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

 
Date: December 27th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


362/01:03:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 5

364/11:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 3

Coasting Arc #1 (Orbit 1149)
---------------------------------------

Vector Time (GMT): 2017/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5440335
40                 A    =         6783117
47  meter
 Y    =        1488395
07  meter          E    =           
0003740
 Z    =       -3772523
07                 I    =           51
73937
 XDOT =      -4247
253081                 Wp   =           55
83719
 YDOT =       4756
583101  meter/sec      RA   =          163
46520  deg
 ZDOT =      -4249
261983                 TA   =          169
23898
                                          MA   =          169
23098
                                          Ha   =            219
942  n
mi
                                          Hp   =            215
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17848869
42                 X    =         5441612
38
 Y    =        4883185
91  feet           Y    =         1549239
95  meter
 Z    =      -12377044
20                 Z    =        -3746092
60
 XDOT =     -13934
557354                 XDOT =       -4279
486112
 YDOT =      15605
587601  feet/sec       YDOT =        4708
907397  meter/sec
 ZDOT =     -13941
148237                 ZDOT =       -4269
971742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3835130
43                 X    =        -1168947
75
 Y    =       18182681
65  feet           Y    =         5542081
37  meter
 Z    =      -12259719
82                 Z    =        -3736762
60
 XDOT =     -15054
276221                 XDOT =       -4588
543392
 YDOT =     -12635
512304  feet/sec       YDOT =       -3851
304150  meter/sec
 ZDOT =     -14033
883830                 ZDOT =       -4277
527791


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   17359
52420138  
00016717  00000-0  10270-3 0  9007
2 25544  51
6374 164
4767 0002775 289
5398  70
5454 15
54229921 11500


Satellite: ISS
Catalog Number: 25544
Epoch time:      17359
52420138   =   yrday
fracday
Element set:     900
Inclination:       51
6374  deg
RA of node:       164
4767  deg
Eccentricity:     
0002775     
Arg of perigee:   289
5398  deg
Mean anomaly:      70
5454  deg
Mean motion:   15
54229921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1150
Checksum:              321


Coasting Arc #2 (Orbit 1165)
---------------------------------------

Vector Time (GMT): 2017/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4157405
08                 A    =         6779463
31  meter
 Y    =       -2410103
04  meter          E    =           
0004829
 Z    =        4779706
24                 I    =           51
75720
 XDOT =       5642
007673                 Wp   =          122
82110
 YDOT =      -4469
086425  meter/sec      RA   =          158
48182  deg
 ZDOT =       2649
462697                 TA   =          301
06183
                                          MA   =          301
10922
                                          Ha   =            220
047  n
mi
                                          Hp   =            215
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13639780
45                 X    =        -4153363
06
 Y    =       -7907162
22  feet           Y    =        -2456571
61  meter
 Z    =       15681450
93                 Z    =         4759520
64
 XDOT =      18510
523861                 XDOT =        5678
693131
 YDOT =     -14662
357039  feet/sec       YDOT =       -4405
788635  meter/sec
 ZDOT =       8692
462917                 ZDOT =        2676
958622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6851418
35                 X    =         2088312
31
 Y    =      -14297621
50  feet           Y    =        -4357915
03  meter
 Z    =       15592011
24                 Z    =         4752445
03
 XDOT =      14963
437434                 XDOT =        4560
855730
 YDOT =      16800
083405  feet/sec       YDOT =        5120
665422  meter/sec
 ZDOT =       8815
350783                 ZDOT =        2686
918919


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   17360
55297841  
00016717  00000-0  10270-3 0  9016
2 25544  51
6363 159
3468 0002849 290
5676  69
5171 15
54224358 11662


Satellite: ISS
Catalog Number: 25544
Epoch time:      17360
55297841   =   yrday
fracday
Element set:     901
Inclination:       51
6363  deg
RA of node:       159
3468  deg
Eccentricity:     
0002849     
Arg of perigee:   290
5676  deg
Mean anomaly:      69
5171  deg
Mean motion:   15
54224358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1166
Checksum:              332


