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

 
Date: November 1st 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6283 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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


307/03:22:44 976 2 3 4 6 4 6
N/A 3 4 -0 5 223 7
000/00:01:29 951 -2 0 -0 1 214 4

308/04:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 5
000/00:00:00 000 0 0 0 0 214 7

311/14:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 215 2

314/21:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 215 5

Coasting Arc #1 (Orbit 2618)
---------------------------------------

Vector Time (GMT): 2016/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3428736
97                 A    =         6783044
79  meter
 Y    =        4600802
70  meter          E    =           
0017999
 Z    =        3607324
16                 I    =           52
00900
 XDOT =      -2791
149988                 Wp   =          106
29948
 YDOT =      -5589
450051  meter/sec      RA   =           97
28748  deg
 ZDOT =       4452
584536                 TA   =          296
18092
                                          MA   =          296
36591
                                          Ha   =            222
878  n
mi
                                          Hp   =            212
168

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11249137
03                 X    =        -3497452
79
 Y    =       15094497
05  feet           Y    =         4562076
23  meter
 Z    =       11835053
02                 Z    =         3590500
62
 XDOT =      -9157
316233                 XDOT =       -2750
069214
 YDOT =     -18338
090718  feet/sec       YDOT =       -5620
432644  meter/sec
 ZDOT =      14608
216981                 ZDOT =        4439
125520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -818205
77                 X    =         -249389
12
 Y    =      -18854035
10  feet           Y    =        -5746709
90  meter
 Z    =       11760582
67                 Z    =         3584625
60
 XDOT =      17408
015113                 XDOT =        5305
963006
 YDOT =       8368
464055  feet/sec       YDOT =        2550
707844  meter/sec
 ZDOT =      14550
242085                 ZDOT =        4434
913787


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   16305
55671803  
00016717  00000-0  10270-3 0  9007
2 25544  51
6396  97
8765 0006846 129
8843 230
2912 15
54415558 26193


Satellite: ISS
Catalog Number: 25544
Epoch time:      16305
55671803   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:        97
8765  deg
Eccentricity:     
0006846     
Arg of perigee:   129
8843  deg
Mean anomaly:     230
2912  deg
Mean motion:   15
54415558  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2619
Checksum:              334


Coasting Arc #2 (Orbit 2633)
---------------------------------------

Vector Time (GMT): 2016/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3824203
71                 A    =         6779111
43  meter
 Y    =       -3005638
99  meter          E    =           
0015379
 Z    =       -4734815
35                 I    =           51
99970
 XDOT =       1920
554765                 Wp   =           93
78890
 YDOT =       6859
250655  meter/sec      RA   =           92
32211  deg
 ZDOT =      -2811
869448                 TA   =          148
48467
                                          MA   =          148
39245
                                          Ha   =            222
836  n
mi
                                          Hp   =            212
274

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12546600
10                 X    =         3880529
63
 Y    =       -9861020
31  feet           Y    =        -2962559
40  meter
 Z    =      -15534171
08                 Z    =        -4716100
90
 XDOT =       6301
032692                 XDOT =        1857
369354
 YDOT =      22504
103198  feet/sec       YDOT =        6880
374201  meter/sec
 ZDOT =      -9225
293465                 ZDOT =       -2802
693326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3252861
80                 X    =         -991472
28
 Y    =       15704512
49  feet           Y    =         4786735
41  meter
 Z    =      -15451684
19                 Z    =        -4709673
34
 XDOT =     -18272
121232                 XDOT =       -5569
342551
 YDOT =     -12794
427873  feet/sec       YDOT =       -3899
741616  meter/sec
 ZDOT =      -9186
310763                 ZDOT =       -2799
987520


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   16306
52107948  
00016717  00000-0  10270-3 0  9010
2 25544  51
6403  93
0681 0006879 131
8023 228
3719 15
54414638 26344


Satellite: ISS
Catalog Number: 25544
Epoch time:      16306
52107948   =   yrday
fracday
Element set:     901
Inclination:       51
6403  deg
RA of node:        93
0681  deg
Eccentricity:     
0006879     
Arg of perigee:   131
8023  deg
Mean anomaly:     228
3719  deg
Mean motion:   15
54414638  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2634
Checksum:              308


