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

 
Date: August 30th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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


245/12:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 215 4

246/19:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 215 4

250/21:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 1

250/21:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 215 2

254/00:41:11 035 3 1 3 6 3 6
N/A -1 3 0 0 220 0
000/00:10:18 071 -1 3 -0 0 217 0

Coasting Arc #1 (Orbit 1638)
---------------------------------------

Vector Time (GMT): 2016/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5214601
83                 A    =         6781745
43  meter
 Y    =       -1399071
84  meter          E    =           
0007466
 Z    =        4099158
91                 I    =           51
92893
 XDOT =      -1299
910617                 Wp   =           74
89224
 YDOT =      -6496
980105  meter/sec      RA   =           51
51007  deg
 ZDOT =      -3863
354548                 TA   =           54
92239
                                          MA   =           54
85240
                                          Ha   =            219
660  n
mi
                                          Hp   =            215
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17108273
72                 X    =        -5218481
10
 Y    =       -4590130
72  feet           Y    =        -1457406
49  meter
 Z    =       13448684
08                 Z    =         4073818
77
 XDOT =      -4264
798613                 XDOT =       -1208
396937
 YDOT =     -21315
551524  feet/sec       YDOT =       -6511
005092  meter/sec
 ZDOT =     -12675
047729                 ZDOT =       -3869
446471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14086484
16                 X    =         4293560
37
 Y    =       10876292
08  feet           Y    =         3315093
82  meter
 Z    =       13338165
84                 Z    =         4065472
95
 XDOT =      -3585
282661                 XDOT =       -1092
794155
 YDOT =      20250
158710  feet/sec       YDOT =        6172
248375  meter/sec
 ZDOT =     -12700
458069                 ZDOT =       -3871
099619


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   16242
54108086  
00016717  00000-0  10270-3 0  9004
2 25544  51
6395  52
0055 0003215 263
1231  96
9556 15
54324514 16390


Satellite: ISS
Catalog Number: 25544
Epoch time:      16242
54108086   =   yrday
fracday
Element set:     900
Inclination:       51
6395  deg
RA of node:        52
0055  deg
Eccentricity:     
0003215     
Arg of perigee:   263
1231  deg
Mean anomaly:      96
9556  deg
Mean motion:   15
54324514  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1639
Checksum:              288


Coasting Arc #2 (Orbit 1653)
---------------------------------------

Vector Time (GMT): 2016/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5564009
49                 A    =         6785562
98  meter
 Y    =        2743134
58  meter          E    =           
0002693
 Z    =       -2747085
66                 I    =           51
92190
 XDOT =       -232
434734                 Wp   =           23
56072
 YDOT =       5650
052532  meter/sec      RA   =           46
54484  deg
 ZDOT =       5175
297914                 TA   =          305
48316
                                          MA   =          305
50829
                                          Ha   =            219
599  n
mi
                                          Hp   =            215
470

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18254624
29                 X    =         5546265
46
 Y    =        8999785
38  feet           Y    =         2805255
66  meter
 Z    =       -9012748
22                 Z    =        -2720100
86
 XDOT =       -762
581148                 XDOT =        -320
736708
 YDOT =      18536
917757  feet/sec       YDOT =        5646
959929  meter/sec
 ZDOT =      16979
323864                 ZDOT =        5173
953956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13675878
05                 X    =        -4168407
63
 Y    =      -15142692
05  feet           Y    =        -4615492
54  meter
 Z    =       -8895297
21                 Z    =        -2711286
59
 XDOT =       6573
751677                 XDOT =        2003
679511
 YDOT =     -15898
988602  feet/sec       YDOT =       -4846
011726  meter/sec
 ZDOT =      16972
382206                 ZDOT =        5173
182096


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   16243
50547786  
00016717  00000-0  10270-3 0  9016
2 25544  51
6402  47
1958 0002972 265
6406  94
4407 15
54350801 16549


