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

 
Date: November 9th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


314/21:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 215 7

322/07:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 216 8

322/20:20:13 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 217 0

324/22:00:36 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 217 3

326/13:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 217 4

Coasting Arc #1 (Orbit 2726)
---------------------------------------

Vector Time (GMT): 2016/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4106321
12                 A    =         6789962
12  meter
 Y    =        5161779
43  meter          E    =           
0004379
 Z    =       -1617612
29                 I    =           51
99124
 XDOT =      -2924
240691                 Wp   =          100
37072
 YDOT =       4125
608624  meter/sec      RA   =           62
54698  deg
 ZDOT =       5753
996816                 TA   =          242
03349
                                          MA   =          242
07782
                                          Ha   =            223
166  n
mi
                                          Hp   =            215
346

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13472182
17                 X    =         4056153
37
 Y    =       16934971
87  feet           Y    =         5207418
54  meter
 Z    =       -5307126
92                 Z    =        -1597786
45
 XDOT =      -9593
965523                 XDOT =       -2998
107798
 YDOT =      13535
461364  feet/sec       YDOT =        4092
494863  meter/sec
 ZDOT =      18877
942309                 ZDOT =        5739
611914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21573107
30                 X    =        -6575483
11
 Y    =       -1948872
22  feet           Y    =         -594016
25  meter
 Z    =       -5221254
58                 Z    =        -1591438
40
 XDOT =      -3205
946449                 XDOT =        -977
172478
 YDOT =     -14805
815660  feet/sec       YDOT =       -4512
812613  meter/sec
 ZDOT =      18814
156203                 ZDOT =        5734
554811


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
50311535  
00016717  00000-0  10270-3 0  9003
2 25544  51
6431  63
2713 0007159 184
8145 175
2940 15
53539505 27274


Satellite: ISS
Catalog Number: 25544
Epoch time:      16312
50311535   =   yrday
fracday
Element set:     900
Inclination:       51
6431  deg
RA of node:        63
2713  deg
Eccentricity:     
0007159     
Arg of perigee:   184
8145  deg
Mean anomaly:     175
2940  deg
Mean motion:   15
53539505  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2727
Checksum:              291


Coasting Arc #2 (Orbit 2742)
---------------------------------------

Vector Time (GMT): 2016/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3692522
91                 A    =         6791012
64  meter
 Y    =       -5685892
45  meter          E    =           
0017499
 Z    =          91277
00                 I    =           51
97833
 XDOT =       3916
830055                 Wp   =          153
36325
 YDOT =      -2647
608509  meter/sec      RA   =           57
60272  deg
 ZDOT =      -6043
959833                 TA   =           25
65759
                                          MA   =           25
57087
                                          Ha   =            223
097  n
mi
                                          Hp   =            215
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12114576
49                 X    =        -3629110
76
 Y    =      -18654502
80  feet           Y    =        -5726830
16  meter
 Z    =         299465
24                 Z    =           73493
58
 XDOT =      12850
492305                 XDOT =        3975
504544
 YDOT =      -8686
379622  feet/sec       YDOT =       -2603
479977  meter/sec
 ZDOT =     -19829
264544                 ZDOT =       -6024
790004

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21922879
32                 X    =         6682093
62
 Y    =        3765754
72  feet           Y    =         1147802
04  meter
 Z    =         222646
11                 Z    =           67862
54
 XDOT =      -2155
667656                 XDOT =        -657
047502
 YDOT =      13829
416150  feet/sec       YDOT =        4215
206043  meter/sec
 ZDOT =     -19744
794084                 ZDOT =       -6018
213237


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
53232747  
00016717  00000-0  10270-3 0  9015
2 25544  51
6422  58
1455 0007280 188
4208 171
6823 15
53550946 27435


Satellite: ISS
Catalog Number: 25544
Epoch time:      16313
53232747   =   yrday
fracday
Element set:     901
Inclination:       51
6422  deg
RA of node:        58
1455  deg
Eccentricity:     
0007280     
Arg of perigee:   188
4208  deg
Mean anomaly:     171
6823  deg
Mean motion:   15
53550946  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2743
Checksum:              304


