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

 
Date: September 12th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


257/13:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 214 1

257/20:59:14 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 214 3

261/11:24:45 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 214 6

267/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 215 2

Coasting Arc #1 (Orbit 1208)
---------------------------------------

Vector Time (GMT): 2018/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3083478
61                 A    =         6789841
01  meter
 Y    =        5982564
97  meter          E    =           
0017816
 Z    =         821545
82                 I    =           51
34102
 XDOT =      -4626
862370                 Wp   =          132
29311
 YDOT =      -1562
397798  meter/sec      RA   =          302
87084  deg
 ZDOT =      -5917
764597                 TA   =           38
78053
                                          MA   =           38
65280
                                          Ha   =            222
673  n
mi
                                          Hp   =            214
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10116399
65                 X    =        -3154138
79
 Y    =       19627837
83  feet           Y    =         5947688
38  meter
 Z    =        2695360
31                 Z    =          806395
02
 XDOT =     -15179
994653                 XDOT =       -4580
301873
 YDOT =      -5125
977027  feet/sec       YDOT =       -1613
878909  meter/sec
 ZDOT =     -19415
238179                 ZDOT =       -5940
127079

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13214214
03                 X    =         4027692
44
 Y    =      -17701519
92  feet           Y    =        -5395423
27  meter
 Z    =        2626645
54                 Z    =          800601
56
 XDOT =      12715
842198                 XDOT =        3875
788702
 YDOT =       6561
359256  feet/sec       YDOT =        1999
902301  meter/sec
 ZDOT =     -19515
326097                 ZDOT =       -5948
271394


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   18255
53375049  
00016717  00000-0  10270-3 0  9004
2 25544  51
6399 303
4235 0004769 150
1493 209
9932 15
53860871 12094


Satellite: ISS
Catalog Number: 25544
Epoch time:      18255
53375049   =   yrday
fracday
Element set:     900
Inclination:       51
6399  deg
RA of node:       303
4235  deg
Eccentricity:     
0004769     
Arg of perigee:   150
1493  deg
Mean anomaly:     209
9932  deg
Mean motion:   15
53860871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1209
Checksum:              322


Coasting Arc #2 (Orbit 1224)
---------------------------------------

Vector Time (GMT): 2018/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3686566
01                 A    =         6790003
23  meter
 Y    =       -5644681
20  meter          E    =           
0013516
 Z    =         773293
78                 I    =           51
32355
 XDOT =       3660
975843                 Wp   =           73
30590
 YDOT =       3213
255716  meter/sec      RA   =          297
88073  deg
 ZDOT =       5919
779177                 TA   =          295
08723
                                          MA   =          295
22744
                                          Ha   =            222
729  n
mi
                                          Hp   =            214
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12095032
83                 X    =         3745656
13
 Y    =      -18519295
27  feet           Y    =        -5603124
99  meter
 Z    =        2537053
07                 Z    =          791345
99
 XDOT =      12011
075602                 XDOT =        3596
016920
 YDOT =      10542
177545  feet/sec       YDOT =        3253
832651  meter/sec
 ZDOT =      19421
847693                 ZDOT =        5937
404931

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14667574
59                 X    =        -4470676
73
 Y    =       16543738
72  feet           Y    =         5042531
56  meter
 Z    =        2618724
81                 Z    =          798187
32
 XDOT =      -8997
407726                 XDOT =       -2742
409875
 YDOT =     -11105
206381  feet/sec       YDOT =       -3384
866905  meter/sec
 ZDOT =      19500
482530                 ZDOT =        5943
747075


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   18256
56277591  
00016717  00000-0  10270-3 0  9012
2 25544  51
6394 298
2961 0004659 151
6492 208
4914 15
53804090 12252


Satellite: ISS
Catalog Number: 25544
Epoch time:      18256
56277591   =   yrday
fracday
Element set:     901
Inclination:       51
6394  deg
RA of node:       298
2961  deg
Eccentricity:     
0004659     
Arg of perigee:   151
6492  deg
Mean anomaly:     208
4914  deg
Mean motion:   15
53804090  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1225
Checksum:              328


