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

 
Date: October 4th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 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


278/06:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 5

281/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 218 7

284/20:40:00 000 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

Coasting Arc #1 (Orbit 3221)
---------------------------------------

Vector Time (GMT): 2019/277/13:29:50
425
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6779147
83                 A    =         6800993
28  meter
 Y    =        -400081
65  meter          E    =           
0019486
 Z    =         159113
57                 I    =           51
67406
 XDOT =        432
412024                 Wp   =          126
35061
 YDOT =       4737
309418  meter/sec      RA   =          177
68378  deg
 ZDOT =      -6010
105061                 TA   =           51
93837
                                          MA   =           51
76272
                                          Ha   =            229
896  n
mi
                                          Hp   =            218
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22241298
65                 X    =         6782344
92
 Y    =       -1312603
83  feet           Y    =         -324254
55  meter
 Z    =         522026
16                 Z    =          192052
29
 XDOT =       1418
674618                 XDOT =         408
600012
 YDOT =      15542
353733  feet/sec       YDOT =        4742
011629  meter/sec
 ZDOT =     -19718
192456                 ZDOT =       -6008
062521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17578152
60                 X    =        -5357820
91
 Y    =       13683116
64  feet           Y    =         4170613
95  meter
 Z    =         672068
52                 Z    =          204846
48
 XDOT =      -9087
665033                 XDOT =       -2769
920302
 YDOT =     -10643
751389  feet/sec       YDOT =       -3244
215423  meter/sec
 ZDOT =     -19709
107118                 ZDOT =       -6007
335850


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   19277
59508336  
00016717  00000-0  10270-3 0  9002
2 25544  51
6430 178
7228 0007257 114
5537 245
6371 15
50119547 32228


Satellite: ISS
Catalog Number: 25544
Epoch time:      19277
59508336   =   yrday
fracday
Element set:     900
Inclination:       51
6430  deg
RA of node:       178
7228  deg
Eccentricity:     
0007257     
Arg of perigee:   114
5537  deg
Mean anomaly:     245
6371  deg
Mean motion:   15
50119547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3222
Checksum:              314


Coasting Arc #2 (Orbit 3232)
---------------------------------------

Vector Time (GMT): 2019/278/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3337481
72                 A    =         6791320
24  meter
 Y    =        3474287
66  meter          E    =           
0017220
 Z    =       -4801724
92                 I    =           51
66238
 XDOT =      -6634
054662                 Wp   =           89
18533
 YDOT =       2763
962012  meter/sec      RA   =          174
13201  deg
 ZDOT =      -2619
099814                 TA   =          154
97360
                                          MA   =          154
89003
                                          Ha   =            229
878  n
mi
                                          Hp   =            218
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10949743
19                 X    =         3321707
51
 Y    =       11398581
56  feet           Y    =         3511521
39  meter
 Z    =      -15753690
67                 Z    =        -4785550
95
 XDOT =     -21765
271200                 XDOT =       -6651
746779
 YDOT =       9068
116837  feet/sec       YDOT =        2689
676331  meter/sec
 ZDOT =      -8592
847158                 ZDOT =       -2651
368913

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5716870
57                 X    =         1742502
15
 Y    =      -14813938
65  feet           Y    =        -4515288
50  meter
 Z    =      -15680176
01                 Z    =        -4779317
65
 XDOT =      16247
823530                 XDOT =        4952
336612
 YDOT =      15493
671893  feet/sec       YDOT =        4722
471193  meter/sec
 ZDOT =      -8739
965415                 ZDOT =       -2663
941458


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   19278
30421791  
00016717  00000-0  10270-3 0  9012
2 25544  51
6394 175
2065 0007359 115
6588 244
5324 15
50147176 32336


Satellite: ISS
Catalog Number: 25544
Epoch time:      19278
30421791   =   yrday
fracday
Element set:     901
Inclination:       51
6394  deg
RA of node:       175
2065  deg
Eccentricity:     
0007359     
Arg of perigee:   115
6588  deg
Mean anomaly:     244
5324  deg
Mean motion:   15
50147176  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3233
Checksum:              312


