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

 
Date: December 18th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14591 557 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 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


355/13:08:55 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 5

356/04:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 5

359/09:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 1
000/00:00:00 000 0 0 0 0 218 3

361/01:32:57 259 -0 9 1 8 1 8
N/A 1 5 -0 0 230 1
000/00:09:54 517 -0 1 -0 0 219 4

361/04:40:25 361 -0 9 1 6 1 6
N/A 1 3 0 0 230 0
000/00:08:50 721 0 1 0 0 220 3

362/07:16:34 000 0 0 0 0 0 0
N/A 0 0 0 0 230 1
000/00:00:00 000 0 0 0 0 220 2

362/13:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 1
000/00:00:00 000 0 0 0 0 220 4

Coasting Arc #1 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2019/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4381805
50                 A    =         6794395
75  meter
 Y    =        3402154
28  meter          E    =           
0011805
 Z    =       -3929708
41                 I    =           51
65650
 XDOT =      -5834
478017                 Wp   =           72
06998
 YDOT =      -2837
873058  meter/sec      RA   =          176
25071  deg
 ZDOT =       4062
424269                 TA   =          240
45291
                                          MA   =          240
57065
                                          Ha   =            229
601  n
mi
                                          Hp   =            218
874

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14376002
29                 X    =        -4400435
53
 Y    =       11161923
50  feet           Y    =         3353050
15  meter
 Z    =      -12892744
14                 Z    =        -3951038
25
 XDOT =     -19141
988246                 XDOT =       -5822
043308
 YDOT =      -9310
607146  feet/sec       YDOT =       -2903
049287  meter/sec
 ZDOT =      13328
163613                 ZDOT =        4034
112632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9592431
93                 X    =        -2923773
25
 Y    =      -15385591
95  feet           Y    =        -4689528
43  meter
 Z    =      -12990367
18                 Z    =        -3959463
92
 XDOT =      10163
622234                 XDOT =        3097
872057
 YDOT =     -17443
448905  feet/sec       YDOT =       -5316
763226  meter/sec
 ZDOT =      13198
976696                 ZDOT =        4023
048097


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   19350
50859596  
00016717  00000-0  10270-3 0  9002
2 25544  51
6378 177
4360 0007414  40
2449 319
9249 15
50120225  3530


Satellite: ISS
Catalog Number: 25544
Epoch time:      19350
50859596   =   yrday
fracday
Element set:     900
Inclination:       51
6378  deg
RA of node:       177
4360  deg
Eccentricity:     
0007414     
Arg of perigee:    40
2449  deg
Mean anomaly:     319
9249  deg
Mean motion:   15
50120225  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              306


Coasting Arc #2 (Orbit 368)
---------------------------------------

Vector Time (GMT): 2019/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4469672
21                 A    =         6795312
44  meter
 Y    =       -3591436
87  meter          E    =           
0017899
 Z    =        3638046
49                 I    =           51
69302
 XDOT =       5705
942459                 Wp   =           69
82212
 YDOT =       2632
944040  meter/sec      RA   =          171
29825  deg
 ZDOT =      -4387
485027                 TA   =           67
11940
                                          MA   =           66
93053
                                          Ha   =            229
582  n
mi
                                          Hp   =            218
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14664278
92                 X    =         4491829
05
 Y    =      -11782929
36  feet           Y    =        -3541330
30  meter
 Z    =       11935848
06                 Z    =         3659811
77
 XDOT =      18720
283658                 XDOT =        5697
387827
 YDOT =       8638
267848  feet/sec       YDOT =        2696
704521  meter/sec
 ZDOT =     -14394
635914                 ZDOT =       -4359
788435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10448277
75                 X    =         3184635
06
 Y    =       15566746
78  feet           Y    =         4744744
42  meter
 Z    =       12035483
21                 Z    =         3668415
28
 XDOT =      -9130
281371                 XDOT =       -2782
909762
 YDOT =      17219
005069  feet/sec       YDOT =        5248
352745  meter/sec
 ZDOT =     -14268
226627                 ZDOT =       -4348
955476


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   19351
54009333  
00016717  00000-0  10270-3 0  9014
2 25544  51
6379 172
3247 0007324  42
8938 317
2782 15
50125834  3691


Satellite: ISS
Catalog Number: 25544
Epoch time:      19351
54009333   =   yrday
fracday
Element set:     901
Inclination:       51
6379  deg
RA of node:       172
3247  deg
Eccentricity:     
0007324     
Arg of perigee:    42
8938  deg
Mean anomaly:     317
2782  deg
Mean motion:   15
50125834  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             369
Checksum:              309