Coasting Arc #3 (Orbit 1239)
---------------------------------------

Vector Time (GMT): 2018/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4093942
68                 A    =         6787747
42  meter
 Y    =        4877783
78  meter          E    =           
0010276
 Z    =       -2340127
22                 I    =           51
30253
 XDOT =      -2647
764951                 Wp   =          143
99379
 YDOT =      -4788
831226  meter/sec      RA   =          292
88675  deg
 ZDOT =      -5369
947586                 TA   =           62
23454
                                          MA   =           62
13038
                                          Ha   =            222
556  n
mi
                                          Hp   =            214
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13431570
47                 X    =        -4136815
97
 Y    =       16003227
61  feet           Y    =         4831762
57  meter
 Z    =       -7677582
75                 Z    =        -2360118
82
 XDOT =      -8686
892885                 XDOT =       -2567
933592
 YDOT =     -15711
388536  feet/sec       YDOT =       -4817
994432  meter/sec
 ZDOT =     -17617
938274                 ZDOT =       -5382
615307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15345310
65                 X    =         4677250
69
 Y    =      -14129319
75  feet           Y    =        -4306616
66  meter
 Z    =       -7767845
29                 Z    =        -2367639
24
 XDOT =       5425
963298                 XDOT =        1653
833613
 YDOT =      15573
591075  feet/sec       YDOT =        4746
830560  meter/sec
 ZDOT =     -17674
144706                 ZDOT =       -5387
079306


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   18257
52748278  
00016717  00000-0  10270-3 0  9025
2 25544  51
6399 293
4889 0004808 156
2823 203
8551 15
53853874 12405


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
52748278   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       293
4889  deg
Eccentricity:     
0004808     
Arg of perigee:   156
2823  deg
Mean anomaly:     203
8551  deg
Mean motion:   15
53853874  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1240
Checksum:              344


Coasting Arc #4 (Orbit 1240)
---------------------------------------

Vector Time (GMT): 2018/257/13:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3747234
17                 A    =         6778299
64  meter
 Y    =       -2031058
02  meter          E    =           
0017382
 Z    =       -5285246
65                 I    =           51
26819
 XDOT =       3208
661758                 Wp   =          107
21844
 YDOT =      -6939
807419  meter/sec      RA   =          292
48125  deg
 ZDOT =        387
959643                 TA   =          166
52957
                                          MA   =          166
48311
                                          Ha   =            222
615  n
mi
                                          Hp   =            214
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12294075
37                 X    =        -3698570
72
 Y    =       -6663576
18  feet           Y    =        -2072690
51  meter
 Z    =      -17340048
07                 Z    =        -5303331
17
 XDOT =      10527
105505                 XDOT =        3284
141620
 YDOT =     -22768
397044  feet/sec       YDOT =       -6903
503874  meter/sec
 ZDOT =       1272
833474                 ZDOT =         403
730174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13727709
81                 X    =         4184205
95
 Y    =        2070582
17  feet           Y    =          631113
45  meter
 Z    =      -17420891
96                 Z    =        -5309887
87
 XDOT =      -1896
686753                 XDOT =        -578
110122
 YDOT =      23995
749473  feet/sec       YDOT =        7313
904439  meter/sec
 ZDOT =       1344
424825                 ZDOT =         409
780687


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   18257
59179597  
00016717  00000-0  10270-3 0  9035
2 25544  51
6385 293
1692 0004743 157
4165 202
7197 15
53825219 12416


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
59179597   =   yrday
fracday
Element set:     903
Inclination:       51
6385  deg
RA of node:       293
1692  deg
Eccentricity:     
0004743     
Arg of perigee:   157
4165  deg
Mean anomaly:     202
7197  deg
Mean motion:   15
53825219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1241
Checksum:              335


Coasting Arc #5 (Orbit 1245)
---------------------------------------

Vector Time (GMT): 2018/257/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         501862
71                 A    =         6785752
70  meter
 Y    =        5934208
58  meter          E    =           
0015307
 Z    =        3234558
51                 I    =           51
29079
 XDOT =      -5224
516084                 Wp   =          108
67110
 YDOT =       3029
874062  meter/sec      RA   =          290
96863  deg
 ZDOT =      -4734
461712                 TA   =           33
62101
                                          MA   =           33
52399
                                          Ha   =            222
537  n
mi
                                          Hp   =            214
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1646531
19                 X    =          419755
57
 Y    =       19469188
24  feet           Y    =         5939361
90  meter
 Z    =       10612068
59                 Z    =         3236796
53
 XDOT =     -17140
800801                 XDOT =       -5235
011023
 YDOT =       9940
531700  feet/sec       YDOT =        2971
390871  meter/sec
 ZDOT =     -15533
010867                 ZDOT =       -4759
866462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14437933
48                 X    =        -4400682
12
 Y    =       13157091
78  feet           Y    =         4010281
57  meter
 Z    =       10621363
78                 Z    =         3237391
68
 XDOT =     -17325
471439                 XDOT =       -5280
803695
 YDOT =      -6344
437327  feet/sec       YDOT =       -1933
784497  meter/sec
 ZDOT =     -15647
314257                 ZDOT =       -4769
301385


