Orbit 412)
---------------------------------------

Vector Time (GMT): 2019/096/14:24:50
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6135395
70                 A    =         6792369
19  meter
 Y    =        2021677
19  meter          E    =           
0015112
 Z    =        2074370
91                 I    =           51
63640
 XDOT =      -3260
376219                 Wp   =          114
64539
 YDOT =      -4189
275079  meter/sec      RA   =          356
48745  deg
 ZDOT =      -5534
867180                 TA   =           42
40452
                                          MA   =           42
28784
                                          Ha   =            223
946  n
mi
                                          Hp   =            217
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20129250
98                 X    =        -6167622
92
 Y    =        6632799
19  feet           Y    =         1952886
90  meter
 Z    =        6805678
83                 Z    =         2044488
69
 XDOT =     -10696
772373                 XDOT =       -3186
402645
 YDOT =     -13744
340810  feet/sec       YDOT =       -4225
321780  meter/sec
 ZDOT =     -18159
013059                 ZDOT =       -5550
524977

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7917505
10                 X    =        -2413255
55
 Y    =       19705792
12  feet           Y    =         6006325
44  meter
 Z    =        6670300
19                 Z    =         2033107
50
 XDOT =     -15888
987350                 XDOT =       -4842
963344
 YDOT =       -184
508994  feet/sec       YDOT =         -56
238341  meter/sec
 ZDOT =     -18229
327990                 ZDOT =       -5556
299171


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   19096
63682025  
00016717  00000-0  10270-3 0  9149
2 25544  51
6430 356
9090 0001544 152
8370 207
2862 15
52483545  4130


Satellite: ISS
Catalog Number: 25544
Epoch time:      19096
63682025   =   yrday
fracday
Element set:     914
Inclination:       51
6430  deg
RA of node:       356
9090  deg
Eccentricity:     
0001544     
Arg of perigee:   152
8370  deg
Mean anomaly:     207
2862  deg
Mean motion:   15
52483545  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             413
Checksum:              303


Coasting Arc #16 (Orbit 427)
---------------------------------------

Vector Time (GMT): 2019/097/14:24:50
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6489706
79                 A    =         6793778
61  meter
 Y    =       -1745950
76  meter          E    =           
0009268
 Z    =        -971752
95                 I    =           51
60600
 XDOT =       2068
265942                 Wp   =           46
60290
 YDOT =       4423
653763  meter/sec      RA   =          351
52148  deg
 ZDOT =       5906
277979                 TA   =          302
87634
                                          MA   =          302
96550
                                          Ha   =            223
887  n
mi
                                          Hp   =            217
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21291688
95                 X    =         6513468
48
 Y    =       -5728184
91  feet           Y    =        -1673245
53  meter
 Z    =       -3188165
85                 Z    =         -940170
15
 XDOT =       6785
649417                 XDOT =        1989
955883
 YDOT =      14513
299747  feet/sec       YDOT =        4446
345135  meter/sec
 ZDOT =      19377
552424                 ZDOT =        5916
134440

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8997428
38                 X    =         2742416
17
 Y    =      -20151573
68  feet           Y    =        -6142199
66  meter
 Z    =       -3045140
89                 Z    =         -928158
94
 XDOT =      13991
809874                 XDOT =        4264
703650
 YDOT =       3333
962159  feet/sec       YDOT =        1016
191666  meter/sec
 ZDOT =      19421
597959                 ZDOT =        5919
703058


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   19097
60237765  
00016717  00000-0  10270-3 0  9155
2 25544  51
6411 352
1075 0001508 159
1609 200
9604 15
52472372  4281


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
60237765   =   yrday
fracday
Element set:     915
Inclination:       51
6411  deg
RA of node:       352
1075  deg
Eccentricity:     
0001508     
Arg of perigee:   159
1609  deg
Mean anomaly:     200
9604  deg
Mean motion:   15
52472372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             428
Checksum:              300


