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

 
Date: December 21st 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


361/06:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 5

362/01:03:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 4

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

Coasting Arc #1 (Orbit 1074)
---------------------------------------

Vector Time (GMT): 2017/354/15:32:15
084
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3285745
60                 A    =         6780895
45  meter
 Y    =       -3968036
13  meter          E    =           
0006964
 Z    =        4405973
86                 I    =           51
57339
 XDOT =       6662
644995                 Wp   =          121
64797
 YDOT =      -1787
790731  meter/sec      RA   =          187
64776  deg
 ZDOT =       3351
082459                 TA   =          294
41461
                                          MA   =          294
48725
                                          Ha   =            219
848  n
mi
                                          Hp   =            215
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10780005
25                 X    =        -3262531
70
 Y    =      -13018491
23  feet           Y    =        -4004650
27  meter
 Z    =       14455294
80                 Z    =         4390068
74
 XDOT =      21859
071507                 XDOT =        6665
863539
 YDOT =      -5865
455154  feet/sec       YDOT =       -1713
266855  meter/sec
 ZDOT =      10994
365023                 ZDOT =        3383
454985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -437377
74                 X    =         -133312
73
 Y    =      -16956440
09  feet           Y    =        -5168322
94  meter
 Z    =       14385166
50                 Z    =         4384598
75
 XDOT =      19480
214783                 XDOT =        5937
569466
 YDOT =       8967
871681  feet/sec       YDOT =        2733
407288  meter/sec
 ZDOT =      11138
463331                 ZDOT =        3395
003623


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   17354
70177205  
00016717  00000-0  10270-3 0  9006
2 25544  51
6366 188
5191 0003004 261
1478  98
9334 15
54223743 10753


Satellite: ISS
Catalog Number: 25544
Epoch time:      17354
70177205   =   yrday
fracday
Element set:     900
Inclination:       51
6366  deg
RA of node:       188
5191  deg
Eccentricity:     
0003004     
Arg of perigee:   261
1478  deg
Mean anomaly:      98
9334  deg
Mean motion:   15
54223743  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1075
Checksum:              303


Coasting Arc #2 (Orbit 1089)
---------------------------------------

Vector Time (GMT): 2017/355/15:32:15
084
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1573412
58                 A    =         6777983
76  meter
 Y    =        4147202
52  meter          E    =           
0010667
 Z    =       -5134607
59                 I    =           51
59721
 XDOT =      -7446
468841                 Wp   =           75
82935
 YDOT =        893
567541  meter/sec      RA   =          182
64914  deg
 ZDOT =      -1560
280312                 TA   =          179
10707
                                          MA   =          179
10517
                                          Ha   =            219
811  n
mi
                                          Hp   =            215
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5162114
77                 X    =         1551861
73
 Y    =       13606307
49  feet           Y    =         4164677
52  meter
 Z    =      -16845825
42                 Z    =        -5127016
42
 XDOT =     -24430
672049                 XDOT =       -7448
328499
 YDOT =       2931
652037  feet/sec       YDOT =         810
285794  meter/sec
 ZDOT =      -5119
029896                 ZDOT =       -1596
457111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4077589
06                 X    =        -1242849
15
 Y    =       14009592
25  feet           Y    =         4270123
72  meter
 Z    =      -16812657
71                 Z    =        -5124498
07
 XDOT =     -20136
833830                 XDOT =       -6137
706951
 YDOT =     -12196
653953  feet/sec       YDOT =       -3717
540125  meter/sec
 ZDOT =      -5279
934143                 ZDOT =       -1609
323927


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   17355
66626477  
00016717  00000-0  10270-3 0  9013
2 25544  51
6376 183
7109 0002909 267
0388  93
0432 15
54207356 10902


Satellite: ISS
Catalog Number: 25544
Epoch time:      17355
66626477   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       183
7109  deg
Eccentricity:     
0002909     
Arg of perigee:   267
0388  deg
Mean anomaly:      93
0432  deg
Mean motion:   15
54207356  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1090
Checksum:              319


