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

 
Date: June 29th 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) : 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


187/05:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 216 1

191/20:25:31 000 0 0 0 2 0 2
N/A -0 2 0 0 220 1
000/00:00:58 000 0 0 -0 0 216 0

193/18:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 215 9

Coasting Arc #1 (Orbit 42)
---------------------------------------

Vector Time (GMT): 2018/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1958919
95                 A    =         6778276
64  meter
 Y    =        3873260
44  meter          E    =           
0000324
 Z    =        5206367
67                 I    =           51
36295
 XDOT =      -6082
675956                 Wp   =          355
98465
 YDOT =       4540
852002  meter/sec      RA   =          316
67149  deg
 ZDOT =      -1089
204467                 TA   =          104
49405
                                          MA   =          104
49046
                                          Ha   =            220
209  n
mi
                                          Hp   =            216
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6426902
74                 X    =         1890172
96
 Y    =       12707547
37  feet           Y    =         3894781
21  meter
 Z    =       17081258
76                 Z    =         5215716
98
 XDOT =     -19956
285944                 XDOT =       -6127
710206
 YDOT =      14897
808405  feet/sec       YDOT =        4472
579699  meter/sec
 ZDOT =      -3573
505468                 ZDOT =       -1118
860368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11892919
13                 X    =         3624961
75
 Y    =       -7741843
82  feet           Y    =        -2359713
99  meter
 Z    =       17122458
03                 Z    =         5218925
21
 XDOT =      16539
480227                 XDOT =        5041
233573
 YDOT =      17207
026514  feet/sec       YDOT =        5244
701682  meter/sec
 ZDOT =      -3706
889694                 ZDOT =       -1129
859979


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   18180
54630952  
00016717  00000-0  10270-3 0  9009
2 25544  51
6394 317
1056 0003726 240
9850 119
0930 15
53954593   438


Satellite: ISS
Catalog Number: 25544
Epoch time:      18180
54630952   =   yrday
fracday
Element set:     900
Inclination:       51
6394  deg
RA of node:       317
1056  deg
Eccentricity:     
0003726     
Arg of perigee:   240
9850  deg
Mean anomaly:     119
0930  deg
Mean motion:   15
53954593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              43
Checksum:              301


Coasting Arc #2 (Orbit 57)
---------------------------------------

Vector Time (GMT): 2018/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -623035
90                 A    =         6780541
95  meter
 Y    =       -4899373
76  meter          E    =           
0008173
 Z    =       -4653786
80                 I    =           51
34800
 XDOT =       6181
776901                 Wp   =          128
66790
 YDOT =      -3505
618554  meter/sec      RA   =          311
65754  deg
 ZDOT =       2861
415631                 TA   =          169
91243
                                          MA   =          169
89601
                                          Ha   =            220
107  n
mi
                                          Hp   =            216
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2044081
04                 X    =         -545598
09
 Y    =      -16074060
90  feet           Y    =        -4905907
30  meter
 Z    =      -15268329
40                 Z    =        -4656625
91
 XDOT =      20281
420278                 XDOT =        6206
619171
 YDOT =     -11501
373208  feet/sec       YDOT =       -3436
351187  meter/sec
 ZDOT =       9387
846559                 ZDOT =        2891
504018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15674933
02                 X    =        -4777719
58
 Y    =        4060287
06  feet           Y    =         1237575
50  meter
 Z    =      -15280252
87                 Z    =        -4657421
07
 XDOT =     -13787
552428                 XDOT =       -4202
445980
 YDOT =     -17369
479717  feet/sec       YDOT =       -5294
217418  meter/sec
 ZDOT =       9522
991224                 ZDOT =        2902
607725


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   18181
51092619  
00016717  00000-0  10270-3 0  9010
2 25544  51
6399 312
2990 0003888 245
5666 114
5081 15
53992481   582