Coasting Arc #3 (Orbit 1180)
---------------------------------------

Vector Time (GMT): 2017/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2621756
80                 A    =         6777277
65  meter
 Y    =        3346437
68  meter          E    =           
0012299
 Z    =       -5288843
88                 I    =           51
78097
 XDOT =      -6534
744758                 Wp   =           77
85573
 YDOT =       3923
841002  meter/sec      RA   =          153
49393  deg
 ZDOT =       -755
576692                 TA   =          184
92532
                                          MA   =          184
93743
                                          Ha   =            220
013  n
mi
                                          Hp   =            215
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8601564
32                 X    =         2609831
77
 Y    =       10979126
24  feet           Y    =         3375689
54  meter
 Z    =      -17351850
00                 Z    =        -5276137
01
 XDOT =     -21439
451307                 XDOT =       -6574
466310
 YDOT =      12873
494101  feet/sec       YDOT =        3850
542955  meter/sec
 ZDOT =      -2478
926155                 ZDOT =        -787
416716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10126903
60                 X    =        -3086680
22
 Y    =        9691035
62  feet           Y    =         2953827
66  meter
 Z    =      -17295793
48                 Z    =        -5271757
85
 XDOT =     -14087
791502                 XDOT =       -4293
958850
 YDOT =     -19405
405035  feet/sec       YDOT =       -5914
767455  meter/sec
 ZDOT =      -2621
077625                 ZDOT =        -798
904460


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   17361
51745567  
00016717  00000-0  10270-3 0  9027
2 25544  51
6371 154
5395 0002696 294
4564  65
6307 15
54228444 11811


Satellite: ISS
Catalog Number: 25544
Epoch time:      17361
51745567   =   yrday
fracday
Element set:     902
Inclination:       51
6371  deg
RA of node:       154
5395  deg
Eccentricity:     
0002696     
Arg of perigee:   294
4564  deg
Mean anomaly:      65
6307  deg
Mean motion:   15
54228444  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1181
Checksum:              322


Coasting Arc #4 (Orbit 1189)
---------------------------------------

Vector Time (GMT): 2017/362/01:03:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4019730
50                 A    =         6778564
49  meter
 Y    =       -2238983
54  meter          E    =           
0003213
 Z    =        4976028
41                 I    =           51
80204
 XDOT =       5431
200615                 Wp   =          124
44762
 YDOT =      -4971
268821  meter/sec      RA   =          150
80145  deg
 ZDOT =       2147
825245                 TA   =          304
66169
                                          MA   =          304
69197
                                          Ha   =            220
086  n
mi
                                          Hp   =            215
455

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13188092
20                 X    =        -4018565
95
 Y    =       -7345746
53  feet           Y    =        -2283928
68  meter
 Z    =       16325552
54                 Z    =         4956504
50
 XDOT =      17818
899657                 XDOT =        5475
953936
 YDOT =     -16309
937078  feet/sec       YDOT =       -4910
283307  meter/sec
 ZDOT =       7046
670752                 ZDOT =        2174
316775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1906980
57                 X    =         -581247
68
 Y    =       15068745
01  feet           Y    =         4592953
48  meter
 Z    =       16239020
37                 Z    =         4949653
41
 XDOT =     -20626
601829                 XDOT =       -6286
988237
 YDOT =     -10341
803439  feet/sec       YDOT =       -3152
181688  meter/sec
 ZDOT =       7165
188111                 ZDOT =        2183
949336


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   17362
09613891  
00016717  00000-0  10270-3 0  9036
2 25544  51
6378 151
6575 0003152 301
0836  59
0007 15
54253584 11908


