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

 
Date: July 17th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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


200/11:54:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 212 7

201/17:45:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 212 7

209/14:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 212 4

212/23:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 212 2

Coasting Arc #1 (Orbit 2645)
---------------------------------------

Vector Time (GMT): 2017/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4073830
98                 A    =         6777354
37  meter
 Y    =        1261016
42  meter          E    =           
0018945
 Z    =       -5283439
54                 I    =           51
27478
 XDOT =      -2759
159706                 Wp   =           79
39606
 YDOT =      -7127
389960  meter/sec      RA   =          246
24520  deg
 ZDOT =        431
092960                 TA   =          194
71581
                                          MA   =          194
77103
                                          Ha   =            222
749  n
mi
                                          Hp   =            212
899

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13365587
21                 X    =        -4061964
94
 Y    =        4137192
99  feet           Y    =         1215526
80  meter
 Z    =      -17334119
22                 Z    =        -5303199
99
 XDOT =      -9052
361240                 XDOT =       -2681
348319
 YDOT =     -23383
825327  feet/sec       YDOT =       -7157
809717  meter/sec
 ZDOT =       1414
346982                 ZDOT =         417
878335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9283612
71                 X    =         2829645
16
 Y    =       10321355
55  feet           Y    =         3145949
17  meter
 Z    =      -17421570
86                 Z    =        -5310094
80
 XDOT =     -16724
694407                 XDOT =       -5097
686855
 YDOT =      17307
735470  feet/sec       YDOT =        5275
397771  meter/sec
 ZDOT =       1357
135935                 ZDOT =         413
655033


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   17198
51539231  
00016717  00000-0  10270-3 0  9002
2 25544  51
6401 247
1538 0005822  41
3984 318
7609 15
54149706 26469


Satellite: ISS
Catalog Number: 25544
Epoch time:      17198
51539231   =   yrday
fracday
Element set:     900
Inclination:       51
6401  deg
RA of node:       247
1538  deg
Eccentricity:     
0005822     
Arg of perigee:    41
3984  deg
Mean anomaly:     318
7609  deg
Mean motion:   15
54149706  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2646
Checksum:              315


Coasting Arc #2 (Orbit 2661)
---------------------------------------

Vector Time (GMT): 2017/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4694022
57                 A    =         6778947
17  meter
 Y    =         449460
82  meter          E    =           
0012471
 Z    =        4864314
15                 I    =           51
29386
 XDOT =       1757
096513                 Wp   =           52
66306
 YDOT =       7093
110430  meter/sec      RA   =          241
22230  deg
 ZDOT =      -2339
403972                 TA   =           60
39759
                                          MA   =           60
27340
                                          Ha   =            222
609  n
mi
                                          Hp   =            212
890

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15400336
53                 X    =         4665019
32
 Y    =        1474608
98  feet           Y    =          501789
97  meter
 Z    =       15959035
91                 Z    =         4887045
80
 XDOT =       5764
752338                 XDOT =        1689
012544
 YDOT =      23271
359677  feet/sec       YDOT =        7112
379002  meter/sec
 ZDOT =      -7675
209881                 ZDOT =       -2331
033296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5283782
22                 X    =        -1610496
82
 Y    =      -14429651
13  feet           Y    =        -4398157
66  meter
 Z    =       16059342
39                 Z    =         4894887
56
 XDOT =      17415
256584                 XDOT =        5308
170207
 YDOT =     -14921
219026  feet/sec       YDOT =       -4547
987559  meter/sec
 ZDOT =      -7639
368230                 ZDOT =       -2328
479437


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   17199
54419415  
00016717  00000-0  10270-3 0  9018
2 25544  51
6392 242
0255 0005827  45
3567 314
8060 15
54197938 26620


Satellite: ISS
Catalog Number: 25544
Epoch time:      17199
54419415   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       242
0255  deg
Eccentricity:     
0005827     
Arg of perigee:    45
3567  deg
Mean anomaly:     314
8060  deg
Mean motion:   15
54197938  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2662
Checksum:              322


