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

 
Date: July 26th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14542 9041 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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


210/10:44:30 000 0 0 0 0 0 0
N/A 0 0 0 0 226 6
000/00:00:00 000 0 0 0 0 219 9

212/15:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 2
000/00:00:00 000 0 0 0 0 220 2

213/11:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 226 2
000/00:00:00 000 0 0 0 0 220 4

216/18:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 8
000/00:00:00 000 0 0 0 0 220 9

Coasting Arc #1 (Orbit 2134)
---------------------------------------

Vector Time (GMT): 2019/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6069029
99                 A    =         6797631
16  meter
 Y    =       -2722536
40  meter          E    =           
0017500
 Z    =        1348158
36                 I    =           51
75165
 XDOT =       3065
790979                 Wp   =          139
04933
 YDOT =       3934
383619  meter/sec      RA   =          165
03273  deg
 ZDOT =      -5826
153929                 TA   =           26
29936
                                          MA   =           26
21061
                                          Ha   =            226
922  n
mi
                                          Hp   =            219
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19911515
71                 X    =         6092474
54
 Y    =       -8932206
05  feet           Y    =        -2654537
28  meter
 Z    =        4423091
75                 Z    =         1377695
97
 XDOT =      10058
369355                 XDOT =        3049
867776
 YDOT =      12908
082741  feet/sec       YDOT =        3968
578950  meter/sec
 ZDOT =     -19114
678245                 ZDOT =       -5811
299861

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18320161
01                 X    =        -5583985
08
 Y    =      -11807500
76  feet           Y    =        -3598926
23  meter
 Z    =        4557535
49                 Z    =         1389136
82
 XDOT =       4414
023468                 XDOT =        1345
394353
 YDOT =     -14237
447352  feet/sec       YDOT =       -4339
573953  meter/sec
 ZDOT =     -19047
421748                 ZDOT =       -5805
654149


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   19207
53495706  
00016717  00000-0  10270-3 0  9005
2 25544  51
6393 166
0584 0006324 184
0196 176
0905 15
50999283 21353


Satellite: ISS
Catalog Number: 25544
Epoch time:      19207
53495706   =   yrday
fracday
Element set:     900
Inclination:       51
6393  deg
RA of node:       166
0584  deg
Eccentricity:     
0006324     
Arg of perigee:   184
0196  deg
Mean anomaly:     176
0905  deg
Mean motion:   15
50999283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2135
Checksum:              322


Coasting Arc #2 (Orbit 2149)
---------------------------------------

Vector Time (GMT): 2019/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6148882
15                 A    =         6798181
93  meter
 Y    =        2812604
83  meter          E    =           
0006110
 Z    =        -698492
89                 I    =           51
78466
 XDOT =      -2537
226259                 Wp   =           74
49110
 YDOT =      -4076
545457  meter/sec      RA   =          160
08518  deg
 ZDOT =       5965
541545                 TA   =          277
99401
                                          MA   =          278
06334
                                          Ha   =            226
844  n
mi
                                          Hp   =            219
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20173497
87                 X    =        -6176483
64
 Y    =        9227706
13  feet           Y    =         2743689
46  meter
 Z    =       -2291643
35                 Z    =         -728428
40
 XDOT =      -8324
233133                 XDOT =       -2520
429685
 YDOT =     -13374
492968  feet/sec       YDOT =       -4104
825244  meter/sec
 ZDOT =      19571
986697                 ZDOT =        5953
257075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18920154
83                 X    =         5766863
19
 Y    =       11554442
06  feet           Y    =         3521793
94  meter
 Z    =       -2427924
25                 Z    =         -740031
31
 XDOT =      -5518
243627                 XDOT =       -1681
960657
 YDOT =      13107
633977  feet/sec       YDOT =        3995
206836  meter/sec
 ZDOT =      19516
415344                 ZDOT =        5948
603397


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   19208
50143343  
00016717  00000-0  10270-3 0  9011
2 25544  51
6385 161
2637 0006353 187
4911 172
6146 15
51006213 21503


