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

 
Date: October 20th 2018

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) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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


300/09:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 215 5

303/21:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 215 1

Coasting Arc #1 (Orbit 1783)
---------------------------------------

Vector Time (GMT): 2018/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3461356
61                 A    =         6778229
90  meter
 Y    =        2375305
22  meter          E    =           
0011755
 Z    =       -5331701
28                 I    =           51
95056
 XDOT =      -3893
279100                 Wp   =           81
84282
 YDOT =       6583
833456  meter/sec      RA   =          118
20475  deg
 ZDOT =        407
998775                 TA   =          192
02162
                                          MA   =          192
04970
                                          Ha   =            220
690  n
mi
                                          Hp   =            216
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11356156
85                 X    =         3460436
91
 Y    =        7792996
14  feet           Y    =         2414007
02  meter
 Z    =      -17492458
28                 Z    =        -5314889
42
 XDOT =     -12773
225393                 XDOT =       -3968
593867
 YDOT =      21600
503463  feet/sec       YDOT =        6539
875021  meter/sec
 ZDOT =       1338
578657                 ZDOT =         388
902999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13760275
53                 X    =        -4194131
98
 Y    =       -1726044
18  feet           Y    =         -526098
27  meter
 Z    =      -17417082
79                 Z    =        -5308726
83
 XDOT =       1441
567668                 XDOT =         439
389825
 YDOT =     -24046
624036  feet/sec       YDOT =       -7329
411006  meter/sec
 ZDOT =       1252
007000                 ZDOT =         381
611734


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   18292
51543861  
00016717  00000-0  10270-3 0  9002
2 25544  51
6366 119
1576 0004006 308
2586  51
8206 15
53844899 17849


Satellite: ISS
Catalog Number: 25544
Epoch time:      18292
51543861   =   yrday
fracday
Element set:     900
Inclination:       51
6366  deg
RA of node:       119
1576  deg
Eccentricity:     
0004006     
Arg of perigee:   308
2586  deg
Mean anomaly:      51
8206  deg
Mean motion:   15
53844899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1784
Checksum:              325


Coasting Arc #2 (Orbit 1799)
---------------------------------------

Vector Time (GMT): 2018/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2594105
70                 A    =         6779827
31  meter
 Y    =       -3812157
27  meter          E    =           
0006504
 Z    =        4970350
28                 I    =           51
97003
 XDOT =       4400
654566                 Wp   =           21
17703
 YDOT =      -5878
947735  meter/sec      RA   =          113
23116  deg
 ZDOT =      -2205
457822                 TA   =           90
27780
                                          MA   =           90
20326
                                          Ha   =            220
852  n
mi
                                          Hp   =            216
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8510845
46                 X    =        -2575427
94
 Y    =      -12507077
65  feet           Y    =        -3841061
53  meter
 Z    =       16306923
50                 Z    =         4957794
53
 XDOT =      14437
843064                 XDOT =        4476
780619
 YDOT =     -19287
886269  feet/sec       YDOT =       -5829
311090  meter/sec
 ZDOT =      -7235
754008                 ZDOT =       -2183
895323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13483801
75                 X    =         4109862
77
 Y    =        6991025
54  feet           Y    =         2130864
58  meter
 Z    =       16250842
69                 Z    =         4953256
85
 XDOT =      -3216
823630                 XDOT =        -980
487843
 YDOT =      22849
270071  feet/sec       YDOT =        6964
457517  meter/sec
 ZDOT =      -7138
144623                 ZDOT =       -2175
706481


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   18293
54446346  
00016717  00000-0  10270-3 0  9017
2 25544  51
6363 114
0299 0004031 311
5402  48
5404 15
53817924 18005


Satellite: ISS
Catalog Number: 25544
Epoch time:      18293
54446346   =   yrday
fracday
Element set:     901
Inclination:       51
6363  deg
RA of node:       114
0299  deg
Eccentricity:     
0004031     
Arg of perigee:   311
5402  deg
Mean anomaly:      48
5404  deg
Mean motion:   15
53817924  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1800
Checksum:              286


