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

 
Date: September 18th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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


261/10:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 216 1

265/22:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 215 0

267/18:16:53 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 214 7

269/19:33:04 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 214 4

Coasting Arc #1 (Orbit 1887)
---------------------------------------

Vector Time (GMT): 2016/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3617888
26                 A    =         6779064
89  meter
 Y    =        2655302
77  meter          E    =           
0001512
 Z    =        5080651
47                 I    =           51
45650
 XDOT =      -5834
943550                 Wp   =          355
64491
 YDOT =       4670
392944  meter/sec      RA   =          331
86300  deg
 ZDOT =       1715
635921                 TA   =           77
74181
                                          MA   =           77
72487
                                          Ha   =            221
005  n
mi
                                          Hp   =            216
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11869712
14                 X    =         3563247
69
 Y    =        8711623
28  feet           Y    =         2695455
49  meter
 Z    =       16668804
04                 Z    =         5098093
10
 XDOT =     -19143
515584                 XDOT =       -5895
069158
 YDOT =      15322
811497  feet/sec       YDOT =        4604
806707  meter/sec
 ZDOT =       5628
726775                 ZDOT =        1687
144900

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10619207
94                 X    =        -3236734
58
 Y    =      -10074036
25  feet           Y    =        -3070566
25  meter
 Z    =       16744482
40                 Z    =         5103718
24
 XDOT =      20160
301600                 XDOT =        6144
859928
 YDOT =     -12112
084542  feet/sec       YDOT =       -3691
763368  meter/sec
 ZDOT =       5503
397447                 ZDOT =        1677
435542


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   16258
55114486  
00016717  00000-0  10270-3 0  9003
2 25544  51
6445 332
1878 0006179 316
1696  43
8966 15
53857578 18889


Satellite: ISS
Catalog Number: 25544
Epoch time:      16258
55114486   =   yrday
fracday
Element set:     900
Inclination:       51
6445  deg
RA of node:       332
1878  deg
Eccentricity:     
0006179     
Arg of perigee:   316
1696  deg
Mean anomaly:      43
8966  deg
Mean motion:   15
53857578  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1888
Checksum:              356


Coasting Arc #2 (Orbit 1902)
---------------------------------------

Vector Time (GMT): 2016/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2228141
93                 A    =         6778230
20  meter
 Y    =       -3597752
36  meter          E    =           
0011871
 Z    =       -5304291
86                 I    =           51
42471
 XDOT =       6453
321281                 Wp   =           66
67862
 YDOT =      -4126
120435  meter/sec      RA   =          326
85356  deg
 ZDOT =         92
593996                 TA   =          204
17940
                                          MA   =          204
23517
                                          Ha   =            221
308  n
mi
                                          Hp   =            216
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7310176
95                 X    =        -2161979
55
 Y    =      -11803649
49  feet           Y    =        -3622299
71  meter
 Z    =      -17402532
34                 Z    =        -5314954
37
 XDOT =      21172
313914                 XDOT =        6498
531206
 YDOT =     -13537
140535  feet/sec       YDOT =       -4053
702274  meter/sec
 ZDOT =        303
786077                 ZDOT =         124
052758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5929710
75                 X    =         1807375
84
 Y    =       12490154
03  feet           Y    =         3806998
95  meter
 Z    =      -17448425
23                 Z    =        -5318280
01
 XDOT =     -21553
024344                 XDOT =       -6569
361820
 YDOT =      10827
916832  feet/sec       YDOT =        3300
349050  meter/sec
 ZDOT =        441
959370                 ZDOT =         134
709216


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   16259
51585638  
00016717  00000-0  10270-3 0  9012
2 25544  51
6439 327
3817 0006276 321
2591  38
8111 15
53829329 19037


Satellite: ISS
Catalog Number: 25544
Epoch time:      16259
51585638   =   yrday
fracday
Element set:     901
Inclination:       51
6439  deg
RA of node:       327
3817  deg
Eccentricity:     
0006276     
Arg of perigee:   321
2591  deg
Mean anomaly:      38
8111  deg
Mean motion:   15
53829329  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1903
Checksum:              323


