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

 
Date: June 14th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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


172/07:16:38 985 1 2 1 3 1 3
N/A 0 2 -0 1 220 4
000/00:03:17 970 0 5 -0 0 216 0

Coasting Arc #1 (Orbit 3793)
---------------------------------------

Vector Time (GMT): 2018/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5918194
51                 A    =         6788483
41  meter
 Y    =       -2988580
17  meter          E    =           
0015385
 Z    =        1417862
61                 I    =           51
88766
 XDOT =       1066
062922                 Wp   =          129
85683
 YDOT =      -4886
602762  meter/sec      RA   =           36
45050  deg
 ZDOT =      -5818
124597                 TA   =           34
72901
                                          MA   =           34
62867
                                          Ha   =            221
246  n
mi
                                          Hp   =            214
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19416648
64                 X    =        -5891222
82
 Y    =       -9805053
05  feet           Y    =        -3054610
94  meter
 Z    =        4651780
23                 Z    =         1389178
82
 XDOT =       3497
581766                 XDOT =        1148
888632
 YDOT =     -16032
161294  feet/sec       YDOT =       -4874
217183  meter/sec
 ZDOT =     -19088
335291                 ZDOT =       -5812
745676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12764531
79                 X    =        -3890629
29
 Y    =       17646118
44  feet           Y    =         5378536
90  meter
 Z    =        4523892
27                 Z    =         1378882
36
 XDOT =     -13969
359468                 XDOT =       -4257
860766
 YDOT =      -5189
875981  feet/sec       YDOT =       -1581
874199  meter/sec
 ZDOT =     -19063
458318                 ZDOT =       -5810
542095


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   18164
53487101  
00016717  00000-0  10270-3 0  9006
2 25544  51
6418  36
9276 0003101 185
1082 175
0039 15
54143578 37941


Satellite: ISS
Catalog Number: 25544
Epoch time:      18164
53487101   =   yrday
fracday
Element set:     900
Inclination:       51
6418  deg
RA of node:        36
9276  deg
Eccentricity:     
0003101     
Arg of perigee:   185
1082  deg
Mean anomaly:     175
0039  deg
Mean motion:   15
54143578  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3794
Checksum:              301


Coasting Arc #2 (Orbit 3809)
---------------------------------------

Vector Time (GMT): 2018/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5657964
67                 A    =         6789075
62  meter
 Y    =        3733616
08  meter          E    =           
0010364
 Z    =         290002
66                 I    =           51
86315
 XDOT =      -2830
551370                 Wp   =           58
00998
 YDOT =       3809
959424  meter/sec      RA   =           31
49543  deg
 ZDOT =       6021
159803                 TA   =          305
10509
                                          MA   =          305
20221
                                          Ha   =            220
962  n
mi
                                          Hp   =            214
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18562876
22                 X    =         5614385
16
 Y    =       12249396
60  feet           Y    =         3796643
62  meter
 Z    =         951452
28                 Z    =          317382
01
 XDOT =      -9286
585859                 XDOT =       -2902
192695
 YDOT =      12499
866875  feet/sec       YDOT =        3777
904562  meter/sec
 ZDOT =      19754
461295                 ZDOT =        6007
236629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14753156
85                 X    =         4496762
21
 Y    =      -16635070
80  feet           Y    =        -5070369
58  meter
 Z    =        1073375
19                 Z    =          327164
76
 XDOT =       9829
273139                 XDOT =        2995
962453
 YDOT =      10016
409474  feet/sec       YDOT =        3053
001608  meter/sec
 ZDOT =      19691
514163                 ZDOT =        6001
973517


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   18165
56367189  
00016717  00000-0  10270-3 0  9014
2 25544  51
6418  31
7982 0003038 193
5291 166
5781 15
54200069 38109


