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

 
Date: January 18th 2018

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) : 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


017/20:15:07 803 0 7 0 8 0 8
N/A 0 4 -0 1 221 6
000/00:00:15 606 -0 2 -0 0 214 1

018/18:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 214 1

023/19:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 213 7

029/16:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 4

Coasting Arc #1 (Orbit 1476)
---------------------------------------

Vector Time (GMT): 2018/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3221176
16                 A    =         6776902
37  meter
 Y    =        2709845
36  meter          E    =           
0004408
 Z    =        5307650
59                 I    =           51
94725
 XDOT =      -4317
727617                 Wp   =           57
07822
 YDOT =      -6313
095794  meter/sec      RA   =           59
17900  deg
 ZDOT =        604
752764                 TA   =           27
18838
                                          MA   =           27
16531
                                          Ha   =            221
580  n
mi
                                          Hp   =            213
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10568163
27                 X    =        -3277020
40
 Y    =        8890568
75  feet           Y    =         2673511
30  meter
 Z    =       17413551
82                 Z    =         5291868
02
 XDOT =     -14165
773023                 XDOT =       -4249
749509
 YDOT =     -20712
256543  feet/sec       YDOT =       -6360
999538  meter/sec
 ZDOT =       1984
096994                 ZDOT =         583
943638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12470368
95                 X    =        -3800968
45
 Y    =       -6138186
27  feet           Y    =        -1870919
18  meter
 Z    =       17342797
99                 Z    =         5286084
83
 XDOT =      12699
714597                 XDOT =        3870
873009
 YDOT =     -20472
178555  feet/sec       YDOT =       -6239
920024  meter/sec
 ZDOT =       1892
469620                 ZDOT =         576
824740


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   18015
54922922  
00016717  00000-0  10270-3 0  9007
2 25544  51
6405  59
6508 0003688  17
3608 342
7670 15
54317764 14777


Satellite: ISS
Catalog Number: 25544
Epoch time:      18015
54922922   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:        59
6508  deg
Eccentricity:     
0003688     
Arg of perigee:    17
3608  deg
Mean anomaly:     342
7670  deg
Mean motion:   15
54317764  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1477
Checksum:              318


Coasting Arc #2 (Orbit 1491)
---------------------------------------

Vector Time (GMT): 2018/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4220909
98                 A    =         6777541
18  meter
 Y    =       -1107721
15  meter          E    =           
0014873
 Z    =       -5198324
03                 I    =           51
93189
 XDOT =       3469
821414                 Wp   =           86
23077
 YDOT =       6682
165967  meter/sec      RA   =           54
19779  deg
 ZDOT =       1397
884255                 TA   =          197
15071
                                          MA   =          197
20102
                                          Ha   =            221
557  n
mi
                                          Hp   =            213
981

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13848129
84                 X    =         4258233
40
 Y    =       -3634255
73  feet           Y    =        -1060310
99  meter
 Z    =      -17054868
87                 Z    =        -5177730
08
 XDOT =      11383
928524                 XDOT =        3388
051680
 YDOT =      21923
116691  feet/sec       YDOT =        6720
510586  meter/sec
 ZDOT =       4586
234433                 ZDOT =        1414
541033

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9195831
35                 X    =         2802889
40
 Y    =       11114947
20  feet           Y    =         3387835
91  meter
 Z    =      -16962950
84                 Z    =        -5170307
42
 XDOT =     -14259
081653                 XDOT =       -4346
168088
 YDOT =      18885
723399  feet/sec       YDOT =        5756
368492  meter/sec
 ZDOT =       4659
297075                 ZDOT =        1420
153749


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   18016
51364683  
00016717  00000-0  10270-3 0  9010
2 25544  51
6410  54
8419 0003718  19
8304 340
2992 15
54293629 14925


Satellite: ISS
Catalog Number: 25544
Epoch time:      18016
51364683   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:        54
8419  deg
Eccentricity:     
0003718     
Arg of perigee:    19
8304  deg
Mean anomaly:     340
2992  deg
Mean motion:   15
54293629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1492
Checksum:              309


