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

 
Date: May 25th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 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


146/20:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

148/06:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 6

153/12:25:00 000 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

154/09:16:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 214 0

156/19:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 214 1

157/11:12:41 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 214 2

159/13:07:21 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 214 3

Coasting Arc #1 (Orbit 3497)
---------------------------------------

Vector Time (GMT): 2018/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3947370
48                 A    =         6789095
84  meter
 Y    =        5470175
50  meter          E    =           
0011783
 Z    =        -738636
40                 I    =           51
93927
 XDOT =      -4233
412892                 Wp   =           59
54314
 YDOT =      -2257
945615  meter/sec      RA   =          130
73318  deg
 ZDOT =       5978
705553                 TA   =          292
51067
                                          MA   =          292
63536
                                          Ha   =            222
354  n
mi
                                          Hp   =            213
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12950690
56                 X    =        -4004658
16
 Y    =       17946770
00  feet           Y    =         5425713
00  meter
 Z    =       -2423347
78                 Z    =         -757950
47
 XDOT =     -13889
149908                 XDOT =       -4236
891040
 YDOT =      -7407
958053  feet/sec       YDOT =       -2305
306299  meter/sec
 ZDOT =      19615
175699                 ZDOT =        5958
132290

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9825093
64                 X    =         2994688
54
 Y    =       19820315
50  feet           Y    =         6041232
17  meter
 Z    =       -2510414
74                 Z    =         -765174
41
 XDOT =     -11652
319189                 XDOT =       -3551
626889
 YDOT =       8218
225920  feet/sec       YDOT =        2504
915260  meter/sec
 ZDOT =      19523
440415                 ZDOT =        5950
744639


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
50148080  
00016717  00000-0  10270-3 0  9002
2 25544  51
6362 131
8073 0003982 119
1445 241
0107 15
54121639 34981


Satellite: ISS
Catalog Number: 25544
Epoch time:      18145
50148080   =   yrday
fracday
Element set:     900
Inclination:       51
6362  deg
RA of node:       131
8073  deg
Eccentricity:     
0003982     
Arg of perigee:   119
1445  deg
Mean anomaly:     241
0107  deg
Mean motion:   15
54121639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3498
Checksum:              287


Coasting Arc #2 (Orbit 3513)
---------------------------------------

Vector Time (GMT): 2018/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4529063
09                 A    =         6789021
72  meter
 Y    =       -4951444
85  meter          E    =           
0013421
 Z    =        -995510
73                 I    =           51
96025
 XDOT =       2936
334509                 Wp   =          135
46283
 YDOT =       3867
506977  meter/sec      RA   =          125
78352  deg
 ZDOT =      -5934
883284                 TA   =           55
27566
                                          MA   =           55
14933
                                          Ha   =            222
367  n
mi
                                          Hp   =            213
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14859130
86                 X    =         4588930
62
 Y    =      -16244897
81  feet           Y    =        -4900462
95  meter
 Z    =       -3266111
31                 Z    =         -973364
69
 XDOT =       9633
643401                 XDOT =        2921
697710
 YDOT =      12688
671186  feet/sec       YDOT =        3900
261633  meter/sec
 ZDOT =     -19471
401849                 ZDOT =       -5920
654680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7767379
03                 X    =        -2367497
13
 Y    =      -20615516
98  feet           Y    =        -6283609
58  meter
 Z    =       -3166423
90                 Z    =         -965126
00
 XDOT =      14226
035339                 XDOT =        4336
095571
 YDOT =      -2408
934794  feet/sec       YDOT =        -734
243325  meter/sec
 ZDOT =     -19408
247721                 ZDOT =       -5915
633905


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
53033623  
00016717  00000-0  10270-3 0  9013
2 25544  51
6370 126
6772 0003778 119
3990 240
7540 15
54097749 35148


Satellite: ISS
Catalog Number: 25544
Epoch time:      18146
53033623   =   yrday
fracday
Element set:     901
Inclination:       51
6370  deg
RA of node:       126
6772  deg
Eccentricity:     
0003778     
Arg of perigee:   119
3990  deg
Mean anomaly:     240
7540  deg
Mean motion:   15
54097749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3514
Checksum:              315


Coasting Arc #3 (Orbit 3519)
---------------------------------------

Vector Time (GMT): 2018/146/20:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -738853
73                 A    =         6781099
56  meter
 Y    =       -5090495
70  meter          E    =           
0011746
 Z    =        4409339
90                 I    =           51
94266
 XDOT =       5746
587505                 Wp   =           83
60902
 YDOT =      -3784
465899  meter/sec      RA   =          123
89412  deg
 ZDOT =      -3397
147398                 TA   =           40
64511
                                          MA   =           40
55749
                                          Ha   =            222
175  n
mi
                                          Hp   =            213
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2424060
78                 X    =         -703294
07
 Y    =      -16701101
38  feet           Y    =        -5098559
56  meter
 Z    =       14466338
24                 Z    =         4405836
76
 XDOT =      18853
633546                 XDOT =        5804
981143
 YDOT =     -12416
226704  feet/sec       YDOT =       -3719
876860  meter/sec
 ZDOT =     -11145
496713                 ZDOT =       -3369
090473

