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

 
Date: December 15th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


349/15:36:09 000 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

351/06:36:00 000 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

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

351/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 215 8

353/08:43:02 000 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

361/06:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 5

362/01:04:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 5

364/11:45:00 000 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

Coasting Arc #1 (Orbit 996)
---------------------------------------

Vector Time (GMT): 2017/349/15:34:47
651
Vector Time (MET): N/A
Weight (LBS)     : 903628
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6115030
18                 A    =         6786486
99  meter
 Y    =        1562196
23  meter          E    =           
0011377
 Z    =        2477806
73                 I    =           51
44016
 XDOT =        750
470511                 Wp   =          114
35327
 YDOT =       5493
380197  meter/sec      RA   =          212
56789  deg
 ZDOT =      -5300
924258                 TA   =           37
78516
                                          MA   =           37
70534
                                          Ha   =            219
877  n
mi
                                          Hp   =            215
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20062434
99                 X    =         6085070
72
 Y    =        5125315
70  feet           Y    =         1630410
94  meter
 Z    =        8129287
19                 Z    =         2507439
31
 XDOT =       2462
173592                 XDOT =         714
735815
 YDOT =      18022
900908  feet/sec       YDOT =        5501
573128  meter/sec
 ZDOT =     -17391
483786                 ZDOT =       -5297
364986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11231581
96                 X    =         3423386
18
 Y    =       17334037
03  feet           Y    =         5283414
49  meter
 Z    =        8260641
36                 Z    =         2517843
49
 XDOT =      -9061
013626                 XDOT =       -2761
796953
 YDOT =      14174
428541  feet/sec       YDOT =        4320
365819  meter/sec
 ZDOT =     -17376
455091                 ZDOT =       -5296
343512


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
68638641  
00016717  00000-0  10270-3 0  9003
2 25544  51
6369 213
5241 0003111 247
0362 113
0463 15
54181843  9973


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
68638641   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       213
5241  deg
Eccentricity:     
0003111     
Arg of perigee:   247
0362  deg
Mean anomaly:     113
0463  deg
Mean motion:   15
54181843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             997
Checksum:              300


Coasting Arc #2 (Orbit 996)
---------------------------------------

Vector Time (GMT): 2017/349/15:36:09
000
Vector Time (MET): N/A
Weight (LBS)     : 903628
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6150126
74                 A    =         6787324
58  meter
 Y    =        2001838
21  meter          E    =           
0011853
 Z    =        2036680
10                 I    =           51
44307
 XDOT =        111
772405                 Wp   =          121
35905
 YDOT =       5307
774834  meter/sec      RA   =          212
56614  deg
 ZDOT =      -5536
692422                 TA   =           36
05331
                                          MA   =           35
97343
                                          Ha   =            219
877  n
mi
                                          Hp   =            215
579

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20177581
18                 X    =         6117391
27
 Y    =        6567710
68  feet           Y    =         2070429
92  meter
 Z    =        6682021
34                 Z    =         2066476
47
 XDOT =        366
707364                 XDOT =          79
305924
 YDOT =      17413
959428  feet/sec       YDOT =        5308
843701  meter/sec
 ZDOT =     -18165
001386                 ZDOT =       -5536
227856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10454760
06                 X    =         3186610
86
 Y    =       18416999
10  feet           Y    =         5613501
33  meter
 Z    =        6814040
73                 Z    =         2076919
61
 XDOT =     -10027
526913                 XDOT =       -3056
390203
 YDOT =      12433
821688  feet/sec       YDOT =        3789
828851  meter/sec
 ZDOT =     -18163
687607                 ZDOT =       -5536
291983


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
68638625  
00016717  00000-0  10270-3 0  9016
2 25544  51
6369 213
5241 0003099 247
6416 112
4408 15
54189543  9971


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
68638625   =   yrday
fracday
Element set:     901
Inclination:       51
6369  deg
RA of node:       213
5241  deg
Eccentricity:     
0003099     
Arg of perigee:   247
6416  deg
Mean anomaly:     112
4408  deg
Mean motion:   15
54189543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             997
Checksum:              331


Coasting Arc #3 (Orbit 1011)
---------------------------------------

Vector Time (GMT): 2017/350/15:36:09
000
Vector Time (MET): N/A
Weight (LBS)     : 903628
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6135022
39                 A    =         6789135
47  meter
 Y    =       -2873318
05  meter          E    =           
0008625
 Z    =        -369083
78                 I    =           51
47658
 XDOT =       1737
012814                 Wp   =           35
14912
 YDOT =      -4467
674603  meter/sec      RA   =          207
58173  deg
 ZDOT =       5984
384976                 TA   =          320
86365
                                          MA   =          320
92600
                                          Ha   =            220
040  n
mi
                                          Hp   =            215
570

