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

 
Date: June 30th 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) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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


182/20:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 214 8

183/15:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 214 9

190/12:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 2350)
---------------------------------------

Vector Time (GMT): 2017/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         177663
60                 A    =         6777990
97  meter
 Y    =        4321053
60  meter          E    =           
0006457
 Z    =        5219152
79                 I    =           51
50351
 XDOT =      -7421
619736                 Wp   =            8
86318
 YDOT =       1606
079576  meter/sec      RA   =          341
35051  deg
 ZDOT =      -1070
643335                 TA   =           91
44973
                                          MA   =           91
37576
                                          Ha   =            221
123  n
mi
                                          Hp   =            215
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         582885
84                 X    =          103979
46
 Y    =       14176685
04  feet           Y    =         4322627
86  meter
 Z    =       17123204
68                 Z    =         5219837
26
 XDOT =     -24349
146117                 XDOT =       -7433
827156
 YDOT =       5269
289949  feet/sec       YDOT =        1523
017838  meter/sec
 ZDOT =      -3512
609366                 ZDOT =       -1106
724332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14054322
88                 X    =         4283757
61
 Y    =       -1928579
41  feet           Y    =         -587831
00  meter
 Z    =       17125387
10                 Z    =         5219817
99
 XDOT =       7605
541340                 XDOT =        2318
169000
 YDOT =      22628
818010  feet/sec       YDOT =        6897
263729  meter/sec
 ZDOT =      -3672
214731                 ZDOT =       -1119
291050


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   17179
54633345  
00016717  00000-0  10270-3 0  9005
2 25544  51
6380 341
7106 0004772 333
0174  27
0730 15
54051394 23515


Satellite: ISS
Catalog Number: 25544
Epoch time:      17179
54633345   =   yrday
fracday
Element set:     900
Inclination:       51
6380  deg
RA of node:       341
7106  deg
Eccentricity:     
0004772     
Arg of perigee:   333
0174  deg
Mean anomaly:      27
0730  deg
Mean motion:   15
54051394  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2351
Checksum:              284


Coasting Arc #2 (Orbit 2365)
---------------------------------------

Vector Time (GMT): 2017/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1491018
59                 A    =         6780266
10  meter
 Y    =       -4701396
62  meter          E    =           
0007900
 Z    =       -4658870
58                 I    =           51
48265
 XDOT =       7076
713772                 Wp   =           83
41776
 YDOT =       -600
688629  meter/sec      RA   =          336
34501  deg
 ZDOT =       2876
080966                 TA   =          215
22382
                                          MA   =          215
27606
                                          Ha   =            221
128  n
mi
                                          Hp   =            215
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4891793
28                 X    =         1566110
32
 Y    =      -15424529
59  feet           Y    =        -4684302
79  meter
 Z    =      -15285008
47                 Z    =        -4651445
74
 XDOT =      23217
564870                 XDOT =        7068
934421
 YDOT =      -1970
763219  feet/sec       YDOT =        -521
595750  meter/sec
 ZDOT =       9435
961173                 ZDOT =        2910
438179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15913668
44                 X    =        -4850486
14
 Y    =       -3103148
66  feet           Y    =         -945839
71  meter
 Z    =      -15251323
33                 Z    =        -4648603
35
 XDOT =      -4962
478694                 XDOT =       -1512
563506
 YDOT =     -21590
822534  feet/sec       YDOT =       -6580
882708  meter/sec
 ZDOT =       9587
751340                 ZDOT =        2922
346608


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   17180
51088504  
00016717  00000-0  10270-3 0  9016
2 25544  51
6397 336
9033 0004804 335
5840  24
5085 15
54096980 23662


Satellite: ISS
Catalog Number: 25544
Epoch time:      17180
51088504   =   yrday
fracday
Element set:     901
Inclination:       51
6397  deg
RA of node:       336
9033  deg
Eccentricity:     
0004804     
Arg of perigee:   335
5840  deg
Mean anomaly:      24
5085  deg
Mean motion:   15
54096980  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2366
Checksum:              312