Coasting Arc #3 (Orbit 2758)
---------------------------------------

Vector Time (GMT): 2016/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3092117
19                 A    =         6790085
39  meter
 Y    =        5875638
11  meter          E    =           
0010617
 Z    =        1413167
06                 I    =           51
95829
 XDOT =      -4853
489812                 Wp   =           91
24951
 YDOT =       1145
445010  meter/sec      RA   =           52
65735  deg
 ZDOT =       5819
396494                 TA   =          284
07761
                                          MA   =          284
19559
                                          Ha   =            222
899  n
mi
                                          Hp   =            215
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10144741
43                 X    =         3019319
82
 Y    =       19277027
93  feet           Y    =         5909809
27  meter
 Z    =        4636374
88                 Z    =         1428010
97
 XDOT =     -15923
523004                 XDOT =       -4894
206301
 YDOT =       3758
021686  feet/sec       YDOT =        1090
942598  meter/sec
 ZDOT =      19092
508181                 ZDOT =        5795
720154

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21115728
82                 X    =        -6436074
15
 Y    =       -5296129
41  feet           Y    =        -1614260
24  meter
 Z    =        4700272
97                 Z    =         1432643
20
 XDOT =       7498
009078                 XDOT =        2285
393167
 YDOT =     -12933
575689  feet/sec       YDOT =       -3942
153870  meter/sec
 ZDOT =      18988
583695                 ZDOT =        5787
720310


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
56153468  
00016717  00000-0  10270-3 0  9022
2 25544  51
6431  53
0198 0007165 192
2869 167
8109 15
53569474 27598


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
56153468   =   yrday
fracday
Element set:     902
Inclination:       51
6431  deg
RA of node:        53
0198  deg
Eccentricity:     
0007165     
Arg of perigee:   192
2869  deg
Mean anomaly:     167
8109  deg
Mean motion:   15
53569474  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2759
Checksum:              334


Coasting Arc #4 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5356239
91                 A    =         6787747
46  meter
 Y    =       -3078449
08  meter          E    =           
0014632
 Z    =        2789553
72                 I    =           51
94017
 XDOT =        566
742867                 Wp   =          127
41358
 YDOT =      -5661
047717  meter/sec      RA   =           50
59179  deg
 ZDOT =      -5149
320277                 TA   =           21
07510
                                          MA   =           21
01487
                                          Ha   =            222
797  n
mi
                                          Hp   =            215
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17572965
57                 X    =        -5334968
48
 Y    =      -10099898
57  feet           Y    =        -3138227
10  meter
 Z    =        9152079
12                 Z    =         2763585
82
 XDOT =       1859
392609                 XDOT =         655
017617
 YDOT =     -18572
991196  feet/sec       YDOT =       -5654
216669  meter/sec
 ZDOT =     -16894
095398                 ZDOT =       -5146
352478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19744225
64                 X    =        -6018039
97
 Y    =       -4800102
91  feet           Y    =        -1463071
37  meter
 Z    =        9038926
29                 Z    =         2755064
73
 XDOT =      -3621
794963                 XDOT =       -1103
923105
 YDOT =     -16950
021563  feet/sec       YDOT =       -5166
366572  meter/sec
 ZDOT =     -16880
013471                 ZDOT =       -5145
028106


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
94748711  
00016717  00000-0  10270-3 0  9036
2 25544  51
6410  51
1000 0006640 194
4291 165
6672 15
53565859 27657


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
94748711   =   yrday
fracday
Element set:     903
Inclination:       51
6410  deg
RA of node:        51
1000  deg
Eccentricity:     
0006640     
Arg of perigee:   194
4291  deg
Mean anomaly:     165
6672  deg
Mean motion:   15
53565859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              307


Coasting Arc #5 (Orbit 2779)
---------------------------------------

Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5362131
99                 A    =         6790163
29  meter
 Y    =        3927862
33  meter          E    =           
0003353
 Z    =       -1388320
40                 I    =           51
92746
 XDOT =      -1872
799463                 Wp   =           78
07707
 YDOT =       4611
102913  meter/sec      RA   =           45
64013  deg
 ZDOT =       5825
021439                 TA   =          266
86969
                                          MA   =          266
90805
                                          Ha   =            222
533  n
mi
                                          Hp   =            215
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17592296
55                 X    =         5324555
09
 Y    =       12886687
44  feet           Y    =         3987615
12  meter
 Z    =       -4554856
95                 Z    =        -1362363
46
 XDOT =      -6144
355193                 XDOT =       -1952
518805
 YDOT =      15128
290396  feet/sec       YDOT =        4589
714561  meter/sec
 ZDOT =      19110
962727                 ZDOT =        5815
729811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20634553
16                 X    =         6289411
80
 Y    =        7126489
15  feet           Y    =         2172153
89  meter
 Z    =       -4441925
37                 Z    =        -1353898
85
 XDOT =      -1015
580278                 XDOT =        -309
548869
 YDOT =      14800
180928  feet/sec       YDOT =        4511
095147  meter/sec
 ZDOT =      19069
377996                 ZDOT =        5812
346413


