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

 
Date: December 11th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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


344/22:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 4

346/16:46:55 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 4

348/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 215 5

348/05:14:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

349/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

351/07:21:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 6

353/08:42:47 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 215 7

Coasting Arc #1 (Orbit 885)
---------------------------------------

Vector Time (GMT): 2017/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3786448
06                 A    =         6777339
71  meter
 Y    =       -1934218
67  meter          E    =           
0003237
 Z    =        5277316
11                 I    =           51
26823
 XDOT =       3084
769984                 Wp   =          169
11722
 YDOT =       7012
683062  meter/sec      RA   =          248
37871  deg
 ZDOT =        353
789888                 TA   =          277
47422
                                          MA   =          277
51099
                                          Ha   =            220
433  n
mi
                                          Hp   =            215
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12422729
86                 X    =         3782161
03
 Y    =       -6345861
79  feet           Y    =        -1891900
35  meter
 Z    =       17314029
24                 Z    =         5295698
93
 XDOT =      10120
636429                 XDOT =        3004
404480
 YDOT =      23007
490362  feet/sec       YDOT =        7046
729694  meter/sec
 ZDOT =       1160
727980                 ZDOT =         368
579995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3311186
70                 X    =         1009249
71
 Y    =       13445770
49  feet           Y    =         4098270
85  meter
 Z    =       17395892
80                 Z    =         5302268
12
 XDOT =     -23747
037536                 XDOT =       -7238
097041
 YDOT =       4249
387046  feet/sec       YDOT =        1295
213172  meter/sec
 ZDOT =       1225
292013                 ZDOT =         373
469006


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   17342
54887608  
00016717  00000-0  10270-3 0  9000
2 25544  51
6404 249
1090 0003068 217
9282 142
1654 15
54147000  8867


Satellite: ISS
Catalog Number: 25544
Epoch time:      17342
54887608   =   yrday
fracday
Element set:     900
Inclination:       51
6404  deg
RA of node:       249
1090  deg
Eccentricity:     
0003068     
Arg of perigee:   217
9282  deg
Mean anomaly:     142
1654  deg
Mean motion:   15
54147000  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             886
Checksum:              301


Coasting Arc #2 (Orbit 900)
---------------------------------------

Vector Time (GMT): 2017/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4459395
21                 A    =         6778162
09  meter
 Y    =         245794
83  meter          E    =           
0012477
 Z    =       -5109826
07                 I    =           51
28462
 XDOT =      -2192
451238                 Wp   =          113
68403
 YDOT =      -7169
410620  meter/sec      RA   =          243
35332  deg
 ZDOT =       1566
634890                 TA   =          171
52420
                                          MA   =          171
50310
                                          Ha   =            220
535  n
mi
                                          Hp   =            215
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14630561
72                 X    =        -4436991
31
 Y    =         806413
48  feet           Y    =          196052
35  meter
 Z    =      -16764521
22                 Z    =        -5131433
99
 XDOT =      -7193
081488                 XDOT =       -2119
727956
 YDOT =     -23521
688387  feet/sec       YDOT =       -7193
521566  meter/sec
 ZDOT =       5139
878249                 ZDOT =        1556
160924

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2343877
76                 X    =          714413
94
 Y    =      -14352156
62  feet           Y    =        -4374537
34  meter
 Z    =      -16860446
26                 Z    =        -5139064
02
 XDOT =      23479
500701                 XDOT =        7156
551814
 YDOT =      -2157
512233  feet/sec       YDOT =        -657
609729  meter/sec
 ZDOT =       5094
468648                 ZDOT =        1552
794044


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   17343
51341512  
00016717  00000-0  10270-3 0  9018
2 25544  51
6412 244
3004 0002894 220
8200 139
2736 15
54126308  9011


Satellite: ISS
Catalog Number: 25544
Epoch time:      17343
51341512   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       244
3004  deg
Eccentricity:     
0002894     
Arg of perigee:   220
8200  deg
Mean anomaly:     139
2736  deg
Mean motion:   15
54126308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             901
Checksum:              263


Coasting Arc #3 (Orbit 916)
---------------------------------------

Vector Time (GMT): 2017/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4976132
74                 A    =         6780972
11  meter
 Y    =        1362512
12  meter          E    =           
0006789
 Z    =        4395255
01                 I    =           51
30908
 XDOT =       1076
876326                 Wp   =           79
88950
 YDOT =       6825
948148  meter/sec      RA   =          238
33542  deg
 ZDOT =      -3329
645585                 TA   =           43
92578
                                          MA   =           43
87183
                                          Ha   =            220
291  n
mi
                                          Hp   =            215
355