Coasting Arc #3 (Orbit 2643)
---------------------------------------

Vector Time (GMT): 2016/307/03:23:29
951
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3292463
68                 A    =         6783191
50  meter
 Y    =       -4098115
13  meter          E    =           
0010568
 Z    =       -4292937
40                 I    =           52
00734
 XDOT =       2907
766677                 Wp   =          110
67383
 YDOT =       6102
266490  meter/sec      RA   =           89
14676  deg
 ZDOT =      -3606
002226                 TA   =          122
70495
                                          MA   =          122
60300
                                          Ha   =            223
660  n
mi
                                          Hp   =            214
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10802046
18                 X    =         3358898
94
 Y    =      -13445259
61  feet           Y    =        -4060925
23  meter
 Z    =      -14084440
28                 Z    =        -4276781
54
 XDOT =       9539
916920                 XDOT =        2856
830333
 YDOT =      20020
559349  feet/sec       YDOT =        6134
498198  meter/sec
 ZDOT =     -11830
715964                 ZDOT =       -3592
000517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13792408
27                 X    =        -4203926
04
 Y    =      -10451657
59  feet           Y    =        -3185665
23  meter
 Z    =      -14012958
06                 Z    =        -4271149
62
 XDOT =      18935
261249                 XDOT =        5771
467629
 YDOT =      -9254
196451  feet/sec       YDOT =       -2820
679078  meter/sec
 ZDOT =     -11770
475451                 ZDOT =       -3587
640918


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   16307
16399036  
00016717  00000-0  10270-3 0  9023
2 25544  51
6418  89
8654 0006925 162
2648 197
8748 15
53582679 26449


Satellite: ISS
Catalog Number: 25544
Epoch time:      16307
16399036   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:        89
8654  deg
Eccentricity:     
0006925     
Arg of perigee:   162
2648  deg
Mean anomaly:     197
8748  deg
Mean motion:   15
53582679  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2644
Checksum:              356


Coasting Arc #4 (Orbit 2659)
---------------------------------------

Vector Time (GMT): 2016/308/03:23:29
951
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3654499
70                 A    =         6780340
21  meter
 Y    =        2740368
70  meter          E    =           
0012132
 Z    =        5008293
27                 I    =           51
99668
 XDOT =      -2356
590415                 Wp   =          146
76444
 YDOT =      -6991
605130  meter/sec      RA   =           84
18413  deg
 ZDOT =       2093
718144                 TA   =          282
89731
                                          MA   =          283
03280
                                          Ha   =            223
577  n
mi
                                          Hp   =            214
541

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11989828
41                 X    =        -3709200
33
 Y    =        8990710
96  feet           Y    =         2699195
84  meter
 Z    =       16431408
36                 Z    =         4990407
29
 XDOT =      -7731
595851                 XDOT =       -2288
403986
 YDOT =     -22938
337040  feet/sec       YDOT =       -7017
576829  meter/sec
 ZDOT =       6869
154015                 ZDOT =        2082
435832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9580948
37                 X    =         2920273
06
 Y    =       11635232
29  feet           Y    =         3546418
80  meter
 Z    =       16352579
23                 Z    =         4984266
15
 XDOT =     -21675
450746                 XDOT =       -6606
677387
 YDOT =       8205
157502  feet/sec       YDOT =        2500
932006  meter/sec
 ZDOT =       6820
996467                 ZDOT =        2079
039723


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   16308
19319066  
00016717  00000-0  10270-3 0  9033
2 25544  51
6420  84
7397 0006981 167
5630 192
5696 15
53595502 26602


Satellite: ISS
Catalog Number: 25544
Epoch time:      16308
19319066   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:        84
7397  deg
Eccentricity:     
0006981     
Arg of perigee:   167
5630  deg
Mean anomaly:     192
5696  deg
Mean motion:   15
53595502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2660
Checksum:              329


