[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: May 7th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 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


128/07:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 213 4

131/03:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 4

132/22:41:21 823 -1 0 1 0 1 0
N/A -0 1 -0 1 222 0
000/00:02:39 647 -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 7

Coasting Arc #1 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2018/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4041321
91                 A    =         6787930
72  meter
 Y    =       -5184806
25  meter          E    =           
0017050
 Z    =        1657617
59                 I    =           51
40714
 XDOT =       4781
220975                 Wp   =           61
84629
 YDOT =      -1894
667521  meter/sec      RA   =          220
45559  deg
 ZDOT =       5693
631645                 TA   =          316
38322
                                          MA   =          316
51788
                                          Ha   =            221
866  n
mi
                                          Hp   =            213
579

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13258930
15                 X    =        -3991095
52
 Y    =      -17010519
19  feet           Y    =        -5229718
32  meter
 Z    =        5438377
92                 Z    =         1638107
92
 XDOT =      15686
420521                 XDOT =        4774
395472
 YDOT =      -6216
100792  feet/sec       YDOT =       -1841
238986  meter/sec
 ZDOT =      18679
893847                 ZDOT =        5716
840666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21400357
36                 X    =        -6522828
92
 Y    =       -2848571
50  feet           Y    =         -868244
59  meter
 Z    =        5351942
76                 Z    =         1631272
15
 XDOT =       6561
072961                 XDOT =        1999
815038
 YDOT =     -13769
117746  feet/sec       YDOT =       -4196
827089  meter/sec
 ZDOT =      18783
694844                 ZDOT =        5725
270188


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   18127
56111127  
00016717  00000-0  10270-3 0  9000
2 25544  51
6408 221
2378 0003166  52
9686 307
1756 15
54223339 32194


Satellite: ISS
Catalog Number: 25544
Epoch time:      18127
56111127   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       221
2378  deg
Eccentricity:     
0003166     
Arg of perigee:    52
9686  deg
Mean anomaly:     307
1756  deg
Mean motion:   15
54223339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3219
Checksum:              298


Coasting Arc #2 (Orbit 3230)
---------------------------------------

Vector Time (GMT): 2018/128/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -232555
99                 A    =         6778840
13  meter
 Y    =        4691161
99  meter          E    =           
0015272
 Z    =       -4902235
29                 I    =           51
39442
 XDOT =      -6778
676358                 Wp   =           70
12728
 YDOT =      -2726
614248  meter/sec      RA   =          216
39350  deg
 ZDOT =      -2288
382135                 TA   =          177
39017
                                          MA   =          177
38219
                                          Ha   =            221
927  n
mi
                                          Hp   =            213
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -762978
98                 X    =         -261183
94
 Y    =       15390951
41  feet           Y    =         4688401
45  meter
 Z    =      -16083449
10                 Z    =        -4903434
37
 XDOT =     -22239
751831                 XDOT =       -6736
566984
 YDOT =      -8945
584803  feet/sec       YDOT =       -2802
182564  meter/sec
 ZDOT =      -7507
815402                 ZDOT =       -2321
208599

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6445100
98                 X    =        -1964466
78
 Y    =       13990494
85  feet           Y    =         4264302
83  meter
 Z    =      -16089362
46                 Z    =        -4904037
68
 XDOT =     -16117
689597                 XDOT =       -4912
671789
 YDOT =     -16224
517288  feet/sec       YDOT =       -4945
232869  meter/sec
 ZDOT =      -7653
992370                 ZDOT =       -2332
936874


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   18128
33268931  
00016717  00000-0  10270-3 0  9013
2 25544  51
6375 217
3902 0003326  57
6043 302
5431 15
54239181 32318


Satellite: ISS
Catalog Number: 25544
Epoch time:      18128
33268931   =   yrday
fracday
Element set:     901
Inclination:       51
6375  deg
RA of node:       217
3902  deg
Eccentricity:     
0003326     
Arg of perigee:    57
6043  deg
Mean anomaly:     302
5431  deg
Mean motion:   15
54239181  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3231
Checksum:              285


