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

 
Date: May 14th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 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


137/14:37:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 213 3

138/21:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 4

140/09:04:46 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 4

142/00:19:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 4

144/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 4

146/20:57:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 6

148/06:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 8

Coasting Arc #1 (Orbit 3326)
---------------------------------------

Vector Time (GMT): 2018/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6056330
72                 A    =         6786433
14  meter
 Y    =        1533811
87  meter          E    =           
0008464
 Z    =       -2652793
54                 I    =           51
60684
 XDOT =      -3406
432866                 Wp   =           70
00178
 YDOT =      -4470
760790  meter/sec      RA   =          185
44972  deg
 ZDOT =       5208
301479                 TA   =          260
08631
                                          MA   =          260
18186
                                          Ha   =            222
479  n
mi
                                          Hp   =            213
280

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19869851
44                 X    =        -6060145
94
 Y    =        5032191
16  feet           Y    =         1466064
59  meter
 Z    =       -8703390
88                 Z    =        -2682222
95
 XDOT =     -11175
960848                 XDOT =       -3381
486165
 YDOT =     -14667
850360  feet/sec       YDOT =       -4508
714613  meter/sec
 ZDOT =      17087
603278                 ZDOT =        5191
814237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8458175
68                 X    =        -2578051
95
 Y    =       18608735
03  feet           Y    =         5671942
44  meter
 Z    =       -8834998
67                 Z    =        -2692907
60
 XDOT =     -17147
441373                 XDOT =       -5226
540130
 YDOT =        259
023024  feet/sec       YDOT =          78
950218  meter/sec
 ZDOT =      17014
490187                 ZDOT =        5186
016609


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
50543685  
00016717  00000-0  10270-3 0  9000
2 25544  51
6386 186
6192 0003886  87
0681 273
0916 15
54065806 33272


Satellite: ISS
Catalog Number: 25544
Epoch time:      18134
50543685   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:       186
6192  deg
Eccentricity:     
0003886     
Arg of perigee:    87
0681  deg
Mean anomaly:     273
0916  deg
Mean motion:   15
54065806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3327
Checksum:              326


Coasting Arc #2 (Orbit 3342)
---------------------------------------

Vector Time (GMT): 2018/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6656180
31                 A    =         6788965
57  meter
 Y    =        -772276
50  meter          E    =           
0016957
 Z    =        1045815
08                 I    =           51
64834
 XDOT =       1479
630813                 Wp   =          116
11490
 YDOT =       4677
608205  meter/sec      RA   =          180
47531  deg
 ZDOT =      -5896
195501                 TA   =           52
54477
                                          MA   =           52
39064
                                          Ha   =            222
480  n
mi
                                          Hp   =            213
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21837861
90                 X    =         6659241
28
 Y    =       -2533715
56  feet           Y    =         -697825
47  meter
 Z    =        3431151
85                 Z    =         1078156
61
 XDOT =       4854
431800                 XDOT =        1455
855798
 YDOT =      15346
483611  feet/sec       YDOT =        4694
021926  meter/sec
 ZDOT =     -19344
473427                 ZDOT =       -5889
065231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11338144
48                 X    =         3455866
44
 Y    =      -18808125
88  feet           Y    =        -5732716
77  meter
 Z    =        3575697
18                 Z    =         1089872
50
 XDOT =      13815
864733                 XDOT =        4211
075571
 YDOT =       4616
901118  feet/sec       YDOT =        1407
231461  meter/sec
 ZDOT =     -19313
171238                 ZDOT =       -5886
654593


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
53431844  
00016717  00000-0  10270-3 0  9018
2 25544  51
6387 181
4901 0003875  88
4115 271
7482 15
54081605 33435


Satellite: ISS
Catalog Number: 25544
Epoch time:      18135
53431844   =   yrday
fracday
Element set:     901
Inclination:       51
6387  deg
RA of node:       181
4901  deg
Eccentricity:     
0003875     
Arg of perigee:    88
4115  deg
Mean anomaly:     271
7482  deg
Mean motion:   15
54081605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3343
Checksum:              307


Coasting Arc #3 (Orbit 3358)
---------------------------------------

Vector Time (GMT): 2018/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6754240
76                 A    =         6789486
14  meter
 Y    =          38334
19  meter          E    =           
0016421
 Z    =         621137
30                 I    =           51
68224
 XDOT =        532
557202                 Wp   =           60
24821
 YDOT =      -4778
508543  meter/sec      RA   =          175
50730  deg
 ZDOT =       5975
419319                 TA   =          306
45448
                                          MA   =          306
60573
                                          Ha   =            222
621  n
mi
                                          Hp   =            213
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22159582
56                 X    =        -6757184
65
 Y    =         125768
33  feet           Y    =          -37212
90  meter
 Z    =        2037852
03                 Z    =          588319
73
 XDOT =       1747
234915                 XDOT =         556
926190
 YDOT =     -15677
521467  feet/sec       YDOT =       -4772
417418  meter/sec
 ZDOT =      19604
394090                 ZDOT =        5978
065097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13156669
73                 X    =        -4010152
94
 Y    =       17847716
89  feet           Y    =         5439984
11  meter
 Z    =        1891243
25                 Z    =          576450
94
 XDOT =     -10296
408825                 XDOT =       -3138
345410
 YDOT =      -9710
229201  feet/sec       YDOT =       -2959
677861  meter/sec
 ZDOT =      19616
775120                 ZDOT =        5979
193057