Coasting Arc #5 (Orbit 2659)
---------------------------------------

Vector Time (GMT): 2016/308/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4159381
10                 A    =         6780259
84  meter
 Y    =        1829932
44  meter          E    =           
0017049
 Z    =       -5047103
57                 I    =           51
99710
 XDOT =       -795
801150                 Wp   =          125
87362
 YDOT =       7345
315330  meter/sec      RA   =           83
95747  deg
 ZDOT =       2002
383978                 TA   =          163
54238
                                          MA   =          163
48697
                                          Ha   =            223
459  n
mi
                                          Hp   =            214
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13646263
45                 X    =         4163126
46
 Y    =        6003715
34  feet           Y    =         1876466
31  meter
 Z    =      -16558738
73                 Z    =        -5026888
75
 XDOT =      -2610
896162                 XDOT =        -887
606158
 YDOT =      24098
803576  feet/sec       YDOT =        7335
902857  meter/sec
 ZDOT =       6569
501239                 ZDOT =        1998
295010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1717272
16                 X    =          523424
56
 Y    =      -14907364
27  feet           Y    =        -4543764
63  meter
 Z    =      -16470531
24                 Z    =        -5020217
92
 XDOT =      22734
591719                 XDOT =        6929
503556
 YDOT =      -4636
345862  feet/sec       YDOT =       -1413
158219  meter/sec
 ZDOT =       6550
271595                 ZDOT =        1996
522782


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   16308
19319068  
00016717  00000-0  10270-3 0  9046
2 25544  51
6429  84
7400 0006881 167
9378 192
1941 15
53587477 26609


Satellite: ISS
Catalog Number: 25544
Epoch time:      16308
19319068   =   yrday
fracday
Element set:     904
Inclination:       51
6429  deg
RA of node:        84
7400  deg
Eccentricity:     
0006881     
Arg of perigee:   167
9378  deg
Mean anomaly:     192
1941  deg
Mean motion:   15
53587477  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2660
Checksum:              339


Coasting Arc #6 (Orbit 2675)
---------------------------------------

Vector Time (GMT): 2016/309/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4073858
88                 A    =         6782965
86  meter
 Y    =       -3261277
24  meter          E    =           
0011051
 Z    =        4321908
64                 I    =           52
00270
 XDOT =       1536
015610                 Wp   =          109
48903
 YDOT =      -6627
933669  meter/sec      RA   =           78
99406  deg
 ZDOT =      -3549
760618                 TA   =           16
47267
                                          MA   =           16
43679
                                          Ha   =            223
411  n
mi
                                          Hp   =            214
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13365678
74                 X    =        -4058082
10
 Y    =      -10699728
47  feet           Y    =        -3306745
64  meter
 Z    =       14179490
30                 Z    =         4302156
74
 XDOT =       5039
421294                 XDOT =        1627
260290
 YDOT =     -21745
189204  feet/sec       YDOT =       -6610
246740  meter/sec
 ZDOT =     -11646
196252                 ZDOT =       -3542
077231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6018599
37                 X    =        -1834469
09
 Y    =       16103763
59  feet           Y    =         4908427
14  meter
 Z    =       14093571
67                 Z    =         4295720
64
 XDOT =     -21088
411153                 XDOT =       -6427
747719
 YDOT =       2291
247352  feet/sec       YDOT =         698
372193  meter/sec
 ZDOT =     -11611
336050                 ZDOT =       -3539
135228


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   16309
22238282  
00016717  00000-0  10270-3 0  9050
2 25544  51
6434  79
6143 0006721 171
1383 188
9890 15
53621139 26765


Satellite: ISS
Catalog Number: 25544
Epoch time:      16309
22238282   =   yrday
fracday
Element set:     905
Inclination:       51
6434  deg
RA of node:        79
6143  deg
Eccentricity:     
0006721     
Arg of perigee:   171
1383  deg
Mean anomaly:     188
9890  deg
Mean motion:   15
53621139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2676
Checksum:              319


Coasting Arc #7 (Orbit 2690)
---------------------------------------

Vector Time (GMT): 2016/310/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3927630
05                 A    =         6786446
49  meter
 Y    =        4483390
47  meter          E    =           
0007866
 Z    =       -3255940
13                 I    =           52
00657
 XDOT =      -2316
337935                 Wp   =          139
19664
 YDOT =       5507
403626  meter/sec      RA   =           74
03749  deg
 ZDOT =       4790
169494                 TA   =          183
33625
                                          MA   =          183
34150
                                          Ha   =            223
201  n
mi
                                          Hp   =            214
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12885925
36                 X    =         3893019
98
 Y    =       14709286
32  feet           Y    =         4527118
35  meter
 Z    =      -10682218
29                 Z    =        -3236944
38
 XDOT =      -7599
533907                 XDOT =       -2401
020004
 YDOT =      18068
909534  feet/sec       YDOT =        5481
027289  meter/sec
 ZDOT =      15715
779179                 ZDOT =        4778
711407

