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

 
Date: October 10th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14601 2445 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


284/20:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 219 1

289/20:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 0
000/00:00:00 000 0 0 0 0 219 5

292/20:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 8
000/00:00:00 000 0 0 0 0 220 1

Coasting Arc #1 (Orbit 3299)
---------------------------------------

Vector Time (GMT): 2019/282/13:49:43
769
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1191367
38                 A    =         6789026
52  meter
 Y    =       -4071150
91  meter          E    =           
0008628
 Z    =        5293472
77                 I    =           51
79410
 XDOT =       7031
853110                 Wp   =          112
81599
 YDOT =      -2976
620251  meter/sec      RA   =          152
86569  deg
 ZDOT =       -709
017732                 TA   =          343
92733
                                          MA   =          343
95469
                                          Ha   =            229
606  n
mi
                                          Hp   =            218
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3908685
62                 X    =        -1171466
92
 Y    =      -13356794
33  feet           Y    =        -4084361
95  meter
 Z    =       17367036
64                 Z    =         5287734
17
 XDOT =      23070
384218                 XDOT =        7068
059950
 YDOT =      -9765
814472  feet/sec       YDOT =       -2897
782715  meter/sec
 ZDOT =      -2326
173660                 ZDOT =        -674
771297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12224767
61                 X    =         3726109
17
 Y    =        6718482
47  feet           Y    =         2047793
46  meter
 Z    =       17341072
34                 Z    =         5285558
85
 XDOT =      -9157
588009                 XDOT =       -2791
232825
 YDOT =      22243
848884  feet/sec       YDOT =        6779
925140  meter/sec
 ZDOT =      -2169
944839                 ZDOT =        -661
399187


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   19282
62344783  
00016717  00000-0  10270-3 0  9006
2 25544  51
6412 153
8040 0006996 131
1061 229
0694 15
50173013 33009


Satellite: ISS
Catalog Number: 25544
Epoch time:      19282
62344783   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:       153
8040  deg
Eccentricity:     
0006996     
Arg of perigee:   131
1061  deg
Mean anomaly:     229
0694  deg
Mean motion:   15
50173013  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3300
Checksum:              279


Coasting Arc #2 (Orbit 3314)
---------------------------------------

Vector Time (GMT): 2019/283/13:49:43
769
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1078200
86                 A    =         6789267
49  meter
 Y    =        4193393
20  meter          E    =           
0020270
 Z    =       -5247041
49                 I    =           51
82236
 XDOT =      -6841
653519                 Wp   =          110
85634
 YDOT =       3213
303168  meter/sec      RA   =          147
91874  deg
 ZDOT =       1158
771846                 TA   =          170
27759
                                          MA   =          170
23830
                                          Ha   =            229
465  n
mi
                                          Hp   =            218
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3537404
40                 X    =         1056716
39
 Y    =       13757851
71  feet           Y    =         4205329
81  meter
 Z    =      -17214703
06                 Z    =        -5241856
51
 XDOT =     -22446
369813                 XDOT =       -6882
705833
 YDOT =      10542
333228  feet/sec       YDOT =        3136
565533  meter/sec
 ZDOT =       3801
744902                 ZDOT =        1125
437423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12362870
73                 X    =        -3768203
00
 Y    =       -7053895
75  feet           Y    =        -2150027
43  meter
 Z    =      -17191268
05                 Z    =        -5239898
50
 XDOT =       7749
588197                 XDOT =        2362
074483
 YDOT =     -22504
051387  feet/sec       YDOT =       -6859
234863  meter/sec
 ZDOT =       3649
644405                 ZDOT =        1112
411615


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   19283
59043526  
00016717  00000-0  10270-3 0  9015
2 25544  51
6393 149
0116 0007020 135
0824 225
0895 15
50189877 33157


Satellite: ISS
Catalog Number: 25544
Epoch time:      19283
59043526   =   yrday
fracday
Element set:     901
Inclination:       51
6393  deg
RA of node:       149
0116  deg
Eccentricity:     
0007020     
Arg of perigee:   135
0824  deg
Mean anomaly:     225
0895  deg
Mean motion:   15
50189877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3315
Checksum:              306