Coasting Arc #3 (Orbit 3246)
---------------------------------------

Vector Time (GMT): 2018/129/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1839219
17                 A    =         6777151
79  meter
 Y    =       -3816874
49  meter          E    =           
0005456
 Z    =        5284752
64                 I    =           51
41619
 XDOT =       6692
250849                 Wp   =           81
49286
 YDOT =       3735
842579  meter/sec      RA   =          211
37660  deg
 ZDOT =        369
588767                 TA   =            4
97723
                                          MA   =            4
97181
                                          Ha   =            221
907  n
mi
                                          Hp   =            213
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6034183
63                 X    =         1856093
09
 Y    =      -12522554
10  feet           Y    =        -3796212
81  meter
 Z    =       17338427
30                 Z    =         5293727
92
 XDOT =      21956
203573                 XDOT =        6648
182975
 YDOT =      12256
701376  feet/sec       YDOT =        3810
433533  meter/sec
 ZDOT =       1212
561573                 ZDOT =         401
990652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10064342
22                 X    =         3067611
51
 Y    =       -9514634
86  feet           Y    =        -2900060
70  meter
 Z    =       17378939
37                 Z    =         5297100
72
 XDOT =      15300
428650                 XDOT =        4663
570652
 YDOT =      18659
786899  feet/sec       YDOT =        5687
503047  meter/sec
 ZDOT =       1356
744336                 ZDOT =         413
535674


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
36145554  
00016717  00000-0  10270-3 0  9023
2 25544  51
6379 212
2595 0003324  59
9793 300
1689 15
54213782 32474


Satellite: ISS
Catalog Number: 25544
Epoch time:      18129
36145554   =   yrday
fracday
Element set:     902
Inclination:       51
6379  deg
RA of node:       212
2595  deg
Eccentricity:     
0003324     
Arg of perigee:    59
9793  deg
Mean anomaly:     300
1689  deg
Mean motion:   15
54213782  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3247
Checksum:              321


Coasting Arc #4 (Orbit 3261)
---------------------------------------

Vector Time (GMT): 2018/130/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3427325
90                 A    =         6777810
67  meter
 Y    =        2853699
83  meter          E    =           
0016412
 Z    =       -5118298
99                 I    =           51
44827
 XDOT =      -6049
461330                 Wp   =           95
03297
 YDOT =      -4414
505746  meter/sec      RA   =          206
36270  deg
 ZDOT =       1592
558034                 TA   =          190
37493
                                          MA   =          190
40884
                                          Ha   =            221
960  n
mi
                                          Hp   =            213
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11244507
53                 X    =        -3434119
80
 Y    =        9362532
25  feet           Y    =         2815335
15  meter
 Z    =      -16792319
53                 Z    =        -5134964
39
 XDOT =     -19847
314076                 XDOT =       -6007
383389
 YDOT =     -14483
286569  feet/sec       YDOT =       -4481
919726  meter/sec
 ZDOT =       5224
927933                 ZDOT =        1563
273762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13691186
17                 X    =        -4173073
55
 Y    =        4912445
90  feet           Y    =         1497313
51  meter
 Z    =      -16867046
32                 Z    =        -5141075
72
 XDOT =     -13256
533012                 XDOT =       -4040
591262
 YDOT =     -19487
315998  feet/sec       YDOT =       -5939
733916  meter/sec
 ZDOT =       5094
721300                 ZDOT =        1552
871052


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
32591802  
00016717  00000-0  10270-3 0  9033
2 25544  51
6387 207
4519 0003357  64
2623 295
8876 15
54247113 32622


Satellite: ISS
Catalog Number: 25544
Epoch time:      18130
32591802   =   yrday
fracday
Element set:     903
Inclination:       51
6387  deg
RA of node:       207
4519  deg
Eccentricity:     
0003357     
Arg of perigee:    64
2623  deg
Mean anomaly:     295
8876  deg
Mean motion:   15
54247113  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3262
Checksum:              309


Coasting Arc #5 (Orbit 3274)
---------------------------------------

Vector Time (GMT): 2018/131/03:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         870169
89                 A    =         6778766
69  meter
 Y    =        4592092
79  meter          E    =           
0015443
 Z    =       -4924334
64                 I    =           51
47470
 XDOT =      -7246
439382                 Wp   =           70
47375
 YDOT =      -1033
696765  meter/sec      RA   =          202
25306  deg
 ZDOT =      -2245
166039                 TA   =          177
51635
                                          MA   =          177
50867
                                          Ha   =            221
950  n
mi
                                          Hp   =            213
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2854888
08                 X    =          842675
27
 Y    =       15065921
22  feet           Y    =         4601669
90  meter
 Z    =      -16155953
53                 Z    =        -4920174
38
 XDOT =     -23774
407422                 XDOT =       -7223
435774
 YDOT =      -3391
393586  feet/sec       YDOT =       -1114
602816  meter/sec
 ZDOT =      -7366
030313                 ZDOT =       -2280
311260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14416133
72                 X    =        -4394037
56
 Y    =        5281100
25  feet           Y    =         1609679
36  meter
 Z    =      -16137914
09                 Z    =        -4918836
21
 XDOT =         25
098048                 XDOT =           7
649885
 YDOT =     -22912
484445  feet/sec       YDOT =       -6983
725259  meter/sec
 ZDOT =      -7522
809080                 ZDOT =       -2292
952208