Satellite: ISS
Catalog Number: 25544
Epoch time:      18181
51092619   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:       312
2990  deg
Eccentricity:     
0003888     
Arg of perigee:   245
5666  deg
Mean anomaly:     114
5081  deg
Mean motion:   15
53992481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              58
Checksum:              326


Coasting Arc #3 (Orbit 73)
---------------------------------------

Vector Time (GMT): 2018/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -619680
00                 A    =         6784204
10  meter
 Y    =        5694494
95  meter          E    =           
0008370
 Z    =        3627368
28                 I    =           51
33967
 XDOT =      -5937
238632                 Wp   =           93
73762
 YDOT =       2136
502432  meter/sec      RA   =          306
64916  deg
 ZDOT =      -4360
134883                 TA   =           43
01521
                                          MA   =           42
94980
                                          Ha   =            220
062  n
mi
                                          Hp   =            216
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2033070
87                 X    =         -700930
96
 Y    =       18682726
21  feet           Y    =         5687110
47  meter
 Z    =       11900814
55                 Z    =         3624161
55
 XDOT =     -19479
129369                 XDOT =       -5939
509373
 YDOT =       7009
522416  feet/sec       YDOT =        2070
096027  meter/sec
 ZDOT =     -14304
904471                 ZDOT =       -4388
980777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18789206
30                 X    =         5726950
08
 Y    =        -711125
69  feet           Y    =         -216751
11  meter
 Z    =       11885581
60                 Z    =         3622725
27
 XDOT =       9781
513651                 XDOT =        2981
405361
 YDOT =      16744
971182  feet/sec       YDOT =        5103
867216  meter/sec
 ZDOT =     -14434
268446                 ZDOT =       -4399
565022


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   18182
53984819  
00016717  00000-0  10270-3 0  9026
2 25544  51
6407 307
1705 0003820 248
8796 111
1949 15
53976578   748


Satellite: ISS
Catalog Number: 25544
Epoch time:      18182
53984819   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:       307
1705  deg
Eccentricity:     
0003820     
Arg of perigee:   248
8796  deg
Mean anomaly:     111
1949  deg
Mean motion:   15
53976578  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              74
Checksum:              338


Coasting Arc #4 (Orbit 88)
---------------------------------------

Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1686913
30                 A    =         6787609
99  meter
 Y    =       -6174023
85  meter          E    =           
0003502
 Z    =       -2253970
22                 I    =           51
33245
 XDOT =       5400
533301                 Wp   =            7
95984
 YDOT =       -500
386151  meter/sec      RA   =          301
65004  deg
 ZDOT =       5416
922704                 TA   =          326
86231
                                          MA   =          326
88424
                                          Ha   =            219
959  n
mi
                                          Hp   =            216
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5534492
47                 X    =         1766776
01
 Y    =      -20255983
77  feet           Y    =        -6154712
82  meter
 Z    =       -7394915
42                 Z    =        -2245582
65
 XDOT =      17718
285107                 XDOT =        5379
415182
 YDOT =      -1641
686847  feet/sec       YDOT =        -440
112385  meter/sec
 ZDOT =      17772
056117                 ZDOT =        5443
104923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20904113
31                 X    =        -6371573
74
 Y    =       -2126256
07  feet           Y    =         -648082
85  meter
 Z    =       -7356448
96                 Z    =        -2242245
64
 XDOT =      -4708
120992                 XDOT =       -1435
035278
 YDOT =     -15555
551599  feet/sec       YDOT =       -4741
332127  meter/sec
 ZDOT =      17889
247326                 ZDOT =        5452
642585


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   18183
50445754  
00016717  00000-0  10270-3 0  9035
2 25544  51
6408 302
3635 0003745 256
0704 104
0033 15
53985710   893


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
50445754   =   yrday
fracday
Element set:     903
Inclination:       51
6408  deg
RA of node:       302
3635  deg
Eccentricity:     
0003745     
Arg of perigee:   256
0704  deg
Mean anomaly:     104
0033  deg
Mean motion:   15
53985710  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              89
Checksum:              292