Satellite: ISS
Catalog Number: 25544
Epoch time:      16243
50547786   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:        47
1958  deg
Eccentricity:     
0002972     
Arg of perigee:   265
6406  deg
Mean anomaly:      94
4407  deg
Mean motion:   15
54350801  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1654
Checksum:              309


Coasting Arc #3 (Orbit 1669)
---------------------------------------

Vector Time (GMT): 2016/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5524385
11                 A    =         6788167
02  meter
 Y    =       -3787656
16  meter          E    =           
0011048
 Z    =        1064025
37                 I    =           51
90690
 XDOT =       1930
196182                 Wp   =          132
04413
 YDOT =      -4485
653997  meter/sec      RA   =           41
58891  deg
 ZDOT =      -5914
192172                 TA   =           36
45720
                                          MA   =           36
38202
                                          Ha   =            219
484  n
mi
                                          Hp   =            215
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18124623
05                 X    =        -5486788
48
 Y    =      -12426693
42  feet           Y    =        -3849223
22  meter
 Z    =        3490896
88                 Z    =         1037281
38
 XDOT =       6332
664638                 XDOT =        2008
940579
 YDOT =     -14716
712587  feet/sec       YDOT =       -4463
629488  meter/sec
 ZDOT =     -19403
517624                 ZDOT =       -5904
624261

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12564624
32                 X    =         3829697
49
 Y    =       18051388
58  feet           Y    =         5502063
24  meter
 Z    =        3374702
55                 Z    =         1028609
34
 XDOT =      -9939
034783                 XDOT =       -3029
417802
 YDOT =      10557
889205  feet/sec       YDOT =        3218
044630  meter/sec
 ZDOT =     -19360
842825                 ZDOT =       -5901
184893


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   16244
53416328  
00016717  00000-0  10270-3 0  9028
2 25544  51
6391  42
0662 0003120 272
2417  87
8379 15
54374490 16706


Satellite: ISS
Catalog Number: 25544
Epoch time:      16244
53416328   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:        42
0662  deg
Eccentricity:     
0003120     
Arg of perigee:   272
2417  deg
Mean anomaly:      87
8379  deg
Mean motion:   15
54374490  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1670
Checksum:              298


Coasting Arc #4 (Orbit 1685)
---------------------------------------

Vector Time (GMT): 2016/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5056785
76                 A    =         6788372
74  meter
 Y    =        4462248
11  meter          E    =           
0011097
 Z    =         717960
16                 I    =           51
88512
 XDOT =      -3630
952830                 Wp   =           42
71327
 YDOT =       3145
324711  meter/sec      RA   =           36
63526  deg
 ZDOT =       5978
978008                 TA   =          325
01926
                                          MA   =          325
09211
                                          Ha   =            219
506  n
mi
                                          Hp   =            215
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16590504
45                 X    =         5003024
44
 Y    =       14639921
62  feet           Y    =         4518495
95  meter
 Z    =        2355512
33                 Z    =          742393
37
 XDOT =     -11912
574902                 XDOT =       -3694
897690
 YDOT =      10319
306794  feet/sec       YDOT =        3104
364053  meter/sec
 ZDOT =      19616
069580                 ZDOT =        5961
184353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10645167
18                 X    =        -3244646
96
 Y    =      -19384069
93  feet           Y    =        -5908264
51  meter
 Z    =        2461469
10                 Z    =          750255
78
 XDOT =      13407
365336                 XDOT =        4086
564954
 YDOT =      -4863
598228  feet/sec       YDOT =       -1482
424740  meter/sec
 ZDOT =      19537
692688                 ZDOT =        5955
088731


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   16245
56284635  
00016717  00000-0  10270-3 0  9037
2 25544  51
6413  36
9364 0003039 272
4082  87
6723 15
54376320 16863


Satellite: ISS
Catalog Number: 25544
Epoch time:      16245
56284635   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:        36
9364  deg
Eccentricity:     
0003039     
Arg of perigee:   272
4082  deg
Mean anomaly:      87
6723  deg
Mean motion:   15
54376320  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1686
Checksum:              314