Coasting Arc #3 (Orbit 1918)
---------------------------------------

Vector Time (GMT): 2016/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         776898
27                 A    =         6779318
27  meter
 Y    =        4488228
26  meter          E    =           
0008491
 Z    =        5022565
25                 I    =           51
40227
 XDOT =      -6655
211349                 Wp   =            7
64026
 YDOT =       3294
450515  meter/sec      RA   =          321
84210  deg
 ZDOT =      -1905
894664                 TA   =          100
95446
                                          MA   =          100
85892
                                          Ha   =            221
410  n
mi
                                          Hp   =            216
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2548878
84                 X    =          702254
63
 Y    =       14725158
33  feet           Y    =         4496499
42  meter
 Z    =       16478232
43                 Z    =         5026157
27
 XDOT =     -21834
682905                 XDOT =       -6682
298114
 YDOT =      10808
564683  feet/sec       YDOT =        3219
875754  meter/sec
 ZDOT =      -6252
935249                 ZDOT =       -1938
290179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1152448
22                 X    =         -351266
22
 Y    =      -14883187
67  feet           Y    =        -4536395
60  meter
 Z    =       16493083
49                 Z    =         5027091
85
 XDOT =      21565
704759                 XDOT =        6573
226811
 YDOT =      -8788
012590  feet/sec       YDOT =       -2678
586237  meter/sec
 ZDOT =      -6395
028437                 ZDOT =       -1949
204668


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   16260
54487297  
00016717  00000-0  10270-3 0  9020
2 25544  51
6437 322
2548 0006318 325
2331  34
8408 15
53886475 19190


Satellite: ISS
Catalog Number: 25544
Epoch time:      16260
54487297   =   yrday
fracday
Element set:     902
Inclination:       51
6437  deg
RA of node:       322
2548  deg
Eccentricity:     
0006318     
Arg of perigee:   325
2331  deg
Mean anomaly:      34
8408  deg
Mean motion:   15
53886475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1919
Checksum:              324


Coasting Arc #4 (Orbit 1932)
---------------------------------------

Vector Time (GMT): 2016/261/10:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3018432
70                 A    =         6787537
50  meter
 Y    =       -5531957
62  meter          E    =           
0008889
 Z    =       -2507631
23                 I    =           51
40554
 XDOT =       5524
608627                 Wp   =            4
41902
 YDOT =        624
493809  meter/sec      RA   =          317
13579  deg
 ZDOT =       5282
241562                 TA   =          327
34881
                                          MA   =          327
40374
                                          Ha   =            221
611  n
mi
                                          Hp   =            216
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9902994
44                 X    =         3092249
14
 Y    =      -18149467
26  feet           Y    =        -5497791
12  meter
 Z    =       -8227136
57                 Z    =        -2492788
31
 XDOT =      18125
356387                 XDOT =        5491
555880
 YDOT =       2048
864204  feet/sec       YDOT =         686
089656  meter/sec
 ZDOT =      17330
188853                 ZDOT =        5308
998392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16812994
29                 X    =        -5124600
66
 Y    =       12077860
89  feet           Y    =         3681332
00  meter
 Z    =       -8161295
00                 Z    =        -2487562
71
 XDOT =     -14484
354723                 XDOT =       -4414
831320
 YDOT =      -8395
877315  feet/sec       YDOT =       -2559
063406  meter/sec
 ZDOT =      17446
919361                 ZDOT =        5317
821021


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   16261
44525952  
00016717  00000-0  10270-3 0  9032
2 25544  51
6433 317
7684 0006286 328
3647  31
7127 15
53841276 19334


Satellite: ISS
Catalog Number: 25544
Epoch time:      16261
44525952   =   yrday
fracday
Element set:     903
Inclination:       51
6433  deg
RA of node:       317
7684  deg
Eccentricity:     
0006286     
Arg of perigee:   328
3647  deg
Mean anomaly:      31
7127  deg
Mean motion:   15
53841276  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1933
Checksum:              320


Coasting Arc #5 (Orbit 1948)
---------------------------------------

Vector Time (GMT): 2016/262/10:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3912459
00                 A    =         6789686
71  meter
 Y    =        5462778
44  meter          E    =           
0008536
 Z    =         957909
91                 I    =           51
38993
 XDOT =      -4420
245897                 Wp   =          104
32269
 YDOT =      -2125
589350  meter/sec      RA   =          312
14740  deg
 ZDOT =      -5889
998731                 TA   =           65
27180
                                          MA   =           65
18298
                                          Ha   =            221
700  n
mi
                                          Hp   =            215
795

