[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: February 4th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


033/17:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 216 5

034/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 216 4

037/01:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 216 1

039/16:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 215 6

040/11:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 215 5

044/15:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 7
000/00:00:00 000 0 0 0 0 215 1

Coasting Arc #1 (Orbit 3417)
---------------------------------------

Vector Time (GMT): 2019/032/14:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5157316
06                 A    =         6783581
05  meter
 Y    =         169470
41  meter          E    =           
0010513
 Z    =       -4413918
84                 I    =           51
36568
 XDOT =       2631
284943                 Wp   =           38
86550
 YDOT =      -6381
540030  meter/sec      RA   =          314
98515  deg
 ZDOT =      -3315
746806                 TA   =          197
45391
                                          MA   =          197
49007
                                          Ha   =            222
645  n
mi
                                          Hp   =            216
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16920328
29                 X    =        -5137387
94
 Y    =         556005
29  feet           Y    =          111909
31  meter
 Z    =      -14481361
01                 Z    =        -4438922
18
 XDOT =       8632
824615                 XDOT =        2718
555260
 YDOT =     -20936
811122  feet/sec       YDOT =       -6351
627079  meter/sec
 ZDOT =     -10878
434403                 ZDOT =       -3302
753583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16052789
29                 X    =        -4892890
18
 Y    =       -5063055
58  feet           Y    =        -1543219
34  meter
 Z    =      -14594173
23                 Z    =        -4448304
00
 XDOT =      14794
963212                 XDOT =        4509
504787
 YDOT =     -15688
041069  feet/sec       YDOT =       -4781
714918  meter/sec
 ZDOT =     -10818
998261                 ZDOT =       -3297
630670


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   19032
60538886  
00016717  00000-0  10270-3 0  9006
2 25544  51
6422 315
5198 0005298 337
7898  22
3024 15
53229580 34182


Satellite: ISS
Catalog Number: 25544
Epoch time:      19032
60538886   =   yrday
fracday
Element set:     900
Inclination:       51
6422  deg
RA of node:       315
5198  deg
Eccentricity:     
0005298     
Arg of perigee:   337
7898  deg
Mean anomaly:      22
3024  deg
Mean motion:   15
53229580  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3418
Checksum:              322


Coasting Arc #2 (Orbit 3433)
---------------------------------------

Vector Time (GMT): 2019/033/14:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4449560
78                 A    =         6781127
53  meter
 Y    =         951063
97  meter          E    =           
0003432
 Z    =        5024934
27                 I    =           51
33520
 XDOT =      -3523
920157                 Wp   =           57
62149
 YDOT =       6546
706655  meter/sec      RA   =          309
97923  deg
 ZDOT =       1882
192715                 TA   =           14
06432
                                          MA   =           14
05477
                                          Ha   =            222
618  n
mi
                                          Hp   =            216
488

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14598296
54                 X    =         4414187
30
 Y    =        3120288
62  feet           Y    =         1000624
12  meter
 Z    =       16486004
81                 Z    =         5046462
14
 XDOT =     -11561
417837                 XDOT =       -3606
007789
 YDOT =      21478
696376  feet/sec       YDOT =        6506
840685  meter/sec
 ZDOT =       6175
172949                 ZDOT =        1864
876094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12760615
78                 X    =         3889435
69
 Y    =        7536958
76  feet           Y    =         2297265
03  meter
 Z    =       16582995
96                 Z    =         5054497
17
 XDOT =     -17242
186838                 XDOT =       -5255
418548
 YDOT =      15785
394035  feet/sec       YDOT =        4811
388102  meter/sec
 ZDOT =       6096
227412                 ZDOT =        1858
130115


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   19033
63482565  
00016717  00000-0  10270-3 0  9013
2 25544  51
6428 310
3950 0005231 341
5761  18
5201 15
53221754 34343


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
63482565   =   yrday
fracday
Element set:     901
Inclination:       51
6428  deg
RA of node:       310
3950  deg
Eccentricity:     
0005231     
Arg of perigee:   341
5761  deg
Mean anomaly:      18
5201  deg
Mean motion:   15
53221754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3434
Checksum:              280


