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

 
Date: August 19th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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


237/06:36:20 931 0 4 1 1 1 1
N/A 0 9 -0 0 221 6
000/00:02:41 861 0 3 0 0 215 1

242/05:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 215 7

Coasting Arc #1 (Orbit 3112)
---------------------------------------

Vector Time (GMT): 2017/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3178453
40                 A    =         6780151
48  meter
 Y    =       -3808704
55  meter          E    =           
0010434
 Z    =        4612597
31                 I    =           52
00400
 XDOT =       3137
782321                 Wp   =           93
42065
 YDOT =      -6308
785821  meter/sec      RA   =           96
73572  deg
 ZDOT =      -3041
794277                 TA   =           26
80129
                                          MA   =           26
74741
                                          Ha   =            222
366  n
mi
                                          Hp   =            213
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10427996
73                 X    =        -3158032
82
 Y    =      -12495749
85  feet           Y    =        -3844134
10  meter
 Z    =       15133193
27                 Z    =         4597206
99
 XDOT =      10294
561420                 XDOT =        3222
871074
 YDOT =     -20698
116210  feet/sec       YDOT =       -6273
221184  meter/sec
 ZDOT =      -9979
640017                 ZDOT =       -3026
345463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1231032
11                 X    =          375218
59
 Y    =       16291476
63  feet           Y    =         4965642
08  meter
 Z    =       15065615
42                 Z    =         4591999
58
 XDOT =     -19321
254081                 XDOT =       -5889
118244
 YDOT =      10640
634615  feet/sec       YDOT =        3243
265431  meter/sec
 ZDOT =      -9910
219604                 ZDOT =       -3020
634935


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   17228
54286976  
00016717  00000-0  10270-3 0  9004
2 25544  51
6416  97
4490 0004886 146
9684 213
1774 15
54202015 31130


Satellite: ISS
Catalog Number: 25544
Epoch time:      17228
54286976   =   yrday
fracday
Element set:     900
Inclination:       51
6416  deg
RA of node:        97
4490  deg
Eccentricity:     
0004886     
Arg of perigee:   146
9684  deg
Mean anomaly:     213
1774  deg
Mean motion:   15
54202015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3113
Checksum:              318


Coasting Arc #2 (Orbit 3127)
---------------------------------------

Vector Time (GMT): 2017/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2594761
72                 A    =         6784015
31  meter
 Y    =        5188985
55  meter          E    =           
0008842
 Z    =       -3527398
46                 I    =           52
01861
 XDOT =      -3699
792088                 Wp   =          122
20252
 YDOT =       4934
391421  meter/sec      RA   =           91
77295  deg
 ZDOT =       4540
889653                 TA   =          196
56550
                                          MA   =          196
59440
                                          Ha   =            222
271  n
mi
                                          Hp   =            213
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8512997
77                 X    =         2553678
45
 Y    =       17024230
81  feet           Y    =         5217772
32  meter
 Z    =      -11572829
60                 Z    =        -3514893
70
 XDOT =     -12138
425484                 XDOT =       -3776
751964
 YDOT =      16188
948230  feet/sec       YDOT =        4892
587407  meter/sec
 ZDOT =      14897
931932                 ZDOT =        4522
730601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2665541
74                 X    =          812457
12
 Y    =      -18879899
77  feet           Y    =        -5754593
45  meter
 Z    =      -11518256
05                 Z    =        -3510764
44
 XDOT =      17911
523832                 XDOT =        5459
432464
 YDOT =      -6503
078519  feet/sec       YDOT =       -1982
138333  meter/sec
 ZDOT =      14816
705731                 ZDOT =        4516
131907


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   17229
50738474  
00016717  00000-0  10270-3 0  9017
2 25544  51
6409  92
6408 0004965 151
0911 209
0517 15
54161015 31285


Satellite: ISS
Catalog Number: 25544
Epoch time:      17229
50738474   =   yrday
fracday
Element set:     901
Inclination:       51
6409  deg
RA of node:        92
6408  deg
Eccentricity:     
0004965     
Arg of perigee:   151
0911  deg
Mean anomaly:     209
0517  deg
Mean motion:   15
54161015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3128
Checksum:              296


