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

 
Date: April 5th 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 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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


101/03:32:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 214 7

105/08:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 214 6

108/10:36:13 344 0 3 1 0 1 0
N/A -0 8 -0 0 220 9
000/00:02:26 689 -0 4 -0 0 214 9

Coasting Arc #1 (Orbit 2704)
---------------------------------------

Vector Time (GMT): 2018/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4337579
67                 A    =         6779596
74  meter
 Y    =       -2100239
68  meter          E    =           
0009288
 Z    =       -4777111
90                 I    =           51
79486
 XDOT =       5292
458849                 Wp   =          104
11749
 YDOT =       4849
629482  meter/sec      RA   =           25
44084  deg
 ZDOT =       2675
536987                 TA   =          192
25951
                                          MA   =          192
28213
                                          Ha   =            220
445  n
mi
                                          Hp   =            215
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14230904
41                 X    =         4383947
66
 Y    =       -6890550
13  feet           Y    =        -2051474
97  meter
 Z    =      -15672939
29                 Z    =        -4755928
46
 XDOT =      17363
710136                 XDOT =        5224
839150
 YDOT =      15910
857879  feet/sec       YDOT =        4908
435508  meter/sec
 ZDOT =       8778
008488                 ZDOT =        2701
081574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12607878
49                 X    =         3842881
36
 Y    =       -9695585
61  feet           Y    =        -2955214
50  meter
 Z    =      -15578073
28                 Z    =        -4748196
74
 XDOT =      19503
826664                 XDOT =        5944
766367
 YDOT =      11087
897175  feet/sec       YDOT =        3379
591059  meter/sec
 ZDOT =       8891
258675                 ZDOT =        2710
055644


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   18094
51129658  
00016717  00000-0  10270-3 0  9006
2 25544  51
6409  26
0109 0001935 310
0788  50
0194 15
54192740 27051


Satellite: ISS
Catalog Number: 25544
Epoch time:      18094
51129658   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:        26
0109  deg
Eccentricity:     
0001935     
Arg of perigee:   310
0788  deg
Mean anomaly:      50
0194  deg
Mean motion:   15
54192740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2705
Checksum:              291


Coasting Arc #2 (Orbit 2720)
---------------------------------------

Vector Time (GMT): 2018/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5545691
41                 A    =         6783292
55  meter
 Y    =        1080648
39  meter          E    =           
0010458
 Z    =        3747179
37                 I    =           51
77726
 XDOT =      -3882
224288                 Wp   =           75
99811
 YDOT =      -5044
830101  meter/sec      RA   =           20
46185  deg
 ZDOT =      -4278
204997                 TA   =           59
29021
                                          MA   =           59
18722
                                          Ha   =            220
518  n
mi
                                          Hp   =            215
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18194525
63                 X    =        -5575565
32
 Y    =        3545434
37  feet           Y    =         1018465
84  meter
 Z    =       12293895
59                 Z    =         3720167
49
 XDOT =     -12736
956325                 XDOT =       -3804
741654
 YDOT =     -16551
279859  feet/sec       YDOT =       -5087
810820  meter/sec
 ZDOT =     -14036
105633                 ZDOT =       -4296
875163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17026521
73                 X    =        -5189683
82
 Y    =        7527414
49  feet           Y    =         2294355
94  meter
 Z    =       12173180
59                 Z    =         3710385
44
 XDOT =     -15463
890935                 XDOT =       -4713
393957
 YDOT =     -12079
127903  feet/sec       YDOT =       -3681
718185  meter/sec
 ZDOT =     -14118
634531                 ZDOT =       -4303
359805


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   18095
54008712  
00016717  00000-0  10270-3 0  9018
2 25544  51
6411  20
8829 0002004 311
8741  48
2241 15
54196375 27219


Satellite: ISS
Catalog Number: 25544
Epoch time:      18095
54008712   =   yrday
fracday
Element set:     901
Inclination:       51
6411  deg
RA of node:        20
8829  deg
Eccentricity:     
0002004     
Arg of perigee:   311
8741  deg
Mean anomaly:      48
2241  deg
Mean motion:   15
54196375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2721
Checksum:              281