Coasting Arc #3 (Orbit 3435)
---------------------------------------

Vector Time (GMT): 2019/033/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1929265
24                 A    =         6788603
41  meter
 Y    =        5881174
93  meter          E    =           
0011595
 Z    =        2782313
19                 I    =           51
35458
 XDOT =      -5703
372020                 Wp   =           76
59203
 YDOT =        547
850003  meter/sec      RA   =          309
22682  deg
 ZDOT =      -5092
187256                 TA   =           71
74304
                                          MA   =           71
61689
                                          Ha   =            222
693  n
mi
                                          Hp   =            216
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6329610
37                 X    =        -2008401
40
 Y    =       19295193
36  feet           Y    =         5859157
99  meter
 Z    =        9128324
10                 Z    =         2772749
75
 XDOT =     -18711
850458                 XDOT =       -5684
339967
 YDOT =       1797
408146  feet/sec       YDOT =         484
177484  meter/sec
 ZDOT =     -16706
651104                 ZDOT =       -5119
845152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5143311
94                 X    =         1567681
48
 Y    =       19665046
54  feet           Y    =         5993906
19  meter
 Z    =        9084439
55                 Z    =         2768937
17
 XDOT =     -13190
594674                 XDOT =       -4020
493257
 YDOT =      11256
738181  feet/sec       YDOT =        3431
053798  meter/sec
 ZDOT =     -16831
484409                 ZDOT =       -5130
236448


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   19033
76350230  
00016717  00000-0  10270-3 0  9021
2 25544  51
6400 309
7516 0005449 339
5414  20
5519 15
53262533 34363


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
76350230   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       309
7516  deg
Eccentricity:     
0005449     
Arg of perigee:   339
5414  deg
Mean anomaly:      20
5519  deg
Mean motion:   15
53262533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3436
Checksum:              288


Coasting Arc #4 (Orbit 3447)
---------------------------------------

Vector Time (GMT): 2019/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2576009
44                 A    =         6790734
51  meter
 Y    =        6033961
30  meter          E    =           
0011321
 Z    =        1740102
91                 I    =           51
34721
 XDOT =      -5147
088227                 Wp   =           94
26344
 YDOT =       -558
451845  meter/sec      RA   =          305
36559  deg
 ZDOT =      -5652
108243                 TA   =           66
57264
                                          MA   =           66
45365
                                          Ha   =            222
896  n
mi
                                          Hp   =            216
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8451474
53                 X    =        -2651743
66
 Y    =       19796460
95  feet           Y    =         6004731
07  meter
 Z    =        5708999
03                 Z    =         1727406
13
 XDOT =     -16886
772397                 XDOT =       -5113
006872
 YDOT =      -1832
191091  feet/sec       YDOT =        -615
819510  meter/sec
 ZDOT =     -18543
662215                 ZDOT =       -5677
027420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20331861
66                 X    =        -6197151
43
 Y    =        7113498
86  feet           Y    =         2168194
45  meter
 Z    =        5650972
78                 Z    =         1722416
50
 XDOT =      -9452
675146                 XDOT =       -2881
175384
 YDOT =     -12115
619714  feet/sec       YDOT =       -3692
840889  meter/sec
 ZDOT =     -18656
001839                 ZDOT =       -5686
349360


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   19034
53558055  
00016717  00000-0  10270-3 0  9033
2 25544  51
6418 305
9106 0005242 345
7096  14
3907 15
53213627 34486


Satellite: ISS
Catalog Number: 25544
Epoch time:      19034
53558055   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:       305
9106  deg
Eccentricity:     
0005242     
Arg of perigee:   345
7096  deg
Mean anomaly:      14
3907  deg
Mean motion:   15
53213627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3448
Checksum:              303


Coasting Arc #5 (Orbit 3462)
---------------------------------------

Vector Time (GMT): 2019/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3166789
67                 A    =         6791921
37  meter
 Y    =       -5986944
84  meter          E    =           
0015216
 Z    =        -369383
99                 I    =           51
33264
 XDOT =       4392
533463                 Wp   =           25
88821
 YDOT =       1961
357353  meter/sec      RA   =          300
37790  deg
 ZDOT =       5975
057208                 TA   =          330
11233
                                          MA   =          330
19913
                                          Ha   =            222
993  n
mi
                                          Hp   =            216
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10389729
89                 X    =         3235296
23
 Y    =      -19642207
47  feet           Y    =        -5951148
54  meter
 Z    =       -1211889
72                 Z    =         -353834
98
 XDOT =      14411
199024                 XDOT =        4341
251879
 YDOT =       6434
899452  feet/sec       YDOT =        2010
190983  meter/sec
 ZDOT =      19603
206062                 ZDOT =        5996
269328