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
56319776  
00016717  00000-0  10270-3 0  9022
2 25544  51
6386 176
3617 0004008  89
0723 271
0889 15
54027288 33590


Satellite: ISS
Catalog Number: 25544
Epoch time:      18136
56319776   =   yrday
fracday
Element set:     902
Inclination:       51
6386  deg
RA of node:       176
3617  deg
Eccentricity:     
0004008     
Arg of perigee:    89
0723  deg
Mean anomaly:     271
0889  deg
Mean motion:   15
54027288  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3359
Checksum:              336


Coasting Arc #4 (Orbit 3373)
---------------------------------------

Vector Time (GMT): 2018/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6346816
80                 A    =         6787340
93  meter
 Y    =         766007
37  meter          E    =           
0009388
 Z    =       -2278403
71                 I    =           51
70872
 XDOT =      -2521
260505                 Wp   =          120
59207
 YDOT =       4773
975842  meter/sec      RA   =          170
53939  deg
 ZDOT =      -5439
641331                 TA   =           84
73157
                                          MA   =           84
62446
                                          Ha   =            222
573  n
mi
                                          Hp   =            213
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20822889
76                 X    =         6348846
84
 Y    =        2513147
53  feet           Y    =          836993
44  meter
 Z    =       -7475077
80                 Z    =        -2247567
57
 XDOT =      -8271
852051                 XDOT =       -2548
033697
 YDOT =      15662
650401  feet/sec       YDOT =        4745
632275  meter/sec
 ZDOT =     -17846
592294                 ZDOT =       -5451
953437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14229739
02                 X    =         4337224
45
 Y    =      -15474580
32  feet           Y    =        -4716652
08  meter
 Z    =       -7337392
45                 Z    =        -2236437
22
 XDOT =       6821
899034                 XDOT =        2079
314826
 YDOT =      14727
748201  feet/sec       YDOT =        4489
017652  meter/sec
 ZDOT =     -17902
168115                 ZDOT =       -5456
580841


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
52776486  
00016717  00000-0  10270-3 0  9035
2 25544  51
6390 171
5536 0003994  94
7119 265
4489 15
54081467 33746


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
52776486   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:       171
5536  deg
Eccentricity:     
0003994     
Arg of perigee:    94
7119  deg
Mean anomaly:     265
4489  deg
Mean motion:   15
54081467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3374
Checksum:              345


Coasting Arc #5 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2018/137/14:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         149946
63                 A    =         6777701
73  meter
 Y    =       -4255002
10  meter          E    =           
0006731
 Z    =        5267890
66                 I    =           51
67650
 XDOT =       7599
888718                 Wp   =           80
28836
 YDOT =       -711
168568  meter/sec      RA   =          169
96891  deg
 ZDOT =       -788
784911                 TA   =           17
25176
                                          MA   =           17
22890
                                          Ha   =            222
511  n
mi
                                          Hp   =            213
346

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         491950
90                 X    =          171927
06
 Y    =      -13959980
66  feet           Y    =        -4253202
99  meter
 Z    =       17283105
84                 Z    =         5268671
97
 XDOT =      24934
018104                 XDOT =        7611
107918
 YDOT =      -2333
230210  feet/sec       YDOT =        -626
118563  meter/sec
 ZDOT =      -2587
877005                 ZDOT =        -751
839548

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13953436
06                 X    =        -4253007
31
 Y    =         535331
53  feet           Y    =          163169
05  meter
 Z    =       17287101
13                 Z    =         5269108
42
 XDOT =      -3919
846681                 XDOT =       -1194
769268
 YDOT =     -23727
276797  feet/sec       YDOT =       -7232
073968  meter/sec
 ZDOT =      -2422
717455                 ZDOT =        -738
444280


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
65637346  
00016717  00000-0  10270-3 0  9041
2 25544  51
6354 170
9128 0003871  94
0139 266
1456 15
54067750 33768


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
65637346   =   yrday
fracday
Element set:     904
Inclination:       51
6354  deg
RA of node:       170
9128  deg
Eccentricity:     
0003871     
Arg of perigee:    94
0139  deg
Mean anomaly:     266
1456  deg
Mean motion:   15
54067750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              323