Coasting Arc #3 (Orbit 1814)
---------------------------------------

Vector Time (GMT): 2018/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1756588
85                 A    =         6782846
35  meter
 Y    =        5061020
34  meter          E    =           
0004493
 Z    =       -4163968
81                 I    =           51
99193
 XDOT =      -4681
653332                 Wp   =           87
76288
 YDOT =       4738
806310  meter/sec      RA   =          108
26393  deg
 ZDOT =       3788
408069                 TA   =          221
08003
                                          MA   =          221
11387
                                          Ha   =            220
886  n
mi
                                          Hp   =            216
134

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5763086
79                 X    =         1720091
25
 Y    =       16604397
45  feet           Y    =         5080459
29  meter
 Z    =      -13661315
00                 Z    =        -4155524
88
 XDOT =     -15359
755025                 XDOT =       -4752
698412
 YDOT =      15547
264795  feet/sec       YDOT =        4686
055914  meter/sec
 ZDOT =      12429
160332                 ZDOT =        3765
492880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13170428
63                 X    =        -4014346
65
 Y    =      -11682496
90  feet           Y    =        -3560825
05  meter
 Z    =      -13623868
30                 Z    =        -4152555
06
 XDOT =       5114
297065                 XDOT =        1558
837745
 YDOT =     -20125
333729  feet/sec       YDOT =       -6134
201721  meter/sec
 ZDOT =      12325
572476                 ZDOT =        3756
834491


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   18294
50917240  
00016717  00000-0  10270-3 0  9021
2 25544  51
6357 109
2219 0003872 314
9576  45
1262 15
53845320 18159


Satellite: ISS
Catalog Number: 25544
Epoch time:      18294
50917240   =   yrday
fracday
Element set:     902
Inclination:       51
6357  deg
RA of node:       109
2219  deg
Eccentricity:     
0003872     
Arg of perigee:   314
9576  deg
Mean anomaly:      45
1262  deg
Mean motion:   15
53845320  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1815
Checksum:              304


Coasting Arc #4 (Orbit 1830)
---------------------------------------

Vector Time (GMT): 2018/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -939921
52                 A    =         6786442
47  meter
 Y    =       -6035340
35  meter          E    =           
0010407
 Z    =        2950211
19                 I    =           52
01382
 XDOT =       4802
747069                 Wp   =           83
29343
 YDOT =      -3218
006476  meter/sec      RA   =          103
30680  deg
 ZDOT =      -5036
677425                 TA   =           63
21429
                                          MA   =           63
10787
                                          Ha   =            220
911  n
mi
                                          Hp   =            216
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3083732
02                 X    =         -886693
66
 Y    =      -19800985
41  feet           Y    =        -6045553
32  meter
 Z    =        9679170
59                 Z    =         2945775
13
 XDOT =      15757
044190                 XDOT =        4862
840766
 YDOT =     -10557
764030  feet/sec       YDOT =       -3163
963278  meter/sec
 ZDOT =     -16524
532234                 ZDOT =       -5013
200638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12623922
03                 X    =         3847771
44
 Y    =       15575567
40  feet           Y    =         4747432
94  meter
 Z    =        9659868
66                 Z    =         2944327
97
 XDOT =      -7328
413731                 XDOT =       -2233
700505
 YDOT =      16155
714256  feet/sec       YDOT =        4924
261705  meter/sec
 ZDOT =     -16418
569961                 ZDOT =       -5004
380124


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   18295
53819121  
00016717  00000-0  10270-3 0  9035
2 25544  51
6361 104
0938 0004109 317
8380  42
2456 15
53858268 18310


Satellite: ISS
Catalog Number: 25544
Epoch time:      18295
53819121   =   yrday
fracday
Element set:     903
Inclination:       51
6361  deg
RA of node:       104
0938  deg
Eccentricity:     
0004109     
Arg of perigee:   317
8380  deg
Mean anomaly:      42
2456  deg
Mean motion:   15
53858268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1831
Checksum:              309


