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

 
Date: December 28th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 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 4

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 1180)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2620792
91                 A    =         6777268
97  meter
 Y    =        3347019
01  meter          E    =           
0012309
 Z    =       -5288948
73                 I    =           51
78090
 XDOT =      -6535
238933                 Wp   =           77
68300
 YDOT =       3923
216364  meter/sec      RA   =          153
49367  deg
 ZDOT =       -754
540346                 TA   =          185
10775
                                          MA   =          185
12032
                                          Ha   =            220
014  n
mi
                                          Hp   =            215
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8598401
94                 X    =         2608861
96
 Y    =       10981033
51  feet           Y    =         3376260
06  meter
 Z    =      -17352194
01                 Z    =        -5276246
56
 XDOT =     -21441
072614                 XDOT =       -6574
958497
 YDOT =      12871
444765  feet/sec       YDOT =        3849
912803  meter/sec
 ZDOT =      -2475
526071                 ZDOT =        -786
382766

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10129094
20                 X    =        -3087347
91
 Y    =        9688064
98  feet           Y    =         2952922
21  meter
 Z    =      -17296158
46                 Z    =        -5271869
10
 XDOT =     -14086
119428                 XDOT =       -4293
449202
 YDOT =     -19407
070947  feet/sec       YDOT =       -5915
275225  meter/sec
 ZDOT =      -2617
688112                 ZDOT =        -797
871336


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
51745382  
00016717  00000-0  10270-3 0  9000
2 25544  51
6371 154
5393 0002711 295
2432  64
8439 15
54231253 11819


Satellite: ISS
Catalog Number: 25544
Epoch time:      17361
51745382   =   yrday
fracday
Element set:     900
Inclination:       51
6371  deg
RA of node:       154
5393  deg
Eccentricity:     
0002711     
Arg of perigee:   295
2432  deg
Mean anomaly:      64
8439  deg
Mean motion:   15
54231253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1181
Checksum:              293


Coasting Arc #2 (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    =       -4018360
82                 A    =         6778553
36  meter
 Y    =       -2240218
83  meter          E    =           
0003189
 Z    =        4976550
12                 I    =           51
80196
 XDOT =       5432
468528                 Wp   =          123
84096
 YDOT =      -4970
594865  meter/sec      RA   =          150
80117  deg
 ZDOT =       2146
240175                 TA   =          305
28472
                                          MA   =          305
31454
                                          Ha   =            220
089  n
mi
                                          Hp   =            215
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13183598
49                 X    =        -4017185
09
 Y    =       -7349799
30  feet           Y    =        -2285148
59  meter
 Z    =       16327264
18                 Z    =         4957032
89
 XDOT =      17823
059474                 XDOT =        5477
221917
 YDOT =     -16307
725934  feet/sec       YDOT =       -4909
595171  meter/sec
 ZDOT =       7041
470390                 ZDOT =        2172
737864

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1912403
51                 X    =         -582900
59
 Y    =       15066079
12  feet           Y    =         4592140
92  meter
 Z    =       16240761
89                 Z    =         4950184
23
 XDOT =     -20626
293214                 XDOT =       -6286
894172
 YDOT =     -10346
122168  feet/sec       YDOT =       -3153
498037  meter/sec
 ZDOT =       7160
015054                 ZDOT =        2182
372588


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
09613597  
00016717  00000-0  10270-3 0  9017
2 25544  51
6377 151
6573 0003170 301
7383  58
3460 15
54256613 11900


Satellite: ISS
Catalog Number: 25544
Epoch time:      17362
09613597   =   yrday
fracday
Element set:     901
Inclination:       51
6377  deg
RA of node:       151
6573  deg
Eccentricity:     
0003170     
Arg of perigee:   301
7383  deg
Mean anomaly:      58
3460  deg
Mean motion:   15
54256613  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1190
Checksum:              301


Coasting Arc #3 (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    =        2547882
51                 A    =         6777103
24  meter
 Y    =        3336246
99  meter          E    =           
0012608
 Z    =       -5331170
31                 I    =           51
82523
 XDOT =      -6241
535222                 Wp   =           79
14992
 YDOT =       4435
134533  meter/sec      RA   =          145
81243  deg
 ZDOT =       -205
557632                 TA   =          188
88259
                                          MA   =          188
90492
                                          Ha   =            220
163  n
mi
                                          Hp   =            215
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8359194
58                 X    =         2536282
59
 Y    =       10945692
24  feet           Y    =         3364674
68  meter
 Z    =      -17490716
25                 Z    =        -5318821
40
 XDOT =     -20477
477763                 XDOT =       -6289
667705
 YDOT =      14550
966317  feet/sec       YDOT =        4365
068306  meter/sec
 ZDOT =       -674
401680                 ZDOT =        -235
993728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6828427
27                 X    =         2081304
63
 Y    =      -12039905
37  feet           Y    =        -3669763
16  meter
 Z    =      -17436247
51                 Z    =        -5314568
24
 XDOT =      20443
864912                 XDOT =        6231
290025
 YDOT =      12777
430890  feet/sec       YDOT =        3894
560935  meter/sec
 ZDOT =       -810
412936                 ZDOT =        -247
013863


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
06060676  
00016717  00000-0  10270-3 0  9020
2 25544  51
6380 146
8476 0003154 308
5111  51
5759 15
54222536 12058


Satellite: ISS
Catalog Number: 25544
Epoch time:      17363
06060676   =   yrday
fracday
Element set:     902
Inclination:       51
6380  deg
RA of node:       146
8476  deg
Eccentricity:     
0003154     
Arg of perigee:   308
5111  deg
Mean anomaly:      51
5759  deg
Mean motion:   15
54222536  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1205
Checksum:              292