Coasting Arc #3 (Orbit 1507)
---------------------------------------

Vector Time (GMT): 2018/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5057450
97                 A    =         6780292
14  meter
 Y    =        -482993
92  meter          E    =           
0012203
 Z    =        4485181
38                 I    =           51
92102
 XDOT =      -2279
428289                 Wp   =           56
03962
 YDOT =      -6557
383378  meter/sec      RA   =           49
22042  deg
 ZDOT =      -3263
417061                 TA   =           66
73875
                                          MA   =           66
61032
                                          Ha   =            221
688  n
mi
                                          Hp   =            213
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16592686
91                 X    =        -5073460
35
 Y    =       -1584625
71  feet           Y    =         -539639
57  meter
 Z    =       14715162
00                 Z    =         4460575
59
 XDOT =      -7478
439267                 XDOT =       -2190
080793
 YDOT =     -21513
724992  feet/sec       YDOT =       -6582
373744  meter/sec
 ZDOT =     -10706
748888                 ZDOT =       -3274
272898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5890349
67                 X    =        -1795378
58
 Y    =      -15695325
42  feet           Y    =        -4783935
19  meter
 Z    =       14605643
80                 Z    =         4451800
23
 XDOT =      14948
030204                 XDOT =        4556
159606
 YDOT =     -15657
215823  feet/sec       YDOT =       -4772
319383  meter/sec
 ZDOT =     -10753
987723                 ZDOT =       -3277
815458


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   18017
54235380  
00016717  00000-0  10270-3 0  9026
2 25544  51
6405  49
7124 0003846  24
7294 335
4043 15
54343027 15089


Satellite: ISS
Catalog Number: 25544
Epoch time:      18017
54235380   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:        49
7124  deg
Eccentricity:     
0003846     
Arg of perigee:    24
7294  deg
Mean anomaly:     335
4043  deg
Mean motion:   15
54343027  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1508
Checksum:              289


Coasting Arc #4 (Orbit 1512)
---------------------------------------

Vector Time (GMT): 2018/017/20:15:15
606
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1187710
84                 A    =         6778725
66  meter
 Y    =       -4471396
53  meter          E    =           
0014639
 Z    =       -4967977
90                 I    =           51
90870
 XDOT =       6087
586055                 Wp   =           61
77886
 YDOT =       4081
605427  meter/sec      RA   =           47
55347  deg
 ZDOT =      -2216
472011                 TA   =          186
63162
                                          MA   =          186
65101
                                          Ha   =            221
591  n
mi
                                          Hp   =            214
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3896689
12                 X    =         1261754
27
 Y    =      -14669936
12  feet           Y    =        -4457700
47  meter
 Z    =      -16299140
10                 Z    =        -4962028
93
 XDOT =      19972
395193                 XDOT =        6052
258245
 YDOT =      13391
093920  feet/sec       YDOT =        4149
483571  meter/sec
 ZDOT =      -7271
889799                 ZDOT =       -2186
986795

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10730930
28                 X    =        -3270787
55
 Y    =      -10776188
37  feet           Y    =        -3284582
21  meter
 Z    =      -16271880
02                 Z    =        -4959669
03
 XDOT =      20793
725223                 XDOT =        6337
927448
 YDOT =      -9914
424748  feet/sec       YDOT =       -3021
916663  meter/sec
 ZDOT =      -7141
251045                 ZDOT =       -2176
653319


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   18017
86382611  
00016717  00000-0  10270-3 0  9032
2 25544  51
6421  48
1103 0003580  16
4212 343
7056 15
54198369 15139


Satellite: ISS
Catalog Number: 25544
Epoch time:      18017
86382611   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:        48
1103  deg
Eccentricity:     
0003580     
Arg of perigee:    16
4212  deg
Mean anomaly:     343
7056  deg
Mean motion:   15
54198369  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1513
Checksum:              285