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   18257
91336716  
00016717  00000-0  10270-3 0  9040
2 25544  51
6400 291
5682 0004631 157
8969 202
2384 15
53829246 12469


Satellite: ISS
Catalog Number: 25544
Epoch time:      18257
91336716   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       291
5682  deg
Eccentricity:     
0004631     
Arg of perigee:   157
8969  deg
Mean anomaly:     202
2384  deg
Mean motion:   15
53829246  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1246
Checksum:              323


Coasting Arc #6 (Orbit 1260)
---------------------------------------

Vector Time (GMT): 2018/258/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         338385
90                 A    =         6788665
12  meter
 Y    =       -6527741
10  meter          E    =           
0006019
 Z    =       -1834871
57                 I    =           51
29138
 XDOT =       5051
354977                 Wp   =           76
69428
 YDOT =      -1310
336605  meter/sec      RA   =          285
96807  deg
 ZDOT =       5610
162600                 TA   =          263
04185
                                          MA   =          263
11032
                                          Ha   =            222
388  n
mi
                                          Hp   =            214
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1110189
95                 X    =          420268
64
 Y    =      -21416473
41  feet           Y    =        -6523499
31  meter
 Z    =       -6019919
85                 Z    =        -1833028
52
 XDOT =      16572
686932                 XDOT =        5038
380753
 YDOT =      -4299
004608  feet/sec       YDOT =       -1253
921050  meter/sec
 ZDOT =      18406
045274                 ZDOT =        5634
669014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17433444
36                 X    =         5313713
84
 Y    =      -12493277
56  feet           Y    =        -3807951
00  meter
 Z    =       -6010850
50                 Z    =        -1832107
23
 XDOT =      12728
314287                 XDOT =        3879
590195
 YDOT =       8879
607117  feet/sec       YDOT =        2706
504249  meter/sec
 ZDOT =      18516
103786                 ZDOT =        5643
708434


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   18258
87807140  
00016717  00000-0  10270-3 0  9051
2 25544  51
6413 286
7604 0004492 162
9650 197
1654 15
53865544 12612


Satellite: ISS
Catalog Number: 25544
Epoch time:      18258
87807140   =   yrday
fracday
Element set:     905
Inclination:       51
6413  deg
RA of node:       286
7604  deg
Eccentricity:     
0004492     
Arg of perigee:   162
9650  deg
Mean anomaly:     197
1654  deg
Mean motion:   15
53865544  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1261
Checksum:              327


Coasting Arc #7 (Orbit 1276)
---------------------------------------

Vector Time (GMT): 2018/259/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1111404
00                 A    =         6790220
41  meter
 Y    =        6685635
11  meter          E    =           
0016544
 Z    =         226668
23                 I    =           51
28777
 XDOT =      -4769
832695                 Wp   =          141
12865
 YDOT =       -582
526494  meter/sec      RA   =          280
97446  deg
 ZDOT =      -5980
648420                 TA   =           36
41618
                                          MA   =           36
30374
                                          Ha   =            222
407  n
mi
                                          Hp   =            214
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3646338
58                 X    =        -1187183
06
 Y    =       21934498
40  feet           Y    =         6672782
93  meter
 Z    =         743662
16                 Z    =          221084
98
 XDOT =     -15649
057397                 XDOT =       -4733
913300
 YDOT =      -1911
176160  feet/sec       YDOT =        -635
665558  meter/sec
 ZDOT =     -19621
549935                 ZDOT =       -6003
731401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19211422
43                 X    =        -5855641
56
 Y    =       11197188
57  feet           Y    =         3412903
08  meter
 Z    =         717812
76                 Z    =          218789
33
 XDOT =      -7621
313658                 XDOT =       -2322
976403
 YDOT =     -11762
609436  feet/sec       YDOT =       -3585
243356  meter/sec
 ZDOT =     -19724
995099                 ZDOT =       -6012
178506