Coasting Arc #3 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2019/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4484695
67                 A    =         6796109
84  meter
 Y    =        3832253
01  meter          E    =           
0011462
 Z    =       -3378555
51                 I    =           51
72826
 XDOT =      -5570
614058                 Wp   =           65
10575
 YDOT =      -2428
196967  meter/sec      RA   =          166
34836  deg
 ZDOT =       4657
271033                 TA   =          255
61932
                                          MA   =          255
74658
                                          Ha   =            229
704  n
mi
                                          Hp   =            218
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14713568
49                 X    =        -4510804
69
 Y    =       12573008
58  feet           Y    =         3781956
25  meter
 Z    =      -11084499
72                 Z    =        -3400403
47
 XDOT =     -18276
292840                 XDOT =       -5565
669533
 YDOT =      -7966
525482  feet/sec       YDOT =       -2490
464225  meter/sec
 ZDOT =      15279
760606                 ZDOT =        4630
223056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11498714
12                 X    =        -3504808
06
 Y    =      -15495853
27  feet           Y    =        -4723136
08  meter
 Z    =      -11184537
60                 Z    =        -3409047
06
 XDOT =       8123
376273                 XDOT =        2476
005088
 YDOT =     -16927
252902  feet/sec       YDOT =       -5159
426685  meter/sec
 ZDOT =      15156
286371                 ZDOT =        4619
636086


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   19352
50712477  
00016717  00000-0  10270-3 0  9022
2 25544  51
6376 167
5328 0007356  48
5103 311
6678 15
50117311  3846


Satellite: ISS
Catalog Number: 25544
Epoch time:      19352
50712477   =   yrday
fracday
Element set:     902
Inclination:       51
6376  deg
RA of node:       167
5328  deg
Eccentricity:     
0007356     
Arg of perigee:    48
5103  deg
Mean anomaly:     311
6678  deg
Mean motion:   15
50117311  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              302


Coasting Arc #4 (Orbit 399)
---------------------------------------

Vector Time (GMT): 2019/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4516863
51                 A    =         6796990
89  meter
 Y    =       -4053821
30  meter          E    =           
0018893
 Z    =        3047816
06                 I    =           51
76400
 XDOT =       5400
414416                 Wp   =           80
28794
 YDOT =       2285
207373  meter/sec      RA   =          161
40112  deg
 ZDOT =      -4934
731234                 TA   =           64
86845
                                          MA   =           64
67257
                                          Ha   =            229
700  n
mi
                                          Hp   =            218
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14819106
00                 X    =         4547054
26
 Y    =      -13299938
63  feet           Y    =        -4003141
93  meter
 Z    =        9999396
53                 Z    =         3069830
30
 XDOT =      17717
895065                 XDOT =        5398
429319
 YDOT =       7497
399517  feet/sec       YDOT =        2345
587853  meter/sec
 ZDOT =     -16190
063105                 ZDOT =       -4908
502772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12483404
81                 X    =         3804941
79
 Y    =       15447730
66  feet           Y    =         4708468
31  meter
 Z    =       10100218
96                 Z    =         3078546
74
 XDOT =      -7321
607694                 XDOT =       -2231
626025
 YDOT =      16485
904386  feet/sec       YDOT =        5024
903657  meter/sec
 ZDOT =     -16070
311729                 ZDOT =       -4898
231015


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   19353
53862159  
00016717  00000-0  10270-3 0  9030
2 25544  51
6381 162
4212 0007313  50
8051 309
3748 15
50127004  4000


Satellite: ISS
Catalog Number: 25544
Epoch time:      19353
53862159   =   yrday
fracday
Element set:     903
Inclination:       51
6381  deg
RA of node:       162
4212  deg
Eccentricity:     
0007313     
Arg of perigee:    50
8051  deg
Mean anomaly:     309
3748  deg
Mean motion:   15
50127004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             400
Checksum:              274


Coasting Arc #5 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2019/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4470496
94                 A    =         6797720
52  meter
 Y    =        4314931
80  meter          E    =           
0012245
 Z    =       -2757435
12                 I    =           51
79809
 XDOT =      -5237
800881                 Wp   =           58
19429
 YDOT =      -2145
390046  meter/sec      RA   =          156
45660  deg
 ZDOT =       5157
726396                 TA   =          270
72807
                                          MA   =          270
86837
                                          Ha   =            229
851  n
mi
                                          Hp   =            218
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14666984
70                 X    =        -4505021
40
 Y    =       14156600
39  feet           Y    =         4264746
69  meter
 Z    =       -9046703
14                 Z    =        -2779234
72
 XDOT =     -17184
386092                 XDOT =       -5238
474631
 YDOT =      -7038
681252  feet/sec       YDOT =       -2203
966957  meter/sec
 ZDOT =      16921
674528                 ZDOT =        5132
281294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13608781
86                 X    =        -4147956
71
 Y    =      -15116675
09  feet           Y    =        -4607562
57  meter
 Z    =       -9146573
31                 Z    =        -2787875
54
 XDOT =       6567
351637                 XDOT =        2001
728779
 YDOT =     -16035
285980  feet/sec       YDOT =       -4887
555167  meter/sec
 ZDOT =      16805
483667                 ZDOT =        5122
311422


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   19354
50565164  
00016717  00000-0  10270-3 0  9045
2 25544  51
6384 157
6294 0007505  56
6864 303
5004 15
50120647  4151