Coasting Arc #5 (Orbit 1685)
---------------------------------------

Vector Time (GMT): 2016/245/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3699928
42                 A    =         6786043
88  meter
 Y    =        5133392
29  meter          E    =           
0010827
 Z    =        2436266
06                 I    =           51
87713
 XDOT =      -5327
766272                 Wp   =           69
44287
 YDOT =       1286
006586  meter/sec      RA   =           36
63173  deg
 ZDOT =       5365
971522                 TA   =          317
73303
                                          MA   =          317
81642
                                          Ha   =            219
457  n
mi
                                          Hp   =            215
389

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12138872
76                 X    =         3630416
37
 Y    =       16841838
22  feet           Y    =         5174378
96  meter
 Z    =        7992998
89                 Z    =         2454069
77
 XDOT =     -17479
548138                 XDOT =       -5367
815975
 YDOT =       4219
181711  feet/sec       YDOT =        1226
204565  meter/sec
 ZDOT =      17604
893446                 ZDOT =        5339
993520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6111503
57                 X    =        -1862786
29
 Y    =      -19809463
28  feet           Y    =        -6037924
41  meter
 Z    =        8069849
23                 Z    =         2459690
05
 XDOT =      16578
109198                 XDOT =        5053
007684
 YDOT =       2031
385468  feet/sec       YDOT =         619
166291  meter/sec
 ZDOT =      17491
093609                 ZDOT =        5331
285332


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   16245
56284633  
00016717  00000-0  10270-3 0  9046
2 25544  51
6411  36
9363 0003093 272
6000  87
4798 15
54376718 16863


Satellite: ISS
Catalog Number: 25544
Epoch time:      16245
56284633   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:        36
9363  deg
Eccentricity:     
0003093     
Arg of perigee:   272
6000  deg
Mean anomaly:      87
4798  deg
Mean motion:   15
54376718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1686
Checksum:              323


Coasting Arc #6 (Orbit 1700)
---------------------------------------

Vector Time (GMT): 2016/246/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2362241
62                 A    =         6782196
55  meter
 Y    =       -5039544
49  meter          E    =           
0003951
 Z    =       -3880330
03                 I    =           51
83855
 XDOT =       6449
838517                 Wp   =           55
07901
 YDOT =        160
083372  meter/sec      RA   =           31
66452  deg
 ZDOT =      -4135
171730                 TA   =          171
58734
                                          MA   =          171
58072
                                          Ha   =            219
541  n
mi
                                          Hp   =            215
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7750136
54                 X    =        -2286863
81
 Y    =      -16533938
61  feet           Y    =        -5065539
64  meter
 Z    =      -12730741
55                 Z    =        -3891621
42
 XDOT =      21160
887524                 XDOT =        6467
655734
 YDOT =        525
207913  feet/sec       YDOT =         232
308930  meter/sec
 ZDOT =     -13566
836383                 ZDOT =       -4103
797106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2330007
76                 X    =          710186
36
 Y    =       18076843
01  feet           Y    =         5509821
75  meter
 Z    =      -12779136
65                 Z    =        -3895080
85
 XDOT =     -18784
979949                 XDOT =       -5725
661888
 YDOT =      -7070
861427  feet/sec       YDOT =       -2155
198563  meter/sec
 ZDOT =     -13429
730840                 ZDOT =       -4093
381960


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   16246
52723258  
00016717  00000-0  10270-3 0  9055
2 25544  51
6418  32
1276 0003000 279
4544  80
6270 15
54370256 17016


Satellite: ISS
Catalog Number: 25544
Epoch time:      16246
52723258   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:        32
1276  deg
Eccentricity:     
0003000     
Arg of perigee:   279
4544  deg
Mean anomaly:      80
6270  deg
Mean motion:   15
54370256  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1701
Checksum:              285