Coasting Arc #5 (Orbit 1527)
---------------------------------------

Vector Time (GMT): 2018/018/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5116157
39                 A    =         6780942
88  meter
 Y    =          11506
13  meter          E    =           
0011974
 Z    =        4445561
48                 I    =           51
89226
 XDOT =      -2917
524052                 Wp   =           56
44305
 YDOT =      -6264
702556  meter/sec      RA   =           42
83312  deg
 ZDOT =      -3328
514345                 TA   =           67
08880
                                          MA   =           66
96246
                                          Ha   =            221
816  n
mi
                                          Hp   =            214
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16785293
27                 X    =        -5137499
56
 Y    =          37749
76  feet           Y    =          -45825
75  meter
 Z    =       14585175
45                 Z    =         4420657
64
 XDOT =      -9571
929306                 XDOT =       -2831
085793
 YDOT =     -20553
486076  feet/sec       YDOT =       -6296
844877  meter/sec
 ZDOT =     -10920
322653                 ZDOT =       -3342
476669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12857435
96                 X    =        -3918946
48
 Y    =       10938799
34  feet           Y    =         3334146
04  meter
 Z    =       14474247
74                 Z    =         4411750
71
 XDOT =     -19734
901318                 XDOT =       -6015
197922
 YDOT =      -8609
280110  feet/sec       YDOT =       -2624
108577  meter/sec
 ZDOT =     -10981
442042                 ZDOT =       -3347
143535


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   18018
82832687  
00016717  00000-0  10270-3 0  9043
2 25544  51
6402  43
3019 0003592  20
3748 339
7547 15
54171843 15286


Satellite: ISS
Catalog Number: 25544
Epoch time:      18018
82832687   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:        43
3019  deg
Eccentricity:     
0003592     
Arg of perigee:    20
3748  deg
Mean anomaly:     339
7547  deg
Mean motion:   15
54171843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1528
Checksum:              313


Coasting Arc #6 (Orbit 1542)
---------------------------------------

Vector Time (GMT): 2018/019/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5805203
18                 A    =         6784688
10  meter
 Y    =        1251634
59  meter          E    =           
0007098
 Z    =       -3281701
74                 I    =           51
88082
 XDOT =       1425
058409                 Wp   =           56
09417
 YDOT =       5837
086174  meter/sec      RA   =           37
86308  deg
 ZDOT =       4758
346610                 TA   =          265
96956
                                          MA   =          266
05070
                                          Ha   =            221
761  n
mi
                                          Hp   =            214
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19045942
20                 X    =         5806716
06
 Y    =        4106412
69  feet           Y    =         1316560
87  meter
 Z    =      -10766737
99                 Z    =        -3253498
96
 XDOT =       4675
388480                 XDOT =        1336
567565
 YDOT =      19150
545190  feet/sec       YDOT =        5852
527272  meter/sec
 ZDOT =      15611
373392                 ZDOT =        4765
054103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17080534
39                 X    =         5206146
88
 Y    =       -9515801
56  feet           Y    =        -2900416
32  meter
 Z    =      -10641336
94                 Z    =        -3243479
50
 XDOT =      15370
261008                 XDOT =        4684
855555
 YDOT =      10140
550589  feet/sec       YDOT =        3090
839819  meter/sec
 ZDOT =      15640
248199                 ZDOT =        4767
147651


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   18019
79282473  
00016717  00000-0  10270-3 0  9053
2 25544  51
6408  38
4930 0003543  22
5574 337
5734 15
54189589 15433


Satellite: ISS
Catalog Number: 25544
Epoch time:      18019
79282473   =   yrday
fracday
Element set:     905
Inclination:       51
6408  deg
RA of node:        38
4930  deg
Eccentricity:     
0003543     
Arg of perigee:    22
5574  deg
Mean anomaly:     337
5734  deg
Mean motion:   15
54189589  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1543
Checksum:              330