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9696003
05                 X    =         2955341
73
 Y    =      -17033815
49  feet           Y    =        -5191906
96  meter
 Z    =      -10599840
49                 Z    =        -3230831
38
 XDOT =      18350
417829                 XDOT =        5593
207354
 YDOT =        699
158604  feet/sec       YDOT =         213
103542  meter/sec
 ZDOT =      15664
576786                 ZDOT =        4774
563004


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   16310
18724502  
00016717  00000-0  10270-3 0  9063
2 25544  51
6430  74
8085 0006700 174
9237 185
1984 15
53600493 26919


Satellite: ISS
Catalog Number: 25544
Epoch time:      16310
18724502   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:        74
8085  deg
Eccentricity:     
0006700     
Arg of perigee:   174
9237  deg
Mean anomaly:     185
1984  deg
Mean motion:   15
53600493  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2691
Checksum:              306


Coasting Arc #8 (Orbit 2706)
---------------------------------------

Vector Time (GMT): 2016/311/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3642046
43                 A    =         6789427
45  meter
 Y    =       -5395340
60  meter          E    =           
0017981
 Z    =        1890281
80                 I    =           52
00657
 XDOT =       3155
063287                 Wp   =          133
29554
 YDOT =      -4118
684843  meter/sec      RA   =           69
08923  deg
 ZDOT =      -5655
192969                 TA   =           25
98118
                                          MA   =           25
89102
                                          Ha   =            223
242  n
mi
                                          Hp   =            214
984

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11948971
24                 X    =        -3590626
00
 Y    =      -17701248
70  feet           Y    =        -5435780
90  meter
 Z    =        6201711
93                 Z    =         1872714
26
 XDOT =      10351
257502                 XDOT =        3228
355926
 YDOT =     -13512
745548  feet/sec       YDOT =       -4082
993012  meter/sec
 ZDOT =     -18553
782708                 ZDOT =       -5639
688181

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12543921
88                 X    =        -3823387
39
 Y    =       17311798
56  feet           Y    =         5276636
20  meter
 Z    =        6125765
64                 Z    =         1867133
37
 XDOT =     -15015
018825                 XDOT =       -4576
577738
 YDOT =      -4313
326854  feet/sec       YDOT =       -1314
702025  meter/sec
 ZDOT =     -18485
101821                 ZDOT =       -5634
259035


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   16311
21642614  
00016717  00000-0  10270-3 0  9072
2 25544  51
6429  69
6830 0006817 177
9633 182
1548 15
53588197 27076


Satellite: ISS
Catalog Number: 25544
Epoch time:      16311
21642614   =   yrday
fracday
Element set:     907
Inclination:       51
6429  deg
RA of node:        69
6830  deg
Eccentricity:     
0006817     
Arg of perigee:   177
9633  deg
Mean anomaly:     182
1548  deg
Mean motion:   15
53588197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2707
Checksum:              332


Coasting Arc #9 (Orbit 2712)
---------------------------------------

Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3982936
09                 A    =         6778900
74  meter
 Y    =       -1306782
69  meter          E    =           
0016597
 Z    =       -5340456
01                 I    =           51
96660
 XDOT =       2758
208802                 Wp   =          117
81800
 YDOT =       7136
052557  meter/sec      RA   =           67
08575  deg
 ZDOT =        304
119473                 TA   =          155
11263
                                          MA   =          155
03250
                                          Ha   =            223
185  n
mi
                                          Hp   =            215
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13067375
61                 X    =         4023194
88
 Y    =       -4287344
77  feet           Y    =        -1262017
74  meter
 Z    =      -17521181
13                 Z    =        -5321009
81
 XDOT =       9049
241477                 XDOT =        2676
729336
 YDOT =      23412
245923  feet/sec       YDOT =        7166
441122  meter/sec
 ZDOT =        997
767301                 ZDOT =         317
320433

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1120831
86                 X    =          341629
55
 Y    =       13815480
77  feet           Y    =         4210958
54  meter
 Z    =      -17435757
68                 Z    =        -5314418
94
 XDOT =     -23862
326529                 XDOT =       -7273
237126
 YDOT =       3294
772226  feet/sec       YDOT =        1004
246574  meter/sec
 ZDOT =       1054
258786                 ZDOT =         321
338078


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   16311
60236511  
00016717  00000-0  10270-3 0  9081
2 25544  51
6426  67
7570 0007142 181
2479 178
8656 15
53610659 27139