Satellite: ISS
Catalog Number: 25544
Epoch time:      18165
56367189   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:        31
7982  deg
Eccentricity:     
0003038     
Arg of perigee:   193
5291  deg
Mean anomaly:     166
5781  deg
Mean motion:   15
54200069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3810
Checksum:              317


Coasting Arc #3 (Orbit 3824)
---------------------------------------

Vector Time (GMT): 2018/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4923317
43                 A    =         6787500
44  meter
 Y    =       -4216081
33  meter          E    =           
0008609
 Z    =       -2000005
36                 I    =           51
82834
 XDOT =       4532
066772                 Wp   =          156
65426
 YDOT =      -2648
289273  meter/sec      RA   =           26
53731  deg
 ZDOT =      -5589
610523                 TA   =           45
37221
                                          MA   =           45
30203
                                          Ha   =            220
887  n
mi
                                          Hp   =            214
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16152616
24                 X    =        -4866091
21
 Y    =      -13832287
83  feet           Y    =        -4270816
92  meter
 Z    =       -6561697
37                 Z    =        -2023782
82
 XDOT =      14868
985473                 XDOT =        4588
495116
 YDOT =      -8688
613101  feet/sec       YDOT =       -2597
292054  meter/sec
 ZDOT =     -18338
617200                 ZDOT =       -5567
458814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15731093
02                 X    =        -4794837
15
 Y    =       14260902
54  feet           Y    =         4346723
09  meter
 Z    =       -6667416
41                 Z    =        -2032228
52
 XDOT =      -5715
899663                 XDOT =       -1742
206217
 YDOT =     -14808
440722  feet/sec       YDOT =       -4513
612732  meter/sec
 ZDOT =     -18239
031506                 ZDOT =       -5559
256803


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   18166
52817336  
00016717  00000-0  10270-3 0  9026
2 25544  51
6413  26
9893 0003030 198
4939 161
6104 15
54154213 38256


Satellite: ISS
Catalog Number: 25544
Epoch time:      18166
52817336   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:        26
9893  deg
Eccentricity:     
0003030     
Arg of perigee:   198
4939  deg
Mean anomaly:     161
6104  deg
Mean motion:   15
54154213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3825
Checksum:              306


Coasting Arc #4 (Orbit 3840)
---------------------------------------

Vector Time (GMT): 2018/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3785649
04                 A    =         6784046
14  meter
 Y    =        4430832
31  meter          E    =           
0011581
 Z    =        3465936
43                 I    =           51
78577
 XDOT =      -5968
937458                 Wp   =          104
38412
 YDOT =       1511
166422  meter/sec      RA   =           21
56970  deg
 ZDOT =       4572
088892                 TA   =          296
20068
                                          MA   =          296
31971
                                          Ha   =            220
789  n
mi
                                          Hp   =            214
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12420108
41                 X    =         3718985
36
 Y    =       14536851
40  feet           Y    =         4472792
73  meter
 Z    =       11371182
53                 Z    =         3484164
48
 XDOT =     -19583
128142                 XDOT =       -6007
600725
 YDOT =       4957
895084  feet/sec       YDOT =        1444
200712  meter/sec
 ZDOT =      15000
291642                 ZDOT =        4543
000441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15779899
82                 X    =         4809713
46
 Y    =      -10711152
47  feet           Y    =        -3264759
27  meter
 Z    =       11452026
39                 Z    =         3490577
64
 XDOT =       2034
719176                 XDOT =         620
182405
 YDOT =      18950
239489  feet/sec       YDOT =        5776
032996  meter/sec
 ZDOT =      14869
849023                 ZDOT =        4532
329982


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   18167
55697253  
00016717  00000-0  10270-3 0  9035
2 25544  51
6401  21
8597 0002860 201
7356 158
3675 15
54169049 38416


Satellite: ISS
Catalog Number: 25544
Epoch time:      18167
55697253   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:        21
8597  deg
Eccentricity:     
0002860     
Arg of perigee:   201
7356  deg
Mean anomaly:     158
3675  deg
Mean motion:   15
54169049  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3841
Checksum:              325