Coasting Arc #3 (Orbit 2676)
---------------------------------------

Vector Time (GMT): 2017/200/11:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4617083
06                 A    =         6778651
12  meter
 Y    =         256713
78  meter          E    =           
0016685
 Z    =       -4970807
56                 I    =           51
30977
 XDOT =      -2609
573565                 Wp   =           88
20792
 YDOT =      -6892
568222  meter/sec      RA   =          236
23512  deg
 ZDOT =       2074
478924                 TA   =          202
06785
                                          MA   =          202
13977
                                          Ha   =            222
839  n
mi
                                          Hp   =            212
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15147910
31                 X    =        -4595464
90
 Y    =         842236
81  feet           Y    =          205203
83  meter
 Z    =      -16308423
74                 Z    =        -4993183
31
 XDOT =      -8561
593060                 XDOT =       -2542
381866
 YDOT =     -22613
412802  feet/sec       YDOT =       -6921
374773  meter/sec
 ZDOT =       6806
033214                 ZDOT =        2061
964934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7171865
61                 X    =         2185984
64
 Y    =       13247593
87  feet           Y    =         4037866
61  meter
 Z    =      -16407279
94                 Z    =        -5000938
92
 XDOT =     -15821
212291                 XDOT =       -4822
305506
 YDOT =      16900
866104  feet/sec       YDOT =        5151
383989  meter/sec
 ZDOT =       6751
849226                 ZDOT =        2057
963644


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   17200
50869503  
00016717  00000-0  10270-3 0  9025
2 25544  51
6400 237
2168 0005924  48
5888 311
5773 15
54164339 26778


Satellite: ISS
Catalog Number: 25544
Epoch time:      17200
50869503   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       237
2168  deg
Eccentricity:     
0005924     
Arg of perigee:    48
5888  deg
Mean anomaly:     311
5773  deg
Mean motion:   15
54164339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2677
Checksum:              317


Coasting Arc #4 (Orbit 2692)
---------------------------------------

Vector Time (GMT): 2017/201/11:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5242499
39                 A    =         6781852
13  meter
 Y    =        1295898
71  meter          E    =           
0016125
 Z    =        4093860
91                 I    =           51
33931
 XDOT =       1358
689922                 Wp   =           67
70031
 YDOT =       6531
416819  meter/sec      RA   =          231
22039  deg
 ZDOT =      -3789
401662                 TA   =           61
61666
                                          MA   =           61
45419
                                          Ha   =            222
762  n
mi
                                          Hp   =            212
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17199801
14                 X    =         5207732
85
 Y    =        4251636
19  feet           Y    =         1354329
02  meter
 Z    =       13431302
21                 Z    =         4119242
89
 XDOT =       4457
644101                 XDOT =        1303
959840
 YDOT =      21428
532872  feet/sec       YDOT =        6546
305047  meter/sec
 ZDOT =     -12432
420151                 ZDOT =       -3782
933768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3743739
70                 X    =        -1141091
86
 Y    =      -17230072
85  feet           Y    =        -5251726
20  meter
 Z    =       13543206
84                 Z    =         4127969
44
 XDOT =      15961
796513                 XDOT =        4865
155577
 YDOT =     -13264
704529  feet/sec       YDOT =       -4043
081941  meter/sec
 ZDOT =     -12404
867649                 ZDOT =       -3781
003660


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   17201
53749030  
00016717  00000-0  10270-3 0  9032
2 25544  51
6394 232
0882 0006023  52
1764 307
9931 15
54212424 26933


Satellite: ISS
Catalog Number: 25544
Epoch time:      17201
53749030   =   yrday
fracday
Element set:     903
Inclination:       51
6394  deg
RA of node:       232
0882  deg
Eccentricity:     
0006023     
Arg of perigee:    52
1764  deg
Mean anomaly:     307
9931  deg
Mean motion:   15
54212424  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2693
Checksum:              289


Coasting Arc #5 (Orbit 2696)
---------------------------------------

Vector Time (GMT): 2017/201/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          50278
77                 A    =         6781325
86  meter
 Y    =       -5258377
01  meter          E    =           
0014153
 Z    =        4269007
65                 I    =           51
34164
 XDOT =       6148
225238                 Wp   =           87
02791
 YDOT =       2936
306435  meter/sec      RA   =          230
05026  deg
 ZDOT =       3534
972437                 TA   =          326
78797
                                          MA   =          326
87673
                                          Ha   =            222
798  n
mi
                                          Hp   =            212
717