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   18259
90708893  
00016717  00000-0  10270-3 0  9062
2 25544  51
6410 281
6333 0004603 165
9834 194
1447 15
53816475 12776


Satellite: ISS
Catalog Number: 25544
Epoch time:      18259
90708893   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:       281
6333  deg
Eccentricity:     
0004603     
Arg of perigee:   165
9834  deg
Mean anomaly:     194
1447  deg
Mean motion:   15
53816475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1277
Checksum:              332


Coasting Arc #8 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2018/260/20:59:14
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1771045
66                 A    =         6789326
35  meter
 Y    =       -6406502
04  meter          E    =           
0012997
 Z    =        1364441
01                 I    =           51
27930
 XDOT =       4400
258985                 Wp   =           78
53693
 YDOT =       2456
396889  meter/sec      RA   =          275
98033  deg
 ZDOT =       5777
696836                 TA   =          296
39870
                                          MA   =          296
53205
                                          Ha   =            222
223  n
mi
                                          Hp   =            214
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5810517
26                 X    =         1835925
58
 Y    =      -21018707
49  feet           Y    =        -6386334
15  meter
 Z    =        4476512
49                 Z    =         1373202
05
 XDOT =      14436
545225                 XDOT =        4344
398821
 YDOT =       8059
044913  feet/sec       YDOT =        2505
291608  meter/sec
 ZDOT =      18955
698282                 ZDOT =        5798
935970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19708898
61                 X    =         6007272
30
 Y    =       -9313822
09  feet           Y    =        -2838852
97  meter
 Z    =        4516566
52                 Z    =         1376649
48
 XDOT =       2533
655286                 XDOT =         772
258131
 YDOT =      14669
659709  feet/sec       YDOT =        4471
312279  meter/sec
 ZDOT =      19050
655551                 ZDOT =        5806
639812


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   18260
93610307  
00016717  00000-0  10270-3 0  9070
2 25544  51
6404 276
5057 0004346 170
5189 189
6046 15
53853935 12938


Satellite: ISS
Catalog Number: 25544
Epoch time:      18260
93610307   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       276
5057  deg
Eccentricity:     
0004346     
Arg of perigee:   170
5189  deg
Mean anomaly:     189
6046  deg
Mean motion:   15
53853935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1293
Checksum:              322


Coasting Arc #9 (Orbit 1301)
---------------------------------------

Vector Time (GMT): 2018/261/11:24:45
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2481348
23                 A    =         6785031
46  meter
 Y    =        5294418
48  meter          E    =           
0013889
 Z    =        3426277
92                 I    =           51
26159
 XDOT =      -3904
154046                 Wp   =          108
35425
 YDOT =       4784
768061  meter/sec      RA   =          272
93007  deg
 ZDOT =      -4555
258498                 TA   =           31
24229
                                          MA   =           31
15982
                                          Ha   =            222
189  n
mi
                                          Hp   =            214
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8140906
26                 X    =         2405317
12
 Y    =       17370139
36  feet           Y    =         5321741
70  meter
 Z    =       11241069
28                 Z    =         3438146
48
 XDOT =     -12808
904349                 XDOT =       -3935
241464
 YDOT =      15698
057943  feet/sec       YDOT =        4740
935035  meter/sec
 ZDOT =     -14945
073813                 ZDOT =       -4574
299270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4161803
11                 X    =        -1268517
59
 Y    =      -18694653
66  feet           Y    =        -5698130
43  meter
 Z    =       11293673
20                 Z    =         3442311
59
 XDOT =      14410
732646                 XDOT =        4392
391311
 YDOT =     -12310
093528  feet/sec       YDOT =       -3752
116507  meter/sec
 ZDOT =     -15031
030696                 ZDOT =       -4581
458156


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   18261
51492274  
00016717  00000-0  10270-3 0  9087
2 25544  51
6386 273
6202 0004584 169
6414 190
4834 15
53876958 13027


Satellite: ISS
Catalog Number: 25544
Epoch time:      18261
51492274   =   yrday
fracday
Element set:     908
Inclination:       51
6386  deg
RA of node:       273
6202  deg
Eccentricity:     
0004584     
Arg of perigee:   169
6414  deg
Mean anomaly:     190
4834  deg
Mean motion:   15
53876958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1302
Checksum:              328