Coasting Arc #3 (Orbit 2735)
---------------------------------------

Vector Time (GMT): 2018/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6366172
05                 A    =         6786876
83  meter
 Y    =        -149256
68  meter          E    =           
0006235
 Z    =       -2339876
31                 I    =           51
75852
 XDOT =       2102
289700                 Wp   =           24
83295
 YDOT =       5007
794890  meter/sec      RA   =           15
48996  deg
 ZDOT =       5411
072326                 TA   =          309
11835
                                          MA   =          309
17376
                                          Ha   =            220
513  n
mi
                                          Hp   =            215
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20886391
23                 X    =         6378733
88
 Y    =        -489687
27  feet           Y    =          -77995
64  meter
 Z    =       -7676759
55                 Z    =        -2308920
95
 XDOT =       6897
275919                 XDOT =        2019
850631
 YDOT =      16429
773260  feet/sec       YDOT =        5030
843467  meter/sec
 ZDOT =      17752
861962                 ZDOT =        5421
084098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20210190
31                 X    =         6160066
01
 Y    =       -5489217
89  feet           Y    =        -1673113
61  meter
 Z    =       -7538598
27                 Z    =        -2297764
75
 XDOT =      10116
741336                 XDOT =        3083
582759
 YDOT =      12856
006428  feet/sec       YDOT =        3918
510759  meter/sec
 ZDOT =      17796
749798                 ZDOT =        5424
449339


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   18096
50457439  
00016717  00000-0  10270-3 0  9020
2 25544  51
6415  16
0743 0002049 315
3867  44
7121 15
54200679 27369


Satellite: ISS
Catalog Number: 25544
Epoch time:      18096
50457439   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:        16
0743  deg
Eccentricity:     
0002049     
Arg of perigee:   315
3867  deg
Mean anomaly:      44
7121  deg
Mean motion:   15
54200679  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2736
Checksum:              303


Coasting Arc #4 (Orbit 2751)
---------------------------------------

Vector Time (GMT): 2018/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6713455
93                 A    =         6788983
07  meter
 Y    =        -723292
28  meter          E    =           
0011167
 Z    =         653113
22                 I    =           51
73416
 XDOT =        -69
752488                 Wp   =          125
84660
 YDOT =      -4806
327013  meter/sec      RA   =           10
52482  deg
 ZDOT =      -5974
663928                 TA   =           47
11002
                                          MA   =           47
01632
                                          Ha   =            220
533  n
mi
                                          Hp   =            215
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22025774
06                 X    =        -6708041
42
 Y    =       -2373006
16  feet           Y    =         -798336
45  meter
 Z    =        2142759
91                 Z    =          620514
64
 XDOT =       -228
846747                 XDOT =          13
020232
 YDOT =     -15768
789412  feet/sec       YDOT =       -4806
644512  meter/sec
 ZDOT =     -19601
915775                 ZDOT =       -5974
801489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21912083
53                 X    =        -6678803
06
 Y    =        3350857
68  feet           Y    =         1021341
42  meter
 Z    =        1997410
62                 Z    =          608810
76
 XDOT =      -3890
669715                 XDOT =       -1185
876129
 YDOT =     -13621
031041  feet/sec       YDOT =       -4151
690261  meter/sec
 ZDOT =     -19601
768917                 ZDOT =       -5974
619166


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   18097
53335701  
00016717  00000-0  10270-3 0  9032
2 25544  51
6421  10
9453 0001992 320
7607  39
3402 15
54193612 27523


Satellite: ISS
Catalog Number: 25544
Epoch time:      18097
53335701   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:        10
9453  deg
Eccentricity:     
0001992     
Arg of perigee:   320
7607  deg
Mean anomaly:      39
3402  deg
Mean motion:   15
54193612  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2752
Checksum:              289


Coasting Arc #5 (Orbit 2767)
---------------------------------------

Vector Time (GMT): 2018/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6528095
50                 A    =         6788600
22  meter
 Y    =        1487694
36  meter          E    =           
0013758
 Z    =        1074036
19                 I    =           51
70018
 XDOT =      -1998
099123                 Wp   =           47
88724
 YDOT =       4483
291483  meter/sec      RA   =            5
55986  deg
 ZDOT =       5895
285840                 TA   =          323
75644
                                          MA   =          323
84957
                                          Ha   =            220
566  n
mi
                                          Hp   =            214
945