Coasting Arc #3 (Orbit 3330)
---------------------------------------

Vector Time (GMT): 2019/284/13:49:43
769
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -991692
77                 A    =         6789679
20  meter
 Y    =       -4311447
95  meter          E    =           
0008831
 Z    =        5142601
70                 I    =           51
85181
 XDOT =       6660
764746                 Wp   =          106
93062
 YDOT =      -3445
414301  meter/sec      RA   =          142
97498  deg
 ZDOT =      -1604
343011                 TA   =          358
49573
                                          MA   =          358
49839
                                          Ha   =            229
465  n
mi
                                          Hp   =            219
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3253585
19                 X    =         -968387
38
 Y    =      -14145170
43  feet           Y    =        -4322406
95  meter
 Z    =       16872052
82                 Z    =         5137841
40
 XDOT =      21852
902709                 XDOT =        6706
590418
 YDOT =     -11303
852695  feet/sec       YDOT =       -3370
672855  meter/sec
 ZDOT =      -5263
592555                 ZDOT =       -1571
875527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12565603
78                 X    =         3829996
03
 Y    =        7314506
75  feet           Y    =         2229461
66  meter
 Z    =       16850561
48                 Z    =         5136051
14
 XDOT =      -6372
754404                 XDOT =       -1942
415542
 YDOT =      22730
469799  feet/sec       YDOT =        6928
247195  meter/sec
 ZDOT =      -5115
416330                 ZDOT =       -1559
178897


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   19284
62188660  
00016717  00000-0  10270-3 0  9020
2 25544  51
6398 143
9005 0006949 139
7006 220
4661 15
50175624 33317


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
62188660   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       143
9005  deg
Eccentricity:     
0006949     
Arg of perigee:   139
7006  deg
Mean anomaly:     220
4661  deg
Mean motion:   15
50175624  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3331
Checksum:              311


Coasting Arc #4 (Orbit 3334)
---------------------------------------

Vector Time (GMT): 2019/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5077494
47                 A    =         6792459
52  meter
 Y    =         480320
33  meter          E    =           
0013350
 Z    =       -4496022
39                 I    =           51
87088
 XDOT =      -3449
239339                 Wp   =          101
34940
 YDOT =       6001
097183  meter/sec      RA   =          141
61984  deg
 ZDOT =      -3264
989876                 TA   =          135
86044
                                          MA   =          135
75383
                                          Ha   =            229
521  n
mi
                                          Hp   =            219
120

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16658446
41                 X    =         5093585
46
 Y    =        1575854
11  feet           Y    =          537189
99  meter
 Z    =      -14750729
62                 Z    =        -4471318
49
 XDOT =     -11316
402031                 XDOT =       -3500
229292
 YDOT =      19688
639051  feet/sec       YDOT =        5962
239931  meter/sec
 ZDOT =     -10711
909043                 ZDOT =       -3281
869622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13376588
58                 X    =         4077184
20
 Y    =       10215826
31  feet           Y    =         3113783
86  meter
 Z    =      -14638133
36                 Z    =        -4461703
05
 XDOT =     -19223
474476                 XDOT =       -5859
315020
 YDOT =       9762
564287  feet/sec       YDOT =        2975
629595  meter/sec
 ZDOT =     -10789
153526                 ZDOT =       -3288
533995


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   19284
87974932  
00016717  00000-0  10270-3 0  9033
2 25544  51
6423 142
6217 0007283 142
7293 217
4364 15
50175322 33356


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
87974932   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:       142
6217  deg
Eccentricity:     
0007283     
Arg of perigee:   142
7293  deg
Mean anomaly:     217
4364  deg
Mean motion:   15
50175322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3335
Checksum:              313


