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

 
Date: June 20th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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


170/05:52:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 0

171/22:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 503)
---------------------------------------

Vector Time (GMT): 2016/169/13:24:18
756
Vector Time (MET): N/A
Weight (LBS)     : 906675
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3627428
80                 A    =         6788024
79  meter
 Y    =       -5722482
00  meter          E    =           
0010806
 Z    =        -322176
41                 I    =           51
97126
 XDOT =       4144
996289                 Wp   =          136
84681
 YDOT =      -2295
123040  meter/sec      RA   =           55
49846  deg
 ZDOT =      -6029
916252                 TA   =           46
61018
                                          MA   =           46
52024
                                          Ha   =            220
188  n
mi
                                          Hp   =            214
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11901013
12                 X    =        -3561603
96
 Y    =      -18774547
25  feet           Y    =        -5762678
24  meter
 Z    =       -1057009
22                 Z    =         -339638
50
 XDOT =      13599
069191                 XDOT =        4199
643819
 YDOT =      -7529
931232  feet/sec       YDOT =       -2248
464647  meter/sec
 ZDOT =     -19783
189804                 ZDOT =       -6009
648288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14636045
84                 X    =        -4461066
77
 Y    =       16725425
48  feet           Y    =         5097909
69  meter
 Z    =       -1131950
13                 Z    =         -345018
40
 XDOT =      -9892
179596                 XDOT =       -3015
136341
 YDOT =      -9963
040507  feet/sec       YDOT =       -3036
734746  meter/sec
 ZDOT =     -19694
383981                 ZDOT =       -6002
848237


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   16169
59006500  
00016717  00000-0  10270-3 0  9005
2 25544  51
6441  56
0279 0000588 321
3039  38
8071 15
54559593  5041


Satellite: ISS
Catalog Number: 25544
Epoch time:      16169
59006500   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:        56
0279  deg
Eccentricity:     
0000588     
Arg of perigee:   321
3039  deg
Mean anomaly:      38
8071  deg
Mean motion:   15
54559593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             504
Checksum:              300


Coasting Arc #2 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2016/170/05:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1358880
05                 A    =         6777791
50  meter
 Y    =        4489827
41  meter          E    =           
0006303
 Z    =        4888501
63                 I    =           51
92156
 XDOT =      -5811
126076                 Wp   =          118
13936
 YDOT =      -4389
983252  meter/sec      RA   =           52
10422  deg
 ZDOT =       2411
361286                 TA   =          308
29781
                                          MA   =          308
35447
                                          Ha   =            220
181  n
mi
                                          Hp   =            214
017

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4458267
87                 X    =        -1432731
82
 Y    =       14730404
90  feet           Y    =         4474217
94  meter
 Z    =       16038391
18                 Z    =         4881721
70
 XDOT =     -19065
374264                 XDOT =       -5773
317715
 YDOT =     -14402
832190  feet/sec       YDOT =       -4454
756050  meter/sec
 ZDOT =       7911
290309                 ZDOT =        2383
223355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6031930
72                 X    =        -1838532
48
 Y    =       14193425
07  feet           Y    =         4326155
96  meter
 Z    =       16007918
96                 Z    =         4879213
70
 XDOT =     -16522
047524                 XDOT =       -5035
920085
 YDOT =     -15826
413480  feet/sec       YDOT =       -4823
890829  meter/sec
 ZDOT =       7789
552928                 ZDOT =        2374
255733


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   16170
29717238  
00016717  00000-0  10270-3 0  9012
2 25544  51
6407  52
5000 0000612 328
1640  31
9476 15
54617783  5158


Satellite: ISS
Catalog Number: 25544
Epoch time:      16170
29717238   =   yrday
fracday
Element set:     901
Inclination:       51
6407  deg
RA of node:        52
5000  deg
Eccentricity:     
0000612     
Arg of perigee:   328
1640  deg
Mean anomaly:      31
9476  deg
Mean motion:   15
54617783  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              284