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21417636
16                 X    =         6505757
41
 Y    =        4880887
00  feet           Y    =         1560571
17  meter
 Z    =        3523740
77                 Z    =         1105693
14
 XDOT =      -6555
443317                 XDOT =       -2076
720251
 YDOT =      14708
961558  feet/sec       YDOT =        4460
508067  meter/sec
 ZDOT =      19341
488978                 ZDOT =        5885
388564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21914138
80                 X    =         6679429
51
 Y    =       -1137981
14  feet           Y    =         -346856
65  meter
 Z    =        3664759
91                 Z    =         1117018
82
 XDOT =      -2501
179028                 XDOT =        -762
359368
 YDOT =      14377
399027  feet/sec       YDOT =        4382
231223  meter/sec
 ZDOT =      19296
616315                 ZDOT =        5881
608653


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   18098
56213700  
00016717  00000-0  10270-3 0  9041
2 25544  51
6418   5
8165 0002109 325
8101  34
2915 15
54198757 27683


Satellite: ISS
Catalog Number: 25544
Epoch time:      18098
56213700   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:         5
8165  deg
Eccentricity:     
0002109     
Arg of perigee:   325
8101  deg
Mean anomaly:      34
2915  deg
Mean motion:   15
54198757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2768
Checksum:              308


Coasting Arc #6 (Orbit 2782)
---------------------------------------

Vector Time (GMT): 2018/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5815181
65                 A    =         6785893
65  meter
 Y    =       -2206809
81  meter          E    =           
0002898
 Z    =       -2714545
75                 I    =           51
65958
 XDOT =       3948
280832                 Wp   =          105
98831
 YDOT =      -4049
628507  meter/sec      RA   =             
58884  deg
 ZDOT =      -5171
321728                 TA   =          104
67429
                                          MA   =          104
64217
                                          Ha   =            220
517  n
mi
                                          Hp   =            214
945

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19078679
94                 X    =        -5776886
46
 Y    =       -7240189
67  feet           Y    =        -2271625
21  meter
 Z    =       -8905989
99                 Z    =        -2742700
75
 XDOT =      12953
677270                 XDOT =        4018
391003
 YDOT =     -13286
182766  feet/sec       YDOT =       -4005
084404  meter/sec
 ZDOT =     -16966
278636                 ZDOT =       -5151
971822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20300789
19                 X    =        -6187680
54
 Y    =       -1430833
62  feet           Y    =         -436118
09  meter
 Z    =       -9031262
69                 Z    =        -2752728
87
 XDOT =       8559
899504                 XDOT =        2609
057369
 YDOT =     -15017
981450  feet/sec       YDOT =       -4577
480746  meter/sec
 ZDOT =     -16879
302025                 ZDOT =       -5144
811257


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   18099
52661389  
00016717  00000-0  10270-3 0  9059
2 25544  51
6429   1
0086 0002144 323
1455  36
9550 15
54204628 27833


Satellite: ISS
Catalog Number: 25544
Epoch time:      18099
52661389   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:         1
0086  deg
Eccentricity:     
0002144     
Arg of perigee:   323
1455  deg
Mean anomaly:      36
9550  deg
Mean motion:   15
54204628  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2783
Checksum:              306


Coasting Arc #7 (Orbit 2798)
---------------------------------------

Vector Time (GMT): 2018/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4636320
39                 A    =         6782056
53  meter
 Y    =        2851805
63  meter          E    =           
0009421
 Z    =        4037809
59                 I    =           51
61414
 XDOT =      -5580
010790                 Wp   =           91
76533
 YDOT =       3531
360193  meter/sec      RA   =          355
60505  deg
 ZDOT =       3904
845963                 TA   =          317
70545
                                          MA   =          317
77806
                                          Ha   =            220
560  n
mi
                                          Hp   =            214
856

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15211024
92                 X    =         4584472
60
 Y    =        9356317
69  feet           Y    =         2903362
54  meter
 Z    =       13247406
81                 Z    =         4060205
10
 XDOT =     -18307
122015                 XDOT =       -5638
052385
 YDOT =      11585
827406  feet/sec       YDOT =        3468
636410  meter/sec
 ZDOT =      12811
174420                 ZDOT =        3877
598998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17259448
49                 X    =         5260679
90
 Y    =        4287437
54  feet           Y    =         1306810
96  meter
 Z    =       13346874
69                 Z    =         4068127
41
 XDOT =     -13657
338122                 XDOT =       -4162
756659
 YDOT =      15394
822723  feet/sec       YDOT =        4692
341966  meter/sec
 ZDOT =      12689
054095                 ZDOT =        3867
623688


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   18100
55538623  
00016717  00000-0  10270-3 0  9060
2 25544  51
6432 355
8791 0002179 333
4546  26
6495 15
54213452 27999