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20128026
21                 X    =        -6100643
36
 Y    =       -9426896
49  feet           Y    =        -2941731
80  meter
 Z    =       -1210904
78                 Z    =         -398802
84
 XDOT =       5698
860938                 XDOT =        1757
773025
 YDOT =     -14657
725076  feet/sec       YDOT =       -4448
134670  meter/sec
 ZDOT =      19633
808977                 ZDOT =        5992
872881

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8870685
80                 X    =        -2703785
03
 Y    =      -20371028
29  feet           Y    =        -6209089
42  meter
 Z    =       -1342477
81                 Z    =         -409187
24
 XDOT =      12379
895783                 XDOT =        3773
392235
 YDOT =      -6672
364479  feet/sec       YDOT =       -2033
736693  meter/sec
 ZDOT =      19672
130180                 ZDOT =        5996
065279


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
65089537  
00016717  00000-0  10270-3 0  9028
2 25544  51
6365 208
7155 0002916 244
7749 115
3102 15
54169779 10122


Satellite: ISS
Catalog Number: 25544
Epoch time:      17350
65089537   =   yrday
fracday
Element set:     902
Inclination:       51
6365  deg
RA of node:       208
7155  deg
Eccentricity:     
0002916     
Arg of perigee:   244
7749  deg
Mean anomaly:     115
3102  deg
Mean motion:   15
54169779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1012
Checksum:              314


Coasting Arc #4 (Orbit 1021)
---------------------------------------

Vector Time (GMT): 2017/351/06:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 903628
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -62796
08                 A    =         6778101
45  meter
 Y    =        4452567
82  meter          E    =           
0010690
 Z    =       -5119708
87                 I    =           51
45937
 XDOT =      -7246
549061                 Wp   =           78
49871
 YDOT =      -1917
166906  meter/sec      RA   =          204
47996  deg
 ZDOT =      -1579
176526                 TA   =          176
22392
                                          MA   =          176
21584
                                          Ha   =            219
949  n
mi
                                          Hp   =            215
574

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -206023
87                 X    =          -87712
04
 Y    =       14608162
15  feet           Y    =         4451726
84  meter
 Z    =      -16796945
11                 Z    =        -5120073
95
 XDOT =     -23774
767259                 XDOT =       -7216
901296
 YDOT =      -6289
917672  feet/sec       YDOT =       -1998
036828  meter/sec
 ZDOT =      -5181
025348                 ZDOT =       -1614
306431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -978260
48                 X    =         -298173
79
 Y    =      -14574237
56  feet           Y    =        -4442227
61  meter
 Z    =      -16799190
99                 Z    =        -5120393
41
 XDOT =      23075
507378                 XDOT =        7033
414649
 YDOT =       4599
913984  feet/sec       YDOT =        1402
053782  meter/sec
 ZDOT =      -5336
776446                 ZDOT =       -1626
649461


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
29389999  
00016717  00000-0  10270-3 0  9035
2 25544  51
6380 205
5137 0002811 256
4363 103
6477 15
54173129 10220


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
29389999   =   yrday
fracday
Element set:     903
Inclination:       51
6380  deg
RA of node:       205
5137  deg
Eccentricity:     
0002811     
Arg of perigee:   256
4363  deg
Mean anomaly:     103
6477  deg
Mean motion:   15
54173129  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1022
Checksum:              309


Coasting Arc #5 (Orbit 1022)
---------------------------------------

Vector Time (GMT): 2017/351/07:21:00
000
Vector Time (MET): N/A
Weight (LBS)     : 903628
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -519609
40                 A    =         6778659
50  meter
 Y    =       -4579415
79  meter          E    =           
0004755
 Z    =        4970142
80                 I    =           51
46284
 XDOT =       7236
192845                 Wp   =          150
61508
 YDOT =       1448
212541  meter/sec      RA   =          204
32846  deg
 ZDOT =       2085
966679                 TA   =          279
00872
                                          MA   =          279
06253
                                          Ha   =            219
880  n
mi
                                          Hp   =            215
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1704755
27                 X    =         -492505
19
 Y    =      -15024330
02  feet           Y    =        -4585075
41  meter
 Z    =       16306242
80                 Z    =         4967684
02
 XDOT =      23740
790173                 XDOT =        7209
328072
 YDOT =       4751
353482  feet/sec       YDOT =        1528
982158  meter/sec
 ZDOT =       6843
722701                 ZDOT =        2121
052983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5759707
74                 X    =         1755558
92
 Y    =       13992767
11  feet           Y    =         4264995
42  meter
 Z    =       16295964
91                 Z    =         4967010
11
 XDOT =     -23083
140694                 XDOT =       -7035
741284
 YDOT =       1331
280687  feet/sec       YDOT =         405
774353  meter/sec
 ZDOT =       6999
346672                 ZDOT =        2133
400866


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
35819933  
00016717  00000-0  10270-3 0  9049
2 25544  51
6384 205
1940 0002973 255
7050 104
3773 15
54197130 10232


