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

 
Date: March 28th 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 1
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

094/14:25:00 000 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 255)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4107361
51                 A    =         6793893
42  meter
 Y    =       -5335796
51  meter          E    =           
0011937
 Z    =        -865275
78                 I    =           51
93988
 XDOT =       4237
812275                 Wp   =          136
81547
 YDOT =      -2305
433086  meter/sec      RA   =           46
63732  deg
 ZDOT =      -5956
659535                 TA   =           52
50020
                                          MA   =           52
39173
                                          Ha   =            224
313  n
mi
                                          Hp   =            216
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13475595
52                 X    =        -4043186
84
 Y    =      -17505894
06  feet           Y    =        -5381369
12  meter
 Z    =       -2838831
31                 Z    =         -885071
62
 XDOT =      13903
583581                 XDOT =        4292
211394
 YDOT =      -7563
756843  feet/sec       YDOT =       -2257
739042  meter/sec
 ZDOT =     -19542
846242                 ZDOT =       -5935
941642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14571340
05                 X    =        -4441344
45
 Y    =      -16589480
94  feet           Y    =        -5056473
79  meter
 Z    =       -2927820
96                 Z    =         -892399
83
 XDOT =      12300
113760                 XDOT =        3749
074674
 YDOT =      -7403
279687  feet/sec       YDOT =       -2256
519649  meter/sec
 ZDOT =     -19448
823938                 ZDOT =       -5928
001536


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
53050576  
00016717  00000-0  10270-3 0  9002
2 25544  51
6400  47
1586 0002034 118
7833 241
3523 15
52443233  2564


Satellite: ISS
Catalog Number: 25544
Epoch time:      19086
53050576   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:        47
1586  deg
Eccentricity:     
0002034     
Arg of perigee:   118
7833  deg
Mean anomaly:     241
3523  deg
Mean motion:   15
52443233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             256
Checksum:              280


Coasting Arc #2 (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    =       -3278572
69                 A    =         6791928
32  meter
 Y    =       -5486412
14  meter          E    =           
0008035
 Z    =       -2293299
26                 I    =           51
91715
 XDOT =       5310
205910                 Wp   =          132
07409
 YDOT =       -902
525642  meter/sec      RA   =           42
80821  deg
 ZDOT =      -5449
925407                 TA   =           73
33440
                                          MA   =           73
24621
                                          Ha   =            224
329  n
mi
                                          Hp   =            216
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10756472
06                 X    =        -3205838
88
 Y    =      -18000039
82  feet           Y    =        -5522668
87  meter
 Z    =       -7523947
71                 Z    =        -2309048
33
 XDOT =      17421
935400                 XDOT =        5346
376130
 YDOT =      -2961
042131  feet/sec       YDOT =        -842
941242  meter/sec
 ZDOT =     -17880
332699                 ZDOT =       -5424
042645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14969375
28                 X    =         4562665
59
 Y    =      -14647620
90  feet           Y    =        -4464594
85  meter
 Z    =       -7594598
05                 Z    =        -2314833
48
 XDOT =       5945
840868                 XDOT =        1812
292297
 YDOT =      15256
954329  feet/sec       YDOT =        4650
319679  meter/sec
 ZDOT =     -17763
094504                 ZDOT =       -5414
191205


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
30296931  
00016717  00000-0  10270-3 0  9016
2 25544  51
6418  43
3179 0002249 125
4430 234
6932 15
52454595  2680


Satellite: ISS
Catalog Number: 25544
Epoch time:      19087
30296931   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:        43
3179  deg
Eccentricity:     
0002249     
Arg of perigee:   125
4430  deg
Mean anomaly:     234
6932  deg
Mean motion:   15
52454595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             268
Checksum:              310