Coasting Arc #3 (Orbit 1105)
---------------------------------------

Vector Time (GMT): 2017/356/15:32:15
084
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         271910
90                 A    =         6777189
49  meter
 Y    =       -4212854
36  meter          E    =           
0000901
 Z    =        5302074
85                 I    =           51
62815
 XDOT =       7658
651836                 Wp   =          336
59766
 YDOT =         -2
555293  meter/sec      RA   =          177
64631  deg
 ZDOT =       -394
009873                 TA   =          117
16444
                                          MA   =          117
15526
                                          Ha   =            219
835  n
mi
                                          Hp   =            215
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         892096
12                 X    =          293245
31
 Y    =      -13821700
67  feet           Y    =        -4209694
84  meter
 Z    =       17395258
68                 Z    =         5303447
15
 XDOT =      25126
810484                 XDOT =        7660
025094
 YDOT =         -8
383507  feet/sec       YDOT =          83
096701  meter/sec
 ZDOT =      -1292
683312                 ZDOT =        -356
803513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8832140
34                 X    =         2692036
38
 Y    =      -10658153
44  feet           Y    =        -3248605
17  meter
 Z    =       17401934
71                 Z    =         5304109
70
 XDOT =      19451
546903                 XDOT =        5928
831496
 YDOT =      14274
210832  feet/sec       YDOT =        4350
779462  meter/sec
 ZDOT =      -1127
301037                 ZDOT =        -343
601356


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   17356
69505116  
00016717  00000-0  10270-3 0  9024
2 25544  51
6384 178
5809 0002853 272
8885  87
1941 15
54196442 11064


Satellite: ISS
Catalog Number: 25544
Epoch time:      17356
69505116   =   yrday
fracday
Element set:     902
Inclination:       51
6384  deg
RA of node:       178
5809  deg
Eccentricity:     
0002853     
Arg of perigee:   272
8885  deg
Mean anomaly:      87
1941  deg
Mean motion:   15
54196442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1106
Checksum:              332


Coasting Arc #4 (Orbit 1120)
---------------------------------------

Vector Time (GMT): 2017/357/15:32:15
084
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2086728
31                 A    =         6778789
41  meter
 Y    =        4187253
22  meter          E    =           
0009448
 Z    =       -4914394
36                 I    =           51
66633
 XDOT =      -7248
917455                 Wp   =          110
42548
 YDOT =       -904
606064  meter/sec      RA   =          172
64900  deg
 ZDOT =       2307
619986                 TA   =          182
15448
                                          MA   =          182
15855
                                          Ha   =            219
818  n
mi
                                          Hp   =            215
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6846221
48                 X    =        -2109524
72
 Y    =       13737707
40  feet           Y    =         4163790
88  meter
 Z    =      -16123341
08                 Z    =        -4924586
02
 XDOT =     -23782
537582                 XDOT =       -7249
472335
 YDOT =      -2967
867665  feet/sec       YDOT =        -985
671685  meter/sec
 ZDOT =       7570
931714                 ZDOT =        2272
405904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13456429
59                 X    =        -4101519
74
 Y    =        7282741
04  feet           Y    =         2219779
47  meter
 Z    =      -16169219
73                 Z    =        -4928378
17
 XDOT =     -17164
265507                 XDOT =       -5231
668127
 YDOT =     -15255
634087  feet/sec       YDOT =       -4649
917270  meter/sec
 ZDOT =       7414
506817                 ZDOT =        2259
941678


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   17357
65953512  
00016717  00000-0  10270-3 0  9039
2 25544  51
6382 173
7735 0002849 274
8704  85
2124 15
54216556 11212


Satellite: ISS
Catalog Number: 25544
Epoch time:      17357
65953512   =   yrday
fracday
Element set:     903
Inclination:       51
6382  deg
RA of node:       173
7735  deg
Eccentricity:     
0002849     
Arg of perigee:   274
8704  deg
Mean anomaly:      85
2124  deg
Mean motion:   15
54216556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1121
Checksum:              315