Coasting Arc #3 (Orbit 2381)
---------------------------------------

Vector Time (GMT): 2017/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3000406
72                 A    =         6784028
27  meter
 Y    =        4904321
29  meter          E    =           
0011546
 Z    =        3597097
45                 I    =           51
46525
 XDOT =      -6249
776580                 Wp   =           63
15002
 YDOT =       -581
657898  meter/sec      RA   =          331
34463  deg
 ZDOT =      -4403
965101                 TA   =           74
15786
                                          MA   =           74
03060
                                          Ha   =            221
287  n
mi
                                          Hp   =            215
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9843854
08                 X    =        -3072497
96
 Y    =       16090292
96  feet           Y    =         4870365
35  meter
 Z    =       11801500
80                 Z    =         3582347
77
 XDOT =     -20504
516337                 XDOT =       -6221
415672
 YDOT =      -1908
326438  feet/sec       YDOT =        -651
388223  meter/sec
 ZDOT =     -14448
704398                 ZDOT =       -4434
255544

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17299846
19                 X    =         5272993
12
 Y    =        7620298
50  feet           Y    =         2322666
98  meter
 Z    =       11735449
91                 Z    =         3576965
13
 XDOT =       1463
091569                 XDOT =         445
950310
 YDOT =      19217
120896  feet/sec       YDOT =        5857
378449  meter/sec
 ZDOT =     -14582
305686                 ZDOT =       -4444
686773


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   17181
53973813  
00016717  00000-0  10270-3 0  9026
2 25544  51
6393 331
7739 0004822 339
5674  20
5285 15
54086724 23824


Satellite: ISS
Catalog Number: 25544
Epoch time:      17181
53973813   =   yrday
fracday
Element set:     902
Inclination:       51
6393  deg
RA of node:       331
7739  deg
Eccentricity:     
0004822     
Arg of perigee:   339
5674  deg
Mean anomaly:      20
5285  deg
Mean motion:   15
54086724  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2382
Checksum:              324


Coasting Arc #4 (Orbit 2396)
---------------------------------------

Vector Time (GMT): 2017/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4175979
84                 A    =         6787415
35  meter
 Y    =       -4875291
66  meter          E    =           
0009721
 Z    =       -2189543
14                 I    =           51
44931
 XDOT =       5044
245395                 Wp   =           16
59802
 YDOT =       1873
420423  meter/sec      RA   =          326
35385  deg
 ZDOT =       5464
303970                 TA   =          319
02173
                                          MA   =          319
09474
                                          Ha   =            221
386  n
mi
                                          Hp   =            215
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13700721
27                 X    =         4240821
96
 Y    =      -15995051
36  feet           Y    =        -4828230
29  meter
 Z    =       -7183540
49                 Z    =        -2169100
50
 XDOT =      16549
361532                 XDOT =        4996
378606
 YDOT =       6146
392465  feet/sec       YDOT =        1929
560520  meter/sec
 ZDOT =      17927
506463                 ZDOT =        5488
691154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17923759
64                 X    =        -5463161
94
 Y    =      -11117182
44  feet           Y    =        -3388517
21  meter
 Z    =       -7092374
80                 Z    =        -2161755
84
 XDOT =       2730
711057                 XDOT =         832
320730
 YDOT =     -15876
100377  feet/sec       YDOT =       -4839
035395  meter/sec
 ZDOT =      18034
796754                 ZDOT =        5497
006051


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   17182
50428495  
00016717  00000-0  10270-3 0  9036
2 25544  51
6400 326
9665 0004853 343
8495  16
2502 15
54103968 23970