Coasting Arc #6 (Orbit 3390)
---------------------------------------

Vector Time (GMT): 2018/138/14:37:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1876702
00                 A    =         6779782
57  meter
 Y    =        4423930
83  meter          E    =           
0015290
 Z    =       -4796954
07                 I    =           51
71591
 XDOT =      -7190
485545                 Wp   =          105
77072
 YDOT =       -211
834434  meter/sec      RA   =          164
97640  deg
 ZDOT =       2620
657379                 TA   =          190
06770
                                          MA   =          190
09836
                                          Ha   =            222
547  n
mi
                                          Hp   =            213
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6157158
80                 X    =        -1902730
82
 Y    =       14514208
76  feet           Y    =         4402799
29  meter
 Z    =      -15738038
30                 Z    =        -4806133
23
 XDOT =     -23590
831841                 XDOT =       -7200
312238
 YDOT =       -694
994862  feet/sec       YDOT =        -292
298648  meter/sec
 ZDOT =       8597
957281                 ZDOT =        2585
704251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14962844
06                 X    =         4560674
87
 Y    =        4834942
94  feet           Y    =         1473690
61  meter
 Z    =      -15779586
00                 Z    =        -4809617
81
 XDOT =       1611
557596                 XDOT =         491
202755
 YDOT =      22532
746899  feet/sec       YDOT =        6867
981255  meter/sec
 ZDOT =       8441
781315                 ZDOT =        2573
054945


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
62093963  
00016717  00000-0  10270-3 0  9051
2 25544  51
6357 166
1050 0003917  96
8223 263
3376 15
54048827 33918


Satellite: ISS
Catalog Number: 25544
Epoch time:      18138
62093963   =   yrday
fracday
Element set:     905
Inclination:       51
6357  deg
RA of node:       166
1050  deg
Eccentricity:     
0003917     
Arg of perigee:    96
8223  deg
Mean anomaly:     263
3376  deg
Mean motion:   15
54048827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3391
Checksum:              323


Coasting Arc #7 (Orbit 3394)
---------------------------------------

Vector Time (GMT): 2018/138/21:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5872781
40                 A    =         6788323
84  meter
 Y    =        3014450
23  meter          E    =           
0010329
 Z    =       -1574016
48                 I    =           51
75744
 XDOT =      -3440
890964                 Wp   =           56
18725
 YDOT =      -3716
478279  meter/sec      RA   =          163
66052  deg
 ZDOT =       5753
388469                 TA   =          286
63629
                                          MA   =          286
74968
                                          Ha   =            222
370  n
mi
                                          Hp   =            213
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19267655
51                 X    =        -5898407
52
 Y    =        9889928
59  feet           Y    =         2948633
65  meter
 Z    =       -5164096
07                 Z    =        -1602606
55
 XDOT =     -11289
012349                 XDOT =       -3427
023715
 YDOT =     -12193
170207  feet/sec       YDOT =       -3754
879835  meter/sec
 ZDOT =      18875
946422                 ZDOT =        5736
706911

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17081239
09                 X    =         5206361
68
 Y    =      -13264415
89  feet           Y    =        -4042993
96  meter
 Z    =       -5292227
03                 Z    =        -1613070
80
 XDOT =      12497
581345                 XDOT =        3809
262794
 YDOT =       8633
969329  feet/sec       YDOT =        2631
633852  meter/sec
 ZDOT =      18801
838438                 ZDOT =        5730
800356


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
87815676  
00016717  00000-0  10270-3 0  9062
2 25544  51
6398 164
8238 0003695  97
1074 263
0499 15
54092873 33954


Satellite: ISS
Catalog Number: 25544
Epoch time:      18138
87815676   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       164
8238  deg
Eccentricity:     
0003695     
Arg of perigee:    97
1074  deg
Mean anomaly:     263
0499  deg
Mean motion:   15
54092873  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3395
Checksum:              360


Coasting Arc #8 (Orbit 3410)
---------------------------------------

Vector Time (GMT): 2018/139/21:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6357328
16                 A    =         6789562
86  meter
 Y    =       -2362216
27  meter          E    =           
0015221
 Z    =        -137810
98                 I    =           51
79289
 XDOT =       1546
523241                 Wp   =          127
93717
 YDOT =       4486
612140  meter/sec      RA   =          158
69980  deg
 ZDOT =      -6024
358364                 TA   =           53
54434
                                          MA   =           53
40415
                                          Ha   =            222
513  n
mi
                                          Hp   =            213
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20857375
84                 X    =         6383940
03
 Y    =       -7750053
38  feet           Y    =        -2290975
44  meter
 Z    =        -452135
75                 Z    =         -106864
77
 XDOT =       5073
895146                 XDOT =        1525
501047
 YDOT =      14719
856104  feet/sec       YDOT =        4503
789545  meter/sec
 ZDOT =     -19764
955262                 ZDOT =       -6016
896427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18874493
57                 X    =        -5752945
64
 Y    =       11787835
82  feet           Y    =         3592932
36  meter
 Z    =        -313528
83                 Z    =          -95563
59
 XDOT =      -7199
290553                 XDOT =       -2194
343760
 YDOT =     -11994
114054  feet/sec       YDOT =       -3655
805964  meter/sec
 ZDOT =     -19732
138570                 ZDOT =       -6014
355836


