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

 
Date: May 10th 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) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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


132/22:41:24 349 -1 0 1 0 1 1
N/A -0 1 -0 1 222 0
000/00:02:44 698 0 0 -0 0 213 8

134/06:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 9

137/14:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 8

140/09:04:46 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 213 8

Coasting Arc #1 (Orbit 3249)
---------------------------------------

Vector Time (GMT): 2018/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1468635
20                 A    =         6780749
51  meter
 Y    =       -4935668
08  meter          E    =           
0011603
 Z    =        4402474
51                 I    =           51
43660
 XDOT =       6847
115386                 Wp   =           98
39796
 YDOT =        944
048990  meter/sec      RA   =          210
46168  deg
 ZDOT =       3333
341515                 TA   =          317
80960
                                          MA   =          317
89883
                                          Ha   =            221
833  n
mi
                                          Hp   =            213
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4818356
95                 X    =        -1434719
11
 Y    =      -16193136
74  feet           Y    =        -4951901
79  meter
 Z    =       14443814
02                 Z    =         4395422
65
 XDOT =      22464
289325                 XDOT =        6819
858148
 YDOT =       3097
273588  feet/sec       YDOT =        1020
465701  meter/sec
 ZDOT =      10936
159827                 ZDOT =        3366
536479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15111632
28                 X    =        -4606025
52
 Y    =       -7613429
75  feet           Y    =        -2320573
39  meter
 Z    =       14412919
97                 Z    =         4393058
01
 XDOT =      17135
159341                 XDOT =        5222
796567
 YDOT =     -12970
321693  feet/sec       YDOT =       -3953
354052  meter/sec
 ZDOT =      11084
215662                 ZDOT =        3378
468934


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   18129
55434548  
00016717  00000-0  10270-3 0  9006
2 25544  51
6408 211
2999 0003044  59
7407 300
4047 15
54259312 32507


Satellite: ISS
Catalog Number: 25544
Epoch time:      18129
55434548   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       211
2999  deg
Eccentricity:     
0003044     
Arg of perigee:    59
7407  deg
Mean anomaly:     300
4047  deg
Mean motion:   15
54259312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3250
Checksum:              297


Coasting Arc #2 (Orbit 3264)
---------------------------------------

Vector Time (GMT): 2018/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -200571
59                 A    =         6777917
40  meter
 Y    =        4436007
63  meter          E    =           
0016600
 Z    =       -5135603
42                 I    =           51
45497
 XDOT =      -7206
952511                 Wp   =           75
42352
 YDOT =      -2087
556668  meter/sec      RA   =          205
45308  deg
 ZDOT =      -1521
754461                 TA   =          179
85412
                                          MA   =          179
85364
                                          Ha   =            221
913  n
mi
                                          Hp   =            213
472

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -658043
28                 X    =         -225215
04
 Y    =       14553830
79  feet           Y    =         4433626
93  meter
 Z    =      -16849092
59                 Z    =        -5136637
57
 XDOT =     -23644
857321                 XDOT =       -7175
681296
 YDOT =      -6848
939199  feet/sec       YDOT =       -2167
974920  meter/sec
 ZDOT =      -4992
632745                 ZDOT =       -1556
687724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10335739
77                 X    =         3150333
48
 Y    =       10258969
40  feet           Y    =         3126933
87  meter
 Z    =      -16854226
86                 Z    =        -5137168
35
 XDOT =     -20283
477701                 XDOT =       -6182
404003
 YDOT =      11977
418393  feet/sec       YDOT =        3650
717126  meter/sec
 ZDOT =      -5148
331493                 ZDOT =       -1569
211439


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   18130
51880989  
00016717  00000-0  10270-3 0  9019
2 25544  51
6400 206
4920 0003116  61
3384 298
8082 15
54217122 32650


Satellite: ISS
Catalog Number: 25544
Epoch time:      18130
51880989   =   yrday
fracday
Element set:     901
Inclination:       51
6400  deg
RA of node:       206
4920  deg
Eccentricity:     
0003116     
Arg of perigee:    61
3384  deg
Mean anomaly:     298
8082  deg
Mean motion:   15
54217122  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3265
Checksum:              293