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16325894
83                 X    =         4939176
90
 Y    =        4470184
12  feet           Y    =         1417951
83  meter
 Z    =       14420127
98                 Z    =         4419337
86
 XDOT =       3533
058813                 XDOT =        1016
640519
 YDOT =      22394
843004  feet/sec       YDOT =        6837
653849  meter/sec
 ZDOT =     -10924
034072                 ZDOT =       -3324
560475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7607780
53                 X    =        -2318851
51
 Y    =       15018356
78  feet           Y    =         4577595
15  meter
 Z    =       14526806
75                 Z    =         4427770
70
 XDOT =     -21568
481504                 XDOT =       -6574
073163
 YDOT =       -362
672394  feet/sec       YDOT =        -110
542546  meter/sec
 ZDOT =     -10902
470457                 ZDOT =       -3323
072995


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   17344
54225286  
00016717  00000-0  10270-3 0  9022
2 25544  51
6405 239
1725 0002836 225
3350 134
7572 15
54140223  9174


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
54225286   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:       239
1725  deg
Eccentricity:     
0002836     
Arg of perigee:   225
3350  deg
Mean anomaly:     134
7572  deg
Mean motion:   15
54140223  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             917
Checksum:              290


Coasting Arc #4 (Orbit 923)
---------------------------------------

Vector Time (GMT): 2017/344/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3259132
77                 A    =         6777320
95  meter
 Y    =       -2730227
74  meter          E    =           
0003362
 Z    =        5277857
69                 I    =           51
30510
 XDOT =       4527
429667                 Wp   =          175
81685
 YDOT =       6177
325377  meter/sec      RA   =          236
13840  deg
 ZDOT =        396
474745                 TA   =          270
36593
                                          MA   =          270
40446
                                          Ha   =            220
335  n
mi
                                          Hp   =            215
422

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10692692
82                 X    =         3263783
36
 Y    =       -8957440
08  feet           Y    =        -2693756
08  meter
 Z    =       17315806
06                 Z    =         5293700
78
 XDOT =      14853
771873                 XDOT =        4456
090783
 YDOT =      20266
815542  feet/sec       YDOT =        6227
555296  meter/sec
 ZDOT =       1300
770160                 ZDOT =         418
294628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2132647
38                 X    =         -650030
92
 Y    =      -13695522
03  feet           Y    =        -4174395
12  meter
 Z    =       17386519
01                 Z    =         5299410
99
 XDOT =      24034
525904                 XDOT =        7325
723495
 YDOT =      -1955
765427  feet/sec       YDOT =        -596
117302  meter/sec
 ZDOT =       1396
706154                 ZDOT =         425
716036


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   17344
99236677  
00016717  00000-0  10270-3 0  9038
2 25544  51
6409 236
9246 0003372 222
3896 137
6996 15
54158287  9248


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
99236677   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       236
9246  deg
Eccentricity:     
0003372     
Arg of perigee:   222
3896  deg
Mean anomaly:     137
6996  deg
Mean motion:   15
54158287  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             924
Checksum:              350


Coasting Arc #5 (Orbit 938)
---------------------------------------

Vector Time (GMT): 2017/345/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4281867
98                 A    =         6778057
00  meter
 Y    =        1220230
64  meter          E    =           
0012114
 Z    =       -5121380
12                 I    =           51
32658
 XDOT =      -3694
509600                 Wp   =          114
37458
 YDOT =      -6532
667066  meter/sec      RA   =          231
11668  deg
 ZDOT =       1530
368501                 TA   =          170
46500
                                          MA   =          170
44198
                                          Ha   =            220
360  n
mi
                                          Hp   =            215
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14048123
31                 X    =        -4270317
39
 Y    =        4003381
38  feet           Y    =         1172412
65  meter
 Z    =      -16802428
23                 Z    =        -5142152
14
 XDOT =     -12121
094489                 XDOT =       -3628
618804
 YDOT =     -21432
634730  feet/sec       YDOT =       -6573
613240  meter/sec
 ZDOT =       5020
894033                 ZDOT =        1512
581391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3604728
45                 X    =        -1098721
23
 Y    =       14045286
33  feet           Y    =         4281003
27  meter
 Z    =      -16894800
68                 Z    =        -5149535
25
 XDOT =     -23611
543096                 XDOT =       -7196
798336
 YDOT =       -106
201906  feet/sec       YDOT =         -32
370341  meter/sec
 ZDOT =       4942
890952                 ZDOT =        1506
593162


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   17345
95689852  
00016717  00000-0  10270-3 0  9043
2 25544  51
6409 232
1171 0003246 226
7446 133
3436 15
54146269  9397


Satellite: ISS
Catalog Number: 25544
Epoch time:      17345
95689852   =   yrday
fracday
Element set:     904
Inclination:       51
6409  deg
RA of node:       232
1171  deg
Eccentricity:     
0003246     
Arg of perigee:   226
7446  deg
Mean anomaly:     133
3436  deg
Mean motion:   15
54146269  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             939
Checksum:              324