Coasting Arc #3 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2016/171/05:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2803593
46                 A    =         6775976
94  meter
 Y    =       -3125067
08  meter          E    =           
0014653
 Z    =       -5331254
88                 I    =           51
89544
 XDOT =       5398
100455                 Wp   =           85
12169
 YDOT =       5422
082708  meter/sec      RA   =           47
11915  deg
 ZDOT =       -339
150449                 TA   =          181
64973
                                          MA   =          181
65457
                                          Ha   =            220
167  n
mi
                                          Hp   =            214
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9198141
27                 X    =         2864227
42
 Y    =      -10252844
74  feet           Y    =        -3093375
64  meter
 Z    =      -17490993
70                 Z    =        -5317488
84
 XDOT =      17710
303329                 XDOT =        5338
715620
 YDOT =      17788
985263  feet/sec       YDOT =        5482
115870  meter/sec
 ZDOT =      -1112
698325                 ZDOT =        -313
071176

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10141811
64                 X    =         3091224
19
 Y    =       -9433353
15  feet           Y    =        -2875286
04  meter
 Z    =      -17430346
92                 Z    =        -5312769
74
 XDOT =      15467
036586                 XDOT =        4714
352751
 YDOT =      18479
160801  feet/sec       YDOT =        5632
448212  meter/sec
 ZDOT =      -1000
154823                 ZDOT =        -304
847190


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   16171
26140197  
00016717  00000-0  10270-3 0  9025
2 25544  51
6413  47
6897 0000592 338
8463  21
2665 15
54613209  5300


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
26140197   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:        47
6897  deg
Eccentricity:     
0000592     
Arg of perigee:   338
8463  deg
Mean anomaly:      21
2665  deg
Mean motion:   15
54613209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             530
Checksum:              299


Coasting Arc #4 (Orbit 540)
---------------------------------------

Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5685774
50                 A    =         6784407
33  meter
 Y    =       -2314138
93  meter          E    =           
0012975
 Z    =        2875284
58                 I    =           51
91150
 XDOT =       -242
843492                 Wp   =           97
90448
 YDOT =      -5740
852936  meter/sec      RA   =           43
68419  deg
 ZDOT =      -5082
847629                 TA   =           49
48503
                                          MA   =           49
37207
                                          Ha   =            220
137  n
mi
                                          Hp   =            214
014

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18654115
82                 X    =        -5673441
56
 Y    =       -7592319
34  feet           Y    =        -2377652
52  meter
 Z    =        9433348
35                 Z    =         2847694
06
 XDOT =       -796
730618                 XDOT =        -153
939453
 YDOT =     -18834
819344  feet/sec       YDOT =       -5743
070729  meter/sec
 ZDOT =     -16676
009281                 ZDOT =       -5083
812217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15325503
50                 X    =         4671213
47
 Y    =      -13152705
10  feet           Y    =        -4008944
52  meter
 Z    =        9313576
21                 Z    =         2838778
03
 XDOT =      16097
648679                 XDOT =        4906
563317
 YDOT =       6904
405020  feet/sec       YDOT =        2104
462650  meter/sec
 ZDOT =     -16679
017907                 ZDOT =       -5083
764658


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   16171
96849524  
00016717  00000-0  10270-3 0  9033
2 25544  51
6442  44
1615 0000481 314
9722  45
1392 15
54645992  5410


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
96849524   =   yrday
fracday
Element set:     903
Inclination:       51
6442  deg
RA of node:        44
1615  deg
Eccentricity:     
0000481     
Arg of perigee:   314
9722  deg
Mean anomaly:      45
1392  deg
Mean motion:   15
54645992  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             541
Checksum:              307