Coasting Arc #3 (Orbit 3143)
---------------------------------------

Vector Time (GMT): 2017/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1936339
78                 A    =         6787442
64  meter
 Y    =       -6166729
16  meter          E    =           
0017803
 Z    =        2039113
76                 I    =           52
03114
 XDOT =       4192
771393                 Wp   =          121
99595
 YDOT =      -3173
582558  meter/sec      RA   =           86
82069  deg
 ZDOT =      -5589
784615                 TA   =           35
56903
                                          MA   =           35
45049
                                          Ha   =            222
198  n
mi
                                          Hp   =            213
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6352820
79                 X    =        -1877142
73
 Y    =      -20232051
06  feet           Y    =        -6188051
68  meter
 Z    =        6690005
79                 Z    =         2029851
43
 XDOT =      13755
811657                 XDOT =        4255
099645
 YDOT =     -10412
016265  feet/sec       YDOT =       -3126
347530  meter/sec
 ZDOT =     -18339
188370                 ZDOT =       -5569
266413

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5947301
44                 X    =        -1812737
48
 Y    =       20368064
68  feet           Y    =         6208186
12  meter
 Z    =        6649958
34                 Z    =         2026907
30
 XDOT =     -15838
598863                 XDOT =       -4827
604933
 YDOT =       1361
396403  feet/sec       YDOT =         414
953624  meter/sec
 ZDOT =     -18247
778946                 ZDOT =       -5561
923023


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   17230
53619678  
00016717  00000-0  10270-3 0  9027
2 25544  51
6418  87
5119 0004855 154
3258 205
8136 15
54179596 31447


Satellite: ISS
Catalog Number: 25544
Epoch time:      17230
53619678   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:        87
5119  deg
Eccentricity:     
0004855     
Arg of perigee:   154
3258  deg
Mean anomaly:     205
8136  deg
Mean motion:   15
54179596  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3144
Checksum:              328


Coasting Arc #4 (Orbit 3158)
---------------------------------------

Vector Time (GMT): 2017/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1244653
56                 A    =         6789172
87  meter
 Y    =        6661496
08  meter          E    =           
0010233
 Z    =        -372395
82                 I    =           52
03244
 XDOT =      -4582
791855                 Wp   =           67
83961
 YDOT =       1185
673602  meter/sec      RA   =           81
87448  deg
 ZDOT =       6028
350515                 TA   =          288
16943
                                          MA   =          288
28082
                                          Ha   =            222
121  n
mi
                                          Hp   =            213
799

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4083509
06                 X    =         1171879
33
 Y    =       21855302
08  feet           Y    =         6675007
73  meter
 Z    =       -1221771
05                 Z    =         -366526
51
 XDOT =     -15035
406350                 XDOT =       -4624
991996
 YDOT =       3890
005256  feet/sec       YDOT =        1134
189726  meter/sec
 ZDOT =      19778
052870                 ZDOT =        6005
986656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8413300
52                 X    =         2564374
00
 Y    =      -20581689
52  feet           Y    =        -6273298
97  meter
 Z    =       -1196842
01                 Z    =         -364797
44
 XDOT =      13351
043932                 XDOT =        4069
398191
 YDOT =       4339
691689  feet/sec       YDOT =        1322
738027  meter/sec
 ZDOT =      19678
778071                 ZDOT =        5998
091556


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   17231
50070569  
00016717  00000-0  10270-3 0  9036
2 25544  51
6402  82
7028 0004861 158
1485 201
9876 15
54160898 31596


Satellite: ISS
Catalog Number: 25544
Epoch time:      17231
50070569   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:        82
7028  deg
Eccentricity:     
0004861     
Arg of perigee:   158
1485  deg
Mean anomaly:     201
9876  deg
Mean motion:   15
54160898  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3159
Checksum:              316