Coasting Arc #3 (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    =        2669192
68                 A    =         6789720
49  meter
 Y    =        5315998
57  meter          E    =           
0014573
 Z    =        3261748
19                 I    =           51
88323
 XDOT =      -6002
962019                 Wp   =           92
82321
 YDOT =         75
017696  meter/sec      RA   =           37
85780  deg
 ZDOT =       4771
092427                 TA   =          304
84684
                                          MA   =          304
98380
                                          Ha   =            224
382  n
mi
                                          Hp   =            216
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8757193
83                 X    =         2593705
65
 Y    =       17440940
20  feet           Y    =         5345425
46  meter
 Z    =       10701273
58                 Z    =         3274530
39
 XDOT =     -19694
757279                 XDOT =       -6026
529890
 YDOT =        246
121050  feet/sec       YDOT =           7
756871  meter/sec
 ZDOT =      15653
190376                 ZDOT =        4741
875252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14684437
13                 X    =        -4475816
44
 Y    =       12806791
36  feet           Y    =         3903510
01  meter
 Z    =       10758508
10                 Z    =         3279193
27
 XDOT =      -4303
048464                 XDOT =       -1311
569172
 YDOT =     -18024
762255  feet/sec       YDOT =       -5493
947535  meter/sec
 ZDOT =      15520
959928                 ZDOT =        4730
788586


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
33291910  
00016717  00000-0  10270-3 0  9023
2 25544  51
6406  38
1965 0002307 125
2498 234
8870 15
52430468  2843


Satellite: ISS
Catalog Number: 25544
Epoch time:      19088
33291910   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:        38
1965  deg
Eccentricity:     
0002307     
Arg of perigee:   125
2498  deg
Mean anomaly:     234
8870  deg
Mean motion:   15
52430468  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             284
Checksum:              310


Coasting Arc #4 (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    =       -1882020
96                 A    =         6786974
37  meter
 Y    =       -5066289
66  meter          E    =           
0008799
 Z    =       -4113644
41                 I    =           51
84935
 XDOT =       6589
899111                 Wp   =           82
90544
 YDOT =        667
710705  meter/sec      RA   =           32
90140  deg
 ZDOT =      -3843
252880                 TA   =          147
46443
                                          MA   =          147
41017
                                          Ha   =            224
264  n
mi
                                          Hp   =            216
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6174609
45                 X    =        -1805246
77
 Y    =      -16621685
23  feet           Y    =        -5086906
74  meter
 Z    =      -13496208
71                 Z    =        -4122599
68
 XDOT =      21620
403909                 XDOT =        6600
611038
 YDOT =       2190
651920  feet/sec       YDOT =         741
463204  meter/sec
 ZDOT =     -12609
097374                 ZDOT =       -3811
215924

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14372913
42                 X    =         4380864
01
 Y    =      -10331793
38  feet           Y    =        -3149130
62  meter
 Z    =      -13536147
03                 Z    =        -4125817
61
 XDOT =       2976
659278                 XDOT =         907
285748
 YDOT =      20445
177756  feet/sec       YDOT =        6231
690180  meter/sec
 ZDOT =     -12464
198158                 ZDOT =       -3799
087599


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
29849073  
00016717  00000-0  10270-3 0  9039
2 25544  51
6425  33
3956 0002182 131
1541 228
9799 15
52465464  2991


Satellite: ISS
Catalog Number: 25544
Epoch time:      19089
29849073   =   yrday
fracday
Element set:     903
Inclination:       51
6425  deg
RA of node:        33
3956  deg
Eccentricity:     
0002182     
Arg of perigee:   131
1541  deg
Mean anomaly:     228
9799  deg
Mean motion:   15
52465464  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             299
Checksum:              334


Coasting Arc #5 (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    =         996944
70                 A    =         6784651
36  meter
 Y    =        4747454
59  meter          E    =           
0009873
 Z    =        4738179
66                 I    =           51
81120
 XDOT =      -7041
279514                 Wp   =          120
22251
 YDOT =      -1280
657726  meter/sec      RA   =           27
93797  deg
 ZDOT =       2755
565240                 TA   =          302
52608
                                          MA   =          302
62144
                                          Ha   =            224
283  n
mi
                                          Hp   =            216
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3270815
95                 X    =          920767
98
 Y    =       15575638
43  feet           Y    =         4758177
57  meter
 Z    =       15545208
87                 Z    =         4742837
01
 XDOT =     -23101
310743                 XDOT =       -7039
820406
 YDOT =      -4201
632960  feet/sec       YDOT =       -1359
389864  meter/sec
 ZDOT =       9040
568373                 ZDOT =        2721
365292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14023806
82                 X    =        -4274456
32
 Y    =        7482856
09  feet           Y    =         2280774
54  meter
 Z    =       15565730
80                 Z    =         4744434
75
 XDOT =      -2042
147653                 XDOT =        -622
446605
 YDOT =     -22373
929633  feet/sec       YDOT =       -6819
573752  meter/sec
 ZDOT =       8885
961436                 ZDOT =        2708
441046