Coasting Arc #5 (Orbit 555)
---------------------------------------

Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5730260
26                 A    =         6787412
58  meter
 Y    =        3443867
94  meter          E    =           
0009661
 Z    =       -1145180
27                 I    =           51
89654
 XDOT =      -1612
321499                 Wp   =           33
99718
 YDOT =       4632
320044  meter/sec      RA   =           38
72546  deg
 ZDOT =       5894
646429                 TA   =          313
61333
                                          MA   =          313
69344
                                          Ha   =            220
153  n
mi
                                          Hp   =            214
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18800066
47                 X    =         5696886
96
 Y    =       11298779
32  feet           Y    =         3507761
09  meter
 Z    =       -3757153
11                 Z    =        -1117424
68
 XDOT =      -5289
768696                 XDOT =       -1692
635043
 YDOT =      15197
900408  feet/sec       YDOT =        4613
840049  meter/sec
 ZDOT =      19339
391171                 ZDOT =        5886
619806

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18468771
30                 X    =        -5629281
49
 Y    =       11870069
70  feet           Y    =         3617997
24  meter
 Z    =       -3636900
49                 Z    =        -1108527
27
 XDOT =     -10362
256303                 XDOT =       -3158
415721
 YDOT =     -10241
287770  feet/sec       YDOT =       -3121
544512  meter/sec
 ZDOT =      19303
436123                 ZDOT =        5883
687330


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   16172
93270684  
00016717  00000-0  10270-3 0  9047
2 25544  51
6434  39
3519 0000679 324
9728  35
1380 15
54607492  5561


Satellite: ISS
Catalog Number: 25544
Epoch time:      16172
93270684   =   yrday
fracday
Element set:     904
Inclination:       51
6434  deg
RA of node:        39
3519  deg
Eccentricity:     
0000679     
Arg of perigee:   324
9728  deg
Mean anomaly:      35
1380  deg
Mean motion:   15
54607492  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             556
Checksum:              322


Coasting Arc #6 (Orbit 571)
---------------------------------------

Vector Time (GMT): 2016/173/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5246853
03                 A    =         6787499
11  meter
 Y    =       -4230417
19  meter          E    =           
0009800
 Z    =        -764509
02                 I    =           51
87101
 XDOT =       3513
641221                 Wp   =          139
66114
 YDOT =      -3287
932277  meter/sec      RA   =           33
77041  deg
 ZDOT =      -5970
409972                 TA   =           48
57661
                                          MA   =           48
49244
                                          Ha   =            220
045  n
mi
                                          Hp   =            213
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17214084
75                 X    =        -5195443
85
 Y    =      -13879321
49  feet           Y    =        -4288803
44  meter
 Z    =       -2508231
68                 Z    =         -789872
55
 XDOT =      11527
694296                 XDOT =        3579
148102
 YDOT =     -10787
179386  feet/sec       YDOT =       -3248
273264  meter/sec
 ZDOT =     -19587
959226                 ZDOT =       -5953
183030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19899831
87                 X    =         6065468
75
 Y    =       -9612223
94  feet           Y    =        -2929805
86  meter
 Z    =       -2617889
87                 Z    =         -797932
83
 XDOT =       4069
671120                 XDOT =        1240
435757
 YDOT =      13696
658911  feet/sec       YDOT =        4174
741636  meter/sec
 ZDOT =     -19512
182835                 ZDOT =       -5947
313328


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   16173
96119159  
00016717  00000-0  10270-3 0  9051
2 25544  51
6426  34
2214 0000494 326
8529  33
2592 15
54664560  5724


Satellite: ISS
Catalog Number: 25544
Epoch time:      16173
96119159   =   yrday
fracday
Element set:     905
Inclination:       51
6426  deg
RA of node:        34
2214  deg
Eccentricity:     
0000494     
Arg of perigee:   326
8529  deg
Mean anomaly:      33
2592  deg
Mean motion:   15
54664560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             572
Checksum:              309


