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

 
Date: July 23rd 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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


217/02:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 212 7

Coasting Arc #1 (Orbit 1047)
---------------------------------------

Vector Time (GMT): 2016/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          65021
58                 A    =         6781780
48  meter
 Y    =       -5758015
45  meter          E    =           
0013903
 Z    =        3570225
54                 I    =           51
31654
 XDOT =       5611
910116                 Wp   =           89
58174
 YDOT =       2810
282986  meter/sec      RA   =          240
88330  deg
 ZDOT =       4415
361501                 TA   =          312
87543
                                          MA   =          312
99209
                                          Ha   =            220
521  n
mi
                                          Hp   =            212
825

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         213325
41                 X    =          112062
07
 Y    =      -18891126
82  feet           Y    =        -5757025
49  meter
 Z    =       11713338
39                 Z    =         3570655
37
 XDOT =      18411
778597                 XDOT =        5558
620254
 YDOT =       9220
088536  feet/sec       YDOT =        2872
740937  meter/sec
 ZDOT =      14486
094162                 ZDOT =        4442
492901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16457724
26                 X    =        -5016314
36
 Y    =        9273400
38  feet           Y    =         2826532
44  meter
 Z    =       11716220
97                 Z    =         3571104
15
 XDOT =       -431
436121                 XDOT =        -131
501730
 YDOT =     -19277
945340  feet/sec       YDOT =       -5875
917740  meter/sec
 ZDOT =      14603
856530                 ZDOT =        4451
255470


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   16204
55673918  
00016717  00000-0  10270-3 0  9004
2 25544  51
6408 241
5667 0002010  67
6285 292
5081 15
54862507 10487


Satellite: ISS
Catalog Number: 25544
Epoch time:      16204
55673918   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       241
5667  deg
Eccentricity:     
0002010     
Arg of perigee:    67
6285  deg
Mean anomaly:     292
5081  deg
Mean motion:   15
54862507  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1048
Checksum:              305


Coasting Arc #2 (Orbit 1062)
---------------------------------------

Vector Time (GMT): 2016/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1475678
75                 A    =         6777559
79  meter
 Y    =        4609794
67  meter          E    =           
0013065
 Z    =       -4756732
95                 I    =           51
31975
 XDOT =      -5603
355053                 Wp   =           71
57772
 YDOT =      -4508
771455  meter/sec      RA   =          235
86570  deg
 ZDOT =      -2633
081474                 TA   =          172
30337
                                          MA   =          172
28330
                                          Ha   =            220
495  n
mi
                                          Hp   =            212
778

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4841465
71                 X    =        -1504011
22
 Y    =       15123998
26  feet           Y    =         4593134
38  meter
 Z    =      -15606079
25                 Z    =        -4763969
97
 XDOT =     -18383
710803                 XDOT =       -5539
730241
 YDOT =     -14792
557266  feet/sec       YDOT =       -4571
076083  meter/sec
 ZDOT =      -8638
718748                 ZDOT =       -2660
146280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15416845
52                 X    =         4699054
51
 Y    =       -3672255
76  feet           Y    =        -1119303
56  meter
 Z    =      -15638421
75                 Z    =        -4766590
95
 XDOT =      -3588
979079                 XDOT =       -1093
920823
 YDOT =      22193
412421  feet/sec       YDOT =        6764
552106  meter/sec
 ZDOT =      -8755
912163                 ZDOT =       -2668
802027


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   16205
52080819  
00016717  00000-0  10270-3 0  9015
2 25544  51
6415 236
7557 0001884  71
4460 288
6898 15
54868746 10635


Satellite: ISS
Catalog Number: 25544
Epoch time:      16205
52080819   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       236
7557  deg
Eccentricity:     
0001884     
Arg of perigee:    71
4460  deg
Mean anomaly:     288
6898  deg
Mean motion:   15
54868746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1063
Checksum:              334