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
91236125  
00016717  00000-0  10270-3 0  9046
2 25544  51
6413  46
2943 0006560 198
2031 161
8887 15
53572335 27806


Satellite: ISS
Catalog Number: 25544
Epoch time:      16315
91236125   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:        46
2943  deg
Eccentricity:     
0006560     
Arg of perigee:   198
2031  deg
Mean anomaly:     161
8887  deg
Mean motion:   15
53572335  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2780
Checksum:              306


Coasting Arc #6 (Orbit 2795)
---------------------------------------

Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5061221
88                 A    =         6790930
97  meter
 Y    =       -4510607
85  meter          E    =           
0015575
 Z    =        -153375
08                 I    =           51
90738
 XDOT =       3248
400719                 Wp   =          158
13166
 YDOT =      -3446
856910  meter/sec      RA   =           40
69157  deg
 ZDOT =      -6035
812938                 TA   =           23
51516
                                          MA   =           23
44402
                                          Ha   =            222
401  n
mi
                                          Hp   =            216
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16605058
65                 X    =        -5009661
89
 Y    =      -14798582
20  feet           Y    =        -4566917
55  meter
 Z    =        -503199
07                 Z    =         -177836
37
 XDOT =      10657
482673                 XDOT =        3316
022998
 YDOT =     -11308
585662  feet/sec       YDOT =       -3410
153282  meter/sec
 ZDOT =     -19802
535887                 ZDOT =       -6019
868245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20379053
24                 X    =        -6211535
43
 Y    =       -8905165
44  feet           Y    =        -2714294
43  meter
 Z    =        -609454
48                 Z    =         -185761
73
 XDOT =       6086
209391                 XDOT =        1855
076622
 YDOT =     -12616
602884  feet/sec       YDOT =       -3845
540559  meter/sec
 ZDOT =     -19732
033959                 ZDOT =       -6014
323951


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
94155572  
00016717  00000-0  10270-3 0  9057
2 25544  51
6419  41
1683 0006517 202
0338 158
0535 15
53574155 27960


Satellite: ISS
Catalog Number: 25544
Epoch time:      16316
94155572   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:        41
1683  deg
Eccentricity:     
0006517     
Arg of perigee:   202
0338  deg
Mean anomaly:     158
0535  deg
Mean motion:   15
53574155  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2796
Checksum:              311


Coasting Arc #7 (Orbit 2811)
---------------------------------------

Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4476792
90                 A    =         6789677
40  meter
 Y    =        4824812
46  meter          E    =           
0009644
 Z    =        1658104
80                 I    =           51
87845
 XDOT =      -4563
546003                 Wp   =           88
47782
 YDOT =       2255
420255  meter/sec      RA   =           35
74112  deg
 ZDOT =       5729
930655                 TA   =          289
61290
                                          MA   =          289
71697
                                          Ha   =            222
225  n
mi
                                          Hp   =            216
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14687640
74                 X    =         4414453
30
 Y    =       15829437
21  feet           Y    =         4874526
45  meter
 Z    =        5439976
38                 Z    =         1679700
98
 XDOT =     -14972
263788                 XDOT =       -4616
261807
 YDOT =       7399
672754  feet/sec       YDOT =        2204
093030  meter/sec
 ZDOT =      18798
985090                 ZDOT =        5707
633381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19024495
64                 X    =         5798666
27
 Y    =       10165577
10  feet           Y    =         3098467
90  meter
 Z    =        5533608
55                 Z    =         1686643
89
 XDOT =     -11100
650404                 XDOT =       -3383
478243
 YDOT =      10544
635868  feet/sec       YDOT =        3214
005013  meter/sec
 ZDOT =      18700
893613                 ZDOT =        5700
032373


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
97074445  
00016717  00000-0  10270-3 0  9061
2 25544  51
6419  36
0428 0006557 206
4586 153
6233 15
53594592 28129