Coasting Arc #10 (Orbit 1316)
---------------------------------------

Vector Time (GMT): 2018/262/11:24:45
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1876882
12                 A    =         6788164
55  meter
 Y    =       -6190997
77  meter          E    =           
0004854
 Z    =       -2059768
33                 I    =           51
27317
 XDOT =       4306
242496                 Wp   =           86
19715
 YDOT =      -3134
082699  meter/sec      RA   =          267
92757  deg
 ZDOT =       5507
734075                 TA   =          250
91744
                                          MA   =          250
97002
                                          Ha   =            222
177  n
mi
                                          Hp   =            214
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6157749
75                 X    =        -1797507
94
 Y    =      -20311672
47  feet           Y    =        -6211542
68  meter
 Z    =       -6757770
10                 Z    =        -2068692
38
 XDOT =      14128
092179                 XDOT =        4314
215041
 YDOT =     -10282
423554  feet/sec       YDOT =       -3085
882398  meter/sec
 ZDOT =      18069
993683                 ZDOT =        5528
671798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1987892
83                 X    =          605909
73
 Y    =       21118649
60  feet           Y    =         6436964
40  meter
 Z    =       -6797080
14                 Z    =        -2071750
03
 XDOT =     -14219
755014                 XDOT =       -4334
181328
 YDOT =       7172
540855  feet/sec       YDOT =        2186
190452  meter/sec
 ZDOT =      18164
259529                 ZDOT =        5536
466304


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   18262
47962088  
00016717  00000-0  10270-3 0  9099
2 25544  51
6400 268
8132 0004645 172
9353 187
1865 15
53901639 13177


Satellite: ISS
Catalog Number: 25544
Epoch time:      18262
47962088   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       268
8132  deg
Eccentricity:     
0004645     
Arg of perigee:   172
9353  deg
Mean anomaly:     187
1865  deg
Mean motion:   15
53901639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1317
Checksum:              330


Coasting Arc #11 (Orbit 1332)
---------------------------------------

Vector Time (GMT): 2018/263/11:24:45
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1202447
70                 A    =         6790015
73  meter
 Y    =        6656946
27  meter          E    =           
0016361
 Z    =         466714
31                 I    =           51
27913
 XDOT =      -4659
677938                 Wp   =          141
36044
 YDOT =       1266
743614  meter/sec      RA   =          262
93197  deg
 ZDOT =      -5962
134492                 TA   =           33
57836
                                          MA   =           33
47478
                                          Ha   =            222
104  n
mi
                                          Hp   =            214
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3945038
38                 X    =         1125651
47
 Y    =       21840374
90  feet           Y    =         6669963
51  meter
 Z    =        1531214
92                 Z    =          472368
35
 XDOT =     -15287
657278                 XDOT =       -4644
535913
 YDOT =       4155
982987  feet/sec       YDOT =        1214
720099  meter/sec
 ZDOT =     -19560
808702                 ZDOT =       -5984
732810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          66881
35                 X    =           20385
43
 Y    =      -22191999
91  feet           Y    =        -6764121
57  meter
 Z    =        1555824
33                 Z    =          474215
26
 XDOT =      14039
638825                 XDOT =        4279
281914
 YDOT =      -1358
964357  feet/sec       YDOT =        -414
212336  meter/sec
 ZDOT =     -19662
307976                 ZDOT =       -5993
071471


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   18263
50863035  
00016717  00000-0  10270-3 0  9108
2 25544  51
6380 263
6855 0004500 176
1010 184
0178 15
53861231 13339


Satellite: ISS
Catalog Number: 25544
Epoch time:      18263
50863035   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       263
6855  deg
Eccentricity:     
0004500     
Arg of perigee:   176
1010  deg
Mean anomaly:     184
0178  deg
Mean motion:   15
53861231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1333
Checksum:              281