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
32843181  
00016717  00000-0  10270-3 0  9040
2 25544  51
6408  28
2740 0002228 131
2442 228
8902 15
52457758  3159


Satellite: ISS
Catalog Number: 25544
Epoch time:      19090
32843181   =   yrday
fracday
Element set:     904
Inclination:       51
6408  deg
RA of node:        28
2740  deg
Eccentricity:     
0002228     
Arg of perigee:   131
2442  deg
Mean anomaly:     228
8902  deg
Mean motion:   15
52457758  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             315
Checksum:              293


Coasting Arc #6 (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    =        3529732
94                 A    =         6789018
85  meter
 Y    =        4651938
79  meter          E    =           
0013760
 Z    =        3453009
66                 I    =           51
80610
 XDOT =      -6033
989707                 Wp   =           98
02459
 YDOT =       1160
323979  meter/sec      RA   =           25
08541  deg
 ZDOT =       4587
355172                 TA   =          302
33905
                                          MA   =          302
47220
                                          Ha   =            224
133  n
mi
                                          Hp   =            216
726

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11580488
63                 X    =         3460678
64
 Y    =       15262266
38  feet           Y    =         4691024
93  meter
 Z    =       11328771
84                 Z    =         3469987
51
 XDOT =     -19796
554157                 XDOT =       -6068
798962
 YDOT =       3806
837201  feet/sec       YDOT =        1092
653450  meter/sec
 ZDOT =      15050
377861                 ZDOT =        4557
959915

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2893968
95                 X    =          882081
73
 Y    =      -18892731
59  feet           Y    =        -5758504
59  meter
 Z    =       11405051
52                 Z    =         3476259
70
 XDOT =      15240
673617                 XDOT =        4645
357318
 YDOT =      11374
128484  feet/sec       YDOT =        3466
834362  meter/sec
 ZDOT =      14917
232934                 ZDOT =        4546
772598


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
90777222  
00016717  00000-0  10270-3 0  9057
2 25544  51
6380  25
3900 0002231 143
2689 216
8616 15
52477646  3241


Satellite: ISS
Catalog Number: 25544
Epoch time:      19090
90777222   =   yrday
fracday
Element set:     905
Inclination:       51
6380  deg
RA of node:        25
3900  deg
Eccentricity:     
0002231     
Arg of perigee:   143
2689  deg
Mean anomaly:     216
8616  deg
Mean motion:   15
52477646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             324
Checksum:              302


Coasting Arc #7 (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    =       -2671450
80                 A    =         6786352
50  meter
 Y    =       -4558995
57  meter          E    =           
0009240
 Z    =       -4267043
86                 I    =           51
76863
 XDOT =       6728
112067                 Wp   =           82
49609
 YDOT =       -566
123577  meter/sec      RA   =           20
12305  deg
 ZDOT =      -3612
914693                 TA   =          150
61554
                                          MA   =          150
56356
                                          Ha   =            224
151  n
mi
                                          Hp   =            216
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8764602
36                 X    =        -2599545
48
 Y    =      -14957334
53  feet           Y    =        -4588467
97  meter
 Z    =      -13999487
73                 Z    =        -4279845
59
 XDOT =      22073
858487                 XDOT =        6751
491994
 YDOT =      -1857
360818  feet/sec       YDOT =        -490
754750  meter/sec
 ZDOT =     -11853
394663                 ZDOT =       -3580
175428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4367233
44                 X    =        -1331132
75
 Y    =       16728935
32  feet           Y    =         5098979
48  meter
 Z    =      -14056875
99                 Z    =        -4284535
80
 XDOT =     -15825
775912                 XDOT =       -4823
696498
 YDOT =     -13951
836123  feet/sec       YDOT =       -4252
519650  meter/sec
 ZDOT =     -11705
199254                 ZDOT =       -3567
744733