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12836151
57                 X    =        -3977907
54
 Y    =       17922501
44  feet           Y    =         5418660
89  meter
 Z    =        3142749
04                 Z    =          938744
31
 XDOT =     -14502
119086                 XDOT =       -4367
537235
 YDOT =      -6973
718341  feet/sec       YDOT =       -2174
725621  meter/sec
 ZDOT =     -19324
142818                 ZDOT =       -5911
342986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19145642
74                 X    =         5835591
91
 Y    =      -10952277
30  feet           Y    =        -3338254
12  meter
 Z    =        3058055
31                 Z    =          932095
26
 XDOT =       9374
681323                 XDOT =        2857
402867
 YDOT =      10926
694168  feet/sec       YDOT =        3330
456382  meter/sec
 ZDOT =     -19416
955747                 ZDOT =       -5918
288112


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   16262
47426479  
00016717  00000-0  10270-3 0  9041
2 25544  51
6431 312
6411 0006225 333
4750  26
6083 15
53878166 19498


Satellite: ISS
Catalog Number: 25544
Epoch time:      16262
47426479   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       312
6411  deg
Eccentricity:     
0006225     
Arg of perigee:   333
4750  deg
Mean anomaly:      26
6083  deg
Mean motion:   15
53878166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1949
Checksum:              313


Coasting Arc #6 (Orbit 1964)
---------------------------------------

Vector Time (GMT): 2016/263/10:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4483835
83                 A    =         6789936
83  meter
 Y    =       -5042291
53  meter          E    =           
0016198
 Z    =         660240
90                 I    =           51
36943
 XDOT =       3207
017185                 Wp   =           29
74731
 YDOT =       3636
953891  meter/sec      RA   =          307
16000  deg
 ZDOT =       5947
111039                 TA   =          337
41389
                                          MA   =          337
48510
                                          Ha   =            221
905  n
mi
                                          Hp   =            215
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14710747
48                 X    =         4536679
57
 Y    =      -16542951
23  feet           Y    =        -4991854
73  meter
 Z    =        2166144
68                 Z    =          682151
44
 XDOT =      10521
709923                 XDOT =        3137
220704
 YDOT =      11932
263422  feet/sec       YDOT =        3672
427403  meter/sec
 ZDOT =      19511
519157                 ZDOT =        5962
520085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20088562
73                 X    =        -6122993
92
 Y    =        9278856
38  feet           Y    =         2828195
42  meter
 Z    =        2262737
61                 Z    =          689682
42
 XDOT =      -4073
981646                 XDOT =       -1241
749606
 YDOT =     -13631
904559  feet/sec       YDOT =       -4155
004510  meter/sec
 ZDOT =      19578
137537                 ZDOT =        5967
416321


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   16263
50326416  
00016717  00000-0  10270-3 0  9057
2 25544  51
6429 307
5132 0006410 338
6693  21
4191 15
53852472 19650


Satellite: ISS
Catalog Number: 25544
Epoch time:      16263
50326416   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:       307
5132  deg
Eccentricity:     
0006410     
Arg of perigee:   338
6693  deg
Mean anomaly:      21
4191  deg
Mean motion:   15
53852472  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1965
Checksum:              301


Coasting Arc #7 (Orbit 1979)
---------------------------------------

Vector Time (GMT): 2016/264/10:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4793289
48                 A    =         6787820
65  meter
 Y    =        4254735
95  meter          E    =           
0002787
 Z    =       -2240302
16                 I    =           51
34310
 XDOT =      -1948
606111                 Wp   =           52
17448
 YDOT =      -5048
946342  meter/sec      RA   =          302
16970  deg
 ZDOT =      -5422
627228                 TA   =          152
82088
                                          MA   =          152
80629
                                          Ha   =            221
975  n
mi
                                          Hp   =            215
315