Satellite: ISS
Catalog Number: 25544
Epoch time:      17182
50428495   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:       326
9665  deg
Eccentricity:     
0004853     
Arg of perigee:   343
8495  deg
Mean anomaly:      16
2502  deg
Mean motion:   15
54103968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2397
Checksum:              320


Coasting Arc #5 (Orbit 2402)
---------------------------------------

Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3747593
32                 A    =         6778151
85  meter
 Y    =       -2366963
92  meter          E    =           
0014490
 Z    =       -5140344
56                 I    =           51
40820
 XDOT =       5359
546034                 Wp   =           57
78852
 YDOT =      -5266
497983  meter/sec      RA   =          324
53216  deg
 ZDOT =      -1477
842081                 TA   =          197
89171
                                          MA   =          197
94278
                                          Ha   =            221
487  n
mi
                                          Hp   =            214
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12295253
66                 X    =        -3695877
57
 Y    =       -7765629
66  feet           Y    =        -2408582
46  meter
 Z    =      -16864647
52                 Z    =        -5158423
75
 XDOT =      17583
812448                 XDOT =        5425
217681
 YDOT =     -17278
536688  feet/sec       YDOT =       -5206
196589  meter/sec
 ZDOT =      -4848
563257                 ZDOT =       -1451
648063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13537441
57                 X    =         4126212
19
 Y    =       -5053036
26  feet           Y    =        -1540165
45  meter
 Z    =      -16943999
02                 Z    =        -5164530
90
 XDOT =       2823
322630                 XDOT =         860
548738
 YDOT =      23480
527955  feet/sec       YDOT =        7156
864921  meter/sec
 ZDOT =      -4731
940002                 ZDOT =       -1442
295312


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   17182
89010207  
00016717  00000-0  10270-3 0  9047
2 25544  51
6398 325
0477 0005158 346
3516  13
7496 15
54093424 24035


Satellite: ISS
Catalog Number: 25544
Epoch time:      17182
89010207   =   yrday
fracday
Element set:     904
Inclination:       51
6398  deg
RA of node:       325
0477  deg
Eccentricity:     
0005158     
Arg of perigee:   346
3516  deg
Mean anomaly:      13
7496  deg
Mean motion:   15
54093424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2403
Checksum:              306


Coasting Arc #6 (Orbit 2414)
---------------------------------------

Vector Time (GMT): 2017/183/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         469470
00                 A    =         6780698
85  meter
 Y    =       -5046220
46  meter          E    =           
0008005
 Z    =       -4510777
82                 I    =           51
39813
 XDOT =       6631
800560                 Wp   =           78
89076
 YDOT =      -2193
376459  meter/sec      RA   =          320
59600  deg
 ZDOT =       3150
231492                 TA   =          222
81779
                                          MA   =          222
88016
                                          Ha   =            221
397  n
mi
                                          Hp   =            214
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1540255
90                 X    =          547774
39
 Y    =      -16555841
40  feet           Y    =        -5040532
29  meter
 Z    =      -14799139
81                 Z    =        -4508307
54
 XDOT =      21757
875853                 XDOT =        6640
532323
 YDOT =      -7196
116993  feet/sec       YDOT =       -2119
166629  meter/sec
 ZDOT =      10335
405157                 ZDOT =        3182
467703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8604858
85                 X    =        -2622760
98
 Y    =       14239928
54  feet           Y    =         4340330
22  meter
 Z    =      -14787280
04                 Z    =        -4507162
96
 XDOT =     -21636
273040                 XDOT =       -6594
736023
 YDOT =      -2214
829279  feet/sec       YDOT =        -675
079964  meter/sec
 ZDOT =      10478
107014                 ZDOT =        3193
727018


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   17183
66173752  
00016717  00000-0  10270-3 0  9059
2 25544  51
6414 321
1997 0004979 346
7640  13
3381 15
54136339 24155