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
87333744  
00016717  00000-0  10270-3 0  9062
2 25544  51
6399  20
5894 0002215 142
3051 217
8257 15
52485597  3397


Satellite: ISS
Catalog Number: 25544
Epoch time:      19091
87333744   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:        20
5894  deg
Eccentricity:     
0002215     
Arg of perigee:   142
3051  deg
Mean anomaly:     217
8257  deg
Mean motion:   15
52485597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             339
Checksum:              323


Coasting Arc #8 (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    =        1708499
06                 A    =         6784086
33  meter
 Y    =        4424146
58  meter          E    =           
0008971
 Z    =        4846827
91                 I    =           51
72947
 XDOT =      -7253
886911                 Wp   =          126
59098
 YDOT =         67
946817  meter/sec      RA   =           15
15257  deg
 ZDOT =       2486
545026                 TA   =          298
96994
                                          MA   =          299
05985
                                          Ha   =            224
037  n
mi
                                          Hp   =            216
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5605311
87                 X    =         1635356
91
 Y    =       14514916
61  feet           Y    =         4442843
77  meter
 Z    =       15901666
36                 Z    =         4854949
00
 XDOT =     -23798
841573                 XDOT =       -7266
185799
 YDOT =        222
922629  feet/sec       YDOT =         -13
239723  meter/sec
 ZDOT =       8157
956122                 ZDOT =        2451
278625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6064525
66                 X    =         1848467
42
 Y    =      -14288826
26  feet           Y    =        -4355234
24  meter
 Z    =       15937888
53                 Z    =         4857868
43
 XDOT =      16344
644578                 XDOT =        4981
847667
 YDOT =      15889
285631  feet/sec       YDOT =        4843
054260  meter/sec
 ZDOT =       7998
399266                 ZDOT =        2437
912096


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
90326717  
00016717  00000-0  10270-3 0  9070
2 25544  51
6399  15
4670 0002177 149
4306 210
6973 15
52493335  3553


Satellite: ISS
Catalog Number: 25544
Epoch time:      19092
90326717   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:        15
4670  deg
Eccentricity:     
0002177     
Arg of perigee:   149
4306  deg
Mean anomaly:     210
6973  deg
Mean motion:   15
52493335  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             355
Checksum:              317


Coasting Arc #9 (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    =        -627370
19                 A    =         6782568
10  meter
 Y    =       -4301727
27  meter          E    =           
0015166
 Z    =       -5219403
88                 I    =           51
69240
 XDOT =       7547
442317                 Wp   =           88
56580
 YDOT =        376
043185  meter/sec      RA   =           10
17848  deg
 ZDOT =      -1219
823647                 TA   =          169
73243
                                          MA   =          169
70142
                                          Ha   =            224
110  n
mi
                                          Hp   =            216
736

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2058301
15                 X    =         -553867
46
 Y    =      -14113278
43  feet           Y    =        -4308332
56  meter
 Z    =      -17124028
46                 Z    =        -5222272
40
 XDOT =      24761
949860                 XDOT =        7548
601581
 YDOT =       1233
737482  feet/sec       YDOT =         460
450313  meter/sec
 ZDOT =      -4002
046087                 ZDOT =       -1183
158242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8155446
77                 X    =        -2485780
18
 Y    =       11682578
99  feet           Y    =         3560850
08  meter
 Z    =      -17136499
60                 Z    =        -5223205
08
 XDOT =     -16510
597114                 XDOT =       -5032
430000
 YDOT =     -17139
991368  feet/sec       YDOT =       -5224
269369  meter/sec
 ZDOT =      -3836
228479                 ZDOT =       -1169
282440


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
86882332  
00016717  00000-0  10270-3 0  9087
2 25544  51
6404  10
6673 0002284 148
8214 211
3074 15
52495649  3707


Satellite: ISS
Catalog Number: 25544
Epoch time:      19093
86882332   =   yrday
fracday
Element set:     908
Inclination:       51
6404  deg
RA of node:        10
6673  deg
Eccentricity:     
0002284     
Arg of perigee:   148
8214  deg
Mean anomaly:     211
3074  deg
Mean motion:   15
52495649  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             370
Checksum:              308