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21407332
18                 X    =         6524954
85
 Y    =       -5971237
76  feet           Y    =        -1820033
27  meter
 Z    =       -1141019
99                 Z    =         -347782
89
 XDOT =       4720
275449                 XDOT =        1438
739957
 YDOT =      13229
423967  feet/sec       YDOT =        4032
328425  meter/sec
 ZDOT =      19698
653295                 ZDOT =        6004
149524


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   19035
50067236  
00016717  00000-0  10270-3 0  9048
2 25544  51
6415 301
1065 0005389 349
2115  10
8921 15
53220326 34636


Satellite: ISS
Catalog Number: 25544
Epoch time:      19035
50067236   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:       301
1065  deg
Eccentricity:     
0005389     
Arg of perigee:   349
2115  deg
Mean anomaly:      10
8921  deg
Mean motion:   15
53220326  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3463
Checksum:              278


Coasting Arc #6 (Orbit 3478)
---------------------------------------

Vector Time (GMT): 2019/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3619348
59                 A    =         6791510
44  meter
 Y    =        5647261
26  meter          E    =           
0005612
 Z    =       -1059347
48                 I    =           51
31541
 XDOT =      -3584
751798                 Wp   =          113
93725
 YDOT =      -3391
852277  meter/sec      RA   =          295
39093  deg
 ZDOT =      -5860
895978                 TA   =           77
59074
                                          MA   =           77
52793
                                          Ha   =            223
054  n
mi
                                          Hp   =            216
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11874503
26                 X    =        -3677083
29
 Y    =       18527760
04  feet           Y    =         5606464
35  meter
 Z    =       -3475549
48                 Z    =        -1077068
73
 XDOT =     -11760
996714                 XDOT =       -3518
088572
 YDOT =     -11128
124270  feet/sec       YDOT =       -3431
566831  meter/sec
 ZDOT =     -19228
661344                 ZDOT =       -5878
146892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21523948
79                 X    =        -6560499
59
 Y    =        4520456
07  feet           Y    =         1377835
01  meter
 Z    =       -3556159
32                 Z    =        -1083917
36
 XDOT =        124
297956                 XDOT =          37
886017
 YDOT =     -14527
992856  feet/sec       YDOT =       -4428
132222  meter/sec
 ZDOT =     -19306
074798                 ZDOT =       -5884
491599


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   19036
53010343  
00016717  00000-0  10270-3 0  9050
2 25544  51
6416 295
9827 0005219 351
5812   8
5252 15
53205540 34794


Satellite: ISS
Catalog Number: 25544
Epoch time:      19036
53010343   =   yrday
fracday
Element set:     905
Inclination:       51
6416  deg
RA of node:       295
9827  deg
Eccentricity:     
0005219     
Arg of perigee:   351
5812  deg
Mean anomaly:       8
5252  deg
Mean motion:   15
53205540  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3479
Checksum:              298


Coasting Arc #7 (Orbit 3487)
---------------------------------------

Vector Time (GMT): 2019/037/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4325389
41                 A    =         6780314
15  meter
 Y    =         458145
62  meter          E    =           
0003948
 Z    =        5198620
16                 I    =           51
26905
 XDOT =      -2085
918865                 Wp   =           40
23246
 YDOT =       7298
922539  meter/sec      RA   =          292
59139  deg
 ZDOT =       1094
794560                 TA   =           39
23832
                                          MA   =           39
20970
                                          Ha   =            222
872  n
mi
                                          Hp   =            216
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14190910
13                 X    =         4294693
53
 Y    =        1503102
43  feet           Y    =          506343
65  meter
 Z    =       17055840
42                 Z    =         5219556
12
 XDOT =      -6843
565831                 XDOT =       -2172
700200
 YDOT =      23946
596257  feet/sec       YDOT =        7275
111143  meter/sec
 ZDOT =       3591
845670                 ZDOT =        1084
451277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12280631
46                 X    =        -3743136
47
 Y    =       -7042640
60  feet           Y    =        -2146596
86  meter
 Z    =       17150225
77                 Z    =         5227388
82
 XDOT =      15411
237247                 XDOT =        4697
345113
 YDOT =     -18262
087423  feet/sec       YDOT =       -5566
284246  meter/sec
 ZDOT =       3544
333084                 ZDOT =        1080
312724