Coasting Arc #7 (Orbit 1558)
---------------------------------------

Vector Time (GMT): 2018/020/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6125218
79                 A    =         6787983
88  meter
 Y    =       -2343567
83  meter          E    =           
0014434
 Z    =        1731825
24                 I    =           51
86585
 XDOT =        334
442053                 Wp   =          101
19164
 YDOT =      -5115
978739  meter/sec      RA   =           32
90211  deg
 ZDOT =      -5702
785058                 TA   =           59
86727
                                          MA   =           59
72430
                                          Ha   =            221
797  n
mi
                                          Hp   =            213
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20095862
19                 X    =        -6106969
28
 Y    =       -7688870
85  feet           Y    =        -2411962
20  meter
 Z    =        5681841
35                 Z    =         1702115
95
 XDOT =       1097
250831                 XDOT =         419
326034
 YDOT =     -16784
707148  feet/sec       YDOT =       -5111
764133  meter/sec
 ZDOT =     -18709
924732                 ZDOT =       -5700
954349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20074974
78                 X    =        -6118852
31
 Y    =        7838332
57  feet           Y    =         2389123
77  meter
 Z    =        5549924
61                 Z    =         1691617
02
 XDOT =      -9806
710875                 XDOT =       -2989
085475
 YDOT =     -11785
990054  feet/sec       YDOT =       -3592
369768  meter/sec
 ZDOT =     -18700
892539                 ZDOT =       -5700
032046


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   18020
82161970  
00016717  00000-0  10270-3 0  9068
2 25544  51
6415  33
3640 0003537  26
7645 333
3689 15
54174788 15596


Satellite: ISS
Catalog Number: 25544
Epoch time:      18020
82161970   =   yrday
fracday
Element set:     906
Inclination:       51
6415  deg
RA of node:        33
3640  deg
Eccentricity:     
0003537     
Arg of perigee:    26
7645  deg
Mean anomaly:     333
3689  deg
Mean motion:   15
54174788  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1559
Checksum:              318


Coasting Arc #8 (Orbit 1574)
---------------------------------------

Vector Time (GMT): 2018/021/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6004346
74                 A    =         6789162
94  meter
 Y    =        3151365
23  meter          E    =           
0015684
 Z    =         -38055
85                 I    =           51
84222
 XDOT =      -2179
744423                 Wp   =           41
28151
 YDOT =       4208
744431  meter/sec      RA   =           27
94526  deg
 ZDOT =       6031
940422                 TA   =          318
30956
                                          MA   =          318
42899
                                          Ha   =            221
858  n
mi
                                          Hp   =            213
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19699300
32                 X    =         5968845
92
 Y    =       10339124
78  feet           Y    =         3218311
46  meter
 Z    =        -124855
15                 Z    =           -8975
56
 XDOT =      -7151
392463                 XDOT =       -2255
945220
 YDOT =      13808
216637  feet/sec       YDOT =        4183
943009  meter/sec
 ZDOT =      19789
830782                 ZDOT =        6021
167059

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21436525
63                 X    =         6533853
01
 Y    =       -5954063
75  feet           Y    =        -1814798
63  meter
 Z    =           4112
42                 Z    =            1253
47
 XDOT =       3715
145559                 XDOT =        1132
376366
 YDOT =      13487
328233  feet/sec       YDOT =        4110
937646  meter/sec
 ZDOT =      19741
127180                 ZDOT =        6017
095564


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   18021
85041131  
00016717  00000-0  10270-3 0  9079
2 25544  51
6418  28
2348 0003689  29
1006 331
0352 15
54187078 15759


Satellite: ISS
Catalog Number: 25544
Epoch time:      18021
85041131   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:        28
2348  deg
Eccentricity:     
0003689     
Arg of perigee:    29
1006  deg
Mean anomaly:     331
0352  deg
Mean motion:   15
54187078  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1575
Checksum:              292


Coasting Arc #9 (Orbit 1589)
---------------------------------------

Vector Time (GMT): 2018/022/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5399372
21                 A    =         6787927
93  meter
 Y    =       -3744483
61  meter          E    =           
0007201
 Z    =       -1701433
72                 I    =           51
80888
 XDOT =       3999
608773                 Wp   =          114
36234
 YDOT =      -3182
660449  meter/sec      RA   =           22
98791  deg
 ZDOT =      -5710
021603                 TA   =           84
23667
                                          MA   =           84
15457
                                          Ha   =            221
821  n
mi
                                          Hp   =            213
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17714475
75                 X    =        -5348834
54
 Y    =      -12285051
21  feet           Y    =        -3804580
54  meter
 Z    =       -5582131
62                 Z    =        -1727538
84
 XDOT =      13122
076027                 XDOT =        4062
636769
 YDOT =     -10441
799372  feet/sec       YDOT =       -3137
581741  meter/sec
 ZDOT =     -18733
666677                 ZDOT =       -5690
440043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21238049
58                 X    =        -6473357
51
 Y    =        3516584
23  feet           Y    =         1071854
87  meter
 Z    =       -5697737
56                 Z    =        -1736670
41
 XDOT =       2471
197828                 XDOT =         753
221098
 YDOT =     -15172
389019  feet/sec       YDOT =       -4624
544173  meter/sec
 ZDOT =     -18645
916970                 ZDOT =       -5683
275492