Coasting Arc #12 (Orbit 1348)
---------------------------------------

Vector Time (GMT): 2018/264/11:24:45
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -494246
53                 A    =         6789468
09  meter
 Y    =       -6671889
28  meter          E    =           
0011671
 Z    =        1136172
63                 I    =           51
28187
 XDOT =       4924
318371                 Wp   =           76
18776
 YDOT =        637
994445  meter/sec      RA   =          257
93847  deg
 ZDOT =       5840
667316                 TA   =          296
20369
                                          MA   =          296
32365
                                          Ha   =            221
968  n
mi
                                          Hp   =            214
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1621543
73                 X    =         -425121
78
 Y    =      -21889400
53  feet           Y    =        -6677029
69  meter
 Z    =        3727600
49                 Z    =         1133940
24
 XDOT =      16155
900167                 XDOT =        4888
447392
 YDOT =       2093
157627  feet/sec       YDOT =         692
861531  meter/sec
 ZDOT =      19162
294345                 ZDOT =        5864
500663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1950838
30                 X    =         -594615
52
 Y    =       21864093
56  feet           Y    =         6664175
72  meter
 Z    =        3718320
51                 Z    =         1133344
09
 XDOT =     -13876
487394                 XDOT =       -4229
553358
 YDOT =      -4541
951449  feet/sec       YDOT =       -1384
386802  meter/sec
 ZDOT =      19269
124803                 ZDOT =        5873
229240


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   18264
53763659  
00016717  00000-0  10270-3 0  9114
2 25544  51
6371 258
5583 0004566 182
4687 177
6444 15
53893813 13494


Satellite: ISS
Catalog Number: 25544
Epoch time:      18264
53763659   =   yrday
fracday
Element set:     911
Inclination:       51
6371  deg
RA of node:       258
5583  deg
Eccentricity:     
0004566     
Arg of perigee:   182
4687  deg
Mean anomaly:     177
6444  deg
Mean motion:   15
53893813  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1349
Checksum:              352


Coasting Arc #13 (Orbit 1363)
---------------------------------------

Vector Time (GMT): 2018/265/11:24:45
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -326510
90                 A    =         6787083
46  meter
 Y    =        6228615
97  meter          E    =           
0008133
 Z    =       -2668674
80                 I    =           51
28138
 XDOT =      -5093
511798                 Wp   =          152
88349
 YDOT =      -2475
554996  meter/sec      RA   =          252
94015  deg
 ZDOT =      -5168
037986                 TA   =           57
39317
                                          MA   =           57
31469
                                          Ha   =            221
908  n
mi
                                          Hp   =            215
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1071230
00                 X    =         -383173
77
 Y    =       20435091
77  feet           Y    =         6224647
60  meter
 Z    =       -8755494
74                 Z    =        -2670399
14
 XDOT =     -16710
996713                 XDOT =       -5040
347367
 YDOT =      -8121
899592  feet/sec       YDOT =       -2532
217454  meter/sec
 ZDOT =     -16955
505205                 ZDOT =       -5192
651037

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3992259
26                 X    =         1216840
62
 Y    =      -20066269
72  feet           Y    =        -6116199
01  meter
 Z    =       -8763896
58                 Z    =        -2671235
68
 XDOT =      13767
333295                 XDOT =        4196
283188
 YDOT =      10173
335567  feet/sec       YDOT =        3100
832681  meter/sec
 ZDOT =     -17065
642465                 ZDOT =       -5201
607823


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   18265
50233051  
00016717  00000-0  10270-3 0  9121
2 25544  51
6369 253
7501 0004405 184
2424 175
8692 15
53859376 13647


Satellite: ISS
Catalog Number: 25544
Epoch time:      18265
50233051   =   yrday
fracday
Element set:     912
Inclination:       51
6369  deg
RA of node:       253
7501  deg
Eccentricity:     
0004405     
Arg of perigee:   184
2424  deg
Mean anomaly:     175
8692  deg
Mean motion:   15
53859376  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1364
Checksum:              312


Coasting Arc #14 (Orbit 1379)
---------------------------------------

Vector Time (GMT): 2018/266/11:24:45
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1198004
34                 A    =         6783496
22  meter
 Y    =       -5404292
99  meter          E    =           
0011861
 Z    =        3917029
05                 I    =           51
27988
 XDOT =       5119
248440                 Wp   =          121
26638
 YDOT =       4057
047260  meter/sec      RA   =          247
93546  deg
 ZDOT =       4016
685191                 TA   =          286
49500
                                          MA   =          286
62529
                                          Ha   =            221
712  n
mi
                                          Hp   =            215
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3930460
43                 X    =         1239320
75
 Y    =      -17730620
06  feet           Y    =        -5390664
60  meter
 Z    =       12851145
16                 Z    =         3922949
52
 XDOT =      16795
434515                 XDOT =        5053
990009
 YDOT =      13310
522506  feet/sec       YDOT =        4113
929840  meter/sec
 ZDOT =      13178
101020                 ZDOT =        4041
393726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6104966
32                 X    =        -1860793
73
 Y    =       17083762
80  feet           Y    =         5207130
90  meter
 Z    =       12878267
50                 Z    =         3925295
93
 XDOT =     -13600
388225                 XDOT =       -4145
398331
 YDOT =     -14914
704015  feet/sec       YDOT =       -4546
001784  meter/sec
 ZDOT =      13288
512295                 ZDOT =        4050
338548


