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

 
Date: April 12th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 67 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


104/12:22:07 990 1 5 1 5 1 5
N/A 0 3 -0 1 221 2
000/00:04:11 979 -0 1 0 0 214 3

Coasting Arc #1 (Orbit 3460)
---------------------------------------

Vector Time (GMT): 2016/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5694930
89                 A    =         6782789
91  meter
 Y    =          44261
19  meter          E    =           
0013978
 Z    =        3674778
07                 I    =           51
83247
 XDOT =      -2869
766054                 Wp   =           78
28998
 YDOT =      -5619
873706  meter/sec      RA   =           30
03032  deg
 ZDOT =      -4362
906582                 TA   =           58
11032
                                          MA   =           57
97440
                                          Ha   =            221
362  n
mi
                                          Hp   =            213
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18684156
47                 X    =        -5712853
26
 Y    =         145213
87  feet           Y    =          -19523
34  meter
 Z    =       12056358
49                 Z    =         3647069
69
 XDOT =      -9415
242958                 XDOT =       -2785
516586
 YDOT =     -18437
905859  feet/sec       YDOT =       -5651
494496  meter/sec
 ZDOT =     -14313
997971                 ZDOT =       -4376
642414

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17660248
89                 X    =        -5382843
86
 Y    =        6334318
30  feet           Y    =         1930700
22  meter
 Z    =       11935936
95                 Z    =         3638073
58
 XDOT =     -14427
808704                 XDOT =       -4397
596093
 YDOT =     -13037
657093  feet/sec       YDOT =       -3973
877882  meter/sec
 ZDOT =     -14372
586023                 ZDOT =       -4380
764220


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   16102
53990315  
00016717  00000-0  10270-3 0  9002
2 25544  51
6430  30
4559 0002631  44
4619 315
6744 15
54446052 34617


Satellite: ISS
Catalog Number: 25544
Epoch time:      16102
53990315   =   yrday
fracday
Element set:     900
Inclination:       51
6430  deg
RA of node:        30
4559  deg
Eccentricity:     
0002631     
Arg of perigee:    44
4619  deg
Mean anomaly:     315
6744  deg
Mean motion:   15
54446052  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3461
Checksum:              283


Coasting Arc #2 (Orbit 3475)
---------------------------------------

Vector Time (GMT): 2016/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6335258
41                 A    =         6786431
30  meter
 Y    =        1072929
77  meter          E    =           
0008944
 Z    =       -2176334
73                 I    =           51
81648
 XDOT =        995
785583                 Wp   =           42
69005
 YDOT =       5243
712494  meter/sec      RA   =           25
06107  deg
 ZDOT =       5503
485339                 TA   =          293
22268
                                          MA   =          293
31684
                                          Ha   =            221
315  n
mi
                                          Hp   =            213
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20784968
53                 X    =         6333361
56
 Y    =        3520110
79  feet           Y    =         1143764
13  meter
 Z    =       -7140205
80                 Z    =        -2145564
06
 XDOT =       3267
013067                 XDOT =         910
341313
 YDOT =      17203
781148  feet/sec       YDOT =        5254
370539  meter/sec
 ZDOT =      18056
054262                 ZDOT =        5508
114873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20759703
58                 X    =         6327557
65
 Y    =       -3915290
71  feet           Y    =        -1193380
61  meter
 Z    =       -7006699
76                 Z    =        -2135642
09
 XDOT =       8631
057131                 XDOT =        2630
746213
 YDOT =      13534
397119  feet/sec       YDOT =        4125
284242  meter/sec
 ZDOT =      18075
136167                 ZDOT =        5509
301504


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   16103
50423071  
00016717  00000-0  10270-3 0  9011
2 25544  51
6429  25
6460 0002619  46
4303 313
7067 15
54458248 34763


Satellite: ISS
Catalog Number: 25544
Epoch time:      16103
50423071   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:        25
6460  deg
Eccentricity:     
0002619     
Arg of perigee:    46
4303  deg
Mean anomaly:     313
7067  deg
Mean motion:   15
54458248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3476
Checksum:              288