Coasting Arc #6 (Orbit 950)
---------------------------------------

Vector Time (GMT): 2017/346/16:46:55
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3514758
97                 A    =         6788273
66  meter
 Y    =        5601089
77  meter          E    =           
0008798
 Z    =       -1512731
36                 I    =           51
37354
 XDOT =      -4855
601298                 Wp   =          161
76967
 YDOT =       1500
727162  meter/sec      RA   =          227
35856  deg
 ZDOT =      -5742
374819                 TA   =           34
81632
                                          MA   =           34
75879
                                          Ha   =            220
278  n
mi
                                          Hp   =            215
430

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11531361
44                 X    =         3459213
02
 Y    =       18376278
76  feet           Y    =         5640083
70  meter
 Z    =       -4963029
39                 Z    =        -1495792
27
 XDOT =     -15930
450454                 XDOT =       -4844
128090
 YDOT =       4923
645545  feet/sec       YDOT =        1446
492915  meter/sec
 ZDOT =     -18839
812397                 ZDOT =       -5765
934082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1747222
08                 X    =          532553
29
 Y    =       21641163
15  feet           Y    =         6596226
53  meter
 Z    =       -4888645
09                 Z    =        -1490059
02
 XDOT =     -14711
518552                 XDOT =       -4484
070855
 YDOT =      -3078
767052  feet/sec       YDOT =        -938
408197  meter/sec
 ZDOT =     -18944
601650                 ZDOT =       -5774
314583


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   17346
72852110  
00016717  00000-0  10270-3 0  9059
2 25544  51
6377 228
2689 0002873 232
4909 127
5983 15
54167178  9512


Satellite: ISS
Catalog Number: 25544
Epoch time:      17346
72852110   =   yrday
fracday
Element set:     905
Inclination:       51
6377  deg
RA of node:       228
2689  deg
Eccentricity:     
0002873     
Arg of perigee:   232
4909  deg
Mean anomaly:     127
5983  deg
Mean motion:   15
54167178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             951
Checksum:              335


Coasting Arc #7 (Orbit 966)
---------------------------------------

Vector Time (GMT): 2017/347/16:46:55
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2462892
18                 A    =         6785387
21  meter
 Y    =       -5536833
98  meter          E    =           
0010604
 Z    =        3044156
03                 I    =           51
38540
 XDOT =       5897
416645                 Wp   =           92
77209
 YDOT =         79
980042  meter/sec      RA   =          222
36473  deg
 ZDOT =       4901
504776                 TA   =          302
29223
                                          MA   =          302
39491
                                          Ha   =            220
301  n
mi
                                          Hp   =            215
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8080354
91                 X    =        -2415581
92
 Y    =      -18165465
82  feet           Y    =        -5564111
37  meter
 Z    =        9987388
56                 Z    =         3032306
55
 XDOT =      19348
479805                 XDOT =        5872
274640
 YDOT =        262
401714  feet/sec       YDOT =         145
788134  meter/sec
 ZDOT =      16081
052414                 ZDOT =        4930
091817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         842896
93                 X    =          256914
99
 Y    =      -19889647
43  feet           Y    =        -6062364
54  meter
 Z    =        9935575
68                 Z    =         3028363
47
 XDOT =      15640
117353                 XDOT =        4767
107769
 YDOT =       8784
458191  feet/sec       YDOT =        2677
502857  meter/sec
 ZDOT =      16207
944101                 ZDOT =        4940
181362


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   17347
75734962  
00016717  00000-0  10270-3 0  9068
2 25544  51
6365 223
1398 0003095 231
7953 128
2922 15
54147604  9678


Satellite: ISS
Catalog Number: 25544
Epoch time:      17347
75734962   =   yrday
fracday
Element set:     906
Inclination:       51
6365  deg
RA of node:       223
1398  deg
Eccentricity:     
0003095     
Arg of perigee:   231
7953  deg
Mean anomaly:     128
2922  deg
Mean motion:   15
54147604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             967
Checksum:              330


Coasting Arc #8 (Orbit 971)
---------------------------------------

Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919742
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2652020
88                 A    =         6777379
43  meter
 Y    =        3304934
67  meter          E    =           
0012485
 Z    =       -5300076
44                 I    =           51
37108
 XDOT =      -5881
656118                 Wp   =           96
51759
 YDOT =      -4905
138556  meter/sec      RA   =          220
52825  deg
 ZDOT =       -117
265376                 TA   =          172
36899
                                          MA   =          172
34997
                                          Ha   =            220
249  n
mi
                                          Hp   =            215
451