Coasting Arc #5 (Orbit 3174)
---------------------------------------

Vector Time (GMT): 2017/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -435986
61                 A    =         6788460
07  meter
 Y    =       -6626765
14  meter          E    =           
0013390
 Z    =       -1375517
60                 I    =           52
02340
 XDOT =       4888
383310                 Wp   =          149
73608
 YDOT =        883
948622  meter/sec      RA   =           76
93110  deg
 ZDOT =      -5843
867925                 TA   =           45
17365
                                          MA   =           45
06490
                                          Ha   =            222
086  n
mi
                                          Hp   =            213
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1430402
25                 X    =         -355170
51
 Y    =      -21741355
45  feet           Y    =        -6631188
79  meter
 Z    =       -4512853
01                 Z    =        -1377439
04
 XDOT =      16038
002987                 XDOT =        4906
521510
 YDOT =       2900
093903  feet/sec       YDOT =         938
715164  meter/sec
 ZDOT =     -19172
795029                 ZDOT =       -5820
078126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10283620
44                 X    =        -3134447
51
 Y    =       19207096
52  feet           Y    =         5854323
02  meter
 Z    =       -4520290
22                 Z    =        -1377784
46
 XDOT =     -10799
247218                 XDOT =       -3291
610552
 YDOT =     -10241
782698  feet/sec       YDOT =       -3121
695366  meter/sec
 ZDOT =     -19067
533910                 ZDOT =       -5811
784336


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   17232
52951416  
00016717  00000-0  10270-3 0  9049
2 25544  51
6393  77
5743 0004939 163
1291 197
0027 15
54150129 31755


Satellite: ISS
Catalog Number: 25544
Epoch time:      17232
52951416   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:        77
5743  deg
Eccentricity:     
0004939     
Arg of perigee:   163
1291  deg
Mean anomaly:     197
0027  deg
Mean motion:   15
54150129  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3175
Checksum:              308


Coasting Arc #6 (Orbit 3190)
---------------------------------------

Vector Time (GMT): 2017/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -428698
61                 A    =         6785495
81  meter
 Y    =        6097990
51  meter          E    =           
0014411
 Z    =        2936826
04                 I    =           52
00528
 XDOT =      -5053
468739                 Wp   =          101
85718
 YDOT =      -2796
241857  meter/sec      RA   =           71
98013  deg
 ZDOT =       5044
675520                 TA   =          291
47514
                                          MA   =          291
62876
                                          Ha   =            221
900  n
mi
                                          Hp   =            214
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1406491
49                 X    =         -511121
46
 Y    =       20006530
54  feet           Y    =         6092735
78  meter
 Z    =        9635256
04                 Z    =         2934543
16
 XDOT =     -16579
621846                 XDOT =       -5046
328898
 YDOT =      -9174
021841  feet/sec       YDOT =       -2852
713054  meter/sec
 ZDOT =      16550
772702                 ZDOT =        5020
145296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11525789
76                 X    =         3513060
72
 Y    =      -16419793
87  feet           Y    =        -5004753
17  meter
 Z    =        9624145
72                 Z    =         2933439
62
 XDOT =       8421
105860                 XDOT =        2566
753066
 YDOT =      15594
327530  feet/sec       YDOT =        4753
151031  meter/sec
 ZDOT =      16442
542964                 ZDOT =        5011
687095


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   17233
55831929  
00016717  00000-0  10270-3 0  9050
2 25544  51
6390  72
4442 0004937 168
7220 191
4044 15
54193401 31918


Satellite: ISS
Catalog Number: 25544
Epoch time:      17233
55831929   =   yrday
fracday
Element set:     905
Inclination:       51
6390  deg
RA of node:        72
4442  deg
Eccentricity:     
0004937     
Arg of perigee:   168
7220  deg
Mean anomaly:     191
4044  deg
Mean motion:   15
54193401  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3191
Checksum:              302