Coasting Arc #7 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2016/246/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         423988
20                 A    =         6777516
61  meter
 Y    =       -4417395
14  meter          E    =           
0010960
 Z    =       -5132454
31                 I    =           51
81606
 XDOT =       7026
500432                 Wp   =           70
26075
 YDOT =       2576
015698  meter/sec      RA   =           30
03286  deg
 ZDOT =      -1635
899041                 TA   =          183
97061
                                          MA   =          183
97931
                                          Ha   =            219
600  n
mi
                                          Hp   =            215
389

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1391037
39                 X    =          498284
14
 Y    =      -14492766
21  feet           Y    =        -4412239
01  meter
 Z    =      -16838760
87                 Z    =        -5130213
73
 XDOT =      23052
822940                 XDOT =        7005
118967
 YDOT =       8451
495072  feet/sec       YDOT =        2654
470989  meter/sec
 ZDOT =      -5367
122839                 ZDOT =       -1601
818622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14529101
48                 X    =         4428470
13
 Y    =       -1112875
73  feet           Y    =         -339204
52  meter
 Z    =      -16828126
54                 Z    =        -5129212
97
 XDOT =      -4272
948235                 XDOT =       -1302
394622
 YDOT =      23165
733568  feet/sec       YDOT =        7060
915592  meter/sec
 ZDOT =      -5218
654337                 ZDOT =       -1590
645842


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   16246
84869292  
00016717  00000-0  10270-3 0  9060
2 25544  51
6441  30
5284 0003031 285
3533  74
7284 15
54360572 17065


Satellite: ISS
Catalog Number: 25544
Epoch time:      16246
84869292   =   yrday
fracday
Element set:     906
Inclination:       51
6441  deg
RA of node:        30
5284  deg
Eccentricity:     
0003031     
Arg of perigee:   285
3533  deg
Mean anomaly:      74
7284  deg
Mean motion:   15
54360572  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1706
Checksum:              309


Coasting Arc #8 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2016/247/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2164381
79                 A    =         6776685
81  meter
 Y    =        3606724
61  meter          E    =           
0001912
 Z    =        5313508
12                 I    =           51
78328
 XDOT =      -6805
712474                 Wp   =          354
12876
 YDOT =      -3514
222402  meter/sec      RA   =           25
04213  deg
 ZDOT =       -384
967474                 TA   =           99
54517
                                          MA   =           99
52356
                                          Ha   =            219
765  n
mi
                                          Hp   =            215
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7100990
12                 X    =        -2230362
83
 Y    =       11833085
98  feet           Y    =         3582152
76  meter
 Z    =       17432769
43                 Z    =         5302833
47
 XDOT =     -22328
453000                 XDOT =       -6764
039738
 YDOT =     -11529
601058  feet/sec       YDOT =       -3590
095479  meter/sec
 ZDOT =      -1263
016648                 ZDOT =        -417
926086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13016514
01                 X    =        -3967433
47
 Y    =       -4760748
07  feet           Y    =        -1451076
01  meter
 Z    =       17385427
10                 Z    =         5299078
18
 XDOT =       6596
591528                 XDOT =        2010
641098
 YDOT =     -23194
000368  feet/sec       YDOT =       -7069
531312  meter/sec
 ZDOT =      -1406
389427                 ZDOT =        -428
667497


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   16247
87736622  
00016717  00000-0  10270-3 0  9075
2 25544  51
6424  25
3991 0002903 291
2907  68
7936 15
54376495 17227


Satellite: ISS
Catalog Number: 25544
Epoch time:      16247
87736622   =   yrday
fracday
Element set:     907
Inclination:       51
6424  deg
RA of node:        25
3991  deg
Eccentricity:     
0002903     
Arg of perigee:   291
2907  deg
Mean anomaly:      68
7936  deg
Mean motion:   15
54376495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1722
Checksum:              336