Coasting Arc #3 (Orbit 1078)
---------------------------------------

Vector Time (GMT): 2016/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2908094
17                 A    =         6775225
51  meter
 Y    =       -3106117
52  meter          E    =           
0004558
 Z    =        5268557
25                 I    =           51
32998
 XDOT =       5142
317159                 Wp   =           96
60319
 YDOT =       5673
254541  meter/sec      RA   =          230
83840  deg
 ZDOT =        505
404686                 TA   =          348
55257
                                          MA   =          348
56293
                                          Ha   =            220
412  n
mi
                                          Hp   =            212
758

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9540991
36                 X    =         2917019
42
 Y    =      -10190674
28  feet           Y    =        -3073547
47  meter
 Z    =       17285292
81                 Z    =         5282705
45
 XDOT =      16871
119287                 XDOT =        5076
040207
 YDOT =      18613
039834  feet/sec       YDOT =        5730
388779  meter/sec
 ZDOT =       1658
151858                 ZDOT =         530
223543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13627837
71                 X    =        -4153764
93
 Y    =       -2647270
68  feet           Y    =         -806888
10  meter
 Z    =       17347498
47                 Z    =         5287517
53
 XDOT =       6746
462497                 XDOT =        2056
321769
 YDOT =     -23142
441762  feet/sec       YDOT =       -7053
816249  meter/sec
 ZDOT =       1765
373027                 ZDOT =         538
085699


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   16206
54914351  
00016717  00000-0  10270-3 0  9026
2 25544  51
6404 231
6237 0002020  73
7837 286
3538 15
54889183 10799


Satellite: ISS
Catalog Number: 25544
Epoch time:      16206
54914351   =   yrday
fracday
Element set:     902
Inclination:       51
6404  deg
RA of node:       231
6237  deg
Eccentricity:     
0002020     
Arg of perigee:    73
7837  deg
Mean anomaly:     286
3538  deg
Mean motion:   15
54889183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1079
Checksum:              309


Coasting Arc #4 (Orbit 1093)
---------------------------------------

Vector Time (GMT): 2016/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4255666
59                 A    =         6776111
61  meter
 Y    =        1452375
18  meter          E    =           
0015076
 Z    =       -5082624
54                 I    =           51
35582
 XDOT =      -4145
214448                 Wp   =           99
36042
 YDOT =      -6211
571960  meter/sec      RA   =          225
81039  deg
 ZDOT =       1697
713587                 TA   =          187
11795
                                          MA   =          187
13938
                                          Ha   =            220
481  n
mi
                                          Hp   =            212
685

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13962160
73                 X    =        -4246902
20
 Y    =        4765010
44  feet           Y    =         1404834
57  meter
 Z    =      -16675277
37                 Z    =        -5103275
97
 XDOT =     -13599
784935                 XDOT =       -4083
693674
 YDOT =     -20379
173096  feet/sec       YDOT =       -6257
582563  meter/sec
 ZDOT =       5569
926466                 ZDOT =        1677
726706

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11504847
58                 X    =         3506677
54
 Y    =        9070106
36  feet           Y    =         2764568
42  meter
 Z    =      -16765553
53                 Z    =        -5110140
72
 XDOT =      -9091
883468                 XDOT =       -2771
206081
 YDOT =      21657
492728  feet/sec       YDOT =        6601
203783  meter/sec
 ZDOT =       5483
844424                 ZDOT =        1671
475780


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   16207
51320209  
00016717  00000-0  10270-3 0  9038
2 25544  51
6423 226
8128 0001869  72
5108 287
6249 15
54873917 10941


Satellite: ISS
Catalog Number: 25544
Epoch time:      16207
51320209   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:       226
8128  deg
Eccentricity:     
0001869     
Arg of perigee:    72
5108  deg
Mean anomaly:     287
6249  deg
Mean motion:   15
54873917  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1094
Checksum:              313