Coasting Arc #10 (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    =        2626254
75                 A    =         6784502
35  meter
 Y    =        4094192
11  meter          E    =           
0009273
 Z    =        4725257
12                 I    =           51
68019
 XDOT =      -7032
458111                 Wp   =          123
36598
 YDOT =       1314
496067  meter/sec      RA   =            7
16902  deg
 ZDOT =       2760
734558                 TA   =          299
27344
                                          MA   =          299
36610
                                          Ha   =            223
872  n
mi
                                          Hp   =            216
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8616321
34                 X    =         2557324
41
 Y    =       13432388
81  feet           Y    =         4123175
84  meter
 Z    =       15502812
07                 Z    =         4737846
63
 XDOT =     -23072
369131                 XDOT =       -7060
044660
 YDOT =       4312
651139  feet/sec       YDOT =        1235
700259  meter/sec
 ZDOT =       9057
528078                 ZDOT =        2726
506292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7794454
02                 X    =         2375749
59
 Y    =       13862272
75  feet           Y    =         4225220
74  meter
 Z    =       15559277
79                 Z    =         4742467
87
 XDOT =     -22316
387274                 XDOT =       -6802
034841
 YDOT =       2522
983218  feet/sec       YDOT =         769
005285  meter/sec
 ZDOT =       8902
546169                 ZDOT =        2713
496072


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
51252414  
00016717  00000-0  10270-3 0  9093
2 25544  51
6414   7
4705 0001818 151
5014 208
6237 15
52512039  3803


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
51252414   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:         7
4705  deg
Eccentricity:     
0001818     
Arg of perigee:   151
5014  deg
Mean anomaly:     208
6237  deg
Mean motion:   15
52512039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             380
Checksum:              280


Coasting Arc #11 (Orbit 381)
---------------------------------------

Vector Time (GMT): 2019/094/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4925505
34                 A    =         6787653
31  meter
 Y    =        2549071
33  meter          E    =           
0011990
 Z    =        3903234
63                 I    =           51
68739
 XDOT =      -5233
734895                 Wp   =           88
16670
 YDOT =      -3838
310552  meter/sec      RA   =            6
42185  deg
 ZDOT =      -4086
576572                 TA   =           44
65191
                                          MA   =           44
55541
                                          Ha   =            223
994  n
mi
                                          Hp   =            216
883

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16159794
44                 X    =        -4972603
51
 Y    =        8363094
93  feet           Y    =         2493727
98  meter
 Z    =       12805887
91                 Z    =         3879193
64
 XDOT =     -17171
046243                 XDOT =       -5170
574457
 YDOT =     -12592
882390  feet/sec       YDOT =       -3896
485141  meter/sec
 ZDOT =     -13407
403450                 ZDOT =       -4111
846331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4660588
23                 X    =        -1420547
29
 Y    =       17667488
99  feet           Y    =         5385050
64  meter
 Z    =       12696843
24                 Z    =         3869997
82
 XDOT =     -19501
463977                 XDOT =       -5944
046220
 YDOT =       4599
428947  feet/sec       YDOT =        1401
905943  meter/sec
 ZDOT =     -13521
254822                 ZDOT =       -4121
278470


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
64126367  
00016717  00000-0  10270-3 0  9106
2 25544  51
6429   6
8313 0001621 148
8179 211
3069 15
52523772  3822


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
64126367   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:         6
8313  deg
Eccentricity:     
0001621     
Arg of perigee:   148
8179  deg
Mean anomaly:     211
3069  deg
Mean motion:   15
52523772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             382
Checksum:              302


Coasting Arc #12 (Orbit 396)
---------------------------------------

Vector Time (GMT): 2019/095/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5646262
30                 A    =         6790306
73  meter
 Y    =       -2253005
86  meter          E    =           
0004815
 Z    =       -3029112
15                 I    =           51
66272
 XDOT =       4252
071335                 Wp   =           87
42924
 YDOT =       4018
717449  meter/sec      RA   =            1
45297  deg
 ZDOT =       4943
806676                 TA   =          237
91942
                                          MA   =          237
96618
                                          Ha   =            223
875  n
mi
                                          Hp   =            217
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18524482
62                 X    =         5685750
26
 Y    =       -7391751
53  feet           Y    =        -2189644
93  meter
 Z    =       -9938032
00                 Z    =        -3001588
40
 XDOT =      13950
365272                 XDOT =        4182
802438
 YDOT =      13184
768534  feet/sec       YDOT =        4065
880295  meter/sec
 ZDOT =      16219
838177                 ZDOT =        4964
293124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6628632
81                 X    =         2020407
28
 Y    =      -18876431
80  feet           Y    =        -5753536
41  meter
 Z    =       -9813280
63                 Z    =        -2991087
94
 XDOT =      17656
855152                 XDOT =        5381
809450
 YDOT =      -2267
649231  feet/sec       YDOT =        -691
179486  meter/sec
 ZDOT =      16312
021049                 ZDOT =        4971
904016