Coasting Arc #3 (Orbit 3280)
---------------------------------------

Vector Time (GMT): 2018/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1943750
29                 A    =         6776986
53  meter
 Y    =       -3764560
95  meter          E    =           
0005746
 Z    =        5284873
24                 I    =           51
48289
 XDOT =       7045
611408                 Wp   =           68
65339
 YDOT =       3006
133011  meter/sec      RA   =          200
44102  deg
 ZDOT =       -447
546086                 TA   =           25
63595
                                          MA   =           25
60747
                                          Ha   =            221
780  n
mi
                                          Hp   =            213
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6377133
50                 X    =         1960030
72
 Y    =      -12350921
74  feet           Y    =        -3742733
57  meter
 Z    =       17338822
97                 Z    =         5294354
96
 XDOT =      23115
522992                 XDOT =        7013
646332
 YDOT =       9862
641113  feet/sec       YDOT =        3084
743164  meter/sec
 ZDOT =      -1468
327053                 ZDOT =        -413
398149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5066059
87                 X    =        -1544135
05
 Y    =      -12886553
19  feet           Y    =        -3927821
41  meter
 Z    =       17381589
86                 Z    =         5297908
59
 XDOT =      21797
907510                 XDOT =        6644
002209
 YDOT =     -10355
488935  feet/sec       YDOT =       -3156
353028  meter/sec
 ZDOT =      -1316
223092                 ZDOT =        -401
184799


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   18131
54756759  
00016717  00000-0  10270-3 0  9021
2 25544  51
6402 201
3633 0003122  64
9601 295
1875 15
54269404 32813


Satellite: ISS
Catalog Number: 25544
Epoch time:      18131
54756759   =   yrday
fracday
Element set:     902
Inclination:       51
6402  deg
RA of node:       201
3633  deg
Eccentricity:     
0003122     
Arg of perigee:    64
9601  deg
Mean anomaly:     295
1875  deg
Mean motion:   15
54269404  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3281
Checksum:              298


Coasting Arc #4 (Orbit 3295)
---------------------------------------

Vector Time (GMT): 2018/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3612510
57                 A    =         6778795
18  meter
 Y    =        3030061
15  meter          E    =           
0014759
 Z    =       -4883872
07                 I    =           51
51944
 XDOT =      -6282
225682                 Wp   =           99
13085
 YDOT =      -3684
309941  meter/sec      RA   =          195
43231  deg
 ZDOT =       2364
848786                 TA   =          194
08467
                                          MA   =          194
12588
                                          Ha   =            221
948  n
mi
                                          Hp   =            213
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11852068
80                 X    =        -3622401
39
 Y    =        9941145
50  feet           Y    =         2989608
31  meter
 Z    =      -16023202
32                 Z    =        -4901444
68
 XDOT =     -20610
976648                 XDOT =       -6252
047188
 YDOT =     -12087
631040  feet/sec       YDOT =       -3754
393397  meter/sec
 ZDOT =       7758
690243                 ZDOT =        2334
404682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -114050
41                 X    =          -34762
57
 Y    =       15386783
77  feet           Y    =         4689891
69  meter
 Z    =      -16102012
27                 Z    =        -4907893
34
 XDOT =     -21510
232996                 XDOT =       -6556
319017
 YDOT =       7805
017485  feet/sec       YDOT =        2378
969329  meter/sec
 ZDOT =       7623
184882                 ZDOT =        2323
546752


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   18132
51202749  
00016717  00000-0  10270-3 0  9035
2 25544  51
6397 196
5549 0003293  67
2970 292
8531 15
54247857 32968


Satellite: ISS
Catalog Number: 25544
Epoch time:      18132
51202749   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       196
5549  deg
Eccentricity:     
0003293     
Arg of perigee:    67
2970  deg
Mean anomaly:     292
8531  deg
Mean motion:   15
54247857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3296
Checksum:              337


Coasting Arc #5 (Orbit 3302)
---------------------------------------

Vector Time (GMT): 2018/132/22:42:46
698
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1253617
16                 A    =         6777554
99  meter
 Y    =        4039954
74  meter          E    =           
0017157
 Z    =       -5310322
15                 I    =           51
52928
 XDOT =      -7397
977898                 Wp   =           87
14067
 YDOT =      -1952
497484  meter/sec      RA   =          193
22173  deg
 ZDOT =        262
616222                 TA   =          185
36128
                                          MA   =          185
37967
                                          Ha   =            221
982  n
mi
                                          Hp   =            213
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4112917
18                 X    =        -1272904
66
 Y    =       13254444
69  feet           Y    =         4025828
16  meter
 Z    =      -17422316
76                 Z    =        -5316458
69
 XDOT =     -24271
581031                 XDOT =       -7376
870377
 YDOT =      -6405
831642  feet/sec       YDOT =       -2035
108753  meter/sec
 ZDOT =        861
601779                 ZDOT =         226
730005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3275034
15                 X    =         -998230
41
 Y    =      -13449861
33  feet           Y    =        -4099517
73  meter
 Z    =      -17450183
23                 Z    =        -5318815
85
 XDOT =      23191
457424                 XDOT =        7068
756223
 YDOT =      -6550
688930  feet/sec       YDOT =       -1996
649986  meter/sec
 ZDOT =        701
590362                 ZDOT =         213
844742