Coasting Arc #5 (Orbit 1109)
---------------------------------------

Vector Time (GMT): 2016/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5333086
24                 A    =         6779489
18  meter
 Y    =         200420
74  meter          E    =           
0012195
 Z    =        4172773
44                 I    =           51
38907
 XDOT =       2660
374353                 Wp   =           74
93222
 YDOT =       6182
631879  meter/sec      RA   =          220
79111  deg
 ZDOT =      -3684
962036                 TA   =           53
04407
                                          MA   =           52
93246
                                          Ha   =            220
353  n
mi
                                          Hp   =            212
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17497002
09                 X    =         5310179
34
 Y    =         657548
35  feet           Y    =          259930
68  meter
 Z    =       13690201
56                 Z    =         4198624
40
 XDOT =       8728
262312                 XDOT =        2608
940698
 YDOT =      20284
225324  feet/sec       YDOT =        6212
094476  meter/sec
 ZDOT =     -12089
770460                 ZDOT =       -3672
163464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9126247
73                 X    =        -2781680
31
 Y    =      -14838844
66  feet           Y    =        -4522879
85  meter
 Z    =       13802875
14                 Z    =         4207116
34
 XDOT =      10887
079581                 XDOT =        3318
381856
 YDOT =     -17927
325571  feet/sec       YDOT =       -5464
248834  meter/sec
 ZDOT =     -12035
008939                 ZDOT =       -3668
270725


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   16208
54152585  
00016717  00000-0  10270-3 0  9043
2 25544  51
6405 221
6809 0002042  75
1654 284
9726 15
54926265 11103


Satellite: ISS
Catalog Number: 25544
Epoch time:      16208
54152585   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       221
6809  deg
Eccentricity:     
0002042     
Arg of perigee:    75
1654  deg
Mean anomaly:     284
9726  deg
Mean motion:   15
54926265  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1110
Checksum:              300


Coasting Arc #6 (Orbit 1124)
---------------------------------------

Vector Time (GMT): 2016/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5993584
87                 A    =         6783803
49  meter
 Y    =       -1649700
62  meter          E    =           
0006710
 Z    =       -2716937
59                 I    =           51
42851
 XDOT =       -780
181405                 Wp   =           65
11031
 YDOT =      -5624
136988  meter/sec      RA   =          215
78731  deg
 ZDOT =       5148
787156                 TA   =          264
07730
                                          MA   =          264
15379
                                          Ha   =            220
447  n
mi
                                          Hp   =            212
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19663992
36                 X    =        -5961494
42
 Y    =       -5412403
62  feet           Y    =        -1716545
35  meter
 Z    =       -8913837
23                 Z    =        -2745974
87
 XDOT =      -2559
650279                 XDOT =        -742
243332
 YDOT =     -18451
893006  feet/sec       YDOT =       -5632
649592  meter/sec
 ZDOT =      16892
346312                 ZDOT =        5145
089161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6726073
40                 X    =         2050107
17
 Y    =       19195270
40  feet           Y    =         5850718
42  meter
 Z    =       -9040173
32                 Z    =        -2755444
83
 XDOT =     -12239
764867                 XDOT =       -3730
680331
 YDOT =      12217
823980  feet/sec       YDOT =        3723
992749  meter/sec
 ZDOT =      16877
161791                 ZDOT =        5144
158914


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   16209
50557597  
00016717  00000-0  10270-3 0  9053
2 25544  51
6406 216
8705 0002026  80
3441 279
7941 15
54920077 11251


Satellite: ISS
Catalog Number: 25544
Epoch time:      16209
50557597   =   yrday
fracday
Element set:     905
Inclination:       51
6406  deg
RA of node:       216
8705  deg
Eccentricity:     
0002026     
Arg of perigee:    80
3441  deg
Mean anomaly:     279
7941  deg
Mean motion:   15
54920077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1125
Checksum:              308