Coasting Arc #7 (Orbit 3205)
---------------------------------------

Vector Time (GMT): 2017/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1421124
47                 A    =         6781651
09  meter
 Y    =       -5113945
19  meter          E    =           
0008704
 Z    =       -4227150
62                 I    =           51
98016
 XDOT =       5026
334706                 Wp   =          103
54548
 YDOT =       4446
658229  meter/sec      RA   =           67
01877  deg
 ZDOT =      -3698
057737                 TA   =          128
71397
                                          MA   =          128
63612
                                          Ha   =            221
921  n
mi
                                          Hp   =            214
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4662481
86                 X    =         1498737
39
 Y    =      -16778035
39  feet           Y    =        -5097619
51  meter
 Z    =      -13868604
41                 Z    =        -4220058
54
 XDOT =      16490
599430                 XDOT =        4994
200453
 YDOT =      14588
773717  feet/sec       YDOT =        4502
686218  meter/sec
 ZDOT =     -12132
735358                 ZDOT =       -3673
720140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12480588
79                 X    =        -3804083
46
 Y    =       12180719
61  feet           Y    =         3712683
34  meter
 Z    =      -13836342
37                 Z    =        -4217317
15
 XDOT =      -6211
467338                 XDOT =       -1893
255244
 YDOT =     -19993
342133  feet/sec       YDOT =       -6093
970682  meter/sec
 ZDOT =     -12025
634122                 ZDOT =       -3665
413280


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   17234
52282373  
00016717  00000-0  10270-3 0  9062
2 25544  51
6379  67
6345 0004882 169
0676 191
0584 15
54177169 32066


Satellite: ISS
Catalog Number: 25544
Epoch time:      17234
52282373   =   yrday
fracday
Element set:     906
Inclination:       51
6379  deg
RA of node:        67
6345  deg
Eccentricity:     
0004882     
Arg of perigee:   169
0676  deg
Mean anomaly:     191
0584  deg
Mean motion:   15
54177169  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3206
Checksum:              332


Coasting Arc #8 (Orbit 3221)
---------------------------------------

Vector Time (GMT): 2017/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2437068
92                 A    =         6778597
46  meter
 Y    =        3820101
05  meter          E    =           
0009739
 Z    =        5039214
47                 I    =           51
95541
 XDOT =      -4767
410083                 Wp   =          145
78216
 YDOT =      -5671
624459  meter/sec      RA   =           62
04748  deg
 ZDOT =       1984
194549                 TA   =          284
98748
                                          MA   =          285
09526
                                          Ha   =            221
946  n
mi
                                          Hp   =            214
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7995632
93                 X    =        -2504082
85
 Y    =       12533139
93  feet           Y    =         3792473
79  meter
 Z    =       16532855
88                 Z    =         5027213
06
 XDOT =     -15641
109197                 XDOT =       -4713
272256
 YDOT =     -18607
691795  feet/sec       YDOT =       -5724
634025  meter/sec
 ZDOT =       6509
824636                 ZDOT =        1961
168234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13151630
98                 X    =         4008617
12
 Y    =       -7058363
79  feet           Y    =        -2151389
28  meter
 Z    =       16479052
43                 Z    =         5022815
18
 XDOT =       4225
365945                 XDOT =        1287
891540
 YDOT =      22909
944598  feet/sec       YDOT =        6982
951114  meter/sec
 ZDOT =       6408
743791                 ZDOT =        1953
385108


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   17235
55162709  
00016717  00000-0  10270-3 0  9077
2 25544  51
6375  62
5051 0004883 172
7385 187
3840 15
54135756 32226


Satellite: ISS
Catalog Number: 25544
Epoch time:      17235
55162709   =   yrday
fracday
Element set:     907
Inclination:       51
6375  deg
RA of node:        62
5051  deg
Eccentricity:     
0004883     
Arg of perigee:   172
7385  deg
Mean anomaly:     187
3840  deg
Mean motion:   15
54135756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3222
Checksum:              317