Satellite: ISS
Catalog Number: 25544
Epoch time:      19208
50143343   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:       161
2637  deg
Eccentricity:     
0006353     
Arg of perigee:   187
4911  deg
Mean anomaly:     172
6146  deg
Mean motion:   15
51006213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2150
Checksum:              278


Coasting Arc #3 (Orbit 2165)
---------------------------------------

Vector Time (GMT): 2019/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6157198
95                 A    =         6798463
15  meter
 Y    =       -2858663
85  meter          E    =           
0016431
 Z    =           6691
64                 I    =           51
81764
 XDOT =       2006
648828                 Wp   =          153
52936
 YDOT =       4294
672966  meter/sec      RA   =          155
13992  deg
 ZDOT =      -6027
689337                 TA   =           26
39878
                                          MA   =           26
31516
                                          Ha   =            226
754  n
mi
                                          Hp   =            219
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20200783
94                 X    =         6188675
23
 Y    =       -9378818
41  feet           Y    =        -2789633
73  meter
 Z    =          21954
19                 Z    =           36676
83
 XDOT =       6583
493530                 XDOT =        1987
754325
 YDOT =      14090
134402  feet/sec       YDOT =        4317
007830  meter/sec
 ZDOT =     -19775
883650                 ZDOT =       -6017
987228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19264443
44                 X    =        -5871802
36
 Y    =      -11175441
33  feet           Y    =        -3406274
52  meter
 Z    =         158488
41                 Z    =           48307
27
 XDOT =       6879
163466                 XDOT =        2096
769024
 YDOT =     -12174
849290  feet/sec       YDOT =       -3710
894064  meter/sec
 ZDOT =     -19732
064183                 ZDOT =       -6014
333163


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   19209
53234192  
00016717  00000-0  10270-3 0  9029
2 25544  51
6398 156
1486 0006337 192
2040 167
8958 15
50992959 21665


Satellite: ISS
Catalog Number: 25544
Epoch time:      19209
53234192   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       156
1486  deg
Eccentricity:     
0006337     
Arg of perigee:   192
2040  deg
Mean anomaly:     167
8958  deg
Mean motion:   15
50992959  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2166
Checksum:              338


Coasting Arc #4 (Orbit 2180)
---------------------------------------

Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3607762
79                 A    =         6787340
31  meter
 Y    =       -2594627
88  meter          E    =           
0009317
 Z    =        5130482
19                 I    =           51
80913
 XDOT =       5775
935291                 Wp   =          165
42204
 YDOT =      -4759
974029  meter/sec      RA   =          150
46394  deg
 ZDOT =       1644
951238                 TA   =          268
67490
                                          MA   =          268
78164
                                          Ha   =            226
633  n
mi
                                          Hp   =            219
859

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11836492
08                 X    =        -3603401
49
 Y    =       -8512558
66  feet           Y    =        -2634948
71  meter
 Z    =       16832290
65                 Z    =         5112967
51
 XDOT =      18949
918933                 XDOT =        5820
743255
 YDOT =     -15616
712692  feet/sec       YDOT =       -4695
133145  meter/sec
 ZDOT =       5396
821647                 ZDOT =        1673
116408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4637238
99                 X    =        -1413430
45
 Y    =       13918734
87  feet           Y    =         4242430
39  meter
 Z    =       16752821
93                 Z    =         5106260
12
 XDOT =     -19457
066624                 XDOT =       -5930
513907
 YDOT =     -13170
152505  feet/sec       YDOT =       -4014
262483  meter/sec
 ZDOT =       5525
235174                 ZDOT =        1684
091681


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   19210
49881567  
00016717  00000-0  10270-3 0  9031
2 25544  51
6398 151
3537 0006324 196
8080 163
2862 15
51027211 21811


Satellite: ISS
Catalog Number: 25544
Epoch time:      19210
49881567   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       151
3537  deg
Eccentricity:     
0006324     
Arg of perigee:   196
8080  deg
Mean anomaly:     163
2862  deg
Mean motion:   15
51027211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2181
Checksum:              306