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   18132
96210858  
00016717  00000-0  10270-3 0  9045
2 25544  51
6413 194
3124 0002690  58
0714 302
0700 15
54066381 33038


Satellite: ISS
Catalog Number: 25544
Epoch time:      18132
96210858   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       194
3124  deg
Eccentricity:     
0002690     
Arg of perigee:    58
0714  deg
Mean anomaly:     302
0700  deg
Mean motion:   15
54066381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3303
Checksum:              277


Coasting Arc #6 (Orbit 3318)
---------------------------------------

Vector Time (GMT): 2018/133/22:42:46
698
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2954048
66                 A    =         6778894
99  meter
 Y    =       -3548839
44  meter          E    =           
0008819
 Z    =        4958204
75                 I    =           51
56585
 XDOT =       6853
277386                 Wp   =           58
02530
 YDOT =       2705
185931  meter/sec      RA   =          188
21777  deg
 ZDOT =      -2139
507276                 TA   =           52
86981
                                          MA   =           52
78927
                                          Ha   =            221
849  n
mi
                                          Hp   =            213
853

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9691760
71                 X    =         2969428
35
 Y    =      -11643174
00  feet           Y    =        -3515719
40  meter
 Z    =       16267075
94                 Z    =         4972592
03
 XDOT =      22484
505861                 XDOT =        6832
910723
 YDOT =       8875
281927  feet/sec       YDOT =        2781
710190  meter/sec
 ZDOT =      -7019
380827                 ZDOT =       -2106
265110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2100273
72                 X    =         -640163
43
 Y    =       14932340
19  feet           Y    =         4551377
29  meter
 Z    =       16331734
53                 Z    =         4977912
68
 XDOT =     -22761
723278                 XDOT =       -6937
773255
 YDOT =       4340
023995  feet/sec       YDOT =        1322
839314  meter/sec
 ZDOT =      -6871
246046                 ZDOT =       -2094
355795


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   18133
99099149  
00016717  00000-0  10270-3 0  9058
2 25544  51
6407 189
1843 0002681  59
1480 300
9936 15
54096516 33191


Satellite: ISS
Catalog Number: 25544
Epoch time:      18133
99099149   =   yrday
fracday
Element set:     905
Inclination:       51
6407  deg
RA of node:       189
1843  deg
Eccentricity:     
0002681     
Arg of perigee:    59
1480  deg
Mean anomaly:     300
9936  deg
Mean motion:   15
54096516  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3319
Checksum:              333


Coasting Arc #7 (Orbit 3323)
---------------------------------------

Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2526415
48                 A    =         6778729
44  meter
 Y    =       -3741632
35  meter          E    =           
0007972
 Z    =        5051480
58                 I    =           51
57251
 XDOT =       7086
969359                 Wp   =           62
10447
 YDOT =       2291
970152  meter/sec      RA   =          186
61342  deg
 ZDOT =      -1840
894989                 TA   =           45
76312
                                          MA   =           45
69770
                                          Ha   =            222
044  n
mi
                                          Hp   =            213
887

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8288764
68                 X    =         2543529
70
 Y    =      -12275696
69  feet           Y    =        -3713284
74  meter
 Z    =       16573099
03                 Z    =         5063794
72
 XDOT =      23251
211808                 XDOT =        7069
755493
 YDOT =       7519
587114  feet/sec       YDOT =        2371
125347  meter/sec
 ZDOT =      -6039
681722                 ZDOT =       -1806
509920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13510944
31                 X    =         4118135
83
 Y    =       -5916967
89  feet           Y    =        -1803491
81  meter
 Z    =       16628524
75                 Z    =         5068374
34
 XDOT =      15114
912958                 XDOT =        4607
025470
 YDOT =      17917
176899  feet/sec       YDOT =        5461
155519  meter/sec
 ZDOT =      -5886
389740                 ZDOT =       -1794
171593