Coasting Arc #3 (Orbit 3248)
---------------------------------------

Vector Time (GMT): 2019/279/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3206670
41                 A    =         6790579
71  meter
 Y    =       -3363177
76  meter          E    =           
0013758
 Z    =        4943837
43                 I    =           51
69297
 XDOT =       6666
364692                 Wp   =          121
04131
 YDOT =      -3065
354659  meter/sec      RA   =          169
17916  deg
 ZDOT =       2227
118572                 TA   =          307
17187
                                          MA   =          307
29742
                                          Ha   =            229
815  n
mi
                                          Hp   =            218
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10520572
21                 X    =        -3192838
62
 Y    =      -11034047
77  feet           Y    =        -3398959
50  meter
 Z    =       16219939
07                 Z    =         4928294
24
 XDOT =      21871
275237                 XDOT =        6689
328746
 YDOT =     -10056
937856  feet/sec       YDOT =       -2990
678188  meter/sec
 ZDOT =       7306
819463                 ZDOT =        2259
557354

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5317979
85                 X    =        -1620920
26
 Y    =       14367980
05  feet           Y    =         4379360
32  meter
 Z    =       16149282
12                 Z    =         4922301
19
 XDOT =     -17491
946175                 XDOT =       -5331
545194
 YDOT =     -14895
905505  feet/sec       YDOT =       -4540
271998  meter/sec
 ZDOT =       7454
747747                 ZDOT =        2272
207113


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   19279
33568475  
00016717  00000-0  10270-3 0  9028
2 25544  51
6390 170
0964 0007178 119
7196 240
4669 15
50181468 32498


Satellite: ISS
Catalog Number: 25544
Epoch time:      19279
33568475   =   yrday
fracday
Element set:     902
Inclination:       51
6390  deg
RA of node:       170
0964  deg
Eccentricity:     
0007178     
Arg of perigee:   119
7196  deg
Mean anomaly:     240
4669  deg
Mean motion:   15
50181468  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3249
Checksum:              340


Coasting Arc #4 (Orbit 3263)
---------------------------------------

Vector Time (GMT): 2019/280/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3041787
40                 A    =         6790069
95  meter
 Y    =        3320745
00  meter          E    =           
0018789
 Z    =       -5097826
51                 I    =           51
72381
 XDOT =      -6641
170231                 Wp   =           92
98064
 YDOT =       3344
382527  meter/sec      RA   =          164
22597  deg
 ZDOT =      -1790
793184                 TA   =          159
70383
                                          MA   =          159
62905
                                          Ha   =            229
746  n
mi
                                          Hp   =            218
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9979617
45                 X    =         3029190
31
 Y    =       10894832
69  feet           Y    =         3354689
76  meter
 Z    =      -16725152
60                 Z    =        -5083081
33
 XDOT =     -21788
616242                 XDOT =       -6669
375784
 YDOT =      10972
383620  feet/sec       YDOT =        3269
958489  meter/sec
 ZDOT =      -5875
305722                 ZDOT =       -1823
122286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5187563
77                 X    =         1581169
44
 Y    =      -13914636
11  feet           Y    =        -4241181
09  meter
 Z    =      -16658119
86                 Z    =        -5077394
93
 XDOT =      18569
923792                 XDOT =        5660
112772
 YDOT =      14107
092476  feet/sec       YDOT =        4299
841787  meter/sec
 ZDOT =      -6022
769023                 ZDOT =       -1835
739998


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   19280
30268476  
00016717  00000-0  10270-3 0  9036
2 25544  51
6392 165
3039 0007217 123
0585 237
1260 15
50153886 32644


Satellite: ISS
Catalog Number: 25544
Epoch time:      19280
30268476   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:       165
3039  deg
Eccentricity:     
0007217     
Arg of perigee:   123
0585  deg
Mean anomaly:     237
1260  deg
Mean motion:   15
50153886  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3264
Checksum:              304