Coasting Arc #7 (Orbit 1140)
---------------------------------------

Vector Time (GMT): 2016/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6094315
88                 A    =         6786690
11  meter
 Y    =        2849057
00  meter          E    =           
0014970
 Z    =         844802
88                 I    =           51
46395
 XDOT =      -1357
997286                 Wp   =          120
25860
 YDOT =       4682
128854  meter/sec      RA   =          210
79597  deg
 ZDOT =      -5922
681179                 TA   =           50
57580
                                          MA   =           50
44338
                                          Ha   =            220
488  n
mi
                                          Hp   =            212
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19994474
68                 X    =         6057900
41
 Y    =        9347299
87  feet           Y    =         2917004
05  meter
 Z    =        2771662
98                 Z    =          874319
05
 XDOT =      -4455
371673                 XDOT =       -1381
483477
 YDOT =      15361
315139  feet/sec       YDOT =        4666
811857  meter/sec
 ZDOT =     -19431
368697                 ZDOT =       -5929
334708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4077665
35                 X    =        -1242872
40
 Y    =      -21674786
05  feet           Y    =        -6606474
79  meter
 Z    =        2899903
99                 Z    =          883890
74
 XDOT =      13416
293477                 XDOT =        4089
286252
 YDOT =      -5157
580608  feet/sec       YDOT =       -1572
030569  meter/sec
 ZDOT =     -19461
162794                 ZDOT =       -5931
762420


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   16210
53388975  
00016717  00000-0  10270-3 0  9061
2 25544  51
6398 211
7377 0002067  80
3383 279
8003 15
54923549 11415


Satellite: ISS
Catalog Number: 25544
Epoch time:      16210
53388975   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       211
7377  deg
Eccentricity:     
0002067     
Arg of perigee:    80
3383  deg
Mean anomaly:     279
8003  deg
Mean motion:   15
54923549  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1141
Checksum:              320


Coasting Arc #8 (Orbit 1156)
---------------------------------------

Vector Time (GMT): 2016/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5585353
95                 A    =         6786401
47  meter
 Y    =       -3679833
04  meter          E    =           
0015297
 Z    =        1106817
30                 I    =           51
49058
 XDOT =       3482
243357                 Wp   =           60
86290
 YDOT =      -3503
754922  meter/sec      RA   =          205
81213  deg
 ZDOT =       5869
537871                 TA   =          311
17947
                                          MA   =          311
31131
                                          Ha   =            220
383  n
mi
                                          Hp   =            212
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18324652
08                 X    =        -5549166
41
 Y    =      -12072943
06  feet           Y    =        -3742089
94  meter
 Z    =        3631290
36                 Z    =         1079772
95
 XDOT =      11424
682930                 XDOT =        3492
653022
 YDOT =     -11495
258930  feet/sec       YDOT =       -3464
756370  meter/sec
 ZDOT =      19257
014013                 ZDOT =        5886
478603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1291924
95                 X    =          393778
73
 Y    =       21925286
66  feet           Y    =         6682827
37  meter
 Z    =        3513948
29                 Z    =         1071051
44
 XDOT =     -14370
195392                 XDOT =       -4380
035556
 YDOT =      -2280
861070  feet/sec       YDOT =        -695
206454  meter/sec
 ZDOT =      19331
480447                 ZDOT =        5892
235240


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   16211
56219533  
00016717  00000-0  10270-3 0  9079
2 25544  51
6389 206
6064 0001928  88
5728 271
5646 15
54970062 11570


Satellite: ISS
Catalog Number: 25544
Epoch time:      16211
56219533   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:       206
6064  deg
Eccentricity:     
0001928     
Arg of perigee:    88
5728  deg
Mean anomaly:     271
5646  deg
Mean motion:   15
54970062  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1157
Checksum:              323