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
60681262  
00016717  00000-0  10270-3 0  9114
2 25544  51
6429   2
0299 0001570 158
2707 201
8511 15
52491080  3976


Satellite: ISS
Catalog Number: 25544
Epoch time:      19095
60681262   =   yrday
fracday
Element set:     911
Inclination:       51
6429  deg
RA of node:         2
0299  deg
Eccentricity:     
0001570     
Arg of perigee:   158
2707  deg
Mean anomaly:     201
8511  deg
Mean motion:   15
52491080  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             397
Checksum:              294


Coasting Arc #13 (Orbit 412)
---------------------------------------

Vector Time (GMT): 2019/096/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6192837
92                 A    =         6792469
12  meter
 Y    =        1945720
11  meter          E    =           
0015121
 Z    =        1974015
56                 I    =           51
63691
 XDOT =      -3118
300687                 Wp   =          116
28324
 YDOT =      -4235
025656  meter/sec      RA   =          356
48626  deg
 ZDOT =      -5581
735975                 TA   =           41
93575
                                          MA   =           41
82005
                                          Ha   =            223
887  n
mi
                                          Hp   =            216
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20317709
71                 X    =        -6223724
02
 Y    =        6383596
15  feet           Y    =         1876294
94  meter
 Z    =        6476429
02                 Z    =         1943857
58
 XDOT =     -10230
645298                 XDOT =       -3043
598411
 YDOT =     -13894
441127  feet/sec       YDOT =       -4269
479499  meter/sec
 ZDOT =     -18312
782070                 ZDOT =       -5596
701840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8213754
74                 X    =        -2503552
45
 Y    =       19693775
02  feet           Y    =         6002662
62  meter
 Z    =        6339812
23                 Z    =         1932374
77
 XDOT =     -15704
746164                 XDOT =       -4786
806631
 YDOT =       -604
458813  feet/sec       YDOT =        -184
239046  meter/sec
 ZDOT =     -18379
962394                 ZDOT =       -5602
212538


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
63672619  
00016717  00000-0  10270-3 0  9125
2 25544  51
6430 356
9082 0001585 156
4926 203
6298 15
52507307  4139


Satellite: ISS
Catalog Number: 25544
Epoch time:      19096
63672619   =   yrday
fracday
Element set:     912
Inclination:       51
6430  deg
RA of node:       356
9082  deg
Eccentricity:     
0001585     
Arg of perigee:   156
4926  deg
Mean anomaly:     203
6298  deg
Mean motion:   15
52507307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             413
Checksum:              318


Coasting Arc #14 (Orbit 427)
---------------------------------------

Vector Time (GMT): 2019/097/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6528683
35                 A    =         6793772
84  meter
 Y    =       -1658672
10  meter          E    =           
0009482
 Z    =        -855408
99                 I    =           51
60625
 XDOT =       1905
285895                 Wp   =           46
96075
 YDOT =       4466
271791  meter/sec      RA   =          351
52039  deg
 ZDOT =       5929
229262                 TA   =          303
78974
                                          MA   =          303
88001
                                          Ha   =            223
814  n
mi
                                          Hp   =            217
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21419564
79                 X    =         6550901
02
 Y    =       -5441837
59  feet           Y    =        -1585539
63  meter
 Z    =       -2806459
95                 Z    =         -823640
61
 XDOT =       6250
937975                 XDOT =        1826
399896
 YDOT =      14653
122675  feet/sec       YDOT =        4487
137388  meter/sec
 ZDOT =      19452
851908                 ZDOT =        5938
292615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9284058
12                 X    =         2829780
91
 Y    =      -20074968
56  feet           Y    =        -6118850
42  meter
 Z    =       -2662606
16                 Z    =         -811562
36
 XDOT =      13771
601347                 XDOT =        4197
584091
 YDOT =       3805
462671  feet/sec       YDOT =        1159
905022  meter/sec
 ZDOT =      19493
305941                 ZDOT =        5941
559651