Satellite: ISS
Catalog Number: 25544
Epoch time:      17362
09613891   =   yrday
fracday
Element set:     903
Inclination:       51
6378  deg
RA of node:       151
6575  deg
Eccentricity:     
0003152     
Arg of perigee:   301
0836  deg
Mean anomaly:      59
0007  deg
Mean motion:   15
54253584  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1190
Checksum:              298


Coasting Arc #5 (Orbit 1204)
---------------------------------------

Vector Time (GMT): 2017/363/01:03:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2550490
28                 A    =         6777113
84  meter
 Y    =        3334389
87  meter          E    =           
0012596
 Z    =       -5331093
02                 I    =           51
82531
 XDOT =      -6240
180610                 Wp   =           79
30156
 YDOT =       4436
904022  meter/sec      RA   =          145
81276  deg
 ZDOT =       -208
443803                 TA   =          188
70370
                                          MA   =          188
72556
                                          Ha   =            220
158  n
mi
                                          Hp   =            215
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8367750
28                 X    =         2538910
57
 Y    =       10939599
32  feet           Y    =         3362846
83  meter
 Z    =      -17490462
67                 Z    =        -5318731
39
 XDOT =     -20473
033498                 XDOT =       -6288
318961
 YDOT =      14556
771725  feet/sec       YDOT =        4366
852910  meter/sec
 ZDOT =       -683
870745                 ZDOT =        -238
873333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6819506
38                 X    =         2078585
55
 Y    =      -12045446
97  feet           Y    =        -3671452
24  meter
 Z    =      -17435937
10                 Z    =        -5314473
63
 XDOT =      20447
077866                 XDOT =        6232
269334
 YDOT =      12771
684626  feet/sec       YDOT =        3892
809474  meter/sec
 ZDOT =       -819
853037                 ZDOT =        -249
891206


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   17363
06061173  
00016717  00000-0  10270-3 0  9045
2 25544  51
6381 146
8478 0003132 307
8657  52
2212 15
54219045 12057


Satellite: ISS
Catalog Number: 25544
Epoch time:      17363
06061173   =   yrday
fracday
Element set:     904
Inclination:       51
6381  deg
RA of node:       146
8478  deg
Eccentricity:     
0003132     
Arg of perigee:   307
8657  deg
Mean anomaly:      52
2212  deg
Mean motion:   15
54219045  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1205
Checksum:              286


Coasting Arc #6 (Orbit 1220)
---------------------------------------

Vector Time (GMT): 2017/364/01:03:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -993895
80                 A    =         6778055
94  meter
 Y    =       -4354578
98  meter          E    =           
0005511
 Z    =        5097806
20                 I    =           51
85503
 XDOT =       6559
420453                 Wp   =           21
74434
 YDOT =      -3562
763811  meter/sec      RA   =          140
82684  deg
 ZDOT =      -1758
876332                 TA   =           85
24251
                                          MA   =           85
17958
                                          Ha   =            220
281  n
mi
                                          Hp   =            215
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3260812
99                 X    =         -969890
54
 Y    =      -14286676
44  feet           Y    =        -4365559
66  meter
 Z    =       16725085
95                 Z    =         5093036
05
 XDOT =      21520
408309                 XDOT =        6607
316497
 YDOT =     -11688
857646  feet/sec       YDOT =       -3489
143917  meter/sec
 ZDOT =      -5770
591639                 ZDOT =       -1726
896645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11729400
36                 X    =        -3575121
23
 Y    =        8823384
72  feet           Y    =         2689367
66  meter
 Z    =       16704477
67                 Z    =         5091524
79
 XDOT =     -18718
710232                 XDOT =       -5705
462879
 YDOT =     -14194
365996  feet/sec       YDOT =       -4326
442756  meter/sec
 ZDOT =      -5627
810544                 ZDOT =       -1715
356654


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   17364
08937929  
00016717  00000-0  10270-3 0  9050
2 25544  51
6379 141
7192 0003129 313
6164  46
4729 15
54221406 12215