Satellite: ISS
Catalog Number: 25544
Epoch time:      19354
50565164   =   yrday
fracday
Element set:     904
Inclination:       51
6384  deg
RA of node:       157
6294  deg
Eccentricity:     
0007505     
Arg of perigee:    56
6864  deg
Mean anomaly:     303
5004  deg
Mean motion:   15
50120647  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              300


Coasting Arc #6 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2019/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957055
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4438989
33                 A    =         6798539
42  meter
 Y    =       -4549853
23  meter          E    =           
0019603
 Z    =        2394097
45                 I    =           51
82951
 XDOT =       5047
866093                 Wp   =           90
41022
 YDOT =       2073
473422  meter/sec      RA   =          151
51497  deg
 ZDOT =      -5380
991213                 TA   =           62
95335
                                          MA   =           62
75341
                                          Ha   =            229
863  n
mi
                                          Hp   =            218
501

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14563613
28                 X    =         4477907
95
 Y    =      -14927339
98  feet           Y    =        -4499995
90  meter
 Z    =        7854650
44                 Z    =         2415754
66
 XDOT =      16561
240462                 XDOT =        5050
442729
 YDOT =       6802
734323  feet/sec       YDOT =        2129
937073  meter/sec
 ZDOT =     -17654
170647                 ZDOT =       -5356
464026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14639328
88                 X    =         4462067
44
 Y    =       14800181
33  feet           Y    =         4511095
27  meter
 Z    =        7953900
12                 Z    =         2424348
76
 XDOT =      -6048
322698                 XDOT =       -1843
528758
 YDOT =      15476
122049  feet/sec       YDOT =        4717
122000  meter/sec
 ZDOT =     -17542
160590                 ZDOT =       -5346
850548


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   19355
53714888  
00016717  00000-0  10270-3 0  9059
2 25544  51
6369 152
5181 0007407  59
7690 300
4193 15
50117307  4317


Satellite: ISS
Catalog Number: 25544
Epoch time:      19355
53714888   =   yrday
fracday
Element set:     905
Inclination:       51
6369  deg
RA of node:       152
5181  deg
Eccentricity:     
0007407     
Arg of perigee:    59
7690  deg
Mean anomaly:     300
4193  deg
Mean motion:   15
50117307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              310


Coasting Arc #7 (Orbit 431)
---------------------------------------

Vector Time (GMT): 2019/355/13:08:55
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4692260
57                 A    =         6791972
90  meter
 Y    =       -1588504
46  meter          E    =           
0014056
 Z    =        4634386
32                 I    =           51
81095
 XDOT =       4727
357454                 Wp   =           89
99626
 YDOT =      -5255
353225  meter/sec      RA   =          151
32077  deg
 ZDOT =       2977
249685                 TA   =          330
36931
                                          MA   =          330
44887
                                          Ha   =            229
955  n
mi
                                          Hp   =            218
519

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15394555
68                 X    =        -4696660
10
 Y    =       -5211628
81  feet           Y    =        -1641001
62  meter
 Z    =       15204679
52                 Z    =         4611582
14
 XDOT =      15509
702933                 XDOT =        4771
311106
 YDOT =     -17241
972523  feet/sec       YDOT =       -5202
243055  meter/sec
 ZDOT =       9767
879544                 ZDOT =        3000
319854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         693869
14                 X    =          211491
31
 Y    =      -16334887
86  feet           Y    =        -4978873
82  meter
 Z    =       15100519
30                 Z    =         4602638
28
 XDOT =      19665
799201                 XDOT =        5994
135597
 YDOT =       9986
670435  feet/sec       YDOT =        3043
937149  meter/sec
 ZDOT =       9873
627580                 ZDOT =        3009
481686


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   19355
60161715  
00016717  00000-0  10270-3 0  9063
2 25544  51
6388 152
1985 0007289  60
8096 299
3783 15
50143729  4326


Satellite: ISS
Catalog Number: 25544
Epoch time:      19355
60161715   =   yrday
fracday
Element set:     906
Inclination:       51
6388  deg
RA of node:       152
1985  deg
Eccentricity:     
0007289     
Arg of perigee:    60
8096  deg
Mean anomaly:     299
3783  deg
Mean motion:   15
50143729  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             432
Checksum:              333


Coasting Arc #8 (Orbit 440)
---------------------------------------

Vector Time (GMT): 2019/356/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         586291
59                 A    =         6789878
28  meter
 Y    =        4402488
87  meter          E    =           
0019862
 Z    =       -5152740
91                 I    =           51
82372
 XDOT =      -6930
595590                 Wp   =           87
15022
 YDOT =       2802
250322  meter/sec      RA   =          148
22394  deg
 ZDOT =       1611
986281                 TA   =          198
36729
                                          MA   =          198
43912
                                          Ha   =            229
971  n
mi
                                          Hp   =            218
471