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7590710
63                 X    =         2313648
60
 Y    =       15087024
48  feet           Y    =         4598525
06  meter
 Z    =       14451318
44                 Z    =         4404761
86
 XDOT =     -13023
850634                 XDOT =       -3969
669673
 YDOT =      17136
216621  feet/sec       YDOT =        5223
118826  meter/sec
 ZDOT =     -11019
510568                 ZDOT =       -3358
746821


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
91615415  
00016717  00000-0  10270-3 0  9021
2 25544  51
6383 124
7535 0003390 122
5009 237
6471 15
54123869 35203


Satellite: ISS
Catalog Number: 25544
Epoch time:      18146
91615415   =   yrday
fracday
Element set:     902
Inclination:       51
6383  deg
RA of node:       124
7535  deg
Eccentricity:     
0003390     
Arg of perigee:   122
5009  deg
Mean anomaly:     237
6471  deg
Mean motion:   15
54123869  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3520
Checksum:              298


Coasting Arc #4 (Orbit 3534)
---------------------------------------

Vector Time (GMT): 2018/147/20:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -380481
29                 A    =         6784919
51  meter
 Y    =        5946860
32  meter          E    =           
0007546
 Z    =       -3252414
12                 I    =           51
97108
 XDOT =      -5532
101823                 Wp   =          102
23571
 YDOT =       2262
306655  meter/sec      RA   =          118
92971  deg
 ZDOT =       4791
481532                 TA   =          220
30440
                                          MA   =          220
36036
                                          Ha   =            222
180  n
mi
                                          Hp   =            213
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1248298
19                 X    =         -431153
66
 Y    =       19510696
58  feet           Y    =         5942322
48  meter
 Z    =      -10670650
00                 Z    =        -3254384
93
 XDOT =     -18149
940364                 XDOT =       -5580
263263
 YDOT =       7422
265928  feet/sec       YDOT =        2200
173159  meter/sec
 ZDOT =      15720
083766                 ZDOT =        4764
491289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5275629
51                 X    =        -1608011
88
 Y    =      -18819896
01  feet           Y    =        -5736304
30  meter
 Z    =      -10680241
02                 Z    =        -3255337
46
 XDOT =      13444
106333                 XDOT =        4097
763610
 YDOT =     -12606
568821  feet/sec       YDOT =       -3842
482177  meter/sec
 ZDOT =      15599
047384                 ZDOT =        4754
589643


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
88070465  
00016717  00000-0  10270-3 0  9039
2 25544  51
6366 119
9449 0003554 127
8246 232
3229 15
54100484 35354


Satellite: ISS
Catalog Number: 25544
Epoch time:      18147
88070465   =   yrday
fracday
Element set:     903
Inclination:       51
6366  deg
RA of node:       119
9449  deg
Eccentricity:     
0003554     
Arg of perigee:   127
8246  deg
Mean anomaly:     232
3229  deg
Mean motion:   15
54100484  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3535
Checksum:              317


Coasting Arc #5 (Orbit 3541)
---------------------------------------

Vector Time (GMT): 2018/148/06:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4705465
07                 A    =         6779854
62  meter
 Y    =        1023899
06  meter          E    =           
0011419
 Z    =        4766746
48                 I    =           51
96215
 XDOT =       1218
840805                 Wp   =          121
86576
 YDOT =      -7072
680605  meter/sec      RA   =          116
97171  deg
 ZDOT =       2711
764455                 TA   =          301
41347
                                          MA   =          301
52509
                                          Ha   =            222
349  n
mi
                                          Hp   =            213
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15437877
51                 X    =        -4739719
58
 Y    =        3359248
90  feet           Y    =          971087
31  meter
 Z    =       15638932
04                 Z    =         4743805
50
 XDOT =       3998
821539                 XDOT =        1284
666335
 YDOT =     -23204
332695  feet/sec       YDOT =       -7058
682905  meter/sec
 ZDOT =       8896
865010                 ZDOT =        2717
844435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15879669
58                 X    =        -4840123
29
 Y    =        -807729
22  feet           Y    =         -246195
87  meter
 Z    =       15536166
77                 Z    =         4735423
63
 XDOT =       9794
542567                 XDOT =        2985
376574
 YDOT =     -20215
851667  feet/sec       YDOT =       -6161
791588  meter/sec
 ZDOT =       8924
993454                 ZDOT =        2720
338005