Coasting Arc #5 (Orbit 3350)
---------------------------------------

Vector Time (GMT): 2019/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4892186
56                 A    =         6791562
60  meter
 Y    =        -437019
97  meter          E    =           
0014902
 Z    =        4685087
30                 I    =           51
89413
 XDOT =       3340
966191                 Wp   =          129
68716
 YDOT =      -6264
778988  meter/sec      RA   =          136
67979  deg
 ZDOT =       2888
901206                 TA   =          291
61557
                                          MA   =          291
77426
                                          Ha   =            229
448  n
mi
                                          Hp   =            219
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16050480
83                 X    =        -4909694
00
 Y    =       -1433792
56  feet           Y    =         -491825
29  meter
 Z    =       15371021
34                 Z    =         4661280
03
 XDOT =      10961
175166                 XDOT =        3396
739550
 YDOT =     -20553
736836  feet/sec       YDOT =       -6227
105814  meter/sec
 ZDOT =       9478
022330                 ZDOT =        2905
266708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13106100
26                 X    =        -3994739
36
 Y    =       -9551342
19  feet           Y    =        -2911249
10  meter
 Z    =       15262502
78                 Z    =         4652010
85
 XDOT =      19232
746071                 XDOT =        5862
141002
 YDOT =     -11044
407283  feet/sec       YDOT =       -3366
335340  meter/sec
 ZDOT =       9552
950371                 ZDOT =        2911
739273


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   19285
91119447  
00016717  00000-0  10270-3 0  9042
2 25544  51
6426 137
5104 0007211 145
5277 214
6343 15
50223472 33515


Satellite: ISS
Catalog Number: 25544
Epoch time:      19285
91119447   =   yrday
fracday
Element set:     904
Inclination:       51
6426  deg
RA of node:       137
5104  deg
Eccentricity:     
0007211     
Arg of perigee:   145
5277  deg
Mean anomaly:     214
6343  deg
Mean motion:   15
50223472  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3351
Checksum:              291


Coasting Arc #6 (Orbit 3365)
---------------------------------------

Vector Time (GMT): 2019/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4703991
15                 A    =         6790918
95  meter
 Y    =         479664
13  meter          E    =           
0015037
 Z    =       -4886050
15                 I    =           51
91356
 XDOT =      -3209
832339                 Wp   =          100
26649
 YDOT =       6495
225938  meter/sec      RA   =          131
74095  deg
 ZDOT =      -2461
637740                 TA   =          145
65696
                                          MA   =          145
55966
                                          Ha   =            229
367  n
mi
                                          Hp   =            219
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15433041
83                 X    =         4722012
00
 Y    =        1573701
21  feet           Y    =          532367
80  meter
 Z    =      -16030348
26                 Z    =        -4863155
73
 XDOT =     -10530
945995                 XDOT =       -3270
267763
 YDOT =      21309
796384  feet/sec       YDOT =        6458
993187  meter/sec
 ZDOT =      -8076
239304                 ZDOT =       -2477
377598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12667761
85                 X    =         3861133
81
 Y    =        9138825
17  feet           Y    =         2785513
91  meter
 Z    =      -15925987
10                 Z    =        -4854240
87
 XDOT =     -19067
573479                 XDOT =       -5811
796396
 YDOT =      12282
619199  feet/sec       YDOT =        3743
742332  meter/sec
 ZDOT =      -8148
343991                 ZDOT =       -2483
615249


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   19286
87817483  
00016717  00000-0  10270-3 0  9054
2 25544  51
6411 132
7190 0007177 148
9094 211
2483 15
50177605 33666


Satellite: ISS
Catalog Number: 25544
Epoch time:      19286
87817483   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:       132
7190  deg
Eccentricity:     
0007177     
Arg of perigee:   148
9094  deg
Mean anomaly:     211
2483  deg
Mean motion:   15
50177605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3366
Checksum:              324


Coasting Arc #7 (Orbit 3381)
---------------------------------------

Vector Time (GMT): 2019/287/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4536401
04                 A    =         6790175
32  meter
 Y    =        -503603
45  meter          E    =           
0012815
 Z    =        5023141
48                 I    =           51
93295
 XDOT =       3032
470860                 Wp   =          139
31724
 YDOT =      -6734
492422  meter/sec      RA   =          126
80312  deg
 ZDOT =       2051
041696                 TA   =          290
74513
                                          MA   =          290
88241
                                          Ha   =            229
311  n
mi
                                          Hp   =            219
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14883205
53                 X    =        -4554832
66
 Y    =       -1652242
30  feet           Y    =         -554435
36  meter
 Z    =       16480122
98                 Z    =         5001060
10
 XDOT =       9949
051379                 XDOT =        3097
589468
 YDOT =     -22094
791411  feet/sec       YDOT =       -6700
216931  meter/sec
 ZDOT =       6729
139421                 ZDOT =        2065
931339