Satellite: ISS
Catalog Number: 25544
Epoch time:      18100
55538623   =   yrday
fracday
Element set:     906
Inclination:       51
6432  deg
RA of node:       355
8791  deg
Eccentricity:     
0002179     
Arg of perigee:   333
4546  deg
Mean anomaly:      26
6495  deg
Mean motion:   15
54213452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2799
Checksum:              323


Coasting Arc #8 (Orbit 2808)
---------------------------------------

Vector Time (GMT): 2018/101/03:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2255144
46                 A    =         6777778
42  meter
 Y    =        3805568
41  meter          E    =           
0003228
 Z    =        5132703
37                 I    =           51
57645
 XDOT =      -7189
757956                 Wp   =          105
50963
 YDOT =       2191
049176  meter/sec      RA   =          352
36122  deg
 ZDOT =       1532
777611                 TA   =          329
70439
                                          MA   =          329
72305
                                          Ha   =            220
641  n
mi
                                          Hp   =            214
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7398767
91                 X    =         2187489
98
 Y    =       12485460
65  feet           Y    =         3830409
10  meter
 Z    =       16839577
98                 Z    =         5143493
46
 XDOT =     -23588
444737                 XDOT =       -7221
169934
 YDOT =       7188
481548  feet/sec       YDOT =        2110
472836  meter/sec
 ZDOT =       5028
797935                 ZDOT =        1497
775801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14150743
34                 X    =        -4313146
57
 Y    =        2963380
11  feet           Y    =          903238
26  meter
 Z    =       16887117
04                 Z    =         5147193
27
 XDOT =        868
164232                 XDOT =         264
616458
 YDOT =     -23650
358314  feet/sec       YDOT =       -7208
629214  meter/sec
 ZDOT =       4872
298864                 ZDOT =        1485
076694


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   18101
19836579  
00016717  00000-0  10270-3 0  9073
2 25544  51
6409 352
6724 0001932 338
5131  21
5940 15
54230718 28091


Satellite: ISS
Catalog Number: 25544
Epoch time:      18101
19836579   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       352
6724  deg
Eccentricity:     
0001932     
Arg of perigee:   338
5131  deg
Mean anomaly:      21
5940  deg
Mean motion:   15
54230718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2809
Checksum:              308


Coasting Arc #9 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2018/102/03:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -444219
24                 A    =         6777188
04  meter
 Y    =       -4214854
10  meter          E    =           
0013947
 Z    =       -5300457
07                 I    =           51
54172
 XDOT =       7528
604901                 Wp   =           85
92515
 YDOT =      -1336
088144  meter/sec      RA   =          347
35608  deg
 ZDOT =        433
439845                 TA   =          188
20810
                                          MA   =          188
23094
                                          Ha   =            220
698  n
mi
                                          Hp   =            214
779

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1457412
20                 X    =         -371307
72
 Y    =      -13828261
49  feet           Y    =        -4219414
47  meter
 Z    =      -17389951
03                 Z    =        -5302437
47
 XDOT =      24700
147314                 XDOT =        7540
880437
 YDOT =      -4383
491285  feet/sec       YDOT =       -1251
829425  meter/sec
 ZDOT =       1422
046737                 ZDOT =         470
041177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13595498
58                 X    =         4143907
97
 Y    =        2867561
66  feet           Y    =          874032
79  meter
 Z    =      -17398125
52                 Z    =        -5302948
66
 XDOT =      -3015
280554                 XDOT =        -919
057513
 YDOT =      23876
730908  feet/sec       YDOT =        7277
627581  meter/sec
 ZDOT =       1585
533521                 ZDOT =         483
270617


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   18102
16283572  
00016717  00000-0  10270-3 0  9081
2 25544  51
6409 347
8650 0002008 336
4009  23
7051 15
54212771 28244


Satellite: ISS
Catalog Number: 25544
Epoch time:      18102
16283572   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       347
8650  deg
Eccentricity:     
0002008     
Arg of perigee:   336
4009  deg
Mean anomaly:      23
7051  deg
Mean motion:   15
54212771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2824
Checksum:              289