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         164956
60                 X    =           88339
02
 Y    =      -17251893
06  feet           Y    =        -5257602
46  meter
 Z    =       14005930
62                 Z    =         4269343
70
 XDOT =      20171
342645                 XDOT =        6097
762718
 YDOT =       9633
551295  feet/sec       YDOT =        3004
777483  meter/sec
 ZDOT =      11597
678600                 ZDOT =        3564
716161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7006289
70                 X    =         2135517
10
 Y    =       15763962
63  feet           Y    =         4804855
81  meter
 Z    =       14008229
88                 Z    =         4269708
47
 XDOT =     -21129
030418                 XDOT =       -6440
128471
 YDOT =      -1059
004948  feet/sec       YDOT =        -322
784708  meter/sec
 ZDOT =      11728
598474                 ZDOT =        3574
876815


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   17201
79468917  
00016717  00000-0  10270-3 0  9043
2 25544  51
6387 230
8063 0005932  51
7991 308
3695 15
54215848 26976


Satellite: ISS
Catalog Number: 25544
Epoch time:      17201
79468917   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:       230
8063  deg
Eccentricity:     
0005932     
Arg of perigee:    51
7991  deg
Mean anomaly:     308
3695  deg
Mean motion:   15
54215848  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2697
Checksum:              343


Coasting Arc #6 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2017/202/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1439004
93                 A    =         6778261
94  meter
 Y    =        4289774
10  meter          E    =           
0018958
 Z    =       -5064197
56                 I    =           51
35223
 XDOT =      -6169
470025                 Wp   =           69
92676
 YDOT =      -4167
342194  meter/sec      RA   =          225
03535  deg
 ZDOT =      -1776
049156                 TA   =          182
78388
                                          MA   =          182
79445
                                          Ha   =            222
949  n
mi
                                          Hp   =            212
557

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4721144
78                 X    =        -1462268
31
 Y    =       14074061
99  feet           Y    =         4273552
70  meter
 Z    =      -16614821
39                 Z    =        -5071243
69
 XDOT =     -20241
043390                 XDOT =       -6113
784121
 YDOT =     -13672
382526  feet/sec       YDOT =       -4236
021821  meter/sec
 ZDOT =      -5826
932925                 ZDOT =       -1805
883388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1816379
52                 X    =         -553632
48
 Y    =      -14697346
94  feet           Y    =        -4479751
35  meter
 Z    =      -16646605
57                 Z    =        -5073885
38
 XDOT =      23029
093691                 XDOT =        7019
267757
 YDOT =       3905
737092  feet/sec       YDOT =        1190
468666  meter/sec
 ZDOT =      -5958
087593                 ZDOT =       -1816
025098


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   17202
75918419  
00016717  00000-0  10270-3 0  9058
2 25544  51
6380 225
9977 0006098  54
9009 305
2715 15
54195156 27123


Satellite: ISS
Catalog Number: 25544
Epoch time:      17202
75918419   =   yrday
fracday
Element set:     905
Inclination:       51
6380  deg
RA of node:       225
9977  deg
Eccentricity:     
0006098     
Arg of perigee:    54
9009  deg
Mean anomaly:     305
2715  deg
Mean motion:   15
54195156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              325