Satellite: ISS
Catalog Number: 25544
Epoch time:      16311
60236511   =   yrday
fracday
Element set:     908
Inclination:       51
6426  deg
RA of node:        67
7570  deg
Eccentricity:     
0007142     
Arg of perigee:   181
2479  deg
Mean anomaly:     178
8656  deg
Mean motion:   15
53610659  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2713
Checksum:              314


Coasting Arc #10 (Orbit 2728)
---------------------------------------

Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4537914
51                 A    =         6780065
47  meter
 Y    =        -160707
99  meter          E    =           
0005711
 Z    =        5030063
26                 I    =           51
95832
 XDOT =      -1984
458319                 Wp   =          129
75821
 YDOT =      -7129
805793  meter/sec      RA   =           62
11415  deg
 ZDOT =      -2020
130213                 TA   =          339
76387
                                          MA   =          339
78650
                                          Ha   =            223
067  n
mi
                                          Hp   =            215
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14888170
96                 X    =        -4560214
39
 Y    =        -527257
19  feet           Y    =         -211578
61  meter
 Z    =       16502832
23                 Z    =         5007964
74
 XDOT =      -6510
690022                 XDOT =       -1894
770457
 YDOT =     -23391
751290  feet/sec       YDOT =       -7151
495893  meter/sec
 ZDOT =      -6627
723797                 ZDOT =       -2029
552403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3733646
13                 X    =         1138015
34
 Y    =      -14532035
09  feet           Y    =        -4429364
30  meter
 Z    =       16406064
40                 Z    =         5000568
43
 XDOT =      23175
816072                 XDOT =        7063
988739
 YDOT =      -1565
450875  feet/sec       YDOT =        -477
149427  meter/sec
 ZDOT =      -6667
654060                 ZDOT =       -2032
300957


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   16312
63153285  
00016717  00000-0  10270-3 0  9092
2 25544  51
6434  62
6304 0006994 185
1103 174
9979 15
53662003 27290


Satellite: ISS
Catalog Number: 25544
Epoch time:      16312
63153285   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:        62
6304  deg
Eccentricity:     
0006994     
Arg of perigee:   185
1103  deg
Mean anomaly:     174
9979  deg
Mean motion:   15
53662003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2729
Checksum:              316


Coasting Arc #11 (Orbit 2743)
---------------------------------------

Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5014959
91                 A    =         6782951
63  meter
 Y    =        1550527
08  meter          E    =           
0012003
 Z    =       -4308065
27                 I    =           51
95071
 XDOT =        999
714025                 Wp   =          144
56188
 YDOT =       6699
525463  meter/sec      RA   =           57
14767  deg
 ZDOT =       3570
459519                 TA   =          161
76821
                                          MA   =          161
72514
                                          Ha   =            222
859  n
mi
                                          Hp   =            215
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16453280
53                 X    =         5018175
81
 Y    =        5087031
09  feet           Y    =         1606625
59  meter
 Z    =      -14134072
40                 Z    =        -4283695
74
 XDOT =       3279
901656                 XDOT =         907
379919
 YDOT =      21980
070418  feet/sec       YDOT =        6710
188765  meter/sec
 ZDOT =      11714
106032                 ZDOT =        3575
091490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8259630
80                 X    =        -2517535
47
 Y    =       15210675
90  feet           Y    =         4636214
01  meter
 Z    =      -14027621
54                 Z    =        -4275619
04
 XDOT =     -21071
247461                 XDOT =       -6422
516226
 YDOT =       -607
629793  feet/sec       YDOT =        -185
205561  meter/sec
 ZDOT =      11733
125489                 ZDOT =        3576
256649


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   16313
59637261  
00016717  00000-0  10270-3 0  9101
2 25544  51
6421  57
8252 0006999 187
0989 173
0066 15
53664268 27441


Satellite: ISS
Catalog Number: 25544
Epoch time:      16313
59637261   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        57
8252  deg
Eccentricity:     
0006999     
Arg of perigee:   187
0989  deg
Mean anomaly:     173
0066  deg
Mean motion:   15
53664268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2744
Checksum:              336