Coasting Arc #5 (Orbit 3855)
---------------------------------------

Vector Time (GMT): 2018/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2267548
98                 A    =         6780183
49  meter
 Y    =       -4452678
27  meter          E    =           
0008261
 Z    =       -4590427
63                 I    =           51
74145
 XDOT =       7013
004213                 Wp   =           83
75737
 YDOT =       -425
080350  meter/sec      RA   =           16
58966  deg
 ZDOT =      -3055
760252                 TA   =          155
73603
                                          MA   =          155
69711
                                          Ha   =            220
694  n
mi
                                          Hp   =            214
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7439465
17                 X    =        -2195291
74
 Y    =      -14608524
51  feet           Y    =        -4477630
89  meter
 Z    =      -15060458
10                 Z    =        -4601267
62
 XDOT =      23008
544005                 XDOT =        7032
079475
 YDOT =      -1394
620572  feet/sec       YDOT =        -346
549012  meter/sec
 ZDOT =     -10025
460144                 ZDOT =       -3021
647589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15212938
26                 X    =        -4636903
58
 Y    =        5989982
58  feet           Y    =         1825746
69  meter
 Z    =      -15108231
09                 Z    =        -4604988
84
 XDOT =       1131
178581                 XDOT =         344
783232
 YDOT =     -21996
827926  feet/sec       YDOT =       -6704
633152  meter/sec
 ZDOT =      -9872
716047                 ZDOT =       -3009
203851


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   18168
52146935  
00016717  00000-0  10270-3 0  9040
2 25544  51
6396  17
0508 0002980 207
1276 152
9721 15
54185023 38560


Satellite: ISS
Catalog Number: 25544
Epoch time:      18168
52146935   =   yrday
fracday
Element set:     904
Inclination:       51
6396  deg
RA of node:        17
0508  deg
Eccentricity:     
0002980     
Arg of perigee:   207
1276  deg
Mean anomaly:     152
9721  deg
Mean motion:   15
54185023  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3856
Checksum:              314


Coasting Arc #6 (Orbit 3871)
---------------------------------------

Vector Time (GMT): 2018/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         535911
78                 A    =         6777723
03  meter
 Y    =        4306432
64  meter          E    =           
0005143
 Z    =        5205410
17                 I    =           51
70154
 XDOT =      -7549
434133                 Wp   =          157
61255
 YDOT =       -556
058240  meter/sec      RA   =           11
59822  deg
 ZDOT =       1232
214025                 TA   =          280
54530
                                          MA   =          280
60324
                                          Ha   =            220
691  n
mi
                                          Hp   =            215
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1758240
75                 X    =          462431
36
 Y    =       14128716
01  feet           Y    =         4312014
10  meter
 Z    =       17078117
34                 Z    =         5207835
46
 XDOT =     -24768
484688                 XDOT =       -7548
640435
 YDOT =      -1824
338057  feet/sec       YDOT =        -640
476924  meter/sec
 ZDOT =       4042
696933                 ZDOT =        1195
543722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14212585
97                 X    =         4331996
20
 Y    =        -606674
43  feet           Y    =         -184914
37  meter
 Z    =       17088255
17                 Z    =         5208500
18
 XDOT =      -3677
755723                 XDOT =       -1120
979945
 YDOT =      23558
374997  feet/sec       YDOT =        7180
592699  meter/sec
 ZDOT =       3878
677005                 ZDOT =        1182
220751


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   18169
55026518  
00016717  00000-0  10270-3 0  9059
2 25544  51
6401  11
9211 0002899 208
9189 151
1804 15
54159142 38726


Satellite: ISS
Catalog Number: 25544
Epoch time:      18169
55026518   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:        11
9211  deg
Eccentricity:     
0002899     
Arg of perigee:   208
9189  deg
Mean anomaly:     151
1804  deg
Mean motion:   15
54159142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3872
Checksum:              309