Coasting Arc #7 (Orbit 2727)
---------------------------------------

Vector Time (GMT): 2017/203/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2860773
08                 A    =         6777065
80  meter
 Y    =       -3115979
27  meter          E    =           
0008141
 Z    =        5288505
83                 I    =           51
37258
 XDOT =       5791
460661                 Wp   =           65
20012
 YDOT =       5033
305916  meter/sec      RA   =          220
01695  deg
 ZDOT =       -163
673514                 TA   =           26
38487
                                          MA   =           26
34344
                                          Ha   =            222
745  n
mi
                                          Hp   =            212
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9385738
47                 X    =         2869715
68
 Y    =      -10223029
09  feet           Y    =        -3083938
74  meter
 Z    =       17350740
92                 Z    =         5302423
71
 XDOT =      19000
855186                 XDOT =        5735
541507
 YDOT =      16513
470853  feet/sec       YDOT =        5097
757315  meter/sec
 ZDOT =       -536
986595                 ZDOT =        -135
676167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3811731
57                 X    =        -1161815
78
 Y    =       13263448
06  feet           Y    =         4042698
97  meter
 Z    =       17412704
25                 Z    =         5307392
25
 XDOT =     -23372
518207                 XDOT =       -7123
943550
 YDOT =      -6158
109510  feet/sec       YDOT =       -1876
991779  meter/sec
 ZDOT =       -414
051177                 ZDOT =        -126
202799


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   17203
78797372  
00016717  00000-0  10270-3 0  9066
2 25544  51
6382 220
8694 0005900  57
2705 302
9016 15
54225249 27287


Satellite: ISS
Catalog Number: 25544
Epoch time:      17203
78797372   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:       220
8694  deg
Eccentricity:     
0005900     
Arg of perigee:    57
2705  deg
Mean anomaly:     302
9016  deg
Mean motion:   15
54225249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2728
Checksum:              317


Coasting Arc #8 (Orbit 2742)
---------------------------------------

Vector Time (GMT): 2017/204/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4209942
93                 A    =         6778535
63  meter
 Y    =        1901202
71  meter          E    =           
0017592
 Z    =       -4976299
87                 I    =           51
40333
 XDOT =      -4926
739875                 Wp   =           91
60085
 YDOT =      -5477
549132  meter/sec      RA   =          214
99894  deg
 ZDOT =       2081
217427                 TA   =          198
72200
                                          MA   =          198
78678
                                          Ha   =            222
978  n
mi
                                          Hp   =            212
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13812148
73                 X    =        -4206717
90
 Y    =        6237541
69  feet           Y    =         1854142
75  meter
 Z    =      -16326443
13                 Z    =        -4996742
02
 XDOT =     -16163
844733                 XDOT =       -4875
231624
 YDOT =     -17970
961718  feet/sec       YDOT =       -5532
355469  meter/sec
 ZDOT =       6828
141164                 ZDOT =        2057
409983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9346547
51                 X    =         2848827
68
 Y    =      -11804974
46  feet           Y    =        -3598156
21  meter
 Z    =      -16417056
74                 Z    =        -5003918
89
 XDOT =      21763
680501                 XDOT =        6633
569817
 YDOT =       7907
463961  feet/sec       YDOT =        2410
195015  meter/sec
 ZDOT =       6723
758072                 ZDOT =        2049
401460


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   17204
75246224  
00016717  00000-0  10270-3 0  9070
2 25544  51
6386 216
0598 0006094  61
1448 299
0316 15
54200760 27431


Satellite: ISS
Catalog Number: 25544
Epoch time:      17204
75246224   =   yrday
fracday
Element set:     907
Inclination:       51
6386  deg
RA of node:       216
0598  deg
Eccentricity:     
0006094     
Arg of perigee:    61
1448  deg
Mean anomaly:     299
0316  deg
Mean motion:   15
54200760  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2743
Checksum:              305


Coasting Arc #9 (Orbit 2758)
---------------------------------------

Vector Time (GMT): 2017/205/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5356573
04                 A    =         6781890
14  meter
 Y    =        -676321
92  meter          E    =           
0016477
 Z    =        4094011
80                 I    =           51
44160
 XDOT =       3625
808593                 Wp   =           72
46182
 YDOT =       5592
300577  meter/sec      RA   =          209
99127  deg
 ZDOT =      -3802
620924                 TA   =           56
94332
                                          MA   =           56
78517
                                          Ha   =            222
929  n
mi
                                          Hp   =            212
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17574058
54                 X    =         5343851
50
 Y    =       -2218903
93  feet           Y    =         -616492
48  meter
 Z    =       13431797
24                 Z    =         4120000
83
 XDOT =      11895
697485                 XDOT =        3581
475378
 YDOT =      18347
442837  feet/sec       YDOT =        5632
599194  meter/sec
 ZDOT =     -12475
790432                 ZDOT =       -3785
115589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14371425
66                 X    =        -4380410
54
 Y    =       10204502
75  feet           Y    =         3110332
44  meter
 Z    =       13546752
15                 Z    =         4129050
05
 XDOT =     -18471
501552                 XDOT =       -5630
113673
 YDOT =      -9478
174758  feet/sec       YDOT =       -2888
947666  meter/sec
 ZDOT =     -12399
250070                 ZDOT =       -3779
291421