Coasting Arc #3 (Orbit 3491)
---------------------------------------

Vector Time (GMT): 2016/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6455907
90                 A    =         6788292
57  meter
 Y    =       -2047379
99  meter          E    =           
0013427
 Z    =         375774
82                 I    =           51
79410
 XDOT =       1109
947495                 Wp   =          119
90744
 YDOT =      -4631
376789  meter/sec      RA   =           20
09844  deg
 ZDOT =      -6010
447300                 TA   =           56
04989
                                          MA   =           55
92233
                                          Ha   =            221
271  n
mi
                                          Hp   =            213
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21180800
21                 X    =        -6434359
13
 Y    =       -6717125
95  feet           Y    =        -2119453
74  meter
 Z    =        1232857
02                 Z    =          344465
94
 XDOT =       3641
560024                 XDOT =        1190
850503
 YDOT =     -15194
805737  feet/sec       YDOT =       -4618
512566  meter/sec
 ZDOT =     -19719
315290                 ZDOT =       -6004
858692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22182006
99                 X    =        -6761075
73
 Y    =        1421517
41  feet           Y    =          433278
51  meter
 Z    =        1097209
67                 Z    =          334429
51
 XDOT =      -1893
741677                 XDOT =        -577
212463
 YDOT =     -13911
366470  feet/sec       YDOT =       -4240
184500  meter/sec
 ZDOT =     -19694
111045                 ZDOT =       -6002
765046


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   16104
53283450  
00016717  00000-0  10270-3 0  9021
2 25544  51
6436  20
5151 0002591  52
0358 308
1023 15
54468853 34925


Satellite: ISS
Catalog Number: 25544
Epoch time:      16104
53283450   =   yrday
fracday
Element set:     902
Inclination:       51
6436  deg
RA of node:        20
5151  deg
Eccentricity:     
0002591     
Arg of perigee:    52
0358  deg
Mean anomaly:     308
1023  deg
Mean motion:   15
54468853  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3492
Checksum:              280


Coasting Arc #4 (Orbit 3491)
---------------------------------------

Vector Time (GMT): 2016/104/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1443920
16                 A    =         6777124
53  meter
 Y    =       -3946013
71  meter          E    =           
0015777
 Z    =       -5330838
29                 I    =           51
75399
 XDOT =       7192
845588                 Wp   =           84
45376
 YDOT =       2625
665388  meter/sec      RA   =           20
01752  deg
 ZDOT =          6
189006                 TA   =          185
59638
                                          MA   =          185
61403
                                          Ha   =            221
246  n
mi
                                          Hp   =            214
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4737270
87                 X    =         1513833
18
 Y    =      -12946239
20  feet           Y    =        -3929476
20  meter
 Z    =      -17489626
95                 Z    =        -5323654
05
 XDOT =      23598
574765                 XDOT =        7162
920092
 YDOT =       8614
387755  feet/sec       YDOT =        2705
933247  meter/sec
 ZDOT =         20
305138                 ZDOT =          41
057380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1636451
81                 X    =         -498790
51
 Y    =      -13729066
02  feet           Y    =        -4184619
32  meter
 Z    =      -17457624
91                 Z    =        -5321084
07
 XDOT =      23917
684266                 XDOT =        7290
110164
 YDOT =      -3062
445230  feet/sec       YDOT =        -933
433306  meter/sec
 ZDOT =        171
305554                 ZDOT =          52
213933


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   16104
53283479  
00016717  00000-0  10270-3 0  9033
2 25544  51
6438  20
5148 0001725  29
1025 331
0223 15
54208672 34925


Satellite: ISS
Catalog Number: 25544
Epoch time:      16104
53283479   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:        20
5148  deg
Eccentricity:     
0001725     
Arg of perigee:    29
1025  deg
Mean anomaly:     331
0223  deg
Mean motion:   15
54208672  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3492
Checksum:              282