Coasting Arc #9 (Orbit 1736)
---------------------------------------

Vector Time (GMT): 2016/248/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3822784
95                 A    =         6778579
09  meter
 Y    =       -2717140
60  meter          E    =           
0008775
 Z    =       -4902272
63                 I    =           51
76089
 XDOT =       5983
312393                 Wp   =          104
09199
 YDOT =       4163
295617  meter/sec      RA   =           20
05131  deg
 ZDOT =       2359
678594                 TA   =          188
98666
                                          MA   =          189
00238
                                          Ha   =            219
712  n
mi
                                          Hp   =            215
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12541945
38                 X    =         3876697
66
 Y    =       -8914503
29  feet           Y    =        -2674090
79  meter
 Z    =      -16083571
64                 Z    =        -4883571
29
 XDOT =      19630
290003                 XDOT =        5924
850397
 YDOT =      13659
106354  feet/sec       YDOT =        4229
878420  meter/sec
 ZDOT =       7741
727669                 ZDOT =        2388
601467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11397783
52                 X    =         3474044
42
 Y    =       10464139
45  feet           Y    =         3189469
71  meter
 Z    =      -16001323
56                 Z    =        -4877203
42
 XDOT =      -8427
686846                 XDOT =       -2568
758951
 YDOT =      21202
680887  feet/sec       YDOT =        6462
577134  meter/sec
 ZDOT =       7867
325103                 ZDOT =        2397
960691


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   16248
84174274  
00016717  00000-0  10270-3 0  9083
2 25544  51
6435  20
5909 0003157 294
9153  65
1672 15
54360681 17374


Satellite: ISS
Catalog Number: 25544
Epoch time:      16248
84174274   =   yrday
fracday
Element set:     908
Inclination:       51
6435  deg
RA of node:        20
5909  deg
Eccentricity:     
0003157     
Arg of perigee:   294
9153  deg
Mean anomaly:      65
1672  deg
Mean motion:   15
54360681  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1737
Checksum:              321


Coasting Arc #10 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2016/249/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5239361
56                 A    =         6782104
94  meter
 Y    =        1786089
84  meter          E    =           
0009106
 Z    =        3914108
77                 I    =           51
74171
 XDOT =      -4613
356157                 Wp   =           67
83477
 YDOT =      -4572
131963  meter/sec      RA   =           15
06577  deg
 ZDOT =      -4078
059671                 TA   =           64
83596
                                          MA   =           64
74155
                                          Ha   =            219
818  n
mi
                                          Hp   =            215
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17189506
43                 X    =        -5277957
73
 Y    =        5859874
81  feet           Y    =         1727284
42  meter
 Z    =       12841564
19                 Z    =         3888563
32
 XDOT =     -15135
682929                 XDOT =       -4542
077082
 YDOT =     -15000
432950  feet/sec       YDOT =       -4623
323505  meter/sec
 ZDOT =     -13379
460863                 ZDOT =       -4100
296569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9662448
98                 X    =        -2945114
45
 Y    =      -15469892
91  feet           Y    =        -4715223
36  meter
 Z    =       12729592
62                 Z    =         3879979
83
 XDOT =      10026
544721                 XDOT =        3056
090831
 YDOT =     -17381
041116  feet/sec       YDOT =       -5297
741332  meter/sec
 ZDOT =     -13475
750460                 ZDOT =       -4107
408740


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   16249
87040532  
00016717  00000-0  10270-3 0  9097
2 25544  51
6427  15
4612 0003133 302
1494  57
9354 15
54416661 17537


Satellite: ISS
Catalog Number: 25544
Epoch time:      16249
87040532   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:        15
4612  deg
Eccentricity:     
0003133     
Arg of perigee:   302
1494  deg
Mean anomaly:      57
9354  deg
Mean motion:   15
54416661  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1753
Checksum:              298