Coasting Arc #5 (Orbit 2195)
---------------------------------------

Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3173642
57                 A    =         6786771
27  meter
 Y    =        2858318
77  meter          E    =           
0012886
 Z    =       -5284302
25                 I    =           51
83558
 XDOT =      -5845
771742                 Wp   =          108
79002
 YDOT =       4861
903785  meter/sec      RA   =          145
50928  deg
 ZDOT =       -886
819152                 TA   =          152
77062
                                          MA   =          152
70300
                                          Ha   =            226
492  n
mi
                                          Hp   =            220
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10412213
15                 X    =         3167111
89
 Y    =        9377686
26  feet           Y    =         2893772
84  meter
 Z    =      -17336949
65                 Z    =        -5268901
66
 XDOT =     -19179
041149                 XDOT =       -5895
396884
 YDOT =      15951
127902  feet/sec       YDOT =        4796
254903  meter/sec
 ZDOT =      -2909
511655                 ZDOT =        -915
335110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5659350
77                 X    =         1724970
11
 Y    =      -12912934
92  feet           Y    =        -3935862
56  meter
 Z    =      -17267103
58                 Z    =        -5263013
17
 XDOT =      20153
966360                 XDOT =        6142
928947
 YDOT =      12871
757819  feet/sec       YDOT =        3923
311783  meter/sec
 ZDOT =      -3039
552719                 ZDOT =        -926
455669


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   19211
46529061  
00016717  00000-0  10270-3 0  9048
2 25544  51
6400 146
5576 0006205 199
5214 160
5700 15
50996815 21962


Satellite: ISS
Catalog Number: 25544
Epoch time:      19211
46529061   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       146
5576  deg
Eccentricity:     
0006205     
Arg of perigee:   199
5214  deg
Mean anomaly:     160
5700  deg
Mean motion:   15
50996815  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2196
Checksum:              304


Coasting Arc #6 (Orbit 2211)
---------------------------------------

Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2780318
15                 A    =         6786439
90  meter
 Y    =       -3138447
23  meter          E    =           
0006001
 Z    =        5336474
18                 I    =           51
86200
 XDOT =       5850
908700                 Wp   =          181
03089
 YDOT =      -4947
861493  meter/sec      RA   =          140
55874  deg
 ZDOT =        132
596518                 TA   =          267
67427
                                          MA   =          267
74298
                                          Ha   =            226
384  n
mi
                                          Hp   =            220
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9121778
70                 X    =        -2770937
51
 Y    =      -10296742
87  feet           Y    =        -3169486
85  meter
 Z    =       17508117
38                 Z    =         5322991
17
 XDOT =      19195
894685                 XDOT =        5905
158196
 YDOT =     -16233
141380  feet/sec       YDOT =       -4882
129210  meter/sec
 ZDOT =        435
027946                 ZDOT =         161
148578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6725216
41                 X    =        -2049845
96
 Y    =       12088731
62  feet           Y    =         3684645
40  meter
 Z    =       17447004
52                 Z    =         5317846
98
 XDOT =     -20717
160419                 XDOT =       -6314
590496
 YDOT =     -12368
975196  feet/sec       YDOT =       -3770
063640  meter/sec
 ZDOT =        565
262322                 ZDOT =         172
291956


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   19212
49619657  
00016717  00000-0  10270-3 0  9054
2 25544  51
6404 141
4442 0006178 204
0505 156
0359 15
51014697 22125


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
49619657   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       141
4442  deg
Eccentricity:     
0006178     
Arg of perigee:   204
0505  deg
Mean anomaly:     156
0359  deg
Mean motion:   15
51014697  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2212
Checksum:              293