Coasting Arc #17 (Orbit 431)
---------------------------------------

Vector Time (GMT): 2019/097/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2093883
89                 A    =         6782623
74  meter
 Y    =       -3832165
63  meter          E    =           
0014569
 Z    =       -5202496
83                 I    =           51
56076
 XDOT =       7211
727331                 Wp   =           88
55297
 YDOT =      -2239
083018  meter/sec      RA   =          350
33725  deg
 ZDOT =      -1255
930441                 TA   =          169
37157
                                          MA   =          169
34074
                                          Ha   =            223
939  n
mi
                                          Hp   =            216
893

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6869697
79                 X    =        -2025604
72
 Y    =      -12572721
88  feet           Y    =        -3855199
49  meter
 Z    =      -17068559
16                 Z    =        -5212502
17
 XDOT =      23660
522739                 XDOT =        7242
330095
 YDOT =      -7346
072894  feet/sec       YDOT =       -2158
265411  meter/sec
 ZDOT =      -4120
506695                 ZDOT =       -1220
823630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3411635
77                 X    =        -1039866
58
 Y    =       13859866
07  feet           Y    =         4224487
18  meter
 Z    =      -17113347
10                 Z    =        -5216148
20
 XDOT =     -21494
614454                 XDOT =       -6551
558485
 YDOT =     -10171
494605  feet/sec       YDOT =       -3100
271556  meter/sec
 ZDOT =      -3961
490405                 ZDOT =       -1207
462275


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   19097
85986093  
00016717  00000-0  10270-3 0  9168
2 25544  51
6408 350
8234 0002122 162
3810 197
7416 15
52486651  4326


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
85986093   =   yrday
fracday
Element set:     916
Inclination:       51
6408  deg
RA of node:       350
8234  deg
Eccentricity:     
0002122     
Arg of perigee:   162
3810  deg
Mean anomaly:     197
7416  deg
Mean motion:   15
52486651  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             432
Checksum:              318


Coasting Arc #18 (Orbit 447)
---------------------------------------

Vector Time (GMT): 2019/098/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1008945
65                 A    =         6782096
32  meter
 Y    =        4096065
51  meter          E    =           
0003348
 Z    =        5307995
65                 I    =           51
52711
 XDOT =      -7429
708049                 Wp   =          121
89230
 YDOT =       1898
050003  meter/sec      RA   =          345
34777  deg
 ZDOT =        -54
149912                 TA   =          328
61450
                                          MA   =          328
63447
                                          Ha   =            223
796  n
mi
                                          Hp   =            217
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3310189
15                 X    =          937283
65
 Y    =       13438535
12  feet           Y    =         4106947
81  meter
 Z    =       17414683
90                 Z    =         5312722
55
 XDOT =     -24375
682577                 XDOT =       -7450
117357
 YDOT =       6227
198172  feet/sec       YDOT =        1814
851690  meter/sec
 ZDOT =       -177
657191                 ZDOT =         -90
290801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6426212
33                 X    =         1958709
52
 Y    =      -12228144
43  feet           Y    =        -3727138
42  meter
 Z    =       17435569
18                 Z    =         5314361
49
 XDOT =      21571
257441                 XDOT =        6574
919268
 YDOT =      10857
599596  feet/sec       YDOT =        3309
396357  meter/sec
 ZDOT =       -341
298128                 ZDOT =        -104
027669


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   19098
88978613  
00016717  00000-0  10270-3 0  9172
2 25544  51
6414 345
7012 0002042 168
5136 191
6062 15
52499215  4487


Satellite: ISS
Catalog Number: 25544
Epoch time:      19098
88978613   =   yrday
fracday
Element set:     917
Inclination:       51
6414  deg
RA of node:       345
7012  deg
Eccentricity:     
0002042     
Arg of perigee:   168
5136  deg
Mean anomaly:     191
6062  deg
Mean motion:   15
52499215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             448
Checksum:              323
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