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
35819933   =   yrday
fracday
Element set:     904
Inclination:       51
6384  deg
RA of node:       205
1940  deg
Eccentricity:     
0002973     
Arg of perigee:   255
7050  deg
Mean anomaly:     104
3773  deg
Mean motion:   15
54197130  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1023
Checksum:              295


Coasting Arc #6 (Orbit 1024)
---------------------------------------

Vector Time (GMT): 2017/351/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5186760
83                 A    =         6787795
53  meter
 Y    =        3928979
25  meter          E    =           
0006431
 Z    =       -1919841
81                 I    =           51
49841
 XDOT =      -4318
509891                 Wp   =          166
99869
 YDOT =       2971
843877  meter/sec      RA   =          203
56972  deg
 ZDOT =      -5595
021599                 TA   =           34
20003
                                          MA   =           34
15863
                                          Ha   =            219
965  n
mi
                                          Hp   =            215
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17016931
86                 X    =         5151766
14
 Y    =       12890351
88  feet           Y    =         3986785
70  meter
 Z    =       -6298693
61                 Z    =        -1894730
56
 XDOT =     -14168
339537                 XDOT =       -4324
242868
 YDOT =       9750
143952  feet/sec       YDOT =        2923
519910  meter/sec
 ZDOT =     -18356
370076                 ZDOT =       -5616
013297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17866016
36                 X    =        -5445561
79
 Y    =       11744288
39  feet           Y    =         3579659
10  meter
 Z    =       -6187716
26                 Z    =        -1886015
92
 XDOT =      -3613
807131                 XDOT =       -1101
488414
 YDOT =     -15201
052555  feet/sec       YDOT =       -4633
280819  meter/sec
 ZDOT =     -18450
018016                 ZDOT =       -5623
565491


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
48680055  
00016717  00000-0  10270-3 0  9055
2 25544  51
6395 204
5538 0003070 255
9739 104
1072 15
54136511 10253


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
48680055   =   yrday
fracday
Element set:     905
Inclination:       51
6395  deg
RA of node:       204
5538  deg
Eccentricity:     
0003070     
Arg of perigee:   255
9739  deg
Mean anomaly:     104
1072  deg
Mean motion:   15
54136511  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1025
Checksum:              292


Coasting Arc #7 (Orbit 1040)
---------------------------------------

Vector Time (GMT): 2017/352/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924798
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4075123
91                 A    =         6784411
82  meter
 Y    =       -4220636
02  meter          E    =           
0009496
 Z    =        3399040
00                 I    =           51
51763
 XDOT =       5827
006959                 Wp   =           91
39365
 YDOT =      -1905
750571  meter/sec      RA   =          198
58213  deg
 ZDOT =       4608
252083                 TA   =          308
42786
                                          MA   =          308
51307
                                          Ha   =            219
908  n
mi
                                          Hp   =            215
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13369829
12                 X    =        -4044135
66
 Y    =      -13847231
02  feet           Y    =        -4266033
97  meter
 Z    =       11151706
04                 Z    =         3379319
04
 XDOT =      19117
476899                 XDOT =        5825
499822
 YDOT =      -6252
462502  feet/sec       YDOT =       -1840
597960  meter/sec
 ZDOT =      15118
937281                 ZDOT =        4636
554062

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17413557
46                 X    =         5307652
31
 Y    =       -8318609
10  feet           Y    =        -2535512
06  meter
 Z    =       11064693
59                 Z    =         3372518
61
 XDOT =       -754
411362                 XDOT =        -229
944583
 YDOT =      18748
274634  feet/sec       YDOT =        5714
474108  meter/sec
 ZDOT =      15244
922050                 ZDOT =        4646
652241


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
51560558  
00016717  00000-0  10270-3 0  9066
2 25544  51
6394 199
4241 0003017 264
5030  95
5779 15
54161089 10419


Satellite: ISS
Catalog Number: 25544
Epoch time:      17352
51560558   =   yrday
fracday
Element set:     906
Inclination:       51
6394  deg
RA of node:       199
4241  deg
Eccentricity:     
0003017     
Arg of perigee:   264
5030  deg
Mean anomaly:      95
5779  deg
Mean motion:   15
54161089  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1041
Checksum:              309