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15726015
34                 X    =        -4829628
22
 Y    =       13959107
45  feet           Y    =         4200930
75  meter
 Z    =       -7350072
70                 Z    =        -2263675
73
 XDOT =      -6393
064670                 XDOT =       -1865
661608
 YDOT =     -16564
784587  feet/sec       YDOT =       -5070
273774  meter/sec
 ZDOT =     -17790
771746                 ZDOT =       -5431
891164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19838939
29                 X    =         6046908
70
 Y    =       -6859922
22  feet           Y    =        -2090904
29  meter
 Z    =       -7452902
99                 Z    =        -2271644
83
 XDOT =      -1072
315827                 XDOT =        -326
841864
 YDOT =      16260
041651  feet/sec       YDOT =        4956
060695  meter/sec
 ZDOT =     -17830
303251                 ZDOT =       -5434
676431


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   16264
46794482  
00016717  00000-0  10270-3 0  9066
2 25544  51
6418 302
7066 0006268 342
3853  17
7081 15
53894248 19802


Satellite: ISS
Catalog Number: 25544
Epoch time:      16264
46794482   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:       302
7066  deg
Eccentricity:     
0006268     
Arg of perigee:   342
3853  deg
Mean anomaly:      17
7081  deg
Mean motion:   15
53894248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1980
Checksum:              332


Coasting Arc #8 (Orbit 1995)
---------------------------------------

Vector Time (GMT): 2016/265/10:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4830057
01                 A    =         6784402
12  meter
 Y    =       -3117432
17  meter          E    =           
0011616
 Z    =        3588836
77                 I    =           51
31574
 XDOT =        755
623154                 Wp   =           62
59033
 YDOT =       6241
633225  meter/sec      RA   =          297
16984  deg
 ZDOT =       4399
100666                 TA   =          340
12857
                                          MA   =          340
17378
                                          Ha   =            221
926  n
mi
                                          Hp   =            215
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15846643
75                 X    =         4847124
75
 Y    =      -10227795
83  feet           Y    =        -3063323
48  meter
 Z    =       11774398
84                 Z    =         3612341
94
 XDOT =       2479
078590                 XDOT =         664
402313
 YDOT =      20477
799293  feet/sec       YDOT =        6249
573457  meter/sec
 ZDOT =      14432
744968                 ZDOT =        4402
549206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18428640
88                 X    =        -5617049
74
 Y    =        3697076
33  feet           Y    =         1126868
87  meter
 Z    =       11877593
00                 Z    =         3620290
35
 XDOT =       5596
973323                 XDOT =        1705
957469
 YDOT =     -18573
563539  feet/sec       YDOT =       -5661
222167  meter/sec
 ZDOT =      14446
674016                 ZDOT =        4403
346240


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   16265
49693122  
00016717  00000-0  10270-3 0  9070
2 25544  51
6420 297
5785 0006303 345
7124  14
3849 15
53909447 19962


Satellite: ISS
Catalog Number: 25544
Epoch time:      16265
49693122   =   yrday
fracday
Element set:     907
Inclination:       51
6420  deg
RA of node:       297
5785  deg
Eccentricity:     
0006303     
Arg of perigee:   345
7124  deg
Mean anomaly:      14
3849  deg
Mean motion:   15
53909447  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1996
Checksum:              336


Coasting Arc #9 (Orbit 2002)
---------------------------------------

Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2889029
25                 A    =         6778941
95  meter
 Y    =       -3455430
46  meter          E    =           
0012032
 Z    =       -5075366
59                 I    =           51
29211
 XDOT =       4307
116683                 Wp   =           72
65843
 YDOT =      -6100
235258  meter/sec      RA   =          294
66046  deg
 ZDOT =       1708
345448                 TA   =          213
90867
                                          MA   =          213
98565
                                          Ha   =            222
145  n
mi
                                          Hp   =            214
988

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9478442
42                 X    =        -2825520
86
 Y    =      -11336714
10  feet           Y    =        -3487382
84  meter
 Z    =      -16651465
21                 Z    =        -5089246
36
 XDOT =      14130
960247                 XDOT =        4366
712469
 YDOT =     -20013
895205  feet/sec       YDOT =       -6051
736832  meter/sec
 ZDOT =       5604
807900                 ZDOT =        1729
413783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4101205
41                 X    =        -1250047
41
 Y    =      -14125895
88  feet           Y    =        -4305573
06  meter
 Z    =      -16711446
09                 Z    =        -5093648
77
 XDOT =      19849
485248                 XDOT =        6050
123104
 YDOT =     -12477
154197  feet/sec       YDOT =       -3803
036599  meter/sec
 ZDOT =       5697
897894                 ZDOT =        1736
719278