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   19037
10915520  
00016717  00000-0  10270-3 0  9066
2 25544  51
6400 293
0979 0005096 353
4285   6
6799 15
53241374 34882


Satellite: ISS
Catalog Number: 25544
Epoch time:      19037
10915520   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       293
0979  deg
Eccentricity:     
0005096     
Arg of perigee:   353
4285  deg
Mean anomaly:       6
6799  deg
Mean motion:   15
53241374  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3488
Checksum:              322


Coasting Arc #8 (Orbit 3502)
---------------------------------------

Vector Time (GMT): 2019/038/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3866957
18                 A    =         6780114
72  meter
 Y    =       -1815294
13  meter          E    =           
0015120
 Z    =       -5277409
33                 I    =           51
25646
 XDOT =       2685
092876                 Wp   =           73
64123
 YDOT =      -7153
040650  meter/sec      RA   =          287
57486  deg
 ZDOT =        498
367441                 TA   =          201
11459
                                          MA   =          201
17707
                                          Ha   =            223
185  n
mi
                                          Hp   =            215
767

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12686867
39                 X    =        -3820736
61
 Y    =       -5955689
39  feet           Y    =        -1858278
92  meter
 Z    =      -17314335
06                 Z    =        -5296080
72
 XDOT =       8809
359831                 XDOT =        2762
459907
 YDOT =     -23467
981135  feet/sec       YDOT =       -7122
581461  meter/sec
 ZDOT =       1635
063783                 ZDOT =         511
598472

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9289629
72                 X    =         2831479
14
 Y    =       10354381
57  feet           Y    =         3156015
50  meter
 Z    =      -17398350
52                 Z    =        -5303017
24
 XDOT =     -16433
258084                 XDOT =       -5008
857064
 YDOT =      17562
967934  feet/sec       YDOT =        5353
192626  meter/sec
 ZDOT =       1695
563305                 ZDOT =         516
807695


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   19038
07424398  
00016717  00000-0  10270-3 0  9072
2 25544  51
6402 288
2936 0005248 358
1319   1
9813 15
53211806 35032


Satellite: ISS
Catalog Number: 25544
Epoch time:      19038
07424398   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:       288
2936  deg
Eccentricity:     
0005248     
Arg of perigee:   358
1319  deg
Mean anomaly:       1
9813  deg
Mean motion:   15
53211806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3503
Checksum:              308


Coasting Arc #9 (Orbit 3518)
---------------------------------------

Vector Time (GMT): 2019/039/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3372517
32                 A    =         6781348
62  meter
 Y    =        3163172
53  meter          E    =           
0010126
 Z    =        4958696
02                 I    =           51
25090
 XDOT =      -3186
582648                 Wp   =           31
71208
 YDOT =       6660
288261  meter/sec      RA   =          282
55922  deg
 ZDOT =      -2070
954903                 TA   =           78
60519
                                          MA   =           78
49145
                                          Ha   =            223
171  n
mi
                                          Hp   =            215
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11064689
36                 X    =         3312809
16
 Y    =       10377862
61  feet           Y    =         3200552
79  meter
 Z    =       16268687
73                 Z    =         4974932
87
 XDOT =     -10454
667481                 XDOT =       -3250
763729
 YDOT =      21851
339438  feet/sec       YDOT =        6624
294699  meter/sec
 ZDOT =      -6794
471466                 ZDOT =       -2086
589997

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6326809
44                 X    =        -1928411
52
 Y    =      -13701166
75  feet           Y    =        -4176115
62  meter
 Z    =       16341575
67                 Z    =         4980912
26
 XDOT =      16769
371731                 XDOT =        5111
304504
 YDOT =     -15973
021022  feet/sec       YDOT =       -4868
576808  meter/sec
 ZDOT =      -6865
738728                 ZDOT =       -2092
677164


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   19039
10366930  
00016717  00000-0  10270-3 0  9085
2 25544  51
6391 283
1694 0005260   2
2526 357
8649 15
53255718 35192


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
10366930   =   yrday
fracday
Element set:     908
Inclination:       51
6391  deg
RA of node:       283
1694  deg
Eccentricity:     
0005260     
Arg of perigee:     2
2526  deg
Mean anomaly:     357
8649  deg
Mean motion:   15
53255718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3519
Checksum:              321


