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

 
Date: July 28th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 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 5
000/00:00:00 000 0 0 0 0 212 7

220/06:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 212 7

223/08:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 212 9

Coasting Arc #1 (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    =       -5991176
54                 A    =         6783833
91  meter
 Y    =       -1632265
77  meter          E    =           
0006721
 Z    =       -2732890
41                 I    =           51
42840
 XDOT =       -803
873407                 Wp   =           65
31309
 YDOT =      -5630
607273  meter/sec      RA   =          215
78727  deg
 ZDOT =       5137
979063                 TA   =          263
67393
                                          MA   =          263
75049
                                          Ha   =            220
489  n
mi
                                          Hp   =            212
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19656091
00                 X    =        -5959203
73
 Y    =       -5355202
67  feet           Y    =        -1699084
22  meter
 Z    =       -8966175
88                 Z    =        -2761916
27
 XDOT =      -2637
379943                 XDOT =        -765
808719
 YDOT =     -18473
120974  feet/sec       YDOT =       -5639
384108  meter/sec
 ZDOT =      16856
886689                 ZDOT =        5134
166286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6768375
15                 X    =         2063000
75
 Y    =       19155902
35  feet           Y    =         5838719
04  meter
 Z    =       -9092465
12                 Z    =        -2771383
37
 XDOT =     -12215
912057                 XDOT =       -3723
409995
 YDOT =      12290
519965  feet/sec       YDOT =        3746
150485  meter/sec
 ZDOT =      16841
202764                 ZDOT =        5133
198603


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
50561190  
00016717  00000-0  10270-3 0  9002
2 25544  51
6406 216
8707 0002047  79
2092 280
9291 15
54896772 11251


Satellite: ISS
Catalog Number: 25544
Epoch time:      16209
50561190   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:       216
8707  deg
Eccentricity:     
0002047     
Arg of perigee:    79
2092  deg
Mean anomaly:     280
9291  deg
Mean motion:   15
54896772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1125
Checksum:              307


Coasting Arc #2 (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    =        6100432
82                 A    =         6786749
27  meter
 Y    =        2828040
51  meter          E    =           
0014997
 Z    =         871397
93                 I    =           51
46390
 XDOT =      -1322
908712                 Wp   =          119
81814
 YDOT =       4698
407893  meter/sec      RA   =          210
79596  deg
 ZDOT =      -5917
672295                 TA   =           50
72521
                                          MA   =           50
59227
                                          Ha   =            220
538  n
mi
                                          Hp   =            212
672

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20014543
36                 X    =         6064122
71
 Y    =        9278348
12  feet           Y    =         2896056
54  meter
 Z    =        2858917
09                 Z    =          900944
07
 XDOT =      -4340
251681                 XDOT =       -1346
603879
 YDOT =      15414
724060  feet/sec       YDOT =        4683
482111  meter/sec
 ZDOT =     -19414
935350                 ZDOT =       -5924
155880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4145021
88                 X    =        -1263402
67
 Y    =      -21650357
39  feet           Y    =        -6599028
93  meter
 Z    =        2987292
28                 Z    =          910526
69
 XDOT =      13394
267132                 XDOT =        4082
572622
 YDOT =      -5277
222112  feet/sec       YDOT =       -1608
497300  meter/sec
 ZDOT =     -19443
991060                 ZDOT =       -5926
528475


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
53394243  
00016717  00000-0  10270-3 0  9011
2 25544  51
6398 211
7380 0002092  79
1826 280
9563 15
54896210 11413


Satellite: ISS
Catalog Number: 25544
Epoch time:      16210
53394243   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       211
7380  deg
Eccentricity:     
0002092     
Arg of perigee:    79
1826  deg
Mean anomaly:     280
9563  deg
Mean motion:   15
54896210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1141
Checksum:              298