Coasting Arc #9 (Orbit 3236)
---------------------------------------

Vector Time (GMT): 2017/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925218
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3488755
29                 A    =         6777207
12  meter
 Y    =       -2311508
65  meter          E    =           
0016018
 Z    =       -5343765
78                 I    =           51
93482
 XDOT =       4190
190115                 Wp   =          107
93885
 YDOT =       6409
124073  meter/sec      RA   =           57
06779  deg
 ZDOT =        -41
616075                 TA   =          161
69451
                                          MA   =          161
63679
                                          Ha   =            221
796  n
mi
                                          Hp   =            214
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11446047
53                 X    =         3540301
02
 Y    =       -7583689
79  feet           Y    =        -2272207
26  meter
 Z    =      -17532039
98                 Z    =        -5326693
28
 XDOT =      13747
342896                 XDOT =        4118
412316
 YDOT =      21027
309951  feet/sec       YDOT =        6455
580295  meter/sec
 ZDOT =       -136
535679                 ZDOT =         -21
436543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13766463
90                 X    =        -4196018
20
 Y    =        1291765
36  feet           Y    =          393730
08  meter
 Z    =      -17456018
86                 Z    =        -5320594
55
 XDOT =      -2212
576455                 XDOT =        -674
393303
 YDOT =     -24012
774367  feet/sec       YDOT =       -7319
093627  meter/sec
 ZDOT =        -48
201702                 ZDOT =         -14
691879


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   17236
51612648  
00016717  00000-0  10270-3 0  9087
2 25544  51
6374  57
6957 0005039 176
1579 183
9613 15
54180629 32377


Satellite: ISS
Catalog Number: 25544
Epoch time:      17236
51612648   =   yrday
fracday
Element set:     908
Inclination:       51
6374  deg
RA of node:        57
6957  deg
Eccentricity:     
0005039     
Arg of perigee:   176
1579  deg
Mean anomaly:     183
9613  deg
Mean motion:   15
54180629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3237
Checksum:              338


Coasting Arc #10 (Orbit 3248)
---------------------------------------

Vector Time (GMT): 2017/237/06:37:41
861
Vector Time (MET): N/A
Weight (LBS)     : 925107
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4764109
73                 A    =         6779967
36  meter
 Y    =          45871
53  meter          E    =           
0012858
 Z    =       -4835731
00                 I    =           51
93286
 XDOT =       2542
402033                 Wp   =          128
33506
 YDOT =       6752
591799  meter/sec      RA   =           53
19854  deg
 ZDOT =       2565
657174                 TA   =          166
86734
                                          MA   =          166
83383
                                          Ha   =            221
617  n
mi
                                          Hp   =            215
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15630281
26                 X    =         4786732
13
 Y    =         150497
14  feet           Y    =           99273
12  meter
 Z    =      -15865259
18                 Z    =        -4812533
67
 XDOT =       8341
214020                 XDOT =        2454
241198
 YDOT =      22154
172570  feet/sec       YDOT =        6780
529954  meter/sec
 ZDOT =       8417
510412                 ZDOT =        2577
792567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4930822
47                 X    =         1502914
69
 Y    =      -14942067
26  feet           Y    =        -4554342
10  meter
 Z    =      -15762499
99                 Z    =        -4804410
00
 XDOT =      22536
080026                 XDOT =        6868
997192
 YDOT =      -1509
352033  feet/sec       YDOT =        -460
050500  meter/sec
 ZDOT =       8470
139442                 ZDOT =        2581
698502


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   17237
28772544  
00016717  00000-0  10270-3 0  9095
2 25544  51
6423  53
8527 0004520 190
0459 170
0604 15
53991232 32498


Satellite: ISS
Catalog Number: 25544
Epoch time:      17237
28772544   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:        53
8527  deg
Eccentricity:     
0004520     
Arg of perigee:   190
0459  deg
Mean anomaly:     170
0604  deg
Mean motion:   15
53991232  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3249
Checksum:              307