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8700855
90                 X    =        -2663035
01
 Y    =       10842961
52  feet           Y    =         3275216
70  meter
 Z    =      -17388702
22                 Z    =        -5312985
81
 XDOT =     -19296
772041                 XDOT =       -5825
798781
 YDOT =     -16092
974264  feet/sec       YDOT =       -4970
598931  meter/sec
 ZDOT =       -384
728923                 ZDOT =        -145
701559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12650713
76                 X    =         3855937
55
 Y    =        5587610
88  feet           Y    =         1703103
80  meter
 Z    =      -17446481
56                 Z    =        -5317687
58
 XDOT =     -10322
956377                 XDOT =       -3146
437104
 YDOT =      21795
222921  feet/sec       YDOT =        6643
183946  meter/sec
 ZDOT =       -510
269667                 ZDOT =        -155
530194


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   17348
07885818  
00016717  00000-0  10270-3 0  9072
2 25544  51
6403 221
5407 0002953 236
0572 124
0300 15
54123068  9729


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
07885818   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:       221
5407  deg
Eccentricity:     
0002953     
Arg of perigee:   236
0572  deg
Mean anomaly:     124
0300  deg
Mean motion:   15
54123068  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             972
Checksum:              295


Coasting Arc #9 (Orbit 974)
---------------------------------------

Vector Time (GMT): 2017/348/05:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904510
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -92262
32                 A    =         6780023
84  meter
 Y    =       -4921147
60  meter          E    =           
0006907
 Z    =        4661162
92                 I    =           51
38098
 XDOT =       6641
507924                 Wp   =          137
02205
 YDOT =       2574
120992  meter/sec      RA   =          219
76953  deg
 ZDOT =       2841
705281                 TA   =          284
62792
                                          MA   =          284
70450
                                          Ha   =            220
123  n
mi
                                          Hp   =            215
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -302697
90                 X    =          -59867
74
 Y    =      -16145497
38  feet           Y    =        -4921998
51  meter
 Z    =       15292529
28                 Z    =         4660793
11
 XDOT =      21789
724160                 XDOT =        6598
426051
 YDOT =       8445
278845  feet/sec       YDOT =        2648
149807  meter/sec
 ZDOT =       9323
180055                 ZDOT =        2873
863522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4921154
97                 X    =        -1499968
03
 Y    =       15381149
87  feet           Y    =         4688174
48  meter
 Z    =       15291586
77                 Z    =         4660875
65
 XDOT =     -16627
256429                 XDOT =       -5067
987760
 YDOT =     -14754
615260  feet/sec       YDOT =       -4497
206731  meter/sec
 ZDOT =       9465
578546                 ZDOT =        2885
108341


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   17348
27176228  
00016717  00000-0  10270-3 0  9083
2 25544  51
6372 220
5798 0002996 240
4679 119
6175 15
54158890  9754


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
27176228   =   yrday
fracday
Element set:     908
Inclination:       51
6372  deg
RA of node:       220
5798  deg
Eccentricity:     
0002996     
Arg of perigee:   240
4679  deg
Mean anomaly:     119
6175  deg
Mean motion:   15
54158890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             975
Checksum:              351


Coasting Arc #10 (Orbit 989)
---------------------------------------

Vector Time (GMT): 2017/349/05:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904510
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1447879
72                 A    =         6777695
03  meter
 Y    =        4075610
00  meter          E    =           
0011638
 Z    =       -5228434
97                 I    =           51
39934
 XDOT =      -6660
342377                 Wp   =           86
70889
 YDOT =      -3648
638611  meter/sec      RA   =          214
75482  deg
 ZDOT =      -1001
012368                 TA   =          173
67248
                                          MA   =          173
65777
                                          Ha   =            220
131  n
mi
                                          Hp   =            215
517

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4750261
53                 X    =        -1467949
25
 Y    =       13371423
89  feet           Y    =         4059307
03  meter
 Z    =      -17153658
04                 Z    =        -5235516
81
 XDOT =     -21851
516984                 XDOT =       -6614
184834
 YDOT =     -11970
599117  feet/sec       YDOT =       -3722
860949  meter/sec
 ZDOT =      -3284
161313                 ZDOT =       -1033
254754

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8578728
64                 X    =         2614796
49
 Y    =      -11254592
53  feet           Y    =        -3430399
80  meter
 Z    =      -17185677
40                 Z    =        -5238194
47
 XDOT =      16181
781852                 XDOT =        4932
207108
 YDOT =      17560
755903  feet/sec       YDOT =        5352
518399  meter/sec
 ZDOT =      -3426
800180                 ZDOT =       -1044
488695


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   17349
23628551  
00016717  00000-0  10270-3 0  9092
2 25544  51
6377 215
7709 0002844 243
9611 116
1249 15
54135970  9908


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
23628551   =   yrday
fracday
Element set:     909
Inclination:       51
6377  deg
RA of node:       215
7709  deg
Eccentricity:     
0002844     
Arg of perigee:   243
9611  deg
Mean anomaly:     116
1249  deg
Mean motion:   15
54135970  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             990
Checksum:              324