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
90702223  
00016717  00000-0  10270-3 0  9071
2 25544  51
6403 159
6953 0003771 102
2574 257
9001 15
54046963 34114


Satellite: ISS
Catalog Number: 25544
Epoch time:      18139
90702223   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:       159
6953  deg
Eccentricity:     
0003771     
Arg of perigee:   102
2574  deg
Mean anomaly:     257
9001  deg
Mean motion:   15
54046963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3411
Checksum:              299


Coasting Arc #9 (Orbit 3418)
---------------------------------------

Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1539037
65                 A    =         6780132
30  meter
 Y    =       -4681797
22  meter          E    =           
0011155
 Z    =        4648243
11                 I    =           51
77649
 XDOT =       7066
396047                 Wp   =           77
08584
 YDOT =       -596
471173  meter/sec      RA   =          156
17067  deg
 ZDOT =      -2932
116331                 TA   =           42
05931
                                          MA   =           41
97373
                                          Ha   =            222
293  n
mi
                                          Hp   =            213
382

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5049336
13                 X    =         1568697
64
 Y    =      -15360227
09  feet           Y    =        -4664421
27  meter
 Z    =       15250141
44                 Z    =         4655790
81
 XDOT =      23183
714066                 XDOT =        7086
783471
 YDOT =      -1956
926419  feet/sec       YDOT =        -517
335577  meter/sec
 ZDOT =      -9619
804237                 ZDOT =       -2897
740685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1284379
37                 X    =          391478
83
 Y    =      -16085253
63  feet           Y    =        -4902785
31  meter
 Z    =       15284442
12                 Z    =         4658697
96
 XDOT =      21000
962800                 XDOT =        6401
093461
 YDOT =      -7343
880476  feet/sec       YDOT =       -2238
414769  meter/sec
 ZDOT =      -9466
067422                 ZDOT =       -2885
257350


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
42145035  
00016717  00000-0  10270-3 0  9083
2 25544  51
6392 157
1285 0003647 105
4204 254
7352 15
54119536 34198


Satellite: ISS
Catalog Number: 25544
Epoch time:      18140
42145035   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:       157
1285  deg
Eccentricity:     
0003647     
Arg of perigee:   105
4204  deg
Mean anomaly:     254
7352  deg
Mean motion:   15
54119536  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3419
Checksum:              295


Coasting Arc #10 (Orbit 3433)
---------------------------------------

Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3010516
11                 A    =         6783777
13  meter
 Y    =        4897121
09  meter          E    =           
0009374
 Z    =       -3611946
06                 I    =           51
81751
 XDOT =      -6220
336436                 Wp   =          103
39630
 YDOT =       -559
073177  meter/sec      RA   =          151
19406  deg
 ZDOT =       4434
135376                 TA   =          214
00668
                                          MA   =          214
06679
                                          Ha   =            222
412  n
mi
                                          Hp   =            213
257

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9877021
34                 X    =        -3047508
36
 Y    =       16066670
25  feet           Y    =         4863248
88  meter
 Z    =      -11850216
74                 Z    =        -3626659
57
 XDOT =     -20407
927941                 XDOT =       -6235
161130
 YDOT =      -1834
229582  feet/sec       YDOT =        -628
716510  meter/sec
 ZDOT =      14547
688240                 ZDOT =        4403
883055

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5533452
75                 X    =        -1686596
40
 Y    =       17986020
82  feet           Y    =         5482139
15  meter
 Z    =      -11916586
59                 Z    =        -3632175
59
 XDOT =     -19010
891182                 XDOT =       -5794
519632
 YDOT =       3683
877111  feet/sec       YDOT =        1122
845744  meter/sec
 ZDOT =      14412
502939                 ZDOT =        4392
930896


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
38600853  
00016717  00000-0  10270-3 0  9094
2 25544  51
6383 152
3211 0003961 108
9980 251
1602 15
54116258 34346


Satellite: ISS
Catalog Number: 25544
Epoch time:      18141
38600853   =   yrday
fracday
Element set:     909
Inclination:       51
6383  deg
RA of node:       152
3211  deg
Eccentricity:     
0003961     
Arg of perigee:   108
9980  deg
Mean anomaly:     251
1602  deg
Mean motion:   15
54116258  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3434
Checksum:              294