Coasting Arc #7 (Orbit 3886)
---------------------------------------

Vector Time (GMT): 2018/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1303233
58                 A    =         6777364
66  meter
 Y    =       -4054820
12  meter          E    =           
0013563
 Z    =       -5283515
23                 I    =           51
66618
 XDOT =       7484
769085                 Wp   =          106
84932
 YDOT =       1448
726745  meter/sec      RA   =            6
59981  deg
 ZDOT =        732
091490                 TA   =          170
16347
                                          MA   =          170
13690
                                          Ha   =            220
612  n
mi
                                          Hp   =            215
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4275700
71                 X    =         1374143
15
 Y    =      -13303215
60  feet           Y    =        -4039849
45  meter
 Z    =      -17334367
54                 Z    =        -5277012
80
 XDOT =      24556
329018                 XDOT =        7464
456658
 YDOT =       4753
040503  feet/sec       YDOT =        1532
312946  meter/sec
 ZDOT =       2401
874967                 ZDOT =         768
400428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13037808
18                 X    =        -3973923
93
 Y    =       -5128740
48  feet           Y    =        -1563240
10  meter
 Z    =      -17304595
88                 Z    =        -5274440
83
 XDOT =       5746
269638                 XDOT =        1751
462986
 YDOT =     -23284
394619  feet/sec       YDOT =       -7097
083480  meter/sec
 ZDOT =       2564
119314                 ZDOT =         781
543567


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   18170
51475767  
00016717  00000-0  10270-3 0  9062
2 25544  51
6383   7
1117 0002936 211
4214 148
6763 15
54195720 38870


Satellite: ISS
Catalog Number: 25544
Epoch time:      18170
51475767   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:         7
1117  deg
Eccentricity:     
0002936     
Arg of perigee:   211
4214  deg
Mean anomaly:     148
6763  deg
Mean motion:   15
54195720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3887
Checksum:              316


Coasting Arc #8 (Orbit 3902)
---------------------------------------

Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3054990
68                 A    =         6779526
40  meter
 Y    =        3702245
28  meter          E    =           
0004930
 Z    =        4784098
01                 I    =           51
64087
 XDOT =      -6846
097529                 Wp   =           75
95496
 YDOT =      -2263
400865  meter/sec      RA   =            1
60339  deg
 ZDOT =      -2616
727702                 TA   =           39
85123
                                          MA   =           39
81504
                                          Ha   =            220
573  n
mi
                                          Hp   =            215
230

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10022935
30                 X    =        -3119401
67
 Y    =       12146474
00  feet           Y    =         3667721
68  meter
 Z    =       15695859
61                 Z    =         4769101
89
 XDOT =     -22460
949899                 XDOT =       -6807
568122
 YDOT =      -7425
855855  feet/sec       YDOT =       -2339
742977  meter/sec
 ZDOT =      -8585
064638                 ZDOT =       -2649
890146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11745371
16                 X    =         3579989
13
 Y    =       10590726
53  feet           Y    =         3228053
45  meter
 Z    =       15628142
55                 Z    =         4763457
85
 XDOT =      -7518
539449                 XDOT =       -2291
650824
 YDOT =      21241
848556  feet/sec       YDOT =        6474
515440  meter/sec
 ZDOT =      -8733
082579                 ZDOT =       -2661
843570


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   18171
54354918  
00016717  00000-0  10270-3 0  9071
2 25544  51
6388   1
9831 0003065 217
9706 142
1231 15
54186117 39039


Satellite: ISS
Catalog Number: 25544
Epoch time:      18171
54354918   =   yrday
fracday
Element set:     907
Inclination:       51
6388  deg
RA of node:         1
9831  deg
Eccentricity:     
0003065     
Arg of perigee:   217
9706  deg
Mean anomaly:     142
1231  deg
Mean motion:   15
54186117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3903
Checksum:              304