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
33082752  
00016717  00000-0  10270-3 0  9043
2 25544  51
6383 117
7018 0003752 130
2982 229
8499 15
54111642 35422


Satellite: ISS
Catalog Number: 25544
Epoch time:      18148
33082752   =   yrday
fracday
Element set:     904
Inclination:       51
6383  deg
RA of node:       117
7018  deg
Eccentricity:     
0003752     
Arg of perigee:   130
2982  deg
Mean anomaly:     229
8499  deg
Mean motion:   15
54111642  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3542
Checksum:              309


Coasting Arc #6 (Orbit 3556)
---------------------------------------

Vector Time (GMT): 2018/149/06:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4198952
75                 A    =         6777728
99  meter
 Y    =         659977
49  meter          E    =           
0017156
 Z    =       -5293922
74                 I    =           51
97028
 XDOT =      -2218
204893                 Wp   =           92
97992
 YDOT =       7277
399963  meter/sec      RA   =          111
99660  deg
 ZDOT =       -855
403032                 TA   =          168
88434
                                          MA   =          168
84639
                                          Ha   =            222
229  n
mi
                                          Hp   =            213
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13776091
71                 X    =         4216976
10
 Y    =        2165280
47  feet           Y    =          707034
47  meter
 Z    =      -17368512
93                 Z    =        -5273481
52
 XDOT =      -7277
575107                 XDOT =       -2295
262750
 YDOT =      23875
984132  feet/sec       YDOT =        7252
163714  meter/sec
 ZDOT =      -2806
440394                 ZDOT =        -866
364762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12942416
17                 X    =         3944848
45
 Y    =        5488943
25  feet           Y    =         1673029
90  meter
 Z    =      -17277145
29                 Z    =        -5266073
88
 XDOT =     -12466
721155                 XDOT =       -3799
856608
 YDOT =      20438
068356  feet/sec       YDOT =        6229
523235  meter/sec
 ZDOT =      -2856
458718                 ZDOT =        -870
648617


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
29537441  
00016717  00000-0  10270-3 0  9050
2 25544  51
6397 112
8933 0003739 132
6415 227
5053 15
54087375 35573


Satellite: ISS
Catalog Number: 25544
Epoch time:      18149
29537441   =   yrday
fracday
Element set:     905
Inclination:       51
6397  deg
RA of node:       112
8933  deg
Eccentricity:     
0003739     
Arg of perigee:   132
6415  deg
Mean anomaly:     227
5053  deg
Mean motion:   15
54087375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3557
Checksum:              327


Coasting Arc #7 (Orbit 3572)
---------------------------------------

Vector Time (GMT): 2018/150/06:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3571363
55                 A    =         6777714
55  meter
 Y    =       -2357638
41  meter          E    =           
0005802
 Z    =        5250828
01                 I    =           51
98198
 XDOT =       3016
382638                 Wp   =           95
72318
 YDOT =      -6972
554317  meter/sec      RA   =          107
02071  deg
 ZDOT =      -1078
642781                 TA   =            4
55792
                                          MA   =            4
55264
                                          Ha   =            222
269  n
mi
                                          Hp   =            213
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11717072
01                 X    =        -3570240
43
 Y    =       -7735034
16  feet           Y    =        -2397570
28  meter
 Z    =       17227126
02                 Z    =         5233481
75
 XDOT =       9896
268498                 XDOT =        3099
367008
 YDOT =     -22875
834374  feet/sec       YDOT =       -6938
358911  meter/sec
 ZDOT =      -3538
854268                 ZDOT =       -1063
789430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9762586
93                 X    =        -2975636
50
 Y    =      -10221035
67  feet           Y    =        -3115371
67  meter
 Z    =       17149831
69                 Z    =         5227268
70
 XDOT =      14115
609421                 XDOT =        4302
437751
 YDOT =     -19309
714300  feet/sec       YDOT =       -5885
600919  meter/sec
 ZDOT =      -3471
441256                 ZDOT =       -1058
095295


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   18150
32421985  
00016717  00000-0  10270-3 0  9062
2 25544  51
6396 107
7653 0003697 134
4885 225
6571 15
54128113 35736


Satellite: ISS
Catalog Number: 25544
Epoch time:      18150
32421985   =   yrday
fracday
Element set:     906
Inclination:       51
6396  deg
RA of node:       107
7653  deg
Eccentricity:     
0003697     
Arg of perigee:   134
4885  deg
Mean anomaly:     225
6571  deg
Mean motion:   15
54128113  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3573
Checksum:              322