Coasting Arc #11 (Orbit 3443)
---------------------------------------

Vector Time (GMT): 2018/142/00:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2033951
12                 A    =         6777466
44  meter
 Y    =        3676267
96  meter          E    =           
0018521
 Z    =       -5334052
18                 I    =           51
81178
 XDOT =      -6572
877605                 Wp   =           95
45306
 YDOT =       3918
615036  meter/sec      RA   =          148
05915  deg
 ZDOT =        193
268123                 TA   =          176
39445
                                          MA   =          176
38108
                                          Ha   =            222
402  n
mi
                                          Hp   =            213
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6673067
97                 X    =         2018600
96
 Y    =       12061246
59  feet           Y    =         3698927
53  meter
 Z    =      -17500171
19                 Z    =        -5324208
97
 XDOT =     -21564
559073                 XDOT =       -6617
146917
 YDOT =      12856
348542  feet/sec       YDOT =        3844
865053  meter/sec
 ZDOT =        634
081768                 ZDOT =         161
232063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13822334
13                 X    =        -4213047
44
 Y    =         685252
86  feet           Y    =          208865
07  meter
 Z    =      -17456603
48                 Z    =        -5320772
74
 XDOT =      -1815
430222                 XDOT =        -553
343132
 YDOT =     -24031
983316  feet/sec       YDOT =       -7324
948515  meter/sec
 ZDOT =        490
371214                 ZDOT =         149
465146


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
02904428  
00016717  00000-0  10270-3 0  9103
2 25544  51
6358 149
1134 0003829 110
3056 249
8508 15
54095227 34442


Satellite: ISS
Catalog Number: 25544
Epoch time:      18142
02904428   =   yrday
fracday
Element set:     910
Inclination:       51
6358  deg
RA of node:       149
1134  deg
Eccentricity:     
0003829     
Arg of perigee:   110
3056  deg
Mean anomaly:     249
8508  deg
Mean motion:   15
54095227  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3444
Checksum:              299


Coasting Arc #12 (Orbit 3459)
---------------------------------------

Vector Time (GMT): 2018/143/00:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -478145
23                 A    =         6778900
74  meter
 Y    =       -4550144
70  meter          E    =           
0008681
 Z    =        4995322
63                 I    =           51
84433
 XDOT =       6741
487360                 Wp   =           78
52361
 YDOT =      -3010
410926  meter/sec      RA   =          143
07338  deg
 ZDOT =      -2092
085635                 TA   =           31
78857
                                          MA   =           31
73619
                                          Ha   =            222
445  n
mi
                                          Hp   =            213
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1568717
93                 X    =         -451493
45
 Y    =      -14928296
26  feet           Y    =        -4555342
88  meter
 Z    =       16388853
76                 Z    =         4993064
46
 XDOT =      22117
740684                 XDOT =        6784
811840
 YDOT =      -9876
676265  feet/sec       YDOT =       -2934
780621  meter/sec
 ZDOT =      -6863
798016                 ZDOT =       -2059
232642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14190420
00                 X    =         4325240
02
 Y    =        4925414
13  feet           Y    =         1501266
23  meter
 Z    =       16379307
33                 Z    =         4992412
87
 XDOT =       -289
159000                 XDOT =         -88
135663
 YDOT =      23220
585932  feet/sec       YDOT =        7077
634592  meter/sec
 ZDOT =      -6716
526006                 ZDOT =       -2047
197127


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
05789873  
00016717  00000-0  10270-3 0  9113
2 25544  51
6363 143
9843 0003791 113
9190 246
2360 15
54071296 34608


Satellite: ISS
Catalog Number: 25544
Epoch time:      18143
05789873   =   yrday
fracday
Element set:     911
Inclination:       51
6363  deg
RA of node:       143
9843  deg
Eccentricity:     
0003791     
Arg of perigee:   113
9190  deg
Mean anomaly:     246
2360  deg
Mean motion:   15
54071296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3460
Checksum:              315


Coasting Arc #13 (Orbit 3474)
---------------------------------------

Vector Time (GMT): 2018/144/00:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -971389
32                 A    =         6782017
17  meter
 Y    =        5268819
26  meter          E    =           
0011752
 Z    =       -4170811
48                 I    =           51
88065
 XDOT =      -6422
267411                 Wp   =          112
65073
 YDOT =       1793
476670  meter/sec      RA   =          138
09583  deg
 ZDOT =       3765
430940                 TA   =          196
01411
                                          MA   =          196
05129
                                          Ha   =            222
406  n
mi
                                          Hp   =            213
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3186972
84                 X    =        -1009974
76
 Y    =       17286152
43  feet           Y    =         5257740
95  meter
 Z    =      -13683764
70                 Z    =        -4175623
67
 XDOT =     -21070
431137                 XDOT =       -6460
135842
 YDOT =       5884
109811  feet/sec       YDOT =        1721
446553  meter/sec
 ZDOT =      12353
776049                 ZDOT =        3734
141680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14433085
95                 X    =        -4399204
60
 Y    =      -10002340
14  feet           Y    =        -3048713
27  meter
 Z    =      -13705929
37                 Z    =        -4177567
27
 XDOT =       2712
073136                 XDOT =         826
639892
 YDOT =     -20631
278373  feet/sec       YDOT =       -6288
413648  meter/sec
 ZDOT =      12213
628737                 ZDOT =        3722
714039