Coasting Arc #5 (Orbit 3507)
---------------------------------------

Vector Time (GMT): 2016/105/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3157079
74                 A    =         6778321
11  meter
 Y    =        3261858
02  meter          E    =           
0007454
 Z    =        5030304
67                 I    =           51
72764
 XDOT =      -6608
063348                 Wp   =           49
48539
 YDOT =      -3370
646820  meter/sec      RA   =           15
02422  deg
 ZDOT =      -1954
999451                 TA   =           59
49339
                                          MA   =           59
41982
                                          Ha   =            221
273  n
mi
                                          Hp   =            214
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10357873
16                 X    =        -3217755
11
 Y    =       10701633
93  feet           Y    =         3226214
51  meter
 Z    =       16503624
26                 Z    =         5014820
77
 XDOT =     -21679
997860                 XDOT =       -6560
384243
 YDOT =     -11058
552559  feet/sec       YDOT =       -3444
276108  meter/sec
 ZDOT =      -6414
040193                 ZDOT =       -1986
983823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4134749
04                 X    =        -1260271
51
 Y    =       14385825
39  feet           Y    =         4384799
58  meter
 Z    =       16435692
78                 Z    =         5009599
16
 XDOT =     -23245
854906                 XDOT =       -7085
336575
 YDOT =        829
697208  feet/sec       YDOT =         252
891709  meter/sec
 ZDOT =      -6552
354051                 ZDOT =       -1997
157515


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   16105
56161377  
00016717  00000-0  10270-3 0  9040
2 25544  51
6436  15
3855 0001721  27
7543 332
3701 15
54248190 35087


Satellite: ISS
Catalog Number: 25544
Epoch time:      16105
56161377   =   yrday
fracday
Element set:     904
Inclination:       51
6436  deg
RA of node:        15
3855  deg
Eccentricity:     
0001721     
Arg of perigee:    27
7543  deg
Mean anomaly:     332
3701  deg
Mean motion:   15
54248190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3508
Checksum:              291


Coasting Arc #6 (Orbit 3522)
---------------------------------------

Vector Time (GMT): 2016/106/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4672506
01                 A    =         6781608
02  meter
 Y    =       -2548975
99  meter          E    =           
0008335
 Z    =       -4210326
15                 I    =           51
70803
 XDOT =       5454
185458                 Wp   =           97
51111
 YDOT =       3919
768590  meter/sec      RA   =           10
03491  deg
 ZDOT =       3685
028855                 TA   =          210
26093
                                          MA   =          210
30909
                                          Ha   =            221
249  n
mi
                                          Hp   =            214
244

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15329744
11                 X    =         4721114
00
 Y    =       -8362782
13  feet           Y    =        -2496453
45  meter
 Z    =      -13813405
99                 Z    =        -4187510
00
 XDOT =      17894
309246                 XDOT =        5392
047954
 YDOT =      12860
133169  feet/sec       YDOT =        3980
413760  meter/sec
 ZDOT =      12089
989682                 ZDOT =        3711
372743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9352019
80                 X    =         2850495
64
 Y    =      -14839807
62  feet           Y    =        -4523173
36  meter
 Z    =      -13713759
51                 Z    =        -4179953
90
 XDOT =      20748
962258                 XDOT =        6324
283696
 YDOT =       1814
150243  feet/sec       YDOT =         552
952994  meter/sec
 ZDOT =      12203
678437                 ZDOT =        3719
681188


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   16106
52608413  
00016717  00000-0  10270-3 0  9055
2 25544  51
6443  10
5764 0001724  31
6829 328
4427 15
54238703 35232


Satellite: ISS
Catalog Number: 25544
Epoch time:      16106
52608413   =   yrday
fracday
Element set:     905
Inclination:       51
6443  deg
RA of node:        10
5764  deg
Eccentricity:     
0001724     
Arg of perigee:    31
6829  deg
Mean anomaly:     328
4427  deg
Mean motion:   15
54238703  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3523
Checksum:              291