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1923528
83                 X    =          562047
40
 Y    =       14443861
11  feet           Y    =         4408910
12  meter
 Z    =      -16905317
95                 Z    =        -5149951
38
 XDOT =     -22738
174508                 XDOT =       -6969
246253
 YDOT =       9193
734652  feet/sec       YDOT =        2724
531241  meter/sec
 ZDOT =       5288
668901                 ZDOT =        1578
226235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5418859
43                 X    =         1651668
35
 Y    =      -13541928
86  feet           Y    =        -4127579
92  meter
 Z    =      -16892808
74                 Z    =        -5148928
10
 XDOT =      23341
352368                 XDOT =        7114
444202
 YDOT =       2961
473974  feet/sec       YDOT =         902
657267  meter/sec
 ZDOT =       5134
171351                 ZDOT =        1564
895428


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   19356
18183597  
00016717  00000-0  10270-3 0  9070
2 25544  51
6406 149
3283 0007631  59
1523 301
0378 15
50115485  4412


Satellite: ISS
Catalog Number: 25544
Epoch time:      19356
18183597   =   yrday
fracday
Element set:     907
Inclination:       51
6406  deg
RA of node:       149
3283  deg
Eccentricity:     
0007631     
Arg of perigee:    59
1523  deg
Mean anomaly:     301
0378  deg
Mean motion:   15
50115485  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             441
Checksum:              306


Coasting Arc #9 (Orbit 456)
---------------------------------------

Vector Time (GMT): 2019/357/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -515296
42                 A    =         6790281
42  meter
 Y    =       -4534464
70  meter          E    =           
0013457
 Z    =        5020057
36                 I    =           51
85351
 XDOT =       6742
057739                 Wp   =           59
92910
 YDOT =      -3033
026424  meter/sec      RA   =          143
28085  deg
 ZDOT =      -2036
930850                 TA   =           49
87043
                                          MA   =           49
75260
                                          Ha   =            229
954  n
mi
                                          Hp   =            218
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1690605
06                 X    =         -488937
20
 Y    =      -14876852
70  feet           Y    =        -4540080
31  meter
 Z    =       16470004
47                 Z    =         5017617
73
 XDOT =      22119
612003                 XDOT =        6785
367174
 YDOT =      -9950
874095  feet/sec       YDOT =       -2957
389574  meter/sec
 ZDOT =      -6682
843997                 ZDOT =       -2004
075436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5600662
27                 X    =        -1707081
86
 Y    =       13898569
75  feet           Y    =         4236284
06  meter
 Z    =       16459109
34                 Z    =         5016736
53
 XDOT =     -23201
422469                 XDOT =       -7071
793569
 YDOT =      -1572
064479  feet/sec       YDOT =        -479
165253  meter/sec
 ZDOT =      -6532
443027                 ZDOT =       -1991
088635


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   19357
21333217  
00016717  00000-0  10270-3 0  9082
2 25544  51
6408 144
2174 0007592  62
1308 298
0611 15
50146720  4576


Satellite: ISS
Catalog Number: 25544
Epoch time:      19357
21333217   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       144
2174  deg
Eccentricity:     
0007592     
Arg of perigee:    62
1308  deg
Mean anomaly:     298
0611  deg
Mean motion:   15
50146720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             457
Checksum:              292


Coasting Arc #10 (Orbit 471)
---------------------------------------

Vector Time (GMT): 2019/358/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         513082
37                 A    =         6790921
92  meter
 Y    =        4689934
39  meter          E    =           
0018382
 Z    =       -4900500
29                 I    =           51
88262
 XDOT =      -6493
904970                 Wp   =           91
45825
 YDOT =       3233
870024  meter/sec      RA   =          138
33943  deg
 ZDOT =       2422
403953                 TA   =          202
24098
                                          MA   =          202
32081
                                          Ha   =            230
038  n
mi
                                          Hp   =            218
344

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1683341
10                 X    =          484404
00
 Y    =       15386923
85  feet           Y    =         4695512
36  meter
 Z    =      -16077756
87                 Z    =        -4898076
94
 XDOT =     -21305
462501                 XDOT =       -6541
351137
 YDOT =      10609
809790  feet/sec       YDOT =        3160
984969  meter/sec
 ZDOT =       7947
519531                 ZDOT =        2390
744096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5607964
80                 X    =         1709307
67
 Y    =      -14439151
01  feet           Y    =        -4401053
23  meter
 Z    =      -16066952
97                 Z    =        -4897207
27
 XDOT =      22788
404313                 XDOT =        6945
905635
 YDOT =        195
561811  feet/sec       YDOT =          59
607240  meter/sec
 ZDOT =       7802
545696                 ZDOT =        2378
215928


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   19358
18036034  
00016717  00000-0  10270-3 0  9097
2 25544  51
6419 139
4254 0007681  65
7269 294
4683 15
50120472  4729


Satellite: ISS
Catalog Number: 25544
Epoch time:      19358
18036034   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       139
4254  deg
Eccentricity:     
0007681     
Arg of perigee:    65
7269  deg
Mean anomaly:     294
4683  deg
Mean motion:   15
50120472  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             472
Checksum:              320