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
60226586  
00016717  00000-0  10270-3 0  9132
2 25544  51
6410 352
1066 0001550 162
9015 197
2190 15
52503886  4283


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
60226586   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:       352
1066  deg
Eccentricity:     
0001550     
Arg of perigee:   162
9015  deg
Mean anomaly:     197
2190  deg
Mean motion:   15
52503886  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             428
Checksum:              299


Coasting Arc #15 (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    =       -2021294
27                 A    =         6782482
04  meter
 Y    =       -3854304
00  meter          E    =           
0014582
 Z    =       -5214663
21                 I    =           51
56052
 XDOT =       7238
025151                 Wp   =           89
22607
 YDOT =      -2190
275822  meter/sec      RA   =          350
33509  deg
 ZDOT =      -1189
381674                 TA   =          169
34817
                                          MA   =          169
31725
                                          Ha   =            223
869  n
mi
                                          Hp   =            216
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6631542
89                 X    =        -1952713
85
 Y    =      -12645354
33  feet           Y    =        -3876524
43  meter
 Z    =      -17108475
09                 Z    =        -5224315
19
 XDOT =      23746
801675                 XDOT =        7267
756923
 YDOT =      -7185
944298  feet/sec       YDOT =       -2109
169000  meter/sec
 ZDOT =      -3902
170847                 ZDOT =       -1154
149236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3637277
43                 X    =        -1108642
16
 Y    =       13754015
81  feet           Y    =         4192224
02  meter
 Z    =      -17151662
58                 Z    =        -5227826
75
 XDOT =     -21457
975456                 XDOT =       -6540
390919
 YDOT =     -10330
744199  feet/sec       YDOT =       -3148
810832  meter/sec
 ZDOT =      -3742
592285                 ZDOT =       -1140
742129


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
85974417  
00016717  00000-0  10270-3 0  9143
2 25544  51
6408 350
8225 0002158 165
0205 195
1011 15
52517464  4323


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
85974417   =   yrday
fracday
Element set:     914
Inclination:       51
6408  deg
RA of node:       350
8225  deg
Eccentricity:     
0002158     
Arg of perigee:   165
0205  deg
Mean anomaly:     195
1011  deg
Mean motion:   15
52517464  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             432
Checksum:              300


Coasting Arc #16 (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    =         921484
36                 A    =         6782014
93  meter
 Y    =        4118011
37  meter          E    =           
0003232
 Z    =        5306859
42                 I    =           51
52708
 XDOT =      -7444
150166                 Wp   =          121
00185
 YDOT =       1836
530711  meter/sec      RA   =          345
34522  deg
 ZDOT =       -134
075258                 TA   =          330
26861
                                          MA   =          330
28698
                                          Ha   =            223
728  n
mi
                                          Hp   =            217
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3023242
64                 X    =          849588
97
 Y    =       13510536
00  feet           Y    =         4127914
31  meter
 Z    =       17410956
10                 Z    =         5311160
89
 XDOT =     -24423
064848                 XDOT =       -7463
482236
 YDOT =       6025
363226  feet/sec       YDOT =        1753
176916  meter/sec
 ZDOT =       -439
879454                 ZDOT =        -170
283682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6689776
63                 X    =         2039043
92
 Y    =      -12093838
01  feet           Y    =        -3686201
83  meter
 Z    =       17429915
16                 Z    =         5312638
14
 XDOT =      21482
772831                 XDOT =        6547
949159
 YDOT =      11020
499353  feet/sec       YDOT =        3359
048203  meter/sec
 ZDOT =       -603
818426                 ZDOT =        -184
043856


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
88964864  
00016717  00000-0  10270-3 0  9153
2 25544  51
6414 345
7001 0002082 171
1412 188
9777 15
52529729  4482