Coasting Arc #5 (Orbit 1845)
---------------------------------------

Vector Time (GMT): 2018/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         198961
67                 A    =         6789195
73  meter
 Y    =        6615986
01  meter          E    =           
0010099
 Z    =       -1484507
15                 I    =           52
03022
 XDOT =      -4794
217727                 Wp   =           16
32782
 YDOT =       1443
334208  meter/sec      RA   =           98
35826  deg
 ZDOT =       5808
914021                 TA   =          327
55501
                                          MA   =          327
61706
                                          Ha   =            221
092  n
mi
                                          Hp   =            215
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         652761
39                 X    =          132176
21
 Y    =       21705990
84  feet           Y    =         6617837
39  meter
 Z    =       -4870430
27                 Z    =        -1483703
40
 XDOT =     -15729
060783                 XDOT =       -4838
218484
 YDOT =       4735
348451  feet/sec       YDOT =        1389
476396  meter/sec
 ZDOT =      19058
116867                 ZDOT =        5785
517833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11758978
43                 X    =        -3584136
63
 Y    =      -18257344
69  feet           Y    =        -5564838
66  meter
 Z    =       -4867547
41                 Z    =        -1483628
45
 XDOT =       9824
938691                 XDOT =        2994
641313
 YDOT =     -11364
265055  feet/sec       YDOT =       -3463
827989  meter/sec
 ZDOT =      18952
703918                 ZDOT =        5776
784154


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   18296
50289564  
00016717  00000-0  10270-3 0  9046
2 25544  51
6368  99
2859 0003832 323
8502  36
2391 15
53852748 18463


Satellite: ISS
Catalog Number: 25544
Epoch time:      18296
50289564   =   yrday
fracday
Element set:     904
Inclination:       51
6368  deg
RA of node:        99
2859  deg
Eccentricity:     
0003832     
Arg of perigee:   323
8502  deg
Mean anomaly:      36
2391  deg
Mean motion:   15
53852748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1846
Checksum:              343


Coasting Arc #6 (Orbit 1861)
---------------------------------------

Vector Time (GMT): 2018/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         519087
19                 A    =         6790010
32  meter
 Y    =       -6765215
51  meter          E    =           
0007929
 Z    =        -147473
85                 I    =           52
03622
 XDOT =       4693
197001                 Wp   =          129
43958
 YDOT =        486
986233  meter/sec      RA   =           93
41591  deg
 ZDOT =      -6041
352427                 TA   =           52
13980
                                          MA   =           52
06809
                                          Ha   =            221
131  n
mi
                                          Hp   =            215
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1703041
95                 X    =          595415
50
 Y    =      -22195588
96  feet           Y    =        -6758983
95  meter
 Z    =        -483838
09                 Z    =         -144766
39
 XDOT =      15397
627957                 XDOT =        4716
749081
 YDOT =       1597
723863  feet/sec       YDOT =         539
600101  meter/sec
 ZDOT =     -19820
710063                 ZDOT =       -6018
496712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10301823
29                 X    =         3139995
74
 Y    =       19733963
61  feet           Y    =         6014912
11  meter
 Z    =        -470890
07                 Z    =         -143527
29
 XDOT =     -12580
923561                 XDOT =       -3834
665501
 YDOT =       6114
933087  feet/sec       YDOT =        1863
831605  meter/sec
 ZDOT =     -19717
941953                 ZDOT =       -6010
028707


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   18297
53190922  
00016717  00000-0  10270-3 0  9050
2 25544  51
6359  94
1581 0004034 328
2213  31
8696 15
53890226 18622


Satellite: ISS
Catalog Number: 25544
Epoch time:      18297
53190922   =   yrday
fracday
Element set:     905
Inclination:       51
6359  deg
RA of node:        94
1581  deg
Eccentricity:     
0004034     
Arg of perigee:   328
2213  deg
Mean anomaly:      31
8696  deg
Mean motion:   15
53890226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1862
Checksum:              316