Coasting Arc #5 (Orbit 1136)
---------------------------------------

Vector Time (GMT): 2017/358/15:32:15
084
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3717314
63                 A    =         6782338
41  meter
 Y    =       -4033145
77  meter          E    =           
0008218
 Z    =        3984495
21                 I    =           51
71103
 XDOT =       6286
318193                 Wp   =           72
72638
 YDOT =       1846
411963  meter/sec      RA   =          167
65986  deg
 ZDOT =      -3986
664114                 TA   =           58
78689
                                          MA   =           58
70637
                                          Ha   =            219
816  n
mi
                                          Hp   =            215
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12195914
15                 X    =         3742783
51
 Y    =      -13232105
55  feet           Y    =        -3991434
04  meter
 Z    =       13072490
84                 Z    =         4002614
25
 XDOT =      20624
403521                 XDOT =        6284
569005
 YDOT =       6057
782032  feet/sec       YDOT =        1916
700325  meter/sec
 ZDOT =     -13079
606673                 ZDOT =       -3956
131520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17470857
39                 X    =         5325117
33
 Y    =       -4058436
86  feet           Y    =        -1237011
56  meter
 Z    =       13153599
82                 Z    =         4009217
23
 XDOT =      13354
015554                 XDOT =        4070
303941
 YDOT =      15437
305817  feet/sec       YDOT =        4705
290813  meter/sec
 ZDOT =     -12944
104094                 ZDOT =       -3945
362928


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   17358
68831632  
00016717  00000-0  10270-3 0  9042
2 25544  51
6389 168
6440 0002833 277
7908  82
2922 15
54187532 11377


Satellite: ISS
Catalog Number: 25544
Epoch time:      17358
68831632   =   yrday
fracday
Element set:     904
Inclination:       51
6389  deg
RA of node:       168
6440  deg
Eccentricity:     
0002833     
Arg of perigee:   277
7908  deg
Mean anomaly:      82
2922  deg
Mean motion:   15
54187532  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1137
Checksum:              333


Coasting Arc #6 (Orbit 1151)
---------------------------------------

Vector Time (GMT): 2017/359/15:32:15
084
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5004858
86                 A    =         6786106
17  meter
 Y    =        3741499
33  meter          E    =           
0003859
 Z    =       -2641990
58                 I    =           51
75665
 XDOT =      -4853
732723                 Wp   =           18
47586
 YDOT =      -2803
982035  meter/sec      RA   =          162
68407  deg
 ZDOT =       5229
431165                 TA   =          311
79928
                                          MA   =          311
83224
                                          Ha   =            219
859  n
mi
                                          Hp   =            215
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16420140
61                 X    =        -5033491
92
 Y    =       12275260
27  feet           Y    =         3685371
61  meter
 Z    =       -8667948
09                 Z    =        -2666371
85
 XDOT =     -15924
319957                 XDOT =       -4847
418960
 YDOT =      -9199
416125  feet/sec       YDOT =       -2858
224747  meter/sec
 ZDOT =      17156
926394                 ZDOT =        5205
868576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20418788
65                 X    =        -6223646
78
 Y    =        1214872
87  feet           Y    =          370293
25  meter
 Z    =       -8776873
61                 Z    =        -2675191
08
 XDOT =      -8216
169206                 XDOT =       -2504
288374
 YDOT =     -15028
165646  feet/sec       YDOT =       -4580
584889  meter/sec
 ZDOT =      17052
531494                 ZDOT =        5197
611599


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17359
65279370  
00016717  00000-0  10270-3 0  9056
2 25544  51
6401 163
8358 0002973 286
5549  73
5277 15
54192348 11525


Satellite: ISS
Catalog Number: 25544
Epoch time:      17359
65279370   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:       163
8358  deg
Eccentricity:     
0002973     
Arg of perigee:   286
5549  deg
Mean anomaly:      73
5277  deg
Mean motion:   15
54192348  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1152
Checksum:              335


Coasting Arc #7 (Orbit 1167)
---------------------------------------

Vector Time (GMT): 2017/360/15:32:15
084
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5871581
62                 A    =         6788646
38  meter
 Y    =       -3248484
51  meter          E    =           
0010894
 Z    =         990822
07                 I    =           51
79540
 XDOT =       3090
780411                 Wp   =          128
34829
 YDOT =       3769
306850  meter/sec      RA   =          157
71983  deg
 ZDOT =      -5920
469497                 TA   =           40
93872
                                          MA   =           40
85697
                                          Ha   =            219
932  n
mi
                                          Hp   =            215
491