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   18134
31252031  
00016717  00000-0  10270-3 0  9067
2 25544  51
6381 187
5764 0002669  74
5163 285
6284 15
54020161 33245


Satellite: ISS
Catalog Number: 25544
Epoch time:      18134
31252031   =   yrday
fracday
Element set:     906
Inclination:       51
6381  deg
RA of node:       187
5764  deg
Eccentricity:     
0002669     
Arg of perigee:    74
5163  deg
Mean anomaly:     285
6284  deg
Mean motion:   15
54020161  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3324
Checksum:              296


Coasting Arc #8 (Orbit 3338)
---------------------------------------

Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4090554
98                 A    =         6781630
16  meter
 Y    =        3293275
04  meter          E    =           
0010729
 Z    =       -4301546
76                 I    =           51
61555
 XDOT =      -6108
038357                 Wp   =          103
40135
 YDOT =      -2974
694476  meter/sec      RA   =          181
61803  deg
 ZDOT =       3536
005081                 TA   =          202
65967
                                          MA   =          202
70707
                                          Ha   =            221
996  n
mi
                                          Hp   =            213
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13420455
97                 X    =        -4106182
14
 Y    =       10804708
12  feet           Y    =         3247444
53  meter
 Z    =      -14112686
23                 Z    =        -4321455
46
 XDOT =     -20039
495922                 XDOT =       -6091
496981
 YDOT =      -9759
496312  feet/sec       YDOT =       -3042
906500  meter/sec
 ZDOT =      11601
066540                 ZDOT =        3506
373667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17015076
18                 X    =        -5186195
22
 Y    =        2192926
77  feet           Y    =          668404
08  meter
 Z    =      -14201990
12                 Z    =        -4328766
59
 XDOT =     -11831
391143                 XDOT =       -3606
208020
 YDOT =     -17629
405116  feet/sec       YDOT =       -5373
442679  meter/sec
 ZDOT =      11469
066971                 ZDOT =        3495
771613


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   18135
27709561  
00016717  00000-0  10270-3 0  9079
2 25544  51
6383 182
7692 0002485  76
0921 284
0508 15
54048929 33399


Satellite: ISS
Catalog Number: 25544
Epoch time:      18135
27709561   =   yrday
fracday
Element set:     907
Inclination:       51
6383  deg
RA of node:       182
7692  deg
Eccentricity:     
0002485     
Arg of perigee:    76
0921  deg
Mean anomaly:     284
0508  deg
Mean motion:   15
54048929  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3339
Checksum:              332


Coasting Arc #9 (Orbit 3354)
---------------------------------------

Vector Time (GMT): 2018/136/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5371224
12                 A    =         6785448
35  meter
 Y    =       -2757624
09  meter          E    =           
0015456
 Z    =        3082040
08                 I    =           51
66162
 XDOT =       4674
357269                 Wp   =           93
12969
 YDOT =       3606
210106  meter/sec      RA   =          176
63299  deg
 ZDOT =      -4899
238836                 TA   =           51
44466
                                          MA   =           51
30625
                                          Ha   =            221
990  n
mi
                                          Hp   =            213
836

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17622126
37                 X    =         5386690
18
 Y    =       -9047323
12  feet           Y    =        -2697473
15  meter
 Z    =       10111680
05                 Z    =         3108169
50
 XDOT =      15335
817811                 XDOT =        4657
482647
 YDOT =      11831
397985  feet/sec       YDOT =        3658
388062  meter/sec
 ZDOT =     -16073
618227                 ZDOT =       -4876
572623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19713202
78                 X    =         6008584
21
 Y    =        1184174
21  feet           Y    =          360936
30  meter
 Z    =       10228725
93                 Z    =         3117715
66
 XDOT =       7323
928670                 XDOT =        2232
333459
 YDOT =      16618
457957  feet/sec       YDOT =        5065
305985  meter/sec
 ZDOT =     -15972
789511                 ZDOT =       -4868
506243


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   18136
30597480  
00016717  00000-0  10270-3 0  9080
2 25544  51
6387 177
6399 0002562  80
8761 279
2681 15
54045926 33551


Satellite: ISS
Catalog Number: 25544
Epoch time:      18136
30597480   =   yrday
fracday
Element set:     908
Inclination:       51
6387  deg
RA of node:       177
6399  deg
Eccentricity:     
0002562     
Arg of perigee:    80
8761  deg
Mean anomaly:     279
2681  deg
Mean motion:   15
54045926  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3355
Checksum:              345