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
16178220  
00016717  00000-0  10270-3 0  9042
2 25544  51
6374 203
2872 0003398  58
2478 301
9005 15
54243419 32752


Satellite: ISS
Catalog Number: 25544
Epoch time:      18131
16178220   =   yrday
fracday
Element set:     904
Inclination:       51
6374  deg
RA of node:       203
2872  deg
Eccentricity:     
0003398     
Arg of perigee:    58
2478  deg
Mean anomaly:     301
9005  deg
Mean motion:   15
54243419  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3275
Checksum:              298


Coasting Arc #6 (Orbit 3290)
---------------------------------------

Vector Time (GMT): 2018/132/03:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907607
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         908385
99                 A    =         6777121
32  meter
 Y    =       -4126873
51  meter          E    =           
0005515
 Z    =        5293647
41                 I    =           51
50062
 XDOT =       7392
778846                 Wp   =           81
61935
 YDOT =       2031
597077  meter/sec      RA   =          197
24313  deg
 ZDOT =        315
723390                 TA   =            5
36993
                                          MA   =            5
36402
                                          Ha   =            221
955  n
mi
                                          Hp   =            213
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2980269
00                 X    =          928752
17
 Y    =      -13539611
25  feet           Y    =        -4116601
46  meter
 Z    =       17367609
60                 Z    =         5298109
54
 XDOT =      24254
523772                 XDOT =        7367
977883
 YDOT =       6665
344742  feet/sec       YDOT =        2114
129550  meter/sec
 ZDOT =       1035
837894                 ZDOT =         351
575256

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13829980
88                 X    =         4215378
17
 Y    =         475104
61  feet           Y    =          144811
89  meter
 Z    =       17388008
62                 Z    =         5299865
03
 XDOT =      -2326
601767                 XDOT =        -709
148219
 YDOT =      24027
008317  feet/sec       YDOT =        7323
432135  meter/sec
 ZDOT =       1195
672982                 ZDOT =         364
441125


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
19053845  
00016717  00000-0  10270-3 0  9052
2 25544  51
6381 198
1579 0003351  62
1050 298
0442 15
54219876 32914


Satellite: ISS
Catalog Number: 25544
Epoch time:      18132
19053845   =   yrday
fracday
Element set:     905
Inclination:       51
6381  deg
RA of node:       198
1579  deg
Eccentricity:     
0003351     
Arg of perigee:    62
1050  deg
Mean anomaly:     298
0442  deg
Mean motion:   15
54219876  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3291
Checksum:              310


Coasting Arc #7 (Orbit 3302)
---------------------------------------

Vector Time (GMT): 2018/132/22:42:41
647
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1219640
52                 A    =         6777520
75  meter
 Y    =        4048849
52  meter          E    =           
0017209
 Z    =       -5311459
07                 I    =           51
52935
 XDOT =      -7405
160154                 Wp   =           86
73967
 YDOT =      -1928
984436  meter/sec      RA   =          193
22273  deg
 ZDOT =        231
574637                 TA   =          185
46509
                                          MA   =          185
48390
                                          Ha   =            221
983  n
mi
                                          Hp   =            213
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4001445
27                 X    =        -1239024
48
 Y    =       13283627
04  feet           Y    =         4035102
35  meter
 Z    =      -17426046
81                 Z    =        -5317430
79
 XDOT =     -24295
144862                 XDOT =       -7384
164242
 YDOT =      -6328
689094  feet/sec       YDOT =       -2011
676645  meter/sec
 ZDOT =        759
759308                 ZDOT =         195
653260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3380985
42                 X    =        -1030524
36
 Y    =      -13419721
35  feet           Y    =        -4090331
07  meter
 Z    =      -17453178
38                 Z    =        -5319728
77
 XDOT =      23176
797284                 XDOT =        7064
287812
 YDOT =      -6612
155106  feet/sec       YDOT =       -2015
384876  meter/sec
 ZDOT =        599
588186                 ZDOT =         182
754479