Coasting Arc #10 (Orbit 2839)
---------------------------------------

Vector Time (GMT): 2018/103/03:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1367122
53                 A    =         6778925
54  meter
 Y    =        4503363
61  meter          E    =           
0007665
 Z    =        4876478
52                 I    =           51
51525
 XDOT =      -7289
656630                 Wp   =           43
48327
 YDOT =        350
753156  meter/sec      RA   =          342
34886  deg
 ZDOT =      -2359
912829                 TA   =           69
70275
                                          MA   =           69
62039
                                          Ha   =            220
766  n
mi
                                          Hp   =            214
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4485310
15                 X    =        -1441066
23
 Y    =       14774814
99  feet           Y    =         4487662
54  meter
 Z    =       15998945
27                 Z    =         4869657
45
 XDOT =     -23916
196294                 XDOT =       -7281
573806
 YDOT =       1150
764947  feet/sec       YDOT =         269
280159  meter/sec
 ZDOT =      -7742
496159                 ZDOT =       -2395
303995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12868304
20                 X    =        -3922259
12
 Y    =       -8591562
93  feet           Y    =        -2618708
38  meter
 Z    =       15967817
90                 Z    =         4866990
90
 XDOT =       5036
119593                 XDOT =        1535
009252
 YDOT =     -22273
113425  feet/sec       YDOT =       -6788
844972  meter/sec
 ZDOT =      -7900
416484                 ZDOT =       -2408
046944


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   18103
19159983  
00016717  00000-0  10270-3 0  9094
2 25544  51
6403 342
7355 0002090 342
2036  17
9043 15
54247853 28403


Satellite: ISS
Catalog Number: 25544
Epoch time:      18103
19159983   =   yrday
fracday
Element set:     909
Inclination:       51
6403  deg
RA of node:       342
7355  deg
Eccentricity:     
0002090     
Arg of perigee:   342
2036  deg
Mean anomaly:      17
9043  deg
Mean motion:   15
54247853  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2840
Checksum:              301


Coasting Arc #11 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2018/104/03:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2984002
62                 A    =         6782537
69  meter
 Y    =       -4645411
71  meter          E    =           
0005909
 Z    =       -3944211
65                 I    =           51
49543
 XDOT =       6481
636509                 Wp   =           86
54696
 YDOT =        757
801432  meter/sec      RA   =          337
34863  deg
 ZDOT =       4016
731084                 TA   =          225
48263
                                          MA   =          225
53093
                                          Ha   =            220
892  n
mi
                                          Hp   =            214
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9790034
85                 X    =         3054886
16
 Y    =      -15240852
07  feet           Y    =        -4611646
60  meter
 Z    =      -12940326
94                 Z    =        -3929543
66
 XDOT =      21265
211644                 XDOT =        6453
169522
 YDOT =       2486
225170  feet/sec       YDOT =         830
124785  meter/sec
 ZDOT =      13178
251589                 ZDOT =        4048
147652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12052341
49                 X    =         3673553
69
 Y    =       13585905
88  feet           Y    =         4140984
11  meter
 Z    =      -12874185
08                 Z    =        -3924051
61
 XDOT =      -7059
932984                 XDOT =       -2151
867574
 YDOT =      18866
208745  feet/sec       YDOT =        5750
420425  meter/sec
 ZDOT =      13318
258439                 ZDOT =        4059
405172


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   18104
15606448  
00016717  00000-0  10270-3 0  9106
2 25544  51
6397 337
9279 0002195 349
0583  11
0521 15
54219667 28558


Satellite: ISS
Catalog Number: 25544
Epoch time:      18104
15606448   =   yrday
fracday
Element set:     910
Inclination:       51
6397  deg
RA of node:       337
9279  deg
Eccentricity:     
0002195     
Arg of perigee:   349
0583  deg
Mean anomaly:      11
0521  deg
Mean motion:   15
54219667  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              318


Coasting Arc #12 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2018/105/03:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4319785
05                 A    =         6786225
90  meter
 Y    =        4559912
66  meter          E    =           
0012874
 Z    =        2556301
06                 I    =           51
47674
 XDOT =      -5220
795034                 Wp   =           94
29521
 YDOT =      -1987
791799  meter/sec      RA   =          332
35561  deg
 ZDOT =      -5254
663425                 TA   =           56
90040
                                          MA   =           56
77688
                                          Ha   =            220
849  n
mi
                                          Hp   =            214
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14172523
13                 X    =        -4382871
49
 Y    =       14960343
36  feet           Y    =         4511253
35  meter
 Z    =        8386814
51                 Z    =         2535163
14
 XDOT =     -17128
592631                 XDOT =       -5172
654288
 YDOT =      -6521
626636  feet/sec       YDOT =       -2045
905641  meter/sec
 ZDOT =     -17239
709399                 ZDOT =       -5279
907428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10922751
27                 X    =        -3329254
59
 Y    =      -17519983
92  feet           Y    =        -5340091
10  meter
 Z    =        8291840
04                 Z    =         2527352
84
 XDOT =       9297
146582                 XDOT =        2833
770278
 YDOT =     -14043
030699  feet/sec       YDOT =       -4280
315757  meter/sec
 ZDOT =     -17351
986424                 ZDOT =       -5288
885462