Coasting Arc #8 (Orbit 3587)
---------------------------------------

Vector Time (GMT): 2018/151/06:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2903761
10                 A    =         6780177
85  meter
 Y    =        3956572
70  meter          E    =           
0013939
 Z    =       -4691767
44                 I    =           51
99946
 XDOT =      -3617
488521                 Wp   =          116
66828
 YDOT =       6093
306158  meter/sec      RA   =          102
04838  deg
 ZDOT =       2900
163481                 TA   =          182
05824
                                          MA   =          182
06398
                                          Ha   =            222
130  n
mi
                                          Hp   =            213
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9526775
26                 X    =         2882092
15
 Y    =       12980881
56  feet           Y    =         3988924
07  meter
 Z    =      -15392937
79                 Z    =        -4677713
90
 XDOT =     -11868
400658                 XDOT =       -3699
444276
 YDOT =      19991
161936  feet/sec       YDOT =        6052
394255  meter/sec
 ZDOT =       9514
972052                 ZDOT =        2882
392615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6679250
24                 X    =         2035835
47
 Y    =       14716168
79  feet           Y    =         4485488
25  meter
 Z    =      -15330598
78                 Z    =        -4672766
51
 XDOT =     -14800
395233                 XDOT =       -4511
160467
 YDOT =      16544
088450  feet/sec       YDOT =        5042
638160  meter/sec
 ZDOT =       9434
602663                 ZDOT =        2875
666892


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   18151
28876287  
00016717  00000-0  10270-3 0  9078
2 25544  51
6404 102
9573 0003671 137
1553 222
9887 15
54100813 35881


Satellite: ISS
Catalog Number: 25544
Epoch time:      18151
28876287   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       102
9573  deg
Eccentricity:     
0003671     
Arg of perigee:   137
1553  deg
Mean anomaly:     222
9887  deg
Mean motion:   15
54100813  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3588
Checksum:              323


Coasting Arc #9 (Orbit 3603)
---------------------------------------

Vector Time (GMT): 2018/152/06:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2191323
72                 A    =         6783775
80  meter
 Y    =       -5291716
58  meter          E    =           
0014470
 Z    =        3621046
08                 I    =           52
01713
 XDOT =       4084
616956                 Wp   =           98
28325
 YDOT =      -4740
321058  meter/sec      RA   =           97
08555  deg
 ZDOT =      -4442
469345                 TA   =           39
03064
                                          MA   =           38
92631
                                          Ha   =            222
116  n
mi
                                          Hp   =            213
726

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7189382
27                 X    =        -2149576
67
 Y    =      -17361274
87  feet           Y    =        -5315988
57  meter
 Z    =       11880072
42                 Z    =         3610501
95
 XDOT =      13400
974264                 XDOT =        4158
900252
 YDOT =     -15552
234443  feet/sec       YDOT =       -4694
228076  meter/sec
 ZDOT =     -14575
030660                 ZDOT =       -4422
447824

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3766846
10                 X    =        -1148134
69
 Y    =      -18439448
34  feet           Y    =        -5620343
85  meter
 Z    =       11833630
83                 Z    =         3606890
68
 XDOT =      14910
047901                 XDOT =        4544
582600
 YDOT =     -12369
167447  feet/sec       YDOT =       -3770
122238  meter/sec
 ZDOT =     -14484
759608                 ZDOT =       -4414
954729


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   18152
31760486  
00016717  00000-0  10270-3 0  9087
2 25544  51
6398  97
8291 0003682 139
9900 220
1524 15
54138885 36047


Satellite: ISS
Catalog Number: 25544
Epoch time:      18152
31760486   =   yrday
fracday
Element set:     908
Inclination:       51
6398  deg
RA of node:        97
8291  deg
Eccentricity:     
0003682     
Arg of perigee:   139
9900  deg
Mean anomaly:     220
1524  deg
Mean motion:   15
54138885  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3604
Checksum:              328


Coasting Arc #10 (Orbit 3618)
---------------------------------------

Vector Time (GMT): 2018/153/06:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1491148
59                 A    =         6787183
12  meter
 Y    =        6243533
54  meter          E    =           
0006600
 Z    =       -2207339
06                 I    =           52
03348
 XDOT =      -4410
020882                 Wp   =           76
79553
 YDOT =       2993
973477  meter/sec      RA   =           92
13291  deg
 ZDOT =       5504
664078                 TA   =          258
84429
                                          MA   =          258
91850
                                          Ha   =            222
004  n
mi
                                          Hp   =            213
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4892219
78                 X    =         1431942
99
 Y    =       20484033
91  feet           Y    =         6259877
86  meter
 Z    =       -7241926
06                 Z    =        -2200238
48
 XDOT =     -14468
572447                 XDOT =       -4469
911392
 YDOT =       9822
747627  feet/sec       YDOT =        2944
321949  meter/sec
 ZDOT =      18059
921517                 ZDOT =        5483
096605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1240080
31                 X    =          377976
48
 Y    =       21034211
65  feet           Y    =         6411227
71  meter
 Z    =       -7211039
74                 Z    =        -2197924
91
 XDOT =     -14561
295235                 XDOT =       -4438
282787
 YDOT =       6999
372063  feet/sec       YDOT =        2133
408605  meter/sec
 ZDOT =      17962
965089                 ZDOT =        5475
111759