Satellite: ISS
Catalog Number: 25544
Epoch time:      16317
97074445   =   yrday
fracday
Element set:     906
Inclination:       51
6419  deg
RA of node:        36
0428  deg
Eccentricity:     
0006557     
Arg of perigee:   206
4586  deg
Mean anomaly:     153
6233  deg
Mean motion:   15
53594592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2812
Checksum:              324


Coasting Arc #8 (Orbit 2826)
---------------------------------------

Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3552097
91                 A    =         6786817
78  meter
 Y    =       -4907378
69  meter          E    =           
0006919
 Z    =       -3052139
64                 I    =           51
84371
 XDOT =       5755
508341                 Wp   =          170
53617
 YDOT =      -1094
816096  meter/sec      RA   =           30
78338  deg
 ZDOT =      -4946
236089                 TA   =           44
36774
                                          MA   =           44
31232
                                          Ha   =            221
986  n
mi
                                          Hp   =            216
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11653864
55                 X    =        -3482131
94
 Y    =      -16100323
78  feet           Y    =        -4946709
44  meter
 Z    =      -10013581
48                 Z    =        -3069225
38
 XDOT =      18882
901382                 XDOT =        5791
350469
 YDOT =      -3591
916326  feet/sec       YDOT =       -1030
253747  meter/sec
 ZDOT =     -16227
808690                 ZDOT =       -4918
189399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16412568
03                 X    =        -5002550
74
 Y    =      -11143434
72  feet           Y    =        -3396518
90  meter
 Z    =      -10087431
40                 Z    =        -3074649
09
 XDOT =      15786
994212                 XDOT =        4811
875836
 YDOT =      -8697
505903  feet/sec       YDOT =       -2650
999799  meter/sec
 ZDOT =     -16104
769027                 ZDOT =       -4908
733599


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
93560295  
00016717  00000-0  10270-3 0  9072
2 25544  51
6432  31
2371 0006411 210
3957 149
6825 15
53613172 28277


Satellite: ISS
Catalog Number: 25544
Epoch time:      16318
93560295   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:        31
2371  deg
Eccentricity:     
0006411     
Arg of perigee:   210
3957  deg
Mean anomaly:     149
6825  deg
Mean motion:   15
53613172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2827
Checksum:              303


Coasting Arc #9 (Orbit 2842)
---------------------------------------

Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2380479
23                 A    =         6783422
68  meter
 Y    =        4793941
71  meter          E    =           
0010209
 Z    =        4167154
87                 I    =           51
80362
 XDOT =      -6684
250866                 Wp   =          140
81175
 YDOT =         46
206658  meter/sec      RA   =           25
81647  deg
 ZDOT =       3752
470134                 TA   =          270
60320
                                          MA   =          270
72019
                                          Ha   =            221
876  n
mi
                                          Hp   =            216
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7809971
22                 X    =         2306452
42
 Y    =       15728155
21  feet           Y    =         4820147
82  meter
 Z    =       13671767
94                 Z    =         4178539
27
 XDOT =     -21929
956909                 XDOT =       -6702
499157
 YDOT =        151
596648  feet/sec       YDOT =         -28
643246  meter/sec
 ZDOT =      12311
253721                 ZDOT =        3719
954491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12859134
41                 X    =         3919464
17
 Y    =       11902682
26  feet           Y    =         3627937
55  meter
 Z    =       13720662
26                 Z    =         4182057
86
 XDOT =     -19615
398736                 XDOT =       -5978
773535
 YDOT =       7116
118811  feet/sec       YDOT =        2168
993014  meter/sec
 ZDOT =      12168
855387                 ZDOT =        3709
067122


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
96477969  
00016717  00000-0  10270-3 0  9082
2 25544  51
6427  26
1115 0006391 213
6983 146
3764 15
53612389 28435


Satellite: ISS
Catalog Number: 25544
Epoch time:      16319
96477969   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:        26
1115  deg
Eccentricity:     
0006391     
Arg of perigee:   213
6983  deg
Mean anomaly:     146
3764  deg
Mean motion:   15
53612389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2843
Checksum:              341