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   16265
94711120  
00016717  00000-0  10270-3 0  9080
2 25544  51
6438 295
3374 0006714 347
3542  12
7441 15
53923827 20037


Satellite: ISS
Catalog Number: 25544
Epoch time:      16265
94711120   =   yrday
fracday
Element set:     908
Inclination:       51
6438  deg
RA of node:       295
3374  deg
Eccentricity:     
0006714     
Arg of perigee:   347
3542  deg
Mean anomaly:      12
7441  deg
Mean motion:   15
53923827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2003
Checksum:              301


Coasting Arc #10 (Orbit 2018)
---------------------------------------

Vector Time (GMT): 2016/266/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1992370
89                 A    =         6781727
12  meter
 Y    =        4800907
24  meter          E    =           
0012663
 Z    =        4354910
07                 I    =           51
28889
 XDOT =      -4683
582556                 Wp   =           38
63982
 YDOT =       5034
308807  meter/sec      RA   =          289
64354  deg
 ZDOT =      -3392
066826                 TA   =           85
97171
                                          MA   =           85
82697
                                          Ha   =            222
269  n
mi
                                          Hp   =            214
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6536649
89                 X    =         1917383
44
 Y    =       15751008
00  feet           Y    =         4822768
31  meter
 Z    =       14287762
68                 Z    =         4364406
07
 XDOT =     -15366
084500                 XDOT =       -4723
052085
 YDOT =      16516
761179  feet/sec       YDOT =        4981
712908  meter/sec
 ZDOT =     -11128
828170                 ZDOT =       -3414
914873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -43959
20                 X    =          -13398
76
 Y    =       17019346
25  feet           Y    =         5187496
74  meter
 Z    =       14328367
94                 Z    =         4367286
55
 XDOT =     -19191
851984                 XDOT =       -5849
676485
 YDOT =       9445
926455  feet/sec       YDOT =        2879
118384  meter/sec
 ZDOT =     -11229
491397                 ZDOT =       -3422
748978


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   16266
97608772  
00016717  00000-0  10270-3 0  9093
2 25544  51
6435 290
2096 0006864 351
0512   9
0517 15
53962645 20195


Satellite: ISS
Catalog Number: 25544
Epoch time:      16266
97608772   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:       290
2096  deg
Eccentricity:     
0006864     
Arg of perigee:   351
0512  deg
Mean anomaly:       9
0517  deg
Mean motion:   15
53962645  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2019
Checksum:              322


Coasting Arc #11 (Orbit 2031)
---------------------------------------

Vector Time (GMT): 2016/267/18:16:53
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4375004
97                 A    =         6778362
70  meter
 Y    =        -262984
54  meter          E    =           
0005084
 Z    =        5167556
51                 I    =           51
26767
 XDOT =      -1034
056086                 Wp   =           32
32007
 YDOT =       7495
893194  meter/sec      RA   =          285
53322  deg
 ZDOT =       1260
588252                 TA   =           45
53991
                                          MA   =           45
49834
                                          Ha   =            222
200  n
mi
                                          Hp   =            214
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14353690
86                 X    =         4352518
73
 Y    =        -862810
16  feet           Y    =         -214185
64  meter
 Z    =       16953925
56                 Z    =         5188754
65
 XDOT =      -3392
572462                 XDOT =       -1123
923631
 YDOT =      24592
825438  feet/sec       YDOT =        7483
827300  meter/sec
 ZDOT =       4135
788229                 ZDOT =        1255
346214

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2441154
21                 X    =          744063
80
 Y    =       14059336
02  feet           Y    =         4285285
62  meter
 Z    =       17046533
70                 Z    =         5195783
47
 XDOT =     -23795
724203                 XDOT =       -7252
936737
 YDOT =       -839
016663  feet/sec       YDOT =        -255
732279  meter/sec
 ZDOT =       4111
570150                 ZDOT =        1253
206582