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   18022
81490208  
00016717  00000-0  10270-3 0  9080
2 25544  51
6421  23
4273 0003461  32
6404 327
4962 15
54168932 15907


Satellite: ISS
Catalog Number: 25544
Epoch time:      18022
81490208   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:        23
4273  deg
Eccentricity:     
0003461     
Arg of perigee:    32
6404  deg
Mean anomaly:     327
4962  deg
Mean motion:   15
54168932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1590
Checksum:              291


Coasting Arc #10 (Orbit 1605)
---------------------------------------

Vector Time (GMT): 2018/023/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4346104
44                 A    =         6784674
71  meter
 Y    =        4081889
04  meter          E    =           
0015273
 Z    =        3220455
01                 I    =           51
76817
 XDOT =      -5589
486747                 Wp   =           75
73995
 YDOT =       2155
141294  meter/sec      RA   =           18
02061  deg
 ZDOT =       4796
232398                 TA   =          321
48879
                                          MA   =          321
59767
                                          Ha   =            221
851  n
mi
                                          Hp   =            213
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14258872
83                 X    =         4284493
54
 Y    =       13392024
41  feet           Y    =         4130145
71  meter
 Z    =       10565797
28                 Z    =         3241416
96
 XDOT =     -18338
211111                 XDOT =       -5636
468013
 YDOT =       7070
673537  feet/sec       YDOT =        2092
373186  meter/sec
 ZDOT =      15735
670597                 ZDOT =        4768
966774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19501371
19                 X    =         5944017
94
 Y    =        -626242
87  feet           Y    =         -190878
83  meter
 Z    =       10658432
62                 Z    =         3248690
26
 XDOT =      -8026
492413                 XDOT =       -2446
474888
 YDOT =      16644
721549  feet/sec       YDOT =        5073
311128  meter/sec
 ZDOT =      15613
887144                 ZDOT =        4759
112802


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   18023
84368914  
00016717  00000-0  10270-3 0  9093
2 25544  51
6427  18
2979 0003695  35
1135 325
0260 15
54189193 16061


Satellite: ISS
Catalog Number: 25544
Epoch time:      18023
84368914   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:        18
2979  deg
Eccentricity:     
0003695     
Arg of perigee:    35
1135  deg
Mean anomaly:     325
0260  deg
Mean motion:   15
54189193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1606
Checksum:              318


Coasting Arc #11 (Orbit 1605)
---------------------------------------

Vector Time (GMT): 2018/023/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1742865
00                 A    =         6779424
77  meter
 Y    =       -4508641
92  meter          E    =           
0014263
 Z    =       -4767212
96                 I    =           51
74937
 XDOT =       7167
595106                 Wp   =           61
86395
 YDOT =         76
334519  meter/sec      RA   =           17
83341  deg
 ZDOT =      -2692
207318                 TA   =          181
53587
                                          MA   =          181
54025
                                          Ha   =            221
821  n
mi
                                          Hp   =            213
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5718061
02                 X    =        -1669162
26
 Y    =      -14792132
29  feet           Y    =        -4527719
79  meter
 Z    =      -15640462
45                 Z    =        -4775500
04
 XDOT =      23515
731975                 XDOT =        7179
285988
 YDOT =        250
441336  feet/sec       YDOT =         156
552819  meter/sec
 ZDOT =      -8832
701175                 ZDOT =       -2657
361609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15545810
70                 X    =        -4738363
10
 Y    =       -2949567
06  feet           Y    =         -899028
04  meter
 Z    =      -15676584
10                 Z    =        -4778222
83
 XDOT =      12324
525073                 XDOT =        3756
515242
 YDOT =     -18829
528927  feet/sec       YDOT =       -5739
240417  meter/sec
 ZDOT =      -8677
550797                 ZDOT =       -2644
917483