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   18153
28214207  
00016717  00000-0  10270-3 0  9090
2 25544  51
6415  93
0214 0003763 143
1432 216
9980 15
54160438 36191


Satellite: ISS
Catalog Number: 25544
Epoch time:      18153
28214207   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:        93
0214  deg
Eccentricity:     
0003763     
Arg of perigee:   143
1432  deg
Mean anomaly:     216
9980  deg
Mean motion:   15
54160438  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3619
Checksum:              295


Coasting Arc #11 (Orbit 3622)
---------------------------------------

Vector Time (GMT): 2018/153/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3571086
74                 A    =         6780866
02  meter
 Y    =       -3624381
51  meter          E    =           
0010862
 Z    =       -4491994
72                 I    =           52
01109
 XDOT =       2450
990330                 Wp   =           86
93626
 YDOT =       6473
200973  meter/sec      RA   =           90
98690  deg
 ZDOT =      -3280
672156                 TA   =          150
17692
                                          MA   =          150
11497
                                          Ha   =            221
966  n
mi
                                          Hp   =            213
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11716163
83                 X    =         3633169
95
 Y    =      -11891015
45  feet           Y    =        -3584099
41  meter
 Z    =      -14737515
48                 Z    =        -4474497
28
 XDOT =       8041
306856                 XDOT =        2394
358879
 YDOT =      21237
536001  feet/sec       YDOT =        6500
293441  meter/sec
 ZDOT =     -10763
360092                 ZDOT =       -3268
902716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8756199
00                 X    =        -2668889
46
 Y    =      -14293744
23  feet           Y    =        -4356733
24  meter
 Z    =      -14658682
11                 Z    =        -4467966
31
 XDOT =      21511
428736                 XDOT =        6556
683479
 YDOT =      -2213
752604  feet/sec       YDOT =        -674
751794  meter/sec
 ZDOT =     -10711
612541                 ZDOT =       -3264
899502


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   18153
53935274  
00016717  00000-0  10270-3 0  9104
2 25544  51
6402  91
7390 0003404 142
6629 217
4760 15
54132804 36234


Satellite: ISS
Catalog Number: 25544
Epoch time:      18153
53935274   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:        91
7390  deg
Eccentricity:     
0003404     
Arg of perigee:   142
6629  deg
Mean anomaly:     217
4760  deg
Mean motion:   15
54132804  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3623
Checksum:              292


Coasting Arc #12 (Orbit 3636)
---------------------------------------

Vector Time (GMT): 2018/154/09:16:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3516053
61                 A    =         6779833
74  meter
 Y    =        3329381
96  meter          E    =           
0010876
 Z    =        4740803
10                 I    =           52
00527
 XDOT =      -2561
471388                 Wp   =          126
83792
 YDOT =      -6676
034263  meter/sec      RA   =           86
67533  deg
 ZDOT =       2777
989031                 TA   =          295
75000
                                          MA   =          295
86221
                                          Ha   =            221
935  n
mi
                                          Hp   =            213
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11535608
95                 X    =        -3576050
69
 Y    =       10923169
18  feet           Y    =         3289726
95  meter
 Z    =       15553815
95                 Z    =         4723578
02
 XDOT =      -8403
777520                 XDOT =       -2500
121788
 YDOT =     -21902
999551  feet/sec       YDOT =       -6704
335735  meter/sec
 ZDOT =       9114
137242                 ZDOT =        2765
694418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4608204
47                 X    =        -1404580
72
 Y    =       15282594
42  feet           Y    =         4658134
78  meter
 Z    =       15476234
97                 Z    =         4717156
42
 XDOT =     -17175
033100                 XDOT =       -5234
950089
 YDOT =     -14389
558921  feet/sec       YDOT =       -4385
937559  meter/sec
 ZDOT =       9060
075899                 ZDOT =        2761
511134


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   18154
43958393  
00016717  00000-0  10270-3 0  9112
2 25544  51
6380  87
2521 0003423 149
8953 210
2397 15
54144983 36378