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19263719
24                 X    =         5902657
75
 Y    =      -10657757
58  feet           Y    =        -3182650
76  meter
 Z    =        3250728
56                 Z    =         1019419
63
 XDOT =      10140
355678                 XDOT =        3077
159937
 YDOT =      12366
492289  feet/sec       YDOT =        3803
794184  meter/sec
 ZDOT =     -19424
112523                 ZDOT =       -5905
488402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21955070
72                 X    =         6691905
56
 Y    =        1344441
15  feet           Y    =          409785
66  meter
 Z    =        3378351
58                 Z    =         1029721
56
 XDOT =       2118
555134                 XDOT =         645
735605
 YDOT =      14343
864120  feet/sec       YDOT =        4372
009784  meter/sec
 ZDOT =     -19358
002511                 ZDOT =       -5900
319165


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17360
68156769  
00016717  00000-0  10270-3 0  9068
2 25544  51
6393 158
7069 0002819 288
0708  72
0138 15
54209161 11689


Satellite: ISS
Catalog Number: 25544
Epoch time:      17360
68156769   =   yrday
fracday
Element set:     906
Inclination:       51
6393  deg
RA of node:       158
7069  deg
Eccentricity:     
0002819     
Arg of perigee:   288
0708  deg
Mean anomaly:      72
0138  deg
Mean motion:   15
54209161  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1168
Checksum:              331


Coasting Arc #8 (Orbit 1177)
---------------------------------------

Vector Time (GMT): 2017/361/06:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939513
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         872815
18                 A    =         6778895
97  meter
 Y    =       -4648577
39  meter          E    =           
0006100
 Z    =        4855379
99                 I    =           51
78310
 XDOT =       7151
709047                 Wp   =           32
05239
 YDOT =      -1245
919835  meter/sec      RA   =          154
56468  deg
 ZDOT =      -2471
992151                 TA   =           82
20458
                                          MA   =           82
13532
                                          Ha   =            219
888  n
mi
                                          Hp   =            215
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2863566
86                 X    =          901146
93
 Y    =      -15251238
16  feet           Y    =        -4638658
79  meter
 Z    =       15929724
37                 Z    =         4859688
44
 XDOT =      23463
612358                 XDOT =        7177
117435
 YDOT =      -4087
663500  feet/sec       YDOT =       -1165
802346  meter/sec
 ZDOT =      -8110
210468                 ZDOT =       -2437
189759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1572192
18                 X    =          479204
18
 Y    =       15417435
68  feet           Y    =         4699234
40  meter
 Z    =       15949523
13                 Z    =         4861414
65
 XDOT =     -20340
443779                 XDOT =       -6199
767264
 YDOT =      10325
954745  feet/sec       YDOT =        3147
351006  meter/sec
 ZDOT =      -7955
254859                 ZDOT =       -2424
761681


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17361
32454785  
00016717  00000-0  10270-3 0  9070
2 25544  51
6398 155
5057 0003264 300
6943  59
3888 15
54267416 11781


Satellite: ISS
Catalog Number: 25544
Epoch time:      17361
32454785   =   yrday
fracday
Element set:     907
Inclination:       51
6398  deg
RA of node:       155
5057  deg
Eccentricity:     
0003264     
Arg of perigee:   300
6943  deg
Mean anomaly:      59
3888  deg
Mean motion:   15
54267416  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1178
Checksum:              335


Coasting Arc #9 (Orbit 1189)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4013579
95                 A    =         6778536
91  meter
 Y    =       -2244618
63  meter          E    =           
0003159
 Z    =        4978417
78                 I    =           51
80174
 XDOT =       5436
990760                 Wp   =          123
87139
 YDOT =      -4968
059696  meter/sec      RA   =          150
80137  deg
 ZDOT =       2140
640494                 TA   =          305
31132
                                          MA   =          305
34085
                                          Ha   =            220
083  n
mi
                                          Hp   =            215
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13167913
23                 X    =        -4012364
45
 Y    =       -7364234
37  feet           Y    =        -2289494
71  meter
 Z    =       16333391
67                 Z    =         4958923
87
 XDOT =      17837
896195                 XDOT =        5481
742665
 YDOT =     -16299
408452  feet/sec       YDOT =       -4907
009440  meter/sec
 ZDOT =       7023
098735                 ZDOT =        2167
160147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1931600
27                 X    =         -588751
76
 Y    =       15056881
67  feet           Y    =         4589337
53  meter
 Z    =       16246993
73                 Z    =         4952083
69
 XDOT =     -20624
768884                 XDOT =       -6286
429556
 YDOT =     -10361
694589  feet/sec       YDOT =       -3158
244511  meter/sec
 ZDOT =       7141
740744                 ZDOT =        2176
802579