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
02244624  
00016717  00000-0  10270-3 0  9122
2 25544  51
6361 139
1756 0003998 117
5474 242
6085 15
54103792 34757


Satellite: ISS
Catalog Number: 25544
Epoch time:      18144
02244624   =   yrday
fracday
Element set:     912
Inclination:       51
6361  deg
RA of node:       139
1756  deg
Eccentricity:     
0003998     
Arg of perigee:   117
5474  deg
Mean anomaly:     242
6085  deg
Mean motion:   15
54103792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3475
Checksum:              313


Coasting Arc #14 (Orbit 3482)
---------------------------------------

Vector Time (GMT): 2018/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3096521
33                 A    =         6787011
82  meter
 Y    =       -5565582
51  meter          E    =           
0017523
 Z    =        2320764
11                 I    =           51
90931
 XDOT =       5370
155764                 Wp   =          108
81695
 YDOT =        710
111522  meter/sec      RA   =          135
68605  deg
 ZDOT =      -5434
332918                 TA   =           45
39748
                                          MA   =           45
25465
                                          Ha   =            222
286  n
mi
                                          Hp   =            213
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10159190
71                 X    =         3147253
91
 Y    =      -18259785
13  feet           Y    =        -5530671
51  meter
 Z    =        7614055
48                 Z    =         2335929
05
 XDOT =      17618
621274                 XDOT =        5388
213332
 YDOT =       2329
762210  feet/sec       YDOT =         770
265504  meter/sec
 ZDOT =     -17829
176241                 ZDOT =       -5408
202448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11119461
79                 X    =        -3389211
95
 Y    =      -17661782
73  feet           Y    =        -5383311
38  meter
 Z    =        7682561
42                 Z    =         2341644
72
 XDOT =       9306
154333                 XDOT =        2836
515841
 YDOT =     -13603
025199  feet/sec       YDOT =       -4146
202081  meter/sec
 ZDOT =     -17712
401030                 ZDOT =       -5398
739834


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
53686927  
00016717  00000-0  10270-3 0  9135
2 25544  51
6361 136
6148 0003736 114
2856 245
8687 15
54127035 34830


Satellite: ISS
Catalog Number: 25544
Epoch time:      18144
53686927   =   yrday
fracday
Element set:     913
Inclination:       51
6361  deg
RA of node:       136
6148  deg
Eccentricity:     
0003736     
Arg of perigee:   114
2856  deg
Mean anomaly:     245
8687  deg
Mean motion:   15
54127035  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3483
Checksum:              329


Coasting Arc #15 (Orbit 3497)
---------------------------------------

Vector Time (GMT): 2018/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3971993
32                 A    =         6789058
72  meter
 Y    =        5456869
08  meter          E    =           
0011795
 Z    =        -703781
45                 I    =           51
93908
 XDOT =      -4203
952819                 Wp   =           59
84546
 YDOT =      -2298
615598  meter/sec      RA   =          130
73364  deg
 ZDOT =       5984
038266                 TA   =          292
58550
                                          MA   =          292
71025
                                          Ha   =            222
315  n
mi
                                          Hp   =            213
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13031474
15                 X    =        -4029299
68
 Y    =       17903113
79  feet           Y    =         5412131
13  meter
 Z    =       -2308994
26                 Z    =         -723215
17
 XDOT =     -13792
496125                 XDOT =       -4207
004278
 YDOT =      -7541
389756  feet/sec       YDOT =       -2345
644453  meter/sec
 ZDOT =      19632
671476                 ZDOT =        5963
609146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9748409
62                 X    =         2971315
25
 Y    =       19872018
01  feet           Y    =         6056991
09  meter
 Z    =       -2396594
75                 Z    =         -730482
08
 XDOT =     -11721
424037                 XDOT =       -3572
690047
 YDOT =       8076
128807  feet/sec       YDOT =        2461
604060  meter/sec
 ZDOT =      19541
585964                 ZDOT =        5956
275402


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   18145
50141333  
00016717  00000-0  10270-3 0  9141
2 25544  51
6360 131
8072 0003991 120
6069 239
5478 15
54141993 34985


Satellite: ISS
Catalog Number: 25544
Epoch time:      18145
50141333   =   yrday
fracday
Element set:     914
Inclination:       51
6360  deg
RA of node:       131
8072  deg
Eccentricity:     
0003991     
Arg of perigee:   120
6069  deg
Mean anomaly:     239
5478  deg
Mean motion:   15
54141993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3498
Checksum:              310