Coasting Arc #7 (Orbit 3538)
---------------------------------------

Vector Time (GMT): 2016/107/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5862306
52                 A    =         6785528
21  meter
 Y    =        1783110
51  meter          E    =           
0014245
 Z    =        2901863
78                 I    =           51
68928
 XDOT =      -3824
464688                 Wp   =           92
54751
 YDOT =      -4336
336827  meter/sec      RA   =            5
05420  deg
 ZDOT =      -5040
841132                 TA   =           54
39556
                                          MA   =           54
26293
                                          Ha   =            221
328  n
mi
                                          Hp   =            214
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19233289
12                 X    =        -5895906
05
 Y    =        5850100
09  feet           Y    =         1717366
68  meter
 Z    =        9520550
47                 Z    =         2873304
35
 XDOT =     -12547
456327                 XDOT =       -3751
204159
 YDOT =     -14226
826860  feet/sec       YDOT =       -4378
695346  meter/sec
 ZDOT =     -16538
192691                 ZDOT =       -5059
241147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13709635
10                 X    =        -4178696
78
 Y    =       14783200
36  feet           Y    =         4505919
47  meter
 Z    =        9396108
52                 Z    =         2863933
88
 XDOT =     -16840
647789                 XDOT =       -5133
029446
 YDOT =      -5012
013900  feet/sec       YDOT =       -1527
661837  meter/sec
 ZDOT =     -16617
276618                 ZDOT =       -5064
945913


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   16107
55484069  
00016717  00000-0  10270-3 0  9069
2 25544  51
6442   5
4470 0001722  38
2105 321
9169 15
54240115 35394


Satellite: ISS
Catalog Number: 25544
Epoch time:      16107
55484069   =   yrday
fracday
Element set:     906
Inclination:       51
6442  deg
RA of node:         5
4470  deg
Eccentricity:     
0001722     
Arg of perigee:    38
2105  deg
Mean anomaly:     321
9169  deg
Mean motion:   15
54240115  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3539
Checksum:              287


Coasting Arc #8 (Orbit 3553)
---------------------------------------

Vector Time (GMT): 2016/108/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6577391
57                 A    =         6788189
14  meter
 Y    =       -1023904
96  meter          E    =           
0010675
 Z    =       -1306660
45                 I    =           51
66733
 XDOT =       1870
258296                 Wp   =           36
98514
 YDOT =       4613
892918  meter/sec      RA   =             
08053  deg
 ZDOT =       5832
027707                 TA   =          308
80020
                                          MA   =          308
89548
                                          Ha   =            221
207  n
mi
                                          Hp   =            214
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21579368
68                 X    =         6594699
51
 Y    =       -3359268
23  feet           Y    =         -950255
54  meter
 Z    =       -4286943
72                 Z    =        -1274666
86
 XDOT =       6136
018030                 XDOT =        1790
195994
 YDOT =      15137
443956  feet/sec       YDOT =        4634
360293  meter/sec
 ZDOT =      19133
949169                 ZDOT =        5840
918087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16722989
39                 X    =         5097167
17
 Y    =      -14087923
40  feet           Y    =        -4293999
05  meter
 Z    =       -4147741
84                 Z    =        -1264231
71
 XDOT =      11970
937750                 XDOT =        3648
741826
 YDOT =       8598
590301  feet/sec       YDOT =        2620
850324  meter/sec
 ZDOT =      19171
657488                 ZDOT =        5843
521202


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   16108
51928701  
00016717  00000-0  10270-3 0  9073
2 25544  51
6448    
6378 0001684  35
5800 324
5465 15
54286296 35548


Satellite: ISS
Catalog Number: 25544
Epoch time:      16108
51928701   =   yrday
fracday
Element set:     907
Inclination:       51
6448  deg
RA of node:          
6378  deg
Eccentricity:     
0001684     
Arg of perigee:    35
5800  deg
Mean anomaly:     324
5465  deg
Mean motion:   15
54286296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3554
Checksum:              315