Coasting Arc #10 (Orbit 2857)
---------------------------------------

Vector Time (GMT): 2016/320/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -958329
52                 A    =         6780354
11  meter
 Y    =       -4539090
15  meter          E    =           
0008222
 Z    =       -4951286
19                 I    =           51
76449
 XDOT =       7276
288201                 Wp   =          100
77844
 YDOT =        890
294246  meter/sec      RA   =           20
83880  deg
 ZDOT =      -2229
155226                 TA   =          147
50680
                                          MA   =          147
45616
                                          Ha   =            221
702  n
mi
                                          Hp   =            216
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3144125
73                 X    =         -883449
24
 Y    =      -14892028
04  feet           Y    =        -4549387
92  meter
 Z    =      -16244377
27                 Z    =        -4955759
96
 XDOT =      23872
336618                 XDOT =        7276
620443
 YDOT =       2920
912879  feet/sec       YDOT =         971
664544  meter/sec
 ZDOT =      -7313
501396                 ZDOT =       -2193
807145

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8408267
80                 X    =        -2562840
03
 Y    =      -12663015
93  feet           Y    =        -3859687
26  meter
 Z    =      -16263052
56                 Z    =        -4956978
42
 XDOT =      22342
362043                 XDOT =        6809
951951
 YDOT =      -5660
774541  feet/sec       YDOT =       -1725
404080  meter/sec
 ZDOT =      -7158
890755                 ZDOT =       -2182
029902


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   16320
92962841  
00016717  00000-0  10270-3 0  9099
2 25544  51
6431  21
3060 0006330 217
6786 142
3924 15
53637196 28587


Satellite: ISS
Catalog Number: 25544
Epoch time:      16320
92962841   =   yrday
fracday
Element set:     909
Inclination:       51
6431  deg
RA of node:        21
3060  deg
Eccentricity:     
0006330     
Arg of perigee:   217
6786  deg
Mean anomaly:     142
3924  deg
Mean motion:   15
53637196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2858
Checksum:              310


Coasting Arc #11 (Orbit 2873)
---------------------------------------

Vector Time (GMT): 2016/321/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -563336
87                 A    =         6778785
34  meter
 Y    =        4188455
12  meter          E    =           
0006041
 Z    =        5302123
54                 I    =           51
72885
 XDOT =      -7460
542781                 Wp   =          197
25670
 YDOT =      -1682
925216  meter/sec      RA   =           15
85359  deg
 ZDOT =        531
298324                 TA   =          247
64704
                                          MA   =          247
71107
                                          Ha   =            221
500  n
mi
                                          Hp   =            216
826

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1848218
07                 X    =         -635887
29
 Y    =       13741650
66  feet           Y    =         4181749
56  meter
 Z    =       17395418
43                 Z    =         5299210
95
 XDOT =     -24476
846395                 XDOT =       -7443
750260
 YDOT =      -5521
408188  feet/sec       YDOT =       -1766
260150  meter/sec
 ZDOT =       1743
104739                 ZDOT =         495
096893

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3573735
12                 X    =         1089274
47
 Y    =       13414558
93  feet           Y    =         4088757
56  meter
 Z    =       17381814
67                 Z    =         5297977
11
 XDOT =     -23717
135807                 XDOT =       -7228
982994
 YDOT =       4241
458406  feet/sec       YDOT =        1292
796522  meter/sec
 ZDOT =       1584
920319                 ZDOT =         483
083713


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   16321
95879351  
00016717  00000-0  10270-3 0  9108
2 25544  51
6430  16
1800 0006501 222
7688 137
2959 15
53662043 28746


Satellite: ISS
Catalog Number: 25544
Epoch time:      16321
95879351   =   yrday
fracday
Element set:     910
Inclination:       51
6430  deg
RA of node:        16
1800  deg
Eccentricity:     
0006501     
Arg of perigee:   222
7688  deg
Mean anomaly:     137
2959  deg
Mean motion:   15
53662043  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2874
Checksum:              308