Coasting Arc #5 (Orbit 104)
---------------------------------------

Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2565143
16                 A    =         6789538
16  meter
 Y    =        6246794
73  meter          E    =           
0011128
 Z    =         637278
33                 I    =           51
32181
 XDOT =      -4668
146107                 Wp   =          143
60900
 YDOT =      -1306
007955  meter/sec      RA   =          296
65728  deg
 ZDOT =      -5943
459768                 TA   =           29
47874
                                          MA   =           29
41603
                                          Ha   =            219
872  n
mi
                                          Hp   =            216
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8415824
03                 X    =        -2637901
42
 Y    =       20494733
37  feet           Y    =         6217702
65  meter
 Z    =        2090808
15                 Z    =          624641
83
 XDOT =     -15315
439983                 XDOT =       -4624
325187
 YDOT =      -4284
803002  feet/sec       YDOT =       -1357
964751  meter/sec
 ZDOT =     -19499
539921                 ZDOT =       -5966
029431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21694809
27                 X    =         6612577
87
 Y    =        4520225
84  feet           Y    =         1377764
83  meter
 Z    =        2033341
55                 Z    =          619762
51
 XDOT =      -1093
501246                 XDOT =        -333
299180
 YDOT =      14132
867758  feet/sec       YDOT =        4307
698093  meter/sec
 ZDOT =     -19600
296520                 ZDOT =       -5974
170379


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   18184
53337196  
00016717  00000-0  10270-3 0  9040
2 25544  51
6400 297
2358 0003813 257
3679 102
7047 15
54001166  1054


Satellite: ISS
Catalog Number: 25544
Epoch time:      18184
53337196   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       297
2358  deg
Eccentricity:     
0003813     
Arg of perigee:   257
3679  deg
Mean anomaly:     102
7047  deg
Mean motion:   15
54001166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             105
Checksum:              298


Coasting Arc #6 (Orbit 120)
---------------------------------------

Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3219934
06                 A    =         6789196
28  meter
 Y    =       -5881874
06  meter          E    =           
0010419
 Z    =        1025046
96                 I    =           51
30812
 XDOT =       3820
721952                 Wp   =           46
81285
 YDOT =       3120
229727  meter/sec      RA   =          291
66524  deg
 ZDOT =       5871
695583                 TA   =          324
35022
                                          MA   =          324
41976
                                          Ha   =            219
825  n
mi
                                          Hp   =            216
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10564088
11                 X    =         3280488
39
 Y    =      -19297487
06  feet           Y    =        -5845528
05  meter
 Z    =        3363014
96                 Z    =         1040834
66
 XDOT =      12535
177007                 XDOT =        3757
025410
 YDOT =      10236
974171  feet/sec       YDOT =        3162
598986  meter/sec
 ZDOT =      19264
093119                 ZDOT =        5890
100723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21019750
13                 X    =        -6406819
84
 Y    =       -6455780
90  feet           Y    =        -1967722
02  meter
 Z    =        3434506
03                 Z    =         1046837
44
 XDOT =       7070
422085                 XDOT =        2155
064651
 YDOT =     -12676
232436  feet/sec       YDOT =       -3863
715646  meter/sec
 ZDOT =      19345
954497                 ZDOT =        5896
646931


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   18185
56228196  
00016717  00000-0  10270-3 0  9054
2 25544  51
6411 292
1077 0003721 263
7056  96
3673 15
54015203  1214


Satellite: ISS
Catalog Number: 25544
Epoch time:      18185
56228196   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:       292
1077  deg
Eccentricity:     
0003721     
Arg of perigee:   263
7056  deg
Mean anomaly:      96
3673  deg
Mean motion:   15
54015203  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             121
Checksum:              292