Coasting Arc #7 (Orbit 1877)
---------------------------------------

Vector Time (GMT): 2018/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1186570
93                 A    =         6788782
09  meter
 Y    =        6445037
49  meter          E    =           
0014134
 Z    =        1740238
50                 I    =           52
03495
 XDOT =      -4526
551834                 Wp   =           49
11424
 YDOT =      -2382
895012  meter/sec      RA   =           88
47284  deg
 ZDOT =       5717
564999                 TA   =          329
88428
                                          MA   =          329
96548
                                          Ha   =            221
213  n
mi
                                          Hp   =            215
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3892949
24                 X    =        -1267006
36
 Y    =       21145136
11  feet           Y    =         6431318
77  meter
 Z    =        5709443
90                 Z    =         1734278
70
 XDOT =     -14850
891843                 XDOT =       -4527
342953
 YDOT =      -7817
897020  feet/sec       YDOT =       -2433
518210  meter/sec
 ZDOT =      18758
415350                 ZDOT =        5695
574121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8201806
81                 X    =        -2499910
71
 Y    =      -19882559
57  feet           Y    =        -6060204
16  meter
 Z    =        5681881
26                 Z    =         1731837
41
 XDOT =      15368
196010                 XDOT =        4684
226144
 YDOT =       -987
188580  feet/sec       YDOT =        -300
895079  meter/sec
 ZDOT =      18659
758222                 ZDOT =        5687
494306


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   18298
56092159  
00016717  00000-0  10270-3 0  9068
2 25544  51
6380  89
0301 0003822 329
9922  30
1011 15
53880859 18789


Satellite: ISS
Catalog Number: 25544
Epoch time:      18298
56092159   =   yrday
fracday
Element set:     906
Inclination:       51
6380  deg
RA of node:        89
0301  deg
Eccentricity:     
0003822     
Arg of perigee:   329
9922  deg
Mean anomaly:      30
1011  deg
Mean motion:   15
53880859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1878
Checksum:              321


Coasting Arc #8 (Orbit 1892)
---------------------------------------

Vector Time (GMT): 2018/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1865084
06                 A    =         6785779
53  meter
 Y    =       -5691072
85  meter          E    =           
0003942
 Z    =       -3196205
66                 I    =           52
02352
 XDOT =       4273
036338                 Wp   =           46
52494
 YDOT =       4120
048136  meter/sec      RA   =           83
52427  deg
 ZDOT =      -4843
690190                 TA   =          170
15207
                                          MA   =          170
14434
                                          Ha   =            221
348  n
mi
                                          Hp   =            215
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6119042
19                 X    =         1944110
55
 Y    =      -18671498
86  feet           Y    =        -5669774
40  meter
 Z    =      -10486239
06                 Z    =        -3186953
37
 XDOT =      14019
148091                 XDOT =        4250
176034
 YDOT =      13517
218294  feet/sec       YDOT =        4167
704254  meter/sec
 ZDOT =     -15891
372014                 ZDOT =       -4822
988262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5288651
12                 X    =         1611980
86
 Y    =       18946851
54  feet           Y    =         5775000
35  meter
 Z    =      -10443933
29                 Z    =        -3183310
87
 XDOT =     -17882
394382                 XDOT =       -5450
553808
 YDOT =      -3715
094228  feet/sec       YDOT =       -1132
360721  meter/sec
 ZDOT =     -15798
726189                 ZDOT =       -4815
451743


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   18299
52561777  
00016717  00000-0  10270-3 0  9073
2 25544  51
6385  84
2229 0003935 336
1397  23
9573 15
53872986 18933


Satellite: ISS
Catalog Number: 25544
Epoch time:      18299
52561777   =   yrday
fracday
Element set:     907
Inclination:       51
6385  deg
RA of node:        84
2229  deg
Eccentricity:     
0003935     
Arg of perigee:   336
1397  deg
Mean anomaly:      23
9573  deg
Mean motion:   15
53872986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1893
Checksum:              360