Coasting Arc #9 (Orbit 3914)
---------------------------------------

Vector Time (GMT): 2018/172/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3165577
71                 A    =         6780785
67  meter
 Y    =       -3810275
17  meter          E    =           
0008608
 Z    =       -4638796
99                 I    =           51
62005
 XDOT =       6771
834597                 Wp   =          127
08111
 YDOT =       2045
707314  meter/sec      RA   =          357
59398  deg
 ZDOT =       2939
557032                 TA   =          172
23358
                                          MA   =          172
22024
                                          Ha   =            220
409  n
mi
                                          Hp   =            216
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10385753
65                 X    =         3230482
77
 Y    =      -12500902
77  feet           Y    =        -3774512
16  meter
 Z    =      -15219150
23                 Z    =        -4623262
44
 XDOT =      22217
305107                 XDOT =        6734
176848
 YDOT =       6711
638169  feet/sec       YDOT =        2121
223812  meter/sec
 ZDOT =       9644
215983                 ZDOT =        2972
360926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6072105
18                 X    =         1850777
66
 Y    =      -15145824
44  feet           Y    =        -4616447
29  meter
 Z    =      -15149010
64                 Z    =        -4617418
44
 XDOT =      22037
265069                 XDOT =        6716
958393
 YDOT =       -962
068521  feet/sec       YDOT =        -293
238485  meter/sec
 ZDOT =       9790
656715                 ZDOT =        2984
192167


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   18172
31514257  
00016717  00000-0  10270-3 0  9082
2 25544  51
6425 358
1388 0003320 238
1950 121
8880 15
53963198 39153


Satellite: ISS
Catalog Number: 25544
Epoch time:      18172
31514257   =   yrday
fracday
Element set:     908
Inclination:       51
6425  deg
RA of node:       358
1388  deg
Eccentricity:     
0003320     
Arg of perigee:   238
1950  deg
Mean anomaly:     121
8880  deg
Mean motion:   15
53963198  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3915
Checksum:              319


Coasting Arc #10 (Orbit 3930)
---------------------------------------

Vector Time (GMT): 2018/173/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4577535
10                 A    =         6784401
34  meter
 Y    =        3471424
35  meter          E    =           
0009335
 Z    =        3599980
10                 I    =           51
59885
 XDOT =      -5608
132229                 Wp   =           95
10556
 YDOT =      -2803
664692  meter/sec      RA   =          352
60553  deg
 ZDOT =      -4418
386244                 TA   =           42
24095
                                          MA   =           42
16908
                                          Ha   =            220
464  n
mi
                                          Hp   =            215
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15018159
78                 X    =        -4633500
14
 Y    =       11389187
49  feet           Y    =         3419921
92  meter
 Z    =       11810958
35                 Z    =         3577608
40
 XDOT =     -18399
383955                 XDOT =       -5554
901855
 YDOT =      -9198
374975  feet/sec       YDOT =       -2866
080629  meter/sec
 ZDOT =     -14496
017860                 ZDOT =       -4445
499636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10530273
37                 X    =        -3209627
32
 Y    =       15707956
79  feet           Y    =         4787785
23  meter
 Z    =       11710289
85                 Z    =         3569296
35
 XDOT =     -19161
481279                 XDOT =       -5840
419494
 YDOT =      -1926
217027  feet/sec       YDOT =        -587
110950  meter/sec
 ZDOT =     -14616
862313                 ZDOT =       -4455
219633


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   18173
34408651  
00016717  00000-0  10270-3 0  9097
2 25544  51
6422 353
0114 0003145 241
4673 118
6163 15
53964720 39313


Satellite: ISS
Catalog Number: 25544
Epoch time:      18173
34408651   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:       353
0114  deg
Eccentricity:     
0003145     
Arg of perigee:   241
4673  deg
Mean anomaly:     118
6163  deg
Mean motion:   15
53964720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3931
Checksum:              294