Coasting Arc #7 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1820864
77                 A    =         6792459
99  meter
 Y    =       -5380730
80  meter          E    =           
0010003
 Z    =        3712522
24                 I    =           51
89001
 XDOT =       6264
119950                 Wp   =          116
27350
 YDOT =       -874
266404  meter/sec      RA   =          139
53585  deg
 ZDOT =      -4334
735075                 TA   =           19
67543
                                          MA   =           19
63686
                                          Ha   =            226
180  n
mi
                                          Hp   =            220
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5973965
78                 X    =         1862865
38
 Y    =      -17653316
28  feet           Y    =        -5360134
18  meter
 Z    =       12180191
08                 Z    =         3721468
53
 XDOT =      20551
574639                 XDOT =        6294
485915
 YDOT =      -2868
328098  feet/sec       YDOT =        -804
046355  meter/sec
 ZDOT =     -14221
571768                 ZDOT =       -4304
233402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5324968
24                 X    =        -1623050
32
 Y    =       17831717
98  feet           Y    =         5435107
64  meter
 Z    =       12221270
16                 Z    =         3725043
15
 XDOT =     -19244
319533                 XDOT =       -5865
668594
 YDOT =       3915
616736  feet/sec       YDOT =        1193
479981  meter/sec
 ZDOT =     -14082
752145                 ZDOT =       -4292
422854


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   19212
68949039  
00016717  00000-0  10270-3 0  9066
2 25544  51
6428 140
4865 0006108 205
4474 154
6377 15
51037600 22158


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
68949039   =   yrday
fracday
Element set:     906
Inclination:       51
6428  deg
RA of node:       140
4865  deg
Eccentricity:     
0006108     
Arg of perigee:   205
4474  deg
Mean anomaly:     154
6377  deg
Mean motion:   15
51037600  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              308


Coasting Arc #8 (Orbit 2227)
---------------------------------------

Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         420733
27                 A    =         6790434
32  meter
 Y    =       -5196975
54  meter          E    =           
0006687
 Z    =        4343330
51                 I    =           51
90262
 XDOT =       6372
460205                 Wp   =          111
91352
 YDOT =      -2418
841390  meter/sec      RA   =          135
40468  deg
 ZDOT =      -3509
645607                 TA   =           13
66642
                                          MA   =           13
64832
                                          Ha   =            226
201  n
mi
                                          Hp   =            220
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1380358
50                 X    =          457719
15
 Y    =      -17050444
68  feet           Y    =        -5192064
18  meter
 Z    =       14249772
02                 Z    =         4345463
60
 XDOT =      20907
021671                 XDOT =        6416
082228
 YDOT =      -7935
831332  feet/sec       YDOT =       -2347
335852  meter/sec
 ZDOT =     -11514
585325                 ZDOT =       -3478
585671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14922009
20                 X    =        -4548228
40
 Y    =        8346825
14  feet           Y    =         2544112
30  meter
 Z    =       14259845
99                 Z    =         4346401
06
 XDOT =     -17598
103989                 XDOT =       -5363
902096
 YDOT =     -12020
378287  feet/sec       YDOT =       -3663
811302  meter/sec
 ZDOT =     -11373
099787                 ZDOT =       -3466
520815


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   19213
52710266  
00016717  00000-0  10270-3 0  9079
2 25544  51
6417 136
3301 0006213 208
0884 151
9933 15
51004486 22284


Satellite: ISS
Catalog Number: 25544
Epoch time:      19213
52710266   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:       136
3301  deg
Eccentricity:     
0006213     
Arg of perigee:   208
0884  deg
Mean anomaly:     151
9933  deg
Mean motion:   15
51004486  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2228
Checksum:              287


Coasting Arc #9 (Orbit 2242)
---------------------------------------

Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -665765
54                 A    =         6791910
34  meter
 Y    =        5512138
26  meter          E    =           
0007685
 Z    =       -3920208
69                 I    =           51
93108
 XDOT =      -6084
259573                 Wp   =          156
66021
 YDOT =       2184
412022  meter/sec      RA   =          130
46046  deg
 ZDOT =       4100
634841                 TA   =          156
23193
                                          MA   =          156
19641
                                          Ha   =            226
011  n
mi
                                          Hp   =            220
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2184270
14                 X    =         -708312
69
 Y    =       18084443
11  feet           Y    =         5504455
53  meter
 Z    =      -12861577
06                 Z    =        -3923545
67
 XDOT =     -19961
481539                 XDOT =       -6128
152172
 YDOT =       7166
706110  feet/sec       YDOT =        2116
127905  meter/sec
 ZDOT =      13453
526382                 ZDOT =        4070
974107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16089089
74                 X    =         4903954
55
 Y    =       -8518120
28  feet           Y    =        -2596323
06  meter
 Z    =      -12877154
23                 Z    =        -3924956
61
 XDOT =      16646
406278                 XDOT =        5073
824633
 YDOT =      11287
555000  feet/sec       YDOT =        3440
446764  meter/sec
 ZDOT =      13318
407130                 ZDOT =        4059
450493