Satellite: ISS
Catalog Number: 25544
Epoch time:      17183
66173752   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:       321
1997  deg
Eccentricity:     
0004979     
Arg of perigee:   346
7640  deg
Mean anomaly:      13
3381  deg
Mean motion:   15
54136339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2415
Checksum:              318


Coasting Arc #7 (Orbit 2430)
---------------------------------------

Vector Time (GMT): 2017/184/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1850587
76                 A    =         6784530
17  meter
 Y    =        5584733
14  meter          E    =           
0012656
 Z    =        3373878
44                 I    =           51
38690
 XDOT =      -6072
005751                 Wp   =           66
77996
 YDOT =        787
651278  meter/sec      RA   =          315
59172  deg
 ZDOT =      -4615
596784                 TA   =           73
67725
                                          MA   =           73
53810
                                          Ha   =            221
581  n
mi
                                          Hp   =            214
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6071482
15                 X    =        -1929288
82
 Y    =       18322615
29  feet           Y    =         5563598
22  meter
 Z    =       11069154
98                 Z    =         3364698
27
 XDOT =     -19921
278712                 XDOT =       -6057
941890
 YDOT =       2584
157735  feet/sec       YDOT =         719
829099  meter/sec
 ZDOT =     -15143
034069                 ZDOT =       -4645
058469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13192077
21                 X    =         4020945
13
 Y    =      -14123342
93  feet           Y    =        -4304794
93  meter
 Z    =       11027583
67                 Z    =         3361207
50
 XDOT =      18077
089694                 XDOT =        5509
896939
 YDOT =       4911
588615  feet/sec       YDOT =        1497
052210  meter/sec
 ZDOT =     -15273
217823                 ZDOT =       -4655
276792


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   17184
69058090  
00016717  00000-0  10270-3 0  9061
2 25544  51
6420 316
0707 0005183 350
5888   9
5166 15
54132556 24312


Satellite: ISS
Catalog Number: 25544
Epoch time:      17184
69058090   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       316
0707  deg
Eccentricity:     
0005183     
Arg of perigee:   350
5888  deg
Mean anomaly:       9
5166  deg
Mean motion:   15
54132556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2431
Checksum:              307


Coasting Arc #8 (Orbit 2445)
---------------------------------------

Vector Time (GMT): 2017/185/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2953086
52                 A    =         6787915
64  meter
 Y    =       -5797224
29  meter          E    =           
0011453
 Z    =       -1914974
53                 I    =           51
37457
 XDOT =       5190
904488                 Wp   =           19
42045
 YDOT =        804
893810  meter/sec      RA   =          310
59643  deg
 ZDOT =       5588
472507                 TA   =          319
39181
                                          MA   =          319
47718
                                          Ha   =            221
758  n
mi
                                          Hp   =            214
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9688604
08                 X    =         3026995
14
 Y    =      -19019764
73  feet           Y    =        -5763787
41  meter
 Z    =       -6282724
84                 Z    =        -1900450
51
 XDOT =      17030
526535                 XDOT =        5154
372106
 YDOT =       2640
727723  feet/sec       YDOT =         862
737115  meter/sec
 ZDOT =      18334
883552                 ZDOT =        5613
599672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16512987
91                 X    =        -5033158
71
 Y    =       13555685
96  feet           Y    =         4131773
08  meter
 Z    =       -6217534
85                 Z    =        -1895104
62
 XDOT =     -13461
433821                 XDOT =       -4103
045029
 YDOT =      -7968
548294  feet/sec       YDOT =       -2428
813520  meter/sec
 ZDOT =      18445
634472                 ZDOT =        5622
229387


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   17185
65511853  
00016717  00000-0  10270-3 0  9070
2 25544  51
6413 311
2630 0005337 353
6153   6
4931 15
54089828 24461


Satellite: ISS
Catalog Number: 25544
Epoch time:      17185
65511853   =   yrday
fracday
Element set:     907
Inclination:       51
6413  deg
RA of node:       311
2630  deg
Eccentricity:     
0005337     
Arg of perigee:   353
6153  deg
Mean anomaly:       6
4931  deg
Mean motion:   15
54089828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2446
Checksum:              305