Coasting Arc #12 (Orbit 2759)
---------------------------------------

Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5304547
60                 A    =         6786398
28  meter
 Y    =       -2746503
01  meter          E    =           
0013764
 Z    =        3202239
67                 I    =           51
94433
 XDOT =        163
833477                 Wp   =          123
50609
 YDOT =      -5959
130533  meter/sec      RA   =           52
18747  deg
 ZDOT =      -4832
149171                 TA   =           19
62157
                                          MA   =           19
56866
                                          Ha   =            222
787  n
mi
                                          Hp   =            215
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17403371
40                 X    =        -5288996
60
 Y    =       -9010836
66  feet           Y    =        -2805734
95  meter
 Z    =       10506035
67                 Z    =         3176508
99
 XDOT =        537
511409                 XDOT =         253
930686
 YDOT =     -19550
953192  feet/sec       YDOT =       -5956
794869  meter/sec
 ZDOT =     -15853
507778                 ZDOT =       -4831
134217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12023799
01                 X    =         3664853
94
 Y    =      -15551376
69  feet           Y    =        -4740059
61  meter
 Z    =       10393855
85                 Z    =         3168047
26
 XDOT =      17979
413697                 XDOT =        5480
125295
 YDOT =       3292
402554  feet/sec       YDOT =        1003
524298  meter/sec
 ZDOT =     -15847
924967                 ZDOT =       -4830
447530


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   16314
62552648  
00016717  00000-0  10270-3 0  9112
2 25544  51
6424  52
6989 0006871 191
8837 168
2154 15
53671956 27602


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
62552648   =   yrday
fracday
Element set:     911
Inclination:       51
6424  deg
RA of node:        52
6989  deg
Eccentricity:     
0006871     
Arg of perigee:   191
8837  deg
Mean anomaly:     168
2154  deg
Mean motion:   15
53671956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2760
Checksum:              338


Coasting Arc #13 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5335930
63                 A    =         6787863
58  meter
 Y    =       -3246933
01  meter          E    =           
0015196
 Z    =        2632606
50                 I    =           51
94121
 XDOT =        772
762625                 Wp   =          128
41315
 YDOT =      -5539
246871  meter/sec      RA   =           50
58878  deg
 ZDOT =      -5254
316254                 TA   =           22
03134
                                          MA   =           21
96609
                                          Ha   =            222
698  n
mi
                                          Hp   =            215
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17506334
09                 X    =        -5312014
29
 Y    =      -10652667
36  feet           Y    =        -3306469
13  meter
 Z    =        8637160
44                 Z    =         2606743
70
 XDOT =       2535
310449                 XDOT =         860
170088
 YDOT =     -18173
382123  feet/sec       YDOT =       -5530
116826  meter/sec
 ZDOT =     -17238
570388                 ZDOT =       -5250
349758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19830677
65                 X    =        -6044390
55
 Y    =       -5350581
00  feet           Y    =        -1630857
09  meter
 Z    =        8524500
14                 Z    =         2598267
64
 XDOT =      -2899
456976                 XDOT =        -883
754486
 YDOT =     -16748
381449  feet/sec       YDOT =       -5104
906666  meter/sec
 ZDOT =     -17220
137370                 ZDOT =       -5248
697871


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   16314
94713717  
00016717  00000-0  10270-3 0  9124
2 25544  51
6410  51
0976 0006554 192
4411 167
6581 15
53648523 27655


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
94713717   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:        51
0976  deg
Eccentricity:     
0006554     
Arg of perigee:   192
4411  deg
Mean anomaly:     167
6581  deg
Mean motion:   15
53648523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              313


Coasting Arc #14 (Orbit 2779)
---------------------------------------

Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5292676
74                 A    =         6790110
93  meter
 Y    =        4085196
80  meter          E    =           
0004111
 Z    =       -1184119
03                 I    =           51
92801
 XDOT =      -2109
638335                 Wp   =           73
88516
 YDOT =       4433
037891  meter/sec      RA   =           45
63741  deg
 ZDOT =       5882
476090                 TA   =          273
31619
                                          MA   =          273
36323
                                          Ha   =            222
431  n
mi
                                          Hp   =            215
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17364425
00                 X    =         5252353
71
 Y    =       13402876
65  feet           Y    =         4144157
55  meter
 Z    =       -3884904
96                 Z    =        -1158506
17
 XDOT =      -6921
385613                 XDOT =       -2187
628001
 YDOT =      14544
087568  feet/sec       YDOT =        4409
010722  meter/sec
 ZDOT =      19299
462238                 ZDOT =        5872
038145