Satellite: ISS
Catalog Number: 25544
Epoch time:      18154
43958393   =   yrday
fracday
Element set:     911
Inclination:       51
6380  deg
RA of node:        87
2521  deg
Eccentricity:     
0003423     
Arg of perigee:   149
8953  deg
Mean anomaly:     210
2397  deg
Mean motion:   15
54144983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3637
Checksum:              324


Coasting Arc #13 (Orbit 3651)
---------------------------------------

Vector Time (GMT): 2018/155/09:16:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3938865
30                 A    =         6777664
13  meter
 Y    =       -1617686
15  meter          E    =           
0016021
 Z    =       -5286639
39                 I    =           51
99517
 XDOT =       1803
253372                 Wp   =           94
46465
 YDOT =       7384
458520  meter/sec      RA   =           81
70216  deg
 ZDOT =       -919
681693                 TA   =          166
78834
                                          MA   =          166
74633
                                          Ha   =            221
871  n
mi
                                          Hp   =            214
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12922786
40                 X    =         3982341
66
 Y    =       -5307369
26  feet           Y    =        -1573395
33  meter
 Z    =      -17344617
41                 Z    =        -5267400
34
 XDOT =       5916
185604                 XDOT =        1725
011641
 YDOT =      24227
226115  feet/sec       YDOT =        7404
186373  meter/sec
 ZDOT =      -3017
328389                 ZDOT =        -911
111277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8437394
50                 X    =         2571717
85
 Y    =      -11267875
71  feet           Y    =        -3434448
51  meter
 Z    =      -17258264
14                 Z    =        -5260318
91
 XDOT =      16749
915093                 XDOT =        5105
374120
 YDOT =      17088
487426  feet/sec       YDOT =        5208
570967  meter/sec
 ZDOT =      -2980
049706                 ZDOT =        -908
319150


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   18155
40411752  
00016717  00000-0  10270-3 0  9124
2 25544  51
6384  82
4432 0003437 151
7291 208
4049 15
54116995 36524


Satellite: ISS
Catalog Number: 25544
Epoch time:      18155
40411752   =   yrday
fracday
Element set:     912
Inclination:       51
6384  deg
RA of node:        82
4432  deg
Eccentricity:     
0003437     
Arg of perigee:   151
7291  deg
Mean anomaly:     208
4049  deg
Mean motion:   15
54116995  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3652
Checksum:              302


Coasting Arc #14 (Orbit 3667)
---------------------------------------

Vector Time (GMT): 2018/156/09:16:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4264855
67                 A    =         6777703
35  meter
 Y    =        -171024
56  meter          E    =           
0004623
 Z    =        5260858
00                 I    =           51
99034
 XDOT =       -958
393294                 Wp   =          103
09104
 YDOT =      -7543
274460  meter/sec      RA   =           76
72687  deg
 ZDOT =      -1022
437777                 TA   =          356
64495
                                          MA   =          356
64804
                                          Ha   =            221
929  n
mi
                                          Hp   =            214
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13992308
64                 X    =        -4288180
73
 Y    =        -561104
22  feet           Y    =         -218848
09  meter
 Z    =       17260032
81                 Z    =         5240084
14
 XDOT =      -3144
334954                 XDOT =        -869
004641
 YDOT =     -24748
275787  feet/sec       YDOT =       -7553
491964  meter/sec
 ZDOT =      -3354
454649                 ZDOT =       -1026
877002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12258946
47                 X    =        -3736526
88
 Y    =        7001300
41  feet           Y    =         2133996
37  meter
 Z    =       17167070
09                 Z    =         5232522
96
 XDOT =     -15253
094759                 XDOT =       -4649
143283
 YDOT =     -18438
563772  feet/sec       YDOT =       -5620
074238  meter/sec
 ZDOT =      -3373
206838                 ZDOT =       -1028
153444


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   18156
43294876  
00016717  00000-0  10270-3 0  9135
2 25544  51
6391  77
3148 0003337 155
1462 204
9852 15
54125104 36688


Satellite: ISS
Catalog Number: 25544
Epoch time:      18156
43294876   =   yrday
fracday
Element set:     913
Inclination:       51
6391  deg
RA of node:        77
3148  deg
Eccentricity:     
0003337     
Arg of perigee:   155
1462  deg
Mean anomaly:     204
9852  deg
Mean motion:   15
54125104  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3668
Checksum:              317