Coasting Arc #7 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2016/174/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4251514
20                 A    =         6784941
18  meter
 Y    =        4623683
54  meter          E    =           
0013569
 Z    =        2548211
19                 I    =           51
83571
 XDOT =      -5225
318825                 Wp   =           73
66588
 YDOT =       1875
654656  meter/sec      RA   =           28
80874  deg
 ZDOT =       5295
144154                 TA   =          314
89771
                                          MA   =          315
00777
                                          Ha   =            220
045  n
mi
                                          Hp   =            213
870

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13948537
40                 X    =         4187117
01
 Y    =       15169565
43  feet           Y    =         4670866
40  meter
 Z    =        8360272
95                 Z    =         2568708
04
 XDOT =     -17143
434464                 XDOT =       -5271
625839
 YDOT =       6153
722626  feet/sec       YDOT =        1816
962030  meter/sec
 ZDOT =      17372
520190                 ZDOT =        5269
648832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19547010
36                 X    =        -5957928
76
 Y    =        6411439
20  feet           Y    =         1954206
67  meter
 Z    =        8448633
53                 Z    =         2575143
50
 XDOT =       1966
727623                 XDOT =         599
458579
 YDOT =     -16833
314089  feet/sec       YDOT =       -5130
794134  meter/sec
 ZDOT =      17261
002776                 ZDOT =        5261
153646


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   16174
98966574  
00016717  00000-0  10270-3 0  9066
2 25544  51
6430  29
0900 0000579 338
0802  22
0326 15
54671125  5889


Satellite: ISS
Catalog Number: 25544
Epoch time:      16174
98966574   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:        29
0900  deg
Eccentricity:     
0000579     
Arg of perigee:   338
0802  deg
Mean anomaly:      22
0326  deg
Mean motion:   15
54671125  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             588
Checksum:              309


Coasting Arc #8 (Orbit 602)
---------------------------------------

Vector Time (GMT): 2016/175/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2766067
74                 A    =         6780743
42  meter
 Y    =       -4698169
42  meter          E    =           
0007294
 Z    =       -4039637
95                 I    =           51
79302
 XDOT =       6558
930888                 Wp   =           66
38687
 YDOT =       -484
497853  meter/sec      RA   =           23
83524  deg
 ZDOT =      -3930
394853                 TA   =          162
86938
                                          MA   =          162
84475
                                          Ha   =            220
086  n
mi
                                          Hp   =            213
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9075025
40                 X    =        -2693703
42
 Y    =      -15413941
68  feet           Y    =        -4728696
34  meter
 Z    =      -13253405
35                 Z    =        -4052899
49
 XDOT =      21518
802127                 XDOT =        6582
953175
 YDOT =      -1589
559884  feet/sec       YDOT =        -411
016731  meter/sec
 ZDOT =     -12894
996237                 ZDOT =       -3898
475216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17715267
44                 X    =         5399613
52
 Y    =       -2146152
96  feet           Y    =         -654147
42  meter
 Z    =      -13310212
79                 Z    =        -4056952
86
 XDOT =      -7254
495497                 XDOT =       -2211
170227
 YDOT =      19172
178613  feet/sec       YDOT =        5843
680041  meter/sec
 ZDOT =     -12755
774677                 ZDOT =       -3887
960122


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   16175
95385241  
00016717  00000-0  10270-3 0  9071
2 25544  51
6428  24
2799 0000615 348
4649  11
6490 15
54682936  6030


Satellite: ISS
Catalog Number: 25544
Epoch time:      16175
95385241   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:        24
2799  deg
Eccentricity:     
0000615     
Arg of perigee:   348
4649  deg
Mean anomaly:      11
6490  deg
Mean motion:   15
54682936  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             603
Checksum:              325