Coasting Arc #11 (Orbit 487)
---------------------------------------

Vector Time (GMT): 2019/359/04:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -496114
79                 A    =         6791533
29  meter
 Y    =       -4853993
99  meter          E    =           
0015528
 Z    =        4714717
03                 I    =           51
90887
 XDOT =       6265
219377                 Wp   =           66
35741
 YDOT =      -3399
611183  meter/sec      RA   =          133
40089  deg
 ZDOT =      -2827
343740                 TA   =           51
64740
                                          MA   =           51
50796
                                          Ha   =            230
032  n
mi
                                          Hp   =            218
255

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1627673
21                 X    =         -464700
60
 Y    =      -15925177
14  feet           Y    =        -4859366
97  meter
 Z    =       15468231
73                 Z    =         4712382
66
 XDOT =      20555
181683                 XDOT =        6316
502830
 YDOT =     -11153
579996  feet/sec       YDOT =       -3329
261898  meter/sec
 ZDOT =      -9276
062140                 ZDOT =       -2796
785632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5655486
18                 X    =        -1723792
19
 Y    =       14986562
45  feet           Y    =         4567904
23  meter
 Z    =       15457852
44                 Z    =         4711553
42
 XDOT =     -22340
114491                 XDOT =       -6809
266897
 YDOT =       1038
359634  feet/sec       YDOT =         316
492017  meter/sec
 ZDOT =      -9136
088657                 ZDOT =       -2784
679823


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   19359
21185671  
00016717  00000-0  10270-3 0  9106
2 25544  51
6415 134
3149 0007665  69
0428 291
1542 15
50149197  4888


Satellite: ISS
Catalog Number: 25544
Epoch time:      19359
21185671   =   yrday
fracday
Element set:     910
Inclination:       51
6415  deg
RA of node:       134
3149  deg
Eccentricity:     
0007665     
Arg of perigee:    69
0428  deg
Mean anomaly:     291
1542  deg
Mean motion:   15
50149197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             488
Checksum:              318


Coasting Arc #12 (Orbit 491)
---------------------------------------

Vector Time (GMT): 2019/359/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4859901
72                 A    =         6800907
17  meter
 Y    =        4714183
93  meter          E    =           
0020141
 Z    =         546593
14                 I    =           51
94122
 XDOT =      -2943
949996                 Wp   =           59
21246
 YDOT =      -3748
755531  meter/sec      RA   =          132
24811  deg
 ZDOT =       6002
610336                 TA   =          306
65323
                                          MA   =          306
83822
                                          Ha   =            230
052  n
mi
                                          Hp   =            218
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15944559
45                 X    =        -4914910
94
 Y    =       15466482
72  feet           Y    =         4659529
42  meter
 Z    =        1793284
57                 Z    =          522852
72
 XDOT =      -9658
628597                 XDOT =       -2930
968803
 YDOT =     -12299
066703  feet/sec       YDOT =       -3781
605205  meter/sec
 ZDOT =      19693
603464                 ZDOT =        5988
340705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5030265
83                 X    =        -1533225
02
 Y    =      -21645233
49  feet           Y    =        -6597467
17  meter
 Z    =        1684406
86                 Z    =          513407
21
 XDOT =      14006
853941                 XDOT =        4269
289081
 YDOT =      -1685
877711  feet/sec       YDOT =        -513
855526  meter/sec
 ZDOT =      19628
566729                 ZDOT =        5982
787139


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   19359
46973140  
00016717  00000-0  10270-3 0  9110
2 25544  51
6376 133
0324 0007568  73
4145 286
7837 15
50117612  4921


Satellite: ISS
Catalog Number: 25544
Epoch time:      19359
46973140   =   yrday
fracday
Element set:     911
Inclination:       51
6376  deg
RA of node:       133
0324  deg
Eccentricity:     
0007568     
Arg of perigee:    73
4145  deg
Mean anomaly:     286
7837  deg
Mean motion:   15
50117612  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              315


Coasting Arc #13 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2019/360/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 987055
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4650710
03                 A    =         6800522
96  meter
 Y    =       -4865188
21  meter          E    =           
0014763
 Z    =        -957820
33                 I    =           51
96338
 XDOT =       2869
402410                 Wp   =          113
14478
 YDOT =       3896
177790  meter/sec      RA   =          127
31671  deg
 ZDOT =      -5936
183785                 TA   =           77
15995
                                          MA   =           76
99504
                                          Ha   =            230
029  n
mi
                                          Hp   =            218
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15258235
00                 X    =         4709420
86
 Y    =      -15961903
58  feet           Y    =        -4812852
26  meter
 Z    =       -3142455
14                 Z    =         -935087
25
 XDOT =       9414
049901                 XDOT =        2854
455433
 YDOT =      12782
735533  feet/sec       YDOT =        3928
182845  meter/sec
 ZDOT =     -19475
668587                 ZDOT =       -5922
281082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6169784
39                 X    =         1880550
28
 Y    =       21217316
58  feet           Y    =         6467038
09  meter
 Z    =       -3038151
29                 Z    =         -926028
51
 XDOT =     -14296
000880                 XDOT =       -4357
421068
 YDOT =       1415
452204  feet/sec       YDOT =         431
429832  meter/sec
 ZDOT =     -19412
316410                 ZDOT =       -5916
874042