Coasting Arc #7 (Orbit 135)
---------------------------------------

Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3694785
25                 A    =         6786720
01  meter
 Y    =        5059141
95  meter          E    =           
0003183
 Z    =       -2605602
52                 I    =           51
28819
 XDOT =      -2916
595089                 Wp   =          174
57511
 YDOT =      -4810
205212  meter/sec      RA   =          286
66884  deg
 ZDOT =      -5207
544375                 TA   =           34
90701
                                          MA   =           34
88614
                                          Ha   =            219
775  n
mi
                                          Hp   =            216
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12121998
84                 X    =        -3738426
81
 Y    =       16598234
76  feet           Y    =         5017580
53  meter
 Z    =       -8548564
69                 Z    =        -2623655
94
 XDOT =      -9568
881524                 XDOT =       -2837
293959
 YDOT =     -15781
513163  feet/sec       YDOT =       -4842
376738  meter/sec
 ZDOT =     -17085
119342                 ZDOT =       -5221
519896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18823896
14                 X    =         5737523
54
 Y    =        8167330
98  feet           Y    =         2489402
48  meter
 Z    =       -8630055
04                 Z    =        -2630440
78
 XDOT =     -12753
634826                 XDOT =       -3887
307895
 YDOT =      11288
403962  feet/sec       YDOT =        3440
705528  meter/sec
 ZDOT =     -17146
927073                 ZDOT =       -5226
383372


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   18186
52688123  
00016717  00000-0  10270-3 0  9062
2 25544  51
6406 287
3004 0003745 267
3375  92
7349 15
54016427  1369


Satellite: ISS
Catalog Number: 25544
Epoch time:      18186
52688123   =   yrday
fracday
Element set:     906
Inclination:       51
6406  deg
RA of node:       287
3004  deg
Eccentricity:     
0003745     
Arg of perigee:   267
3375  deg
Mean anomaly:      92
7349  deg
Mean motion:   15
54016427  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             136
Checksum:              315


Coasting Arc #8 (Orbit 146)
---------------------------------------

Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2052373
69                 A    =         6783029
79  meter
 Y    =       -5134733
81  meter          E    =           
0003018
 Z    =       -3931776
48                 I    =           51
26590
 XDOT =       4407
465692                 Wp   =          119
38085
 YDOT =      -4825
592417  meter/sec      RA   =          282
98683  deg
 ZDOT =       4002
211693                 TA   =          192
64305
                                          MA   =          192
65062
                                          Ha   =            219
773  n
mi
                                          Hp   =            216
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6733509
47                 X    =        -1975704
74
 Y    =      -16846239
54  feet           Y    =        -5157255
84  meter
 Z    =      -12899529
14                 Z    =        -3941560
39
 XDOT =      14460
189277                 XDOT =        4441
658681
 YDOT =     -15831
996120  feet/sec       YDOT =       -4776
114262  meter/sec
 ZDOT =      13130
615790                 ZDOT =        4023
704159

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7956054
67                 X    =        -2425005
46
 Y    =      -16270384
32  feet           Y    =        -4959213
14  meter
 Z    =      -12942549
07                 Z    =        -3944888
96
 XDOT =      11892
826041                 XDOT =        3624
933377
 YDOT =     -16335
192697  feet/sec       YDOT =       -4978
966734  meter/sec
 ZDOT =      13227
446261                 ZDOT =        4031
725620


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   18187
23425148  
00016717  00000-0  10270-3 0  9078
2 25544  51
6371 283
7757 0003792 276
4977  83
5743 15
54026951  1477


Satellite: ISS
Catalog Number: 25544
Epoch time:      18187
23425148   =   yrday
fracday
Element set:     907
Inclination:       51
6371  deg
RA of node:       283
7757  deg
Eccentricity:     
0003792     
Arg of perigee:   276
4977  deg
Mean anomaly:      83
5743  deg
Mean motion:   15
54026951  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             147
Checksum:              339