Coasting Arc #3 (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    =       -5606701
60                 A    =         6786525
79  meter
 Y    =       -3658211
92  meter          E    =           
0015301
 Z    =        1070660
22                 I    =           51
49071
 XDOT =       3438
119448                 Wp   =           60
39491
 YDOT =      -3532
668158  meter/sec      RA   =          205
81226  deg
 ZDOT =       5878
136923                 TA   =          311
24824
                                          MA   =          311
37997
                                          Ha   =            220
440  n
mi
                                          Hp   =            212
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18394690
28                 X    =        -5570578
60
 Y    =      -12002007
63  feet           Y    =        -3720707
91  meter
 Z    =        3512664
75                 Z    =         1043512
01
 XDOT =      11279
919450                 XDOT =        3448
813937
 YDOT =     -11590
118627  feet/sec       YDOT =       -3494
161436  meter/sec
 ZDOT =      19285
226124                 ZDOT =        5894
864003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1390191
99                 X    =          423730
52
 Y    =       21938411
10  feet           Y    =         6686827
70  meter
 Z    =        3394866
15                 Z    =         1034755
20
 XDOT =     -14358
620696                 XDOT =       -4376
507588
 YDOT =      -2115
129331  feet/sec       YDOT =        -644
691420  meter/sec
 ZDOT =      19358
765526                 ZDOT =        5900
551732


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
56226791  
00016717  00000-0  10270-3 0  9028
2 25544  51
6389 206
6068 0001952  87
2690 272
8686 15
54938425 11570


Satellite: ISS
Catalog Number: 25544
Epoch time:      16211
56226791   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:       206
6068  deg
Eccentricity:     
0001952     
Arg of perigee:    87
2690  deg
Mean anomaly:     272
8686  deg
Mean motion:   15
54938425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1157
Checksum:              332


Coasting Arc #4 (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    =        4483579
15                 A    =         6783599
04  meter
 Y    =        4179824
70  meter          E    =           
0006438
 Z    =       -2908643
33                 I    =           51
50892
 XDOT =      -5339
175500                 Wp   =          107
10244
 YDOT =       2240
907176  meter/sec      RA   =          200
82379  deg
 ZDOT =      -5020
962000                 TA   =          106
10797
                                          MA   =          106
03707
                                          Ha   =            220
570  n
mi
                                          Hp   =            212
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14709905
35                 X    =         4450634
81
 Y    =       13713335
64  feet           Y    =         4229779
10  meter
 Z    =       -9542793
08                 Z    =        -2886943
23
 XDOT =     -17516
979987                 XDOT =       -5339
447744
 YDOT =       7352
057663  feet/sec       YDOT =        2181
199806  meter/sec
 ZDOT =     -16472
972441                 ZDOT =       -5046
898512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1815792
11                 X    =          553453
44
 Y    =      -20072976
66  feet           Y    =        -6118243
29  meter
 Z    =       -9448825
15                 Z    =        -2880001
91
 XDOT =      14999
340052                 XDOT =        4571
798848
 YDOT =       9147
230283  feet/sec       YDOT =        2788
075790  meter/sec
 ZDOT =     -16586
479076                 ZDOT =       -5055
558822


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
52632563  
00016717  00000-0  10270-3 0  9034
2 25544  51
6380 201
7948 0002040  84
3410 275
7975 15
54888552 11726


Satellite: ISS
Catalog Number: 25544
Epoch time:      16212
52632563   =   yrday
fracday
Element set:     903
Inclination:       51
6380  deg
RA of node:       201
7948  deg
Eccentricity:     
0002040     
Arg of perigee:    84
3410  deg
Mean anomaly:     275
7975  deg
Mean motion:   15
54888552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1172
Checksum:              304


Coasting Arc #5 (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    =       -2858893
90                 A    =         6779188
36  meter
 Y    =       -4372570
88  meter          E    =           
0011557
 Z    =        4312420
26                 I    =           51
52527
 XDOT =       6763
979477                 Wp   =          104
79163
 YDOT =       -967
496760  meter/sec      RA   =          195
82611  deg
 ZDOT =       3492
425162                 TA   =          309
61258
                                          MA   =          309
71454
                                          Ha   =            220
481  n
mi
                                          Hp   =            212
760

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9379573
17                 X    =        -2830733
73
 Y    =      -14345704
98  feet           Y    =        -4404383
79  meter
 Z    =       14148360
42                 Z    =         4298600
81
 XDOT =      22191
533717                 XDOT =        6757
331170
 YDOT =      -3174
201967  feet/sec       YDOT =        -891
894842  meter/sec
 ZDOT =      11458
087802                 ZDOT =        3525
266075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5276713
49                 X    =        -1608342
27
 Y    =       16358915
75  feet           Y    =         4986197
52  meter
 Z    =       14088786
92                 Z    =         4294262
25
 XDOT =     -15108
794272                 XDOT =       -4605
160494
 YDOT =     -14895
483387  feet/sec       YDOT =       -4540
143336  meter/sec
 ZDOT =      11601
523040                 ZDOT =        3536
144223