Coasting Arc #10 (Orbit 3369)
---------------------------------------

Vector Time (GMT): 2018/137/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6227727
83                 A    =         6788421
08  meter
 Y    =        2178444
90  meter          E    =           
0010014
 Z    =       -1585780
46                 I    =           51
70456
 XDOT =      -2909
857034                 Wp   =           48
58482
 YDOT =      -4158
404965  meter/sec      RA   =          171
66066  deg
 ZDOT =       5745
106488                 TA   =          294
09155
                                          MA   =          294
19628
                                          Ha   =            222
038  n
mi
                                          Hp   =            213
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20432177
91                 X    =        -6243921
92
 Y    =        7147128
92  feet           Y    =         2108711
78  meter
 Z    =       -5202691
79                 Z    =        -1616072
22
 XDOT =      -9546
775046                 XDOT =       -2891
047515
 YDOT =     -13643
060909  feet/sec       YDOT =       -4190
840434  meter/sec
 ZDOT =      18848
774568                 ZDOT =        5731
016411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21257607
93                 X    =        -6479318
90
 Y    =       -3903861
84  feet           Y    =        -1189897
09  meter
 Z    =       -5338287
71                 Z    =        -1627110
09
 XDOT =      -1922
134838                 XDOT =        -585
866699
 YDOT =     -15091
488808  feet/sec       YDOT =       -4599
885789  meter/sec
 ZDOT =      18786
314122                 ZDOT =        5726
068544


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   18137
27054602  
00016717  00000-0  10270-3 0  9092
2 25544  51
6388 172
8323 0002648  80
2152 279
9300 15
54053037 33703


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
27054602   =   yrday
fracday
Element set:     909
Inclination:       51
6388  deg
RA of node:       172
8323  deg
Eccentricity:     
0002648     
Arg of perigee:    80
2152  deg
Mean anomaly:     279
9300  deg
Mean motion:   15
54053037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3370
Checksum:              299


Coasting Arc #11 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2018/137/14:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -986910
23                 A    =         6777578
40  meter
 Y    =       -4088230
87  meter          E    =           
0005122
 Z    =        5310452
63                 I    =           51
67597
 XDOT =       7518
435220                 Wp   =           88
60991
 YDOT =      -1513
705650  meter/sec      RA   =          169
98596  deg
 ZDOT =        231
856446                 TA   =          359
18221
                                          MA   =          359
18305
                                          Ha   =            222
131  n
mi
                                          Hp   =            213
798

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3237894
45                 X    =         -966916
93
 Y    =      -13412830
95  feet           Y    =        -4099155
99  meter
 Z    =       17422744
85                 Z    =         5305706
59
 XDOT =      24666
782218                 XDOT =        7533
676850
 YDOT =      -4966
225887  feet/sec       YDOT =       -1429
544138  meter/sec
 ZDOT =        760
683877                 ZDOT =         268
415810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13209053
09                 X    =        -4026119
38
 Y    =        4078053
62  feet           Y    =         1242990
74  meter
 Z    =       17402023
67                 Z    =         5304136
81
 XDOT =      -6003
687532                 XDOT =       -1829
923960
 YDOT =     -23391
135633  feet/sec       YDOT =       -7129
618141  meter/sec
 ZDOT =        924
213792                 ZDOT =         281
700364


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   18137
65637351  
00016717  00000-0  10270-3 0  9104
2 25544  51
6355 170
9123 0002759  74
7809 285
3648 15
54057260 33768


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
65637351   =   yrday
fracday
Element set:     910
Inclination:       51
6355  deg
RA of node:       170
9123  deg
Eccentricity:     
0002759     
Arg of perigee:    74
7809  deg
Mean anomaly:     285
3648  deg
Mean motion:   15
54057260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              326