Coasting Arc #11 (Orbit 3945)
---------------------------------------

Vector Time (GMT): 2018/174/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5640600
61                 A    =         6787730
42  meter
 Y    =       -3045841
91  meter          E    =           
0003438
 Z    =       -2226435
40                 I    =           51
57726
 XDOT =       4060
956983                 Wp   =           19
36343
 YDOT =       3537
981431  meter/sec      RA   =          347
62358  deg
 ZDOT =       5453
807067                 TA   =          315
87915
                                          MA   =          315
90657
                                          Ha   =            220
259  n
mi
                                          Hp   =            216
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18505907
50                 X    =         5685055
71
 Y    =       -9992919
66  feet           Y    =        -2982516
01  meter
 Z    =       -7304578
08                 Z    =        -2198927
59
 XDOT =      13323
349681                 XDOT =        3994
600681
 YDOT =      11607
550627  feet/sec       YDOT =        3583
022218  meter/sec
 ZDOT =      17893
067806                 ZDOT =        5473
373086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13985728
57                 X    =         4262850
07
 Y    =      -15764403
91  feet           Y    =        -4804990
31  meter
 Z    =       -7181008
44                 Z    =        -2188771
37
 XDOT =      15241
783240                 XDOT =        4645
695532
 YDOT =       5340
306195  feet/sec       YDOT =        1627
725328  meter/sec
 ZDOT =      17980
017083                 ZDOT =        5480
309207


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   18174
30871908  
00016717  00000-0  10270-3 0  9105
2 25544  51
6419 348
2037 0003281 246
3917 113
6891 15
53978738 39468


Satellite: ISS
Catalog Number: 25544
Epoch time:      18174
30871908   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       348
2037  deg
Eccentricity:     
0003281     
Arg of perigee:   246
3917  deg
Mean anomaly:     113
6891  deg
Mean motion:   15
53978738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3946
Checksum:              337


Coasting Arc #12 (Orbit 3961)
---------------------------------------

Vector Time (GMT): 2018/175/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6284944
57                 A    =         6789759
10  meter
 Y    =        2475541
34  meter          E    =           
0011806
 Z    =         615160
54                 I    =           51
55186
 XDOT =      -2264
841872                 Wp   =          142
63971
 YDOT =      -4254
856818  meter/sec      RA   =          342
64767  deg
 ZDOT =      -5965
918081                 TA   =           30
71037
                                          MA   =           30
64133
                                          Ha   =            220
269  n
mi
                                          Hp   =            216
121

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20619896
88                 X    =        -6315147
78
 Y    =        8121854
80  feet           Y    =         2405089
80  meter
 Z    =        2018243
24                 Z    =          584557
30
 XDOT =      -7430
583568                 XDOT =       -2188
115180
 YDOT =     -13959
503996  feet/sec       YDOT =       -4279
754062  meter/sec
 ZDOT =     -19573
222050                 ZDOT =       -5976
734135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16325744
09                 X    =        -4976086
80
 Y    =       15005004
91  feet           Y    =         4573525
50  meter
 Z    =        1880926
97                 Z    =          573306
54
 XDOT =     -10742
882698                 XDOT =       -3274
430646
 YDOT =      -9206
447223  feet/sec       YDOT =       -2806
125114  meter/sec
 ZDOT =     -19620
904483                 ZDOT =       -5980
451686


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   18175
33766063  
00016717  00000-0  10270-3 0  9115
2 25544  51
6421 343
0762 0003325 248
0007 112
0792 15
53933372 39623


Satellite: ISS
Catalog Number: 25544
Epoch time:      18175
33766063   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:       343
0762  deg
Eccentricity:     
0003325     
Arg of perigee:   248
0007  deg
Mean anomaly:     112
0792  deg
Mean motion:   15
53933372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3962
Checksum:              292