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   18105
18482381  
00016717  00000-0  10270-3 0  9119
2 25544  51
6383 332
7982 0002344 349
5426  10
5678 15
54265064 28711


Satellite: ISS
Catalog Number: 25544
Epoch time:      18105
18482381   =   yrday
fracday
Element set:     911
Inclination:       51
6383  deg
RA of node:       332
7982  deg
Eccentricity:     
0002344     
Arg of perigee:   349
5426  deg
Mean anomaly:      10
5678  deg
Mean motion:   15
54265064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              314


Coasting Arc #13 (Orbit 2873)
---------------------------------------

Vector Time (GMT): 2018/105/08:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1801114
05                 A    =         6781111
37  meter
 Y    =       -4913262
34  meter          E    =           
0007561
 Z    =       -4319605
97                 I    =           51
45605
 XDOT =       6800
785900                 Wp   =           94
63174
 YDOT =       -565
399037  meter/sec      RA   =          331
25159  deg
 ZDOT =       3483
451682                 TA   =          210
88742
                                          MA   =          210
93192
                                          Ha   =            220
849  n
mi
                                          Hp   =            214
620

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5909166
84                 X    =         1876904
27
 Y    =      -16119627
11  feet           Y    =        -4892697
67  meter
 Z    =      -14171935
59                 Z    =        -4310672
14
 XDOT =      22312
289697                 XDOT =        6789
681903
 YDOT =      -1854
983717  feet/sec       YDOT =        -489
409737  meter/sec
 ZDOT =      11428
647252                 ZDOT =        3516
461049

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12233278
32                 X    =         3728703
23
 Y    =      -12093660
82  feet           Y    =        -3686147
82  meter
 Z    =      -14131336
06                 Z    =        -4307231
23
 XDOT =      20067
295926                 XDOT =        6116
511798
 YDOT =       6790
547467  feet/sec       YDOT =        2069
758868  meter/sec
 ZDOT =      11575
947389                 ZDOT =        3528
348764


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   18105
37771793  
00016717  00000-0  10270-3 0  9129
2 25544  51
6412 331
8373 0002323 349
6663  10
4442 15
54251657 28743


Satellite: ISS
Catalog Number: 25544
Epoch time:      18105
37771793   =   yrday
fracday
Element set:     912
Inclination:       51
6412  deg
RA of node:       331
8373  deg
Eccentricity:     
0002323     
Arg of perigee:   349
6663  deg
Mean anomaly:      10
4442  deg
Mean motion:   15
54251657  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2874
Checksum:              306


Coasting Arc #14 (Orbit 2889)
---------------------------------------

Vector Time (GMT): 2018/106/08:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3245113
69                 A    =         6785098
00  meter
 Y    =        5104984
19  meter          E    =           
0012736
 Z    =        3063574
73                 I    =           51
44075
 XDOT =      -5856
373786                 Wp   =           85
67650
 YDOT =       -776
356570  meter/sec      RA   =          326
25314  deg
 ZDOT =      -4891
200016                 TA   =           59
02817
                                          MA   =           58
90310
                                          Ha   =            220
942  n
mi
                                          Hp   =            214
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10646698
45                 X    =        -3316839
31
 Y    =       16748635
80  feet           Y    =         5068294
29  meter
 Z    =       10051098
19                 Z    =         3047636
23
 XDOT =     -19213
824758                 XDOT =       -5823
497826
 YDOT =      -2547
101607  feet/sec       YDOT =        -841
663124  meter/sec
 ZDOT =     -16047
244147                 ZDOT =       -4919
568812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16584005
17                 X    =        -5054804
78
 Y    =       10967184
73  feet           Y    =         3342797
90  meter
 Z    =        9979238
22                 Z    =         3041671
81
 XDOT =     -15633
294228                 XDOT =       -4765
028081
 YDOT =      -8867
472127  feet/sec       YDOT =       -2702
805504  meter/sec
 ZDOT =     -16173
632630                 ZDOT =       -4929
723226