Coasting Arc #10 (Orbit 3527)
---------------------------------------

Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2556072
11                 A    =         6784689
80  meter
 Y    =       -4752930
81  meter          E    =           
0007999
 Z    =       -4116660
70                 I    =           51
25494
 XDOT =       3956
100925                 Wp   =           70
72161
 YDOT =      -5376
897724  meter/sec      RA   =          279
47193  deg
 ZDOT =       3760
165782                 TA   =          238
23445
                                          MA   =          238
31241
                                          Ha   =            223
253  n
mi
                                          Hp   =            215
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8386063
34                 X    =        -2482737
50
 Y    =      -15593605
03  feet           Y    =        -4781104
80  meter
 Z    =      -13506104
67                 Z    =        -4128898
48
 XDOT =      12979
333742                 XDOT =        3997
668487
 YDOT =     -17640
740565  feet/sec       YDOT =       -5332
425203  meter/sec
 ZDOT =      12336
501910                 ZDOT =        3779
483893

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13148223
94                 X    =        -4007578
66
 Y    =      -11795370
63  feet           Y    =        -3595228
97  meter
 Z    =      -13560784
58                 Z    =        -4133327
14
 XDOT =       5191
200095                 XDOT =        1582
277789
 YDOT =     -20038
073472  feet/sec       YDOT =       -6107
604794  meter/sec
 ZDOT =      12424
229677                 ZDOT =        3786
905205


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   19039
68272204  
00016717  00000-0  10270-3 0  9099
2 25544  51
6363 280
2834 0005134   4
6640 355
4559 15
53236639 35283


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
68272204   =   yrday
fracday
Element set:     909
Inclination:       51
6363  deg
RA of node:       280
2834  deg
Eccentricity:     
0005134     
Arg of perigee:     4
6640  deg
Mean anomaly:     355
4559  deg
Mean motion:   15
53236639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3528
Checksum:              316


Coasting Arc #11 (Orbit 3540)
---------------------------------------

Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3836973
08                 A    =         6780885
25  meter
 Y    =        2407063
82  meter          E    =           
0009860
 Z    =        5044275
93                 I    =           51
24377
 XDOT =      -2125
331592                 Wp   =           29
69750
 YDOT =       7148
805658  meter/sec      RA   =          275
48154  deg
 ZDOT =      -1784
737962                 TA   =           77
72194
                                          MA   =           77
61155
                                          Ha   =            223
232  n
mi
                                          Hp   =            215
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12588494
35                 X    =         3785269
61
 Y    =        7897191
01  feet           Y    =         2449682
75  meter
 Z    =       16549461
71                 Z    =         5062788
43
 XDOT =      -6972
872678                 XDOT =       -2196
444493
 YDOT =      23454
086806  feet/sec       YDOT =        7124
640990  meter/sec
 ZDOT =      -5855
439507                 ZDOT =       -1795
234988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1716114
34                 X    =          523071
65
 Y    =       14667259
90  feet           Y    =         4470580
82  meter
 Z    =       16632706
87                 Z    =         5069649
05
 XDOT =     -21519
601802                 XDOT =       -6559
174629
 YDOT =       9249
259726  feet/sec       YDOT =        2819
174365  meter/sec
 ZDOT =      -5903
557158                 ZDOT =       -1799
404222


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   19040
51912777  
00016717  00000-0  10270-3 0  9101
2 25544  51
6411 276
1240 0005503   4
6478 355
4725 15
53284242 35414


Satellite: ISS
Catalog Number: 25544
Epoch time:      19040
51912777   =   yrday
fracday
Element set:     910
Inclination:       51
6411  deg
RA of node:       276
1240  deg
Eccentricity:     
0005503     
Arg of perigee:     4
6478  deg
Mean anomaly:     355
4725  deg
Mean motion:   15
53284242  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              289