Coasting Arc #9 (Orbit 3569)
---------------------------------------

Vector Time (GMT): 2016/109/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6764963
79                 A    =         6788850
32  meter
 Y    =         201349
61  meter          E    =           
0010877
 Z    =        -475002
91                 I    =           51
63720
 XDOT =        271
343089                 Wp   =          130
13950
 YDOT =      -4780
514832  meter/sec      RA   =          355
11058  deg
 ZDOT =      -5988
362936                 TA   =           54
98325
                                          MA   =           54
88122
                                          Ha   =            221
182  n
mi
                                          Hp   =            214
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22194763
08                 X    =        -6764405
17
 Y    =         660595
84  feet           Y    =          125702
36  meter
 Z    =       -1558408
49                 Z    =         -507864
30
 XDOT =        890
233232                 XDOT =         353
868929
 YDOT =     -15684
103781  feet/sec       YDOT =       -4777
019663  meter/sec
 ZDOT =     -19646
860027                 ZDOT =       -5986
843886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18407475
08                 X    =        -5610598
40
 Y    =       12399326
27  feet           Y    =         3779314
65  meter
 Z    =       -1701205
87                 Z    =         -518527
55
 XDOT =      -6608
463993                 XDOT =       -2014
259825
 YDOT =     -12464
966354  feet/sec       YDOT =       -3799
321745  meter/sec
 ZDOT =     -19639
311916                 ZDOT =       -5986
062272


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   16109
54801989  
00016717  00000-0  10270-3 0  9086
2 25544  51
6448 355
5084 0001527  40
4954 319
6312 15
54253245 35707


Satellite: ISS
Catalog Number: 25544
Epoch time:      16109
54801989   =   yrday
fracday
Element set:     908
Inclination:       51
6448  deg
RA of node:       355
5084  deg
Eccentricity:     
0001527     
Arg of perigee:    40
4954  deg
Mean anomaly:     319
6312  deg
Mean motion:   15
54253245  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3570
Checksum:              317


Coasting Arc #10 (Orbit 3585)
---------------------------------------

Vector Time (GMT): 2016/110/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6391054
29                 A    =         6786753
10  meter
 Y    =         634407
00  meter          E    =           
0015331
 Z    =        2169920
93                 I    =           51
59848
 XDOT =      -2349
651699                 Wp   =           67
05725
 YDOT =       4821
940891  meter/sec      RA   =          350
13534  deg
 ZDOT =       5485
641815                 TA   =          317
04990
                                          MA   =          317
16950
                                          Ha   =            221
104  n
mi
                                          Hp   =            213
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20968025
90                 X    =         6372944
54
 Y    =        2081387
81  feet           Y    =          705774
98  meter
 Z    =        7119163
15                 Z    =         2200923
34
 XDOT =      -7708
831032                 XDOT =       -2430
044381
 YDOT =      15820
016048  feet/sec       YDOT =        4795
216561  meter/sec
 ZDOT =      17997
512517                 ZDOT =        5474
031935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18639079
78                 X    =         5681191
52
 Y    =       -9728370
74  feet           Y    =        -2965207
40  meter
 Z    =        7253707
79                 Z    =         2210930
13
 XDOT =       1420
396292                 XDOT =         432
936790
 YDOT =      16162
518410  feet/sec       YDOT =        4926
335611  meter/sec
 ZDOT =      17946
123962                 ZDOT =        5469
978583


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   16110
57673933  
00016717  00000-0  10270-3 0  9098
2 25544  51
6444 350
3783 0001730  36
5869 323
5402 15
54302883 35863


Satellite: ISS
Catalog Number: 25544
Epoch time:      16110
57673933   =   yrday
fracday
Element set:     909
Inclination:       51
6444  deg
RA of node:       350
3783  deg
Eccentricity:     
0001730     
Arg of perigee:    36
5869  deg
Mean anomaly:     323
5402  deg
Mean motion:   15
54302883  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3586
Checksum:              315