Coasting Arc #11 (Orbit 993)
---------------------------------------

Vector Time (GMT): 2017/349/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6080650
34                 A    =         6788367
52  meter
 Y    =        2608138
15  meter          E    =           
0012360
 Z    =        1487106
11                 I    =           51
44496
 XDOT =       -737
417787                 Wp   =          129
10756
 YDOT =       5015
516220  meter/sec      RA   =          213
53508  deg
 ZDOT =      -5756
617707                 TA   =           34
60725
                                          MA   =           34
52688
                                          Ha   =            220
092  n
mi
                                          Hp   =            215
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19949640
24                 X    =         6043809
81
 Y    =        8556883
69  feet           Y    =         2675930
03  meter
 Z    =        4878957
04                 Z    =         1516555
05
 XDOT =      -2419
349695                 XDOT =        -765
484734
 YDOT =      16455
105709  feet/sec       YDOT =        5007
113463  meter/sec
 ZDOT =     -18886
541033                 ZDOT =       -5760
267638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15281866
83                 X    =        -4657913
01
 Y    =       15374772
78  feet           Y    =         4686230
74  meter
 Z    =        5009344
66                 Z    =         1526848
25
 XDOT =     -13335
512413                 XDOT =       -4064
664184
 YDOT =      -7070
345417  feet/sec       YDOT =       -2155
041283  meter/sec
 ZDOT =     -18903
455358                 ZDOT =       -5761
773193


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   17349
49349168  
00016717  00000-0  10270-3 0  9106
2 25544  51
6412 214
4911 0002913 245
0312 115
0538 15
54120181  9948


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
49349168   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       214
4911  deg
Eccentricity:     
0002913     
Arg of perigee:   245
0312  deg
Mean anomaly:     115
0538  deg
Mean motion:   15
54120181  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             994
Checksum:              288


Coasting Arc #12 (Orbit 1009)
---------------------------------------

Vector Time (GMT): 2017/350/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5874930
66                 A    =         6789202
98  meter
 Y    =       -3385750
19  meter          E    =           
0009833
 Z    =         208637
91                 I    =           51
47538
 XDOT =       2549
783311                 Wp   =           40
04898
 YDOT =      -4045
724978  meter/sec      RA   =          208
55136  deg
 ZDOT =       5994
416140                 TA   =          322
20397
                                          MA   =          322
27298
                                          Ha   =            219
933  n
mi
                                          Hp   =            215
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19274706
89                 X    =        -5837647
12
 Y    =      -11108104
30  feet           Y    =        -3451239
24  meter
 Z    =         684507
59                 Z    =          180189
31
 XDOT =       8365
430810                 XDOT =        2565
716021
 YDOT =     -13273
375913  feet/sec       YDOT =       -4017
123068  meter/sec
 ZDOT =      19666
719620                 ZDOT =        6006
840596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17178455
53                 X    =         5235993
24
 Y    =      -14140771
93  feet           Y    =        -4310107
28  meter
 Z    =         558652
31                 Z    =          170277
22
 XDOT =       8496
326929                 XDOT =        2589
680448
 YDOT =      11124
494324  feet/sec       YDOT =        3390
745870  meter/sec
 ZDOT =      19722
461893                 ZDOT =        6011
406385


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   17350
52230896  
00016717  00000-0  10270-3 0  9110
2 25544  51
6406 209
3616 0002969 252
9983 107
0844 15
54168061 10108


Satellite: ISS
Catalog Number: 25544
Epoch time:      17350
52230896   =   yrday
fracday
Element set:     911
Inclination:       51
6406  deg
RA of node:       209
3616  deg
Eccentricity:     
0002969     
Arg of perigee:   252
9983  deg
Mean anomaly:     107
0844  deg
Mean motion:   15
54168061  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1010
Checksum:              302


Coasting Arc #13 (Orbit 1022)
---------------------------------------

Vector Time (GMT): 2017/351/07:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -534624
44                 A    =         6778722
57  meter
 Y    =       -4582451
17  meter          E    =           
0004833
 Z    =        4965834
57                 I    =           51
46297
 XDOT =       7234
748117                 Wp   =          150
59845
 YDOT =       1436
137103  meter/sec      RA   =          204
32920  deg
 ZDOT =       2099
160482                 TA   =          278
89037
                                          MA   =          278
94509
                                          Ha   =            219
913  n
mi
                                          Hp   =            215
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1754017
19                 X    =         -507464
23
 Y    =      -15034288
63  feet           Y    =        -4588278
39  meter
 Z    =       16292108
17                 Z    =         4963302
98
 XDOT =      23736
050253                 XDOT =        7207
954393
 YDOT =       4711
735902  feet/sec       YDOT =        1516
890959  meter/sec
 ZDOT =       6887
009455                 ZDOT =        2134
239939