Coasting Arc #16 (Orbit 3513)
---------------------------------------

Vector Time (GMT): 2018/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4549311
57                 A    =         6788924
80  meter
 Y    =       -4924245
35  meter          E    =           
0013334
 Z    =       -1036770
12                 I    =           51
95987
 XDOT =       2895
962321                 Wp   =          135
96053
 YDOT =       3911
557895  meter/sec      RA   =          125
78384  deg
 ZDOT =      -5925
874547                 TA   =           55
22882
                                          MA   =           55
10338
                                          Ha   =            222
325  n
mi
                                          Hp   =            213
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14925562
88                 X    =         4609073
87
 Y    =      -16155660
59  feet           Y    =        -4873037
59  meter
 Z    =       -3401476
78                 Z    =        -1014525
98
 XDOT =       9501
188718                 XDOT =        2880
792173
 YDOT =      12833
195193  feet/sec       YDOT =        3943
858098  meter/sec
 ZDOT =     -19441
845626                 ZDOT =       -5911
843353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7657358
25                 X    =        -2333962
79
 Y    =      -20635255
44  feet           Y    =        -6289625
86  meter
 Z    =       -3301353
97                 Z    =        -1006252
69
 XDOT =      14293
580471                 XDOT =        4356
683328
 YDOT =      -2233
315836  feet/sec       YDOT =        -680
714667  meter/sec
 ZDOT =     -19379
580101                 ZDOT =       -5906
896015


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   18146
53025504  
00016717  00000-0  10270-3 0  9157
2 25544  51
6368 126
6770 0003781 120
9389 239
2135 15
54119230 35140


Satellite: ISS
Catalog Number: 25544
Epoch time:      18146
53025504   =   yrday
fracday
Element set:     915
Inclination:       51
6368  deg
RA of node:       126
6770  deg
Eccentricity:     
0003781     
Arg of perigee:   120
9389  deg
Mean anomaly:     239
2135  deg
Mean motion:   15
54119230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3514
Checksum:              301


Coasting Arc #17 (Orbit 3519)
---------------------------------------

Vector Time (GMT): 2018/146/20:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1039568
76                 A    =         6780399
32  meter
 Y    =       -4882548
44  meter          E    =           
0010783
 Z    =        4580009
59                 I    =           51
94021
 XDOT =       5686
817221                 Wp   =           82
09996
 YDOT =      -4120
060589  meter/sec      RA   =          123
89879  deg
 ZDOT =      -3093
772671                 TA   =           38
73847
                                          MA   =           38
66120
                                          Ha   =            222
148  n
mi
                                          Hp   =            213
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3410658
67                 X    =        -1007141
12
 Y    =      -16018859
73  feet           Y    =        -4893992
63  meter
 Z    =       15026278
20                 Z    =         4575038
07
 XDOT =      18657
536815                 XDOT =        5747
494356
 YDOT =     -13517
259151  feet/sec       YDOT =       -4056
127196  meter/sec
 ZDOT =     -10150
172805                 ZDOT =       -3066
000571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8257645
80                 X    =         2516930
44
 Y    =       14166751
71  feet           Y    =         4318025
92  meter
 Z    =       15004663
53                 Z    =         4573421
44
 XDOT =     -12637
356357                 XDOT =       -3851
866218
 YDOT =      18011
193261  feet/sec       YDOT =        5489
811706  meter/sec
 ZDOT =     -10025
417879                 ZDOT =       -3055
747370


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   18146
91606752  
00016717  00000-0  10270-3 0  9160
2 25544  51
6381 124
7534 0003410 124
4260 235
7215 15
54142876 35207


Satellite: ISS
Catalog Number: 25544
Epoch time:      18146
91606752   =   yrday
fracday
Element set:     916
Inclination:       51
6381  deg
RA of node:       124
7534  deg
Eccentricity:     
0003410     
Arg of perigee:   124
4260  deg
Mean anomaly:     235
7215  deg
Mean motion:   15
54142876  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3520
Checksum:              291


Coasting Arc #18 (Orbit 3534)
---------------------------------------

Vector Time (GMT): 2018/147/20:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -96595
92                 A    =         6784164
91  meter
 Y    =        5821051
31  meter          E    =           
0008208
 Z    =       -3492256
03                 I    =           51
96854
 XDOT =      -5547
714004                 Wp   =          108
45563
 YDOT =       2646
329488  meter/sec      RA   =          118
93224  deg
 ZDOT =       4570
730124                 TA   =          210
77112
                                          MA   =          210
81926
                                          Ha   =            222
130  n
mi
                                          Hp   =            213
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -316915
76                 X    =         -144717
52
 Y    =       19097937
36  feet           Y    =         5819702
36  meter
 Z    =      -11457532
91                 Z    =        -3492841
62
 XDOT =     -18201
161431                 XDOT =       -5599
096221
 YDOT =       8682
183360  feet/sec       YDOT =        2584
003418  meter/sec
 ZDOT =      14995
833740                 ZDOT =        4543
656253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5946039
07                 X    =        -1812352
71
 Y    =      -18149348
55  feet           Y    =        -5531921
44  meter
 Z    =      -11460910
70                 Z    =        -3493285
58
 XDOT =      13186
315515                 XDOT =        4019
188969
 YDOT =     -13699
939715  feet/sec       YDOT =       -4175
741625  meter/sec
 ZDOT =      14874
373249                 ZDOT =        4533
708966