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
55464740  
00016717  00000-0  10270-3 0  9049
2 25544  51
6383 196
6631 0001830  87
8638 272
2724 15
54921190 11883


Satellite: ISS
Catalog Number: 25544
Epoch time:      16213
55464740   =   yrday
fracday
Element set:     904
Inclination:       51
6383  deg
RA of node:       196
6631  deg
Eccentricity:     
0001830     
Arg of perigee:    87
8638  deg
Mean anomaly:     272
2724  deg
Mean motion:   15
54921190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1188
Checksum:              316


Coasting Arc #6 (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    =         856763
57                 A    =         6775882
82  meter
 Y    =        4330880
46  meter          E    =           
0015681
 Z    =       -5154195
33                 I    =           51
54548
 XDOT =      -7512
647500                 Wp   =           80
12224
 YDOT =       -252
907544  meter/sec      RA   =          190
81629  deg
 ZDOT =      -1462
477889                 TA   =          175
76914
                                          MA   =          175
75587
                                          Ha   =            220
527  n
mi
                                          Hp   =            212
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2810904
09                 X    =          833307
21
 Y    =       14208925
39  feet           Y    =         4340330
51  meter
 Z    =      -16910089
67                 Z    =        -5150090
20
 XDOT =     -24647
793636                 XDOT =       -7502
157137
 YDOT =       -829
749160  feet/sec       YDOT =        -336
860246  meter/sec
 ZDOT =      -4798
155805                 ZDOT =       -1498
946207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9071098
67                 X    =         2764870
88
 Y    =      -11317753
59  feet           Y    =        -3449651
29  meter
 Z    =      -16892883
05                 Z    =        -5148950
76
 XDOT =      14251
028414                 XDOT =        4343
713461
 YDOT =      18815
549730  feet/sec       YDOT =        5734
979558  meter/sec
 ZDOT =      -4957
240707                 ZDOT =       -1510
966967


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
51869797  
00016717  00000-0  10270-3 0  9058
2 25544  51
6385 191
8509 0002009  87
4705 272
6678 15
54895313 12033


Satellite: ISS
Catalog Number: 25544
Epoch time:      16214
51869797   =   yrday
fracday
Element set:     905
Inclination:       51
6385  deg
RA of node:       191
8509  deg
Eccentricity:     
0002009     
Arg of perigee:    87
4705  deg
Mean anomaly:     272
6678  deg
Mean motion:   15
54895313  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1203
Checksum:              335


Coasting Arc #7 (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    =        1274773
60                 A    =         6775272
33  meter
 Y    =       -4066981
47  meter          E    =           
0004841
 Z    =        5262905
53                 I    =           51
57521
 XDOT =       7512
138555                 Wp   =           73
78497
 YDOT =       1369
203790  meter/sec      RA   =          185
80342  deg
 ZDOT =       -759
604952                 TA   =           23
48509
                                          MA   =           23
46299
                                          Ha   =            220
443  n
mi
                                          Hp   =            212
760

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4182328
09                 X    =         1294592
54
 Y    =      -13343115
07  feet           Y    =        -4052615
50  meter
 Z    =       17266750
42                 Z    =         5269145
89
 XDOT =      24646
123868                 XDOT =        7499
959206
 YDOT =       4492
138419  feet/sec       YDOT =        1453
141473  meter/sec
 ZDOT =      -2492
142230                 ZDOT =        -723
143241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12773142
31                 X    =        -3893253
78
 Y    =        5604771
46  feet           Y    =         1708334
34  meter
 Z    =       17294641
66                 Z    =         5271406
78
 XDOT =     -12252
255009                 XDOT =       -3734
487327
 YDOT =     -20703
667297  feet/sec       YDOT =       -6310
477792  meter/sec
 ZDOT =      -2333
243765                 ZDOT =        -711
172699


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
54701604  
00016717  00000-0  10270-3 0  9065
2 25544  51
6383 186
7191 0001902  90
4883 269
6488 15
54898081 12190