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   17205
78124664  
00016717  00000-0  10270-3 0  9088
2 25544  51
6383 210
9312 0006116  65
1568 295
0220 15
54197320 27591


Satellite: ISS
Catalog Number: 25544
Epoch time:      17205
78124664   =   yrday
fracday
Element set:     908
Inclination:       51
6383  deg
RA of node:       210
9312  deg
Eccentricity:     
0006116     
Arg of perigee:    65
1568  deg
Mean anomaly:     295
0220  deg
Mean motion:   15
54197320  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2759
Checksum:              303


Coasting Arc #10 (Orbit 2773)
---------------------------------------

Vector Time (GMT): 2017/206/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6162758
94                 A    =         6785623
48  meter
 Y    =        -402200
50  meter          E    =           
0010662
 Z    =       -2813779
78                 I    =           51
48379
 XDOT =      -1962
950860                 Wp   =           66
27931
 YDOT =      -5383
346391  meter/sec      RA   =          204
99506  deg
 ZDOT =       5088
264841                 TA   =          261
72252
                                          MA   =          261
84343
                                          Ha   =            222
951  n
mi
                                          Hp   =            212
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20219025
40                 X    =        -6144135
74
 Y    =       -1319555
44  feet           Y    =         -471012
41  meter
 Z    =       -9231560
97                 Z    =        -2843670
69
 XDOT =      -6440
127493                 XDOT =       -1927
322724
 YDOT =     -17661
897609  feet/sec       YDOT =       -5405
098435  meter/sec
 ZDOT =      16693
782287                 ZDOT =        5078
815961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18250609
87                 X    =         5562785
89
 Y    =       -8660822
19  feet           Y    =        -2639818
60  meter
 Z    =       -9363617
42                 Z    =        -2854030
59
 XDOT =      13687
233341                 XDOT =        4171
868722
 YDOT =      10906
657492  feet/sec       YDOT =        3324
349204  meter/sec
 ZDOT =      16652
800124                 ZDOT =        5075
773478


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   17206
74572948  
00016717  00000-0  10270-3 0  9098
2 25544  51
6391 206
1224 0006026  68
5034 291
6761 15
54213673 27743


Satellite: ISS
Catalog Number: 25544
Epoch time:      17206
74572948   =   yrday
fracday
Element set:     909
Inclination:       51
6391  deg
RA of node:       206
1224  deg
Eccentricity:     
0006026     
Arg of perigee:    68
5034  deg
Mean anomaly:     291
6761  deg
Mean motion:   15
54213673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2774
Checksum:              315


Coasting Arc #11 (Orbit 2789)
---------------------------------------

Vector Time (GMT): 2017/207/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6534305
11                 A    =         6788503
57  meter
 Y    =        1385230
98  meter          E    =           
0018257
 Z    =        1175765
55                 I    =           51
52413
 XDOT =         15
052022                 Wp   =          107
60961
 YDOT =       4956
271825  meter/sec      RA   =          200
01096  deg
 ZDOT =      -5853
293977                 TA   =           59
59666
                                          MA   =           59
41635
                                          Ha   =            223
040  n
mi
                                          Hp   =            212
385

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21438008
89                 X    =         6512618
27
 Y    =        4544721
08  feet           Y    =         1458180
74  meter
 Z    =        3857498
52                 Z    =         1207453
93
 XDOT =         49
383275                 XDOT =         -11
939550
 YDOT =      16260
734334  feet/sec       YDOT =        4956
289353  meter/sec
 ZDOT =     -19203
720396                 ZDOT =       -5853
286311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20801920
65                 X    =        -6340425
41
 Y    =        6813523
72  feet           Y    =         2076762
03  meter
 Z    =        3997374
34                 Z    =         1218399
70
 XDOT =      -7813
578957                 XDOT =       -2381
578866
 YDOT =     -12458
960977  feet/sec       YDOT =       -3797
491306  meter/sec
 ZDOT =     -19204
397342                 ZDOT =       -5853
500310