Coasting Arc #9 (Orbit 162)
---------------------------------------

Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1259651
64                 A    =         6786595
38  meter
 Y    =        6129043
14  meter          E    =           
0009534
 Z    =        2616574
18                 I    =           51
27260
 XDOT =      -4655
062083                 Wp   =          103
00972
 YDOT =       3181
667129  meter/sec      RA   =          277
97993  deg
 ZDOT =      -5197
777580                 TA   =           47
35141
                                          MA   =           47
27109
                                          Ha   =            219
691  n
mi
                                          Hp   =            216
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4132715
35                 X    =         1178311
46
 Y    =       20108409
24  feet           Y    =         6142674
38  meter
 Z    =        8584560
96                 Z    =         2622496
15
 XDOT =     -15272
513395                 XDOT =       -4665
046375
 YDOT =      10438
540451  feet/sec       YDOT =        3129
555686  meter/sec
 ZDOT =     -17053
076049                 ZDOT =       -5220
414161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5987691
37                 X    =         1825048
33
 Y    =       19624845
77  feet           Y    =         5981652
99  meter
 Z    =        8610175
71                 Z    =         2624381
56
 XDOT =     -12655
871855                 XDOT =       -3857
509741
 YDOT =      11407
857804  feet/sec       YDOT =        3477
115059  meter/sec
 ZDOT =     -17154
780410                 ZDOT =       -5228
777069


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   18188
26315142  
00016717  00000-0  10270-3 0  9085
2 25544  51
6379 278
6471 0004060 282
2466  77
8231 15
54064836  1638


Satellite: ISS
Catalog Number: 25544
Epoch time:      18188
26315142   =   yrday
fracday
Element set:     908
Inclination:       51
6379  deg
RA of node:       278
6471  deg
Eccentricity:     
0004060     
Arg of perigee:   282
2466  deg
Mean anomaly:      77
8231  deg
Mean motion:   15
54064836  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             163
Checksum:              317


Coasting Arc #10 (Orbit 177)
---------------------------------------

Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -498643
39                 A    =         6789136
77  meter
 Y    =       -6682825
69  meter          E    =           
0008717
 Z    =       -1054371
31                 I    =           51
27650
 XDOT =       4774
149836                 Wp   =           15
05481
 YDOT =      -1278
247642  meter/sec      RA   =          272
98025  deg
 ZDOT =       5863
170730                 TA   =          333
45401
                                          MA   =          333
49863
                                          Ha   =            219
844  n
mi
                                          Hp   =            216
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1635969
13                 X    =         -418755
56
 Y    =      -21925281
14  feet           Y    =        -6687955
07  meter
 Z    =       -3459223
47                 Z    =        -1056600
26
 XDOT =      15663
221247                 XDOT =        4759
608544
 YDOT =      -4193
725860  feet/sec       YDOT =       -1224
941760  meter/sec
 ZDOT =      19236
124443                 ZDOT =        5886
326434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4082961
02                 X    =        -1244486
52
 Y    =      -21602343
04  feet           Y    =        -6584394
16  meter
 Z    =       -3468253
10                 Z    =        -1057123
55
 XDOT =      13386
113354                 XDOT =        4080
087350
 YDOT =      -5624
972925  feet/sec       YDOT =       -1714
491747  meter/sec
 ZDOT =      19339
879425                 ZDOT =        5894
795249


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   18189
22774509  
00016717  00000-0  10270-3 0  9099
2 25544  51
6372 273
8382 0003794 283
8159  76
2571 15
54031019  1781


Satellite: ISS
Catalog Number: 25544
Epoch time:      18189
22774509   =   yrday
fracday
Element set:     909
Inclination:       51
6372  deg
RA of node:       273
8382  deg
Eccentricity:     
0003794     
Arg of perigee:   283
8159  deg
Mean anomaly:      76
2571  deg
Mean motion:   15
54031019  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             178
Checksum:              334