Coasting Arc #11 (Orbit 1767)
---------------------------------------

Vector Time (GMT): 2016/250/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6244413
89                 A    =         6785964
56  meter
 Y    =        -889132
91  meter          E    =           
0005629
 Z    =       -2495730
63                 I    =           51
72236
 XDOT =       2800
101368                 Wp   =           15
91715
 YDOT =       4760
769061  meter/sec      RA   =           10
09055  deg
 ZDOT =       5318
007370                 TA   =          316
13377
                                          MA   =          316
17845
                                          Ha   =            219
902  n
mi
                                          Hp   =            215
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20486922
22                 X    =         6266015
51
 Y    =       -2917102
73  feet           Y    =         -819183
16  meter
 Z    =       -8188092
63                 Z    =        -2465344
23
 XDOT =       9186
684279                 XDOT =        2720
824497
 YDOT =      15619
321065  feet/sec       YDOT =        4791
638938  meter/sec
 ZDOT =      17447
530742                 ZDOT =        5331
416553

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7877428
72                 X    =         2401040
27
 Y    =       19191899
99  feet           Y    =         5849691
12  meter
 Z    =       -8055148
83                 Z    =        -2455209
36
 XDOT =     -11511
489874                 XDOT =       -3508
702114
 YDOT =      12060
800042  feet/sec       YDOT =        3676
131853  meter/sec
 ZDOT =      17505
201449                 ZDOT =        5335
585402


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   16250
83477387  
00016717  00000-0  10270-3 0  9109
2 25544  51
6419  10
6533 0003030 305
8665  54
2206 15
54405259 17686


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
83477387   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:        10
6533  deg
Eccentricity:     
0003030     
Arg of perigee:   305
8665  deg
Mean anomaly:      54
2206  deg
Mean motion:   15
54405259  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1768
Checksum:              299


Coasting Arc #12 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2016/250/21:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909415
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2246938
50                 A    =         6778780
54  meter
 Y    =       -4239003
60  meter          E    =           
0009975
 Z    =       -4798420
15                 I    =           51
69553
 XDOT =       7154
674902                 Wp   =           56
43633
 YDOT =       -841
687279  meter/sec      RA   =            9
88824  deg
 ZDOT =      -2605
250988                 TA   =          187
87374
                                          MA   =          187
88941
                                          Ha   =            219
855  n
mi
                                          Hp   =            215
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7371845
48                 X    =        -2176061
19
 Y    =      -13907492
14  feet           Y    =        -4263734
55  meter
 Z    =      -15742848
27                 Z    =        -4809162
66
 XDOT =      23473
342854                 XDOT =        7176
210321
 YDOT =      -2761
441204  feet/sec       YDOT =        -761
558758  meter/sec
 ZDOT =      -8547
411377                 ZDOT =       -2570
442923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7995212
19                 X    =         2436940
68
 Y    =      -13504991
48  feet           Y    =        -4116321
40  meter
 Z    =      -15788967
75                 Z    =        -4812477
37
 XDOT =      13754
128337                 XDOT =        4192
258317
 YDOT =      17963
326443  feet/sec       YDOT =        5475
221900  meter/sec
 ZDOT =      -8395
156910                 ZDOT =       -2558
843826


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   16250
89906566  
00016717  00000-0  10270-3 0  9112
2 25544  51
6406  10
3317 0003162 306
4343  53
6518 15
54384249 17690


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
89906566   =   yrday
fracday
Element set:     911
Inclination:       51
6406  deg
RA of node:        10
3317  deg
Eccentricity:     
0003162     
Arg of perigee:   306
4343  deg
Mean anomaly:      53
6518  deg
Mean motion:   15
54384249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1769
Checksum:              306