Coasting Arc #9 (Orbit 618)
---------------------------------------

Vector Time (GMT): 2016/176/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         944333
48                 A    =         6777024
32  meter
 Y    =        4480936
31  meter          E    =           
0005524
 Z    =        4992381
62                 I    =           51
75044
 XDOT =      -7343
979409                 Wp   =          118
28879
 YDOT =       -774
362791  meter/sec      RA   =           18
84737  deg
 ZDOT =       2079
876593                 TA   =          311
49299
                                          MA   =          311
54039
                                          Ha   =            220
034  n
mi
                                          Hp   =            213
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3098206
94                 X    =          869905
73
 Y    =       14701234
60  feet           Y    =         4491079
81  meter
 Z    =       16379204
78                 Z    =         4996788
59
 XDOT =     -24094
420633                 XDOT =       -7344
877517
 YDOT =      -2540
560339  feet/sec       YDOT =        -856
493298  meter/sec
 ZDOT =       6823
742102                 ZDOT =        2044
199458

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14735948
12                 X    =        -4491516
99
 Y    =       -2824622
87  feet           Y    =         -860945
05  meter
 Z    =       16397465
44                 Z    =         4997947
47
 XDOT =      11323
927693                 XDOT =        3451
533161
 YDOT =     -20283
166896  feet/sec       YDOT =       -6182
309270  meter/sec
 ZDOT =       6668
415235                 ZDOT =        2032
532964


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   16176
98230914  
00016717  00000-0  10270-3 0  9082
2 25544  51
6422  19
1491 0000665 347
4559  12
6577 15
54709441  6195


Satellite: ISS
Catalog Number: 25544
Epoch time:      16176
98230914   =   yrday
fracday
Element set:     908
Inclination:       51
6422  deg
RA of node:        19
1491  deg
Eccentricity:     
0000665     
Arg of perigee:   347
4559  deg
Mean anomaly:      12
6577  deg
Mean motion:   15
54709441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             619
Checksum:              321


Coasting Arc #10 (Orbit 633)
---------------------------------------

Vector Time (GMT): 2016/177/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1059377
21                 A    =         6775710
15  meter
 Y    =       -4068694
51  meter          E    =           
0014773
 Z    =       -5326279
17                 I    =           51
71622
 XDOT =       7426
510086                 Wp   =           87
40348
 YDOT =       1870
591925  meter/sec      RA   =           13
84856  deg
 ZDOT =         48
948047                 TA   =          183
05852
                                          MA   =          183
06756
                                          Ha   =            220
084  n
mi
                                          Hp   =            213
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3475647
01                 X    =         1130668
20
 Y    =      -13348735
28  feet           Y    =        -4056448
78  meter
 Z    =      -17474669
19                 Z    =        -5320960
22
 XDOT =      24365
190572                 XDOT =        7404
802938
 YDOT =       6137
112615  feet/sec       YDOT =        1953
518734  meter/sec
 ZDOT =        160
590704                 ZDOT =          84
971327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11124990
53                 X    =         3390897
11
 Y    =        8206278
76  feet           Y    =         2501273
77  meter
 Z    =      -17450630
18                 Z    =        -5318952
08
 XDOT =     -13994
545169                 XDOT =       -4265
537367
 YDOT =      19641
074664  feet/sec       YDOT =        5986
599558  meter/sec
 ZDOT =        317
186866                 ZDOT =          96
678557


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   16177
94647990  
00016717  00000-0  10270-3 0  9096
2 25544  51
6434  14
3385 0000754 351
3101   8
8039 15
54695099  6343


Satellite: ISS
Catalog Number: 25544
Epoch time:      16177
94647990   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:        14
3385  deg
Eccentricity:     
0000754     
Arg of perigee:   351
3101  deg
Mean anomaly:       8
8039  deg
Mean motion:   15
54695099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             634
Checksum:              323