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5809749
33                 X    =         1770811
60
 Y    =       13989229
06  feet           Y    =         4263917
02  meter
 Z    =       16281507
38                 Z    =         4962603
45
 XDOT =     -23067
973363                 XDOT =       -7031
118281
 YDOT =       1364
463160  feet/sec       YDOT =         415
888371  meter/sec
 ZDOT =       7042
604709                 ZDOT =        2146
585915


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   17351
35822377  
00016717  00000-0  10270-3 0  9124
2 25544  51
6384 205
1942 0002982 254
5994 105
4829 15
54181910 10231


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
35822377   =   yrday
fracday
Element set:     912
Inclination:       51
6384  deg
RA of node:       205
1942  deg
Eccentricity:     
0002982     
Arg of perigee:   254
5994  deg
Mean anomaly:     105
4829  deg
Mean motion:   15
54181910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1023
Checksum:              309


Coasting Arc #14 (Orbit 1037)
---------------------------------------

Vector Time (GMT): 2017/352/07:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1198639
27                 A    =         6777263
19  meter
 Y    =        4054792
73  meter          E    =           
0012014
 Z    =       -5306934
08                 I    =           51
48882
 XDOT =      -7274
053731                 Wp   =           90
64087
 YDOT =      -2393
096283  meter/sec      RA   =          199
31834  deg
 ZDOT =       -186
016801                 TA   =          177
58356
                                          MA   =          177
57775
                                          Ha   =            219
915  n
mi
                                          Hp   =            215
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3932543
54                 X    =        -1218113
41
 Y    =       13303125
76  feet           Y    =         4041280
46  meter
 Z    =      -17411201
05                 Z    =        -5312803
54
 XDOT =     -23865
005680                 XDOT =       -7245
849283
 YDOT =      -7851
365757  feet/sec       YDOT =       -2474
282001  meter/sec
 ZDOT =       -610
291343                 ZDOT =        -221
283776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -112630
97                 X    =          -34329
92
 Y    =      -13838246
03  feet           Y    =        -4217897
39  meter
 Z    =      -17437839
22                 Z    =        -5315053
39
 XDOT =      24098
471415                 XDOT =        7345
214087
 YDOT =        767
830921  feet/sec       YDOT =         234
034865  meter/sec
 ZDOT =       -766
611057                 ZDOT =        -233
663050


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   17352
32273907  
00016717  00000-0  10270-3 0  9132
2 25544  51
6390 200
3854 0002872 259
8310 100
2519 15
54166528 10388


Satellite: ISS
Catalog Number: 25544
Epoch time:      17352
32273907   =   yrday
fracday
Element set:     913
Inclination:       51
6390  deg
RA of node:       200
3854  deg
Eccentricity:     
0002872     
Arg of perigee:   259
8310  deg
Mean anomaly:     100
2519  deg
Mean motion:   15
54166528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1038
Checksum:              294


Coasting Arc #15 (Orbit 1053)
---------------------------------------

Vector Time (GMT): 2017/353/07:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925679
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2911288
90                 A    =         6778143
24  meter
 Y    =       -3420583
72  meter          E    =           
0003063
 Z    =        5075687
90                 I    =           51
52319
 XDOT =       6765
592258                 Wp   =           26
38143
 YDOT =       3159
659027  meter/sec      RA   =          194
31005  deg
 ZDOT =      -1748
139707                 TA   =           80
56429
                                          MA   =           80
52967
                                          Ha   =            219
749  n
mi
                                          Hp   =            215
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9551472
77                 X    =         2924667
23
 Y    =      -11222387
54  feet           Y    =        -3387953
49  meter
 Z    =       16652519
36                 Z    =         5089862
13
 XDOT =      22196
824995                 XDOT =        6738
248869
 YDOT =      10366
335390  feet/sec       YDOT =        3235
163822  meter/sec
 ZDOT =      -5735
366493                 ZDOT =       -1715
340618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5638355
14                 X    =        -1718570
65
 Y    =       13537519
65  feet           Y    =         4126235
99  meter
 Z    =       16715966
27                 Z    =         5095026
52
 XDOT =     -23333
060875                 XDOT =       -7111
916955
 YDOT =      -2803
119418  feet/sec       YDOT =        -854
390799  meter/sec
 ZDOT =      -5590
090522                 ZDOT =       -1703
859591


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   17353
35154969  
00016717  00000-0  10270-3 0  9143
2 25544  51
6388 195
2570 0002921 266
0165  94
0654 15
54186098 10547


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
35154969   =   yrday
fracday
Element set:     914
Inclination:       51
6388  deg
RA of node:       195
2570  deg
Eccentricity:     
0002921     
Arg of perigee:   266
0165  deg
Mean anomaly:      94
0654  deg
Mean motion:   15
54186098  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1054
Checksum:              324