Coasting Arc #8 (Orbit 1054)
---------------------------------------

Vector Time (GMT): 2017/353/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1731294
10                 A    =         6779264
06  meter
 Y    =       -4406734
97  meter          E    =           
0005044
 Z    =        4850586
15                 I    =           51
52968
 XDOT =       7270
767082                 Wp   =          139
10690
 YDOT =       -172
514664  meter/sec      RA   =          194
05772  deg
 ZDOT =       2433
218380                 TA   =          286
95907
                                          MA   =          287
01435
                                          Ha   =            219
938  n
mi
                                          Hp   =            215
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5680098
75                 X    =        -1705449
88
 Y    =      -14457791
89  feet           Y    =        -4425951
55  meter
 Z    =       15913996
57                 Z    =         4842238
33
 XDOT =      23854
222709                 XDOT =        7260
336440
 YDOT =       -565
992991  feet/sec       YDOT =         -91
266583  meter/sec
 ZDOT =       7982
999936                 ZDOT =        2468
512132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13462927
59                 X    =         4103500
33
 Y    =        7823069
97  feet           Y    =         2384471
73  meter
 Z    =       15877522
22                 Z    =         4839468
77
 XDOT =     -17828
849131                 XDOT =       -5434
233215
 YDOT =      14127
238869  feet/sec       YDOT =        4305
982407  meter/sec
 ZDOT =       8139
823514                 ZDOT =        2481
018207


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
41580868  
00016717  00000-0  10270-3 0  9073
2 25544  51
6401 194
9359 0002840 265
5225  94
5603 15
54171814 10555


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
41580868   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:       194
9359  deg
Eccentricity:     
0002840     
Arg of perigee:   265
5225  deg
Mean anomaly:      94
5603  deg
Mean motion:   15
54171814  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1055
Checksum:              312


Coasting Arc #9 (Orbit 1069)
---------------------------------------

Vector Time (GMT): 2017/354/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -61284
67                 A    =         6777271
62  meter
 Y    =        4245148
70  meter          E    =           
0011788
 Z    =       -5292893
44                 I    =           51
55471
 XDOT =      -7601
312014                 Wp   =           84
59850
 YDOT =       -779
397120  meter/sec      RA   =          189
05290  deg
 ZDOT =       -537
046279                 TA   =          180
26534
                                          MA   =          180
26596
                                          Ha   =            219
818  n
mi
                                          Hp   =            215
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -201065
18                 X    =          -83040
33
 Y    =       13927653
21  feet           Y    =         4244342
32  meter
 Z    =      -17365135
95                 Z    =        -5293243
50
 XDOT =     -24938
687711                 XDOT =       -7589
422946
 YDOT =      -2557
077165  feet/sec       YDOT =        -864
333650  meter/sec
 ZDOT =      -1761
962859                 ZDOT =        -573
942159

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8699765
25                 X    =        -2651688
45
 Y    =      -10874723
66  feet           Y    =        -3314615
77  meter
 Z    =      -17367278
64                 Z    =        -5293546
53
 XDOT =      20183
862209                 XDOT =        6152
041201
 YDOT =     -13071
220982  feet/sec       YDOT =       -3984
108155  meter/sec
 ZDOT =      -1925
799083                 ZDOT =        -586
983560


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
38030970  
00016717  00000-0  10270-3 0  9085
2 25544  51
6395 190
1279 0002926 270
8621  89
2197 15
54196549 10708


Satellite: ISS
Catalog Number: 25544
Epoch time:      17354
38030970   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       190
1279  deg
Eccentricity:     
0002926     
Arg of perigee:   270
8621  deg
Mean anomaly:      89
2197  deg
Mean motion:   15
54196549  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1070
Checksum:              327


Coasting Arc #10 (Orbit 1085)
---------------------------------------

Vector Time (GMT): 2017/355/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1883099
49                 A    =         6777707
93  meter
 Y    =       -3969202
69  meter          E    =           
0002771
 Z    =        5161187
08                 I    =           51
58956
 XDOT =       7355
148046                 Wp   =           11
00932
 YDOT =       1645
526068  meter/sec      RA   =          184
04821  deg
 ZDOT =      -1415
306132                 TA   =           92
62936
                                          MA   =           92
59764
                                          Ha   =            219
660  n
mi
                                          Hp   =            215
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6178147
93                 X    =         1902273
88
 Y    =      -13022318
54  feet           Y    =        -3948037
91  meter
 Z    =       16933028
47                 Z    =         5170380
69
 XDOT =      24131
063142                 XDOT =        7343
075498
 YDOT =       5398
707572  feet/sec       YDOT =        1727
709007  meter/sec
 ZDOT =      -4643
392822                 ZDOT =       -1379
606495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3722975
15                 X    =         1134762
83
 Y    =       13873926
95  feet           Y    =         4228772
94  meter
 Z    =       16974432
31                 Z    =         5173806
97
 XDOT =     -20966
250343                 XDOT =       -6390
513105
 YDOT =      11124
568876  feet/sec       YDOT =        3390
768593  meter/sec
 ZDOT =      -4484
965402                 ZDOT =       -1367
017455


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
40910921  
00016717  00000-0  10270-3 0  9093
2 25544  51
6400 184
9990 0003110 274
0448  86
0349 15
54217798 10866


Satellite: ISS
Catalog Number: 25544
Epoch time:      17355
40910921   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       184
9990  deg
Eccentricity:     
0003110     
Arg of perigee:   274
0448  deg
Mean anomaly:      86
0349  deg
Mean motion:   15
54217798  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1086
Checksum:              313