Coasting Arc #11 (Orbit 3264)
---------------------------------------

Vector Time (GMT): 2017/238/06:37:41
861
Vector Time (MET): N/A
Weight (LBS)     : 925107
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5363995
13                 A    =         6783417
79  meter
 Y    =       -1436684
89  meter          E    =           
0010642
 Z    =        3884903
21                 I    =           51
92392
 XDOT =      -1306
422675                 Wp   =          104
43021
 YDOT =      -6328
293087  meter/sec      RA   =           48
22963  deg
 ZDOT =      -4137
232237                 TA   =           28
83336
                                          MA   =           28
77460
                                          Ha   =            221
675  n
mi
                                          Hp   =            215
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17598409
21                 X    =        -5366401
94
 Y    =       -4713533
11  feet           Y    =        -1496681
89  meter
 Z    =       12745745
44                 Z    =         3858840
98
 XDOT =      -4286
163631                 XDOT =       -1215
464378
 YDOT =     -20762
116426  feet/sec       YDOT =       -6342
394142  meter/sec
 ZDOT =     -13573
596577                 ZDOT =       -4143
356981

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9603901
25                 X    =        -2927269
10
 Y    =       15575945
24  feet           Y    =         4747548
11  meter
 Z    =       12630535
95                 Z    =         3849787
36
 XDOT =     -19956
628452                 XDOT =       -6082
780352
 YDOT =      -1258
578464  feet/sec       YDOT =        -383
614716  meter/sec
 ZDOT =     -13599
657398                 ZDOT =       -4145
175575


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   17238
31665041  
00016717  00000-0  10270-3 0  9105
2 25544  51
6421  48
7252 0004415 192
1859 167
9187 15
53997409 32655


Satellite: ISS
Catalog Number: 25544
Epoch time:      17238
31665041   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        48
7252  deg
Eccentricity:     
0004415     
Arg of perigee:   192
1859  deg
Mean anomaly:     167
9187  deg
Mean motion:   15
53997409  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3265
Checksum:              324


Coasting Arc #12 (Orbit 3279)
---------------------------------------

Vector Time (GMT): 2017/239/06:37:41
861
Vector Time (MET): N/A
Weight (LBS)     : 925107
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5714142
83                 A    =         6786963
33  meter
 Y    =        2611816
20  meter          E    =           
0002817
 Z    =       -2570773
58                 I    =           51
91358
 XDOT =       -156
711855                 Wp   =          108
37103
 YDOT =       5543
176660  meter/sec      RA   =           43
26827  deg
 ZDOT =       5287
223300                 TA   =          222
86853
                                          MA   =          222
89049
                                          Ha   =            221
385  n
mi
                                          Hp   =            215
287

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18747187
77                 X    =         5696999
65
 Y    =        8568950
78  feet           Y    =         2675619
61  meter
 Z    =       -8434296
51                 Z    =        -2543057
94
 XDOT =       -514
146507                 XDOT =        -244
368141
 YDOT =      18186
275131  feet/sec       YDOT =        5540
934442  meter/sec
 ZDOT =      17346
533136                 ZDOT =        5286
248768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13349715
67                 X    =         4068993
34
 Y    =      -15770781
12  feet           Y    =        -4806934
09  meter
 Z    =       -8311972
02                 Z    =        -2533489
07
 XDOT =      16184
604954                 XDOT =        4933
067590
 YDOT =       4567
119349  feet/sec       YDOT =        1392
057977  meter/sec
 ZDOT =      17341
269084                 ZDOT =        5285
618817


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   17239
28126549  
00016717  00000-0  10270-3 0  9118
2 25544  51
6423  43
9176 0004466 197
7916 162
3081 15
54005582 32802


Satellite: ISS
Catalog Number: 25544
Epoch time:      17239
28126549   =   yrday
fracday
Element set:     911
Inclination:       51
6423  deg
RA of node:        43
9176  deg
Eccentricity:     
0004466     
Arg of perigee:   197
7916  deg
Mean anomaly:     162
3081  deg
Mean motion:   15
54005582  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3280
Checksum:              314