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   19360
43675898  
00016717  00000-0  10270-3 0  9129
2 25544  51
6389 128
2405 0007611  75
0420 285
1573 15
50159779  5071


Satellite: ISS
Catalog Number: 25544
Epoch time:      19360
43675898   =   yrday
fracday
Element set:     912
Inclination:       51
6389  deg
RA of node:       128
2405  deg
Eccentricity:     
0007611     
Arg of perigee:    75
0420  deg
Mean anomaly:     285
1573  deg
Mean motion:   15
50159779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              324


Coasting Arc #14 (Orbit 516)
---------------------------------------

Vector Time (GMT): 2019/361/01:37:54
517
Vector Time (MET): N/A
Weight (LBS)     : 986864
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2348219
37                 A    =         6790857
11  meter
 Y    =        3751279
96  meter          E    =           
0019287
 Z    =       -5167551
30                 I    =           51
94359
 XDOT =      -5159
737435                 Wp   =           93
19124
 YDOT =       5415
112626  meter/sec      RA   =          124
03451  deg
 ZDOT =       1590
401914                 TA   =          192
10095
                                          MA   =          192
14735
                                          Ha   =            230
099  n
mi
                                          Hp   =            219
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7704131
78                 X    =         2331197
77
 Y    =       12307348
96  feet           Y    =         3777445
04  meter
 Z    =      -16953908
47                 Z    =        -5156185
40
 XDOT =     -16928
272425                 XDOT =       -5227
632534
 YDOT =      17766
117539  feet/sec       YDOT =        5357
032921  meter/sec
 ZDOT =       5217
854047                 ZDOT =        1565
174035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7008276
59                 X    =         2136122
71
 Y    =      -12785180
73  feet           Y    =        -3896923
09  meter
 Z    =      -16902151
06                 Z    =        -5151775
64
 XDOT =      22813
118298                 XDOT =        6953
438457
 YDOT =       5777
882397  feet/sec       YDOT =        1761
098555  meter/sec
 ZDOT =       5102
085843                 ZDOT =        1555
115765


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   19361
08144647  
00016717  00000-0  10270-3 0  9135
2 25544  51
6420 125
0504 0006230  73
3223 286
8611 15
49777852  5178


Satellite: ISS
Catalog Number: 25544
Epoch time:      19361
08144647   =   yrday
fracday
Element set:     913
Inclination:       51
6420  deg
RA of node:       125
0504  deg
Eccentricity:     
0006230     
Arg of perigee:    73
3223  deg
Mean anomaly:     286
8611  deg
Mean motion:   15
49777852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             517
Checksum:              297


Coasting Arc #15 (Orbit 518)
---------------------------------------

Vector Time (GMT): 2019/361/04:44:50
721
Vector Time (MET): N/A
Weight (LBS)     : 986693
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2006062
59                 A    =         6792251
94  meter
 Y    =        4114587
64  meter          E    =           
0016889
 Z    =       -5033027
00                 I    =           51
94912
 XDOT =      -5304
053278                 Wp   =           95
27918
 YDOT =       5107
944278  meter/sec      RA   =          123
39204  deg
 ZDOT =       2066
201297                 TA   =          194
76046
                                          MA   =          194
80983
                                          Ha   =            230
045  n
mi
                                          Hp   =            220
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6581570
19                 X    =         1984350
36
 Y    =       13499303
28  feet           Y    =         4136900
23  meter
 Z    =      -16512555
78                 Z    =        -5023334
50
 XDOT =     -17401
749600                 XDOT =       -5370
813945
 YDOT =      16758
347370  feet/sec       YDOT =        5048
257003  meter/sec
 ZDOT =       6778
875645                 ZDOT =        2040
275111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3152510
08                 X    =         -960885
07
 Y    =      -14733081
05  feet           Y    =        -4490643
10  meter
 Z    =      -16468477
67                 Z    =        -5019591
99
 XDOT =      19971
029367                 XDOT =        6087
169751
 YDOT =     -11701
312392  feet/sec       YDOT =       -3566
560017  meter/sec
 ZDOT =       6659
929329                 ZDOT =        2029
946459


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   19361
21041083  
00016717  00000-0  10270-3 0  9141
2 25544  51
6431 124
4127 0004909  68
3107 291
8565 15
49492758  5195


Satellite: ISS
Catalog Number: 25544
Epoch time:      19361
21041083   =   yrday
fracday
Element set:     914
Inclination:       51
6431  deg
RA of node:       124
4127  deg
Eccentricity:     
0004909     
Arg of perigee:    68
3107  deg
Mean anomaly:     291
8565  deg
Mean motion:   15
49492758  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             519
Checksum:              310