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20564645
79                 X    =         6268104
04
 Y    =        7688225
07  feet           Y    =         2343371
00  meter
 Z    =       -3773510
73                 Z    =        -1150166
07
 XDOT =      -1890
363475                 XDOT =        -576
182787
 YDOT =      14476
137076  feet/sec       YDOT =        4412
326581  meter/sec
 ZDOT =      19252
891079                 ZDOT =        5868
281201


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   16315
91195751  
00016717  00000-0  10270-3 0  9135
2 25544  51
6413  46
2915 0006470 196
1138 163
9810 15
53664508 27803


Satellite: ISS
Catalog Number: 25544
Epoch time:      16315
91195751   =   yrday
fracday
Element set:     913
Inclination:       51
6413  deg
RA of node:        46
2915  deg
Eccentricity:     
0006470     
Arg of perigee:   196
1138  deg
Mean anomaly:     163
9810  deg
Mean motion:   15
53664508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2780
Checksum:              312


Coasting Arc #15 (Orbit 2795)
---------------------------------------

Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4925979
05                 A    =         6790590
38  meter
 Y    =       -4643601
91  meter          E    =           
0015294
 Z    =        -394933
03                 I    =           51
90700
 XDOT =       3504
293174                 Wp   =          159
29959
 YDOT =      -3212
458135  meter/sec      RA   =           40
68866  deg
 ZDOT =      -6021
800407                 TA   =           24
94425
                                          MA   =           24
87041
                                          Ha   =            222
280  n
mi
                                          Hp   =            215
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16161348
58                 X    =        -4871768
53
 Y    =      -15234914
41  feet           Y    =        -4698384
43  meter
 Z    =       -1295712
03                 Z    =         -418730
88
 XDOT =      11497
024848                 XDOT =        3569
207259
 YDOT =     -10539
560810  feet/sec       YDOT =       -3172
908087  meter/sec
 ZDOT =     -19756
563014                 ZDOT =       -6004
619211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20088102
50                 X    =        -6122853
64
 Y    =       -9459466
75  feet           Y    =        -2883245
47  meter
 Z    =       -1399035
98                 Z    =         -426426
17
 XDOT =       7082
487151                 XDOT =        2158
742084
 YDOT =     -12167
750347  feet/sec       YDOT =       -3708
730306  meter/sec
 ZDOT =     -19680
691188                 ZDOT =       -5998
674674


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   16316
94109109  
00016717  00000-0  10270-3 0  9142
2 25544  51
6418  41
1651 0006408 200
0739 160
0162 15
53669562 27962


Satellite: ISS
Catalog Number: 25544
Epoch time:      16316
94109109   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:        41
1651  deg
Eccentricity:     
0006408     
Arg of perigee:   200
0739  deg
Mean anomaly:     160
0162  deg
Mean motion:   15
53669562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2796
Checksum:              298


Coasting Arc #16 (Orbit 2811)
---------------------------------------

Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4263997
68                 A    =         6788995
51  meter
 Y    =        4920265
78  meter          E    =           
0010259
 Z    =        1915688
95                 I    =           51
87699
 XDOT =      -4816
788290                 Wp   =           92
64482
 YDOT =       1973
465296  meter/sec      RA   =           35
73721  deg
 ZDOT =       5626
264672                 TA   =          288
38199
                                          MA   =          288
49353
                                          Ha   =            222
107  n
mi
                                          Hp   =            215
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13989493
71                 X    =         4199355
25
 Y    =       16142604
25  feet           Y    =         4967587
28  meter
 Z    =        6285068
75                 Z    =         1936245
80
 XDOT =     -15803
111187                 XDOT =       -4865
828802
 YDOT =       6474
623673  feet/sec       YDOT =        1919
326691  meter/sec
 ZDOT =      18458
873597                 ZDOT =        5602
746112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18462078
06                 X    =         5627241
39
 Y    =       10691764
56  feet           Y    =         3258849
84  meter
 Z    =        6374130
53                 Z    =         1942834
99
 XDOT =     -12147
944160                 XDOT =       -3702
693380
 YDOT =       9982
548998  feet/sec       YDOT =        3042
680935  meter/sec
 ZDOT =      18355
488919                 ZDOT =        5594
753023


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   16317
97021547  
00016717  00000-0  10270-3 0  9156
2 25544  51
6419  36
0392 0006441 204
4383 155
6465 15
53693820 28127