Coasting Arc #11 (Orbit 193)
---------------------------------------

Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -272590
88                 A    =         6789302
48  meter
 Y    =        6749698
65  meter          E    =           
0007567
 Z    =        -635640
43                 I    =           51
27669
 XDOT =      -4791
052832                 Wp   =          152
92186
 YDOT =       -749
496758  meter/sec      RA   =          267
98569  deg
 ZDOT =      -5938
680303                 TA   =           33
97479
                                          MA   =           33
92635
                                          Ha   =            219
931  n
mi
                                          Hp   =            216
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -894327
04                 X    =         -344960
00
 Y    =       22144680
59  feet           Y    =         6746245
79  meter
 Z    =       -2085434
48                 Z    =         -637139
48
 XDOT =     -15718
677270                 XDOT =       -4753
468695
 YDOT =      -2458
978864  feet/sec       YDOT =        -802
862697  meter/sec
 ZDOT =     -19483
859262                 ZDOT =       -5961
862396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2010198
98                 X    =          612708
65
 Y    =       22070656
06  feet           Y    =         6727135
97  meter
 Z    =       -2093078
53                 Z    =         -637970
34
 XDOT =     -14167
395608                 XDOT =       -4318
222181
 YDOT =       -556
492017  feet/sec       YDOT =        -169
618767  meter/sec
 ZDOT =     -19587
452726                 ZDOT =       -5970
255591


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   18190
25663964  
00016717  00000-0  10270-3 0  9108
2 25544  51
6370 268
7098 0003776 291
6383  68
4367 15
54077679  1948


Satellite: ISS
Catalog Number: 25544
Epoch time:      18190
25663964   =   yrday
fracday
Element set:     910
Inclination:       51
6370  deg
RA of node:       268
7098  deg
Eccentricity:     
0003776     
Arg of perigee:   291
6383  deg
Mean anomaly:      68
4367  deg
Mean motion:   15
54077679  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             194
Checksum:              350


Coasting Arc #12 (Orbit 209)
---------------------------------------

Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1034688
08                 A    =         6787445
90  meter
 Y    =       -6315693
60  meter          E    =           
0011233
 Z    =        2241896
17                 I    =           51
27145
 XDOT =       4710
134090                 Wp   =           60
09677
 YDOT =       2700
285812  meter/sec      RA   =          262
98818  deg
 ZDOT =       5418
251354                 TA   =          324
97717
                                          MA   =          325
05100
                                          Ha   =            219
959  n
mi
                                          Hp   =            216
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3394645
93                 X    =         1094345
07
 Y    =      -20720779
52  feet           Y    =        -6303789
78  meter
 Z    =        7355302
40                 Z    =         2247066
27
 XDOT =      15453
195833                 XDOT =        4653
269724
 YDOT =       8859
205419  feet/sec       YDOT =        2752
639020  meter/sec
 ZDOT =      17776
415205                 ZDOT =        5440
993811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         258615
82                 X    =           78826
10
 Y    =      -20986992
91  feet           Y    =        -6396835
44  meter
 Z    =        7379298
41                 Z    =         2249210
16
 XDOT =      14942
055012                 XDOT =        4554
338368
 YDOT =       6487
368052  feet/sec       YDOT =        1977
349782  meter/sec
 ZDOT =      17877
782380                 ZDOT =        5449
148069


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   18191
28553428  
00016717  00000-0  10270-3 0  9116
2 25544  51
6362 263
5810 0003656 290
5108  69
5652 15
54039370  2108


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
28553428   =   yrday
fracday
Element set:     911
Inclination:       51
6362  deg
RA of node:       263
5810  deg
Eccentricity:     
0003656     
Arg of perigee:   290
5108  deg
Mean anomaly:      69
5652  deg
Mean motion:   15
54039370  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             210
Checksum:              298