Coasting Arc #12 (Orbit 3390)
---------------------------------------

Vector Time (GMT): 2018/138/14:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -771338
57                 A    =         6778473
33  meter
 Y    =        4391446
91  meter          E    =           
0016099
 Z    =       -5120029
90                 I    =           51
71148
 XDOT =      -7445
495574                 Wp   =           98
54996
 YDOT =        633
573510  meter/sec      RA   =          164
99134  deg
 ZDOT =       1667
238029                 TA   =          187
54554
                                          MA   =          187
56979
                                          Ha   =            222
139  n
mi
                                          Hp   =            213
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2530638
34                 X    =         -795516
95
 Y    =       14407634
23  feet           Y    =         4382686
69  meter
 Z    =      -16797998
37                 Z    =        -5123835
04
 XDOT =     -24427
478916                 XDOT =       -7460
125643
 YDOT =       2078
653248  feet/sec       YDOT =         550
230854  meter/sec
 ZDOT =       5469
941041                 ZDOT =        1631
034571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14542538
82                 X    =         4432565
83
 Y    =        1381825
16  feet           Y    =          421180
31  meter
 Z    =      -16815526
39                 Z    =        -5125372
44
 XDOT =       3925
977691                 XDOT =        1196
638000
 YDOT =      23191
032891  feet/sec       YDOT =        7068
626825  meter/sec
 ZDOT =       5308
076834                 ZDOT =        1617
901819


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   18138
62094367  
00016717  00000-0  10270-3 0  9117
2 25544  51
6358 166
1045 0002800  77
7133 282
4333 15
54043505 33914


Satellite: ISS
Catalog Number: 25544
Epoch time:      18138
62094367   =   yrday
fracday
Element set:     911
Inclination:       51
6358  deg
RA of node:       166
1045  deg
Eccentricity:     
0002800     
Arg of perigee:    77
7133  deg
Mean anomaly:     282
4333  deg
Mean motion:   15
54043505  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3391
Checksum:              295


Coasting Arc #13 (Orbit 3406)
---------------------------------------

Vector Time (GMT): 2018/139/14:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2432173
29                 A    =         6781259
39  meter
 Y    =       -4560685
62  meter          E    =           
0012100
 Z    =        4381926
19                 I    =           51
75324
 XDOT =       6861
044342                 Wp   =           72
77495
 YDOT =        367
415839  meter/sec      RA   =          160
00358  deg
 ZDOT =      -3414
521596                 TA   =           51
79748
                                          MA   =           51
68858
                                          Ha   =            222
017  n
mi
                                          Hp   =            213
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7979571
15                 X    =         2461706
16
 Y    =      -14962879
33  feet           Y    =        -4533322
75  meter
 Z    =       14376398
25                 Z    =         4393812
12
 XDOT =      22509
987998                 XDOT =        6873
011898
 YDOT =       1205
432543  feet/sec       YDOT =         444
208060  meter/sec
 ZDOT =     -11202
498673                 ZDOT =       -3381
163739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15602366
50                 X    =        -4755601
31
 Y    =       -6525442
03  feet           Y    =        -1988954
73  meter
 Z    =       14430069
51                 Z    =         4398285
19
 XDOT =      -1280
183893                 XDOT =        -390
200050
 YDOT =     -21463
650997  feet/sec       YDOT =       -6542
120824  meter/sec
 ZDOT =     -11053
445151                 ZDOT =       -3369
090082


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   18139
64981495  
00016717  00000-0  10270-3 0  9128
2 25544  51
6363 160
9755 0002736  79
3337 280
8123 15
54078621 34076


Satellite: ISS
Catalog Number: 25544
Epoch time:      18139
64981495   =   yrday
fracday
Element set:     912
Inclination:       51
6363  deg
RA of node:       160
9755  deg
Eccentricity:     
0002736     
Arg of perigee:    79
3337  deg
Mean anomaly:     280
8123  deg
Mean motion:   15
54078621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3407
Checksum:              328


Coasting Arc #14 (Orbit 3418)
---------------------------------------

Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1529499
37                 A    =         6780150
99  meter
 Y    =       -4681675
25  meter          E    =           
0010509
 Z    =        4653008
63                 I    =           51
77654
 XDOT =       7068
145085                 Wp   =           69
33849
 YDOT =       -604
971473  meter/sec      RA   =          156
17076  deg
 ZDOT =      -2923
131641                 TA   =           49
71685
                                          MA   =           49
62503
                                          Ha   =            221
914  n
mi
                                          Hp   =            213
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5018042
56                 X    =         1559135
56
 Y    =      -15359826
92  feet           Y    =        -4664406
10  meter
 Z    =       15265776
35                 Z    =         4660509
93
 XDOT =      23189
452380                 XDOT =        7088
583788
 YDOT =      -1984
814545  feet/sec       YDOT =        -525
816033  meter/sec
 ZDOT =      -9590
326906                 ZDOT =       -2888
747375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1253916
50                 X    =          382193
75
 Y    =      -16077644
25  feet           Y    =        -4900465
97  meter
 Z    =       15299869
62                 Z    =         4663400
26
 XDOT =      21000
500781                 XDOT =        6400
952638
 YDOT =      -7370
072262  feet/sec       YDOT =       -2246
398025  meter/sec
 ZDOT =      -9436
550540                 ZDOT =       -2876
260605