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17362
09612570  
00016717  00000-0  10270-3 0  9084
2 25544  51
6375 151
6574 0003186 301
8014  58
2828 15
54259513 11907


Satellite: ISS
Catalog Number: 25544
Epoch time:      17362
09612570   =   yrday
fracday
Element set:     908
Inclination:       51
6375  deg
RA of node:       151
6574  deg
Eccentricity:     
0003186     
Arg of perigee:   301
8014  deg
Mean anomaly:      58
2828  deg
Mean motion:   15
54259513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1190
Checksum:              305


Coasting Arc #10 (Orbit 1204)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2541333
65                 A    =         6777092
71  meter
 Y    =        3340906
54  meter          E    =           
0012599
 Z    =       -5331354
96                 I    =           51
82504
 XDOT =      -6244
958808                 Wp   =           79
15106
 YDOT =       4430
662900  meter/sec      RA   =          145
81257  deg
 ZDOT =       -198
428709                 TA   =          188
94924
                                          MA   =          188
97172
                                          Ha   =            220
157  n
mi
                                          Hp   =            215
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8337708
82                 X    =         2529683
01
 Y    =       10960979
47  feet           Y    =         3369260
71  meter
 Z    =      -17491322
05                 Z    =        -5319037
98
 XDOT =     -20488
710000                 XDOT =       -6293
075662
 YDOT =      14536
295605  feet/sec       YDOT =        4360
558475  meter/sec
 ZDOT =       -651
012826                 ZDOT =        -228
881399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6850817
49                 X    =         2088129
17
 Y    =      -12025983
37  feet           Y    =        -3665519
73  meter
 Z    =      -17436996
02                 Z    =        -5314796
39
 XDOT =      20435
738611                 XDOT =        6228
813129
 YDOT =      12791
961215  feet/sec       YDOT =        3898
989778  meter/sec
 ZDOT =       -787
097272                 ZDOT =        -239
907249


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17363
06059454  
00016717  00000-0  10270-3 0  9099
2 25544  51
6378 146
8477 0003170 308
5585  51
5283 15
54225774 12058


Satellite: ISS
Catalog Number: 25544
Epoch time:      17363
06059454   =   yrday
fracday
Element set:     909
Inclination:       51
6378  deg
RA of node:       146
8477  deg
Eccentricity:     
0003170     
Arg of perigee:   308
5585  deg
Mean anomaly:      51
5283  deg
Mean motion:   15
54225774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1205
Checksum:              321


Coasting Arc #11 (Orbit 1220)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -981574
51                 A    =         6778048
47  meter
 Y    =       -4361281
51  meter          E    =           
0005583
 Z    =        5094460
73                 I    =           51
85481
 XDOT =       6561
785895                 Wp   =           21
71289
 YDOT =      -3552
323864  meter/sec      RA   =          140
82656  deg
 ZDOT =      -1771
115541                 TA   =           85
39602
                                          MA   =           85
33225
                                          Ha   =            220
279  n
mi
                                          Hp   =            215
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3220388
80                 X    =         -957478
96
 Y    =      -14308666
38  feet           Y    =        -4372123
90  meter
 Z    =       16714109
99                 Z    =         5089750
65
 XDOT =      21528
168946                 XDOT =        6609
624474
 YDOT =     -11654
605852  feet/sec       YDOT =       -3478
677838  meter/sec
 ZDOT =      -5810
746527                 ZDOT =       -1739
124503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11765801
41                 X    =        -3586216
27
 Y    =        8795127
82  feet           Y    =         2680754
96  meter
 Z    =       16693769
92                 Z    =         5088261
07
 XDOT =     -18692
627190                 XDOT =       -5697
512768
 YDOT =     -14212
813437  feet/sec       YDOT =       -4332
065536  meter/sec
 ZDOT =      -5667
916399                 ZDOT =       -1727
580918