Satellite: ISS
Catalog Number: 25544
Epoch time:      16215
54701604   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:       186
7191  deg
Eccentricity:     
0001902     
Arg of perigee:    90
4883  deg
Mean anomaly:     269
6488  deg
Mean motion:   15
54898081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1219
Checksum:              329


Coasting Arc #8 (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    =       -3300006
48                 A    =         6777784
08  meter
 Y    =        3653836
12  meter          E    =           
0012526
 Z    =       -4670196
78                 I    =           51
61682
 XDOT =      -6691
292825                 Wp   =          107
36843
 YDOT =      -2371
101027  meter/sec      RA   =          180
79586  deg
 ZDOT =       2875
766815                 TA   =          191
23619
                                          MA   =          191
26418
                                          Ha   =            220
473  n
mi
                                          Hp   =            212
682

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10826792
91                 X    =        -3317934
07
 Y    =       11987651
31  feet           Y    =         3616833
09  meter
 Z    =      -15322167
90                 Z    =        -4686270
47
 XDOT =     -21953
060449                 XDOT =       -6678
250171
 YDOT =      -7779
202843  feet/sec       YDOT =       -2445
854665  meter/sec
 ZDOT =       9434
930495                 ZDOT =        2843
294591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16085636
84                 X    =         4902902
11
 Y    =          51496
70  feet           Y    =           15696
19  meter
 Z    =      -15392910
49                 Z    =        -4691759
12
 XDOT =       8819
400241                 XDOT =        2688
153193
 YDOT =      20446
093703  feet/sec       YDOT =        6231
969361  meter/sec
 ZDOT =       9293
583350                 ZDOT =        2832
684205


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
51106128  
00016717  00000-0  10270-3 0  9074
2 25544  51
6393 181
9079 0001878  92
5222 267
6146 15
54893953 12344


Satellite: ISS
Catalog Number: 25544
Epoch time:      16216
51106128   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       181
9079  deg
Eccentricity:     
0001878     
Arg of perigee:    92
5222  deg
Mean anomaly:     267
6146  deg
Mean motion:   15
54893953  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1234
Checksum:              322


Coasting Arc #9 (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    =       -3181303
04                 A    =         6777460
18  meter
 Y    =       -3638576
87  meter          E    =           
0009627
 Z    =        4745609
32                 I    =           51
63904
 XDOT =       6773
364201                 Wp   =          116
34615
 YDOT =      -2392
592851  meter/sec      RA   =          177
83688  deg
 ZDOT =       2697
764694                 TA   =          306
97068
                                          MA   =          307
05878
                                          Ha   =            220
451  n
mi
                                          Hp   =            212
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10437345
92                 X    =        -3163430
70
 Y    =      -11937588
17  feet           Y    =        -3674052
44  meter
 Z    =       15569584
37                 Z    =         4730199
08
 XDOT =      22222
323495                 XDOT =        6786
511097
 YDOT =      -7849
714077  feet/sec       YDOT =       -2316
775078  meter/sec
 ZDOT =       8850
934037                 ZDOT =        2730
699153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7943329
85                 X    =        -2421126
94
 Y    =      -13799263
42  feet           Y    =        -4206015
49  meter
 Z    =       15502902
91                 Z    =         4725284
81
 XDOT =      22279
011821                 XDOT =        6790
642803
 YDOT =      -2687
805224  feet/sec       YDOT =        -819
243032  meter/sec
 ZDOT =       8995
073300                 ZDOT =        2741
698342


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
15375514  
00016717  00000-0  10270-3 0  9083
2 25544  51
6429 178
6972 0001861 109
8384 250
2970 15
54946207 12447


Satellite: ISS
Catalog Number: 25544
Epoch time:      16217
15375514   =   yrday
fracday
Element set:     908
Inclination:       51
6429  deg
RA of node:       178
6972  deg
Eccentricity:     
0001861     
Arg of perigee:   109
8384  deg
Mean anomaly:     250
2970  deg
Mean motion:   15
54946207  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1244
Checksum:              324