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   18266
53133184  
00016717  00000-0  10270-3 0  9132
2 25544  51
6364 248
6226 0004344 190
8020 169
3040 15
53888700 13802


Satellite: ISS
Catalog Number: 25544
Epoch time:      18266
53133184   =   yrday
fracday
Element set:     913
Inclination:       51
6364  deg
RA of node:       248
6226  deg
Eccentricity:     
0004344     
Arg of perigee:   190
8020  deg
Mean anomaly:     169
3040  deg
Mean motion:   15
53888700  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1380
Checksum:              298


Coasting Arc #15 (Orbit 1388)
---------------------------------------

Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4011669
30                 A    =         6778180
27  meter
 Y    =       -1410878
59  meter          E    =           
0004198
 Z    =        5276607
42                 I    =           51
27065
 XDOT =       2968
926894                 Wp   =          157
29574
 YDOT =       7062
219974  meter/sec      RA   =          244
96296  deg
 ZDOT =       -372
584620                 TA   =          296
25279
                                          MA   =          296
29592
                                          Ha   =            221
717  n
mi
                                          Hp   =            215
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13161644
69                 X    =         4001516
97
 Y    =       -4628866
77  feet           Y    =        -1366073
43  meter
 Z    =       17311704
14                 Z    =         5296070
26
 XDOT =       9740
573799                 XDOT =        2891
544354
 YDOT =      23170
013037  feet/sec       YDOT =        7094
987856  meter/sec
 ZDOT =      -1222
390485                 ZDOT =        -358
351410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9958867
94                 X    =         3035462
95
 Y    =       -9614609
06  feet           Y    =        -2930532
84  meter
 Z    =       17399156
33                 Z    =         5303262
85
 XDOT =      17766
852651                 XDOT =        5415
336688
 YDOT =      16327
028857  feet/sec       YDOT =        4976
478396  meter/sec
 ZDOT =      -1159
270810                 ZDOT =        -353
345743


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   18267
11014762  
00016717  00000-0  10270-3 0  9148
2 25544  51
6376 245
7337 0004650 190
7664 169
3389 15
53856166 13895


Satellite: ISS
Catalog Number: 25544
Epoch time:      18267
11014762   =   yrday
fracday
Element set:     914
Inclination:       51
6376  deg
RA of node:       245
7337  deg
Eccentricity:     
0004650     
Arg of perigee:   190
7664  deg
Mean anomaly:     169
3389  deg
Mean motion:   15
53856166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1389
Checksum:              337


Coasting Arc #16 (Orbit 1403)
---------------------------------------

Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4659171
14                 A    =         6779607
66  meter
 Y    =        -155990
60  meter          E    =           
0013366
 Z    =       -4934503
54                 I    =           51
29145
 XDOT =      -2067
508109                 Wp   =          126
84808
 YDOT =      -7046
589672  meter/sec      RA   =          239
94254  deg
 ZDOT =       2171
131557                 TA   =          164
47704
                                          MA   =          164
43601
                                          Ha   =            221
688  n
mi
                                          Hp   =            215
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15285994
54                 X    =        -4633111
18
 Y    =        -511780
19  feet           Y    =         -207947
61  meter
 Z    =      -16189316
08                 Z    =        -4957072
98
 XDOT =      -6783
163088                 XDOT =       -1999
103795
 YDOT =     -23118
732519  feet/sec       YDOT =       -7069
327231  meter/sec
 ZDOT =       7123
135029                 ZDOT =        2161
255317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13925799
60                 X    =        -4244583
72
 Y    =        6058686
93  feet           Y    =         1846687
77  meter
 Z    =      -16290547
00                 Z    =        -4965358
73
 XDOT =     -15659
555577                 XDOT =       -4773
032540
 YDOT =     -16924
759624  feet/sec       YDOT =       -5158
666733  meter/sec
 ZDOT =       7079
540917                 ZDOT =        2157
844071


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   18268
07483378  
00016717  00000-0  10270-3 0  9158
2 25544  51
6383 240
9271 0004738 195
2412 164
8598 15
53886754 14041