Coasting Arc #11 (Orbit 1100)
---------------------------------------

Vector Time (GMT): 2017/356/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3571684
00                 A    =         6780497
51  meter
 Y    =        3617374
12  meter          E    =           
0006651
 Z    =       -4493730
67                 I    =           51
63170
 XDOT =      -6513
541230                 Wp   =          115
96200
 YDOT =      -2437
929317  meter/sec      RA   =          179
04971  deg
 ZDOT =       3215
426698                 TA   =          186
39413
                                          MA   =          186
40262
                                          Ha   =            219
776  n
mi
                                          Hp   =            215
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11718123
35                 X    =        -3590040
85
 Y    =       11868025
32  feet           Y    =         3577330
88  meter
 Z    =      -14743210
86                 Z    =        -4511124
91
 XDOT =     -21369
885925                 XDOT =       -6501
414380
 YDOT =      -7998
455765  feet/sec       YDOT =       -2510
700676  meter/sec
 ZDOT =      10549
300190                 ZDOT =        3183
815437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         988516
24                 X    =          301299
75
 Y    =      -16579713
54  feet           Y    =        -5053496
69  meter
 Z    =      -14821020
24                 Z    =        -4517446
97
 XDOT =      20219
631313                 XDOT =        6162
943624
 YDOT =      -8096
942679  feet/sec       YDOT =       -2467
948128  meter/sec
 ZDOT =      10409
128056                 ZDOT =        3172
702231


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
37360851  
00016717  00000-0  10270-3 0  9103
2 25544  51
6402 180
1900 0003103 279
4571  80
6230 15
54192988 11015


Satellite: ISS
Catalog Number: 25544
Epoch time:      17356
37360851   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:       180
1900  deg
Eccentricity:     
0003103     
Arg of perigee:   279
4571  deg
Mean anomaly:      80
6230  deg
Mean motion:   15
54192988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1101
Checksum:              282


Coasting Arc #12 (Orbit 1116)
---------------------------------------

Vector Time (GMT): 2017/357/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4985330
74                 A    =         6784276
97  meter
 Y    =       -3165849
92  meter          E    =           
0009601
 Z    =        3331557
10                 I    =           51
67707
 XDOT =       5165
339253                 Wp   =           86
44502
 YDOT =       3188
039564  meter/sec      RA   =          174
06364  deg
 ZDOT =      -4687
690175                 TA   =           54
77800
                                          MA   =           54
68817
                                          Ha   =            219
769  n
mi
                                          Hp   =            215
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16356071
99                 X    =         5004178
69
 Y    =      -10386646
72  feet           Y    =        -3109995
41  meter
 Z    =       10930305
43                 Z    =         3355819
60
 XDOT =      16946
651091                 XDOT =        5152
076125
 YDOT =      10459
447387  feet/sec       YDOT =        3245
728117  meter/sec
 ZDOT =     -15379
560943                 ZDOT =       -4662
630762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5160357
70                 X    =        -1572877
03
 Y    =       18611696
17  feet           Y    =         5672844
99  meter
 Z    =       11038594
66                 Z    =         3364563
65
 XDOT =     -18311
102150                 XDOT =       -5581
223935
 YDOT =       4002
362868  feet/sec       YDOT =        1219
920202  meter/sec
 ZDOT =     -15268
595513                 ZDOT =       -4653
867912


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
40240499  
00016717  00000-0  10270-3 0  9114
2 25544  51
6399 175
0609 0003056 286
3136  73
7681 15
54215101 11173


Satellite: ISS
Catalog Number: 25544
Epoch time:      17357
40240499   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       175
0609  deg
Eccentricity:     
0003056     
Arg of perigee:   286
3136  deg
Mean anomaly:      73
7681  deg
Mean motion:   15
54215101  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1117
Checksum:              301


Coasting Arc #13 (Orbit 1131)
---------------------------------------

Vector Time (GMT): 2017/358/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5980686
98                 A    =         6787708
73  meter
 Y    =        2625669
92  meter          E    =           
0006721
 Z    =       -1832615
35                 I    =           51
72005
 XDOT =      -3432
546849                 Wp   =           13
19083
 YDOT =      -3880
980029  meter/sec      RA   =          169
09004  deg
 ZDOT =       5652
036826                 TA   =          326
68029
                                          MA   =          326
72258
                                          Ha   =            219
843  n
mi
                                          Hp   =            215
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19621676
45                 X    =        -6000701
56
 Y    =        8614402
62  feet           Y    =         2558677
99  meter
 Z    =       -6012517
56                 Z    =        -1861715
87
 XDOT =     -11261
636643                 XDOT =       -3416
348156
 YDOT =     -12732
874110  feet/sec       YDOT =       -3919
274892  meter/sec
 ZDOT =      18543
427906                 ZDOT =        5635
401825