Satellite: ISS
Catalog Number: 25544
Epoch time:      16317
97021547   =   yrday
fracday
Element set:     915
Inclination:       51
6419  deg
RA of node:        36
0392  deg
Eccentricity:     
0006441     
Arg of perigee:   204
4383  deg
Mean anomaly:     155
6465  deg
Mean motion:   15
53693820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2812
Checksum:              307


Coasting Arc #17 (Orbit 2826)
---------------------------------------

Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3252244
38                 A    =         6785842
00  meter
 Y    =       -4954795
17  meter          E    =           
0006129
 Z    =       -3299721
27                 I    =           51
84129
 XDOT =       5977
600659                 Wp   =          163
22698
 YDOT =       -773
307470  meter/sec      RA   =           30
77748  deg
 ZDOT =      -4738
320686                 TA   =           54
98979
                                          MA   =           54
93228
                                          Ha   =            221
865  n
mi
                                          Hp   =            216
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10670093
11                 X    =        -3180567
79
 Y    =      -16255889
67  feet           Y    =        -4990763
19  meter
 Z    =      -10825857
18                 Z    =        -3315346
20
 XDOT =      19611
550717                 XDOT =        6008
821095
 YDOT =      -2537
097998  feet/sec       YDOT =        -706
287376  meter/sec
 ZDOT =     -15545
671543                 ZDOT =       -4709
206323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15537116
08                 X    =        -4735712
98
 Y    =      -11629189
50  feet           Y    =        -3544576
96  meter
 Z    =      -10893300
48                 Z    =        -3320277
99
 XDOT =      16793
951610                 XDOT =        5118
796451
 YDOT =      -8019
250492  feet/sec       YDOT =       -2444
267550  meter/sec
 ZDOT =     -15418
020023                 ZDOT =       -4699
412503


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   16318
93501034  
00016717  00000-0  10270-3 0  9168
2 25544  51
6431  31
2331 0006277 208
2832 151
7980 15
53719642 28275


Satellite: ISS
Catalog Number: 25544
Epoch time:      16318
93501034   =   yrday
fracday
Element set:     916
Inclination:       51
6431  deg
RA of node:        31
2331  deg
Eccentricity:     
0006277     
Arg of perigee:   208
2832  deg
Mean anomaly:     151
7980  deg
Mean motion:   15
53719642  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2827
Checksum:              297


Coasting Arc #18 (Orbit 2842)
---------------------------------------

Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893386
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1994793
35                 A    =         6782349
80  meter
 Y    =        4786176
80  meter          E    =           
0010206
 Z    =        4372046
89                 I    =           51
80095
 XDOT =      -6843
786520                 Wp   =          145
90981
 YDOT =       -301
938136  meter/sec      RA   =           25
80803  deg
 ZDOT =       3440
952590                 TA   =          269
20069
                                          MA   =          269
31764
                                          Ha   =            221
746  n
mi
                                          Hp   =            216
211

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6544597
60                 X    =         1919886
73
 Y    =       15702679
78  feet           Y    =         4808064
98  meter
 Z    =       14343985
87                 Z    =         4381555
54
 XDOT =     -22453
367847                 XDOT =       -6856
616649
 YDOT =       -990
610684  feet/sec       YDOT =        -378
541773  meter/sec
 ZDOT =      11289
214534                 ZDOT =        3407
675093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11665158
65                 X    =         3555540
36
 Y    =       12335365
88  feet           Y    =         3759819
52  meter
 Z    =       14384667
63                 Z    =         4384446
69
 XDOT =     -20476
687742                 XDOT =       -6241
294424
 YDOT =       6322
989379  feet/sec       YDOT =        1927
247163  meter/sec
 ZDOT =      11143
549645                 ZDOT =        3396
553932


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   16319
96411570  
00016717  00000-0  10270-3 0  9178
2 25544  51
6426  26
1071 0006291 211
6181 148
4594 15
53727919 28432


Satellite: ISS
Catalog Number: 25544
Epoch time:      16319
96411570   =   yrday
fracday
Element set:     917
Inclination:       51
6426  deg
RA of node:        26
1071  deg
Eccentricity:     
0006291     
Arg of perigee:   211
6181  deg
Mean anomaly:     148
4594  deg
Mean motion:   15
53727919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2843
Checksum:              314
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