Coasting Arc #13 (Orbit 3977)
---------------------------------------

Vector Time (GMT): 2018/176/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6467245
91                 A    =         6789248
63  meter
 Y    =       -1766762
36  meter          E    =           
0010508
 Z    =        1035248
97                 I    =           51
51947
 XDOT =        390
526781                 Wp   =           50
10190
 YDOT =       4898
545087  meter/sec      RA   =          337
66995  deg
 ZDOT =       5887
148438                 TA   =          321
13974
                                          MA   =          321
21525
                                          Ha   =            220
058  n
mi
                                          Hp   =            216
048

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21217998
38                 X    =         6481492
96
 Y    =       -5796464
44  feet           Y    =        -1694361
65  meter
 Z    =        3396486
11                 Z    =         1066699
04
 XDOT =       1281
255843                 XDOT =         307
124147
 YDOT =      16071
342149  feet/sec       YDOT =        4902
445030  meter/sec
 ZDOT =      19314
791463                 ZDOT =        5888
843634

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17460647
75                 X    =         5322005
43
 Y    =      -13339815
48  feet           Y    =        -4065975
76  meter
 Z    =        3537467
49                 Z    =         1078220
09
 XDOT =       6138
970508                 XDOT =        1871
158211
 YDOT =      13186
739255  feet/sec       YDOT =        4019
318125  meter/sec
 ZDOT =      19321
565256                 ZDOT =        5889
213090


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   18176
36659608  
00016717  00000-0  10270-3 0  9126
2 25544  51
6419 337
9471 0003368 256
5711 103
5067 15
53987445 39789


Satellite: ISS
Catalog Number: 25544
Epoch time:      18176
36659608   =   yrday
fracday
Element set:     912
Inclination:       51
6419  deg
RA of node:       337
9471  deg
Eccentricity:     
0003368     
Arg of perigee:   256
5711  deg
Mean anomaly:     103
5067  deg
Mean motion:   15
53987445  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3978
Checksum:              349


Coasting Arc #14 (Orbit 3992)
---------------------------------------

Vector Time (GMT): 2018/177/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6204285
84                 A    =         6786878
07  meter
 Y    =         870235
45  meter          E    =           
0003626
 Z    =       -2604962
18                 I    =           51
47997
 XDOT =       1431
975961                 Wp   =          168
91490
 YDOT =      -5421
840482  meter/sec      RA   =          332
68759  deg
 ZDOT =      -5226
526749                 TA   =           40
47257
                                          MA   =           40
44560
                                          Ha   =            220
020  n
mi
                                          Hp   =            216
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20355268
50                 X    =        -6200902
40
 Y    =        2855103
18  feet           Y    =          800874
18  meter
 Z    =       -8546463
84                 Z    =        -2635092
11
 XDOT =       4698
083862                 XDOT =        1517
885759
 YDOT =     -17788
190558  feet/sec       YDOT =       -5405
345953  meter/sec
 ZDOT =     -17147
397469                 ZDOT =       -5219
362909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17556266
02                 X    =        -5351149
88
 Y    =       10580248
09  feet           Y    =         3224859
62  meter
 Z    =       -8681387
45                 Z    =        -2646086
89
 XDOT =      -1772
778609                 XDOT =        -540
342920
 YDOT =     -16972
086173  feet/sec       YDOT =       -5173
091866  meter/sec
 ZDOT =     -17114
458365                 ZDOT =       -5216
486910


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   18177
33122431  
00016717  00000-0  10270-3 0  9134
2 25544  51
6407 333
1397 0003425 259
4612 100
6155 15
53950036 39936


Satellite: ISS
Catalog Number: 25544
Epoch time:      18177
33122431   =   yrday
fracday
Element set:     913
Inclination:       51
6407  deg
RA of node:       333
1397  deg
Eccentricity:     
0003425     
Arg of perigee:   259
4612  deg
Mean anomaly:     100
6155  deg
Mean motion:   15
53950036  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3993
Checksum:              294