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   18023
84368770  
00016717  00000-0  10270-3 0  9105
2 25544  51
6424  18
2983 0003630  33
0826 327
0553 15
54214783 16067


Satellite: ISS
Catalog Number: 25544
Epoch time:      18023
84368770   =   yrday
fracday
Element set:     910
Inclination:       51
6424  deg
RA of node:        18
2983  deg
Eccentricity:     
0003630     
Arg of perigee:    33
0826  deg
Mean anomaly:     327
0553  deg
Mean motion:   15
54214783  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1606
Checksum:              296


Coasting Arc #12 (Orbit 1621)
---------------------------------------

Vector Time (GMT): 2018/024/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -32302
53                 A    =         6777310
33  meter
 Y    =        4258145
10  meter          E    =           
0005240
 Z    =        5267963
34                 I    =           51
71044
 XDOT =      -7555
277024                 Wp   =           74
20832
 YDOT =      -1063
257278  meter/sec      RA   =           12
84116  deg
 ZDOT =        813
834754                 TA   =            8
02954
                                          MA   =            8
02116
                                          Ha   =            221
937  n
mi
                                          Hp   =            213
648

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -105979
44                 X    =         -105504
63
 Y    =       13970292
31  feet           Y    =         4257374
58  meter
 Z    =       17283344
28                 Z    =         5267628
62
 XDOT =     -24787
654279                 XDOT =       -7546
779020
 YDOT =      -3488
376895  feet/sec       YDOT =       -1147
698047  meter/sec
 ZDOT =       2670
061528                 ZDOT =         777
154790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11921509
85                 X    =         3633676
20
 Y    =        7289372
54  feet           Y    =         2221800
75  meter
 Z    =       17281115
10                 Z    =         5267283
88
 XDOT =     -15077
647470                 XDOT =       -4595
666949
 YDOT =      18721
333363  feet/sec       YDOT =        5706
262409  meter/sec
 ZDOT =       2506
926125                 ZDOT =         764
111083


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   18024
87247133  
00016717  00000-0  10270-3 0  9119
2 25544  51
6422  13
1689 0003669  38
4133 321
7280 15
54205752 16226


Satellite: ISS
Catalog Number: 25544
Epoch time:      18024
87247133   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:        13
1689  deg
Eccentricity:     
0003669     
Arg of perigee:    38
4133  deg
Mean anomaly:     321
7280  deg
Mean motion:   15
54205752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1622
Checksum:              289


Coasting Arc #13 (Orbit 1636)
---------------------------------------

Vector Time (GMT): 2018/025/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1849950
72                 A    =         6777556
63  meter
 Y    =       -3915816
48  meter          E    =           
0016350
 Z    =       -5227390
99                 I    =           51
67767
 XDOT =       7320
349077                 Wp   =           87
71615
 YDOT =       1926
833972  meter/sec      RA   =            7
84410  deg
 ZDOT =       1151
004654                 TA   =          193
30915
                                          MA   =          193
35233
                                          Ha   =            221
915  n
mi
                                          Hp   =            213
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6069392
13                 X    =         1918992
66
 Y    =      -12847166
92  feet           Y    =        -3894742
96  meter
 Z    =      -17150232
92                 Z    =        -5218237
00
 XDOT =      24016
893297                 XDOT =        7292
667707
 YDOT =       6321
633768  feet/sec       YDOT =        2008
540342  meter/sec
 ZDOT =       3776
261987                 ZDOT =        1186
496896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8127015
42                 X    =        -2477114
30
 Y    =      -11715735
86  feet           Y    =        -3570956
29  meter
 Z    =      -17108794
86                 Z    =        -5214760
67
 XDOT =      16479
459526                 XDOT =        5022
939263
 YDOT =     -17158
378133  feet/sec       YDOT =       -5229
873655  meter/sec
 ZDOT =       3933
948503                 ZDOT =        1199
067504


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   18025
83695317  
00016717  00000-0  10270-3 0  9128
2 25544  51
6408   8
3603 0003660  40
8612 319
2814 15
54223198 16377