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   19214
49357483  
00016717  00000-0  10270-3 0  9085
2 25544  51
6422 131
5345 0006125 211
6110 148
4674 15
51011122 22434


Satellite: ISS
Catalog Number: 25544
Epoch time:      19214
49357483   =   yrday
fracday
Element set:     908
Inclination:       51
6422  deg
RA of node:       131
5345  deg
Eccentricity:     
0006125     
Arg of perigee:   211
6110  deg
Mean anomaly:     148
4674  deg
Mean motion:   15
51011122  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2243
Checksum:              273


Coasting Arc #10 (Orbit 2258)
---------------------------------------

Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         850079
88                 A    =         6793458
79  meter
 Y    =       -5799358
68  meter          E    =           
0010142
 Z    =        3421764
33                 I    =           51
95675
 XDOT =       5806
413907                 Wp   =          119
27141
 YDOT =      -1888
304286  meter/sec      RA   =          125
52083  deg
 ZDOT =      -4637
384945                 TA   =           20
92413
                                          MA   =           20
88265
                                          Ha   =            225
912  n
mi
                                          Hp   =            220
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2788975
97                 X    =          898246
17
 Y    =      -19026767
33  feet           Y    =        -5789583
28  meter
 Z    =       11226260
92                 Z    =         3426010
41
 XDOT =      19049
914394                 XDOT =        5849
623215
 YDOT =      -6195
224034  feet/sec       YDOT =       -1823
131149  meter/sec
 ZDOT =     -15214
517537                 ZDOT =       -4609
075366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17064972
20                 X    =        -5201403
53
 Y    =        8839649
27  feet           Y    =         2694325
10  meter
 Z    =       11246000
22                 Z    =         3427780
87
 XDOT =     -15521
482770                 XDOT =       -4730
947948
 YDOT =     -10749
162134  feet/sec       YDOT =       -3276
344619  meter/sec
 ZDOT =     -15085
554816                 ZDOT =       -4598
077108


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   19215
52447818  
00016717  00000-0  10270-3 0  9093
2 25544  51
6420 126
4206 0006073 215
2651 144
8099 15
51004159 22593


Satellite: ISS
Catalog Number: 25544
Epoch time:      19215
52447818   =   yrday
fracday
Element set:     909
Inclination:       51
6420  deg
RA of node:       126
4206  deg
Eccentricity:     
0006073     
Arg of perigee:   215
2651  deg
Mean anomaly:     144
8099  deg
Mean motion:   15
51004159  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2259
Checksum:              300


Coasting Arc #11 (Orbit 2273)
---------------------------------------

Vector Time (GMT): 2019/216/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -976993
41                 A    =         6794864
41  meter
 Y    =        6078288
37  meter          E    =           
0002724
 Z    =       -2879658
08                 I    =           51
98020
 XDOT =      -5518
497762                 Wp   =          174
74603
 YDOT =       1523
239656  meter/sec      RA   =          120
58278  deg
 ZDOT =       5085
231215                 TA   =          152
71834
                                          MA   =          152
70403
                                          Ha   =            225
723  n
mi
                                          Hp   =            220
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3205358
96                 X    =        -1030902
47
 Y    =       19941890
96  feet           Y    =         6067061
55  meter
 Z    =       -9447697
10                 Z    =        -2884534
71
 XDOT =     -18105
307617                 XDOT =       -5559
821653
 YDOT =       4997
505432  feet/sec       YDOT =        1461
296815  meter/sec
 ZDOT =      16683
829447                 ZDOT =        5058
324615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17900952
51                 X    =         5456210
33
 Y    =       -9331720
30  feet           Y    =        -2844308
35  meter
 Z    =       -9470333
53                 Z    =        -2886557
66
 XDOT =      14170
824599                 XDOT =        4319
267338
 YDOT =      10368
997130  feet/sec       YDOT =        3160
470325  meter/sec
 ZDOT =      16561
267406                 ZDOT =        5047
874305