Coasting Arc #10 (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    =        1130410
87                 A    =         6775178
53  meter
 Y    =        4083089
89  meter          E    =           
0016375
 Z    =       -5301295
45                 I    =           51
66337
 XDOT =      -7513
313051                 Wp   =           88
53284
 YDOT =       1377
087206  meter/sec      RA   =          172
83329  deg
 ZDOT =       -542
484964                 TA   =          176
29148
                                          MA   =          176
27933
                                          Ha   =            220
394  n
mi
                                          Hp   =            212
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3708697
09                 X    =         1110419
58
 Y    =       13395964
20  feet           Y    =         4095619
06  meter
 Z    =      -17392701
61                 Z    =        -5295852
91
 XDOT =     -24649
977203                 XDOT =       -7525
518485
 YDOT =       4518
002644  feet/sec       YDOT =        1293
000067  meter/sec
 ZDOT =      -1779
806311                 ZDOT =        -579
011642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1309430
61                 X    =          399114
45
 Y    =       13867045
65  feet           Y    =         4226675
51  meter
 Z    =      -17369594
02                 Z    =        -5294252
26
 XDOT =     -24037
477265                 XDOT =       -7326
623070
 YDOT =       -155
275788  feet/sec       YDOT =         -47
328060  meter/sec
 ZDOT =      -1939
479306                 ZDOT =        -591
153292


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
11779664  
00016717  00000-0  10270-3 0  9095
2 25544  51
6430 173
8871 0001819 110
0245 250
1104 15
54916974 12599


Satellite: ISS
Catalog Number: 25544
Epoch time:      16218
11779664   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       173
8871  deg
Eccentricity:     
0001819     
Arg of perigee:   110
0245  deg
Mean anomaly:     250
1104  deg
Mean motion:   15
54916974  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1259
Checksum:              308


Coasting Arc #11 (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    =        1004451
47                 A    =         6775830
38  meter
 Y    =       -4338948
55  meter          E    =           
0006166
 Z    =        5102053
87                 I    =           51
69816
 XDOT =       7482
247238                 Wp   =           69
78007
 YDOT =       -252
920766  meter/sec      RA   =          167
82820  deg
 ZDOT =      -1684
403859                 TA   =           36
48383
                                          MA   =           36
44184
                                          Ha   =            220
302  n
mi
                                          Hp   =            212
758

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3295444
45                 X    =         1028112
91
 Y    =      -14235395
50  feet           Y    =        -4327583
68  meter
 Z    =       16739021
87                 Z    =         5106990
72
 XDOT =      24548
055243                 XDOT =        7492
701327
 YDOT =       -829
792538  feet/sec       YDOT =        -169
190864  meter/sec
 ZDOT =      -5526
259381                 ZDOT =       -1648
032247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5502648
96                 X    =         1677207
40
 Y    =      -13508594
01  feet           Y    =        -4117419
45  meter
 Z    =       16761265
91                 Z    =         5108833
85
 XDOT =      23395
707147                 XDOT =        7131
011538
 YDOT =       2855
108280  feet/sec       YDOT =         870
237004  meter/sec
 ZDOT =      -5367
426579                 ZDOT =       -1635
991621


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
14610404  
00016717  00000-0  10270-3 0  9107
2 25544  51
6432 168
7550 0001806 113
2194 246
9150 15
54953307 12755


Satellite: ISS
Catalog Number: 25544
Epoch time:      16219
14610404   =   yrday
fracday
Element set:     910
Inclination:       51
6432  deg
RA of node:       168
7550  deg
Eccentricity:     
0001806     
Arg of perigee:   113
2194  deg
Mean anomaly:     246
9150  deg
Mean motion:   15
54953307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1275
Checksum:              286