Coasting Arc #11 (Orbit 3600)
---------------------------------------

Vector Time (GMT): 2016/111/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5501516
24                 A    =         6783014
95  meter
 Y    =       -1548157
33  meter          E    =           
0006893
 Z    =       -3660954
23                 I    =           51
55407
 XDOT =       4212
950395                 Wp   =           70
04468
 YDOT =      -4691
127389  meter/sec      RA   =          345
15013  deg
 ZDOT =      -4351
604255                 TA   =          153
48307
                                          MA   =          153
44779
                                          Ha   =            221
083  n
mi
                                          Hp   =            213
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18049593
97                 X    =        -5466011
89
 Y    =       -5079256
34  feet           Y    =        -1609480
77  meter
 Z    =      -12011004
69                 Z    =        -3687593
21
 XDOT =      13822
015732                 XDOT =        4286
233150
 YDOT =     -15390
837889  feet/sec       YDOT =       -4643
606023  meter/sec
 ZDOT =     -14276
916848                 ZDOT =       -4330
960088

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17716715
05                 X    =        -5400054
75
 Y    =        5909250
49  feet           Y    =         1801139
55  meter
 Z    =      -12126404
58                 Z    =        -3696128
12
 XDOT =       3276
025667                 XDOT =         998
532623
 YDOT =     -19260
693623  feet/sec       YDOT =       -5870
659416  meter/sec
 ZDOT =     -14186
317946                 ZDOT =       -4323
989710


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   16111
54115318  
00016717  00000-0  10270-3 0  9106
2 25544  51
6437 345
5692 0001553  36
6853 323
4406 15
54309637 36012


Satellite: ISS
Catalog Number: 25544
Epoch time:      16111
54115318   =   yrday
fracday
Element set:     910
Inclination:       51
6437  deg
RA of node:       345
5692  deg
Eccentricity:     
0001553     
Arg of perigee:    36
6853  deg
Mean anomaly:     323
4406  deg
Mean motion:   15
54309637  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3601
Checksum:              292


Coasting Arc #12 (Orbit 3616)
---------------------------------------

Vector Time (GMT): 2016/112/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4190781
57                 A    =         6779228
91  meter
 Y    =        2472548
29  meter          E    =           
0008312
 Z    =        4714410
52                 I    =           51
51044
 XDOT =      -5676
030344                 Wp   =          105
47757
 YDOT =       4371
100770  meter/sec      RA   =          340
15092  deg
 ZDOT =       2746
885536                 TA   =          317
27115
                                          MA   =          317
33575
                                          Ha   =            221
070  n
mi
                                          Hp   =            213
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13749283
37                 X    =         4139920
49
 Y    =        8112035
09  feet           Y    =         2519128
40  meter
 Z    =       15467226
12                 Z    =         4734644
90
 XDOT =     -18622
146799                 XDOT =       -5737
830640
 YDOT =      14340
881791  feet/sec       YDOT =        4307
282294  meter/sec
 ZDOT =       9012
091653                 ZDOT =        2719
161883

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15830127
04                 X    =         4825022
72
 Y    =       -1242554
10  feet           Y    =         -378730
49  meter
 Z    =       15554617
56                 Z    =         4741047
43
 XDOT =      -7081
397822                 XDOT =       -2158
410056
 YDOT =      21334
430629  feet/sec       YDOT =        6502
734456  meter/sec
 ZDOT =       8890
815428                 ZDOT =        2709
920542


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   16112
56985141  
00016717  00000-0  10270-3 0  9119
2 25544  51
6435 340
4388 0001755  42
4989 317
6299 15
54317621 36179


Satellite: ISS
Catalog Number: 25544
Epoch time:      16112
56985141   =   yrday
fracday
Element set:     911
Inclination:       51
6435  deg
RA of node:       340
4388  deg
Eccentricity:     
0001755     
Arg of perigee:    42
4989  deg
Mean anomaly:     317
6299  deg
Mean motion:   15
54317621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3617
Checksum:              322