Coasting Arc #16 (Orbit 534)
---------------------------------------

Vector Time (GMT): 2019/362/04:44:50
721
Vector Time (MET): N/A
Weight (LBS)     : 986693
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2200141
05                 A    =         6792436
83  meter
 Y    =       -4079459
07  meter          E    =           
0011251
 Z    =        4958367
85                 I    =           51
96743
 XDOT =       4939
134604                 Wp   =           63
71410
 YDOT =      -5412
933704  meter/sec      RA   =          118
46322  deg
 ZDOT =      -2253
042012                 TA   =           48
24210
                                          MA   =           48
14598
                                          Ha   =            230
081  n
mi
                                          Hp   =            220
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7218310
53                 X    =        -2178444
47
 Y    =      -13384052
08  feet           Y    =        -4103942
00  meter
 Z    =       16267611
04                 Z    =         4947732
66
 XDOT =      16204
509857                 XDOT =        5010
240389
 YDOT =     -17758
968846  feet/sec       YDOT =       -5357
302912  meter/sec
 ZDOT =      -7391
870117                 ZDOT =       -2228
877965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4050017
63                 X    =         1234445
38
 Y    =       14710757
32  feet           Y    =         4483838
83  meter
 Z    =       16219217
07                 Z    =         4943617
36
 XDOT =     -18833
696489                 XDOT =       -5740
510690
 YDOT =      13244
574974  feet/sec       YDOT =        4036
946452  meter/sec
 ZDOT =      -7280
944141                 ZDOT =       -2219
231774


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   19362
24233354  
00016717  00000-0  10270-3 0  9150
2 25544  51
6431 119
3047 0004877  71
0179 289
1499 15
49518344  5357


Satellite: ISS
Catalog Number: 25544
Epoch time:      19362
24233354   =   yrday
fracday
Element set:     915
Inclination:       51
6431  deg
RA of node:       119
3047  deg
Eccentricity:     
0004877     
Arg of perigee:    71
0179  deg
Mean anomaly:     289
1499  deg
Mean motion:   15
49518344  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             535
Checksum:              321


Coasting Arc #17 (Orbit 535)
---------------------------------------

Vector Time (GMT): 2019/362/07:16:34
000
Vector Time (MET): N/A
Weight (LBS)     : 956693
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1716273
23                 A    =         6801431
94  meter
 Y    =        6314654
83  meter          E    =           
0011550
 Z    =       -1846275
91                 I    =           51
99506
 XDOT =      -5144
808470                 Wp   =           53
44067
 YDOT =        249
402277  meter/sec      RA   =          117
94212  deg
 ZDOT =       5666
791632                 TA   =          286
40097
                                          MA   =          286
52791
                                          Ha   =            230
098  n
mi
                                          Hp   =            220
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5630817
69                 X    =        -1777789
94
 Y    =       20717371
48  feet           Y    =         6295118
55  meter
 Z    =       -6057335
66                 Z    =        -1854761
32
 XDOT =     -16879
292882                 XDOT =       -5174
740697
 YDOT =        818
248940  feet/sec       YDOT =         191
701235  meter/sec
 ZDOT =      18591
836062                 ZDOT =        5641
727789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3587119
12                 X    =        -1093353
91
 Y    =      -21155878
03  feet           Y    =        -6448311
62  meter
 Z    =       -6096581
46                 Z    =        -1858238
03
 XDOT =      13560
684482                 XDOT =        4133
296630
 YDOT =      -7594
595290  feet/sec       YDOT =       -2314
832644  meter/sec
 ZDOT =      18477
132684                 ZDOT =        5631
830042


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   19362
30682995  
00016717  00000-0  10270-3 0  9167
2 25544  51
6394 118
9825 0004921  74
2023 285
9670 15
49473916  5368


Satellite: ISS
Catalog Number: 25544
Epoch time:      19362
30682995   =   yrday
fracday
Element set:     916
Inclination:       51
6394  deg
RA of node:       118
9825  deg
Eccentricity:     
0004921     
Arg of perigee:    74
2023  deg
Mean anomaly:     285
9670  deg
Mean motion:   15
49473916  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             536
Checksum:              339


Coasting Arc #18 (Orbit 539)
---------------------------------------

Vector Time (GMT): 2019/362/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956693
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3745810
46                 A    =         6790929
66  meter
 Y    =        1882306
30  meter          E    =           
0019626
 Z    =       -5359434
21                 I    =           51
96746
 XDOT =      -3438
785742                 Wp   =           87
21754
 YDOT =       6829
428822  meter/sec      RA   =          116
74943  deg
 ZDOT =         -3
931879                 TA   =          182
73967
                                          MA   =          182
75044
                                          Ha   =            230
086  n
mi
                                          Hp   =            220
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12289404
40                 X    =         3750516
31
 Y    =        6175545
59  feet           Y    =         1924221
64  meter
 Z    =      -17583445
57                 Z    =        -5341227
06
 XDOT =     -11282
105452                 XDOT =       -3514
879735
 YDOT =      22406
262541  feet/sec       YDOT =        6790
548421  meter/sec
 ZDOT =        -12
899867                 ZDOT =         -20
819838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -757352
48                 X    =         -230841
04
 Y    =       13838779
54  feet           Y    =         4218060
00  meter
 Z    =      -17500256
56                 Z    =        -5334078
20
 XDOT =     -24032
858568                 XDOT =       -7325
215292
 YDOT =      -1433
657616  feet/sec       YDOT =        -436
978841  meter/sec
 ZDOT =        -90
632391                 ZDOT =         -27
624753