Coasting Arc #5 (Orbit 3279)
---------------------------------------

Vector Time (GMT): 2019/281/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2896651
93                 A    =         6789490
62  meter
 Y    =       -3275525
52  meter          E    =           
0011564
 Z    =        5187363
19                 I    =           51
75541
 XDOT =       6601
156042                 Wp   =          126
64444
 YDOT =      -3652
634052  meter/sec      RA   =          159
27679  deg
 ZDOT =       1370
832311                 TA   =          310
14728
                                          MA   =          310
24851
                                          Ha   =            229
679  n
mi
                                          Hp   =            218
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9503451
23                 X    =        -2885006
19
 Y    =      -10746474
81  feet           Y    =        -3307852
52  meter
 Z    =       17018908
10                 Z    =         5173320
76
 XDOT =      21657
336095                 XDOT =        6634
851477
 YDOT =     -11983
707521  feet/sec       YDOT =       -3578
626786  meter/sec
 ZDOT =       4497
481336                 ZDOT =        1402
980412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5036722
62                 X    =        -1535193
05
 Y    =       13513054
96  feet           Y    =         4118779
15  meter
 Z    =       16955067
38                 Z    =         5167904
54
 XDOT =     -19683
993141                 XDOT =       -5999
681109
 YDOT =     -13200
521101  feet/sec       YDOT =       -4023
518832  meter/sec
 ZDOT =       4644
154288                 ZDOT =        1415
538227


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   19281
33414628  
00016717  00000-0  10270-3 0  9043
2 25544  51
6405 160
1937 0007055 127
1931 232
9865 15
50194409 32807


Satellite: ISS
Catalog Number: 25544
Epoch time:      19281
33414628   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       160
1937  deg
Eccentricity:     
0007055     
Arg of perigee:   127
1931  deg
Mean anomaly:     232
9865  deg
Mean motion:   15
50194409  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3280
Checksum:              304


Coasting Arc #6 (Orbit 3281)
---------------------------------------

Vector Time (GMT): 2019/281/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         876947
89                 A    =         6788973
40  meter
 Y    =        4156005
08  meter          E    =           
0020983
 Z    =       -5314109
77                 I    =           51
76157
 XDOT =      -7254
366752                 Wp   =          105
39343
 YDOT =       2335
155985  meter/sec      RA   =          158
44695  deg
 ZDOT =        625
761687                 TA   =          170
60675
                                          MA   =          170
56744
                                          Ha   =            229
591  n
mi
                                          Hp   =            218
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2877125
63                 X    =          856222
15
 Y    =       13635187
27  feet           Y    =         4165695
53  meter
 Z    =      -17434743
34                 Z    =        -5309900
46
 XDOT =     -23800
415854                 XDOT =       -7282
979598
 YDOT =       7661
272916  feet/sec       YDOT =        2253
872589  meter/sec
 ZDOT =       2053
023909                 ZDOT =         590
452936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2310460
18                 X    =         -704228
26
 Y    =      -13766616
94  feet           Y    =        -4196064
84  meter
 Z    =      -17415754
10                 Z    =        -5308321
85
 XDOT =      23162
530996                 XDOT =        7059
939447
 YDOT =      -6294
862776  feet/sec       YDOT =       -1918
674174  meter/sec
 ZDOT =       1892
005314                 ZDOT =         576
683220


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   19281
46307950  
00016717  00000-0  10270-3 0  9057
2 25544  51
6432 159
5556 0007080 127
0636 233
1162 15
50187305 32827


Satellite: ISS
Catalog Number: 25544
Epoch time:      19281
46307950   =   yrday
fracday
Element set:     905
Inclination:       51
6432  deg
RA of node:       159
5556  deg
Eccentricity:     
0007080     
Arg of perigee:   127
0636  deg
Mean anomaly:     233
1162  deg
Mean motion:   15
50187305  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3282
Checksum:              298