Satellite: ISS
Catalog Number: 25544
Epoch time:      18268
07483378   =   yrday
fracday
Element set:     915
Inclination:       51
6383  deg
RA of node:       240
9271  deg
Eccentricity:     
0004738     
Arg of perigee:   195
2412  deg
Mean anomaly:     164
8598  deg
Mean motion:   15
53886754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1404
Checksum:              343


Coasting Arc #17 (Orbit 1419)
---------------------------------------

Vector Time (GMT): 2018/269/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5145416
94                 A    =         6782826
19  meter
 Y    =        1603531
79  meter          E    =           
0008835
 Z    =        4109387
71                 I    =           51
32070
 XDOT =        954
463550                 Wp   =          103
01664
 YDOT =       6612
929831  meter/sec      RA   =          234
92846  deg
 ZDOT =      -3770
638860                 TA   =           26
02423
                                          MA   =           25
97984
                                          Ha   =            221
513  n
mi
                                          Hp   =            215
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16881289
17                 X    =         5107141
95
 Y    =        5260931
08  feet           Y    =         1660857
93  meter
 Z    =       13482243
15                 Z    =         4134289
44
 XDOT =       3131
442093                 XDOT =         898
760949
 YDOT =      21695
964012  feet/sec       YDOT =        6623
291376  meter/sec
 ZDOT =     -12370
862400                 ZDOT =       -3766
138490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17378161
03                 X    =         5296863
48
 Y    =       -2763032
63  feet           Y    =         -842172
35  meter
 Z    =       13593798
97                 Z    =         4143389
93
 XDOT =      12333
940048                 XDOT =        3759
384927
 YDOT =      16729
066449  feet/sec       YDOT =        5099
019454  meter/sec
 ZDOT =     -12351
327547                 ZDOT =       -3764
684636


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   18269
10383116  
00016717  00000-0  10270-3 0  9163
2 25544  51
6395 235
7986 0004712 198
1389 161
9596 15
53858312 14209


Satellite: ISS
Catalog Number: 25544
Epoch time:      18269
10383116   =   yrday
fracday
Element set:     916
Inclination:       51
6395  deg
RA of node:       235
7986  deg
Eccentricity:     
0004712     
Arg of perigee:   198
1389  deg
Mean anomaly:     161
9596  deg
Mean motion:   15
53858312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1420
Checksum:              336


Coasting Arc #18 (Orbit 1434)
---------------------------------------

Vector Time (GMT): 2018/270/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5433822
95                 A    =         6786417
92  meter
 Y    =       -2845234
07  meter          E    =           
0003354
 Z    =       -2909284
07                 I    =           51
35310
 XDOT =        354
933636                 Wp   =          134
97514
 YDOT =      -5791
787719  meter/sec      RA   =          229
92612  deg
 ZDOT =       5002
570231                 TA   =          191
74598
                                          MA   =          191
75381
                                          Ha   =            221
473  n
mi
                                          Hp   =            215
516

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17827503
11                 X    =        -5387470
93
 Y    =       -9334757
46  feet           Y    =        -2905740
02  meter
 Z    =       -9544895
25                 Z    =        -2935567
14
 XDOT =       1164
480434                 XDOT =         395
372452
 YDOT =     -19001
928212  feet/sec       YDOT =       -5787
591913  meter/sec
 ZDOT =      16412
631992                 ZDOT =        5004
393296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20067053
10                 X    =        -6116437
78
 Y    =        -106602
32  feet           Y    =          -32492
39  meter
 Z    =       -9662536
16                 Z    =        -2945141
02
 XDOT =      -7820
784970                 XDOT =       -2383
775259
 YDOT =     -15888
892953  feet/sec       YDOT =       -4842
934572  meter/sec
 ZDOT =      16421
376127                 ZDOT =        5005
235444


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   18270
06851218  
00016717  00000-0  10270-3 0  9174
2 25544  51
6399 230
9920 0004538 203
4208 156
6738 15
53865481 14354


Satellite: ISS
Catalog Number: 25544
Epoch time:      18270
06851218   =   yrday
fracday
Element set:     917
Inclination:       51
6399  deg
RA of node:       230
9920  deg
Eccentricity:     
0004538     
Arg of perigee:   203
4208  deg
Mean anomaly:     156
6738  deg
Mean motion:   15
53865481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1435
Checksum:              322
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