Coasting Arc #12 (Orbit 1289)
---------------------------------------

Vector Time (GMT): 2016/220/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2975848
07                 A    =         6779321
59  meter
 Y    =        4402431
22  meter          E    =           
0009955
 Z    =       -4220209
58                 I    =           51
74120
 XDOT =      -6650
860711                 Wp   =          111
73570
 YDOT =       -977
441614  meter/sec      RA   =          162
83362  deg
 ZDOT =       3673
517098                 TA   =          195
88897
                                          MA   =          195
92023
                                          Ha   =            220
319  n
mi
                                          Hp   =            212
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9763281
07                 X    =        -3004356
35
 Y    =       14443671
98  feet           Y    =         4368993
77  meter
 Z    =      -13845831
96                 Z    =        -4234734
66
 XDOT =     -21820
409156                 XDOT =       -6657
280500
 YDOT =      -3206
829443  feet/sec       YDOT =       -1051
851771  meter/sec
 ZDOT =      12052
221451                 ZDOT =        3641
193811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11714699
87                 X    =        -3570640
52
 Y    =       12842406
18  feet           Y    =         3914365
40  meter
 Z    =      -13909952
94                 Z    =        -4239753
66
 XDOT =     -20240
679453                 XDOT =       -6169
359097
 YDOT =      -5573
820112  feet/sec       YDOT =       -1698
900370  meter/sec
 ZDOT =      11911
245254                 ZDOT =        3630
547553


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   16220
11014008  
00016717  00000-0  10270-3 0  9115
2 25544  51
6432 163
9449 0001845 116
6830 243
4512 15
54951494 12902


Satellite: ISS
Catalog Number: 25544
Epoch time:      16220
11014008   =   yrday
fracday
Element set:     911
Inclination:       51
6432  deg
RA of node:       163
9449  deg
Eccentricity:     
0001845     
Arg of perigee:   116
6830  deg
Mean anomaly:     243
4512  deg
Mean motion:   15
54951494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1290
Checksum:              281


Coasting Arc #13 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2016/220/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3988247
23                 A    =         6777370
29  meter
 Y    =       -2673432
03  meter          E    =           
0009594
 Z    =        4777569
43                 I    =           51
73771
 XDOT =       5923
883263                 Wp   =          116
00202
 YDOT =      -4099
402403  meter/sec      RA   =          162
13549  deg
 ZDOT =       2643
002881                 TA   =          307
93602
                                          MA   =          308
02269
                                          Ha   =            220
548  n
mi
                                          Hp   =            212
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13084800
62                 X    =        -3981262
86
 Y    =       -8771102
47  feet           Y    =        -2717992
08  meter
 Z    =       15674440
38                 Z    =         4758212
85
 XDOT =      19435
312544                 XDOT =        5956
445164
 YDOT =     -13449
482951  feet/sec       YDOT =       -4032
975437  meter/sec
 ZDOT =       8671
269294                 ZDOT =        2671
858407

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15506040
26                 X    =        -4726241
07
 Y    =        3214973
82  feet           Y    =          979924
02  meter
 Z    =       15590349
13                 Z    =         4751938
41
 XDOT =       4289
565152                 XDOT =        1307
459458
 YDOT =     -22106
397203  feet/sec       YDOT =       -6738
029867  meter/sec
 ZDOT =       8797
914289                 ZDOT =        2681
604275


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   16220
30294688  
00016717  00000-0  10270-3 0  9121
2 25544  51
6420 162
9836 0002002 106
3819 253
7554 15
54939966 12930


Satellite: ISS
Catalog Number: 25544
Epoch time:      16220
30294688   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:       162
9836  deg
Eccentricity:     
0002002     
Arg of perigee:   106
3819  deg
Mean anomaly:     253
7554  deg
Mean motion:   15
54939966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1293
Checksum:              315


Coasting Arc #14 (Orbit 1307)
---------------------------------------

Vector Time (GMT): 2016/221/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2119343
99                 A    =         6775135
61  meter
 Y    =        3650621
74  meter          E    =           
0016498
 Z    =       -5313669
78                 I    =           51
76146
 XDOT =      -6888
855031                 Wp   =           89
10508
 YDOT =       3310
302143  meter/sec      RA   =          157
13769  deg
 ZDOT =       -474
364948                 TA   =          176
37737
                                          MA   =          176
36541
                                          Ha   =            220
414  n
mi
                                          Hp   =            212
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6953228
32                 X    =         2104175
52
 Y    =       11977105
46  feet           Y    =         3674236
70  meter
 Z    =      -17433299
79                 Z    =        -5303411
60
 XDOT =     -22601
230418                 XDOT =       -6923
055441
 YDOT =      10860
571336  feet/sec       YDOT =        3233
075121  meter/sec
 ZDOT =      -1556
315445                 ZDOT =        -507
912043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13540970
87                 X    =         4127287
92
 Y    =        3159130
15  feet           Y    =          962902
87  meter
 Z    =      -17389088
12                 Z    =        -5300194
06
 XDOT =      -7514
432304                 XDOT =       -2290
398966
 YDOT =      22851
756139  feet/sec       YDOT =        6965
215271  meter/sec
 ZDOT =      -1703
335063                 ZDOT =        -519
176527