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   16267
81212963  
00016717  00000-0  10270-3 0  9102
2 25544  51
6419 286
0433 0006663 354
2920   5
8155 15
53956321 20321


Satellite: ISS
Catalog Number: 25544
Epoch time:      16267
81212963   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       286
0433  deg
Eccentricity:     
0006663     
Arg of perigee:   354
2920  deg
Mean anomaly:       5
8155  deg
Mean motion:   15
53956321  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2032
Checksum:              297


Coasting Arc #12 (Orbit 2046)
---------------------------------------

Vector Time (GMT): 2016/268/18:16:53
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4035223
58                 A    =         6778041
22  meter
 Y    =       -1423666
44  meter          E    =           
0015522
 Z    =       -5268731
21                 I    =           51
25928
 XDOT =       1854
042086                 Wp   =           68
98782
 YDOT =      -7406
831809  meter/sec      RA   =          280
50906  deg
 ZDOT =        588
299085                 TA   =          206
62456
                                          MA   =          206
70435
                                          Ha   =            222
479  n
mi
                                          Hp   =            214
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13238922
50                 X    =        -3993410
65
 Y    =       -4670821
65  feet           Y    =        -1468557
66  meter
 Z    =      -17285863
53                 Z    =        -5288231
63
 XDOT =       6082
815244                 XDOT =        1933
871664
 YDOT =     -24300
629293  feet/sec       YDOT =       -7385
652265  meter/sec
 ZDOT =       1930
115107                 ZDOT =         597
500062

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2948619
71                 X    =          898739
29
 Y    =      -13617961
74  feet           Y    =        -4150754
74  meter
 Z    =      -17370765
15                 Z    =        -5294609
22
 XDOT =      23885
594410                 XDOT =        7280
329176
 YDOT =       2685
514127  feet/sec       YDOT =         818
544706  meter/sec
 ZDOT =       1971
589976                 ZDOT =         600
940625


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   16268
77678820  
00016717  00000-0  10270-3 0  9117
2 25544  51
6425 281
2359 0006730 358
8252   1
2884 15
53933571 20472


Satellite: ISS
Catalog Number: 25544
Epoch time:      16268
77678820   =   yrday
fracday
Element set:     911
Inclination:       51
6425  deg
RA of node:       281
2359  deg
Eccentricity:     
0006730     
Arg of perigee:   358
8252  deg
Mean anomaly:       1
2884  deg
Mean motion:   15
53933571  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2047
Checksum:              323


Coasting Arc #13 (Orbit 2062)
---------------------------------------

Vector Time (GMT): 2016/269/18:16:53
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3604101
49                 A    =         6779815
52  meter
 Y    =        3088376
12  meter          E    =           
0012132
 Z    =        4839757
79                 I    =           51
26019
 XDOT =      -2589
916594                 Wp   =           31
42128
 YDOT =       6806
898069  meter/sec      RA   =          275
48708  deg
 ZDOT =      -2402
072423                 TA   =           82
32404
                                          MA   =           82
18629
                                          Ha   =            222
560  n
mi
                                          Hp   =            214
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11824479
95                 X    =         3545789
20
 Y    =       10132467
59  feet           Y    =         3128354
02  meter
 Z    =       15878470
45                 Z    =         4857123
65
 XDOT =      -8497
101686                 XDOT =       -2654
172362
 YDOT =      22332
342746  feet/sec       YDOT =        6777
576380  meter/sec
 ZDOT =      -7880
815035                 ZDOT =       -2414
810282

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8321753
10                 X    =        -2536470
34
 Y    =       13070452
67  feet           Y    =         3983873
98  meter
 Z    =       15953768
88                 Z    =         4862708
76
 XDOT =     -22369
297008                 XDOT =       -6818
161728
 YDOT =      -4502
082066  feet/sec       YDOT =       -1372
234614  meter/sec
 ZDOT =      -7937
614929                 ZDOT =       -2419
385030


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   16269
80574861  
00016717  00000-0  10270-3 0  9123
2 25544  51
6423 276
1089 0006822   2
9497 357
1694 15
53950526 20632