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
96210313  
00016717  00000-0  10270-3 0  9063
2 25544  51
6414 194
3128 0002754  57
4079 302
7339 15
54076753 33030


Satellite: ISS
Catalog Number: 25544
Epoch time:      18132
96210313   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       194
3128  deg
Eccentricity:     
0002754     
Arg of perigee:    57
4079  deg
Mean anomaly:     302
7339  deg
Mean motion:   15
54076753  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3303
Checksum:              297


Coasting Arc #8 (Orbit 3318)
---------------------------------------

Vector Time (GMT): 2018/133/22:42:41
647
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2926799
92                 A    =         6778826
84  meter
 Y    =       -3559496
73  meter          E    =           
0008820
 Z    =        4966627
03                 I    =           51
56582
 XDOT =       6868
243398                 Wp   =           57
74185
 YDOT =       2687
167257  meter/sec      RA   =          188
21860  deg
 ZDOT =      -2114
204517                 TA   =           52
89526
                                          MA   =           52
81468
                                          Ha   =            221
850  n
mi
                                          Hp   =            213
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9602361
93                 X    =         2942259
89
 Y    =      -11678138
89  feet           Y    =        -3526680
96  meter
 Z    =       16294708
11                 Z    =         4980882
15
 XDOT =      22533
606949                 XDOT =        6847
954202
 YDOT =       8816
165540  feet/sec       YDOT =        2763
859308  meter/sec
 ZDOT =      -6936
366526                 ZDOT =       -2080
889463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2011107
18                 X    =         -612985
47
 Y    =       14914678
51  feet           Y    =         4545994
01  meter
 Z    =       16358777
69                 Z    =         4986155
44
 XDOT =     -22775
149518                 XDOT =       -6941
865573
 YDOT =       4400
492074  feet/sec       YDOT =        1341
269984  meter/sec
 ZDOT =      -6787
904170                 ZDOT =       -2068
953191


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
99097890  
00016717  00000-0  10270-3 0  9071
2 25544  51
6407 189
1847 0002745  58
5548 301
5873 15
54107868 33194


Satellite: ISS
Catalog Number: 25544
Epoch time:      18133
99097890   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       189
1847  deg
Eccentricity:     
0002745     
Arg of perigee:    58
5548  deg
Mean anomaly:     301
5873  deg
Mean motion:   15
54107868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3319
Checksum:              349


Coasting Arc #9 (Orbit 3323)
---------------------------------------

Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2535506
52                 A    =         6778705
66  meter
 Y    =       -3738636
58  meter          E    =           
0008057
 Z    =        5049084
80                 I    =           51
57263
 XDOT =       7082
857295                 Wp   =           61
89303
 YDOT =       2298
132284  meter/sec      RA   =          186
61371  deg
 ZDOT =      -1849
169145                 TA   =           46
05783
                                          MA   =           45
99138
                                          Ha   =            222
043  n
mi
                                          Hp   =            213
853

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8318590
94                 X    =         2552598
21
 Y    =      -12265868
05  feet           Y    =        -3710187
43  meter
 Z    =       16565238
85                 Z    =         5061443
05
 XDOT =      23237
720783                 XDOT =        7065
615020
 YDOT =       7539
804081  feet/sec       YDOT =        2377
241336  meter/sec
 ZDOT =      -6066
827903                 ZDOT =       -1814
804120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13530788
98                 X    =         4124184
48
 Y    =       -5892566
06  feet           Y    =        -1796054
13  meter
 Z    =       16620861
21                 Z    =         5066038
50
 XDOT =      15094
574760                 XDOT =        4600
826387
 YDOT =      17925
560273  feet/sec       YDOT =        5463
710771  meter/sec
 ZDOT =      -5913
626149                 ZDOT =       -1802
473250


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
31250535  
00016717  00000-0  10270-3 0  9086
2 25544  51
6382 187
5767 0002725  73
5980 286
5472 15
54031739 33240


Satellite: ISS
Catalog Number: 25544
Epoch time:      18134
31250535   =   yrday
fracday
Element set:     908
Inclination:       51
6382  deg
RA of node:       187
5767  deg
Eccentricity:     
0002725     
Arg of perigee:    73
5980  deg
Mean anomaly:     286
5472  deg
Mean motion:   15
54031739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3324
Checksum:              320