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   18147
88060308  
00016717  00000-0  10270-3 0  9179
2 25544  51
6365 119
9446 0003568 129
4653 230
6816 15
54126759 35351


Satellite: ISS
Catalog Number: 25544
Epoch time:      18147
88060308   =   yrday
fracday
Element set:     917
Inclination:       51
6365  deg
RA of node:       119
9446  deg
Eccentricity:     
0003568     
Arg of perigee:   129
4653  deg
Mean anomaly:     230
6816  deg
Mean motion:   15
54126759  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3535
Checksum:              334


Coasting Arc #19 (Orbit 3540)
---------------------------------------

Vector Time (GMT): 2018/148/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3805187
15                 A    =         6777450
95  meter
 Y    =        1745928
89  meter          E    =           
0017699
 Z    =       -5344806
06                 I    =           51
95352
 XDOT =      -3373
470948                 Wp   =           97
26468
 YDOT =       6870
331264  meter/sec      RA   =          117
08986  deg
 ZDOT =       -160
086257                 TA   =          171
22923
                                          MA   =          171
19827
                                          Ha   =            222
190  n
mi
                                          Hp   =            213
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12484209
80                 X    =         3811343
55
 Y    =        5728113
15  feet           Y    =         1788516
06  meter
 Z    =      -17535452
97                 Z    =        -5326306
36
 XDOT =     -11067
818071                 XDOT =       -3449
268521
 YDOT =      22540
456902  feet/sec       YDOT =        6832
182994  meter/sec
 ZDOT =       -525
217379                 ZDOT =        -176
657099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8973389
86                 X    =         2735089
23
 Y    =       10537206
99  feet           Y    =         3211740
69  meter
 Z    =      -17452920
35                 Z    =        -5319650
12
 XDOT =     -18823
705453                 XDOT =       -5737
465422
 YDOT =      15050
245803  feet/sec       YDOT =        4587
314921  meter/sec
 ZDOT =       -600
251494                 ZDOT =        -182
956655


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   18148
26641699  
00016717  00000-0  10270-3 0  9181
2 25544  51
6383 118
0218 0003714 133
1268 227
0196 15
54101136 35415


Satellite: ISS
Catalog Number: 25544
Epoch time:      18148
26641699   =   yrday
fracday
Element set:     918
Inclination:       51
6383  deg
RA of node:       118
0218  deg
Eccentricity:     
0003714     
Arg of perigee:   133
1268  deg
Mean anomaly:     227
0196  deg
Mean motion:   15
54101136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              300


Coasting Arc #20 (Orbit 3556)
---------------------------------------

Vector Time (GMT): 2018/149/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922320
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2950189
95                 A    =         6778263
26  meter
 Y    =       -3339309
69  meter          E    =           
0006849
 Z    =        5102069
48                 I    =           51
97189
 XDOT =       4043
319366                 Wp   =           87
04379
 YDOT =      -6277
451654  meter/sec      RA   =          112
11273  deg
 ZDOT =      -1768
231380                 TA   =           19
97965
                                          MA   =           19
95285
                                          Ha   =            222
162  n
mi
                                          Hp   =            213
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9679100
88                 X    =        -2937413
14
 Y    =      -10955740
46  feet           Y    =        -3372229
91  meter
 Z    =       16739073
10                 Z    =         5087768
90
 XDOT =      13265
483484                 XDOT =        4121
804303
 YDOT =     -20595
313826  feet/sec       YDOT =       -6231
797427  meter/sec
 ZDOT =      -5801
284055                 ZDOT =       -1748
400153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4449861
87                 X    =        -1356317
90
 Y    =      -14001248
98  feet           Y    =        -4267580
69  meter
 Z    =       16675537
99                 Z    =         5082703
98
 XDOT =      19545
700519                 XDOT =        5957
529518
 YDOT =     -13024
014340  feet/sec       YDOT =       -3969
719571  meter/sec
 ZDOT =      -5711
717246                 ZDOT =       -1740
931416


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   18149
29524686  
00016717  00000-0  10270-3 0  9192
2 25544  51
6393 112
8930 0003640 136
4940 223
6500 15
54157387 35577


Satellite: ISS
Catalog Number: 25544
Epoch time:      18149
29524686   =   yrday
fracday
Element set:     919
Inclination:       51
6393  deg
RA of node:       112
8930  deg
Eccentricity:     
0003640     
Arg of perigee:   136
4940  deg
Mean anomaly:     223
6500  deg
Mean motion:   15
54157387  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3557
Checksum:              323
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