Coasting Arc #11 (Orbit 649)
---------------------------------------

Vector Time (GMT): 2016/178/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3027258
30                 A    =         6777168
44  meter
 Y    =        3490420
69  meter          E    =           
0006962
 Z    =        4954869
20                 I    =           51
68981
 XDOT =      -6802
586831                 Wp   =           51
18607
 YDOT =      -2799
983535  meter/sec      RA   =            8
84878  deg
 ZDOT =      -2177
398070                 TA   =           60
05355
                                          MA   =           59
98444
                                          Ha   =            220
136  n
mi
                                          Hp   =            213
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9931949
80                 X    =        -3090132
57
 Y    =       11451511
44  feet           Y    =         3456215
93  meter
 Z    =       16256132
54                 Z    =         4940011
16
 XDOT =     -22318
198264                 XDOT =       -6760
194321
 YDOT =      -9186
297687  feet/sec       YDOT =       -2875
817396  meter/sec
 ZDOT =      -7143
694455                 ZDOT =       -2210
340422

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7239946
35                 X    =        -2206735
65
 Y    =      -13397338
68  feet           Y    =        -4083508
83  meter
 Z    =       16190647
90                 Z    =         4934909
48
 XDOT =      15392
225218                 XDOT =        4691
550246
 YDOT =     -17149
077592  feet/sec       YDOT =       -5227
038850  meter/sec
 ZDOT =      -7286
658856                 ZDOT =       -2220
973619


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   16178
97491778  
00016717  00000-0  10270-3 0  9103
2 25544  51
6431   9
2081 0000879 359
9361    
1791 15
54751796  6501


Satellite: ISS
Catalog Number: 25544
Epoch time:      16178
97491778   =   yrday
fracday
Element set:     910
Inclination:       51
6431  deg
RA of node:         9
2081  deg
Eccentricity:     
0000879     
Arg of perigee:   359
9361  deg
Mean anomaly:        
1791  deg
Mean motion:   15
54751796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             650
Checksum:              328


Coasting Arc #12 (Orbit 664)
---------------------------------------

Vector Time (GMT): 2016/179/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4729695
98                 A    =         6780970
49  meter
 Y    =       -2821175
08  meter          E    =           
0006564
 Z    =       -3962653
34                 I    =           51
67104
 XDOT =       5477
057693                 Wp   =           97
99417
 YDOT =       3550
084711  meter/sec      RA   =            3
85489  deg
 ZDOT =       4014
594149                 TA   =          213
88664
                                          MA   =          213
92860
                                          Ha   =            220
130  n
mi
                                          Hp   =            213
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15517375
25                 X    =         4780140
38
 Y    =       -9255823
75  feet           Y    =        -2768002
11  meter
 Z    =      -13000831
15                 Z    =        -3939555
38
 XDOT =      17969
349387                 XDOT =        5417
451548
 YDOT =      11647
259549  feet/sec       YDOT =        3610
999234  meter/sec
 ZDOT =      13171
240645                 ZDOT =        4041
055786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3549881
29                 X    =         1082003
82
 Y    =       17789880
07  feet           Y    =         5422355
45  meter
 Z    =      -12899586
36                 Z    =        -3931793
92
 XDOT =     -15629
914071                 XDOT =       -4763
997809
 YDOT =      12740
991358  feet/sec       YDOT =        3883
454166  meter/sec
 ZDOT =      13285
797206                 ZDOT =        4049
510988


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   16179
93907259  
00016717  00000-0  10270-3 0  9117
2 25544  51
6436   4
3978 0000919   8
9752 351
1417 15
54749306  6651


Satellite: ISS
Catalog Number: 25544
Epoch time:      16179
93907259   =   yrday
fracday
Element set:     911
Inclination:       51
6436  deg
RA of node:         4
3978  deg
Eccentricity:     
0000919     
Arg of perigee:     8
9752  deg
Mean anomaly:     351
1417  deg
Mean motion:   15
54749306  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             665
Checksum:              332