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12306939
73                 X    =        -3751155
23
 Y    =       -8722760
86  feet           Y    =        -2658697
51  meter
 Z    =       16379464
04                 Z    =         4992460
64
 XDOT =      18748
186402                 XDOT =        5714
447215
 YDOT =     -13610
856476  feet/sec       YDOT =       -4148
589054  meter/sec
 ZDOT =       6797
400172                 ZDOT =        2071
847572


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   19287
90961611  
00016717  00000-0  10270-3 0  9063
2 25544  51
6411 127
6077 0007158 152
6872 207
4656 15
50222180 33824


Satellite: ISS
Catalog Number: 25544
Epoch time:      19287
90961611   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:       127
6077  deg
Eccentricity:     
0007158     
Arg of perigee:   152
6872  deg
Mean anomaly:     207
4656  deg
Mean motion:   15
50222180  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3382
Checksum:              311


Coasting Arc #8 (Orbit 3396)
---------------------------------------

Vector Time (GMT): 2019/288/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4381429
90                 A    =         6789728
85  meter
 Y    =         607737
91  meter          E    =           
0016479
 Z    =       -5164106
10                 I    =           51
94971
 XDOT =      -2833
269936                 Wp   =          102
95520
 YDOT =       6925
269876  meter/sec      RA   =          121
86545  deg
 ZDOT =      -1596
733106                 TA   =          151
72121
                                          MA   =          151
63165
                                          Ha   =            229
184  n
mi
                                          Hp   =            219
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14374770
00                 X    =         4399393
37
 Y    =        1993890
78  feet           Y    =          656834
29  meter
 Z    =      -16942605
32                 Z    =        -5142778
61
 XDOT =      -9295
505038                 XDOT =       -2902
743491
 YDOT =      22720
701694  feet/sec       YDOT =        6893
197706  meter/sec
 ZDOT =      -5238
625676                 ZDOT =       -1610
665582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11848561
90                 X    =         3611441
67
 Y    =        8573570
12  feet           Y    =         2613224
17  meter
 Z    =      -16845384
07                 Z    =        -5134473
06
 XDOT =     -18233
224929                 XDOT =       -5557
486958
 YDOT =      14830
664224  feet/sec       YDOT =        4520
386456  meter/sec
 ZDOT =      -5302
554821                 ZDOT =       -1616
218709


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   19288
87659126  
00016717  00000-0  10270-3 0  9076
2 25544  51
6407 122
8155 0007088 155
9989 204
1493 15
50183400 33970


Satellite: ISS
Catalog Number: 25544
Epoch time:      19288
87659126   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       122
8155  deg
Eccentricity:     
0007088     
Arg of perigee:   155
9989  deg
Mean anomaly:     204
1493  deg
Mean motion:   15
50183400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3397
Checksum:              340


Coasting Arc #9 (Orbit 3411)
---------------------------------------

Vector Time (GMT): 2019/289/20:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1427298
49                 A    =         6792263
57  meter
 Y    =        4914820
48  meter          E    =           
0015032
 Z    =       -4481047
02                 I    =           51
97550
 XDOT =      -5207
128191                 Wp   =          130
84494
 YDOT =       4525
975051  meter/sec      RA   =          117
01614  deg
 ZDOT =       3303
219581                 TA   =          172
40979
                                          MA   =          172
38701
                                          Ha   =            229
018  n
mi
                                          Hp   =            219
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4682737
84                 X    =         1394000
49
 Y    =       16124739
09  feet           Y    =         4930595
18  meter
 Z    =      -14701597
83                 Z    =        -4474194
62
 XDOT =     -17083
753906                 XDOT =       -5273
397587
 YDOT =      14848
999511  feet/sec       YDOT =        4467
374862  meter/sec
 ZDOT =      10837
334584                 ZDOT =        3277
763489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5566162
88                 X    =        -1696566
44
 Y    =       15870171
11  feet           Y    =         4837228
15  meter
 Z    =      -14670641
54                 Z    =        -4471611
54
 XDOT =     -21445
728382                 XDOT =       -6536
658011
 YDOT =       2395
972238  feet/sec       YDOT =         730
292338  meter/sec
 ZDOT =      10720
972143                 ZDOT =        3267
752309