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   17207
77450794  
00016717  00000-0  10270-3 0  9108
2 25544  51
6401 200
9931 0006030  72
6283 287
5529 15
54197222 27904


Satellite: ISS
Catalog Number: 25544
Epoch time:      17207
77450794   =   yrday
fracday
Element set:     910
Inclination:       51
6401  deg
RA of node:       200
9931  deg
Eccentricity:     
0006030     
Arg of perigee:    72
6283  deg
Mean anomaly:     287
5529  deg
Mean motion:   15
54197222  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2790
Checksum:              306


Coasting Arc #12 (Orbit 2805)
---------------------------------------

Vector Time (GMT): 2017/208/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6405873
58                 A    =         6788996
59  meter
 Y    =       -2159840
70  meter          E    =           
0018674
 Z    =         534566
24                 I    =           51
55711
 XDOT =       1987
214696                 Wp   =           58
42346
 YDOT =      -4378
887880  meter/sec      RA   =          195
03346  deg
 ZDOT =       5976
831944                 TA   =          307
35297
                                          MA   =          307
52293
                                          Ha   =            223
054  n
mi
                                          Hp   =            212
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21016645
61                 X    =        -6383842
20
 Y    =       -7086091
53  feet           Y    =        -2231352
35  meter
 Z    =        1753826
23                 Z    =          503502
46
 XDOT =       6519
733255                 XDOT =        2007
000822
 YDOT =     -14366
430051  feet/sec       YDOT =       -4356
554934  meter/sec
 ZDOT =      19609
028687                 ZDOT =        5986
533070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21664982
71                 X    =         6603486
73
 Y    =       -4796087
51  feet           Y    =        -1461847
47  meter
 Z    =        1616805
78                 Z    =          492802
40
 XDOT =       1599
021390                 XDOT =         487
381720
 YDOT =      14021
296405  feet/sec       YDOT =        4273
691144  meter/sec
 ZDOT =      19652
538454                 ZDOT =        5990
093721


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   17208
80328277  
00016717  00000-0  10270-3 0  9114
2 25544  51
6405 195
8639 0006089  74
6137 285
5688 15
54209143 28067


Satellite: ISS
Catalog Number: 25544
Epoch time:      17208
80328277   =   yrday
fracday
Element set:     911
Inclination:       51
6405  deg
RA of node:       195
8639  deg
Eccentricity:     
0006089     
Arg of perigee:    74
6137  deg
Mean anomaly:     285
5688  deg
Mean motion:   15
54209143  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2806
Checksum:              335


Coasting Arc #13 (Orbit 2818)
---------------------------------------

Vector Time (GMT): 2017/209/14:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3208823
83                 A    =         6781121
69  meter
 Y    =        4114988
57  meter          E    =           
0014620
 Z    =       -4345268
50                 I    =           51
55686
 XDOT =      -6653
748882                 Wp   =           73
48537
 YDOT =       1540
751787  meter/sec      RA   =          190
67545  deg
 ZDOT =      -3460
070207                 TA   =          161
30121
                                          MA   =          161
24744
                                          Ha   =            223
055  n
mi
                                          Hp   =            212
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10527637
25                 X    =         3183677
37
 Y    =       13500618
68  feet           Y    =         4150731
27  meter
 Z    =      -14256130
24                 Z    =        -4329742
26
 XDOT =     -21829
884783                 XDOT =       -6653
676349
 YDOT =       5054
959931  feet/sec       YDOT =        1466
345489  meter/sec
 ZDOT =     -11351
936374                 ZDOT =       -3492
391450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7472727
64                 X    =        -2277687
39
 Y    =      -15465839
05  feet           Y    =        -4713987
74  meter
 Z    =      -14188067
67                 Z    =        -4324523
03
 XDOT =      21205
100316                 XDOT =        6463
314576
 YDOT =        282
558509  feet/sec       YDOT =          86
123833  meter/sec
 ZDOT =     -11495
054106                 ZDOT =       -3503
692492