Coasting Arc #9 (Orbit 1906)
---------------------------------------

Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3388325
34                 A    =         6779559
43  meter
 Y    =       -3084289
80  meter          E    =           
0013018
 Z    =       -5008529
34                 I    =           51
99698
 XDOT =       2988
817820                 Wp   =           56
17468
 YDOT =       6725
535764  meter/sec      RA   =           79
02561  deg
 ZDOT =      -2116
560554                 TA   =          193
27494
                                          MA   =          193
30923
                                          Ha   =            221
507  n
mi
                                          Hp   =            215
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11116552
94                 X    =         3446892
40
 Y    =      -10119061
01  feet           Y    =        -3046071
75  meter
 Z    =      -16432182
88                 Z    =        -4991927
29
 XDOT =       9805
832742                 XDOT =        2923
670302
 YDOT =      22065
406051  feet/sec       YDOT =        6758
594527  meter/sec
 ZDOT =      -6944
096306                 ZDOT =       -2102
199764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11033552
83                 X    =        -3363026
90
 Y    =       10329346
31  feet           Y    =         3148384
75  meter
 Z    =      -16357111
48                 Z    =        -4985647
58
 XDOT =      -9511
349407                 XDOT =       -2899
059299
 YDOT =     -21071
361854  feet/sec       YDOT =       -6422
551093  meter/sec
 ZDOT =      -6880
306892                 ZDOT =       -2097
117541


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   18300
42599820  
00016717  00000-0  10270-3 0  9086
2 25544  51
6371  79
7379 0004086 341
5543  18
5461 15
53873826 19070


Satellite: ISS
Catalog Number: 25544
Epoch time:      18300
42599820   =   yrday
fracday
Element set:     908
Inclination:       51
6371  deg
RA of node:        79
7379  deg
Eccentricity:     
0004086     
Arg of perigee:   341
5543  deg
Mean anomaly:      18
5461  deg
Mean motion:   15
53873826  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1907
Checksum:              330


Coasting Arc #10 (Orbit 1922)
---------------------------------------

Vector Time (GMT): 2018/301/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3914445
77                 A    =         6778247
21  meter
 Y    =        1473354
66  meter          E    =           
0003657
 Z    =        5332622
30                 I    =           51
98465
 XDOT =      -2334
637257                 Wp   =           21
93326
 YDOT =      -7299
289995  meter/sec      RA   =           74
05331  deg
 ZDOT =        306
206417                 TA   =           65
18104
                                          MA   =           65
14300
                                          Ha   =            221
804  n
mi
                                          Hp   =            215
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12842669
84                 X    =        -3956534
03
 Y    =        4833840
75  feet           Y    =         1429345
21  meter
 Z    =       17495480
00                 Z    =         5313504
58
 XDOT =      -7659
571054                 XDOT =       -2254
328474
 YDOT =     -23947
801822  feet/sec       YDOT =       -7324
948499  meter/sec
 ZDOT =       1004
614228                 ZDOT =         295
060233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12776443
25                 X    =         3894259
90
 Y    =       -5298252
23  feet           Y    =        -1614907
28  meter
 Z    =       17409279
89                 Z    =         5306348
51
 XDOT =       8136
425488                 XDOT =        2479
982489
 YDOT =      22724
720797  feet/sec       YDOT =        6926
494899  meter/sec
 ZDOT =        955
376342                 ZDOT =         291
198709


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   18301
45500401  
00016717  00000-0  10270-3 0  9098
2 25544  51
6369  74
6098 0004118 344
8439  15
2589 15
53828865 19231


Satellite: ISS
Catalog Number: 25544
Epoch time:      18301
45500401   =   yrday
fracday
Element set:     909
Inclination:       51
6369  deg
RA of node:        74
6098  deg
Eccentricity:     
0004118     
Arg of perigee:   344
8439  deg
Mean anomaly:      15
2589  deg
Mean motion:   15
53828865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1923
Checksum:              323