Coasting Arc #7 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2019/282/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -762069
03                 A    =         6789092
33  meter
 Y    =       -4233243
61  meter          E    =           
0008772
 Z    =        5245047
70                 I    =           51
79298
 XDOT =       7130
403038                 Wp   =          107
67510
 YDOT =      -2611
580480  meter/sec      RA   =          153
49896  deg
 ZDOT =      -1072
914809                 TA   =          352
57415
                                          MA   =          352
58713
                                          Ha   =            229
516  n
mi
                                          Hp   =            218
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2500226
49                 X    =         -740152
69
 Y    =      -13888594
51  feet           Y    =        -4241642
67  meter
 Z    =       17208161
74                 Z    =         5241399
38
 XDOT =      23393
710755                 XDOT =        7164
288191
 YDOT =      -8568
177427  feet/sec       YDOT =       -2531
653896  meter/sec
 ZDOT =      -3520
061709                 ZDOT =       -1038
195333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2160416
92                 X    =          658495
08
 Y    =       13965742
55  feet           Y    =         4256758
33  meter
 Z    =       17191732
15                 Z    =         5240039
96
 XDOT =     -22666
345474                 XDOT =       -6908
702100
 YDOT =       7640
031627  feet/sec       YDOT =        2328
681640  meter/sec
 ZDOT =      -3361
696348                 ZDOT =       -1024
645047


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
49453679  
00016717  00000-0  10270-3 0  9062
2 25544  51
6432 154
4447 0006982 130
8875 229
2881 15
50219539 32983


Satellite: ISS
Catalog Number: 25544
Epoch time:      19282
49453679   =   yrday
fracday
Element set:     906
Inclination:       51
6432  deg
RA of node:       154
4447  deg
Eccentricity:     
0006982     
Arg of perigee:   130
8875  deg
Mean anomaly:     229
2881  deg
Mean motion:   15
50219539  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3298
Checksum:              349


Coasting Arc #8 (Orbit 3312)
---------------------------------------

Vector Time (GMT): 2019/283/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         659819
61                 A    =         6789563
30  meter
 Y    =        4366123
40  meter          E    =           
0019963
 Z    =       -5175154
44                 I    =           51
82303
 XDOT =      -6934
531978                 Wp   =          112
56099
 YDOT =       2845
518891  meter/sec      RA   =          148
55307  deg
 ZDOT =       1513
758975                 TA   =          172
03998
                                          MA   =          172
00826
                                          Ha   =            229
469  n
mi
                                          Hp   =            218
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2164762
50                 X    =          636085
52
 Y    =       14324551
84  feet           Y    =         4373368
81  meter
 Z    =      -16978853
15                 Z    =        -5172007
29
 XDOT =     -22751
089166                 XDOT =       -6973
189058
 YDOT =       9335
691900  feet/sec       YDOT =        2767
756045  meter/sec
 ZDOT =       4966
400837                 ZDOT =        1479
979248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2056598
03                 X    =         -626851
08
 Y    =      -14357203
19  feet           Y    =        -4376075
53  meter
 Z    =      -16964715
07                 Z    =        -5170845
15
 XDOT =      21879
307290                 XDOT =        6668
812862
 YDOT =      -8831
189313  feet/sec       YDOT =       -2691
746503  meter/sec
 ZDOT =       4812
290173                 ZDOT =        1466
786045


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
46152888  
00016717  00000-0  10270-3 0  9079
2 25544  51
6426 149
6533 0007001 134
0902 226
0826 15
50191944 33139


Satellite: ISS
Catalog Number: 25544
Epoch time:      19283
46152888   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:       149
6533  deg
Eccentricity:     
0007001     
Arg of perigee:   134
0902  deg
Mean anomaly:     226
0826  deg
Mean motion:   15
50191944  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3313
Checksum:              302


Coasting Arc #9 (Orbit 3328)
---------------------------------------

Vector Time (GMT): 2019/284/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -583643
81                 A    =         6789924
14  meter
 Y    =       -4494520
41  meter          E    =           
0009431
 Z    =        5047309
64                 I    =           51
85274
 XDOT =       6750
930664                 Wp   =          102
52669
 YDOT =      -3070
458414  meter/sec      RA   =          143
60957  deg
 ZDOT =      -1952
458510                 TA   =            6
36783
                                          MA   =            6
35586
                                          Ha   =            229
352  n
mi
                                          Hp   =            218
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1914841
89                 X    =         -557858
69
 Y    =      -14745801
86  feet           Y    =        -4500902
47  meter
 Z    =       16559414
84                 Z    =         5044537
55
 XDOT =      22148
722651                 XDOT =        6794
247735
 YDOT =     -10073
682462  feet/sec       YDOT =       -2994
722728  meter/sec
 ZDOT =      -6405
703774                 ZDOT =       -1919
559177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2051220
91                 X    =          625212
13
 Y    =       14741402
44  feet           Y    =         4493179
46  meter
 Z    =       16546995
46                 Z    =         5043524
22
 XDOT =     -21099
528444                 XDOT =       -6431
136270
 YDOT =       9961
694748  feet/sec       YDOT =        3036
324559  meter/sec
 ZDOT =      -6255
579147                 ZDOT =       -1906
700524