Coasting Arc #12 (Orbit 2879)
---------------------------------------

Vector Time (GMT): 2016/322/07:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4582573
66                 A    =         6782849
84  meter
 Y    =        2420367
55  meter          E    =           
0005287
 Z    =        4370487
56                 I    =           51
72909
 XDOT =      -5465
432920                 Wp   =          113
73718
 YDOT =      -4141
194521  meter/sec      RA   =           13
86516  deg
 ZDOT =      -3436
061534                 TA   =           11
06262
                                          MA   =           11
05100
                                          Ha   =            221
865  n
mi
                                          Hp   =            216
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15034690
50                 X    =        -4630528
54
 Y    =        7940838
42  feet           Y    =         2368853
76  meter
 Z    =       14338869
94                 Z    =         4348109
85
 XDOT =     -17931
210368                 XDOT =       -5402
027638
 YDOT =     -13586
596199  feet/sec       YDOT =       -4201
957946  meter/sec
 ZDOT =     -11273
167763                 ZDOT =       -3462
457907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16672329
93                 X    =         5081726
16
 Y    =       -3734544
70  feet           Y    =        -1138289
23  meter
 Z    =       14240386
76                 Z    =         4340469
88
 XDOT =      13437
051664                 XDOT =        4095
613347
 YDOT =      16548
708057  feet/sec       YDOT =        5044
046216  meter/sec
 ZDOT =     -11387
915558                 ZDOT =       -3471
036662


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   16322
34473081  
00016717  00000-0  10270-3 0  9113
2 25544  51
6426  14
2526 0006766 219
9083 140
1572 15
53607655 28804


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
34473081   =   yrday
fracday
Element set:     911
Inclination:       51
6426  deg
RA of node:        14
2526  deg
Eccentricity:     
0006766     
Arg of perigee:   219
9083  deg
Mean anomaly:     140
1572  deg
Mean motion:   15
53607655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2880
Checksum:              301


Coasting Arc #13 (Orbit 2887)
---------------------------------------

Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3333709
02                 A    =         6780643
92  meter
 Y    =       -3293490
04  meter          E    =           
0010501
 Z    =       -4909542
23                 I    =           51
70462
 XDOT =       6571
550632                 Wp   =          138
34333
 YDOT =       3172
000526  meter/sec      RA   =           11
16501  deg
 ZDOT =       2329
574565                 TA   =          154
48216
                                          MA   =          154
43028
                                          Ha   =            221
396  n
mi
                                          Hp   =            217
045

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10937365
57                 X    =         3394138
67
 Y    =      -10805413
53  feet           Y    =        -3255872
12  meter
 Z    =      -16107422
03                 Z    =        -4893201
09
 XDOT =      21560
205487                 XDOT =        6524
275872
 YDOT =      10406
825874  feet/sec       YDOT =        3245
223562  meter/sec
 ZDOT =       7642
961170                 ZDOT =        2361
383301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10751734
22                 X    =         3277128
59
 Y    =      -11095256
14  feet           Y    =        -3381834
07  meter
 Z    =      -16035194
84                 Z    =        -4887527
39
 XDOT =      20968
980125                 XDOT =        6391
345142
 YDOT =       9050
711320  feet/sec       YDOT =        2758
656810  meter/sec
 ZDOT =       7781
604845                 ZDOT =        2371
833157


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   16322
85930994  
00016717  00000-0  10270-3 0  9121
2 25544  51
6423  11
6931 0006281 225
7659 134
2978 15
53640249 28886


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
85930994   =   yrday
fracday
Element set:     912
Inclination:       51
6423  deg
RA of node:        11
6931  deg
Eccentricity:     
0006281     
Arg of perigee:   225
7659  deg
Mean anomaly:     134
2978  deg
Mean motion:   15
53640249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2888
Checksum:              331


Coasting Arc #14 (Orbit 2903)
---------------------------------------

Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4645183
20                 A    =         6783742
69  meter
 Y    =        2754933
84  meter          E    =           
0005890
 Z    =        4098987
44                 I    =           51
68281
 XDOT =      -5550
173600                 Wp   =          107
09696
 YDOT =      -3649
028875  meter/sec      RA   =            6
18257  deg
 ZDOT =      -3834
367624                 TA   =           22
49976
                                          MA   =           22
47394
                                          Ha   =            221
333  n
mi
                                          Hp   =            217
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15240102
37                 X    =        -4695555
65
 Y    =        9038496
85  feet           Y    =         2702706
46  meter
 Z    =       13448121
53                 Z    =         4076299
85
 XDOT =     -18209
230972                 XDOT =       -5490
330832
 YDOT =     -11971
879510  feet/sec       YDOT =       -3710
759877  meter/sec
 ZDOT =     -12579
946272                 ZDOT =       -3861
184052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14917758
34                 X    =        -4546932
74
 Y    =        9700143
20  feet           Y    =         2956603
65  meter
 Z    =       13348214
35                 Z    =         4068535
73
 XDOT =     -17925
310093                 XDOT =       -5463
634516
 YDOT =     -10082
533054  feet/sec       YDOT =       -3073
156075  meter/sec
 ZDOT =     -12696
629130                 ZDOT =       -3869
932559