Coasting Arc #9 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2017/186/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3803633
79                 A    =         6789302
26  meter
 Y    =        5616490
78  meter          E    =           
0009640
 Z    =         222117
21                 I    =           51
35867
 XDOT =      -4078
857841                 Wp   =          109
13469
 YDOT =      -2517
458299  meter/sec      RA   =          305
60698  deg
 ZDOT =      -5981
394960                 TA   =           68
46387
                                          MA   =           68
36115
                                          Ha   =            221
796  n
mi
                                          Hp   =            214
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12479113
48                 X    =        -3867235
11
 Y    =       18426807
03  feet           Y    =         5573600
33  meter
 Z    =         728731
01                 Z    =          203486
60
 XDOT =     -13382
079532                 XDOT =       -4021
349174
 YDOT =      -8259
377623  feet/sec       YDOT =       -2562
748542  meter/sec
 ZDOT =     -19623
999213                 ZDOT =       -6001
069403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18593618
47                 X    =         5667334
91
 Y    =      -12233857
79  feet           Y    =        -3728879
85  meter
 Z    =         645457
33                 Z    =          196735
39
 XDOT =       8182
146111                 XDOT =        2493
918135
 YDOT =      11354
683934  feet/sec       YDOT =        3460
907663  meter/sec
 ZDOT =     -19710
365668                 ZDOT =       -6007
719456


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   17186
68395667  
00016717  00000-0  10270-3 0  9088
2 25544  51
6407 306
1347 0005239 359
1739    
9404 15
54130920 24626


Satellite: ISS
Catalog Number: 25544
Epoch time:      17186
68395667   =   yrday
fracday
Element set:     908
Inclination:       51
6407  deg
RA of node:       306
1347  deg
Eccentricity:     
0005239     
Arg of perigee:   359
1739  deg
Mean anomaly:        
9404  deg
Mean motion:   15
54130920  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2462
Checksum:              318


Coasting Arc #10 (Orbit 2477)
---------------------------------------

Vector Time (GMT): 2017/187/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4323816
10                 A    =         6788467
53  meter
 Y    =       -5011535
07  meter          E    =           
0017321
 Z    =        1460866
43                 I    =           51
33778
 XDOT =       2882
728121                 Wp   =           45
97288
 YDOT =       4174
610785  meter/sec      RA   =          300
61598  deg
 ZDOT =       5758
161904                 TA   =          330
04945
                                          MA   =          330
14843
                                          Ha   =            221
923  n
mi
                                          Hp   =            214
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14185748
34                 X    =         4372438
90
 Y    =      -16442044
20  feet           Y    =        -4962911
56  meter
 Z    =        4792868
88                 Z    =         1481987
53
 XDOT =       9457
769426                 XDOT =        2807
862054
 YDOT =      13696
229610  feet/sec       YDOT =        4206
428020  meter/sec
 ZDOT =      18891
607297                 ZDOT =        5771
983987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19204730
11                 X    =        -5853601
74
 Y    =       10091743
49  feet           Y    =         3075963
42  meter
 Z    =        4887015
49                 Z    =         1489562
32
 XDOT =      -2912
885788                 XDOT =        -887
847588
 YDOT =     -14768
767148  feet/sec       YDOT =       -4501
520227  meter/sec
 ZDOT =      18951
842006                 ZDOT =        5776
521443


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   17187
71279131  
00016717  00000-0  10270-3 0  9091
2 25544  51
6411 301
0058 0005406   3
2745 356
8442 15
54103459 24783


Satellite: ISS
Catalog Number: 25544
Epoch time:      17187
71279131   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       301
0058  deg
Eccentricity:     
0005406     
Arg of perigee:     3
2745  deg
Mean anomaly:     356
8442  deg
Mean motion:   15
54103459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2478
Checksum:              298