Coasting Arc #15 (Orbit 3673)
---------------------------------------

Vector Time (GMT): 2018/156/19:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4062055
20                 A    =         6783776
37  meter
 Y    =        4043105
07  meter          E    =           
0007975
 Z    =       -3639142
27                 I    =           52
00660
 XDOT =      -1949
666365                 Wp   =          121
54594
 YDOT =       5939
619336  meter/sec      RA   =           74
59996  deg
 ZDOT =       4425
771350                 TA   =          195
59648
                                          MA   =          195
62107
                                          Ha   =            221
837  n
mi
                                          Hp   =            214
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13326952
75                 X    =         4034219
23
 Y    =       13264780
42  feet           Y    =         4088374
49  meter
 Z    =      -11939443
13                 Z    =        -3619477
41
 XDOT =      -6396
543192                 XDOT =       -2037
437981
 YDOT =      19486
940079  feet/sec       YDOT =        5917
325622  meter/sec
 ZDOT =      14520
247210                 ZDOT =        4416
087951

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14573000
13                 X    =        -4441850
44
 Y    =      -11969529
40  feet           Y    =        -3648312
56  meter
 Z    =      -11852021
11                 Z    =        -3612496
03
 XDOT =       3792
773848                 XDOT =        1156
037469
 YDOT =     -18941
600280  feet/sec       YDOT =       -5773
399765  meter/sec
 ZDOT =      14476
017176                 ZDOT =        4412
290035


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   18156
81875946  
00016717  00000-0  10270-3 0  9141
2 25544  51
6383  75
3877 0003737 157
1691 202
9628 15
54137579 36741


Satellite: ISS
Catalog Number: 25544
Epoch time:      18156
81875946   =   yrday
fracday
Element set:     914
Inclination:       51
6383  deg
RA of node:        75
3877  deg
Eccentricity:     
0003737     
Arg of perigee:   157
1691  deg
Mean anomaly:     202
9628  deg
Mean motion:   15
54137579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3674
Checksum:              356


Coasting Arc #16 (Orbit 3684)
---------------------------------------

Vector Time (GMT): 2018/157/11:12:41
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -95700
63                 A    =         6786314
40  meter
 Y    =        6235930
94  meter          E    =           
0014455
 Z    =        2663220
37                 I    =           52
01057
 XDOT =      -5097
934506                 Wp   =           90
56363
 YDOT =      -2325
238804  meter/sec      RA   =           71
39772  deg
 ZDOT =       5236
762896                 TA   =          299
32364
                                          MA   =          299
46798
                                          Ha   =            221
701  n
mi
                                          Hp   =            214
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -313978
43                 X    =         -178361
94
 Y    =       20459091
02  feet           Y    =         6234398
32  meter
 Z    =        8737599
64                 Z    =         2662555
29
 XDOT =     -16725
506908                 XDOT =       -5096
991627
 YDOT =      -7628
736232  feet/sec       YDOT =       -2382
242630  meter/sec
 ZDOT =      17180
980631                 ZDOT =        5212
000935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17910211
78                 X    =         5459032
55
 Y    =        9897760
34  feet           Y    =         3016837
35  meter
 Z    =        8733687
06                 Z    =         2662027
82
 XDOT =     -13895
566224                 XDOT =       -4235
368585
 YDOT =      10010
263954  feet/sec       YDOT =        3051
128453  meter/sec
 ZDOT =      17070
489130                 ZDOT =        5203
085087


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   18157
52607886  
00016717  00000-0  10270-3 0  9157
2 25544  51
6398  71
8661 0003276 158
7211 201
4078 15
54133273 36854


Satellite: ISS
Catalog Number: 25544
Epoch time:      18157
52607886   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:        71
8661  deg
Eccentricity:     
0003276     
Arg of perigee:   158
7211  deg
Mean anomaly:     201
4078  deg
Mean motion:   15
54133273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3685
Checksum:              325


Coasting Arc #17 (Orbit 3699)
---------------------------------------

Vector Time (GMT): 2018/158/11:12:41
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1085603
18                 A    =         6782441
85  meter
 Y    =       -5361852
48  meter          E    =           
0007655
 Z    =       -4015018
84                 I    =           51
98752
 XDOT =       5156
824060                 Wp   =           96
95220
 YDOT =       4025
536997  meter/sec      RA   =           66
44008  deg
 ZDOT =      -3988
971276                 TA   =          131
72222
                                          MA   =          131
65672
                                          Ha   =            221
600  n
mi
                                          Hp   =            214
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3561690
23                 X    =         1164983
12
 Y    =      -17591379
53  feet           Y    =        -5349268
34  meter
 Z    =      -13172633
99                 Z    =        -4009552
99
 XDOT =      16918
714109                 XDOT =        5130
802531
 YDOT =      13207
142378  feet/sec       YDOT =        4083
059001  meter/sec
 ZDOT =     -13087
176104                 ZDOT =       -3963
983972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14038091
24                 X    =        -4278810
21
 Y    =      -11213368
09  feet           Y    =        -3417834
59  meter
 Z    =      -13147354
41                 Z    =        -4007313
62
 XDOT =      18653
077916                 XDOT =        5685
458149
 YDOT =      -8166
528051  feet/sec       YDOT =       -2489
157750  meter/sec
 ZDOT =     -12975
939105                 ZDOT =       -3955
066239