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   19216
49094963  
00016717  00000-0  10270-3 0  9101
2 25544  51
6421 121
6252 0006132 219
2557 140
8150 15
51019162 22748


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
49094963   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:       121
6252  deg
Eccentricity:     
0006132     
Arg of perigee:   219
2557  deg
Mean anomaly:     140
8150  deg
Mean motion:   15
51019162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2274
Checksum:              283


Coasting Arc #12 (Orbit 2278)
---------------------------------------

Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3782299
20                 A    =         6798207
62  meter
 Y    =        5600430
17  meter          E    =           
0007128
 Z    =         713584
97                 I    =           51
99204
 XDOT =      -3574
641893                 Wp   =           64
75367
 YDOT =      -3181
845202  meter/sec      RA   =          119
30001  deg
 ZDOT =       5981
342723                 TA   =          302
90497
                                          MA   =          302
97353
                                          Ha   =            225
805  n
mi
                                          Hp   =            220
877

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12409118
12                 X    =        -3848109
85
 Y    =       18374114
72  feet           Y    =         5557765
86  meter
 Z    =        2341158
05                 Z    =          695052
55
 XDOT =     -11727
827732                 XDOT =       -3567
849404
 YDOT =     -10439
124678  feet/sec       YDOT =       -3221
781440  meter/sec
 ZDOT =      19623
827831                 ZDOT =        5963
995247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3108366
14                 X    =         -947430
00
 Y    =      -21961830
90  feet           Y    =        -6693966
06  meter
 Z    =        2256406
13                 Z    =          687752
59
 XDOT =      14195
838424                 XDOT =        4326
891552
 YDOT =         14
162704  feet/sec       YDOT =           4
316792  meter/sec
 ZDOT =      19545
111821                 ZDOT =        5957
350083


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   19216
81310566  
00016717  00000-0  10270-3 0  9118
2 25544  51
6385 120
0228 0006389 219
0670 141
0020 15
51010125 22795


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
81310566   =   yrday
fracday
Element set:     911
Inclination:       51
6385  deg
RA of node:       120
0228  deg
Eccentricity:     
0006389     
Arg of perigee:   219
0670  deg
Mean anomaly:     141
0020  deg
Mean motion:   15
51010125  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2279
Checksum:              267


Coasting Arc #13 (Orbit 2293)
---------------------------------------

Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3695741
34                 A    =         6797506
05  meter
 Y    =       -5523631
91  meter          E    =           
0011366
 Z    =       -1392331
03                 I    =           52
00647
 XDOT =       3329
169967                 Wp   =          174
80249
 YDOT =       3694
283397  meter/sec      RA   =          114
36731  deg
 ZDOT =      -5833
809733                 TA   =           20
27868
                                          MA   =           20
23357
                                          Ha   =            225
587  n
mi
                                          Hp   =            220
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12125135
63                 X    =         3763996
58
 Y    =      -18122151
94  feet           Y    =        -5481921
88  meter
 Z    =       -4568015
20                 Z    =        -1374213
03
 XDOT =      10922
473646                 XDOT =        3315
949005
 YDOT =      12120
352354  feet/sec       YDOT =        3731
438644  meter/sec
 ZDOT =     -19139
795712                 ZDOT =       -5817
670181

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3509970
19                 X    =         1069838
91
 Y    =       21537448
46  feet           Y    =         6564614
29  meter
 Z    =       -4485141
17                 Z    =        -1367071
03
 XDOT =     -14779
393625                 XDOT =       -4504
759177
 YDOT =      -1551
750725  feet/sec       YDOT =        -472
973621  meter/sec
 ZDOT =     -19066
616668                 ZDOT =       -5811
504760


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   19217
77957484  
00016717  00000-0  10270-3 0  9121
2 25544  51
6396 115
2271 0006144 223
6673 136
3992 15
51049196 22946