Coasting Arc #16 (Orbit 1054)
---------------------------------------

Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1866184
54                 A    =         6779495
94  meter
 Y    =       -4402599
77  meter          E    =           
0005316
 Z    =        4804270
34                 I    =           51
53038
 XDOT =       7227
990829                 Wp   =          136
98207
 YDOT =       -277
098745  meter/sec      RA   =          194
06016  deg
 ZDOT =       2548
256720                 TA   =          287
87631
                                          MA   =          287
93428
                                          Ha   =            219
964  n
mi
                                          Hp   =            215
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6122652
70                 X    =        -1840151
56
 Y    =      -14444224
98  feet           Y    =        -4423323
73  meter
 Z    =       15762041
79                 Z    =         4795267
71
 XDOT =      23713
880672                 XDOT =        7218
174054
 YDOT =       -909
116619  feet/sec       YDOT =        -196
325599  meter/sec
 ZDOT =       8360
422310                 ZDOT =        2583
344157

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13794114
80                 X    =         4204446
19
 Y    =        7555455
07  feet           Y    =         2302902
71  meter
 Z    =       15722657
81                 Z    =         4792266
10
 XDOT =     -17541
205866                 XDOT =       -5346
559548
 YDOT =      14265
560712  feet/sec       YDOT =        4348
142905  meter/sec
 ZDOT =       8516
343820                 ZDOT =        2595
781596


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   17353
41585080  
00016717  00000-0  10270-3 0  9153
2 25544  51
6402 194
9362 0002843 264
5025  95
5803 15
54158556 10551


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
41585080   =   yrday
fracday
Element set:     915
Inclination:       51
6402  deg
RA of node:       194
9362  deg
Eccentricity:     
0002843     
Arg of perigee:   264
5025  deg
Mean anomaly:      95
5803  deg
Mean motion:   15
54158556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1055
Checksum:              308


Coasting Arc #17 (Orbit 1069)
---------------------------------------

Vector Time (GMT): 2017/354/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          84569
88                 A    =         6777355
39  meter
 Y    =        4259119
54  meter          E    =           
0011694
 Z    =       -5281362
03                 I    =           51
55495
 XDOT =      -7601
014481                 Wp   =           83
60274
 YDOT =       -675
627097  meter/sec      RA   =          189
05581  deg
 ZDOT =       -666
565575                 TA   =          180
01818
                                          MA   =          180
01822
                                          Ha   =            219
831  n
mi
                                          Hp   =            215
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         277460
23                 X    =           62591
13
 Y    =       13973489
31  feet           Y    =         4259942
96  meter
 Z    =      -17327303
25                 Z    =        -5281004
12
 XDOT =     -24937
711551                 XDOT =       -7589
656680
 YDOT =      -2216
624334  feet/sec       YDOT =        -760
563256  meter/sec
 ZDOT =      -2186
894931                 ZDOT =        -703
461288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9088607
43                 X    =        -2770207
54
 Y    =      -10619194
78  feet           Y    =        -3236730
57  meter
 Z    =      -17326302
05                 Z    =        -5281056
86
 XDOT =      20000
521716                 XDOT =        6096
159019
 YDOT =     -13282
265906  feet/sec       YDOT =       -4048
434648  meter/sec
 ZDOT =      -2350
744757                 ZDOT =        -716
507002


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   17354
38035841  
00016717  00000-0  10270-3 0  9166
2 25544  51
6395 190
1282 0002932 269
8200  90
2617 15
54186952 10706


Satellite: ISS
Catalog Number: 25544
Epoch time:      17354
38035841   =   yrday
fracday
Element set:     916
Inclination:       51
6395  deg
RA of node:       190
1282  deg
Eccentricity:     
0002932     
Arg of perigee:   269
8200  deg
Mean anomaly:      90
2617  deg
Mean motion:   15
54186952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1070
Checksum:              306


Coasting Arc #18 (Orbit 1085)
---------------------------------------

Vector Time (GMT): 2017/355/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1737640
65                 A    =         6777622
96  meter
 Y    =       -4000653
97  meter          E    =           
0002480
 Z    =        5187837
09                 I    =           51
58923
 XDOT =       7400
690531                 Wp   =            7
03660
 YDOT =       1545
307047  meter/sec      RA   =          184
05113  deg
 ZDOT =      -1284
671603                 TA   =           95
32218
                                          MA   =           95
29389
                                          Ha   =            219
675  n
mi
                                          Hp   =            215
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5700920
75                 X    =         1757048
10
 Y    =      -13125505
14  feet           Y    =        -3981114
51  meter
 Z    =       17020462
89                 Z    =         5196324
67
 XDOT =      24280
480746                 XDOT =        7389
100721
 YDOT =       5069
905010  feet/sec       YDOT =        1628
001959  meter/sec
 ZDOT =      -4214
801847                 ZDOT =       -1248
749574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4140369
19                 X    =         1261984
53
 Y    =       13650366
23  feet           Y    =         4160631
63  meter
 Z    =       17058733
37                 Z    =         5199501
93
 XDOT =     -20896
339323                 XDOT =       -6369
204226
 YDOT =      11416
267213  feet/sec       YDOT =        3479
678246  meter/sec
 ZDOT =      -4055
372308                 ZDOT =       -1236
077479