Coasting Arc #10 (Orbit 3338)
---------------------------------------

Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4102317
02                 A    =         6781618
77  meter
 Y    =        3287485
17  meter          E    =           
0010725
 Z    =       -4294707
32                 I    =           51
61572
 XDOT =      -6097
955244                 Wp   =          103
01699
 YDOT =      -2982
829663  meter/sec      RA   =          181
61826  deg
 ZDOT =       3546
620637                 TA   =          203
16869
                                          MA   =          203
21708
                                          Ha   =            221
995  n
mi
                                          Hp   =            213
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13459045
33                 X    =        -4117911
79
 Y    =       10785712
49  feet           Y    =         3241523
31  meter
 Z    =      -14090247
12                 Z    =        -4314673
08
 XDOT =     -20006
414843                 XDOT =       -6081
375214
 YDOT =      -9786
186557  feet/sec       YDOT =       -3050
928715  meter/sec
 ZDOT =      11635
894479                 ZDOT =        3517
038297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17038061
82                 X    =        -5193201
24
 Y    =        2156416
83  feet           Y    =          657275
85  meter
 Z    =      -14179805
17                 Z    =        -4322004
62
 XDOT =     -11792
082097                 XDOT =       -3594
226623
 YDOT =     -17633
183056  feet/sec       YDOT =       -5374
594196  meter/sec
 ZDOT =      11504
115045                 ZDOT =        3506
454266


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
27707316  
00016717  00000-0  10270-3 0  9097
2 25544  51
6384 182
7695 0002543  75
1259 285
0175 15
54061292 33391


Satellite: ISS
Catalog Number: 25544
Epoch time:      18135
27707316   =   yrday
fracday
Element set:     909
Inclination:       51
6384  deg
RA of node:       182
7695  deg
Eccentricity:     
0002543     
Arg of perigee:    75
1259  deg
Mean anomaly:     285
0175  deg
Mean motion:   15
54061292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3339
Checksum:              322


Coasting Arc #11 (Orbit 3354)
---------------------------------------

Vector Time (GMT): 2018/136/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5383686
03                 A    =         6785443
60  meter
 Y    =       -2747923
96  meter          E    =           
0015522
 Z    =        3068920
82                 I    =           51
66182
 XDOT =       4655
995436                 Wp   =           93
11308
 YDOT =       3615
627633  meter/sec      RA   =          176
63322  deg
 ZDOT =      -4909
776460                 TA   =           51
63465
                                          MA   =           51
49528
                                          Ha   =            221
988  n
mi
                                          Hp   =            213
796

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17663011
92                 X    =         5399106
43
 Y    =       -9015498
57  feet           Y    =        -2687633
93  meter
 Z    =       10068637
88                 Z    =         3095110
67
 XDOT =      15275
575576                 XDOT =        4639
068057
 YDOT =      11862
295385  feet/sec       YDOT =        3667
599961  meter/sec
 ZDOT =     -16108
190487                 ZDOT =       -4887
199573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19732355
48                 X    =         6014421
95
 Y    =        1232554
70  feet           Y    =          375682
67  meter
 Z    =       10185952
55                 Z    =         3104678
34
 XDOT =       7260
081985                 XDOT =        2212
872989
 YDOT =      16612
986183  feet/sec       YDOT =        5063
638189  meter/sec
 ZDOT =     -16007
761897                 ZDOT =       -4879
165826


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
30594376  
00016717  00000-0  10270-3 0  9104
2 25544  51
6388 177
6401 0002619  79
9284 280
2164 15
54059410 33559


Satellite: ISS
Catalog Number: 25544
Epoch time:      18136
30594376   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       177
6401  deg
Eccentricity:     
0002619     
Arg of perigee:    79
9284  deg
Mean anomaly:     280
2164  deg
Mean motion:   15
54059410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3355
Checksum:              317