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8460434
27                 X    =         2578740
37
 Y    =      -19648466
23  feet           Y    =        -5988852
51  meter
 Z    =       -6142256
37                 Z    =        -1872159
74
 XDOT =      15574
148677                 XDOT =        4747
000517
 YDOT =        942
730584  feet/sec       YDOT =         287
344282  meter/sec
 ZDOT =      18469
996022                 ZDOT =        5629
654788


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   17358
36690165  
00016717  00000-0  10270-3 0  9120
2 25544  51
6394 170
2525 0003175 288
5576  71
5232 15
54173626 11326


Satellite: ISS
Catalog Number: 25544
Epoch time:      17358
36690165   =   yrday
fracday
Element set:     912
Inclination:       51
6394  deg
RA of node:       170
2525  deg
Eccentricity:     
0003175     
Arg of perigee:   288
5576  deg
Mean anomaly:      71
5232  deg
Mean motion:   15
54173626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1132
Checksum:              310


Coasting Arc #14 (Orbit 1147)
---------------------------------------

Vector Time (GMT): 2017/359/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6499266
82                 A    =         6789222
64  meter
 Y    =       -1941698
78  meter          E    =           
0009605
 Z    =         114081
76                 I    =           51
75767
 XDOT =       1460
253795                 Wp   =          140
85932
 YDOT =       4518
210124  meter/sec      RA   =          164
12561  deg
 ZDOT =      -6021
073012                 TA   =           37
91384
                                          MA   =           37
84624
                                          Ha   =            219
950  n
mi
                                          Hp   =            215
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21323053
88                 X    =         6519942
23
 Y    =       -6370402
82  feet           Y    =        -1868903
93  meter
 Z    =         374284
01                 Z    =          145703
09
 XDOT =       4790
858906                 XDOT =        1438
868645
 YDOT =      14823
524029  feet/sec       YDOT =        4534
420415  meter/sec
 ZDOT =     -19754
176548                 ZDOT =       -6014
031310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10929825
23                 X    =        -3331410
73
 Y    =       19382164
06  feet           Y    =         5907683
61  meter
 Z    =         515154
42                 Z    =          157019
07
 XDOT =     -12415
484786                 XDOT =       -3784
239763
 YDOT =      -6459
969583  feet/sec       YDOT =       -1968
998729  meter/sec
 ZDOT =     -19723
479312                 ZDOT =       -6011
716494


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   17359
39569639  
00016717  00000-0  10270-3 0  9136
2 25544  51
6402 165
1234 0003130 289
8372  70
2443 15
54161447 11480


Satellite: ISS
Catalog Number: 25544
Epoch time:      17359
39569639   =   yrday
fracday
Element set:     913
Inclination:       51
6402  deg
RA of node:       165
1234  deg
Eccentricity:     
0003130     
Arg of perigee:   289
8372  deg
Mean anomaly:      70
2443  deg
Mean motion:   15
54161447  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1148
Checksum:              310


Coasting Arc #15 (Orbit 1163)
---------------------------------------

Vector Time (GMT): 2017/360/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6493599
32                 A    =         6788050
84  meter
 Y    =        1126948
15  meter          E    =           
0012205
 Z    =        1595984
74                 I    =           51
78412
 XDOT =        542
013876                 Wp   =           51
08195
 YDOT =      -5049
525243  meter/sec      RA   =          159
16272  deg
 ZDOT =       5748
820492                 TA   =          326
34893
                                          MA   =          326
42637
                                          Ha   =            219
947  n
mi
                                          Hp   =            215
620

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21304459
72                 X    =        -6513471
02
 Y    =        3697336
45  feet           Y    =         1054221
10  meter
 Z    =        5236170
42                 Z    =         1564392
76
 XDOT =       1778
260748                 XDOT =         570
513906
 YDOT =     -16566
683868  feet/sec       YDOT =       -5043
304982  meter/sec
 ZDOT =      18860
959621                 ZDOT =        5751
522408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12495301
50                 X    =         3808567
90
 Y    =      -17688155
61  feet           Y    =        -5391349
83  meter
 Z    =        5095524
77                 Z    =         1553115
95
 XDOT =       9238
200182                 XDOT =        2815
803415
 YDOT =      11984
494603  feet/sec       YDOT =        3652
873955  meter/sec
 ZDOT =      18873
663341                 ZDOT =        5752
692586


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   17360
42448642  
00016717  00000-0  10270-3 0  9143
2 25544  51
6388 159
9932 0003178 294
6467  65
4355 15
54217620 11641


Satellite: ISS
Catalog Number: 25544
Epoch time:      17360
42448642   =   yrday
fracday
Element set:     914
Inclination:       51
6388  deg
RA of node:       159
9932  deg
Eccentricity:     
0003178     
Arg of perigee:   294
6467  deg
Mean anomaly:      65
4355  deg
Mean motion:   15
54217620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1164
Checksum:              328