Satellite: ISS
Catalog Number: 25544
Epoch time:      16269
80574861   =   yrday
fracday
Element set:     912
Inclination:       51
6423  deg
RA of node:       276
1089  deg
Eccentricity:     
0006822     
Arg of perigee:     2
9497  deg
Mean anomaly:     357
1694  deg
Mean motion:   15
53950526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2063
Checksum:              329


Coasting Arc #14 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2016/269/19:33:04
000
Vector Time (MET): N/A
Weight (LBS)     : 908286
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3624035
02                 A    =         6782901
54  meter
 Y    =       -4060682
88  meter          E    =           
0011708
 Z    =        4035136
61                 I    =           51
27147
 XDOT =       2548
918848                 Wp   =           67
34660
 YDOT =       6120
376423  meter/sec      RA   =          275
26595  deg
 ZDOT =       3865
339035                 TA   =          342
42056
                                          MA   =          342
46105
                                          Ha   =            222
548  n
mi
                                          Hp   =            214
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11889878
67                 X    =         3649572
34
 Y    =      -13322450
40  feet           Y    =        -4020013
31  meter
 Z    =       13238637
18                 Z    =         4052803
65
 XDOT =       8362
594647                 XDOT =        2461
513686
 YDOT =      20079
975140  feet/sec       YDOT =        6148
391804  meter/sec
 ZDOT =      12681
558515                 ZDOT =        3877
508132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17263476
28                 X    =         5261907
57
 Y    =        4331511
29  feet           Y    =         1320244
64  meter
 Z    =       13316486
41                 Z    =         4058865
06
 XDOT =     -13684
747471                 XDOT =       -4171
111029
 YDOT =      15348
286749  feet/sec       YDOT =        4678
157801  meter/sec
 ZDOT =      12733
640521                 ZDOT =        3881
213631


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   16269
87005865  
00016717  00000-0  10270-3 0  9134
2 25544  51
6436 275
7880 0006801   3
4370 356
6828 15
53932075 20646


Satellite: ISS
Catalog Number: 25544
Epoch time:      16269
87005865   =   yrday
fracday
Element set:     913
Inclination:       51
6436  deg
RA of node:       275
7880  deg
Eccentricity:     
0006801     
Arg of perigee:     3
4370  deg
Mean anomaly:     356
6828  deg
Mean motion:   15
53932075  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2064
Checksum:              324


Coasting Arc #15 (Orbit 2078)
---------------------------------------

Vector Time (GMT): 2016/270/19:33:04
000
Vector Time (MET): N/A
Weight (LBS)     : 908286
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3942895
98                 A    =         6779538
44  meter
 Y    =        2558423
84  meter          E    =           
0016083
 Z    =       -4900140
77                 I    =           51
25781
 XDOT =      -1784
364401                 Wp   =           50
35101
 YDOT =      -7093
068553  meter/sec      RA   =          270
25031  deg
 ZDOT =      -2262
492615                 TA   =          197
35684
                                          MA   =          197
41188
                                          Ha   =            222
681  n
mi
                                          Hp   =            214
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12936010
42                 X    =        -3947409
16
 Y    =        8393779
00  feet           Y    =         2514305
95  meter
 Z    =      -16076577
33                 Z    =        -4919305
58
 XDOT =      -5854
213913                 XDOT =       -1693
925094
 YDOT =     -23271
222288  feet/sec       YDOT =       -7112
517090  meter/sec
 ZDOT =      -7422
876033                 ZDOT =       -2270
940128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13491059
89                 X    =        -4112075
06
 Y    =       -7285272
97  feet           Y    =        -2220551
20  meter
 Z    =      -16160703
30                 Z    =        -4925782
37
 XDOT =      17165
731020                 XDOT =        5232
114815
 YDOT =     -15205
949841  feet/sec       YDOT =       -4634
773511  meter/sec
 ZDOT =      -7458
556940                 ZDOT =       -2273
368155


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   16270
83470243  
00016717  00000-0  10270-3 0  9149
2 25544  51
6428 270
9816 0006825   6
0686 354
0549 15
53969655 20790


Satellite: ISS
Catalog Number: 25544
Epoch time:      16270
83470243   =   yrday
fracday
Element set:     914
Inclination:       51
6428  deg
RA of node:       270
9816  deg
Eccentricity:     
0006825     
Arg of perigee:     6
0686  deg
Mean anomaly:     354
0549  deg
Mean motion:   15
53969655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2079
Checksum:              333