Coasting Arc #15 (Orbit 4008)
---------------------------------------

Vector Time (GMT): 2018/178/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5545154
17                 A    =         6783260
16  meter
 Y    =         170401
60  meter          E    =           
0007878
 Z    =        3898249
24                 I    =           51
43931
 XDOT =      -3038
302700                 Wp   =          105
28459
 YDOT =       5751
864767  meter/sec      RA   =          327
69434  deg
 ZDOT =       4061
571877                 TA   =          302
04372
                                          MA   =          302
12023
                                          Ha   =            219
937  n
mi
                                          Hp   =            216
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18192763
03                 X    =         5523900
98
 Y    =         559060
38  feet           Y    =          232291
85  meter
 Z    =       12789531
63                 Z    =         3925134
02
 XDOT =      -9968
184711                 XDOT =       -3122
124738
 YDOT =      18870
947398  feet/sec       YDOT =        5717
419015  meter/sec
 ZDOT =      13325
367050                 ZDOT =        4046
610264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16763214
15                 X    =         5109427
67
 Y    =       -6869781
75  feet           Y    =        -2093909
48  meter
 Z    =       12909765
46                 Z    =         3934896
51
 XDOT =      -1990
969539                 XDOT =        -606
847516
 YDOT =      20109
774465  feet/sec       YDOT =        6129
459257  meter/sec
 ZDOT =      13257
498048                 ZDOT =        4040
885405


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   18178
36015964  
00016717  00000-0  10270-3 0  9141
2 25544  51
6409 328
0113 0003343 266
0438  94
0332 15
53957637 40092


Satellite: ISS
Catalog Number: 25544
Epoch time:      18178
36015964   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       328
0113  deg
Eccentricity:     
0003343     
Arg of perigee:   266
0438  deg
Mean anomaly:      94
0332  deg
Mean motion:   15
53957637  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4009
Checksum:              307


Coasting Arc #16 (Orbit 4023)
---------------------------------------

Vector Time (GMT): 2018/179/07:18:17
970
Vector Time (MET): N/A
Weight (LBS)     : 922901
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4575693
38                 A    =         6779770
37  meter
 Y    =       -1354621
98  meter          E    =           
0008481
 Z    =       -4824034
89                 I    =           51
40018
 XDOT =       4339
685266                 Wp   =           65
10960
 YDOT =      -5803
162146  meter/sec      RA   =          322
68845  deg
 ZDOT =      -2486
654489                 TA   =          180
35076
                                          MA   =          180
35136
                                          Ha   =            219
941  n
mi
                                          Hp   =            216
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15012117
37                 X    =        -4536773
07
 Y    =       -4444297
82  feet           Y    =        -1405572
11  meter
 Z    =      -15826886
13                 Z    =        -4846167
59
 XDOT =      14237
812553                 XDOT =        4416
334067
 YDOT =     -19039
245887  feet/sec       YDOT =       -5754
203808  meter/sec
 ZDOT =      -8158
315251                 ZDOT =       -2465
388730

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15387362
88                 X    =        -4690068
20
 Y    =        2282079
31  feet           Y    =          695577
77  meter
 Z    =      -15925669
64                 Z    =        -4854144
11
 XDOT =       5055
383639                 XDOT =        1540
880933
 YDOT =     -22177
387214  feet/sec       YDOT =       -6759
667623  meter/sec
 ZDOT =      -8062
246322                 ZDOT =       -2457
372679


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   18179
32478216  
00016717  00000-0  10270-3 0  9152
2 25544  51
6406 323
2028 0003471 269
5498  90
5257 15
53985367 40242


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
32478216   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:       323
2028  deg
Eccentricity:     
0003471     
Arg of perigee:   269
5498  deg
Mean anomaly:      90
5257  deg
Mean motion:   15
53985367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4024
Checksum:              328
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