Satellite: ISS
Catalog Number: 25544
Epoch time:      18025
83695317   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:         8
3603  deg
Eccentricity:     
0003660     
Arg of perigee:    40
8612  deg
Mean anomaly:     319
2814  deg
Mean motion:   15
54223198  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1637
Checksum:              299


Coasting Arc #14 (Orbit 1652)
---------------------------------------

Vector Time (GMT): 2018/026/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3569998
14                 A    =         6780067
96  meter
 Y    =        3465727
67  meter          E    =           
0011935
 Z    =        4600105
27                 I    =           51
65436
 XDOT =      -6518
143490                 Wp   =           58
40371
 YDOT =      -2706
488410  meter/sec      RA   =            2
84918  deg
 ZDOT =      -3007
591124                 TA   =           61
64712
                                          MA   =           61
52681
                                          Ha   =            221
940  n
mi
                                          Hp   =            213
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11712592
33                 X    =        -3630832
21
 Y    =       11370497
60  feet           Y    =         3425465
22  meter
 Z    =       15092208
90                 Z    =         4582615
96
 XDOT =     -21384
985203                 XDOT =       -6472
785199
 YDOT =      -8879
555150  feet/sec       YDOT =       -2779
125051  meter/sec
 ZDOT =      -9867
424948                 ZDOT =       -3039
143655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4338058
17                 X    =         1322240
13
 Y    =       15811915
58  feet           Y    =         4819471
87  meter
 Z    =       15013739
75                 Z    =         4576187
87
 XDOT =     -16841
869215                 XDOT =       -5133
401737
 YDOT =      14160
038306  feet/sec       YDOT =        4315
979676  meter/sec
 ZDOT =     -10007
427194                 ZDOT =       -3050
263809


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   18026
86572979  
00016717  00000-0  10270-3 0  9131
2 25544  51
6415   3
2314 0003603  41
3240 318
8185 15
54255194 16533


Satellite: ISS
Catalog Number: 25544
Epoch time:      18026
86572979   =   yrday
fracday
Element set:     913
Inclination:       51
6415  deg
RA of node:         3
2314  deg
Eccentricity:     
0003603     
Arg of perigee:    41
3240  deg
Mean anomaly:     318
8185  deg
Mean motion:   15
54255194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1653
Checksum:              298


Coasting Arc #15 (Orbit 1667)
---------------------------------------

Vector Time (GMT): 2018/027/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4994528
87                 A    =         6783923
58  meter
 Y    =       -2966043
49  meter          E    =           
0007943
 Z    =       -3508419
73                 I    =           51
63314
 XDOT =       5178
712125                 Wp   =           73
11579
 YDOT =       3386
960325  meter/sec      RA   =          357
85960  deg
 ZDOT =       4519
696211                 TA   =          245
63073
                                          MA   =          245
71366
                                          Ha   =            221
990  n
mi
                                          Hp   =            213
583

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16386249
58                 X    =         5044366
63
 Y    =       -9731113
82  feet           Y    =        -2909912
43  meter
 Z    =      -11510563
42                 Z    =        -3484037
41
 XDOT =      16990
525346                 XDOT =        5118
499282
 YDOT =      11112
074558  feet/sec       YDOT =        3444
535353  meter/sec
 ZDOT =      14828
399643                 ZDOT =        4544
706225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1002878
90                 X    =         -305677
49
 Y    =      -19097040
26  feet           Y    =        -5820777
87  meter
 Z    =      -11401495
92                 Z    =        -3475175
96
 XDOT =      16279
713287                 XDOT =        4962
056610
 YDOT =      -9752
827728  feet/sec       YDOT =       -2972
661891  meter/sec
 ZDOT =      14939
151138                 ZDOT =        4553
453267


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   18027
83020600  
00016717  00000-0  10270-3 0  9149
2 25544  51
6405 358
4215 0003603  46
5320 313
6132 15
54226306 16687


Satellite: ISS
Catalog Number: 25544
Epoch time:      18027
83020600   =   yrday
fracday
Element set:     914
Inclination:       51
6405  deg
RA of node:       358
4215  deg
Eccentricity:     
0003603     
Arg of perigee:    46
5320  deg
Mean anomaly:     313
6132  deg
Mean motion:   15
54226306  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1668
Checksum:              270