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   18158
49060235  
00016717  00000-0  10270-3 0  9166
2 25544  51
6409  67
0579 0003214 162
5922 197
5342 15
54157005 37002


Satellite: ISS
Catalog Number: 25544
Epoch time:      18158
49060235   =   yrday
fracday
Element set:     916
Inclination:       51
6409  deg
RA of node:        67
0579  deg
Eccentricity:     
0003214     
Arg of perigee:   162
5922  deg
Mean anomaly:     197
5342  deg
Mean motion:   15
54157005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              302


Coasting Arc #18 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2018/159/11:12:41
000
Vector Time (MET): N/A
Weight (LBS)     : 907753
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2120527
54                 A    =         6779008
83  meter
 Y    =        4153500
49  meter          E    =           
0009243
 Z    =        4916932
32                 I    =           51
96228
 XDOT =      -4988
297105                 Wp   =          136
08554
 YDOT =      -5334
193217  meter/sec      RA   =           61
47155  deg
 ZDOT =       2345
551747                 TA   =          291
01968
                                          MA   =          291
11852
                                          Ha   =            221
552  n
mi
                                          Hp   =            214
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6957111
34                 X    =        -2190699
54
 Y    =       13626970
12  feet           Y    =         4129394
52  meter
 Z    =       16131667
72                 Z    =         4906461
38
 XDOT =     -16365
804150                 XDOT =       -4939
671487
 YDOT =     -17500
633914  feet/sec       YDOT =       -5389
704109  meter/sec
 ZDOT =       7695
379749                 ZDOT =        2321
437809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9170913
99                 X    =         2795294
58
 Y    =       12309366
82  feet           Y    =         3751895
01  meter
 Z    =       16084161
19                 Z    =         4902452
33
 XDOT =     -22017
133912                 XDOT =       -6710
822416
 YDOT =       6449
057286  feet/sec       YDOT =        1965
672661  meter/sec
 ZDOT =       7588
262983                 ZDOT =        2312
902557


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   18159
51942260  
00016717  00000-0  10270-3 0  9178
2 25544  51
6412  61
9293 0003264 168
2532 191
8698 15
54168441 37161


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
51942260   =   yrday
fracday
Element set:     917
Inclination:       51
6412  deg
RA of node:        61
9293  deg
Eccentricity:     
0003264     
Arg of perigee:   168
2532  deg
Mean anomaly:     191
8698  deg
Mean motion:   15
54168441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              323


Coasting Arc #19 (Orbit 3716)
---------------------------------------

Vector Time (GMT): 2018/159/13:07:21
000
Vector Time (MET): N/A
Weight (LBS)     : 922985
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4579677
96                 A    =         6786900
74  meter
 Y    =       -4374013
96  meter          E    =           
0015642
 Z    =        2416789
54                 I    =           51
98814
 XDOT =       2000
660482                 Wp   =          116
49891
 YDOT =      -5083
195381  meter/sec      RA   =           61
03882  deg
 ZDOT =      -5388
614206                 TA   =           36
59468
                                          MA   =           36
48793
                                          Ha   =            221
634  n
mi
                                          Hp   =            214
329

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15025190
17                 X    =        -4542165
74
 Y    =      -14350439
49  feet           Y    =        -4425017
53  meter
 Z    =        7929099
54                 Z    =         2394633
63
 XDOT =       6563
846725                 XDOT =        2083
528706
 YDOT =     -16677
150200  feet/sec       YDOT =       -5060
358812  meter/sec
 ZDOT =     -17679
180465                 ZDOT =       -5378
694779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13587612
95                 X    =        -4141504
43
 Y    =       15767705
66  feet           Y    =         4805996
69  meter
 Z    =        7830600
55                 Z    =         2386767
05
 XDOT =     -15838
377827                 XDOT =       -4827
537562
 YDOT =      -4858
001495  feet/sec       YDOT =       -1480
718856  meter/sec
 ZDOT =     -17633
998977                 ZDOT =       -5374
842888


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   18159
58372480  
00016717  00000-0  10270-3 0  9187
2 25544  51
6424  61
6098 0003257 166
9867 193
1371 15
54133682 37175


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
58372480   =   yrday
fracday
Element set:     918
Inclination:       51
6424  deg
RA of node:        61
6098  deg
Eccentricity:     
0003257     
Arg of perigee:   166
9867  deg
Mean anomaly:     193
1371  deg
Mean motion:   15
54133682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3717
Checksum:              336
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