Coasting Arc #11 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2017/188/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4594092
70                 A    =         6785349
59  meter
 Y    =        3981557
09  meter          E    =           
0006411
 Z    =       -3023091
94                 I    =           51
31222
 XDOT =      -1657
649330                 Wp   =           51
35196
 YDOT =      -5639
372874  meter/sec      RA   =          295
61884  deg
 ZDOT =      -4911
397529                 TA   =          163
42840
                                          MA   =          163
40744
                                          Ha   =            222
040  n
mi
                                          Hp   =            214
041

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15072482
62                 X    =        -4623589
48
 Y    =       13062851
34  feet           Y    =         3930018
33  meter
 Z    =       -9918280
64                 Z    =        -3045479
56
 XDOT =      -5438
482055                 XDOT =       -1570
608177
 YDOT =     -18501
879507  feet/sec       YDOT =       -5657
422467  meter/sec
 ZDOT =     -16113
508955                 ZDOT =       -4919
239208

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18639700
09                 X    =         5681380
59
 Y    =       -6956646
25  feet           Y    =        -2120385
78  meter
 Z    =      -10017822
20                 Z    =        -3053432
21
 XDOT =      -2015
187440                 XDOT =        -614
229132
 YDOT =      17838
156200  feet/sec       YDOT =        5437
070010  meter/sec
 ZDOT =     -16147
088381                 ZDOT =       -4921
632539


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   17188
67731900  
00016717  00000-0  10270-3 0  9106
2 25544  51
6413 296
1979 0005425   7
8161 352
3075 15
54138550 24934


Satellite: ISS
Catalog Number: 25544
Epoch time:      17188
67731900   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:       296
1979  deg
Eccentricity:     
0005425     
Arg of perigee:     7
8161  deg
Mean anomaly:     352
3075  deg
Mean motion:   15
54138550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2493
Checksum:              314


Coasting Arc #12 (Orbit 2508)
---------------------------------------

Vector Time (GMT): 2017/189/15:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4605598
40                 A    =         6781511
35  meter
 Y    =       -2587566
33  meter          E    =           
0010777
 Z    =        4241573
07                 I    =           51
28546
 XDOT =        511
262846                 Wp   =           76
79270
 YDOT =       6773
201209  meter/sec      RA   =          290
61123  deg
 ZDOT =       3571
593675                 TA   =          336
56603
                                          MA   =          336
61510
                                          Ha   =            221
947  n
mi
                                          Hp   =            214
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15110230
96                 X    =         4613587
67
 Y    =       -8489390
86  feet           Y    =        -2536019
33  meter
 Z    =       13915922
15                 Z    =         4263964
47
 XDOT =       1677
371541                 XDOT =         418
136248
 YDOT =      22221
788745  feet/sec       YDOT =        6778
397300  meter/sec
 ZDOT =      11717
827019                 ZDOT =        3573
851959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16995151
44                 X    =        -5180122
16
 Y    =        2963118
78  feet           Y    =          903158
61  meter
 Z    =       14015223
17                 Z    =         4271840
02
 XDOT =       6156
622461                 XDOT =        1876
538526
 YDOT =     -20234
547663  feet/sec       YDOT =       -6167
490128  meter/sec
 ZDOT =      11726
569536                 ZDOT =        3574
258395


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   17189
70614602  
00016717  00000-0  10270-3 0  9111
2 25544  51
6404 291
0698 0005409  11
1107 349
0164 15
54150322 25097


Satellite: ISS
Catalog Number: 25544
Epoch time:      17189
70614602   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:       291
0698  deg
Eccentricity:     
0005409     
Arg of perigee:    11
1107  deg
Mean anomaly:     349
0164  deg
Mean motion:   15
54150322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2509
Checksum:              282