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   19289
84356185  
00016717  00000-0  10270-3 0  9084
2 25544  51
6411 118
0234 0007054 157
6876 202
4582 15
50234375 34123


Satellite: ISS
Catalog Number: 25544
Epoch time:      19289
84356185   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:       118
0234  deg
Eccentricity:     
0007054     
Arg of perigee:   157
6876  deg
Mean anomaly:     202
4582  deg
Mean motion:   15
50234375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3412
Checksum:              311


Coasting Arc #10 (Orbit 3427)
---------------------------------------

Vector Time (GMT): 2019/290/20:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1503826
32                 A    =         6793101
60  meter
 Y    =       -5087214
07  meter          E    =           
0012440
 Z    =        4230458
90                 I    =           51
99284
 XDOT =       4956
330269                 Wp   =          108
23299
 YDOT =      -4540
209640  meter/sec      RA   =          112
08311  deg
 ZDOT =      -3692
747805                 TA   =           19
46014
                                          MA   =           19
41269
                                          Ha   =            228
930  n
mi
                                          Hp   =            219
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4933813
39                 X    =        -1467377
60
 Y    =      -16690334
89  feet           Y    =        -5103827
05  meter
 Z    =       13879458
34                 Z    =         4223242
31
 XDOT =      16260
926080                 XDOT =        5024
669626
 YDOT =     -14895
700920  feet/sec       YDOT =       -4484
402417  meter/sec
 ZDOT =     -12115
314320                 ZDOT =       -3668
505114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5414192
14                 X    =         1650245
77
 Y    =      -16568043
46  feet           Y    =        -5049939
65  meter
 Z    =       13846863
05                 Z    =         4220523
86
 XDOT =      20715
922502                 XDOT =        6314
213179
 YDOT =      -3277
153839  feet/sec       YDOT =        -998
876490  meter/sec
 ZDOT =     -12004
462668                 ZDOT =       -3658
960221


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   19290
87499475  
00016717  00000-0  10270-3 0  9090
2 25544  51
6413 112
9121 0006903 162
4515 197
6875 15
50246790 34280


Satellite: ISS
Catalog Number: 25544
Epoch time:      19290
87499475   =   yrday
fracday
Element set:     909
Inclination:       51
6413  deg
RA of node:       112
9121  deg
Eccentricity:     
0006903     
Arg of perigee:   162
4515  deg
Mean anomaly:     197
6875  deg
Mean motion:   15
50246790  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3428
Checksum:              334


Coasting Arc #11 (Orbit 3442)
---------------------------------------

Vector Time (GMT): 2019/291/20:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1625209
31                 A    =         6794021
46  meter
 Y    =        5272403
68  meter          E    =           
0012069
 Z    =       -3978733
98                 I    =           52
00670
 XDOT =      -4690
041614                 Wp   =          136
56965
 YDOT =       4495
454744  meter/sec      RA   =          107
15171  deg
 ZDOT =       4040
137143                 TA   =          175
51075
                                          MA   =          175
49991
                                          Ha   =            228
854  n
mi
                                          Hp   =            219
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5332051
53                 X    =         1585457
90
 Y    =       17297912
35  feet           Y    =         5290355
65  meter
 Z    =      -13053589
19                 Z    =        -3970935
70
 XDOT =     -15387
275635                 XDOT =       -4759
587716
 YDOT =      14748
867270  feet/sec       YDOT =        4442
618539  meter/sec
 ZDOT =      13255
043119                 ZDOT =        4017
185223

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5141064
40                 X    =        -1566996
43
 Y    =       17382071
11  feet           Y    =         5298055
27  meter
 Z    =      -13018363
82                 Z    =        -3967997
29
 XDOT =     -19802
983515                 XDOT =       -6035
949375
 YDOT =       3994
738503  feet/sec       YDOT =        1217
596296  meter/sec
 ZDOT =      13150
059835                 ZDOT =        4008
138238