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
08937929   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:       141
7192  deg
Eccentricity:     
0003129     
Arg of perigee:   313
6164  deg
Mean anomaly:      46
4729  deg
Mean motion:   15
54221406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1221
Checksum:              309


Coasting Arc #7 (Orbit 1227)
---------------------------------------

Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3513099
18                 A    =         6777334
39  meter
 Y    =       -2416651
40  meter          E    =           
0000729
 Z    =        5267244
61                 I    =           51
86357
 XDOT =       5207
692274                 Wp   =          100
39697
 YDOT =      -5553
943097  meter/sec      RA   =          138
63054  deg
 ZDOT =        924
951822                 TA   =          340
78170
                                          MA   =          340
78445
                                          Ha   =            220
260  n
mi
                                          Hp   =            215
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11525915
94                 X    =        -3511400
14
 Y    =       -7928646
34  feet           Y    =        -2455928
33  meter
 Z    =       17280986
25                 Z    =         5250182
92
 XDOT =      17085
604575                 XDOT =        5264
917948
 YDOT =     -18221
598086  feet/sec       YDOT =       -5495
387247  meter/sec
 ZDOT =       3034
618839                 ZDOT =         950
387614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6991823
63                 X    =         2131107
84
 Y    =      -12224185
15  feet           Y    =        -3725931
63  meter
 Z    =       17205416
49                 Z    =         5244210
95
 XDOT =      18609
748485                 XDOT =        5672
251338
 YDOT =      15076
842157  feet/sec       YDOT =        4595
421489  meter/sec
 ZDOT =       3148
578362                 ZDOT =         959
686685


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   17364
53946392  
00016717  00000-0  10270-3 0  9065
2 25544  51
6375 139
4706 0002864 307
1921  52
8970 15
54237784 12282


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
53946392   =   yrday
fracday
Element set:     906
Inclination:       51
6375  deg
RA of node:       139
4706  deg
Eccentricity:     
0002864     
Arg of perigee:   307
1921  deg
Mean anomaly:      52
8970  deg
Mean motion:   15
54237784  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1228
Checksum:              331


Coasting Arc #8 (Orbit 1242)
---------------------------------------

Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925079
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2164560
03                 A    =         6777343
00  meter
 Y    =        3704715
65  meter          E    =           
0012096
 Z    =       -5256603
52                 I    =           51
88905
 XDOT =      -5804
207223                 Wp   =           90
82119
 YDOT =       4885
800783  meter/sec      RA   =          133
64670  deg
 ZDOT =       1055
257013                 TA   =          189
25160
                                          MA   =          189
27391
                                          Ha   =            220
218  n
mi
                                          Hp   =            215
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7101574
90                 X    =         2148505
94
 Y    =       12154578
92  feet           Y    =         3728832
13  meter
 Z    =      -17246074
53                 Z    =        -5246127
33
 XDOT =     -19042
674616                 XDOT =       -5863
536084
 YDOT =      16029
530129  feet/sec       YDOT =        4820
562312  meter/sec
 ZDOT =       3462
129309                 ZDOT =        1026
918565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11409301
78                 X    =        -3477555
18
 Y    =        8341551
53  feet           Y    =         2542504
91  meter
 Z    =      -17199988
15                 Z    =        -5242556
39
 XDOT =     -17167
381561                 XDOT =       -5232
617900
 YDOT =     -16616
724591  feet/sec       YDOT =       -5064
777655  meter/sec
 ZDOT =       3335
322290                 ZDOT =        1016
606234


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   17365
50392964  
00016717  00000-0  10270-3 0  9074
2 25544  51
6389 134
6628 0002806 311
2416  48
8495 15
54250141 12434


Satellite: ISS
Catalog Number: 25544
Epoch time:      17365
50392964   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:       134
6628  deg
Eccentricity:     
0002806     
Arg of perigee:   311
2416  deg
Mean anomaly:      48
8495  deg
Mean motion:   15
54250141  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1243
Checksum:              312
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