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
49298248  
00016717  00000-0  10270-3 0  9085
2 25544  51
6428 144
5425 0006866 138
8565 221
3104 15
50228075 33290


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
49298248   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:       144
5425  deg
Eccentricity:     
0006866     
Arg of perigee:   138
8565  deg
Mean anomaly:     221
3104  deg
Mean motion:   15
50228075  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3329
Checksum:              329


Coasting Arc #10 (Orbit 3334)
---------------------------------------

Vector Time (GMT): 2019/284/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3788749
31                 A    =         6789609
24  meter
 Y    =        2205863
42  meter          E    =           
0018131
 Z    =       -5199153
22                 I    =           51
86140
 XDOT =      -5133
251146                 Wp   =          100
35200
 YDOT =       5491
002181  meter/sec      RA   =          141
59204  deg
 ZDOT =      -1418
413356                 TA   =          156
05393
                                          MA   =          155
96949
                                          Ha   =            229
479  n
mi
                                          Hp   =            219
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12430279
89                 X    =         3789056
02
 Y    =        7237084
70  feet           Y    =         2248233
09  meter
 Z    =      -17057589
29                 Z    =        -5180748
14
 XDOT =     -16841
375152                 XDOT =       -5187
381662
 YDOT =      18015
099018  feet/sec       YDOT =        5433
295741  meter/sec
 ZDOT =      -4653
587127                 ZDOT =       -1443
481076

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7082278
15                 X    =         2158678
38
 Y    =       12632510
22  feet           Y    =         3850389
12  meter
 Z    =      -16973792
37                 Z    =        -5173611
91
 XDOT =     -22735
550433                 XDOT =       -6929
795772
 YDOT =       6372
363276  feet/sec       YDOT =        1942
296327  meter/sec
 ZDOT =      -4768
133993                 ZDOT =       -1453
327241


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
87977826  
00016717  00000-0  10270-3 0  9094
2 25544  51
6422 142
6221 0007234 142
9706 217
1945 15
50168365 33358


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
87977826   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:       142
6221  deg
Eccentricity:     
0007234     
Arg of perigee:   142
9706  deg
Mean anomaly:     217
1945  deg
Mean motion:   15
50168365  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3335
Checksum:              326


Coasting Arc #11 (Orbit 3350)
---------------------------------------

Vector Time (GMT): 2019/285/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3645631
13                 A    =         6789102
72  meter
 Y    =       -2239762
27  meter          E    =           
0010645
 Z    =        5266128
89                 I    =           51
88605
 XDOT =       4970
103930                 Wp   =          138
15416
 YDOT =      -5753
917914  meter/sec      RA   =          136
65043  deg
 ZDOT =        984
599513                 TA   =          302
40010
                                          MA   =          302
50305
                                          Ha   =            229
455  n
mi
                                          Hp   =            219
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11960732
06                 X    =        -3645894
86
 Y    =       -7348301
42  feet           Y    =        -2280531
25  meter
 Z    =       17277325
76                 Z    =         5248419
07
 XDOT =      16306
115257                 XDOT =        5029
293803
 YDOT =     -18877
683444  feet/sec       YDOT =       -5698
007655  meter/sec
 ZDOT =       3230
313362                 ZDOT =        1008
887132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6837006
67                 X    =        -2083919
63
 Y    =      -12373018
15  feet           Y    =        -3771295
93  meter
 Z    =       17196697
14                 Z    =         5241553
29
 XDOT =      22604
373165                 XDOT =        6889
812941
 YDOT =      -7805
965576  feet/sec       YDOT =       -2379
258307  meter/sec
 ZDOT =       3341
333785                 ZDOT =        1018
438538