Coasting Arc #11 (Orbit 1937)
---------------------------------------

Vector Time (GMT): 2018/302/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4390391
72                 A    =         6778849
91  meter
 Y    =         157405
57  meter          E    =           
0012640
 Z    =       -5173142
86                 I    =           51
97887
 XDOT =       1530
547661                 Wp   =           84
22087
 YDOT =       7347
605974  meter/sec      RA   =           69
08008  deg
 ZDOT =       1526
963689                 TA   =          200
41325
                                          MA   =          200
46381
                                          Ha   =            221
702  n
mi
                                          Hp   =            215
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14404172
30                 X    =         4413434
19
 Y    =         516422
47  feet           Y    =          206630
93  meter
 Z    =      -16972253
48                 Z    =        -5151759
43
 XDOT =       5021
481826                 XDOT =        1440
853587
 YDOT =      24106
318812  feet/sec       YDOT =        7364
220074  meter/sec
 ZDOT =       5009
723389                 ZDOT =        1534
181030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14523657
86                 X    =        -4426810
92
 Y    =         257338
17  feet           Y    =           78436
68  meter
 Z    =      -16876059
94                 Z    =        -5143823
07
 XDOT =      -6243
859742                 XDOT =       -1903
128449
 YDOT =     -22748
320838  feet/sec       YDOT =       -6933
688192  meter/sec
 ZDOT =       5041
261568                 ZDOT =        1536
576526


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   18302
41969161  
00016717  00000-0  10270-3 0  9109
2 25544  51
6388  69
8028 0004066 348
8496  11
2566 15
53882859 19380


Satellite: ISS
Catalog Number: 25544
Epoch time:      18302
41969161   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:        69
8028  deg
Eccentricity:     
0004066     
Arg of perigee:   348
8496  deg
Mean anomaly:      11
2566  deg
Mean motion:   15
53882859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1938
Checksum:              343


Coasting Arc #12 (Orbit 1953)
---------------------------------------

Vector Time (GMT): 2018/303/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4758951
47                 A    =         6781637
69  meter
 Y    =       -1732431
20  meter          E    =           
0010786
 Z    =        4507363
49                 I    =           51
97393
 XDOT =       -552
107310                 Wp   =           47
18278
 YDOT =      -6931
056498  meter/sec      RA   =           64
10976  deg
 ZDOT =      -3234
887684                 TA   =           75
25485
                                          MA   =           75
13535
                                          Ha   =            221
897  n
mi
                                          Hp   =            215
181

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15613357
83                 X    =        -4761120
00
 Y    =       -5683829
39  feet           Y    =        -1785661
32  meter
 Z    =       14787937
95                 Z    =         4484240
47
 XDOT =      -1811
375688                 XDOT =        -458
847633
 YDOT =     -22739
686674  feet/sec       YDOT =       -6936
709028  meter/sec
 ZDOT =     -10613
148568                 ZDOT =       -3237
343308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16072212
57                 X    =         4898810
39
 Y    =        4563619
49  feet           Y    =         1390991
22  meter
 Z    =       14684118
24                 Z    =         4475719
24
 XDOT =       3668
622483                 XDOT =        1118
196133
 YDOT =      21389
711360  feet/sec       YDOT =        6519
584023  meter/sec
 ZDOT =     -10623
301157                 ZDOT =       -3237
982193


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   18303
44869050  
00016717  00000-0  10270-3 0  9110
2 25544  51
6377  64
6745 0004031 353
0650   7
0446 15
53852056 19543


Satellite: ISS
Catalog Number: 25544
Epoch time:      18303
44869050   =   yrday
fracday
Element set:     911
Inclination:       51
6377  deg
RA of node:        64
6745  deg
Eccentricity:     
0004031     
Arg of perigee:   353
0650  deg
Mean anomaly:       7
0446  deg
Mean motion:   15
53852056  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1954
Checksum:              297