Coasting Arc #12 (Orbit 3555)
---------------------------------------

Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3547858
44                 A    =         6783385
50  meter
 Y    =       -3690386
36  meter          E    =           
0009941
 Z    =       -4457822
14                 I    =           51
24947
 XDOT =       2641
557074                 Wp   =           77
14787
 YDOT =      -6426
181852  meter/sec      RA   =          270
46746  deg
 ZDOT =       3225
816390                 TA   =          225
49305
                                          MA   =          225
57434
                                          Ha   =            223
445  n
mi
                                          Hp   =            215
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11639955
50                 X    =        -3484674
52
 Y    =      -12107566
80  feet           Y    =        -3729707
97  meter
 Z    =      -14625400
71                 Z    =        -4474902
36
 XDOT =       8666
525833                 XDOT =        2697
551143
 YDOT =     -21083
273792  feet/sec       YDOT =       -6396
328845  meter/sec
 ZDOT =      10583
387106                 ZDOT =        3238
784260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1858744
59                 X    =          566545
35
 Y    =      -16624641
07  feet           Y    =        -5067190
60  meter
 Z    =      -14702056
37                 Z    =        -4481186
78
 XDOT =      20463
848059                 XDOT =        6237
380888
 YDOT =      -7099
900617  feet/sec       YDOT =       -2164
049708  meter/sec
 ZDOT =      10642
557001                 ZDOT =        3243
851374


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   19041
48421202  
00016717  00000-0  10270-3 0  9117
2 25544  51
6408 271
3190 0005580   8
7638 351
3611 15
53250463 35562


Satellite: ISS
Catalog Number: 25544
Epoch time:      19041
48421202   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:       271
3190  deg
Eccentricity:     
0005580     
Arg of perigee:     8
7638  deg
Mean anomaly:     351
3611  deg
Mean motion:   15
53250463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3556
Checksum:              283


Coasting Arc #13 (Orbit 3571)
---------------------------------------

Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3215734
21                 A    =         6786501
49  meter
 Y    =        4825750
31  meter          E    =           
0014697
 Z    =        3519534
67                 I    =           51
26035
 XDOT =      -3162
586316                 Wp   =           65
70892
 YDOT =       5375
272197  meter/sec      RA   =          265
46020  deg
 ZDOT =      -4459
901746                 TA   =           72
59510
                                          MA   =           72
43445
                                          Ha   =            223
559  n
mi
                                          Hp   =            215
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10550309
09                 X    =         3144436
58
 Y    =       15832514
15  feet           Y    =         4861312
42  meter
 Z    =       11547029
75                 Z    =         3534981
90
 XDOT =     -10375
939356                 XDOT =       -3200
795625
 YDOT =      17635
407470  feet/sec       YDOT =        5339
692087  meter/sec
 ZDOT =     -14632
223575                 ZDOT =       -4475
357277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5085560
29                 X    =        -1550078
78
 Y    =       18289672
59  feet           Y    =         5574692
21  meter
 Z    =       11616211
76                 Z    =         3540621
34
 XDOT =     -18719
451567                 XDOT =       -5705
688838
 YDOT =       4175
751603  feet/sec       YDOT =        1272
769088  meter/sec
 ZDOT =     -14702
493611                 ZDOT =       -4481
320053


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   19042
51363275  
00016717  00000-0  10270-3 0  9128
2 25544  51
6403 266
1940 0005711  12
9840 347
1458 15
53275939 35725


Satellite: ISS
Catalog Number: 25544
Epoch time:      19042
51363275   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:       266
1940  deg
Eccentricity:     
0005711     
Arg of perigee:    12
9840  deg
Mean anomaly:     347
1458  deg
Mean motion:   15
53275939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3572
Checksum:              307


Coasting Arc #14 (Orbit 3586)
---------------------------------------

Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2875919
92                 A    =         6789523
17  meter
 Y    =       -5672968
68  meter          E    =           
0010839
 Z    =       -2364300
11                 I    =           51
27347
 XDOT =       3667
449275                 Wp   =           30
65233
 YDOT =      -4082
152028  meter/sec      RA   =          260
46027  deg
 ZDOT =       5353
798525                 TA   =          302
82013
                                          MA   =          302
92446
                                          Ha   =            223
625  n
mi
                                          Hp   =            215
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9435432
82                 X    =        -2800785
12
 Y    =      -18612101
98  feet           Y    =        -5704709
20  meter
 Z    =       -7756890
13                 Z    =        -2378087
41
 XDOT =      12032
313895                 XDOT =        3686
818994
 YDOT =     -13392
887230  feet/sec       YDOT =       -4041
031559  meter/sec
 ZDOT =      17564
955790                 ZDOT =        5371
660604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7565322
46                 X    =         2305910
29
 Y    =      -19422766
58  feet           Y    =        -5920059
25  meter
 Z    =       -7818510
82                 Z    =        -2383082
10
 XDOT =      16508
102382                 XDOT =        5031
669606
 YDOT =       -646
979861  feet/sec       YDOT =        -197
199462  meter/sec
 ZDOT =      17645
942878                 ZDOT =        5378
483389