Coasting Arc #13 (Orbit 3295)
---------------------------------------

Vector Time (GMT): 2017/240/06:37:41
861
Vector Time (MET): N/A
Weight (LBS)     : 925107
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5705807
40                 A    =         6789436
16  meter
 Y    =       -3529318
60  meter          E    =           
0015279
 Z    =         979755
31                 I    =           51
89750
 XDOT =       1775
250106                 Wp   =          141
29241
 YDOT =      -4527
961314  meter/sec      RA   =           38
31445  deg
 ZDOT =      -5934
096046                 TA   =           28
12626
                                          MA   =           28
04381
                                          Ha   =            221
430  n
mi
                                          Hp   =            215
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18719840
54                 X    =        -5670676
71
 Y    =      -11579129
28  feet           Y    =        -3592928
34  meter
 Z    =        3214420
30                 Z    =          952123
85
 XDOT =       5824
311372                 XDOT =        1854
575892
 YDOT =     -14855
516123  feet/sec       YDOT =       -4507
666053  meter/sec
 ZDOT =     -19468
819050                 ZDOT =       -5925
279530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15972011
21                 X    =        -4868269
02
 Y    =       15171407
92  feet           Y    =         4624245
13  meter
 Z    =        3092636
73                 Z    =          942635
67
 XDOT =     -11743
787391                 XDOT =       -3579
506397
 YDOT =      -8376
435099  feet/sec       YDOT =       -2553
137418  meter/sec
 ZDOT =     -19428
985981                 ZDOT =       -5921
954927


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   17240
31018785  
00016717  00000-0  10270-3 0  9127
2 25544  51
6428  38
7902 0004569 200
6274 159
4695 15
53963723 32965


Satellite: ISS
Catalog Number: 25544
Epoch time:      17240
31018785   =   yrday
fracday
Element set:     912
Inclination:       51
6428  deg
RA of node:        38
7902  deg
Eccentricity:     
0004569     
Arg of perigee:   200
6274  deg
Mean anomaly:     159
4695  deg
Mean motion:   15
53963723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3296
Checksum:              326


Coasting Arc #14 (Orbit 3311)
---------------------------------------

Vector Time (GMT): 2017/241/06:37:41
861
Vector Time (MET): N/A
Weight (LBS)     : 925107
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5326594
44                 A    =         6789431
44  meter
 Y    =        4148467
03  meter          E    =           
0009472
 Z    =         682580
19                 I    =           51
87175
 XDOT =      -3405
026921                 Wp   =           63
97569
 YDOT =       3378
118613  meter/sec      RA   =           33
36081  deg
 ZDOT =       5980
332094                 TA   =          303
37096
                                          MA   =          303
46156
                                          Ha   =            221
112  n
mi
                                          Hp   =            215
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17475703
53                 X    =         5276493
66
 Y    =       13610456
13  feet           Y    =         4207752
54  meter
 Z    =        2239436
31                 Z    =          708333
18
 XDOT =     -11171
348165                 XDOT =       -3471
598312
 YDOT =      11083
066317  feet/sec       YDOT =        3339
669335  meter/sec
 ZDOT =      19620
512121                 ZDOT =        5963
629729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17377218
93                 X    =         5296576
33
 Y    =      -13717014
41  feet           Y    =        -4180945
99  meter
 Z    =        2352781
93                 Z    =          717127
93
 XDOT =       7074
582856                 XDOT =        2156
332855
 YDOT =      12347
192452  feet/sec       YDOT =        3763
424259  meter/sec
 ZDOT =      19545
945909                 ZDOT =        5957
604313


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   17241
33910382  
00016717  00000-0  10270-3 0  9135
2 25544  51
6426  33
6613 0004408 207
1231 152
9692 15
54018278 33124


Satellite: ISS
Catalog Number: 25544
Epoch time:      17241
33910382   =   yrday
fracday
Element set:     913
Inclination:       51
6426  deg
RA of node:        33
6613  deg
Eccentricity:     
0004408     
Arg of perigee:   207
1231  deg
Mean anomaly:     152
9692  deg
Mean motion:   15
54018278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3312
Checksum:              283