Coasting Arc #9 (Orbit 1171)
---------------------------------------

Vector Time (GMT): 2016/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4440170
65                 A    =         6783392
22  meter
 Y    =        4197649
92  meter          E    =           
0006415
 Z    =       -2949030
76                 I    =           51
50856
 XDOT =      -5385
256222                 Wp   =          106
20064
 YDOT =       2197
762310  meter/sec      RA   =          200
82326  deg
 ZDOT =      -4990
736142                 TA   =          107
53294
                                          MA   =          107
46283
                                          Ha   =            220
502  n
mi
                                          Hp   =            212
725

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14567489
01                 X    =         4407226
39
 Y    =       13771817
33  feet           Y    =         4247118
90  meter
 Z    =       -9675297
77                 Z    =        -2927541
52
 XDOT =     -17668
163459                 XDOT =       -5385
189407
 YDOT =       7210
506266  feet/sec       YDOT =        2137
541529  meter/sec
 ZDOT =     -16373
806241                 ZDOT =       -5016
895679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1948623
65                 X    =          593940
49
 Y    =      -19996734
16  feet           Y    =        -6095004
57  meter
 Z    =       -9582252
59                 Z    =        -2920670
59
 XDOT =      14985
759127                 XDOT =        4567
659382
 YDOT =       9344
226132  feet/sec       YDOT =        2848
120125  meter/sec
 ZDOT =     -16488
278613                 ZDOT =       -5025
627321


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   16212
52623142  
00016717  00000-0  10270-3 0  9082
2 25544  51
6380 201
7943 0002011  85
7549 274
3834 15
54925293 11720


Satellite: ISS
Catalog Number: 25544
Epoch time:      16212
52623142   =   yrday
fracday
Element set:     908
Inclination:       51
6380  deg
RA of node:       201
7943  deg
Eccentricity:     
0002011     
Arg of perigee:    85
7549  deg
Mean anomaly:     274
3834  deg
Mean motion:   15
54925293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1172
Checksum:              296


Coasting Arc #10 (Orbit 1187)
---------------------------------------

Vector Time (GMT): 2016/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2789267
68                 A    =         6778937
40  meter
 Y    =       -4382132
95  meter          E    =           
0011392
 Z    =        4347922
00                 I    =           51
52481
 XDOT =       6801
122710                 Wp   =          105
70188
 YDOT =       -910
007968  meter/sec      RA   =          195
82488  deg
 ZDOT =       3435
348609                 TA   =          309
36906
                                          MA   =          309
46993
                                          Ha   =            220
406  n
mi
                                          Hp   =            212
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9151140
70                 X    =        -2761178
21
 Y    =      -14377076
62  feet           Y    =        -4413167
65  meter
 Z    =       14264835
97                 Z    =         4334440
60
 XDOT =      22313
394717                 XDOT =        6794
106037
 YDOT =      -2985
590447  feet/sec       YDOT =        -833
992746  meter/sec
 ZDOT =      11270
828770                 ZDOT =        3468
369061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5443507
28                 X    =        -1659181
02
 Y    =       16200804
09  feet           Y    =         4938005
09  meter
 Z    =       14206738
85                 Z    =         4330214
00
 XDOT =     -15050
041733                 XDOT =       -4587
252720
 YDOT =     -15097
269281  feet/sec       YDOT =       -4601
647677  meter/sec
 ZDOT =      11415
037864                 ZDOT =        3479
303541


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   16213
55452702  
00016717  00000-0  10270-3 0  9099
2 25544  51
6383 196
6623 0001802  89
4110 270
7250 15
54962004 11882


Satellite: ISS
Catalog Number: 25544
Epoch time:      16213
55452702   =   yrday
fracday
Element set:     909
Inclination:       51
6383  deg
RA of node:       196
6623  deg
Eccentricity:     
0001802     
Arg of perigee:    89
4110  deg
Mean anomaly:     270
7250  deg
Mean motion:   15
54962004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1188
Checksum:              295