Coasting Arc #16 (Orbit 1177)
---------------------------------------

Vector Time (GMT): 2017/361/06:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940029
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         792163
91                 A    =         6778872
92  meter
 Y    =       -4634142
20  meter          E    =           
0005919
 Z    =        4882957
76                 I    =           51
78300
 XDOT =       7163
704233                 Wp   =           30
93167
 YDOT =      -1312
600354  meter/sec      RA   =          154
56733  deg
 ZDOT =      -2401
638184                 TA   =           82
59291
                                          MA   =           82
52565
                                          Ha   =            219
924  n
mi
                                          Hp   =            215
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2598962
95                 X    =          820206
28
 Y    =      -15203878
60  feet           Y    =        -4625127
12  meter
 Z    =       16020202
63                 Z    =         4886873
73
 XDOT =      23502
966645                 XDOT =        7189
515626
 YDOT =      -4306
431606  feet/sec       YDOT =       -1232
346477  meter/sec
 ZDOT =      -7879
390366                 ZDOT =       -2366
776548

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1813898
26                 X    =          552876
19
 Y    =       15298483
98  feet           Y    =         4662977
92  meter
 Z    =       16038253
84                 Z    =         4888459
77
 XDOT =     -20324
897112                 XDOT =       -6195
028640
 YDOT =      10529
000220  feet/sec       YDOT =        3209
239267  meter/sec
 ZDOT =      -7724
162139                 ZDOT =       -2354
324620


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   17361
32467922  
00016717  00000-0  10270-3 0  9156
2 25544  51
6402 155
5071 0003233 299
6407  60
4423 15
54236899 11780


Satellite: ISS
Catalog Number: 25544
Epoch time:      17361
32467922   =   yrday
fracday
Element set:     915
Inclination:       51
6402  deg
RA of node:       155
5071  deg
Eccentricity:     
0003233     
Arg of perigee:   299
6407  deg
Mean anomaly:      60
4423  deg
Mean motion:   15
54236899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1178
Checksum:              310


Coasting Arc #17 (Orbit 1189)
---------------------------------------

Vector Time (GMT): 2017/362/01:04:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925596
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3750215
08                 A    =         6778230
83  meter
 Y    =       -2476894
83  meter          E    =           
0002443
 Z    =        5072773
33                 I    =           51
80070
 XDOT =       5672
180601                 Wp   =          129
15479
 YDOT =      -4824
870390  meter/sec      RA   =          150
79822  deg
 ZDOT =       1835
399508                 TA   =          303
10427
                                          MA   =          303
12771
                                          Ha   =            220
123  n
mi
                                          Hp   =            215
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12303855
26                 X    =        -3746880
11
 Y    =       -8126295
37  feet           Y    =        -2518813
93  meter
 Z    =       16642957
10                 Z    =         5054563
90
 XDOT =      18609
516408                 XDOT =        5716
796557
 YDOT =     -15829
627265  feet/sec       YDOT =       -4761
190824  meter/sec
 ZDOT =       6021
651928                 ZDOT =        1863
061318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2894753
96                 X    =         -882321
01
 Y    =       14550602
16  feet           Y    =         4435023
54  meter
 Z    =       16562304
44                 Z    =         5048190
39
 XDOT =     -20562
741643                 XDOT =       -6267
523653
 YDOT =     -11093
684106  feet/sec       YDOT =       -3381
354916  meter/sec
 ZDOT =       6145
354440                 ZDOT =        1873
104033


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   17362
09627261  
00016717  00000-0  10270-3 0  9166
2 25544  51
6379 151
6590 0003163 301
1143  58
9699 15
54224567 11904


Satellite: ISS
Catalog Number: 25544
Epoch time:      17362
09627261   =   yrday
fracday
Element set:     916
Inclination:       51
6379  deg
RA of node:       151
6590  deg
Eccentricity:     
0003163     
Arg of perigee:   301
1143  deg
Mean anomaly:      58
9699  deg
Mean motion:   15
54224567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1190
Checksum:              314


Coasting Arc #18 (Orbit 1204)
---------------------------------------

Vector Time (GMT): 2017/363/01:04:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925596
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2253341
43                 A    =         6777172
80  meter
 Y    =        3538462
98  meter          E    =           
0012509
 Z    =       -5333425
91                 I    =           51
82530
 XDOT =      -6384
071370                 Wp   =           82
26766
 YDOT =       4230
969950  meter/sec      RA   =          145
80922  deg
 ZDOT =        111
669112                 TA   =          188
78401
                                          MA   =          188
80592
                                          Ha   =            220
194  n
mi
                                          Hp   =            215
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7392852
46                 X    =         2239513
13
 Y    =       11609130
50  feet           Y    =         3563584
45  meter
 Z    =      -17498116
52                 Z    =        -5322513
19
 XDOT =     -20945
116044                 XDOT =       -6431
451171
 YDOT =      13881
135008  feet/sec       YDOT =        4159
313972  meter/sec
 ZDOT =        366
368479                 ZDOT =          80
542432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7763275
85                 X    =         2366246
48
 Y    =      -11438402
34  feet           Y    =        -3486425
03  meter
 Z    =      -17450064
76                 Z    =        -5318779
74
 XDOT =      20113
769592                 XDOT =        6130
676972
 YDOT =      13313
844267  feet/sec       YDOT =        4058
059733  meter/sec
 ZDOT =        227
313620                 ZDOT =          69
285191