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
91122743  
00016717  00000-0  10270-3 0  9102
2 25544  51
6426 137
5109 0007191 145
7704 214
3911 15
50217347 33516


Satellite: ISS
Catalog Number: 25544
Epoch time:      19285
91122743   =   yrday
fracday
Element set:     910
Inclination:       51
6426  deg
RA of node:       137
5109  deg
Eccentricity:     
0007191     
Arg of perigee:   145
7704  deg
Mean anomaly:     214
3911  deg
Mean motion:   15
50217347  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3351
Checksum:              292


Coasting Arc #12 (Orbit 3365)
---------------------------------------

Vector Time (GMT): 2019/286/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3509028
40                 A    =         6789002
12  meter
 Y    =        2345780
98  meter          E    =           
0018991
 Z    =       -5332784
28                 I    =           51
90719
 XDOT =      -4765
535313                 Wp   =          105
64195
 YDOT =       5960
119618  meter/sec      RA   =          131
71010  deg
 ZDOT =       -520
558531                 TA   =          159
43546
                                          MA   =          159
35891
                                          Ha   =            229
325  n
mi
                                          Hp   =            219
352

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11512560
37                 X    =         3508440
63
 Y    =        7696131
83  feet           Y    =         2385017
64  meter
 Z    =      -17496011
41                 Z    =        -5315740
03
 XDOT =     -15634
958375                 XDOT =       -4829
300277
 YDOT =      19554
198223  feet/sec       YDOT =        5906
471458  meter/sec
 ZDOT =      -1707
869196                 ZDOT =        -543
863603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6489870
31                 X    =         1978112
47
 Y    =       12343422
79  feet           Y    =         3762275
27  meter
 Z    =      -17418421
39                 Z    =        -5309134
84
 XDOT =     -22206
642211                 XDOT =       -6768
584546
 YDOT =       9145
578553  feet/sec       YDOT =        2787
572343  meter/sec
 ZDOT =      -1814
439348                 ZDOT =        -553
041113


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
87821108  
00016717  00000-0  10270-3 0  9110
2 25544  51
6410 132
7194 0007128 149
0343 211
1229 15
50172901 33665


Satellite: ISS
Catalog Number: 25544
Epoch time:      19286
87821108   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:       132
7194  deg
Eccentricity:     
0007128     
Arg of perigee:   149
0343  deg
Mean anomaly:     211
1229  deg
Mean motion:   15
50172901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3366
Checksum:              289


Coasting Arc #13 (Orbit 3381)
---------------------------------------

Vector Time (GMT): 2019/287/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3402603
25                 A    =         6788750
39  meter
 Y    =       -2435604
67  meter          E    =           
0008685
 Z    =        5340976
44                 I    =           51
92832
 XDOT =       4543
801724                 Wp   =          139
51805
 YDOT =      -6174
853653  meter/sec      RA   =          126
77138  deg
 ZDOT =         72
372404                 TA   =          309
75668
                                          MA   =          309
83316
                                          Ha   =            229
303  n
mi
                                          Hp   =            219
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11163396
50                 X    =        -3401058
84
 Y    =       -7990828
97  feet           Y    =        -2473645
93  meter
 Z    =       17522888
57                 Z    =         5324451
41
 XDOT =      14907
485970                 XDOT =        4612
161468
 YDOT =     -20258
706212  feet/sec       YDOT =       -6123
659426  meter/sec
 ZDOT =        237
442270                 ZDOT =          94
611529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6255114
54                 X    =        -1906558
91
 Y    =      -12327964
88  feet           Y    =        -3757563
70  meter
 Z    =       17447670
81                 Z    =         5318050
06
 XDOT =      21732
616157                 XDOT =        6624
101405
 YDOT =     -10516
608032  feet/sec       YDOT =       -3205
462128  meter/sec
 ZDOT =        339
184701                 ZDOT =         103
383497


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
90965641  
00016717  00000-0  10270-3 0  9127
2 25544  51
6411 127
6083 0007147 153
0912 207
0611 15
50220332 33823