Coasting Arc #12 (Orbit 3369)
---------------------------------------

Vector Time (GMT): 2018/137/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6237587
98                 A    =         6788405
80  meter
 Y    =        2164152
26  meter          E    =           
0010144
 Z    =       -1566106
12                 I    =           51
70474
 XDOT =      -2882
581942                 Wp   =           48
48929
 YDOT =      -4167
935851  meter/sec      RA   =          171
66091  deg
 ZDOT =       5752
063887                 TA   =          294
40849
                                          MA   =          294
51431
                                          Ha   =            222
036  n
mi
                                          Hp   =            213
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20464527
49                 X    =        -6253717
08
 Y    =        7100237
08  feet           Y    =         2094309
24  meter
 Z    =       -5138143
45                 Z    =        -1596445
62
 XDOT =      -9457
289836                 XDOT =       -2863
701669
 YDOT =     -13674
330219  feet/sec       YDOT =       -4200
065916  meter/sec
 ZDOT =      18871
600679                 ZDOT =        5738
106475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21262832
38                 X    =        -6480911
31
 Y    =       -3960829
54  feet           Y    =        -1207260
84  meter
 Z    =       -5273950
98                 Z    =        -1607500
26
 XDOT =      -1833
205007                 XDOT =        -558
760886
 YDOT =     -15073
982377  feet/sec       YDOT =       -4594
549829  meter/sec
 ZDOT =      18809
734088                 ZDOT =        5733
206950


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
27050637  
00016717  00000-0  10270-3 0  9119
2 25544  51
6389 172
8325 0002709  79
4172 280
7285 15
54067548 33700


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
27050637   =   yrday
fracday
Element set:     911
Inclination:       51
6389  deg
RA of node:       172
8325  deg
Eccentricity:     
0002709     
Arg of perigee:    79
4172  deg
Mean anomaly:     280
7285  deg
Mean motion:   15
54067548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3370
Checksum:              323


Coasting Arc #13 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2018/137/14:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -958947
70                 A    =         6777530
53  meter
 Y    =       -4093764
16  meter          E    =           
0005170
 Z    =        5311210
17                 I    =           51
67604
 XDOT =       7523
121780                 Wp   =           87
54862
 YDOT =      -1494
279402  meter/sec      RA   =          169
98580  deg
 ZDOT =        206
596996                 TA   =             
48478
                                          MA   =             
48428
                                          Ha   =            222
127  n
mi
                                          Hp   =            213
755

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3146153
86                 X    =         -938898
28
 Y    =      -13430984
79  feet           Y    =        -4104376
27  meter
 Z    =       17425230
20                 Z    =         5306600
10
 XDOT =      24682
158071                 XDOT =        7538
268531
 YDOT =      -4902
491477  feet/sec       YDOT =       -1410
066009  meter/sec
 ZDOT =        677
811666                 ZDOT =         243
178898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13232172
07                 X    =        -4033166
05
 Y    =        3987455
51  feet           Y    =         1215376
44  meter
 Z    =       17405117
21                 Z    =         5305079
72
 XDOT =      -5947
527444                 XDOT =       -1812
806365
 YDOT =     -23408
818416  feet/sec       YDOT =       -7135
007853  meter/sec
 ZDOT =        841
439979                 ZDOT =         256
470906


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
65633025  
00016717  00000-0  10270-3 0  9120
2 25544  51
6356 170
9125 0002823  74
1493 285
9971 15
54072126 33769


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
65633025   =   yrday
fracday
Element set:     912
Inclination:       51
6356  deg
RA of node:       170
9125  deg
Eccentricity:     
0002823     
Arg of perigee:    74
1493  deg
Mean anomaly:     285
9971  deg
Mean motion:   15
54072126  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              313


Coasting Arc #14 (Orbit 3390)
---------------------------------------

Vector Time (GMT): 2018/138/14:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -805105
50                 A    =         6778460
17  meter
 Y    =        4394241
17  meter          E    =           
0016096
 Z    =       -5112397
45                 I    =           51
71168
 XDOT =      -7440
943921                 Wp   =           98
52910
 YDOT =        608
215717  meter/sec      RA   =          164
99107  deg
 ZDOT =       1696
826356                 TA   =          187
85966
                                          MA   =          187
88491
                                          Ha   =            222
137  n
mi
                                          Hp   =            213
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2641422
24                 X    =         -829349
69
 Y    =       14416801
73  feet           Y    =         4385102
97  meter
 Z    =      -16772957
52                 Z    =        -5116366
78
 XDOT =     -24412
545673                 XDOT =       -7455
434497
 YDOT =       1995
458388  feet/sec       YDOT =         524
924737  meter/sec
 ZDOT =       5567
015603                 ZDOT =        1660
645344