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   18140
42146572  
00016717  00000-0  10270-3 0  9136
2 25544  51
6393 157
1282 0002505  84
5686 275
5753 15
54107960 34193


Satellite: ISS
Catalog Number: 25544
Epoch time:      18140
42146572   =   yrday
fracday
Element set:     913
Inclination:       51
6393  deg
RA of node:       157
1282  deg
Eccentricity:     
0002505     
Arg of perigee:    84
5686  deg
Mean anomaly:     275
5753  deg
Mean motion:   15
54107960  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3419
Checksum:              313


Coasting Arc #15 (Orbit 3433)
---------------------------------------

Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2996296
42                 A    =         6783787
34  meter
 Y    =        4897594
37  meter          E    =           
0008262
 Z    =       -3621201
80                 I    =           51
81751
 XDOT =      -6229
693773                 Wp   =           96
46041
 YDOT =       -545
458367  meter/sec      RA   =          151
19420  deg
 ZDOT =       4424
681510                 TA   =          220
79948
                                          MA   =          220
86137
                                          Ha   =            222
049  n
mi
                                          Hp   =            213
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9830368
83                 X    =        -3033250
06
 Y    =       16068222
99  feet           Y    =         4863881
39  meter
 Z    =      -11880583
34                 Z    =        -3635846
14
 XDOT =     -20438
627864                 XDOT =       -6244
624094
 YDOT =      -1789
561572  feet/sec       YDOT =        -615
206930  meter/sec
 ZDOT =      14516
671621                 ZDOT =        4394
383479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5487665
28                 X    =        -1672640
38
 Y    =       17975968
09  feet           Y    =         5479075
07  meter
 Z    =      -11946644
00                 Z    =        -3641337
09
 XDOT =     -19030
160492                 XDOT =       -5800
392918
 YDOT =       3731
344757  feet/sec       YDOT =        1137
313882  meter/sec
 ZDOT =      14381
280322                 ZDOT =        4383
414242


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   18141
38603188  
00016717  00000-0  10270-3 0  9144
2 25544  51
6384 152
3209 0002800  90
3681 269
7792 15
54102507 34344


Satellite: ISS
Catalog Number: 25544
Epoch time:      18141
38603188   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       152
3209  deg
Eccentricity:     
0002800     
Arg of perigee:    90
3681  deg
Mean anomaly:     269
7792  deg
Mean motion:   15
54102507  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3434
Checksum:              302


Coasting Arc #16 (Orbit 3449)
---------------------------------------

Vector Time (GMT): 2018/142/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4189882
31                 A    =         6787307
65  meter
 Y    =       -4863371
22  meter          E    =           
0016404
 Z    =        2182267
63                 I    =           51
85836
 XDOT =       5018
781643                 Wp   =          106
10003
 YDOT =       1841
536239  meter/sec      RA   =          146
22877  deg
 ZDOT =      -5502
068330                 TA   =           49
74272
                                          MA   =           49
59938
                                          Ha   =            221
972  n
mi
                                          Hp   =            213
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13746333
05                 X    =         4233354
14
 Y    =      -15955942
32  feet           Y    =        -4816274
14  meter
 Z    =        7159670
70                 Z    =         2202725
95
 XDOT =      16465
819038                 XDOT =        5024
542268
 YDOT =       6041
785561  feet/sec       YDOT =        1897
692256  meter/sec
 ZDOT =     -18051
405281                 ZDOT =       -5477
674680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9014974
15                 X    =         2747764
12
 Y    =      -18998874
90  feet           Y    =        -5790857
07  meter
 Z    =        7251733
98                 Z    =         2210328
52
 XDOT =      16204
621555                 XDOT =        4939
168650
 YDOT =        803
704292  feet/sec       YDOT =         244
969068  meter/sec
 ZDOT =     -17942
554776                 ZDOT =       -5468
890696


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   18142
41489746  
00016717  00000-0  10270-3 0  9152
2 25544  51
6391 147
1920 0002655  89
3872 270
7585 15
54112562 34504