Satellite: ISS
Catalog Number: 25544
Epoch time:      19287
90965641   =   yrday
fracday
Element set:     912
Inclination:       51
6411  deg
RA of node:       127
6083  deg
Eccentricity:     
0007147     
Arg of perigee:   153
0912  deg
Mean anomaly:     207
0611  deg
Mean motion:   15
50220332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3382
Checksum:              284


Coasting Arc #14 (Orbit 3396)
---------------------------------------

Vector Time (GMT): 2019/288/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3316964
79                 A    =         6788926
26  meter
 Y    =        2587866
28  meter          E    =           
0019019
 Z    =       -5343825
67                 I    =           51
94704
 XDOT =      -4287
666582                 Wp   =          112
39673
 YDOT =       6321
610259  meter/sec      RA   =          121
83291  deg
 ZDOT =        394
064638                 TA   =          161
38954
                                          MA   =          161
31989
                                          Ha   =            229
146  n
mi
                                          Hp   =            219
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10882430
41                 X    =         3313738
01
 Y    =        8490374
92  feet           Y    =         2624940
56  meter
 Z    =      -17532236
46                 Z    =        -5327720
68
 XDOT =     -14067
147579                 XDOT =       -4359
952188
 YDOT =      20740
191137  feet/sec       YDOT =        6273
258393  meter/sec
 ZDOT =       1292
862984                 ZDOT =         373
060270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5990268
40                 X    =         1825833
81
 Y    =       12537745
03  feet           Y    =         3821504
69  meter
 Z    =      -17458943
48                 Z    =        -5321485
97
 XDOT =     -21001
570800                 XDOT =       -6401
278780
 YDOT =      11727
704451  feet/sec       YDOT =        3574
604317  meter/sec
 ZDOT =       1196
719484                 ZDOT =         364
760099


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
87663529  
00016717  00000-0  10270-3 0  9135
2 25544  51
6406 122
8159 0007041 156
0326 204
1153 15
50180416 33976


Satellite: ISS
Catalog Number: 25544
Epoch time:      19288
87663529   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:       122
8159  deg
Eccentricity:     
0007041     
Arg of perigee:   156
0326  deg
Mean anomaly:     204
1153  deg
Mean motion:   15
50180416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3397
Checksum:              305


Coasting Arc #15 (Orbit 3412)
---------------------------------------

Vector Time (GMT): 2019/289/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3261593
16                 A    =         6788943
62  meter
 Y    =       -2720053
73  meter          E    =           
0007264
 Z    =        5291333
94                 I    =           51
96486
 XDOT =       4025
850163                 Wp   =          133
03276
 YDOT =      -6469
625292  meter/sec      RA   =          116
89660  deg
 ZDOT =       -848
310182                 TA   =          325
01883
                                          MA   =          325
06653
                                          Ha   =            229
111  n
mi
                                          Hp   =            219
522

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10700764
97                 X    =        -3256637
38
 Y    =       -8924060
80  feet           Y    =        -2756499
25  meter
 Z    =       17360019
48                 Z    =         5275502
06
 XDOT =      13208
169825                 XDOT =        4102
016908
 YDOT =     -21225
804765  feet/sec       YDOT =       -6424
179552  meter/sec
 ZDOT =      -2783
169888                 ZDOT =        -828
568337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5851594
98                 X    =        -1783566
15
 Y    =      -12743627
64  feet           Y    =        -3884257
70  meter
 Z    =       17287981
35                 Z    =         5269376
72
 XDOT =      20221
437609                 XDOT =        6163
494183
 YDOT =     -12919
935481  feet/sec       YDOT =       -3937
996335  meter/sec
 ZDOT =      -2692
750261                 ZDOT =        -820
750280


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
90807405  
00016717  00000-0  10270-3 0  9144
2 25544  51
6412 117
7047 0006986 159
3458 200
7976 15
50228401 34132


Satellite: ISS
Catalog Number: 25544
Epoch time:      19289
90807405   =   yrday
fracday
Element set:     914
Inclination:       51
6412  deg
RA of node:       117
7047  deg
Eccentricity:     
0006986     
Arg of perigee:   159
3458  deg
Mean anomaly:     200
7976  deg
Mean motion:   15
50228401  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3413
Checksum:              320