Coasting Arc #13 (Orbit 218)
---------------------------------------

Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947556
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4346389
17                 A    =         6778841
13  meter
 Y    =       -1340974
71  meter          E    =           
0009273
 Z    =       -5034620
46                 I    =           51
24777
 XDOT =        165
152189                 Wp   =           98
16705
 YDOT =      -7435
224992  meter/sec      RA   =          259
82197  deg
 ZDOT =       1839
425187                 TA   =          189
75501
                                          MA   =          189
77302
                                          Ha   =            220
091  n
mi
                                          Hp   =            216
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14259806
99                 X    =        -4306615
56
 Y    =       -4399523
33  feet           Y    =        -1389355
84  meter
 Z    =      -16517783
65                 Z    =        -5055637
24
 XDOT =        541
837890                 XDOT =         239
347723
 YDOT =     -24393
782783  feet/sec       YDOT =       -7432
963588  meter/sec
 ZDOT =       6034
859536                 ZDOT =        1840
406455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11825744
08                 X    =         3604486
79
 Y    =       -8929769
40  feet           Y    =        -2721793
71  meter
 Z    =      -16611624
64                 Z    =        -5063223
19
 XDOT =      18873
928173                 XDOT =        5752
773307
 YDOT =      13768
290977  feet/sec       YDOT =        4196
575090  meter/sec
 ZDOT =       6040
262428                 ZDOT =        1841
071988


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   18191
86428632  
00016717  00000-0  10270-3 0  9129
2 25544  51
6387 260
6999 0003994 297
0944  62
9801 15
54002786  2199


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
86428632   =   yrday
fracday
Element set:     912
Inclination:       51
6387  deg
RA of node:       260
6999  deg
Eccentricity:     
0003994     
Arg of perigee:   297
0944  deg
Mean anomaly:      62
9801  deg
Mean motion:   15
54002786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             219
Checksum:              342


Coasting Arc #14 (Orbit 234)
---------------------------------------

Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947556
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4353775
48                 A    =         6781837
71  meter
 Y    =        2967174
19  meter          E    =           
0007828
 Z    =        4268156
25                 I    =           51
26500
 XDOT =      -1108
858998                 Wp   =           49
55360
 YDOT =       6716
624128  meter/sec      RA   =          254
80310  deg
 ZDOT =      -3528
943035                 TA   =           76
64675
                                          MA   =           76
55949
                                          Ha   =            220
165  n
mi
                                          Hp   =            216
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14284040
29                 X    =         4299539
88
 Y    =        9734823
45  feet           Y    =         3015557
14  meter
 Z    =       14003137
29                 Z    =         4289173
96
 XDOT =      -3637
988837                 XDOT =       -1166
742138
 YDOT =      22036
168399  feet/sec       YDOT =        6703
901049  meter/sec
 ZDOT =     -11577
897097                 ZDOT =       -3534
468900

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16080889
32                 X    =        -4901455
07
 Y    =        6129790
36  feet           Y    =         1868360
10  meter
 Z    =       14096776
84                 Z    =         4296697
58
 XDOT =     -15647
000250                 XDOT =       -4769
205676
 YDOT =     -14294
007391  feet/sec       YDOT =       -4356
813453  meter/sec
 ZDOT =     -11603
522211                 ZDOT =       -3536
753570


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   18192
89319967  
00016717  00000-0  10270-3 0  9134
2 25544  51
6390 255
5721 0004051 302
3775  57
6986 15
54012628  2355


Satellite: ISS
Catalog Number: 25544
Epoch time:      18192
89319967   =   yrday
fracday
Element set:     913
Inclination:       51
6390  deg
RA of node:       255
5721  deg
Eccentricity:     
0004051     
Arg of perigee:   302
3775  deg
Mean anomaly:      57
6986  deg
Mean motion:   15
54012628  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             235
Checksum:              323