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   19043
47871464  
00016717  00000-0  10270-3 0  9139
2 25544  51
6399 261
3895 0005639  14
8830 345
2487 15
53233033 35870


Satellite: ISS
Catalog Number: 25544
Epoch time:      19043
47871464   =   yrday
fracday
Element set:     913
Inclination:       51
6399  deg
RA of node:       261
3895  deg
Eccentricity:     
0005639     
Arg of perigee:    14
8830  deg
Mean anomaly:     345
2487  deg
Mean motion:   15
53233033  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3587
Checksum:              333


Coasting Arc #15 (Orbit 3602)
---------------------------------------

Vector Time (GMT): 2019/044/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2445482
82                 A    =         6791494
82  meter
 Y    =        6253725
84  meter          E    =           
0013324
 Z    =         995435
52                 I    =           51
28725
 XDOT =      -4192
625614                 Wp   =          100
09667
 YDOT =       2584
638482  meter/sec      RA   =          255
46629  deg
 ZDOT =      -5872
713112                 TA   =           69
07126
                                          MA   =           68
92871
                                          Ha   =            223
768  n
mi
                                          Hp   =            215
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8023237
60                 X    =         2370534
93
 Y    =       20517473
23  feet           Y    =         6280653
89  meter
 Z    =        3265864
57                 Z    =         1007132
48
 XDOT =     -13755
333378                 XDOT =       -4192
690120
 YDOT =       8479
785046  feet/sec       YDOT =        2537
753148  meter/sec
 ZDOT =     -19267
431469                 ZDOT =       -5893
079282

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9566244
21                 X    =        -2915791
24
 Y    =       19836398
06  feet           Y    =         6046134
13  meter
 Z    =        3318012
08                 Z    =         1011330
08
 XDOT =     -14043
621403                 XDOT =       -4280
495804
 YDOT =      -3499
265001  feet/sec       YDOT =       -1066
575972  meter/sec
 ZDOT =     -19359
563565                 ZDOT =       -5900
794975


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   19044
50813331  
00016717  00000-0  10270-3 0  9144
2 25544  51
6406 256
2640 0005607  19
8365 340
3004 15
53234790 36034


Satellite: ISS
Catalog Number: 25544
Epoch time:      19044
50813331   =   yrday
fracday
Element set:     914
Inclination:       51
6406  deg
RA of node:       256
2640  deg
Eccentricity:     
0005607     
Arg of perigee:    19
8365  deg
Mean anomaly:     340
3004  deg
Mean motion:   15
53234790  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3603
Checksum:              282


Coasting Arc #16 (Orbit 3605)
---------------------------------------

Vector Time (GMT): 2019/044/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4438716
00                 A    =         6783115
62  meter
 Y    =        2374531
98  meter          E    =           
0012985
 Z    =        4541860
35                 I    =           51
25755
 XDOT =       -605
657035                 Wp   =           51
09926
 YDOT =       7007
211286  meter/sec      RA   =          254
52522  deg
 ZDOT =      -3057
603032                 TA   =           69
71142
                                          MA   =           69
57190
                                          Ha   =            223
669  n
mi
                                          Hp   =            215
072

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14562716
55                 X    =         4389771
85
 Y    =        7790459
25  feet           Y    =         2423895
20  meter
 Z    =       14901116
63                 Z    =         4563302
80
 XDOT =      -1987
063762                 XDOT =        -669
116674
 YDOT =      22989
538339  feet/sec       YDOT =        7000
083535  meter/sec
 ZDOT =     -10031
506012                 ZDOT =       -3060
699289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16234338
83                 X    =         4948226
48
 Y    =        2514963
09  feet           Y    =          766560
75  meter
 Z    =       14997614
77                 Z    =         4571272
98
 XDOT =       6049
967383                 XDOT =        1844
030058
 YDOT =      21126
625386  feet/sec       YDOT =        6439
395418  meter/sec
 ZDOT =     -10046
166119                 ZDOT =       -3062
071433


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   19044
70115064  
00016717  00000-0  10270-3 0  9155
2 25544  51
6374 255
2977 0005221  25
0778 335
0627 15
53218925 36066