Coasting Arc #11 (Orbit 1202)
---------------------------------------

Vector Time (GMT): 2016/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         760988
04                 A    =         6775665
47  meter
 Y    =        4327099
12  meter          E    =           
0015770
 Z    =       -5172164
98                 I    =           51
54519
 XDOT =      -7525
861898                 Wp   =           80
83144
 YDOT =       -322
957123  meter/sec      RA   =          190
81430  deg
 ZDOT =      -1378
619843                 TA   =          175
88453
                                          MA   =          175
87154
                                          Ha   =            220
441  n
mi
                                          Hp   =            212
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2496679
92                 X    =          737668
38
 Y    =       14196519
41  feet           Y    =         4335478
90  meter
 Z    =      -16969045
21                 Z    =        -5168524
76
 XDOT =     -24691
147958                 XDOT =       -7514
994578
 YDOT =      -1059
570613  feet/sec       YDOT =        -407
055494  meter/sec
 ZDOT =      -4523
030981                 ZDOT =       -1415
151440

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9261902
77                 X    =         2823027
96
 Y    =      -11068271
52  feet           Y    =        -3373609
16  meter
 Z    =      -16953866
58                 Z    =        -5167538
53
 XDOT =      14121
160405                 XDOT =        4304
129692
 YDOT =      18983
077969  feet/sec       YDOT =        5786
042165  meter/sec
 ZDOT =      -4682
380587                 ZDOT =       -1427
189603


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   16214
51854995  
00016717  00000-0  10270-3 0  9108
2 25544  51
6385 191
8500 0001974  89
1313 271
0066 15
54942016 12035


Satellite: ISS
Catalog Number: 25544
Epoch time:      16214
51854995   =   yrday
fracday
Element set:     910
Inclination:       51
6385  deg
RA of node:       191
8500  deg
Eccentricity:     
0001974     
Arg of perigee:    89
1313  deg
Mean anomaly:     271
0066  deg
Mean motion:   15
54942016  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1203
Checksum:              297


Coasting Arc #12 (Orbit 1218)
---------------------------------------

Vector Time (GMT): 2016/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1390652
45                 A    =         6775171
82  meter
 Y    =       -4045131
89  meter          E    =           
0004937
 Z    =        5250249
32                 I    =           51
57537
 XDOT =       7485
834366                 Wp   =           72
54504
 YDOT =       1449
399040  meter/sec      RA   =          185
80083  deg
 ZDOT =       -863
968398                 TA   =           25
73003
                                          MA   =           25
70547
                                          Ha   =            220
342  n
mi
                                          Hp   =            212
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4562508
03                 X    =         1410279
93
 Y    =      -13271430
08  feet           Y    =        -4029471
15  meter
 Z    =       17225227
44                 Z    =         5257052
12
 XDOT =      24559
824037                 XDOT =        7473
267149
 YDOT =       4755
246195  feet/sec       YDOT =        1533
040407  meter/sec
 ZDOT =      -2834
541988                 ZDOT =        -827
635402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12966643
71                 X    =        -3952233
00
 Y    =        5269465
24  feet           Y    =         1606133
00  meter
 Z    =       17255569
63                 Z    =         5259497
62
 XDOT =     -12022
349974                 XDOT =       -3664
412272
 YDOT =     -20797
179152  feet/sec       YDOT =       -6338
980206  meter/sec
 ZDOT =      -2676
218209                 ZDOT =        -815
711310


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   16215
54683522  
00016717  00000-0  10270-3 0  9119
2 25544  51
6383 186
7180 0001861  92
4598 267
6768 15
54950847 12195


Satellite: ISS
Catalog Number: 25544
Epoch time:      16215
54683522   =   yrday
fracday
Element set:     911
Inclination:       51
6383  deg
RA of node:       186
7180  deg
Eccentricity:     
0001861     
Arg of perigee:    92
4598  deg
Mean anomaly:     267
6768  deg
Mean motion:   15
54950847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1219
Checksum:              338