Coasting Arc #15 (Orbit 248)
---------------------------------------

Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947556
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3358435
27                 A    =         6778375
34  meter
 Y    =        2871184
07  meter          E    =           
0011466
 Z    =       -5150412
75                 I    =           51
26014
 XDOT =      -3562
388892                 Wp   =           64
79098
 YDOT =      -6639
906481  meter/sec      RA   =          250
21177  deg
 ZDOT =      -1376
211927                 TA   =          191
87823
                                          MA   =          191
90530
                                          Ha   =            220
353  n
mi
                                          Hp   =            215
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11018488
42                 X    =        -3365274
42
 Y    =        9419895
25  feet           Y    =         2833590
34  meter
 Z    =      -16897679
62                 Z    =        -5166742
77
 XDOT =     -11687
627600                 XDOT =       -3481
190059
 YDOT =     -21784
470081  feet/sec       YDOT =       -6679
289335  meter/sec
 ZDOT =      -4515
130995                 ZDOT =       -1393
320393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5036403
91                 X    =         1535095
91
 Y    =      -13501424
37  feet           Y    =        -4115234
15  meter
 Z    =      -16971130
37                 Z    =        -5172800
54
 XDOT =      19709
225748                 XDOT =        6007
372008
 YDOT =      13132
470399  feet/sec       YDOT =        4002
776978  meter/sec
 ZDOT =      -4590
809965                 ZDOT =       -1399
278877


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   18193
79349735  
00016717  00000-0  10270-3 0  9141
2 25544  51
6370 251
0843 0004012 305
8935  54
1845 15
54001810  2494


Satellite: ISS
Catalog Number: 25544
Epoch time:      18193
79349735   =   yrday
fracday
Element set:     914
Inclination:       51
6370  deg
RA of node:       251
0843  deg
Eccentricity:     
0004012     
Arg of perigee:   305
8935  deg
Mean anomaly:      54
1845  deg
Mean motion:   15
54001810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             249
Checksum:              299


Coasting Arc #16 (Orbit 264)
---------------------------------------

Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947556
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4079034
32                 A    =         6777778
34  meter
 Y    =       -1245651
99  meter          E    =           
0003614
 Z    =        5268393
89                 I    =           51
27056
 XDOT =       2834
333795                 Wp   =          351
19547
 YDOT =       7106
728680  meter/sec      RA   =          245
18805  deg
 ZDOT =       -510
703234                 TA   =          103
72217
                                          MA   =          103
68194
                                          Ha   =            220
305  n
mi
                                          Hp   =            215
984

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13382658
54                 X    =         4067069
82
 Y    =       -4086784
75  feet           Y    =        -1200105
08  meter
 Z    =       17284756
86                 Z    =         5288178
79
 XDOT =       9298
995392                 XDOT =        2757
134426
 YDOT =      23316
038978  feet/sec       YDOT =        7137
992582  meter/sec
 ZDOT =      -1675
535543                 ZDOT =        -497
121764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9497977
62                 X    =        -2894983
58
 Y    =       10124796
24  feet           Y    =         3086037
90  meter
 Z    =       17373459
68                 Z    =         5295430
51
 XDOT =     -18904
706351                 XDOT =       -5762
154496
 YDOT =     -14942
544290  feet/sec       YDOT =       -4554
487500  meter/sec
 ZDOT =      -1615
673508                 ZDOT =        -492
457285


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   18194
82240795  
00016717  00000-0  10270-3 0  9153
2 25544  51
6372 245
9568 0004063 309
7025  50
3769 15
54008885  2651


Satellite: ISS
Catalog Number: 25544
Epoch time:      18194
82240795   =   yrday
fracday
Element set:     915
Inclination:       51
6372  deg
RA of node:       245
9568  deg
Eccentricity:     
0004063     
Arg of perigee:   309
7025  deg
Mean anomaly:      50
3769  deg
Mean motion:   15
54008885  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             265
Checksum:              328
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