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   19291
84196332  
00016717  00000-0  10270-3 0  9106
2 25544  51
6407 108
1206 0007050 164
5208 195
6159 15
50242845 34437


Satellite: ISS
Catalog Number: 25544
Epoch time:      19291
84196332   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:       108
1206  deg
Eccentricity:     
0007050     
Arg of perigee:   164
5208  deg
Mean anomaly:     195
6159  deg
Mean motion:   15
50242845  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3443
Checksum:              297


Coasting Arc #12 (Orbit 3458)
---------------------------------------

Vector Time (GMT): 2019/292/20:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1762217
13                 A    =         6794931
44  meter
 Y    =       -5424543
75  meter          E    =           
0014250
 Z    =        3676774
97                 I    =           52
01969
 XDOT =       4464
897302                 Wp   =          113
87036
 YDOT =      -4430
017426  meter/sec      RA   =          102
22113  deg
 ZDOT =      -4388
116582                 TA   =           22
70560
                                          MA   =           22
64263
                                          Ha   =            228
721  n
mi
                                          Hp   =            219
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5781552
27                 X    =        -1719287
42
 Y    =      -17797059
56  feet           Y    =        -5444010
10  meter
 Z    =       12062909
99                 Z    =         3668318
84
 XDOT =      14648
613197                 XDOT =        4535
418647
 YDOT =     -14534
177907  feet/sec       YDOT =       -4379
693449  meter/sec
 ZDOT =     -14396
707946                 ZDOT =       -4366
256113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4740545
25                 X    =         1444918
19
 Y    =      -18127580
90  feet           Y    =        -5525286
66  meter
 Z    =       12024704
35                 Z    =         3665129
89
 XDOT =      18952
908558                 XDOT =        5776
846528
 YDOT =      -4544
127204  feet/sec       YDOT =       -1385
049972  meter/sec
 ZDOT =     -14296
687418                 ZDOT =       -4357
630325


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   19292
87339040  
00016717  00000-0  10270-3 0  9116
2 25544  51
6417 103
0090 0006798 169
4200 190
7095 15
50255698 34599


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
87339040   =   yrday
fracday
Element set:     911
Inclination:       51
6417  deg
RA of node:       103
0090  deg
Eccentricity:     
0006798     
Arg of perigee:   169
4200  deg
Mean anomaly:     190
7095  deg
Mean motion:   15
50255698  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3459
Checksum:              319


Coasting Arc #13 (Orbit 3458)
---------------------------------------

Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4031470
38                 A    =         6788839
49  meter
 Y    =        1150078
00  meter          E    =           
0017718
 Z    =       -5353950
43                 I    =           51
99910
 XDOT =      -1790
473488                 Wp   =          113
99433
 YDOT =       7433
480981  meter/sec      RA   =          102
12443  deg
 ZDOT =        242
209239                 TA   =          158
34595
                                          MA   =          158
27093
                                          Ha   =            228
794  n
mi
                                          Hp   =            220
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13226608
84                 X    =         4044317
26
 Y    =        3773221
77  feet           Y    =         1195232
62  meter
 Z    =      -17565454
18                 Z    =        -5334335
47
 XDOT =      -5874
256849                 XDOT =       -1874
640296
 YDOT =      24388
060962  feet/sec       YDOT =        7412
988035  meter/sec
 ZDOT =        794
649735                 ZDOT =         233
307254

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10638950
28                 X    =         3242752
05
 Y    =        8895267
32  feet           Y    =         2711277
48  meter
 Z    =      -17476055
64                 Z    =        -5326701
76
 XDOT =     -14681
995271                 XDOT =       -4475
072159
 YDOT =      19081
669673  feet/sec       YDOT =        5816
092916  meter/sec
 ZDOT =        753
536937                 ZDOT =         229
678058


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   19292
87339200  
00016717  00000-0  10270-3 0  9125
2 25544  51
6419 103
0089 0006852 168
3121 191
8190 15
50200288 34593