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   16221
26697902  
00016717  00000-0  10270-3 0  9134
2 25544  51
6430 158
1728 0001901 110
1125 250
0233 15
54922664 13086


Satellite: ISS
Catalog Number: 25544
Epoch time:      16221
26697902   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:       158
1728  deg
Eccentricity:     
0001901     
Arg of perigee:   110
1125  deg
Mean anomaly:     250
0233  deg
Mean motion:   15
54922664  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1308
Checksum:              274


Coasting Arc #15 (Orbit 1323)
---------------------------------------

Vector Time (GMT): 2016/222/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -124617
66                 A    =         6775906
51  meter
 Y    =       -4465821
24  meter          E    =           
0006512
 Z    =        5089782
87                 I    =           51
79199
 XDOT =       7136
278887                 Wp   =           70
24600
 YDOT =      -2207
085701  meter/sec      RA   =          152
13954  deg
 ZDOT =      -1757
818930                 TA   =           36
72520
                                          MA   =           36
68059
                                          Ha   =            220
406  n
mi
                                          Hp   =            212
685

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -408850
59                 X    =          -99394
19
 Y    =      -14651644
47  feet           Y    =        -4467073
65  meter
 Z    =       16698762
70                 Z    =         5089238
88
 XDOT =      23412
988476                 XDOT =        7168
967341
 YDOT =      -7241
094821  feet/sec       YDOT =       -2127
100328  meter/sec
 ZDOT =      -5767
122474                 ZDOT =       -1723
073564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11119046
53                 X    =        -3389085
38
 Y    =       -9553012
70  feet           Y    =        -2911758
27  meter
 Z    =       16697103
73                 Z    =         5089277
22
 XDOT =       9879
458695                 XDOT =        3011
259010
 YDOT =     -21335
952480  feet/sec       YDOT =       -6503
198316  meter/sec
 ZDOT =      -5615
030150                 ZDOT =       -1711
461190


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   16222
29527644  
00016717  00000-0  10270-3 0  9144
2 25544  51
6411 153
0410 0001988 111
7317 248
4048 15
54956151 13243


Satellite: ISS
Catalog Number: 25544
Epoch time:      16222
29527644   =   yrday
fracday
Element set:     914
Inclination:       51
6411  deg
RA of node:       153
0410  deg
Eccentricity:     
0001988     
Arg of perigee:   111
7317  deg
Mean anomaly:     248
4048  deg
Mean motion:   15
54956151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1324
Checksum:              291


Coasting Arc #16 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2016/223/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1755914
38                 A    =         6779522
62  meter
 Y    =        5046820
39  meter          E    =           
0009732
 Z    =       -4182533
79                 I    =           51
83341
 XDOT =      -6638
909989                 Wp   =          110
74372
 YDOT =        787
038108  meter/sec      RA   =          147
15084  deg
 ZDOT =       3740
492438                 TA   =          197
63149
                                          MA   =          197
66529
                                          Ha   =            220
359  n
mi
                                          Hp   =            212
734

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5760873
95                 X    =        -1791901
92
 Y    =       16557809
68  feet           Y    =         5026983
30  meter
 Z    =      -13722223
73                 Z    =        -4191150
99
 XDOT =     -21781
200751                 XDOT =       -6665
386983
 YDOT =       2582
146023  feet/sec       YDOT =         712
649390  meter/sec
 ZDOT =      12271
956817                 ZDOT =        3708
178221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8587901
27                 X    =         2617592
31
 Y    =       15249259
66  feet           Y    =         4647974
34  meter
 Z    =      -13760675
34                 Z    =        -4194253
84
 XDOT =     -11501
968902                 XDOT =       -3505
800121
 YDOT =      17413
253323  feet/sec       YDOT =        5307
559613  meter/sec
 ZDOT =      12130
694636                 ZDOT =        3697
435725


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   16223
25930194  
00016717  00000-0  10270-3 0  9150
2 25544  51
6425 148
2300 0001853 112
8484 247
2865 15
54938103 13397