Coasting Arc #13 (Orbit 1233)
---------------------------------------

Vector Time (GMT): 2016/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3423043
88                 A    =         6777828
44  meter
 Y    =        3609104
73  meter          E    =           
0012175
 Z    =       -4615803
88                 I    =           51
61752
 XDOT =      -6612
197230                 Wp   =          107
99894
 YDOT =      -2456
595704  meter/sec      RA   =          180
79317  deg
 ZDOT =       2985
545182                 TA   =          191
80434
                                          MA   =          191
83290
                                          Ha   =            220
368  n
mi
                                          Hp   =            212
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11230458
93                 X    =        -3440726
34
 Y    =       11840894
79  feet           Y    =         3570727
19  meter
 Z    =      -15143713
50                 Z    =        -4632474
65
 XDOT =     -21693
560466                 XDOT =       -6598
737675
 YDOT =      -8059
697192  feet/sec       YDOT =       -2530
462514  meter/sec
 ZDOT =       9795
095740                 ZDOT =        2953
458186

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16244981
72                 X    =         4951470
43
 Y    =         451513
85  feet           Y    =          137621
42  meter
 Z    =      -15217054
91                 Z    =        -4638158
34
 XDOT =       8468
096957                 XDOT =        2581
075952
 YDOT =      20428
667795  feet/sec       YDOT =        6226
657944  meter/sec
 ZDOT =       9655
443698                 ZDOT =        2942
979239


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   16216
51084659  
00016717  00000-0  10270-3 0  9124
2 25544  51
6393 181
9066 0001840  94
6087 265
5277 15
54951129 12343


Satellite: ISS
Catalog Number: 25544
Epoch time:      16216
51084659   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:       181
9066  deg
Eccentricity:     
0001840     
Arg of perigee:    94
6087  deg
Mean anomaly:     265
5277  deg
Mean motion:   15
54951129  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1234
Checksum:              321


Coasting Arc #14 (Orbit 1243)
---------------------------------------

Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3041926
22                 A    =         6777065
68  meter
 Y    =       -3686410
68  meter          E    =           
0009292
 Z    =        4799425
44                 I    =           51
63829
 XDOT =       6854
841810                 Wp   =          117
82220
 YDOT =      -2296
835915  meter/sec      RA   =          177
83376  deg
 ZDOT =       2572
433605                 TA   =          306
82359
                                          MA   =          306
90880
                                          Ha   =            220
342  n
mi
                                          Hp   =            212
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9980072
91                 X    =        -3023790
77
 Y    =      -12094523
22  feet           Y    =        -3720326
16  meter
 Z    =       15746146
46                 Z    =         4784692
89
 XDOT =      22489
638483                 XDOT =        6867
520662
 YDOT =      -7535
550902  feet/sec       YDOT =       -2220
109621  meter/sec
 ZDOT =       8439
742797                 ZDOT =        2605
762716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7465065
18                 X    =        -2275351
87
 Y    =      -13861985
63  feet           Y    =        -4225133
22  meter
 Z    =       15682430
67                 Z    =         4780004
87
 XDOT =      22476
275203                 XDOT =        6850
768682
 YDOT =      -2360
992157  feet/sec       YDOT =        -719
630409  meter/sec
 ZDOT =       8585
589354                 ZDOT =        2616
887635


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   16217
15351617  
00016717  00000-0  10270-3 0  9137
2 25544  51
6430 178
6957 0001842 112
1919 247
9430 15
55005516 12446


Satellite: ISS
Catalog Number: 25544
Epoch time:      16217
15351617   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:       178
6957  deg
Eccentricity:     
0001842     
Arg of perigee:   112
1919  deg
Mean anomaly:     247
9430  deg
Mean motion:   15
55005516  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1244
Checksum:              297