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14559628
14                 X    =         4437774
66
 Y    =        1491831
05  feet           Y    =          454710
11  meter
 Z    =      -16791219
62                 Z    =        -5117963
74
 XDOT =       3850
002702                 XDOT =        1173
480824
 YDOT =      23181
488471  feet/sec       YDOT =        7065
717686  meter/sec
 ZDOT =       5405
254727                 ZDOT =        1647
521641


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
62089105  
00016717  00000-0  10270-3 0  9133
2 25544  51
6359 166
1046 0002865  77
1064 283
0409 15
54058986 33914


Satellite: ISS
Catalog Number: 25544
Epoch time:      18138
62089105   =   yrday
fracday
Element set:     913
Inclination:       51
6359  deg
RA of node:       166
1046  deg
Eccentricity:     
0002865     
Arg of perigee:    77
1064  deg
Mean anomaly:     283
0409  deg
Mean motion:   15
54058986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3391
Checksum:              321


Coasting Arc #15 (Orbit 3406)
---------------------------------------

Vector Time (GMT): 2018/139/14:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2469467
24                 A    =         6781279
78  meter
 Y    =       -4558541
38  meter          E    =           
0012250
 Z    =        4363217
96                 I    =           51
75356
 XDOT =       6844
036999                 Wp   =           72
98749
 YDOT =        399
145818  meter/sec      RA   =          160
00330  deg
 ZDOT =      -3445
048285                 TA   =           51
93837
                                          MA   =           51
82791
                                          Ha   =            222
013  n
mi
                                          Hp   =            213
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8101926
65                 X    =         2499064
25
 Y    =      -14955844
41  feet           Y    =        -4530761
10  meter
 Z    =       14315019
55                 Z    =         4375285
21
 XDOT =      22454
189628                 XDOT =        6855
799289
 YDOT =       1309
533522  feet/sec       YDOT =         475
746706  meter/sec
 ZDOT =     -11302
651855                 ZDOT =       -3411
773540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15606258
16                 X    =        -4756787
49
 Y    =       -6648340
41  feet           Y    =        -2026414
16  meter
 Z    =       14369500
98                 Z    =         4379823
90
 XDOT =      -1180
570754                 XDOT =        -359
837966
 YDOT =     -21417
687622  feet/sec       YDOT =       -6528
111187  meter/sec
 ZDOT =     -11153
973603                 ZDOT =       -3399
731154


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
64975174  
00016717  00000-0  10270-3 0  9147
2 25544  51
6364 160
9755 0002802  78
7548 281
3919 15
54095270 34076


Satellite: ISS
Catalog Number: 25544
Epoch time:      18139
64975174   =   yrday
fracday
Element set:     914
Inclination:       51
6364  deg
RA of node:       160
9755  deg
Eccentricity:     
0002802     
Arg of perigee:    78
7548  deg
Mean anomaly:     281
3919  deg
Mean motion:   15
54095270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3407
Checksum:              337


Coasting Arc #16 (Orbit 3418)
---------------------------------------

Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1572993
96                 A    =         6780171
84  meter
 Y    =       -4685226
92  meter          E    =           
0010679
 Z    =        4634844
58                 I    =           51
77687
 XDOT =       7055
985684                 Wp   =           69
55750
 YDOT =       -568
103435  meter/sec      RA   =          156
17032  deg
 ZDOT =      -2959
814835                 TA   =           49
89783
                                          MA   =           49
80427
                                          Ha   =            221
909  n
mi
                                          Hp   =            213
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5160741
34                 X    =         1602754
86
 Y    =      -15371479
40  feet           Y    =        -4667470
69  meter
 Z    =       15206183
01                 Z    =         4642557
47
 XDOT =      23149
559332                 XDOT =        7076
191211
 YDOT =      -1863
856415  feet/sec       YDOT =        -489
085270  meter/sec
 ZDOT =      -9710
678591                 ZDOT =       -2925
490197

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1390492
58                 X    =          423822
14
 Y    =      -16121888
78  feet           Y    =        -4913951
70  meter
 Z    =       15241222
53                 Z    =         4645524
63
 XDOT =      20987
034686                 XDOT =        6396
848172
 YDOT =      -7253
334366  feet/sec       YDOT =       -2210
816315  meter/sec
 ZDOT =      -9557
173194                 ZDOT =       -2913
026389


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
42139420  
00016717  00000-0  10270-3 0  9152
2 25544  51
6394 157
1282 0002570  83
8880 276
2565 15
54125073 34198