Coasting Arc #13 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2016/250/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1950692
44                 A    =         6778281
38  meter
 Y    =        4259062
08  meter          E    =           
0003326
 Z    =        4897035
09                 I    =           51
69332
 XDOT =      -7275
344233                 Wp   =          117
82512
 YDOT =        632
682591  meter/sec      RA   =            9
72449  deg
 ZDOT =       2345
078896                 TA   =          309
22872
                                          MA   =          309
25824
                                          Ha   =            219
732  n
mi
                                          Hp   =            215
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6399909
57                 X    =         1879133
81
 Y    =       13973300
79  feet           Y    =         4280476
41  meter
 Z    =       16066388
07                 Z    =         4906336
85
 XDOT =     -23869
239611                 XDOT =       -7293
269735
 YDOT =       2075
730287  feet/sec       YDOT =         551
224823  meter/sec
 ZDOT =       7693
828399                 ZDOT =        2309
693437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5788078
07                 X    =        -1764206
19
 Y    =       14192568
89  feet           Y    =         4325895
00  meter
 Z    =       16106208
24                 Z    =         4909172
27
 XDOT =     -16952
519640                 XDOT =       -5167
127986
 YDOT =     -15479
426532  feet/sec       YDOT =       -4718
129207  meter/sec
 ZDOT =       7539
091769                 ZDOT =        2297
915171


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   16250
96335634  
00016717  00000-0  10270-3 0  9123
2 25544  51
6408  10
0115 0003332 305
1113  54
9727 15
54408495 17703


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
96335634   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:        10
0115  deg
Eccentricity:     
0003332     
Arg of perigee:   305
1113  deg
Mean anomaly:      54
9727  deg
Mean motion:   15
54408495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1770
Checksum:              280


Coasting Arc #14 (Orbit 1784)
---------------------------------------

Vector Time (GMT): 2016/251/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -55672
64                 A    =         6776611
21  meter
 Y    =       -4220814
23  meter          E    =           
0012588
 Z    =       -5312078
18                 I    =           51
65583
 XDOT =       7643
656676                 Wp   =           77
06320
 YDOT =        349
490202  meter/sec      RA   =            4
72558  deg
 ZDOT =       -355
761049                 TA   =          189
52991
                                          MA   =          189
55382
                                          Ha   =            219
889  n
mi
                                          Hp   =            215
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -182653
02                 X    =           17333
56
 Y    =      -13847815
71  feet           Y    =        -4221029
06  meter
 Z    =      -17428078
03                 Z    =        -5312170
93
 XDOT =      25077
613766                 XDOT =        7640
908632
 YDOT =       1146
621399  feet/sec       YDOT =         434
951295  meter/sec
 ZDOT =      -1167
195042                 ZDOT =        -318
636704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9821155
21                 X    =         2993488
11
 Y    =       -9764971
25  feet           Y    =        -2976363
24  meter
 Z    =      -17427665
15                 Z    =        -5311952
34
 XDOT =      16067
350296                 XDOT =        4897
328370
 YDOT =      17965
495007  feet/sec       YDOT =        5475
882878  meter/sec
 ZDOT =      -1005
060846                 ZDOT =        -306
342546


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   16251
92771981  
00016717  00000-0  10270-3 0  9130
2 25544  51
6411   5
2021 0003285 309
7869  50
2995 15
54394910 17852


Satellite: ISS
Catalog Number: 25544
Epoch time:      16251
92771981   =   yrday
fracday
Element set:     913
Inclination:       51
6411  deg
RA of node:         5
2021  deg
Eccentricity:     
0003285     
Arg of perigee:   309
7869  deg
Mean anomaly:      50
2995  deg
Mean motion:   15
54394910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1785
Checksum:              316