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   16323
88846722  
00016717  00000-0  10270-3 0  9131
2 25544  51
6420   6
5678 0006289 229
6156 130
4448 15
53634868 29046


Satellite: ISS
Catalog Number: 25544
Epoch time:      16323
88846722   =   yrday
fracday
Element set:     913
Inclination:       51
6420  deg
RA of node:         6
5678  deg
Eccentricity:     
0006289     
Arg of perigee:   229
6156  deg
Mean anomaly:     130
4448  deg
Mean motion:   15
53634868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2904
Checksum:              331


Coasting Arc #15 (Orbit 2918)
---------------------------------------

Vector Time (GMT): 2016/324/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5702687
14                 A    =         6787126
30  meter
 Y    =       -2209426
01  meter          E    =           
0002057
 Z    =       -2944848
09                 I    =           51
66274
 XDOT =       4155
294184                 Wp   =          207
19540
 YDOT =       4047
616537  meter/sec      RA   =            1
20448  deg
 ZDOT =       5006
741931                 TA   =          119
22405
                                          MA   =          119
20347
                                          Ha   =            221
034  n
mi
                                          Hp   =            217
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18709603
46                 X    =         5741274
58
 Y    =       -7248773
00  feet           Y    =        -2145438
90  meter
 Z    =       -9661575
10                 Z    =        -2917051
98
 XDOT =      13632
854936                 XDOT =        4085
403081
 YDOT =      13279
581815  feet/sec       YDOT =        4093
692907  meter/sec
 ZDOT =      16426
318672                 ZDOT =        5026
757822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18296090
79                 X    =         5576648
47
 Y    =       -8378105
78  feet           Y    =        -2553646
64  meter
 Z    =       -9539413
53                 Z    =        -2907613
24
 XDOT =      13697
971059                 XDOT =        4175
141579
 YDOT =      11099
541050  feet/sec       YDOT =        3383
140112  meter/sec
 ZDOT =      16513
139733                 ZDOT =        5033
204991


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   16324
85329819  
00016717  00000-0  10270-3 0  9143
2 25544  51
6426   1
7612 0006353 233
6169 126
4398 15
53654133 29190


Satellite: ISS
Catalog Number: 25544
Epoch time:      16324
85329819   =   yrday
fracday
Element set:     914
Inclination:       51
6426  deg
RA of node:         1
7612  deg
Eccentricity:     
0006353     
Arg of perigee:   233
6169  deg
Mean anomaly:     126
4398  deg
Mean motion:   15
53654133  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2919
Checksum:              317


Coasting Arc #16 (Orbit 2919)
---------------------------------------

Vector Time (GMT): 2016/324/22:00:36
000
Vector Time (MET): N/A
Weight (LBS)     : 909067
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6778332
73                 A    =         6790657
18  meter
 Y    =        -149670
45  meter          E    =           
0005392
 Z    =        -320782
05                 I    =           51
67371
 XDOT =        386
743513                 Wp   =           29
07441
 YDOT =       4751
286363  meter/sec      RA   =             
87849  deg
 ZDOT =       6002
291595                 TA   =          327
47182
                                          MA   =          327
50503
                                          Ha   =            220
994  n
mi
                                          Hp   =            217
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22238624
45                 X    =         6781060
84
 Y    =        -491044
79  feet           Y    =          -73855
32  meter
 Z    =       -1052434
56                 Z    =         -287847
73
 XDOT =       1268
843547                 XDOT =         304
427894
 YDOT =      15588
209853  feet/sec       YDOT =        4755
150779  meter/sec
 ZDOT =      19692
557727                 ZDOT =        6003
970500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19285556
10                 X    =         5878237
50
 Y    =      -11097192
06  feet           Y    =        -3382424
14  meter
 Z    =        -908193
42                 Z    =         -276817
36
 XDOT =       7667
419587                 XDOT =        2337
029490
 YDOT =      11727
498468  feet/sec       YDOT =        3574
541533  meter/sec
 ZDOT =      19698
942697                 ZDOT =        6004
237734


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   16324
91761937  
00016717  00000-0  10270-3 0  9152
2 25544  51
6438   1
4415 0006425 234
6748 125
3804 15
53659099 29203