Satellite: ISS
Catalog Number: 25544
Epoch time:      18142
41489746   =   yrday
fracday
Element set:     915
Inclination:       51
6391  deg
RA of node:       147
1920  deg
Eccentricity:     
0002655     
Arg of perigee:    89
3872  deg
Mean anomaly:     270
7585  deg
Mean motion:   15
54112562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3450
Checksum:              320


Coasting Arc #17 (Orbit 3464)
---------------------------------------

Vector Time (GMT): 2018/143/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4988665
74                 A    =         6789389
45  meter
 Y    =        4563994
39  meter          E    =           
0012798
 Z    =        -560462
59                 I    =           51
89166
 XDOT =      -3566
032418                 Wp   =           50
67414
 YDOT =      -3173
157056  meter/sec      RA   =          141
27314  deg
 ZDOT =       6000
544348                 TA   =          303
29949
                                          MA   =          303
42200
                                          Ha   =            222
111  n
mi
                                          Hp   =            213
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16367013
57                 X    =        -5036608
36
 Y    =       14973734
89  feet           Y    =         4507939
66  meter
 Z    =       -1838788
04                 Z    =         -584812
14
 XDOT =     -11699
581425                 XDOT =       -3559
431883
 YDOT =     -10410
620264  feet/sec       YDOT =       -3212
998265  meter/sec
 ZDOT =      19686
825290                 ZDOT =        5983
237603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11511288
97                 X    =        -3508640
88
 Y    =       18951718
66  feet           Y    =         5776483
85  meter
 Z    =       -1948229
27                 Z    =         -593820
28
 XDOT =     -12887
685920                 XDOT =       -3928
166669
 YDOT =      -5843
692370  feet/sec       YDOT =       -1781
157434  meter/sec
 ZDOT =      19609
818157                 ZDOT =        5977
072574


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   18143
37945812  
00016717  00000-0  10270-3 0  9160
2 25544  51
6393 142
3843 0002771  89
8678 270
2792 15
54055308 34650


Satellite: ISS
Catalog Number: 25544
Epoch time:      18143
37945812   =   yrday
fracday
Element set:     916
Inclination:       51
6393  deg
RA of node:       142
3843  deg
Eccentricity:     
0002771     
Arg of perigee:    89
8678  deg
Mean anomaly:     270
2792  deg
Mean motion:   15
54055308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3465
Checksum:              334


Coasting Arc #18 (Orbit 3480)
---------------------------------------

Vector Time (GMT): 2018/144/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907497
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5419913
95                 A    =         6788872
46  meter
 Y    =       -3911575
06  meter          E    =           
0011532
 Z    =       -1166446
70                 I    =           51
91550
 XDOT =       1982
171800                 Wp   =          132
04357
 YDOT =       4489
648379  meter/sec      RA   =          136
32147  deg
 ZDOT =      -5890
209010                 TA   =           60
57239
                                          MA   =           60
45735
                                          Ha   =            222
115  n
mi
                                          Hp   =            213
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17781869
93                 X    =         5468917
47
 Y    =      -12833251
52  feet           Y    =        -3850691
80  meter
 Z    =       -3826924
85                 Z    =        -1139999
56
 XDOT =       6503
188319                 XDOT =        1960
431766
 YDOT =      14729
817516  feet/sec       YDOT =        4511
693087  meter/sec
 ZDOT =     -19324
832711                 ZDOT =       -5880
632838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13204763
19                 X    =         4024811
82
 Y    =      -17533291
79  feet           Y    =        -5344147
34  meter
 Z    =       -3708167
28                 Z    =        -1130249
39
 XDOT =       9418
476297                 XDOT =        2870
751575
 YDOT =      11139
358195  feet/sec       YDOT =        3395
276378  meter/sec
 ZDOT =     -19282
557012                 ZDOT =       -5877
323377


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   18144
40832007  
00016717  00000-0  10270-3 0  9177
2 25544  51
6394 137
2556 0002833  96
0806 264
0670 15
54098178 34813


Satellite: ISS
Catalog Number: 25544
Epoch time:      18144
40832007   =   yrday
fracday
Element set:     917
Inclination:       51
6394  deg
RA of node:       137
2556  deg
Eccentricity:     
0002833     
Arg of perigee:    96
0806  deg
Mean anomaly:     264
0670  deg
Mean motion:   15
54098178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3481
Checksum:              314
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