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   17209
63916032  
00016717  00000-0  10270-3 0  9129
2 25544  51
6386 191
6957 0006102  77
9323 282
2513 15
54231156 28195


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
63916032   =   yrday
fracday
Element set:     912
Inclination:       51
6386  deg
RA of node:       191
6957  deg
Eccentricity:     
0006102     
Arg of perigee:    77
9323  deg
Mean anomaly:     282
2513  deg
Mean motion:   15
54231156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2819
Checksum:              308


Coasting Arc #14 (Orbit 2834)
---------------------------------------

Vector Time (GMT): 2017/210/14:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1504106
22                 A    =         6777956
53  meter
 Y    =       -4206244
05  meter          E    =           
0010333
 Z    =        5089490
48                 I    =           51
57953
 XDOT =       7461
043349                 Wp   =          102
67703
 YDOT =       -609
993661  meter/sec      RA   =          185
67657  deg
 ZDOT =       1695
716918                 TA   =          330
91581
                                          MA   =          330
97333
                                          Ha   =            222
952  n
mi
                                          Hp   =            212
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4934731
71                 X    =        -1481681
10
 Y    =      -13800013
30  feet           Y    =        -4222938
69  meter
 Z    =       16697803
42                 Z    =         5082238
47
 XDOT =      24478
488677                 XDOT =        7459
073063
 YDOT =      -2001
291540  feet/sec       YDOT =        -526
570249  meter/sec
 ZDOT =       5563
375715                 ZDOT =        1731
955193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2212026
09                 X    =          674225
55
 Y    =       14524081
27  feet           Y    =         4426939
97  meter
 Z    =       16666330
94                 Z    =         5079897
67
 XDOT =     -23294
701257                 XDOT =       -7100
224943
 YDOT =      -3039
456263  feet/sec       YDOT =        -926
426269  meter/sec
 ZDOT =       5723
696880                 ZDOT =        1744
582809


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   17210
66792859  
00016717  00000-0  10270-3 0  9134
2 25544  51
6392 186
5674 0005825  81
9981 278
1833 15
54264317 28359


Satellite: ISS
Catalog Number: 25544
Epoch time:      17210
66792859   =   yrday
fracday
Element set:     913
Inclination:       51
6392  deg
RA of node:       186
5674  deg
Eccentricity:     
0005825     
Arg of perigee:    81
9981  deg
Mean anomaly:     278
1833  deg
Mean motion:   15
54264317  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2835
Checksum:              347


Coasting Arc #15 (Orbit 2849)
---------------------------------------

Vector Time (GMT): 2017/211/14:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -354177
35                 A    =         6777087
52  meter
 Y    =        4209393
21  meter          E    =           
0020868
 Z    =       -5317535
86                 I    =           51
60905
 XDOT =      -7642
406034                 Wp   =           90
04909
 YDOT =       -303
417239  meter/sec      RA   =          180
67230  deg
 ZDOT =        269
739430                 TA   =          182
52297
                                          MA   =          182
53352
                                          Ha   =            223
052  n
mi
                                          Hp   =            212
263

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1161999
17                 X    =         -375391
80
 Y    =       13810345
17  feet           Y    =         4205314
08  meter
 Z    =      -17445983
78                 Z    =        -5319307
74
 XDOT =     -25073
510609                 XDOT =       -7639
755396
 YDOT =       -995
463381  feet/sec       YDOT =        -388
865003  meter/sec
 ZDOT =        884
971882                 ZDOT =         232
621729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3531289
97                 X    =         1076337
18
 Y    =      -13390730
68  feet           Y    =        -4081494
71  meter
 Z    =      -17454413
45                 Z    =        -5320105
22
 XDOT =      23507
311695                 XDOT =        7165
028605
 YDOT =       5263
359836  feet/sec       YDOT =        1604
272078  meter/sec
 ZDOT =        720
872086                 ZDOT =         219
721812


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   17211
63239795  
00016717  00000-0  10270-3 0  9148
2 25544  51
6394 181
7581 0006055  84
3911 275
7932 15
54228484 28506