Satellite: ISS
Catalog Number: 25544
Epoch time:      16324
91761937   =   yrday
fracday
Element set:     915
Inclination:       51
6438  deg
RA of node:         1
4415  deg
Eccentricity:     
0006425     
Arg of perigee:   234
6748  deg
Mean anomaly:     125
3804  deg
Mean motion:   15
53659099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2920
Checksum:              319


Coasting Arc #17 (Orbit 2935)
---------------------------------------

Vector Time (GMT): 2016/325/22:00:36
000
Vector Time (MET): N/A
Weight (LBS)     : 909067
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6649415
53                 A    =         6790105
32  meter
 Y    =        -508749
29  meter          E    =           
0010529
 Z    =       -1240069
75                 I    =           51
63986
 XDOT =       1451
743468                 Wp   =          179
59238
 YDOT =      -4744
460538  meter/sec      RA   =          355
91216  deg
 ZDOT =      -5848
574523                 TA   =           13
88999
                                          MA   =           13
86105
                                          Ha   =            220
865  n
mi
                                          Hp   =            217
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21815667
74                 X    =        -6637208
59
 Y    =       -1669124
96  feet           Y    =         -583039
25  meter
 Z    =       -4068470
31                 Z    =        -1272341
55
 XDOT =       4762
937887                 XDOT =        1533
099416
 YDOT =     -15565
815413  feet/sec       YDOT =       -4727
771214  meter/sec
 ZDOT =     -19188
236624                 ZDOT =       -5841
324710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19763807
44                 X    =        -6024008
51
 Y    =        9323753
46  feet           Y    =         2841880
06  meter
 Z    =       -4209670
33                 Z    =        -1283107
52
 XDOT =      -2770
605613                 XDOT =        -844
480591
 YDOT =     -14506
474337  feet/sec       YDOT =       -4421
573378  meter/sec
 ZDOT =     -19155
529925                 ZDOT =       -5838
605521


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   16325
94676783  
00016717  00000-0  10270-3 0  9161
2 25544  51
6444 356
3155 0006487 237
7901 122
2623 15
53621833 29363


Satellite: ISS
Catalog Number: 25544
Epoch time:      16325
94676783   =   yrday
fracday
Element set:     916
Inclination:       51
6444  deg
RA of node:       356
3155  deg
Eccentricity:     
0006487     
Arg of perigee:   237
7901  deg
Mean anomaly:     122
2623  deg
Mean motion:   15
53621833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              328


Coasting Arc #18 (Orbit 2945)
---------------------------------------

Vector Time (GMT): 2016/326/13:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 895793
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6432426
42                 A    =         6790115
64  meter
 Y    =        1782825
25  meter          E    =           
0012286
 Z    =        1201543
38                 I    =           51
61682
 XDOT =      -2311
477724                 Wp   =          148
43298
 YDOT =      -4381
227386  meter/sec      RA   =          352
70622  deg
 ZDOT =      -5856
787310                 TA   =           18
50494
                                          MA   =           18
46029
                                          Ha   =            220
811  n
mi
                                          Hp   =            217
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21103761
21                 X    =        -6457720
98
 Y    =        5849164
21  feet           Y    =         1710752
10  meter
 Z    =        3942071
45                 Z    =         1170234
57
 XDOT =      -7583
588333                 XDOT =       -2233
863937
 YDOT =     -14374
105598  feet/sec       YDOT =       -4406
641896  meter/sec
 ZDOT =     -19215
181464                 ZDOT =       -5867
827484

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2136166
09                 X    =         -651103
42
 Y    =      -21819325
96  feet           Y    =        -6650530
55  meter
 Z    =        3804628
18                 Z    =         1159650
67
 XDOT =      13851
666047                 XDOT =        4221
987811
 YDOT =      -4724
927131  feet/sec       YDOT =       -1440
157790  meter/sec
 ZDOT =     -19262
631586                 ZDOT =       -5871
250107


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   16326
58998220  
00016717  00000-0  10270-3 0  9176
2 25544  51
6416 353
1100 0006121 238
5494 121
5060 15
53662990 29465


Satellite: ISS
Catalog Number: 25544
Epoch time:      16326
58998220   =   yrday
fracday
Element set:     917
Inclination:       51
6416  deg
RA of node:       353
1100  deg
Eccentricity:     
0006121     
Arg of perigee:   238
5494  deg
Mean anomaly:     121
5060  deg
Mean motion:   15
53662990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2946
Checksum:              305
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