Satellite: ISS
Catalog Number: 25544
Epoch time:      19098
88964864   =   yrday
fracday
Element set:     915
Inclination:       51
6414  deg
RA of node:       345
7001  deg
Eccentricity:     
0002082     
Arg of perigee:   171
1412  deg
Mean anomaly:     188
9777  deg
Mean motion:   15
52529729  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             448
Checksum:              339


Coasting Arc #17 (Orbit 462)
---------------------------------------

Vector Time (GMT): 2019/099/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         176956
36                 A    =         6782734
02  meter
 Y    =       -4418344
36  meter          E    =           
0014551
 Z    =       -5156156
45                 I    =           51
49809
 XDOT =       7382
486104                 Wp   =          108
69374
 YDOT =      -1405
241732  meter/sec      RA   =          340
35481  deg
 ZDOT =       1456
340679                 TA   =          175
38284
                                          MA   =          175
36940
                                          Ha   =            223
757  n
mi
                                          Hp   =            216
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         580565
49                 X    =          251396
44
 Y    =      -14495880
45  feet           Y    =        -4415949
43  meter
 Z    =      -16916523
79                 Z    =        -5155115
93
 XDOT =      24220
754933                 XDOT =        7390
577053
 YDOT =      -4610
373135  feet/sec       YDOT =       -1322
640329  meter/sec
 ZDOT =       4778
020602                 ZDOT =        1492
222155

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9869348
56                 X    =        -3008177
44
 Y    =       10641452
82  feet           Y    =         3243514
82  meter
 Z    =      -16911292
80                 Z    =        -5154562
05
 XDOT =     -20694
681581                 XDOT =       -6307
738946
 YDOT =     -11335
713687  feet/sec       YDOT =       -3455
125532  meter/sec
 ZDOT =       4940
421252                 ZDOT =        1505
840397


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   19099
85518081  
00016717  00000-0  10270-3 0  9168
2 25544  51
6419 340
8995 0002090 170
8133 189
3057 15
52541584  4636


Satellite: ISS
Catalog Number: 25544
Epoch time:      19099
85518081   =   yrday
fracday
Element set:     916
Inclination:       51
6419  deg
RA of node:       340
8995  deg
Eccentricity:     
0002090     
Arg of perigee:   170
8133  deg
Mean anomaly:     189
3057  deg
Mean motion:   15
52541584  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              328


Coasting Arc #18 (Orbit 478)
---------------------------------------

Vector Time (GMT): 2019/100/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1219786
92                 A    =         6784595
12  meter
 Y    =        4702763
73  meter          E    =           
0007418
 Z    =        4730102
82                 I    =           51
47257
 XDOT =      -7118
209332                 Wp   =           77
80245
 YDOT =        887
833093  meter/sec      RA   =          335
36346  deg
 ZDOT =      -2713
186044                 TA   =           39
11013
                                          MA   =           39
05654
                                          Ha   =            223
816  n
mi
                                          Hp   =            217
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4001925
57                 X    =        -1295260
32
 Y    =       15429014
88  feet           Y    =         4688701
28  meter
 Z    =       15518710
03                 Z    =         4723994
13
 XDOT =     -23353
705157                 XDOT =       -7114
429024
 YDOT =       2912
838230  feet/sec       YDOT =         808
253403  meter/sec
 ZDOT =      -8901
529017                 ZDOT =       -2747
754775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12920642
81                 X    =         3938211
93
 Y    =       -9380866
26  feet           Y    =        -2859288
04  meter
 Z    =       15490532
82                 Z    =         4721514
40
 XDOT =      19225
499118                 XDOT =        5859
932131
 YDOT =      11494
880446  feet/sec       YDOT =        3503
639560  meter/sec
 ZDOT =      -9057
926267                 ZDOT =       -2760
855926


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   19100
88507925  
00016717  00000-0  10270-3 0  9170
2 25544  51
6415 335
7775 0002077 171
8008 188
3178 15
52507650  4794


Satellite: ISS
Catalog Number: 25544
Epoch time:      19100
88507925   =   yrday
fracday
Element set:     917
Inclination:       51
6415  deg
RA of node:       335
7775  deg
Eccentricity:     
0002077     
Arg of perigee:   171
8008  deg
Mean anomaly:     188
3178  deg
Mean motion:   15
52507650  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             479
Checksum:              328
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