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   17363
06076187  
00016717  00000-0  10270-3 0  9170
2 25544  51
6381 146
8494 0003137 307
5170  52
5697 15
54192084 12050


Satellite: ISS
Catalog Number: 25544
Epoch time:      17363
06076187   =   yrday
fracday
Element set:     917
Inclination:       51
6381  deg
RA of node:       146
8494  deg
Eccentricity:     
0003137     
Arg of perigee:   307
5170  deg
Mean anomaly:      52
5697  deg
Mean motion:   15
54192084  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1205
Checksum:              314


Coasting Arc #19 (Orbit 1220)
---------------------------------------

Vector Time (GMT): 2017/364/01:04:30
000
Vector Time (MET): N/A
Weight (LBS)     : 925596
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -694356
07                 A    =         6778503
37  meter
 Y    =       -4510821
50  meter          E    =           
0006027
 Z    =        5011202
95                 I    =           51
85630
 XDOT =       6608
496750                 Wp   =           26
44689
 YDOT =      -3305
121095  meter/sec      RA   =          140
82406  deg
 ZDOT =      -2053
207081                 TA   =           83
49021
                                          MA   =           83
42160
                                          Ha   =            220
307  n
mi
                                          Hp   =            215
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2278071
08                 X    =         -668205
24
 Y    =      -14799283
14  feet           Y    =        -4518440
52  meter
 Z    =       16440954
57                 Z    =         5007893
08
 XDOT =      21681
419782                 XDOT =        6654
937833
 YDOT =     -10843
573147  feet/sec       YDOT =       -3230
960505  meter/sec
 ZDOT =      -6736
243704                 ZDOT =       -2020
992506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12558568
62                 X    =        -3827851
72
 Y    =        8182532
20  feet           Y    =         2494035
81  meter
 Z    =       16426865
12                 Z    =         5006908
49
 XDOT =     -18126
403007                 XDOT =       -5524
927636
 YDOT =     -14544
801642  feet/sec       YDOT =       -4433
255540  meter/sec
 ZDOT =      -6592
453911                 ZDOT =       -2009
379952


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   17364
08954826  
00016717  00000-0  10270-3 0  9189
2 25544  51
6380 141
7209 0003131 313
0844  47
0047 15
54192632 12216


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
08954826   =   yrday
fracday
Element set:     918
Inclination:       51
6380  deg
RA of node:       141
7209  deg
Eccentricity:     
0003131     
Arg of perigee:   313
0844  deg
Mean anomaly:      47
0047  deg
Mean motion:   15
54192632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1221
Checksum:              289


Coasting Arc #20 (Orbit 1227)
---------------------------------------

Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925596
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3592066
53                 A    =         6777483
77  meter
 Y    =       -2331643
21  meter          E    =           
0000885
 Z    =        5252415
06                 I    =           51
86382
 XDOT =       5138
569074                 Wp   =          111
81033
 YDOT =      -5600
006184  meter/sec      RA   =          138
63427  deg
 ZDOT =       1027
804330                 TA   =          328
37708
                                          MA   =          328
38240
                                          Ha   =            220
294  n
mi
                                          Hp   =            215
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11784995
19                 X    =        -3591240
17
 Y    =       -7649748
06  feet           Y    =        -2371808
08  meter
 Z    =       17232332
86                 Z    =         5234967
66
 XDOT =      16858
822422                 XDOT =        5195
815368
 YDOT =     -18372
723701  feet/sec       YDOT =       -5542
223213  meter/sec
 ZDOT =       3372
061449                 ZDOT =        1052
904388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6693532
28                 X    =         2040188
64
 Y    =      -12460315
25  feet           Y    =        -3797904
09  meter
 Z    =       17155034
90                 Z    =         5228854
64
 XDOT =      18725
238951                 XDOT =        5707
452832
 YDOT =      14858
471345  feet/sec       YDOT =        4528
862066  meter/sec
 ZDOT =       3484
533713                 ZDOT =        1062
085876


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   17364
53964146  
00016717  00000-0  10270-3 0  9196
2 25544  51
6376 139
4724 0002875 306
5492  53
5396 15
54210039 12285


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
53964146   =   yrday
fracday
Element set:     919
Inclination:       51
6376  deg
RA of node:       139
4724  deg
Eccentricity:     
0002875     
Arg of perigee:   306
5492  deg
Mean anomaly:      53
5396  deg
Mean motion:   15
54210039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1228
Checksum:              325
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