Satellite: ISS
Catalog Number: 25544
Epoch time:      19217
77957484   =   yrday
fracday
Element set:     912
Inclination:       51
6396  deg
RA of node:       115
2271  deg
Eccentricity:     
0006144     
Arg of perigee:   223
6673  deg
Mean anomaly:     136
3992  deg
Mean motion:   15
51049196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2294
Checksum:              331


Coasting Arc #14 (Orbit 2309)
---------------------------------------

Vector Time (GMT): 2019/218/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933877
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3585870
37                 A    =         6796683
95  meter
 Y    =        5402371
42  meter          E    =           
0008496
 Z    =        2028646
93                 I    =           52
01574
 XDOT =      -3146
166870                 Wp   =           85
47589
 YDOT =      -4193
375248  meter/sec      RA   =          109
43428  deg
 ZDOT =       5586
463359                 TA   =          296
78568
                                          MA   =          296
87257
                                          Ha   =            225
530  n
mi
                                          Hp   =            221
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11764666
57                 X    =        -3655868
67
 Y    =       17724315
67  feet           Y    =         5361880
27  meter
 Z    =        6655665
77                 Z    =         2011058
38
 XDOT =     -10322
069783                 XDOT =       -3126
177165
 YDOT =     -13757
792808  feet/sec       YDOT =       -4228
446228  meter/sec
 ZDOT =      18328
291859                 ZDOT =        5571
229095

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3851982
02                 X    =        -1174084
12
 Y    =      -20947211
76  feet           Y    =        -6384710
14  meter
 Z    =        6575194
77                 Z    =         2004119
37
 XDOT =      15546
597169                 XDOT =        4738
602817
 YDOT =       2892
883795  feet/sec       YDOT =         881
750981  meter/sec
 ZDOT =      18259
275639                 ZDOT =        5565
427215


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   19218
81047548  
00016717  00000-0  10270-3 0  9139
2 25544  51
6391 110
1114 0006298 225
3447 134
7191 15
51020533 23105


Satellite: ISS
Catalog Number: 25544
Epoch time:      19218
81047548   =   yrday
fracday
Element set:     913
Inclination:       51
6391  deg
RA of node:       110
1114  deg
Eccentricity:     
0006298     
Arg of perigee:   225
3447  deg
Mean anomaly:     134
7191  deg
Mean motion:   15
51020533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2310
Checksum:              278


Coasting Arc #15 (Orbit 2324)
---------------------------------------

Vector Time (GMT): 2019/219/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933877
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3481415
55                 A    =         6795433
99  meter
 Y    =       -5192926
87  meter          E    =           
0007082
 Z    =       -2651694
97                 I    =           52
02187
 XDOT =       3016
631017                 Wp   =          185
58749
 YDOT =       4699
578301  meter/sec      RA   =          104
50212  deg
 ZDOT =      -5248
516673                 TA   =           24
10636
                                          MA   =           24
07323
                                          Ha   =            225
424  n
mi
                                          Hp   =            221
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11421967
02                 X    =         3552105
96
 Y    =      -17037161
66  feet           Y    =        -5153599
90  meter
 Z    =       -8699786
66                 Z    =        -2634612
18
 XDOT =       9897
083388                 XDOT =        2989
348941
 YDOT =      15418
563981  feet/sec       YDOT =        4733
160018  meter/sec
 ZDOT =     -17219
542889                 ZDOT =       -5233
929243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3957531
57                 X    =         1206255
62
 Y    =       20159815
55  feet           Y    =         6144711
78  meter
 Z    =       -8621616
82                 Z    =        -2627868
81
 XDOT =     -16517
073443                 XDOT =       -5034
403985
 YDOT =      -4085
467507  feet/sec       YDOT =       -1245
250496  meter/sec
 ZDOT =     -17153
517324                 ZDOT =       -5228
392080


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   19219
77694402  
00016717  00000-0  10270-3 0  9143
2 25544  51
6393 105
3167 0006210 229
4013 130
6598 15
51029260 23257


Satellite: ISS
Catalog Number: 25544
Epoch time:      19219
77694402   =   yrday
fracday
Element set:     914
Inclination:       51
6393  deg
RA of node:       105
3167  deg
Eccentricity:     
0006210     
Arg of perigee:   229
4013  deg
Mean anomaly:     130
6598  deg
Mean motion:   15
51029260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2325
Checksum:              294