Satellite: ISS
Catalog Number: 25544
Epoch time:      19292
87339200   =   yrday
fracday
Element set:     912
Inclination:       51
6419  deg
RA of node:       103
0089  deg
Eccentricity:     
0006852     
Arg of perigee:   168
3121  deg
Mean anomaly:     191
8190  deg
Mean motion:   15
50200288  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3459
Checksum:              302


Coasting Arc #14 (Orbit 3474)
---------------------------------------

Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4017795
68                 A    =         6788840
57  meter
 Y    =       -1301097
79  meter          E    =           
0006544
 Z    =        5311546
18                 I    =           52
00513
 XDOT =       1498
989014                 Wp   =          144
77248
 YDOT =      -7484
810803  meter/sec      RA   =           97
19157  deg
 ZDOT =       -704
346601                 TA   =          311
89499
                                          MA   =          311
95080
                                          Ha   =            228
768  n
mi
                                          Hp   =            219
980

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13181744
35                 X    =        -4028748
74
 Y    =       -4268693
55  feet           Y    =        -1346088
90  meter
 Z    =       17426332
62                 Z    =         5292002
33
 XDOT =       4917
942958                 XDOT =        1585
996307
 YDOT =     -24556
465888  feet/sec       YDOT =       -7467
561556  meter/sec
 ZDOT =      -2310
848428                 ZDOT =        -696
853696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10553642
43                 X    =        -3216750
21
 Y    =       -9148611
36  feet           Y    =        -2788496
74  meter
 Z    =       17337264
46                 Z    =         5284398
21
 XDOT =      13515
847492                 XDOT =        4119
630316
 YDOT =     -19875
236708  feet/sec       YDOT =       -6057
972149  meter/sec
 ZDOT =      -2276
140364                 ZDOT =        -693
767583


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   19293
90481624  
00016717  00000-0  10270-3 0  9139
2 25544  51
6416  97
8982 0006784 171
1867 188
9404 15
50242272 34757


Satellite: ISS
Catalog Number: 25544
Epoch time:      19293
90481624   =   yrday
fracday
Element set:     913
Inclination:       51
6416  deg
RA of node:        97
8982  deg
Eccentricity:     
0006784     
Arg of perigee:   171
1867  deg
Mean anomaly:     188
9404  deg
Mean motion:   15
50242272  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3475
Checksum:              340


Coasting Arc #15 (Orbit 3489)
---------------------------------------

Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4049645
36                 A    =         6789247
55  meter
 Y    =        1488101
04  meter          E    =           
0017053
 Z    =       -5256171
19                 I    =           52
00976
 XDOT =      -1211
356440                 Wp   =          121
56393
 YDOT =       7461
828599  meter/sec      RA   =           92
25794  deg
 ZDOT =       1173
392700                 TA   =          159
69262
                                          MA   =          159
62471
                                          Ha   =            228
572  n
mi
                                          Hp   =            220
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13286238
05                 X    =         4058235
86
 Y    =        4882221
25  feet           Y    =         1533435
05  meter
 Z    =      -17244656
13                 Z    =        -5236478
44
 XDOT =      -3974
266534                 XDOT =       -1300
406498
 YDOT =      24481
064957  feet/sec       YDOT =        7447
784449  meter/sec
 ZDOT =       3849
713582                 ZDOT =        1167
292009

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10573839
57                 X    =         3222906
30
 Y    =        9572933
34  feet           Y    =         2917830
08  meter
 Z    =      -17154918
69                 Z    =        -5228819
22
 XDOT =     -12234
868630                 XDOT =       -3729
187958
 YDOT =      20396
704092  feet/sec       YDOT =        6216
915407  meter/sec
 ZDOT =       3821
342124                 ZDOT =        1164
745079


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   19294
87177608  
00016717  00000-0  10270-3 0  9141
2 25544  51
6421  93
1062 0006747 175
1642 184
9575 15
50209303 34905


Satellite: ISS
Catalog Number: 25544
Epoch time:      19294
87177608   =   yrday
fracday
Element set:     914
Inclination:       51
6421  deg
RA of node:        93
1062  deg
Eccentricity:     
0006747     
Arg of perigee:   175
1642  deg
Mean anomaly:     184
9575  deg
Mean motion:   15
50209303  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3490
Checksum:              320