Coasting Arc #16 (Orbit 2094)
---------------------------------------

Vector Time (GMT): 2016/271/19:33:04
000
Vector Time (MET): N/A
Weight (LBS)     : 908286
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4173152
33                 A    =         6777843
76  meter
 Y    =        -845649
84  meter          E    =           
0006775
 Z    =        5269912
18                 I    =           51
25332
 XDOT =        989
192704                 Wp   =           32
10422
 YDOT =       7594
983205  meter/sec      RA   =          265
22659  deg
 ZDOT =        440
806773                 TA   =           53
70215
                                          MA   =           53
63960
                                          Ha   =            222
576  n
mi
                                          Hp   =            214
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13691444
66                 X    =         4156699
50
 Y    =       -2774441
74  feet           Y    =         -799074
18  meter
 Z    =       17289738
13                 Z    =         5290144
44
 XDOT =       3245
382888                 XDOT =         902
048902
 YDOT =      24917
923902  feet/sec       YDOT =        7605
557828  meter/sec
 ZDOT =       1446
216447                 ZDOT =         445
399390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9087425
56                 X    =         2769847
31
 Y    =       10464412
30  feet           Y    =         3189552
87  meter
 Z    =       17378233
53                 Z    =         5296885
58
 XDOT =     -19349
393328                 XDOT =       -5897
695086
 YDOT =      14399
515764  feet/sec       YDOT =        4388
972405  meter/sec
 ZDOT =       1464
996840                 ZDOT =         446
531037


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   16271
86365042  
00016717  00000-0  10270-3 0  9154
2 25544  51
6430 265
8536 0006714   9
3053 350
8223 15
53978767 20951


Satellite: ISS
Catalog Number: 25544
Epoch time:      16271
86365042   =   yrday
fracday
Element set:     915
Inclination:       51
6430  deg
RA of node:       265
8536  deg
Eccentricity:     
0006714     
Arg of perigee:     9
3053  deg
Mean anomaly:     350
8223  deg
Mean motion:   15
53978767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2095
Checksum:              319


Coasting Arc #17 (Orbit 2109)
---------------------------------------

Vector Time (GMT): 2016/272/19:33:04
000
Vector Time (MET): N/A
Weight (LBS)     : 908286
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4340233
23                 A    =         6778423
82  meter
 Y    =        -879215
07  meter          E    =           
0015612
 Z    =       -5144129
53                 I    =           51
25888
 XDOT =       -145
930006                 Wp   =           74
81744
 YDOT =      -7524
310677  meter/sec      RA   =          260
20143  deg
 ZDOT =       1416
776451                 TA   =          208
86039
                                          MA   =          208
94683
                                          Ha   =            222
774  n
mi
                                          Hp   =            213
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14239610
32                 X    =        -4305091
03
 Y    =       -2884563
88  feet           Y    =         -927554
70  meter
 Z    =      -16877065
40                 Z    =        -5165127
85
 XDOT =       -478
772986                 XDOT =         -68
662505
 YDOT =     -24686
058651  feet/sec       YDOT =       -7525
510338  meter/sec
 ZDOT =       4648
216702                 ZDOT =        1416
256282

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4664803
68                 X    =        -1421832
16
 Y    =      -13646541
07  feet           Y    =        -4159465
72  meter
 Z    =      -16968620
18                 Z    =        -5172035
43
 XDOT =      20035
523375                 XDOT =        6106
827525
 YDOT =     -12596
305855  feet/sec       YDOT =       -3839
354025  meter/sec
 ZDOT =       4647
191383                 ZDOT =        1416
463934


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   16272
82828287  
00016717  00000-0  10270-3 0  9167
2 25544  51
6429 261
0458 0006852  12
4060 347
7260 15
53988164 21102


Satellite: ISS
Catalog Number: 25544
Epoch time:      16272
82828287   =   yrday
fracday
Element set:     916
Inclination:       51
6429  deg
RA of node:       261
0458  deg
Eccentricity:     
0006852     
Arg of perigee:    12
4060  deg
Mean anomaly:     347
7260  deg
Mean motion:   15
53988164  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2110
Checksum:              313
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