Coasting Arc #15 (Orbit 1258)
---------------------------------------

Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         949973
99                 A    =         6774927
18  meter
 Y    =        4114445
05  meter          E    =           
0016428
 Z    =       -5312173
05                 I    =           51
66318
 XDOT =      -7545
130693                 Wp   =           89
87366
 YDOT =       1252
371973  meter/sec      RA   =          172
82907  deg
 ZDOT =       -380
273596                 TA   =          176
50232
                                          MA   =          176
49082
                                          Ha   =            220
273  n
mi
                                          Hp   =            212
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3116712
55                 X    =          929698
32
 Y    =       13498835
46  feet           Y    =         4124954
86  meter
 Z    =      -17428389
26                 Z    =        -5307607
70
 XDOT =     -24754
365790                 XDOT =       -7556
727100
 YDOT =       4108
831933  feet/sec       YDOT =        1167
932436  meter/sec
 ZDOT =      -1247
616786                 ZDOT =        -416
953353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         708854
98                 X    =          216059
00
 Y    =       13860065
46  feet           Y    =         4224547
95  meter
 Z    =      -17409115
95                 Z    =        -5306298
54
 XDOT =     -24069
246717                 XDOT =       -7336
306399
 YDOT =       -533
417279  feet/sec       YDOT =        -162
585587  meter/sec
 ZDOT =      -1407
938148                 ZDOT =        -429
139548


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   16218
11751845  
00016717  00000-0  10270-3 0  9142
2 25544  51
6430 173
8854 0001800 112
5529 247
5814 15
54984580 12598


Satellite: ISS
Catalog Number: 25544
Epoch time:      16218
11751845   =   yrday
fracday
Element set:     914
Inclination:       51
6430  deg
RA of node:       173
8854  deg
Eccentricity:     
0001800     
Arg of perigee:   112
5529  deg
Mean anomaly:     247
5814  deg
Mean motion:   15
54984580  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1259
Checksum:              314


Coasting Arc #16 (Orbit 1274)
---------------------------------------

Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1211397
60                 A    =         6775837
66  meter
 Y    =       -4343751
06  meter          E    =           
0006526
 Z    =        5052658
40                 I    =           51
69885
 XDOT =       7442
962965                 Wp   =           69
66439
 YDOT =        -98
903956  meter/sec      RA   =          167
82349  deg
 ZDOT =      -1865
343864                 TA   =           38
40294
                                          MA   =           38
35651
                                          Ha   =            220
173  n
mi
                                          Hp   =            212
668

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3974401
58                 X    =         1235337
30
 Y    =      -14251151
79  feet           Y    =        -4330070
43  meter
 Z    =       16576963
24                 Z    =         5058601
20
 XDOT =      24419
169834                 XDOT =        7452
576631
 YDOT =       -324
488046  feet/sec       YDOT =         -15
618061  meter/sec
 ZDOT =      -6119
894568                 ZDOT =       -1829
165127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6175845
49                 X    =         1882397
70
 Y    =      -13411424
60  feet           Y    =        -4087802
22  meter
 Z    =       16603599
86                 Z    =         5060777
24
 XDOT =      23195
721327                 XDOT =        7070
055861
 YDOT =       3283
549034  feet/sec       YDOT =        1000
825745  meter/sec
 ZDOT =      -5961
928322                 ZDOT =       -1817
195753


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   16219
14578055  
00016717  00000-0  10270-3 0  9157
2 25544  51
6432 168
7530 0001789 116
0015 244
1323 15
55022182 12757


Satellite: ISS
Catalog Number: 25544
Epoch time:      16219
14578055   =   yrday
fracday
Element set:     915
Inclination:       51
6432  deg
RA of node:       168
7530  deg
Eccentricity:     
0001789     
Arg of perigee:   116
0015  deg
Mean anomaly:     244
1323  deg
Mean motion:   15
55022182  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1275
Checksum:              288
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