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17364
08935740  
00016717  00000-0  10270-3 0  9105
2 25544  51
6377 141
7190 0003168 314
2896  45
7997 15
54228827 12216


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
08935740   =   yrday
fracday
Element set:     910
Inclination:       51
6377  deg
RA of node:       141
7190  deg
Eccentricity:     
0003168     
Arg of perigee:   314
2896  deg
Mean anomaly:      45
7997  deg
Mean motion:   15
54228827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1221
Checksum:              325


Coasting Arc #12 (Orbit 1227)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3502314
96                 A    =         6777304
11  meter
 Y    =       -2428144
18  meter          E    =           
0000703
 Z    =        5269104
42                 I    =           51
86328
 XDOT =       5216
943914                 Wp   =           94
24645
 YDOT =      -5547
580448  meter/sec      RA   =          138
63020  deg
 ZDOT =        911
015846                 TA   =          347
06659
                                          MA   =          347
06840
                                          Ha   =            220
257  n
mi
                                          Hp   =            215
305

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11490534
66                 X    =        -3500497
24
 Y    =       -7966352
30  feet           Y    =        -2467299
85  meter
 Z    =       17287088
00                 Z    =         5252095
41
 XDOT =      17115
957723                 XDOT =        5274
165446
 YDOT =     -18200
723254  feet/sec       YDOT =       -5488
921162  meter/sec
 ZDOT =       2988
897132                 ZDOT =         936
496570

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7032179
51                 X    =         2143408
32
 Y    =      -12191904
48  feet           Y    =        -3716092
48  meter
 Z    =       17211754
24                 Z    =         5246142
69
 XDOT =      18593
694804                 XDOT =        5667
358176
 YDOT =      15106
092380  feet/sec       YDOT =        4604
336957  meter/sec
 ZDOT =       3103
055671                 ZDOT =         945
811368


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17364
53943983  
00016717  00000-0  10270-3 0  9114
2 25544  51
6373 139
4704 0002897 308
0648  52
0243 15
54245188 12282


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
53943983   =   yrday
fracday
Element set:     911
Inclination:       51
6373  deg
RA of node:       139
4704  deg
Eccentricity:     
0002897     
Arg of perigee:   308
0648  deg
Mean anomaly:      52
0243  deg
Mean motion:   15
54245188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1228
Checksum:              320


Coasting Arc #13 (Orbit 1242)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2150046
95                 A    =         6777329
99  meter
 Y    =        3716920
62  meter          E    =           
0012077
 Z    =       -5253900
55                 I    =           51
88882
 XDOT =      -5811
091630                 Wp   =           90
69648
 YDOT =       4873
990501  meter/sec      RA   =          133
64625  deg
 ZDOT =       1072
066302                 TA   =          189
53833
                                          MA   =          189
56129
                                          Ha   =            220
216  n
mi
                                          Hp   =            215
284

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7053959
80                 X    =         2133844
33
 Y    =       12194621
46  feet           Y    =         3740873
97  meter
 Z    =      -17237206
54                 Z    =        -5243495
22
 XDOT =     -19065
261254                 XDOT =       -5870
369565
 YDOT =      15990
782482  feet/sec       YDOT =        4808
675325  meter/sec
 ZDOT =       3517
277894                 ZDOT =        1043
694534

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11453710
74                 X    =        -3491091
03
 Y    =        8297917
02  feet           Y    =         2529205
11  meter
 Z    =      -17191437
24                 Z    =        -5239950
07
 XDOT =     -17134
186777                 XDOT =       -5222
500130
 YDOT =     -16640
027156  feet/sec       YDOT =       -5071
880277  meter/sec
 ZDOT =       3390
324298                 ZDOT =        1033
370846


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17365
50390049  
00016717  00000-0  10270-3 0  9122
2 25544  51
6386 134
6626 0002841 312
1132  47
9779 15
54258523 12430


Satellite: ISS
Catalog Number: 25544
Epoch time:      17365
50390049   =   yrday
fracday
Element set:     912
Inclination:       51
6386  deg
RA of node:       134
6626  deg
Eccentricity:     
0002841     
Arg of perigee:   312
1132  deg
Mean anomaly:      47
9779  deg
Mean motion:   15
54258523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1243
Checksum:              306
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