Coasting Arc #13 (Orbit 2521)
---------------------------------------

Vector Time (GMT): 2017/190/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3307584
20                 A    =         6787537
26  meter
 Y    =        5577242
51  meter          E    =           
0005482
 Z    =       -2010897
42                 I    =           51
29743
 XDOT =      -3440
979826                 Wp   =           90
43734
 YDOT =      -4030
848645  meter/sec      RA   =          286
28276  deg
 ZDOT =      -5532
932223                 TA   =          111
86855
                                          MA   =          111
81024
                                          Ha   =            222
067  n
mi
                                          Hp   =            213
959

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10851654
20                 X    =        -3359936
74
 Y    =       18298039
73  feet           Y    =         5539962
41  meter
 Z    =       -6597432
47                 Z    =        -2027090
86
 XDOT =     -11289
303892                 XDOT =       -3368
774135
 YDOT =     -13224
569045  feet/sec       YDOT =       -4068
923555  meter/sec
 ZDOT =     -18152
664773                 ZDOT =       -5549
472396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21000870
33                 X    =         6401065
28
 Y    =        3252466
77  feet           Y    =          991351
87  meter
 Z    =       -6669908
34                 Z    =        -2032988
06
 XDOT =      -7903
761516                 XDOT =       -2409
066510
 YDOT =      13747
111311  feet/sec       YDOT =        4190
119528  meter/sec
 ZDOT =     -18224
952145                 ZDOT =       -5554
965414


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   17190
54206666  
00016717  00000-0  10270-3 0  9123
2 25544  51
6416 286
9016 0005137  13
3149 346
8138 15
54140618 25223


Satellite: ISS
Catalog Number: 25544
Epoch time:      17190
54206666   =   yrday
fracday
Element set:     912
Inclination:       51
6416  deg
RA of node:       286
9016  deg
Eccentricity:     
0005137     
Arg of perigee:    13
3149  deg
Mean anomaly:     346
8138  deg
Mean motion:   15
54140618  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2522
Checksum:              300


Coasting Arc #14 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2017/191/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3721399
41                 A    =         6784070
04  meter
 Y    =       -4483344
04  meter          E    =           
0014582
 Z    =        3458052
22                 I    =           51
27842
 XDOT =       2575
933188                 Wp   =           70
79280
 YDOT =       5637
632278  meter/sec      RA   =          281
27992  deg
 ZDOT =       4526
124311                 TA   =          330
06359
                                          MA   =          330
14690
                                          Ha   =            222
042  n
mi
                                          Hp   =            213
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12209315
66                 X    =         3754459
49
 Y    =      -14709133
98  feet           Y    =        -4441544
39  meter
 Z    =       11345315
68                 Z    =         3476209
12
 XDOT =       8451
224369                 XDOT =        2490
714880
 YDOT =      18496
168892  feet/sec       YDOT =        5665
961080  meter/sec
 ZDOT =      14849
489210                 ZDOT =        4538
430918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18256730
03                 X    =        -5564651
31
 Y    =       -5502246
94  feet           Y    =        -1677084
87  meter
 Z    =       11426254
26                 Z    =         3482722
30
 XDOT =      13426
049944                 XDOT =        4092
260023
 YDOT =     -13526
393541  feet/sec       YDOT =       -4122
844751  meter/sec
 ZDOT =      14902
818559                 ZDOT =        4542
379097


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   17191
57088689  
00016717  00000-0  10270-3 0  9131
2 25544  51
6421 281
7729 0005283  16
9840 343
1489 15
54166057 25383


Satellite: ISS
Catalog Number: 25544
Epoch time:      17191
57088689   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:       281
7729  deg
Eccentricity:     
0005283     
Arg of perigee:    16
9840  deg
Mean anomaly:     343
1489  deg
Mean motion:   15
54166057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2538
Checksum:              338