Coasting Arc #13 (Orbit 3631)
---------------------------------------

Vector Time (GMT): 2016/113/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2598456
37                 A    =         6776848
37  meter
 Y    =       -3412512
47  meter          E    =           
0015820
 Z    =       -5260582
95                 I    =           51
47168
 XDOT =       6610
618222                 Wp   =           79
57650
 YDOT =      -3777
463459  meter/sec      RA   =          335
13972  deg
 ZDOT =       -814
171166                 TA   =          182
60772
                                          MA   =          182
61598
                                          Ha   =            221
058  n
mi
                                          Hp   =            213
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8525119
32                 X    =        -2534549
55
 Y    =      -11195907
04  feet           Y    =        -3441213
15  meter
 Z    =      -17259130
41                 Z    =        -5273050
39
 XDOT =      21688
379992                 XDOT =        6656
322410
 YDOT =     -12393
252817  feet/sec       YDOT =       -3703
283633  meter/sec
 ZDOT =      -2671
165243                 ZDOT =        -781
946576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13403099
73                 X    =        -4085264
80
 Y    =       -4066254
08  feet           Y    =        -1239394
24  meter
 Z    =      -17312598
64                 Z    =        -5276880
06
 XDOT =       9898
378720                 XDOT =        3017
025834
 YDOT =     -21843
115255  feet/sec       YDOT =       -6657
781530  meter/sec
 ZDOT =      -2530
467549                 ZDOT =        -771
286509


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   16113
53424296  
00016717  00000-0  10270-3 0  9127
2 25544  51
6421 335
6285 0001644  41
6019 318
5258 15
54371296 36328


Satellite: ISS
Catalog Number: 25544
Epoch time:      16113
53424296   =   yrday
fracday
Element set:     912
Inclination:       51
6421  deg
RA of node:       335
6285  deg
Eccentricity:     
0001644     
Arg of perigee:    41
6019  deg
Mean anomaly:     318
5258  deg
Mean motion:   15
54371296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3632
Checksum:              299


Coasting Arc #14 (Orbit 3647)
---------------------------------------

Vector Time (GMT): 2016/114/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         870205
22                 A    =         6777143
15  meter
 Y    =        4268824
17  meter          E    =           
0005706
 Z    =        5188020
44                 I    =           51
44416
 XDOT =      -6996
496907                 Wp   =           52
10112
 YDOT =       2904
882042  meter/sec      RA   =          330
12434  deg
 ZDOT =      -1212
306584                 TA   =           49
58171
                                          MA   =           49
53194
                                          Ha   =            221
019  n
mi
                                          Hp   =            213
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2855004
00                 X    =          797203
82
 Y    =       14005328
65  feet           Y    =         4278147
46  meter
 Z    =       17021064
42                 Z    =         5192070
24
 XDOT =     -22954
386178                 XDOT =       -7022
571045
 YDOT =       9530
452894  feet/sec       YDOT =        2826
496712  meter/sec
 ZDOT =      -3977
383806                 ZDOT =       -1246
357958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10653246
34                 X    =         3247109
48
 Y    =        9499392
09  feet           Y    =         2895414
71  meter
 Z    =       17037805
17                 Z    =         5193123
01
 XDOT =     -11813
326422                 XDOT =       -3600
701894
 YDOT =      20673
784507  feet/sec       YDOT =        6301
369518  meter/sec
 ZDOT =      -4125
833890                 ZDOT =       -1257
554170


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   16114
56291761  
00016717  00000-0  10270-3 0  9131
2 25544  51
6423 330
4984 0001575  44
5812 315
5467 15
54378029 36482


Satellite: ISS
Catalog Number: 25544
Epoch time:      16114
56291761   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:       330
4984  deg
Eccentricity:     
0001575     
Arg of perigee:    44
5812  deg
Mean anomaly:     315
5467  deg
Mean motion:   15
54378029  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3648
Checksum:              317