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
25930194   =   yrday
fracday
Element set:     915
Inclination:       51
6425  deg
RA of node:       148
2300  deg
Eccentricity:     
0001853     
Arg of perigee:   112
8484  deg
Mean anomaly:     247
2865  deg
Mean motion:   15
54938103  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1339
Checksum:              301


Coasting Arc #17 (Orbit 1340)
---------------------------------------

Vector Time (GMT): 2016/223/08:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5392162
09                 A    =         6779934
71  meter
 Y    =         313181
36  meter          E    =           
0008760
 Z    =       -4106612
84                 I    =           51
83519
 XDOT =      -3260
718129                 Wp   =           79
62636
 YDOT =       5767
988256  meter/sec      RA   =          146
62960  deg
 ZDOT =      -3847
012631                 TA   =          150
70886
                                          MA   =          150
65972
                                          Ha   =            220
386  n
mi
                                          Hp   =            212
870

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17690820
50                 X    =         5408207
25
 Y    =        1027497
90  feet           Y    =          373569
78  meter
 Z    =      -13473139
24                 Z    =        -4080380
31
 XDOT =     -10697
894125                 XDOT =       -3306
287912
 YDOT =      18923
845983  feet/sec       YDOT =        5731
269879  meter/sec
 ZDOT =     -12621
432517                 ZDOT =       -3862
963013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1131577
12                 X    =          344904
71
 Y    =      -17771136
10  feet           Y    =        -5416642
28  meter
 Z    =      -13358615
86                 Z    =        -4071706
12
 XDOT =      17563
579194                 XDOT =        5353
378938
 YDOT =      10645
492588  feet/sec       YDOT =        3244
746141  meter/sec
 ZDOT =     -12692
030387                 ZDOT =       -3868
530862


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   16223
38783933  
00016717  00000-0  10270-3 0  9162
2 25544  51
6400 147
5877 0001845 111
6438 248
4911 15
54943134 13416


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
38783933   =   yrday
fracday
Element set:     916
Inclination:       51
6400  deg
RA of node:       147
5877  deg
Eccentricity:     
0001845     
Arg of perigee:   111
6438  deg
Mean anomaly:     248
4911  deg
Mean motion:   15
54943134  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1341
Checksum:              312


Coasting Arc #18 (Orbit 1356)
---------------------------------------

Vector Time (GMT): 2016/224/08:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4130893
78                 A    =         6776128
37  meter
 Y    =       -1797398
13  meter          E    =           
0007346
 Z    =        5057494
83                 I    =           51
84894
 XDOT =       4793
889288                 Wp   =          122
43291
 YDOT =      -5685
882318  meter/sec      RA   =          141
64424  deg
 ZDOT =       1889
022252                 TA   =          309
29105
                                          MA   =          309
35618
                                          Ha   =            220
375  n
mi
                                          Hp   =            212
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13552801
11                 X    =        -4135054
74
 Y    =       -5896975
48  feet           Y    =        -1843615
79  meter
 Z    =       16592830
80                 Z    =         5037418
04
 XDOT =      15727
983228                 XDOT =        4847
937986
 YDOT =     -18654
469546  feet/sec       YDOT =       -5631
971633  meter/sec
 ZDOT =       6197
579568                 ZDOT =        1912
440876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5741043
73                 X    =        -1749870
13
 Y    =       13725381
13  feet           Y    =         4183496
17  meter
 Z    =       16505426
42                 Z    =         5030853
97
 XDOT =     -17828
764140                 XDOT =       -5434
207310
 YDOT =     -15057
578586  feet/sec       YDOT =       -4589
549953  meter/sec
 ZDOT =       6300
800584                 ZDOT =        1920
484018


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   16224
41612778  
00016717  00000-0  10270-3 0  9176
2 25544  51
6398 142
4562 0001652 115
1182 245
0142 15
54967399 13573


Satellite: ISS
Catalog Number: 25544
Epoch time:      16224
41612778   =   yrday
fracday
Element set:     917
Inclination:       51
6398  deg
RA of node:       142
4562  deg
Eccentricity:     
0001652     
Arg of perigee:   115
1182  deg
Mean anomaly:     245
0142  deg
Mean motion:   15
54967399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              313
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