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   18106
40647469  
00016717  00000-0  10270-3 0  9137
2 25544  51
6411 326
7084 0002313 352
7186   7
3932 15
54234963 28906


Satellite: ISS
Catalog Number: 25544
Epoch time:      18106
40647469   =   yrday
fracday
Element set:     913
Inclination:       51
6411  deg
RA of node:       326
7084  deg
Eccentricity:     
0002313     
Arg of perigee:   352
7186  deg
Mean anomaly:       7
3932  deg
Mean motion:   15
54234963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2890
Checksum:              307


Coasting Arc #15 (Orbit 2904)
---------------------------------------

Vector Time (GMT): 2018/107/08:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4324235
54                 A    =         6788023
77  meter
 Y    =       -5005354
98  meter          E    =           
0010304
 Z    =       -1502383
66                 I    =           51
42459
 XDOT =       4560
746220                 Wp   =           28
24049
 YDOT =       2221
520448  meter/sec      RA   =          321
26166  deg
 ZDOT =       5750
803692                 TA   =          315
30146
                                          MA   =          315
38446
                                          Ha   =            220
955  n
mi
                                          Hp   =            214
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14187124
49                 X    =         4387183
33
 Y    =      -16421768
29  feet           Y    =        -4956646
52  meter
 Z    =       -4929080
23                 Z    =        -1481224
45
 XDOT =      14963
078148                 XDOT =        4507
630701
 YDOT =       7288
452912  feet/sec       YDOT =        2272
225187  meter/sec
 ZDOT =      18867
466181                 ZDOT =        5772
829501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19494698
53                 X    =         5941984
11
 Y    =       -9583023
83  feet           Y    =        -2920905
66  meter
 Z    =       -4833962
19                 Z    =        -1473391
68
 XDOT =      10125
640630                 XDOT =        3086
295264
 YDOT =      11074
171810  feet/sec       YDOT =        3375
407568  meter/sec
 ZDOT =      18965
342011                 ZDOT =        5780
636245


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   18107
37093043  
00016717  00000-0  10270-3 0  9148
2 25544  51
6417 321
8991 0002423 355
9393   4
1740 15
54259797 29053


Satellite: ISS
Catalog Number: 25544
Epoch time:      18107
37093043   =   yrday
fracday
Element set:     914
Inclination:       51
6417  deg
RA of node:       321
8991  deg
Eccentricity:     
0002423     
Arg of perigee:   355
9393  deg
Mean anomaly:       4
1740  deg
Mean motion:   15
54259797  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2905
Checksum:              315


Coasting Arc #16 (Orbit 2920)
---------------------------------------

Vector Time (GMT): 2018/108/08:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5039473
24                 A    =         6789011
83  meter
 Y    =        4536075
79  meter          E    =           
0009922
 Z    =        -256962
77                 I    =           51
40222
 XDOT =      -3038
155781                 Wp   =          127
68022
 YDOT =      -3705
042396  meter/sec      RA   =          316
27578  deg
 ZDOT =      -5985
120194                 TA   =           55
09725
                                          MA   =           55
00404
                                          Ha   =            220
996  n
mi
                                          Hp   =            214
499

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16533704
86                 X    =        -5088574
12
 Y    =       14882138
43  feet           Y    =         4479446
39  meter
 Z    =        -843053
70                 Z    =         -281562
66
 XDOT =      -9967
702693                 XDOT =       -2967
426065
 YDOT =     -12155
650906  feet/sec       YDOT =       -3738
621868  meter/sec
 ZDOT =     -19636
221110                 ZDOT =       -5999
706870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20892401
87                 X    =        -6368004
09
 Y    =        7625659
59  feet           Y    =         2324301
04  meter
 Z    =        -953435
93                 Z    =         -290607
27
 XDOT =      -4024
524884                 XDOT =       -1226
675184
 YDOT =     -13429
655305  feet/sec       YDOT =       -4093
358937  meter/sec
 ZDOT =     -19700
697067                 ZDOT =       -6004
772466


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   18108
39968312  
00016717  00000-0  10270-3 0  9152
2 25544  51
6413 316
7704 0002292 358
8166   1
2981 15
54224534 29212