Coasting Arc #16 (Orbit 2340)
---------------------------------------

Vector Time (GMT): 2019/220/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933877
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3376570
10                 A    =         6794043
24  meter
 Y    =        4940732
71  meter          E    =           
0008276
 Z    =        3213491
70                 I    =           52
02560
 XDOT =      -2950
937648                 Wp   =          111
41536
 YDOT =      -5165
177706  meter/sec      RA   =           99
56818  deg
 ZDOT =       4827
837614                 TA   =          285
46543
                                          MA   =          285
55682
                                          Ha   =            225
219  n
mi
                                          Hp   =            221
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11077985
88                 X    =        -3447177
06
 Y    =       16209752
98  feet           Y    =         4902578
58  meter
 Z    =       10542951
76                 Z    =         3196918
47
 XDOT =      -9681
553962                 XDOT =       -2916
410579
 YDOT =     -16946
121083  feet/sec       YDOT =       -5197
984346  meter/sec
 ZDOT =      15839
362250                 ZDOT =        4813
586795

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3938024
66                 X    =        -1200309
92
 Y    =      -19275979
43  feet           Y    =        -5875318
53  meter
 Z    =       10467104
34                 Z    =         3190373
40
 XDOT =      17588
282444                 XDOT =        5360
908489
 YDOT =       4995
921306  feet/sec       YDOT =        1522
756814  meter/sec
 ZDOT =      15774
914859                 ZDOT =        4808
194049


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   19220
80784283  
00016717  00000-0  10270-3 0  9157
2 25544  51
6403 100
2013 0006397 232
9235 127
1331 15
51034254 23417


Satellite: ISS
Catalog Number: 25544
Epoch time:      19220
80784283   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:       100
2013  deg
Eccentricity:     
0006397     
Arg of perigee:   232
9235  deg
Mean anomaly:     127
1331  deg
Mean motion:   15
51034254  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2341
Checksum:              268


Coasting Arc #17 (Orbit 2355)
---------------------------------------

Vector Time (GMT): 2019/221/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933877
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3302413
33                 A    =         6792535
68  meter
 Y    =       -4607784
36  meter          E    =           
0002318
 Z    =       -3740108
66                 I    =           52
02582
 XDOT =       2930
341471                 Wp   =          170
12816
 YDOT =       5606
293191  meter/sec      RA   =           94
63369  deg
 ZDOT =      -4322
112426                 TA   =           54
18633
                                          MA   =           54
16479
                                          Ha   =            225
124  n
mi
                                          Hp   =            221
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10834689
39                 X    =         3371860
64
 Y    =      -15117402
76  feet           Y    =        -4570465
92  meter
 Z    =      -12270697
70                 Z    =        -3723898
55
 XDOT =       9613
981203                 XDOT =        2888
426702
 YDOT =      18393
350365  feet/sec       YDOT =        5638
828235  meter/sec
 ZDOT =     -14180
158877                 ZDOT =       -4307
979529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3627388
33                 X    =         1105627
96
 Y    =       18291622
98  feet           Y    =         5575286
68  meter
 Z    =      -12196514
46                 Z    =        -3717497
61
 XDOT =     -18743
982276                 XDOT =       -5713
165798
 YDOT =      -5689
633121  feet/sec       YDOT =       -1734
200175  meter/sec
 ZDOT =     -14116
294010                 ZDOT =       -4302
646414


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   19221
77430993  
00016717  00000-0  10270-3 0  9161
2 25544  51
6412  95
4063 0006235 237
0335 123
0217 15
51022102 23568


Satellite: ISS
Catalog Number: 25544
Epoch time:      19221
77430993   =   yrday
fracday
Element set:     916
Inclination:       51
6412  deg
RA of node:        95
4063  deg
Eccentricity:     
0006235     
Arg of perigee:   237
0335  deg
Mean anomaly:     123
0217  deg
Mean motion:   15
51022102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2356
Checksum:              273
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