Coasting Arc #15 (Orbit 3325)
---------------------------------------

Vector Time (GMT): 2017/242/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925107
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4885666
25                 A    =         6781208
98  meter
 Y    =       -1373807
07  meter          E    =           
0009684
 Z    =       -4507118
18                 I    =           51
81709
 XDOT =       4469
972192                 Wp   =          136
48671
 YDOT =       5321
315594  meter/sec      RA   =           28
59476  deg
 ZDOT =       3220
688950                 TA   =          165
86592
                                          MA   =          165
83880
                                          Ha   =            221
032  n
mi
                                          Hp   =            215
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16029088
73                 X    =         4922558
69
 Y    =       -4507241
04  feet           Y    =        -1318966
12  meter
 Z    =      -14787133
14                 Z    =        -4483295
56
 XDOT =      14665
263097                 XDOT =        4394
491146
 YDOT =      17458
384496  feet/sec       YDOT =        5370
879952  meter/sec
 ZDOT =      10566
564797                 ZDOT =        3242
219066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4091014
17                 X    =         1246941
12
 Y    =      -16236590
81  feet           Y    =        -4948912
88  meter
 Z    =      -14681380
59                 Z    =        -4474884
80
 XDOT =      21217
607330                 XDOT =        6467
126714
 YDOT =      -4301
950999  feet/sec       YDOT =       -1311
234665  meter/sec
 ZDOT =      10660
992914                 ZDOT =        3249
470640


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   17242
23940701  
00016717  00000-0  10270-3 0  9144
2 25544  51
6422  29
1747 0004370 210
2574 149
8327 15
54007055 33267


Satellite: ISS
Catalog Number: 25544
Epoch time:      17242
23940701   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:        29
1747  deg
Eccentricity:     
0004370     
Arg of perigee:   210
2574  deg
Mean anomaly:     149
8327  deg
Mean motion:   15
54007055  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3326
Checksum:              285


Coasting Arc #16 (Orbit 3341)
---------------------------------------

Vector Time (GMT): 2017/243/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925107
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5860354
29                 A    =         6784872
06  meter
 Y    =         347622
92  meter          E    =           
0010824
 Z    =        3388807
02                 I    =           51
80061
 XDOT =      -3008
523576                 Wp   =          110
02574
 YDOT =      -5309
175900  meter/sec      RA   =           23
62118  deg
 ZDOT =      -4649
691417                 TA   =           30
46849
                                          MA   =           30
40564
                                          Ha   =            221
014  n
mi
                                          Hp   =            215
642

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19226884
15                 X    =        -5880267
02
 Y    =        1140495
14  feet           Y    =          281977
23  meter
 Z    =       11118133
27                 Z    =         3360291
02
 XDOT =      -9870
484174                 XDOT =       -2926
345573
 YDOT =     -17418
556102  feet/sec       YDOT =       -5342
359934  meter/sec
 ZDOT =     -15254
893102                 ZDOT =       -4664
106028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8290149
45                 X    =        -2526837
55
 Y    =       17465421
30  feet           Y    =         5323460
41  meter
 Z    =       10991777
45                 Z    =         3350293
77
 XDOT =     -18698
322728                 XDOT =       -5699
248768
 YDOT =        782
398292  feet/sec       YDOT =         238
474999  meter/sec
 ZDOT =     -15317
801315                 ZDOT =       -4668
865841


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   17243
26832188  
00016717  00000-0  10270-3 0  9158
2 25544  51
6425  24
0471 0004288 214
0883 145
9995 15
54023397 33424


Satellite: ISS
Catalog Number: 25544
Epoch time:      17243
26832188   =   yrday
fracday
Element set:     915
Inclination:       51
6425  deg
RA of node:        24
0471  deg
Eccentricity:     
0004288     
Arg of perigee:   214
0883  deg
Mean anomaly:     145
9995  deg
Mean motion:   15
54023397  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3342
Checksum:              316
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