Satellite: ISS
Catalog Number: 25544
Epoch time:      18108
39968312   =   yrday
fracday
Element set:     915
Inclination:       51
6413  deg
RA of node:       316
7704  deg
Eccentricity:     
0002292     
Arg of perigee:   358
8166  deg
Mean anomaly:       1
2981  deg
Mean motion:   15
54224534  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2921
Checksum:              308


Coasting Arc #17 (Orbit 2921)
---------------------------------------

Vector Time (GMT): 2018/108/10:37:26
689
Vector Time (MET): N/A
Weight (LBS)     : 928411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4968138
64                 A    =         6780339
08  meter
 Y    =        -321456
58  meter          E    =           
0010610
 Z    =       -4613539
81                 I    =           51
36924
 XDOT =       3148
324694                 Wp   =           57
64542
 YDOT =      -6329
003244  meter/sec      RA   =          315
92124  deg
 ZDOT =      -2948
732050                 TA   =          182
82475
                                          MA   =          182
83074
                                          Ha   =            220
948  n
mi
                                          Hp   =            214
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16299667
46                 X    =        -4941764
21
 Y    =       -1054647
56  feet           Y    =         -376866
40  meter
 Z    =      -15136285
48                 Z    =        -4637609
70
 XDOT =      10329
149259                 XDOT =        3233
187003
 YDOT =     -20764
446337  feet/sec       YDOT =       -6293
322107  meter/sec
 ZDOT =      -9674
317750                 ZDOT =       -2933
231971

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16229774
88                 X    =        -4946835
38
 Y    =         356051
68  feet           Y    =          108524
55  meter
 Z    =      -15243563
02                 Z    =        -4646238
01
 XDOT =       8574
756719                 XDOT =        2613
585848
 YDOT =     -20406
381763  feet/sec       YDOT =       -6219
865161  meter/sec
 ZDOT =      -9604
238021                 ZDOT =       -2927
371749


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   18108
46397930  
00016717  00000-0  10270-3 0  9163
2 25544  51
6404 316
4494 0002252 338
8150  21
2909 15
54079102 29224


Satellite: ISS
Catalog Number: 25544
Epoch time:      18108
46397930   =   yrday
fracday
Element set:     916
Inclination:       51
6404  deg
RA of node:       316
4494  deg
Eccentricity:     
0002252     
Arg of perigee:   338
8150  deg
Mean anomaly:      21
2909  deg
Mean motion:   15
54079102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2922
Checksum:              301


Coasting Arc #18 (Orbit 2937)
---------------------------------------

Vector Time (GMT): 2018/109/10:37:26
689
Vector Time (MET): N/A
Weight (LBS)     : 928411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3994736
57                 A    =         6777941
70  meter
 Y    =        1732702
20  meter          E    =           
0002589
 Z    =        5192006
17                 I    =           51
33897
 XDOT =      -4230
664624                 Wp   =           89
33284
 YDOT =       6293
445817  meter/sec      RA   =          310
90526  deg
 ZDOT =       1154
329145                 TA   =          349
55287
                                          MA   =          349
55824
                                          Ha   =            220
902  n
mi
                                          Hp   =            214
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13106091
11                 X    =         3949843
67
 Y    =        5684718
49  feet           Y    =         1777123
12  meter
 Z    =       17034140
98                 Z    =         5211302
49
 XDOT =     -13880
133282                 XDOT =       -4306
332436
 YDOT =      20647
788114  feet/sec       YDOT =        6245
712539  meter/sec
 ZDOT =       3787
169111                 ZDOT =        1133
593853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13514296
83                 X    =         4119157
68
 Y    =        4303463
01  feet           Y    =         1311695
53  meter
 Z    =       17119918
07                 Z    =         5218151
03
 XDOT =     -11367
479232                 XDOT =       -3464
807670
 YDOT =      20997
139185  feet/sec       YDOT =        6399
928024  meter/sec
 ZDOT =       3693
757208                 ZDOT =        1125
857197


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   18109
49284631  
00016717  00000-0  10270-3 0  9171
2 25544  51
6412 311
3206 0002242 343
7020  16
4061 15
54067716 29388


Satellite: ISS
Catalog Number: 25544
Epoch time:      18109
49284631   =   yrday
fracday
Element set:     917
Inclination:       51
6412  deg
RA of node:       311
3206  deg
Eccentricity:     
0002242     
Arg of perigee:   343
7020  deg
Mean anomaly:      16
4061  deg
Mean motion:   15
54067716  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2938
Checksum:              283
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