Satellite: ISS
Catalog Number: 25544
Epoch time:      17211
63239795   =   yrday
fracday
Element set:     914
Inclination:       51
6394  deg
RA of node:       181
7581  deg
Eccentricity:     
0006055     
Arg of perigee:    84
3911  deg
Mean anomaly:     275
7932  deg
Mean motion:   15
54228484  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2850
Checksum:              328


Coasting Arc #16 (Orbit 2865)
---------------------------------------

Vector Time (GMT): 2017/212/14:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2192257
83                 A    =         6778578
19  meter
 Y    =       -4083955
97  meter          E    =           
0011915
 Z    =        4937528
41                 I    =           51
64649
 XDOT =       7249
799327                 Wp   =           72
72338
 YDOT =       1207
186928  meter/sec      RA   =          175
67313  deg
 ZDOT =      -2212
541247                 TA   =           38
88648
                                          MA   =           38
80083
                                          Ha   =            222
975  n
mi
                                          Hp   =            212
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7192446
95                 X    =         2213778
87
 Y    =      -13398805
68  feet           Y    =        -4059320
50  meter
 Z    =       16199240
21                 Z    =         4948229
76
 XDOT =      23785
430864                 XDOT =        7246
508782
 YDOT =       3960
587034  feet/sec       YDOT =        1288
240794  meter/sec
 ZDOT =      -7258
993591                 ZDOT =       -2177
332188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9189442
42                 X    =        -2800942
05
 Y    =       12052345
66  feet           Y    =         3673554
96  meter
 Z    =       16247146
89                 Z    =         4952130
37
 XDOT =     -21980
171294                 XDOT =       -6699
556210
 YDOT =      -7148
542931  feet/sec       YDOT =       -2178
875885  meter/sec
 ZDOT =      -7103
442601                 ZDOT =       -2165
129305


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   17212
66116107  
00016717  00000-0  10270-3 0  9154
2 25544  51
6390 176
6301 0006033  87
9619 272
2225 15
54238803 28665


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
66116107   =   yrday
fracday
Element set:     915
Inclination:       51
6390  deg
RA of node:       176
6301  deg
Eccentricity:     
0006033     
Arg of perigee:    87
9619  deg
Mean anomaly:     272
2225  deg
Mean motion:   15
54238803  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2866
Checksum:              303


Coasting Arc #17 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2600366
67                 A    =         6779329
17  meter
 Y    =        4072981
67  meter          E    =           
0017291
 Z    =       -4771116
96                 I    =           51
65909
 XDOT =      -7041
537191                 Wp   =          103
97654
 YDOT =      -1371
755046  meter/sec      RA   =          173
89887  deg
 ZDOT =       2670
821692                 TA   =          192
41509
                                          MA   =          192
45774
                                          Ha   =            223
062  n
mi
                                          Hp   =            212
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8531386
71                 X    =        -2622543
00
 Y    =       13362800
74  feet           Y    =         4043778
80  meter
 Z    =      -15653270
86                 Z    =        -4783802
33
 XDOT =     -23102
156139                 XDOT =       -7038
647964
 YDOT =      -4500
508682  feet/sec       YDOT =       -1450
482254  meter/sec
 ZDOT =       8762
538361                 ZDOT =        2636
623315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15764558
40                 X    =        -4805037
40
 Y    =       -1024664
21  feet           Y    =         -312317
65  meter
 Z    =      -15709953
95                 Z    =        -4788393
96
 XDOT =      -7180
924549                 XDOT =       -2188
745803
 YDOT =     -21346
888793  feet/sec       YDOT =       -6506
531704  meter/sec
 ZDOT =       8611
473783                 ZDOT =        2624
777209


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   17212
98264874  
00016717  00000-0  10270-3 0  9165
2 25544  51
6375 175
0227 0006118  94
3323 265
8529 15
54235071 28711


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
98264874   =   yrday
fracday
Element set:     916
Inclination:       51
6375  deg
RA of node:       175
0227  deg
Eccentricity:     
0006118     
Arg of perigee:    94
3323  deg
Mean anomaly:     265
8529  deg
Mean motion:   15
54235071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              320
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