Satellite: ISS
Catalog Number: 25544
Epoch time:      18140
42139420   =   yrday
fracday
Element set:     915
Inclination:       51
6394  deg
RA of node:       157
1282  deg
Eccentricity:     
0002570     
Arg of perigee:    83
8880  deg
Mean anomaly:     276
2565  deg
Mean motion:   15
54125073  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3419
Checksum:              304


Coasting Arc #17 (Orbit 3433)
---------------------------------------

Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3040486
52                 A    =         6783830
89  meter
 Y    =        4893523
29  meter          E    =           
0008226
 Z    =       -3589606
53                 I    =           51
81792
 XDOT =      -6202
342065                 Wp   =           95
48351
 YDOT =       -589
830817  meter/sec      RA   =          151
19387  deg
 ZDOT =       4457
467919                 TA   =          222
23640
                                          MA   =          222
29979
                                          Ha   =            222
043  n
mi
                                          Hp   =            213
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9975349
48                 X    =        -3077544
83
 Y    =       16054866
45  feet           Y    =         4859315
56  meter
 Z    =      -11776924
32                 Z    =        -3604465
79
 XDOT =     -20348
891290                 XDOT =       -6216
937493
 YDOT =      -1935
140476  feet/sec       YDOT =        -659
271645  meter/sec
 ZDOT =      14624
238579                 ZDOT =        4427
303563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5632121
07                 X    =        -1716670
50
 Y    =       17998956
96  feet           Y    =         5486082
08  meter
 Z    =      -11843945
34                 Z    =        -3610034
54
 XDOT =     -18978
112998                 XDOT =       -5784
528842
 YDOT =       3578
849384  feet/sec       YDOT =        1090
833292  meter/sec
 ZDOT =      14489
450247                 ZDOT =        4416
384435


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
38594947  
00016717  00000-0  10270-3 0  9168
2 25544  51
6385 152
3209 0002862  89
7878 270
3603 15
54120458 34347


Satellite: ISS
Catalog Number: 25544
Epoch time:      18141
38594947   =   yrday
fracday
Element set:     916
Inclination:       51
6385  deg
RA of node:       152
3209  deg
Eccentricity:     
0002862     
Arg of perigee:    89
7878  deg
Mean anomaly:     270
3603  deg
Mean motion:   15
54120458  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3434
Checksum:              329


Coasting Arc #18 (Orbit 3449)
---------------------------------------

Vector Time (GMT): 2018/142/09:04:46
000
Vector Time (MET): N/A
Weight (LBS)     : 907500
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4230613
99                 A    =         6787336
60  meter
 Y    =       -4848098
27  meter          E    =           
0016472
 Z    =        2137270
30                 I    =           51
85873
 XDOT =       4974
874424                 Wp   =          106
47668
 YDOT =       1892
192779  meter/sec      RA   =          146
22858  deg
 ZDOT =      -5524
698252                 TA   =           49
89508
                                          MA   =           49
75082
                                          Ha   =            221
969  n
mi
                                          Hp   =            213
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13879967
17                 X    =         4274130
58
 Y    =      -15905834
20  feet           Y    =        -4800545
44  meter
 Z    =        7012041
68                 Z    =         2157926
60
 XDOT =      16321
766483                 XDOT =        4980
181782
 YDOT =       6207
981559  feet/sec       YDOT =        1947
855262  meter/sec
 ZDOT =     -18125
650432                 ZDOT =       -5500
518986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9158022
18                 X    =         2791365
16
 Y    =      -18985982
98  feet           Y    =        -5786927
61  meter
 Z    =        7104988
31                 Z    =         2165600
44
 XDOT =      16110
819274                 XDOT =        4910
577715
 YDOT =        991
394119  feet/sec       YDOT =         302
176927  meter/sec
 ZDOT =     -18017
764626                 ZDOT =       -5491
814658


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
41480288  
00016717  00000-0  10270-3 0  9176
2 25544  51
6392 147
1918 0002724  88
8514 271
2951 15
54131174 34509


Satellite: ISS
Catalog Number: 25544
Epoch time:      18142
41480288   =   yrday
fracday
Element set:     917
Inclination:       51
6392  deg
RA of node:       147
1918  deg
Eccentricity:     
0002724     
Arg of perigee:    88
8514  deg
Mean anomaly:     271
2951  deg
Mean motion:   15
54131174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3450
Checksum:              309
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