Coasting Arc #16 (Orbit 3505)
---------------------------------------

Vector Time (GMT): 2019/295/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4103221
69                 A    =         6789523
92  meter
 Y    =       -1639951
71  meter          E    =           
0005808
 Z    =        5150111
79                 I    =           52
01028
 XDOT =        927
543504                 Wp   =          131
65450
 YDOT =      -7433
079339  meter/sec      RA   =           87
32523  deg
 ZDOT =      -1630
492420                 TA   =          333
98727
                                          MA   =          334
01644
                                          Ha   =            228
563  n
mi
                                          Hp   =            220
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13462013
41                 X    =        -4109594
94
 Y    =       -5380418
99  feet           Y    =        -1685872
36  meter
 Z    =       16896692
22                 Z    =         5130164
24
 XDOT =       3043
121733                 XDOT =        1018
513522
 YDOT =     -24386
743237  feet/sec       YDOT =       -7422
198281  meter/sec
 ZDOT =      -5349
384581                 ZDOT =       -1625
765611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10718848
82                 X    =        -3267105
12
 Y    =       -9916865
94  feet           Y    =        -3022660
74  meter
 Z    =       16805801
72                 Z    =         5122408
36
 XDOT =      10950
832596                 XDOT =        3337
813775
 YDOT =     -20850
014907  feet/sec       YDOT =       -6355
084544  meter/sec
 ZDOT =      -5327
269669                 ZDOT =       -1623
751795


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   19295
90319577  
00016717  00000-0  10270-3 0  9150
2 25544  51
6411  87
9950 0006724 177
9760 182
1419 15
50252221 35069


Satellite: ISS
Catalog Number: 25544
Epoch time:      19295
90319577   =   yrday
fracday
Element set:     915
Inclination:       51
6411  deg
RA of node:        87
9950  deg
Eccentricity:     
0006724     
Arg of perigee:   177
9760  deg
Mean anomaly:     182
1419  deg
Mean motion:   15
50252221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3506
Checksum:              323


Coasting Arc #17 (Orbit 3520)
---------------------------------------

Vector Time (GMT): 2019/296/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4203990
43                 A    =         6790191
54  meter
 Y    =        1811347
52  meter          E    =           
0015442
 Z    =       -5028555
02                 I    =           52
01111
 XDOT =       -661
558153                 Wp   =          129
88591
 YDOT =       7331
923866  meter/sec      RA   =           82
39196  deg
 ZDOT =       2082
590720                 TA   =          160
34948
                                          MA   =          160
28991
                                          Ha   =            228
298  n
mi
                                          Hp   =            220
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13792619
52                 X    =         4207849
15
 Y    =        5942741
20  feet           Y    =         1858380
87  meter
 Z    =      -16497883
92                 Z    =        -5008124
11
 XDOT =      -2170
466381                 XDOT =        -753
612858
 YDOT =      24054
868328  feet/sec       YDOT =        7324
011234  meter/sec
 ZDOT =       6832
646719                 ZDOT =        2079
153188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11001716
13                 X    =         3353323
08
 Y    =       10371954
04  feet           Y    =         3161371
59  meter
 Z    =      -16404801
49                 Z    =        -5000183
49
 XDOT =      -9619
698981                 XDOT =       -2932
084249
 YDOT =      21013
038630  feet/sec       YDOT =        6404
774174  meter/sec
 ZDOT =       6816
409570                 ZDOT =        2077
641637


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   19296
87014862  
00016717  00000-0  10270-3 0  9167
2 25544  51
6427  83
2027 0006590 182
6829 177
4287 15
50222112 35213


Satellite: ISS
Catalog Number: 25544
Epoch time:      19296
87014862   =   yrday
fracday
Element set:     916
Inclination:       51
6427  deg
RA of node:        83
2027  deg
Eccentricity:     
0006590     
Arg of perigee:   182
6829  deg
Mean anomaly:     177
4287  deg
Mean motion:   15
50222112  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3521
Checksum:              314
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