Coasting Arc #15 (Orbit 2552)
---------------------------------------

Vector Time (GMT): 2017/192/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4018482
44                 A    =         6780379
67  meter
 Y    =        3013804
43  meter          E    =           
0014127
 Z    =       -4568532
05                 I    =           51
25892
 XDOT =      -1687
407765                 Wp   =           53
15493
 YDOT =      -6830
468006  meter/sec      RA   =          276
26717  deg
 ZDOT =      -3019
920332                 TA   =          186
45923
                                          MA   =          186
47746
                                          Ha   =            222
266  n
mi
                                          Hp   =            213
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13183997
52                 X    =        -4029693
60
 Y    =        9887809
80  feet           Y    =         2968804
82  meter
 Z    =      -14988622
20                 Z    =        -4588079
20
 XDOT =      -5536
114716                 XDOT =       -1596
233203
 YDOT =     -22409
671937  feet/sec       YDOT =       -6848
827640  meter/sec
 ZDOT =      -9907
875105                 ZDOT =       -3027
896379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14317711
87                 X    =         4364038
58
 Y    =        7998737
37  feet           Y    =         2438015
15  meter
 Z    =      -15075433
52                 Z    =        -4594992
14
 XDOT =     -17728
835535                 XDOT =       -5403
749071
 YDOT =      12985
659468  feet/sec       YDOT =        3958
029006  meter/sec
 ZDOT =      -9941
898177                 ZDOT =       -3030
290564


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   17192
53540575  
00016717  00000-0  10270-3 0  9146
2 25544  51
6407 276
9657 0005311  20
1239 340
0122 15
54136632 25537


Satellite: ISS
Catalog Number: 25544
Epoch time:      17192
53540575   =   yrday
fracday
Element set:     914
Inclination:       51
6407  deg
RA of node:       276
9657  deg
Eccentricity:     
0005311     
Arg of perigee:    20
1239  deg
Mean anomaly:     340
0122  deg
Mean motion:   15
54136632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2553
Checksum:              287


Coasting Arc #16 (Orbit 2568)
---------------------------------------

Vector Time (GMT): 2017/193/12:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4181359
31                 A    =         6777680
84  meter
 Y    =       -1277719
20  meter          E    =           
0006045
 Z    =        5173661
35                 I    =           51
24778
 XDOT =        807
472857                 Wp   =           64
27735
 YDOT =       7534
234709  meter/sec      RA   =          271
24409  deg
 ZDOT =       1209
575740                 TA   =           14
06946
                                          MA   =           14
05263
                                          Ha   =            222
111  n
mi
                                          Hp   =            213
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13718370
45                 X    =         4170205
63
 Y    =       -4191992
13  feet           Y    =        -1231023
22  meter
 Z    =       16973954
57                 Z    =         5193945
58
 XDOT =       2649
189162                 XDOT =         717
287614
 YDOT =      24718
617811  feet/sec       YDOT =        7542
760056  meter/sec
 ZDOT =       3968
424345                 ZDOT =        1213
279749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9497360
85                 X    =        -2894795
59
 Y    =      -10607134
00  feet           Y    =        -3233054
44  meter
 Z    =       17063717
78                 Z    =         5201021
18
 XDOT =      20582
557284                 XDOT =        6273
563460
 YDOT =     -12028
603492  feet/sec       YDOT =       -3666
318344  meter/sec
 ZDOT =       3983
488655                 ZDOT =        1214
167342


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   17193
56422171  
00016717  00000-0  10270-3 0  9152
2 25544  51
6407 271
8371 0005327  23
3286 336
8107 15
54179487 25696


Satellite: ISS
Catalog Number: 25544
Epoch time:      17193
56422171   =   yrday
fracday
Element set:     915
Inclination:       51
6407  deg
RA of node:       271
8371  deg
Eccentricity:     
0005327     
Arg of perigee:    23
3286  deg
Mean anomaly:     336
8107  deg
Mean motion:   15
54179487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2569
Checksum:              322
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