Coasting Arc #13 (Orbit 1960)
---------------------------------------

Vector Time (GMT): 2018/303/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4836130
18                 A    =         6785070
90  meter
 Y    =        3250556
38  meter          E    =           
0006327
 Z    =       -3475516
63                 I    =           51
97845
 XDOT =       -799
204061                 Wp   =           45
83506
 YDOT =       6086
499693  meter/sec      RA   =           61
70472  deg
 ZDOT =       4589
905478                 TA   =          273
60475
                                          MA   =          273
67711
                                          Ha   =            222
023  n
mi
                                          Hp   =            215
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15866568
82                 X    =         4816304
59
 Y    =       10664555
06  feet           Y    =         3304526
55  meter
 Z    =      -11402613
62                 Z    =        -3452072
15
 XDOT =      -2622
060566                 XDOT =        -889
501261
 YDOT =      19968
831014  feet/sec       YDOT =        6077
057479  meter/sec
 ZDOT =      15058
745008                 ZDOT =        4585
803947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15803365
63                 X    =         4816865
85
 Y    =       10868276
68  feet           Y    =         3312650
73  meter
 Z    =      -11297545
52                 Z    =        -3443491
87
 XDOT =      -2186
808934                 XDOT =        -666
539363
 YDOT =      18780
796133  feet/sec       YDOT =        5724
386661  meter/sec
 ZDOT =      15039
497262                 ZDOT =        4584
038765


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   18303
89887529  
00016717  00000-0  10270-3 0  9121
2 25544  51
6377  62
4358 0004525 355
1985   4
9123 15
53863423 19617


Satellite: ISS
Catalog Number: 25544
Epoch time:      18303
89887529   =   yrday
fracday
Element set:     912
Inclination:       51
6377  deg
RA of node:        62
4358  deg
Eccentricity:     
0004525     
Arg of perigee:   355
1985  deg
Mean anomaly:       4
9123  deg
Mean motion:   15
53863423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1961
Checksum:              332


Coasting Arc #14 (Orbit 1976)
---------------------------------------

Vector Time (GMT): 2018/304/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4780295
34                 A    =         6788252
81  meter
 Y    =       -4350913
58  meter          E    =           
0012779
 Z    =        2061486
36                 I    =           51
97301
 XDOT =       2016
443949                 Wp   =           91
82586
 YDOT =      -4868
102663  meter/sec      RA   =           56
75051  deg
 ZDOT =      -5569
306189                 TA   =           65
48520
                                          MA   =           65
35202
                                          Ha   =            221
974  n
mi
                                          Hp   =            214
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15683383
67                 X    =        -4741300
66
 Y    =      -14274650
84  feet           Y    =        -4404152
12  meter
 Z    =        6763406
71                 Z    =         2038359
79
 XDOT =       6615
629755                 XDOT =        2097
783633
 YDOT =     -15971
465430  feet/sec       YDOT =       -4845
098592  meter/sec
 ZDOT =     -18272
001933                 ZDOT =       -5559
313324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15789504
91                 X    =        -4812641
10
 Y    =      -14206156
30  feet           Y    =        -4330036
44  meter
 Z    =        6659918
03                 Z    =         2029943
02
 XDOT =       5632
173211                 XDOT =        1716
686395
 YDOT =     -14850
335573  feet/sec       YDOT =       -4526
382283  meter/sec
 ZDOT =     -18226
396886                 ZDOT =       -5555
405771


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   18304
92787006  
00016717  00000-0  10270-3 0  9136
2 25544  51
6380  57
3074 0004602 357
5035   2
6094 15
53898740 19776


Satellite: ISS
Catalog Number: 25544
Epoch time:      18304
92787006   =   yrday
fracday
Element set:     913
Inclination:       51
6380  deg
RA of node:        57
3074  deg
Eccentricity:     
0004602     
Arg of perigee:   357
5035  deg
Mean anomaly:       2
6094  deg
Mean motion:   15
53898740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1977
Checksum:              316