Coasting Arc #4 (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    =        -989710
27                 A    =         6778049
31  meter
 Y    =       -4356859
65  meter          E    =           
0005560
 Z    =        5096663
90                 I    =           51
85497
 XDOT =       6560
214123                 Wp   =           21
73215
 YDOT =      -3559
247995  meter/sec      RA   =          140
82646  deg
 ZDOT =      -1763
042078                 TA   =           85
29636
                                          MA   =           85
23287
                                          Ha   =            220
285  n
mi
                                          Hp   =            215
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3247080
95                 X    =         -965674
27
 Y    =      -14294158
96  feet           Y    =        -4367793
35  meter
 Z    =       16721338
26                 Z    =         5091914
16
 XDOT =      21523
012215                 XDOT =        6608
091029
 YDOT =     -11677
322818  feet/sec       YDOT =       -3485
619333  meter/sec
 ZDOT =      -5784
258785                 ZDOT =       -1731
058582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11741777
31                 X    =        -3578893
72
 Y    =        8813790
82  feet           Y    =         2686443
44  meter
 Z    =       16700821
09                 Z    =         5090410
27
 XDOT =     -18709
928577                 XDOT =       -5702
786230
 YDOT =     -14200
561897  feet/sec       YDOT =       -4328
331266  meter/sec
 ZDOT =      -5641
461238                 ZDOT =       -1719
517385


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
08937185  
00016717  00000-0  10270-3 0  9032
2 25544  51
6379 141
7189 0003151 314
2536  45
8358 15
54225335 12212


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
08937185   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:       141
7189  deg
Eccentricity:     
0003151     
Arg of perigee:   314
2536  deg
Mean anomaly:      45
8358  deg
Mean motion:   15
54225335  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1221
Checksum:              308


Coasting Arc #5 (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    =       -3509241
90                 A    =         6777319
56  meter
 Y    =       -2420747
51  meter          E    =           
0000726
 Z    =        5267905
86                 I    =           51
86349
 XDOT =       5210
983605                 Wp   =           96
46855
 YDOT =      -5551
706188  meter/sec      RA   =          138
63014  deg
 ZDOT =        919
973097                 TA   =          344
75825
                                          MA   =          344
76044
                                          Ha   =            220
264  n
mi
                                          Hp   =            215
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11513260
82                 X    =        -3507500
55
 Y    =       -7942085
01  feet           Y    =        -2459981
06  meter
 Z    =       17283155
69                 Z    =         5250863
01
 XDOT =      17096
402904                 XDOT =        5268
208205
 YDOT =     -18214
259148  feet/sec       YDOT =       -5493
113539  meter/sec
 ZDOT =       3018
284439                 ZDOT =         945
424875

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7006210
27                 X    =         2135492
89
 Y    =      -12212635
21  feet           Y    =        -3722411
21  meter
 Z    =       17207670
34                 Z    =         5244897
92
 XDOT =      18604
129280                 XDOT =        5670
538605
 YDOT =      15087
239549  feet/sec       YDOT =        4598
590615  meter/sec
 ZDOT =       3132
314772                 ZDOT =         954
729543


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
53945531  
00016717  00000-0  10270-3 0  9047
2 25544  51
6375 139
4704 0002882 307
9591  52
1301 15
54241796 12280


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
53945531   =   yrday
fracday
Element set:     904
Inclination:       51
6375  deg
RA of node:       139
4704  deg
Eccentricity:     
0002882     
Arg of perigee:   307
9591  deg
Mean anomaly:      52
1301  deg
Mean motion:   15
54241796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1228
Checksum:              311


Coasting Arc #6 (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    =        2158956
49                 A    =         6777334
18  meter
 Y    =        3709435
66  meter          E    =           
0012099
 Z    =       -5255564
24                 I    =           51
88899
 XDOT =      -5806
858133                 Wp   =           90
68068
 YDOT =       4881
247777  meter/sec      RA   =          133
64625  deg
 ZDOT =       1061
781980                 TA   =          189
45488
                                          MA   =          189
47768
                                          Ha   =            220
222  n
mi
                                          Hp   =            215
287

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7083190
60                 X    =         2142844
99
 Y    =       12170064
49  feet           Y    =         3733489
15  meter
 Z    =      -17242664
83                 Z    =        -5245115
41
 XDOT =     -19051
371827                 XDOT =       -5866
167579
 YDOT =      16014
592443  feet/sec       YDOT =        4815
979768  meter/sec
 ZDOT =       3483
536680                 ZDOT =        1033
430701

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11426473
12                 X    =        -3482789
01
 Y    =        8324706
62  feet           Y    =         2537370
58  meter
 Z    =      -17196700
87                 Z    =        -5241554
43
 XDOT =     -17154
585399                 XDOT =       -5228
717630
 YDOT =     -16625
695080  feet/sec       YDOT =       -5067
511860  meter/sec
 ZDOT =       3356
673218                 ZDOT =        1023
113997


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
50391832  
00016717  00000-0  10270-3 0  9055
2 25544  51
6388 134
6625 0002824 312
0208  48
0704 15
54254678 12432


Satellite: ISS
Catalog Number: 25544
Epoch time:      17365
50391832   =   yrday
fracday
Element set:     905
Inclination:       51
6388  deg
RA of node:       134
6625  deg
Eccentricity:     
0002824     
Arg of perigee:   312
0208  deg
Mean anomaly:      48
0704  deg
Mean motion:   15
54254678  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1243
Checksum:              301
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