Coasting Arc #13 (Orbit 680)
---------------------------------------

Vector Time (GMT): 2016/180/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5993831
43                 A    =         6785047
31  meter
 Y    =        2037056
72  meter          E    =           
0013761
 Z    =        2425209
59                 I    =           51
65184
 XDOT =      -3589
302164                 Wp   =          101
74700
 YDOT =      -4163
327413  meter/sec      RA   =          358
87162  deg
 ZDOT =      -5350
911824                 TA   =           51
11357
                                          MA   =           50
99091
                                          Ha   =            220
143  n
mi
                                          Hp   =            213
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19664801
26                 X    =        -6027945
47
 Y    =        6683256
97  feet           Y    =         1969838
75  meter
 Z    =        7956724
38                 Z    =         2396010
33
 XDOT =     -11775
925735                 XDOT =       -3516
487563
 YDOT =     -13659
210673  feet/sec       YDOT =       -4203
057788  meter/sec
 ZDOT =     -17555
484986                 ZDOT =       -5368
171287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -114337
84                 X    =          -34850
17
 Y    =      -20817599
37  feet           Y    =        -6345204
29  meter
 Z    =        7829066
27                 Z    =         2386299
40
 XDOT =      15127
179775                 XDOT =        4610
764395
 YDOT =      -6742
065202  feet/sec       YDOT =       -2054
981474  meter/sec
 ZDOT =     -17629
807878                 ZDOT =       -5373
565441


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   16180
96749447  
00016717  00000-0  10270-3 0  9126
2 25544  51
6427 359
2668 0000979  12
6991 347
4186 15
54771332  6815


Satellite: ISS
Catalog Number: 25544
Epoch time:      16180
96749447   =   yrday
fracday
Element set:     912
Inclination:       51
6427  deg
RA of node:       359
2668  deg
Eccentricity:     
0000979     
Arg of perigee:    12
6991  deg
Mean anomaly:     347
4186  deg
Mean motion:   15
54771332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             681
Checksum:              345


Coasting Arc #14 (Orbit 695)
---------------------------------------

Vector Time (GMT): 2016/181/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6649639
57                 A    =         6787257
60  meter
 Y    =       -1188538
26  meter          E    =           
0011769
 Z    =        -599610
57                 I    =           51
62846
 XDOT =       1356
854415                 Wp   =           38
29871
 YDOT =       4613
051235  meter/sec      RA   =          353
89634  deg
 ZDOT =       5975
348067                 TA   =          315
22586
                                          MA   =          315
32078
                                          Ha   =            220
082  n
mi
                                          Hp   =            213
533

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21816402
79                 X    =         6665348
55
 Y    =       -3899403
73  feet           Y    =        -1114089
66  meter
 Z    =       -1967226
29                 Z    =         -567270
15
 XDOT =       4451
622096                 XDOT =        1276
143520
 YDOT =      15134
682528  feet/sec       YDOT =        4627
772584  meter/sec
 ZDOT =      19604
160326                 ZDOT =        5981
743788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2817003
29                 X    =         -858622
60
 Y    =       21994561
33  feet           Y    =         6703942
29  meter
 Z    =       -1826067
88                 Z    =         -556585
49
 XDOT =     -14133
191561                 XDOT =       -4307
796788
 YDOT =       -201
381357  feet/sec       YDOT =         -61
381038  meter/sec
 ZDOT =      19631
049465                 ZDOT =        5983
543877


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   16181
93163111  
00016717  00000-0  10270-3 0  9133
2 25544  51
6438 354
4566 0000985  11
6036 348
5140 15
54795542  6964


Satellite: ISS
Catalog Number: 25544
Epoch time:      16181
93163111   =   yrday
fracday
Element set:     913
Inclination:       51
6438  deg
RA of node:       354
4566  deg
Eccentricity:     
0000985     
Arg of perigee:    11
6036  deg
Mean anomaly:     348
5140  deg
Mean motion:   15
54795542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             696
Checksum:              311