Coasting Arc #15 (Orbit 3662)
---------------------------------------

Vector Time (GMT): 2016/115/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         803006
48                 A    =         6779828
91  meter
 Y    =       -4977449
99  meter          E    =           
0010598
 Z    =       -4542968
34                 I    =           51
42451
 XDOT =       6790
812080                 Wp   =          102
37912
 YDOT =      -1725
918471  meter/sec      RA   =          325
10973  deg
 ZDOT =       3095
210213                 TA   =          198
72362
                                          MA   =          198
76263
                                          Ha   =            221
032  n
mi
                                          Hp   =            213
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2634535
68                 X    =          880674
10
 Y    =      -16330216
51  feet           Y    =        -4968036
12  meter
 Z    =      -14904751
77                 Z    =        -4538878
66
 XDOT =      22279
567190                 XDOT =        6794
571528
 YDOT =      -5662
462176  feet/sec       YDOT =       -1649
957977  meter/sec
 ZDOT =      10154
889151                 ZDOT =        3128
208107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7946998
11                 X    =        -2422245
02
 Y    =      -14526541
34  feet           Y    =        -4427689
80  meter
 Z    =      -14886006
61                 Z    =        -4537254
82
 XDOT =      12905
069827                 XDOT =        3933
465283
 YDOT =     -17600
191942  feet/sec       YDOT =       -5364
538504  meter/sec
 ZDOT =      10298
524525                 ZDOT =        3138
990275


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   16115
52728964  
00016717  00000-0  10270-3 0  9149
2 25544  51
6408 325
6872 0001572  47
8245 312
3041 15
54398196 36637


Satellite: ISS
Catalog Number: 25544
Epoch time:      16115
52728964   =   yrday
fracday
Element set:     914
Inclination:       51
6408  deg
RA of node:       325
6872  deg
Eccentricity:     
0001572     
Arg of perigee:    47
8245  deg
Mean anomaly:     312
3041  deg
Mean motion:   15
54398196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3663
Checksum:              320


Coasting Arc #16 (Orbit 3678)
---------------------------------------

Vector Time (GMT): 2016/116/12:24:13
979
Vector Time (MET): N/A
Weight (LBS)     : 945061
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2321109
16                 A    =         6783703
26  meter
 Y    =        5419332
95  meter          E    =           
0013657
 Z    =        3345017
90                 I    =           51
41265
 XDOT =      -6098
705185                 Wp   =           86
17982
 YDOT =        266
358541  meter/sec      RA   =          320
10474  deg
 ZDOT =      -4646
120132                 TA   =           54
67166
                                          MA   =           54
54406
                                          Ha   =            220
948  n
mi
                                          Hp   =            213
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7615187
55                 X    =        -2397785
94
 Y    =       17779963
74  feet           Y    =         5392948
09  meter
 Z    =       10974468
19                 Z    =         3333556
00
 XDOT =     -20008
875279                 XDOT =       -6078
661143
 YDOT =        873
879727  feet/sec       YDOT =         198
270759  meter/sec
 ZDOT =     -15243
176285                 ZDOT =       -4675
697969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5268606
00                 X    =         1605871
11
 Y    =       18640636
99  feet           Y    =         5681666
15  meter
 Z    =       10923625
19                 Z    =         3329520
96
 XDOT =     -13528
353916                 XDOT =       -4123
442274
 YDOT =      12865
066579  feet/sec       YDOT =        3921
272293  meter/sec
 ZDOT =     -15371
667547                 ZDOT =       -4685
284268


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   16116
55594064  
00016717  00000-0  10270-3 0  9156
2 25544  51
6413 320
5567 0001544  43
1304 316
9970 15
54446093 36790


Satellite: ISS
Catalog Number: 25544
Epoch time:      16116
55594064   =   yrday
fracday
Element set:     915
Inclination:       51
6413  deg
RA of node:       320
5567  deg
Eccentricity:     
0001544     
Arg of perigee:    43
1304  deg
Mean anomaly:     316
9970  deg
Mean motion:   15
54446093  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3679
Checksum:              310
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