Coasting Arc #16 (Orbit 3427)
---------------------------------------

Vector Time (GMT): 2019/290/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3239827
42                 A    =         6789405
95  meter
 Y    =        2899715
98  meter          E    =           
0018330
 Z    =       -5230004
82                 I    =           51
97935
 XDOT =      -3739
488249                 Wp   =          119
50924
 YDOT =       6543
263625  meter/sec      RA   =          111
96100  deg
 ZDOT =       1306
011053                 TA   =          163
03926
                                          MA   =          162
97791
                                          Ha   =            228
984  n
mi
                                          Hp   =            219
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10629355
05                 X    =         3232566
28
 Y    =        9513503
87  feet           Y    =         2935905
32  meter
 Z    =      -17158808
47                 Z    =        -5214284
24
 XDOT =     -12268
662233                 XDOT =       -3818
723033
 YDOT =      21467
400346  feet/sec       YDOT =        6501
003023  meter/sec
 ZDOT =       4284
813166                 ZDOT =        1287
652982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5756349
06                 X    =         1754535
19
 Y    =       13145477
94  feet           Y    =         4006741
68  meter
 Z    =      -17087290
84                 Z    =        -5208206
25
 XDOT =     -19217
502230                 XDOT =       -5857
494680
 YDOT =      13898
371515  feet/sec       YDOT =        4236
223638  meter/sec
 ZDOT =       4200
674343                 ZDOT =        1280
365540


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
87504865  
00016717  00000-0  10270-3 0  9157
2 25544  51
6405 112
9127 0006953 161
5728 198
5676 15
50187793 34284


Satellite: ISS
Catalog Number: 25544
Epoch time:      19290
87504865   =   yrday
fracday
Element set:     915
Inclination:       51
6405  deg
RA of node:       112
9127  deg
Eccentricity:     
0006953     
Arg of perigee:   161
5728  deg
Mean anomaly:     198
5676  deg
Mean motion:   15
50187793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3428
Checksum:              345


Coasting Arc #17 (Orbit 3443)
---------------------------------------

Vector Time (GMT): 2019/291/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3246621
59                 A    =         6789702
52  meter
 Y    =       -3053037
12  meter          E    =           
0007080
 Z    =        5116204
75                 I    =           51
99233
 XDOT =       3459
008910                 Wp   =          122
25520
 YDOT =      -6614
099948  meter/sec      RA   =          107
02732  deg
 ZDOT =      -1753
793808                 TA   =          344
61015
                                          MA   =          344
63167
                                          Ha   =            228
950  n
mi
                                          Hp   =            219
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10651645
62                 X    =        -3237092
60
 Y    =      -10016525
98  feet           Y    =        -3089289
85  meter
 Z    =       16785448
65                 Z    =         5100456
66
 XDOT =      11348
454428                 XDOT =        3541
231765
 YDOT =     -21699
802980  feet/sec       YDOT =       -6574
959135  meter/sec
 ZDOT =      -5753
916692                 ZDOT =       -1736
791132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5796325
56                 X    =        -1766720
03
 Y    =      -13512607
29  feet           Y    =        -4118642
70  meter
 Z    =       16713817
26                 Z    =         5094371
50
 XDOT =      18202
889726                 XDOT =        5548
240789
 YDOT =     -14821
061951  feet/sec       YDOT =       -4517
459683  meter/sec
 ZDOT =      -5675
930343                 ZDOT =       -1730
023568


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
90648364  
00016717  00000-0  10270-3 0  9166
2 25544  51
6406 107
8019 0006960 166
0410 194
0934 15
50231241 34448


Satellite: ISS
Catalog Number: 25544
Epoch time:      19291
90648364   =   yrday
fracday
Element set:     916
Inclination:       51
6406  deg
RA of node:       107
8019  deg
Eccentricity:     
0006960     
Arg of perigee:   166
0410  deg
Mean anomaly:     194
0934  deg
Mean motion:   15
50231241  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3444
Checksum:              298
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