Coasting Arc #16 (Orbit 1683)
---------------------------------------

Vector Time (GMT): 2018/028/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6039099
61                 A    =         6787326
19  meter
 Y    =        2350265
81  meter          E    =           
0015980
 Z    =        1998871
36                 I    =           51
61158
 XDOT =      -3418
219021                 Wp   =           99
76414
 YDOT =      -4018
187384  meter/sec      RA   =          352
88018  deg
 ZDOT =      -5567
449827                 TA   =           58
14707
                                          MA   =           57
99163
                                          Ha   =            221
993  n
mi
                                          Hp   =            213
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19813318
92                 X    =        -6074641
38
 Y    =        7710845
85  feet           Y    =         2282533
63  meter
 Z    =        6557976
91                 Z    =         1969449
79
 XDOT =     -11214
629333                 XDOT =       -3345
989222
 YDOT =     -13183
029475  feet/sec       YDOT =       -4056
008088  meter/sec
 ZDOT =     -18265
911506                 ZDOT =       -5583
878869

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1995408
25                 X    =         -608200
44
 Y    =       21207290
17  feet           Y    =         6463982
04  meter
 Z    =        6426585
49                 Z    =         1958823
26
 XDOT =     -15209
952388                 XDOT =       -4635
993488
 YDOT =       4161
880397  feet/sec       YDOT =        1268
541145  meter/sec
 ZDOT =     -18338
350311                 ZDOT =       -5589
529175


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   18028
85897607  
00016717  00000-0  10270-3 0  9152
2 25544  51
6401 353
2925 0003727  49
1963 310
9512 15
54259019 16840


Satellite: ISS
Catalog Number: 25544
Epoch time:      18028
85897607   =   yrday
fracday
Element set:     915
Inclination:       51
6401  deg
RA of node:       353
2925  deg
Eccentricity:     
0003727     
Arg of perigee:    49
1963  deg
Mean anomaly:     310
9512  deg
Mean motion:   15
54259019  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1684
Checksum:              326


Coasting Arc #17 (Orbit 1697)
---------------------------------------

Vector Time (GMT): 2018/029/16:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905759
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3132087
35                 A    =         6778496
98  meter
 Y    =        3383117
26  meter          E    =           
0008256
 Z    =        4962476
72                 I    =           51
55541
 XDOT =      -6699
377950                 Wp   =           98
21959
 YDOT =       3082
327285  meter/sec      RA   =          348
50324  deg
 ZDOT =       2122
815301                 TA   =          331
07452
                                          MA   =          331
12025
                                          Ha   =            221
984  n
mi
                                          Hp   =            213
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10275877
12                 X    =         3069919
05
 Y    =       11099466
09  feet           Y    =         3417794
55  meter
 Z    =       16281091
61                 Z    =         4977540
18
 XDOT =     -21979
586449                 XDOT =       -6743
658757
 YDOT =      10112
622325  feet/sec       YDOT =        3007
162552  meter/sec
 ZDOT =       6964
617128                 ZDOT =        2090
165342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13658704
46                 X    =         4163173
12
 Y    =        6329510
14  feet           Y    =         1929234
69  meter
 Z    =       16347563
61                 Z    =         4982737
39
 XDOT =     -15971
063899                 XDOT =       -4867
980276
 YDOT =      16818
233088  feet/sec       YDOT =        5126
197445  meter/sec
 ZDOT =       6818
729449                 ZDOT =        2078
348736


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   18029
75915023  
00016717  00000-0  10270-3 0  9166
2 25544  51
6422 348
8058 0003708  55
8539 304
2965 15
54223831 16988


Satellite: ISS
Catalog Number: 25544
Epoch time:      18029
75915023   =   yrday
fracday
Element set:     916
Inclination:       51
6422  deg
RA of node:       348
8058  deg
Eccentricity:     
0003708     
Arg of perigee:    55
8539  deg
Mean anomaly:     304
2965  deg
Mean motion:   15
54223831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1698
Checksum:              328
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