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   19362
56481166  
00016717  00000-0  10270-3 0  9173
2 25544  51
6431 117
7054 0004863  78
5130 281
6566 15
49480354  5408


Satellite: ISS
Catalog Number: 25544
Epoch time:      19362
56481166   =   yrday
fracday
Element set:     917
Inclination:       51
6431  deg
RA of node:       117
7054  deg
Eccentricity:     
0004863     
Arg of perigee:    78
5130  deg
Mean anomaly:     281
6566  deg
Mean motion:   15
49480354  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             540
Checksum:              315


Coasting Arc #19 (Orbit 555)
---------------------------------------

Vector Time (GMT): 2019/363/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956693
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3801627
74                 A    =         6790814
91  meter
 Y    =       -1744376
53  meter          E    =           
0007225
 Z    =        5343611
26                 I    =           51
98167
 XDOT =       2981
340417                 Wp   =           82
58319
 YDOT =      -7061
089362  meter/sec      RA   =          111
82161  deg
 ZDOT =       -182
886354                 TA   =            9
15852
                                          MA   =            9
14535
                                          Ha   =            230
159  n
mi
                                          Hp   =            220
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12472531
94                 X    =        -3807794
90
 Y    =       -5723020
12  feet           Y    =        -1786924
13  meter
 Z    =       17531533
01                 Z    =         5325129
52
 XDOT =       9781
300581                 XDOT =        3060
966348
 YDOT =     -23166
303682  feet/sec       YDOT =       -7027
304668  meter/sec
 ZDOT =       -600
020847                 ZDOT =        -168
211801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          31555
17                 X    =            9618
02
 Y    =      -13830052
57  feet           Y    =        -4215400
02  meter
 Z    =       17447071
74                 Z    =         5317867
47
 XDOT =      24132
001902                 XDOT =        7355
434180
 YDOT =       -621
214303  feet/sec       YDOT =        -189
346120  meter/sec
 ZDOT =       -532
385221                 ZDOT =        -162
271015


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   19363
59673552  
00016717  00000-0  10270-3 0  9180
2 25544  51
6432 112
5972 0004775  82
5947 277
5746 15
49515571  5565


Satellite: ISS
Catalog Number: 25544
Epoch time:      19363
59673552   =   yrday
fracday
Element set:     918
Inclination:       51
6432  deg
RA of node:       112
5972  deg
Eccentricity:     
0004775     
Arg of perigee:    82
5947  deg
Mean anomaly:     277
5746  deg
Mean motion:   15
49515571  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             556
Checksum:              349


Coasting Arc #20 (Orbit 570)
---------------------------------------

Vector Time (GMT): 2019/364/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956693
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3881356
32                 A    =         6790984
23  meter
 Y    =        1610957
96  meter          E    =           
0019528
 Z    =       -5351399
25                 I    =           51
99309
 XDOT =      -2492
223109                 Wp   =           90
96292
 YDOT =       7219
518269  meter/sec      RA   =          106
89552  deg
 ZDOT =        366
560378                 TA   =          182
52026
                                          MA   =          182
53011
                                          Ha   =            230
082  n
mi
                                          Hp   =            220
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12734108
67                 X    =         3889047
31
 Y    =        5285295
15  feet           Y    =         1654405
55  meter
 Z    =      -17557084
14                 Z    =        -5332526
57
 XDOT =      -8176
585002                 XDOT =       -2574
549160
 YDOT =      23686
083560  feet/sec       YDOT =        7191
188118  meter/sec
 ZDOT =       1202
625912                 ZDOT =         354
255054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         713937
67                 X    =          217608
20
 Y    =       13878177
93  feet           Y    =         4230068
63  meter
 Z    =      -17470819
73                 Z    =        -5325105
85
 XDOT =     -23900
219725                 XDOT =       -7284
786972
 YDOT =       2668
454435  feet/sec       YDOT =         813
344912  meter/sec
 ZDOT =       1145
807820                 ZDOT =         349
242223


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   19364
56416563  
00016717  00000-0  10270-3 0  9196
2 25544  51
6431 107
8093 0004790  85
0216 275
1481 15
49475334  5718


Satellite: ISS
Catalog Number: 25544
Epoch time:      19364
56416563   =   yrday
fracday
Element set:     919
Inclination:       51
6431  deg
RA of node:       107
8093  deg
Eccentricity:     
0004790     
Arg of perigee:    85
0216  deg
Mean anomaly:     275
1481  deg
Mean motion:   15
49475334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             571
Checksum:              318
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list