Coasting Arc #15 (Orbit 1991)
---------------------------------------

Vector Time (GMT): 2018/305/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4475159
75                 A    =         6789873
09  meter
 Y    =        5072228
43  meter          E    =           
0014868
 Z    =        -486198
46                 I    =           51
96023
 XDOT =      -3272
050236                 Wp   =           30
40260
 YDOT =       3454
783836  meter/sec      RA   =           51
80235  deg
 ZDOT =       6017
098531                 TA   =          324
37457
                                          MA   =          324
47372
                                          Ha   =            222
056  n
mi
                                          Hp   =            214
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14682282
65                 X    =         4420469
80
 Y    =       16641169
38  feet           Y    =         5121966
97  meter
 Z    =       -1595139
31                 Z    =         -464592
39
 XDOT =     -10735
072954                 XDOT =       -3339
667627
 YDOT =      11334
592638  feet/sec       YDOT =        3417
815557  meter/sec
 ZDOT =      19741
136912                 ZDOT =        6001
039560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15047222
75                 X    =         4586393
50
 Y    =       16321081
82  feet           Y    =         4974665
74  meter
 Z    =       -1498595
04                 Z    =         -456771
77
 XDOT =      -9429
657129                 XDOT =       -2874
159493
 YDOT =      10469
942269  feet/sec       YDOT =        3191
238404  meter/sec
 ZDOT =      19668
419700                 ZDOT =        5994
934324


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   18305
89254925  
00016717  00000-0  10270-3 0  9143
2 25544  51
6387  52
5005 0004492   2
0805 358
0366 15
53911375 19925


Satellite: ISS
Catalog Number: 25544
Epoch time:      18305
89254925   =   yrday
fracday
Element set:     914
Inclination:       51
6387  deg
RA of node:        52
5005  deg
Eccentricity:     
0004492     
Arg of perigee:     2
0805  deg
Mean anomaly:     358
0366  deg
Mean motion:   15
53911375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1992
Checksum:              312


Coasting Arc #16 (Orbit 2007)
---------------------------------------

Vector Time (GMT): 2018/306/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3859797
38                 A    =         6789371
39  meter
 Y    =       -5460180
91  meter          E    =           
0006557
 Z    =       -1172145
59                 I    =           51
93768
 XDOT =       4509
491128                 Wp   =          112
17955
 YDOT =      -1930
055545  meter/sec      RA   =           46
85402  deg
 ZDOT =      -5887
414926                 TA   =           80
48831
                                          MA   =           80
41422
                                          Ha   =            222
150  n
mi
                                          Hp   =            214
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12663377
24                 X    =        -3792759
51
 Y    =      -17913979
36  feet           Y    =        -5502969
06  meter
 Z    =       -3845622
02                 Z    =        -1190732
35
 XDOT =      14794
918399                 XDOT =        4559
336723
 YDOT =      -6332
203232  feet/sec       YDOT =       -1879
348815  meter/sec
 ZDOT =     -19315
665768                 ZDOT =       -5865
387952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13321492
38                 X    =        -4060390
88
 Y    =      -17411638
71  feet           Y    =        -5307067
48  meter
 Z    =       -3928519
61                 Z    =        -1197412
78
 XDOT =      13397
121040                 XDOT =        4083
442493
 YDOT =      -5935
116917  feet/sec       YDOT =       -1809
023636  meter/sec
 ZDOT =     -19216
299401                 ZDOT =       -5857
128058


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   18306
92153707  
00016717  00000-0  10270-3 0  9155
2 25544  51
6391  47
3722 0004750   5
0359 355
0841 15
53903050 20087


Satellite: ISS
Catalog Number: 25544
Epoch time:      18306
92153707   =   yrday
fracday
Element set:     915
Inclination:       51
6391  deg
RA of node:        47
3722  deg
Eccentricity:     
0004750     
Arg of perigee:     5
0359  deg
Mean anomaly:     355
0841  deg
Mean motion:   15
53903050  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2008
Checksum:              286
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