Satellite: ISS
Catalog Number: 25544
Epoch time:      19044
70115064   =   yrday
fracday
Element set:     915
Inclination:       51
6374  deg
RA of node:       255
2977  deg
Eccentricity:     
0005221     
Arg of perigee:    25
0778  deg
Mean anomaly:     335
0627  deg
Mean motion:   15
53218925  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3606
Checksum:              305


Coasting Arc #17 (Orbit 3620)
---------------------------------------

Vector Time (GMT): 2019/045/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4471355
34                 A    =         6786077
98  meter
 Y    =       -3544166
95  meter          E    =           
0008832
 Z    =       -3677630
74                 I    =           51
27818
 XDOT =       1373
372960                 Wp   =           66
38755
 YDOT =      -6187
434998  meter/sec      RA   =          249
51921  deg
 ZDOT =       4304
820017                 TA   =          249
63241
                                          MA   =          249
72731
                                          Ha   =            223
733  n
mi
                                          Hp   =            214
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14669800
99                 X    =        -4413527
51
 Y    =      -11627844
33  feet           Y    =        -3593845
43  meter
 Z    =      -12065717
65                 Z    =        -3699210
15
 XDOT =       4505
816797                 XDOT =        1421
550404
 YDOT =     -20299
983588  feet/sec       YDOT =       -6171
807607  meter/sec
 ZDOT =      14123
425252                 ZDOT =        4311
608264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17736580
07                 X    =        -5406109
60
 Y    =       -5785586
79  feet           Y    =        -1763446
85  meter
 Z    =      -12162733
26                 Z    =        -3707201
10
 XDOT =      -3396
028266                 XDOT =       -1035
109415
 YDOT =     -19265
403403  feet/sec       YDOT =       -5872
094957  meter/sec
 ZDOT =      14154
650520                 ZDOT =        4314
337479


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   19045
66622783  
00016717  00000-0  10270-3 0  9163
2 25544  51
6379 250
4941 0005270  28
0900 332
0536 15
53244968 36212


Satellite: ISS
Catalog Number: 25544
Epoch time:      19045
66622783   =   yrday
fracday
Element set:     916
Inclination:       51
6379  deg
RA of node:       250
4941  deg
Eccentricity:     
0005270     
Arg of perigee:    28
0900  deg
Mean anomaly:     332
0536  deg
Mean motion:   15
53244968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3621
Checksum:              309


Coasting Arc #18 (Orbit 3636)
---------------------------------------

Vector Time (GMT): 2019/046/15:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4384152
92                 A    =         6789187
03  meter
 Y    =        4530305
99  meter          E    =           
0015972
 Z    =        2507440
06                 I    =           51
30055
 XDOT =      -2242
460011                 Wp   =           86
27814
 YDOT =       5101
606825  meter/sec      RA   =          244
51988  deg
 ZDOT =      -5266
335116                 TA   =           65
45698
                                          MA   =           65
29057
                                          Ha   =            223
790  n
mi
                                          Hp   =            214
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14383703
81                 X    =         4320988
39
 Y    =       14863208
62  feet           Y    =         4578979
45  meter
 Z    =        8226509
38                 Z    =         2528582
88
 XDOT =      -7357
152266                 XDOT =       -2273
760486
 YDOT =      16737
555201  feet/sec       YDOT =        5076
355111  meter/sec
 ZDOT =     -17278
002349                 ZDOT =       -5277
303923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18775637
81                 X    =         5722814
40
 Y    =        8585439
31  feet           Y    =         2616841
90  meter
 Z    =        8321479
40                 Z    =         2536386
92
 XDOT =         15
322475                 XDOT =           4
670290
 YDOT =      16856
417519  feet/sec       YDOT =        5137
836060  meter/sec
 ZDOT =     -17327
977963                 ZDOT =       -5281
567683


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   19046
69564348  
00016717  00000-0  10270-3 0  9170
2 25544  51
6373 245
3686 0005175  31
3196 328
8263 15
53241803 36375


Satellite: ISS
Catalog Number: 25544
Epoch time:      19046
69564348   =   yrday
fracday
Element set:     917
Inclination:       51
6373  deg
RA of node:       245
3686  deg
Eccentricity:     
0005175     
Arg of perigee:    31
3196  deg
Mean anomaly:     328
8263  deg
Mean motion:   15
53241803  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3637
Checksum:              329
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