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   17355
40916398  
00016717  00000-0  10270-3 0  9176
2 25544  51
6401 184
9994 0003114 272
9345  87
1451 15
54208120 10863


Satellite: ISS
Catalog Number: 25544
Epoch time:      17355
40916398   =   yrday
fracday
Element set:     917
Inclination:       51
6401  deg
RA of node:       184
9994  deg
Eccentricity:     
0003114     
Arg of perigee:   272
9345  deg
Mean anomaly:      87
1451  deg
Mean motion:   15
54208120  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1086
Checksum:              313


Coasting Arc #19 (Orbit 1100)
---------------------------------------

Vector Time (GMT): 2017/356/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3439789
22                 A    =         6780274
10  meter
 Y    =        3665448
59  meter          E    =           
0007025
 Z    =       -4557279
19                 I    =           51
63095
 XDOT =      -6603
364756                 Wp   =          115
75932
 YDOT =      -2344
659282  meter/sec      RA   =          179
05220  deg
 ZDOT =       3099
069942                 TA   =          185
29397
                                          MA   =          185
30140
                                          Ha   =            219
779  n
mi
                                          Hp   =            215
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11285397
70                 X    =        -3458384
77
 Y    =       12025749
96  feet           Y    =         3626878
95  meter
 Z    =      -14951703
37                 Z    =        -4574033
31
 XDOT =     -21664
582533                 XDOT =       -6591
709002
 YDOT =      -7692
451712  feet/sec       YDOT =       -2418
437732  meter/sec
 ZDOT =      10167
552303                 ZDOT =        3067
021215

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         575359
73                 X    =          175369
65
 Y    =      -16413419
00  feet           Y    =        -5002810
11  meter
 Z    =      -15026674
11                 Z    =        -4580130
27
 XDOT =      20260
847012                 XDOT =        6175
506169
 YDOT =      -8465
950393  feet/sec       YDOT =       -2580
421680  meter/sec
 ZDOT =      10025
422951                 ZDOT =        3055
748916


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   17356
37366784  
00016717  00000-0  10270-3 0  9182
2 25544  51
6403 180
1904 0003109 278
4730  81
6070 15
54186979 11018


Satellite: ISS
Catalog Number: 25544
Epoch time:      17356
37366784   =   yrday
fracday
Element set:     918
Inclination:       51
6403  deg
RA of node:       180
1904  deg
Eccentricity:     
0003109     
Arg of perigee:   278
4730  deg
Mean anomaly:      81
6070  deg
Mean motion:   15
54186979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1101
Checksum:              314


Coasting Arc #20 (Orbit 1116)
---------------------------------------

Vector Time (GMT): 2017/357/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 940911
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4878373
17                 A    =         6784014
14  meter
 Y    =       -3230146
78  meter          E    =           
0009403
 Z    =        3426564
96                 I    =           51
67622
 XDOT =       5294
249496                 Wp   =           84
44634
 YDOT =       3104
497137  meter/sec      RA   =          174
06544  deg
 ZDOT =      -4599
093126                 TA   =           55
45017
                                          MA   =           55
36146
                                          Ha   =            219
757  n
mi
                                          Hp   =            215
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16005161
30                 X    =         4897486
55
 Y    =      -10597594
41  feet           Y    =        -3175486
86  meter
 Z    =       11242011
03                 Z    =         3450308
54
 XDOT =      17369
584962                 XDOT =        5281
480625
 YDOT =      10185
358062  feet/sec       YDOT =        3163
630010  meter/sec
 ZDOT =     -15088
888210                 ZDOT =       -4573
406319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4777159
44                 X    =        -1456078
20
 Y    =       18527239
46  feet           Y    =         5647102
59  meter
 Z    =       11348002
18                 Z    =         3458871
06
 XDOT =     -18451
456711                 XDOT =       -5624
004005
 YDOT =       4438
083628  feet/sec       YDOT =        1352
727890  meter/sec
 ZDOT =     -14975
122351                 ZDOT =       -4564
417293


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   17357
40246806  
00016717  00000-0  10270-3 0  9190
2 25544  51
6400 175
0614 0003071 285
3239  74
7575 15
54211551 11170


Satellite: ISS
Catalog Number: 25544
Epoch time:      17357
40246806   =   yrday
fracday
Element set:     919
Inclination:       51
6400  deg
RA of node:       175
0614  deg
Eccentricity:     
0003071     
Arg of perigee:   285
3239  deg
Mean anomaly:      74
7575  deg
Mean motion:   15
54211551  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1117
Checksum:              294
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