Coasting Arc #15 (Orbit 711)
---------------------------------------

Vector Time (GMT): 2016/182/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6646047
38                 A    =         6786647
41  meter
 Y    =         216578
43  meter          E    =           
0008099
 Z    =       -1342704
96                 I    =           51
59227
 XDOT =       1009
721431                 Wp   =          136
00424
 YDOT =      -4894
758888  meter/sec      RA   =          348
92159  deg
 ZDOT =      -5814
161321                 TA   =           58
62634
                                          MA   =           58
54713
                                          Ha   =            220
104  n
mi
                                          Hp   =            213
522

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21804617
39                 X    =        -6641452
97
 Y    =         710559
15  feet           Y    =          142283
75  meter
 Z    =       -4405200
01                 Z    =        -1374978
69
 XDOT =       3312
734354                 XDOT =        1092
623567
 YDOT =     -16058
920236  feet/sec       YDOT =       -4883
003264  meter/sec
 ZDOT =     -19075
332417                 ZDOT =       -5809
055574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5482300
71                 X    =         1671005
26
 Y    =      -21086289
02  feet           Y    =        -6427100
89  meter
 Z    =       -4545856
93                 Z    =        -1385577
19
 XDOT =      12893
878217                 XDOT =        3930
054081
 YDOT =       7441
284376  feet/sec       YDOT =        2268
103478  meter/sec
 ZDOT =     -19052
049647                 ZDOT =       -5807
064732


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   16182
96003568  
00016717  00000-0  10270-3 0  9147
2 25544  51
6416 349
3252 0001015  17
7491 342
3698 15
54769801  7120


Satellite: ISS
Catalog Number: 25544
Epoch time:      16182
96003568   =   yrday
fracday
Element set:     914
Inclination:       51
6416  deg
RA of node:       349
3252  deg
Eccentricity:     
0001015     
Arg of perigee:    17
7491  deg
Mean anomaly:     342
3698  deg
Mean motion:   15
54769801  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             712
Checksum:              311


Coasting Arc #16 (Orbit 727)
---------------------------------------

Vector Time (GMT): 2016/183/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 891443
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5982787
70                 A    =         6783254
58  meter
 Y    =         818954
84  meter          E    =           
0013312
 Z    =        3075834
26                 I    =           51
54936
 XDOT =      -3203
803031                 Wp   =           79
96408
 YDOT =       4966
038280  meter/sec      RA   =          343
93781  deg
 ZDOT =       4893
697109                 TA   =          315
45527
                                          MA   =          315
56220
                                          Ha   =            219
967  n
mi
                                          Hp   =            213
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19628568
58                 X    =         5958244
22
 Y    =        2686859
72  feet           Y    =          885720
71  meter
 Z    =       10091319
76                 Z    =         3104837
64
 XDOT =     -10511
164800                 XDOT =       -3282
867869
 YDOT =      16292
776508  feet/sec       YDOT =        4929
768467  meter/sec
 ZDOT =      16055
436709                 ZDOT =        4877
942483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7804162
61                 X    =        -2378708
76
 Y    =       18139246
59  feet           Y    =         5528842
36  meter
 Z    =       10217506
21                 Z    =         3114295
89
 XDOT =     -11553
495850                 XDOT =       -3521
505535
 YDOT =     -14003
998070  feet/sec       YDOT =       -4268
418612  meter/sec
 ZDOT =      15985
744664                 ZDOT =        4872
454973


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   16183
98843048  
00016717  00000-0  10270-3 0  9156
2 25544  51
6411 344
1936 0001100  11
0349 349
0828 15
54802532  7286


Satellite: ISS
Catalog Number: 25544
Epoch time:      16183
98843048   =   yrday
fracday
Element set:     915
Inclination:       51
6411  deg
RA of node:       344
1936  deg
Eccentricity:     
0001100     
Arg of perigee:    11
0349  deg
Mean anomaly:     349
0828  deg
Mean motion:   15
54802532  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             728
Checksum:              296
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