Coasting Arc #15 (Orbit 1800)
---------------------------------------

Vector Time (GMT): 2016/252/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1877629
91                 A    =         6777516
17  meter
 Y    =        4048096
47  meter          E    =           
0005681
 Z    =        5100958
53                 I    =           51
62744
 XDOT =      -7370
063833                 Wp   =           18
82395
 YDOT =      -1294
522356  meter/sec      RA   =          359
72365  deg
 ZDOT =      -1679
763079                 TA   =           87
43165
                                          MA   =           87
36661
                                          Ha   =            220
022  n
mi
                                          Hp   =            215
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6160203
13                 X    =        -1947535
51
 Y    =       13281156
41  feet           Y    =         4026709
08  meter
 Z    =       16735428
24                 Z    =         5091667
35
 XDOT =     -24179
999451                 XDOT =       -7346
880816
 YDOT =      -4247
120592  feet/sec       YDOT =       -1376
809852  meter/sec
 ZDOT =      -5511
033724                 ZDOT =       -1715
508653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13777973
89                 X    =        -4199526
44
 Y    =        5088015
98  feet           Y    =         1550827
27  meter
 Z    =       16694050
00                 Z    =         5088346
44
 XDOT =     -13883
527866                 XDOT =       -4231
699294
 YDOT =     -18939
599494  feet/sec       YDOT =       -5772
789926  meter/sec
 ZDOT =      -5666
951608                 ZDOT =       -1727
286850


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   16252
95636657  
00016717  00000-0  10270-3 0  9145
2 25544  51
6418    
0725 0003389 314
4617  45
6258 15
54411136 18011


Satellite: ISS
Catalog Number: 25544
Epoch time:      16252
95636657   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:          
0725  deg
Eccentricity:     
0003389     
Arg of perigee:   314
4617  deg
Mean anomaly:      45
6258  deg
Mean motion:   15
54411136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1801
Checksum:              300


Coasting Arc #16 (Orbit 1815)
---------------------------------------

Vector Time (GMT): 2016/253/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3634508
88                 A    =         6780716
35  meter
 Y    =       -3768555
82  meter          E    =           
0005613
 Z    =       -4313884
87                 I    =           51
60523
 XDOT =       6445
996216                 Wp   =           92
49704
 YDOT =       2200
210732  meter/sec      RA   =          354
72571  deg
 ZDOT =       3512
479427                 TA   =          213
27430
                                          MA   =          213
30960
                                          Ha   =            220
108  n
mi
                                          Hp   =            215
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11924241
72                 X    =         3697334
70
 Y    =      -12364028
27  feet           Y    =        -3727561
32  meter
 Z    =      -14153165
59                 Z    =        -4296076
49
 XDOT =      21148
281549                 XDOT =        6403
851707
 YDOT =       7218
539148  feet/sec       YDOT =        2272
058774  meter/sec
 ZDOT =      11523
882634                 ZDOT =        3543
689948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17227250
83                 X    =         5250866
05
 Y    =        -703796
94  feet           Y    =         -214517
31  meter
 Z    =      -14074634
30                 Z    =        -4289948
54
 XDOT =      10271
146766                 XDOT =        3130
645534
 YDOT =      18483
388759  feet/sec       YDOT =        5633
736894  meter/sec
 ZDOT =      11659
804847                 ZDOT =        3553
908517


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   16253
92071725  
00016717  00000-0  10270-3 0  9153
2 25544  51
6412 355
2636 0003466 319
2076  40
8817 15
54407701 18166


Satellite: ISS
Catalog Number: 25544
Epoch time:      16253
92071725   =   yrday
fracday
Element set:     915
Inclination:       51
6412  deg
RA of node:       355
2636  deg
Eccentricity:     
0003466     
Arg of perigee:   319
2076  deg
Mean anomaly:      40
8817  deg
Mean motion:   15
54407701  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1816
Checksum:              303


Coasting Arc #17 (Orbit 1817)
---------------------------------------

Vector Time (GMT): 2016/254/00:46:20
071
Vector Time (MET): N/A
Weight (LBS)     : 893926
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1164491
78                 A    =         6778602
83  meter
 Y    =       -4093032
17  meter          E    =           
0010163
 Z    =       -5285152
20                 I    =           51
59056
 XDOT =       7522
327614                 Wp   =           74
90182
 YDOT =      -1292
441186  meter/sec      RA   =          354
15219  deg
 ZDOT =       -654
961785                 TA   =          188
82524
                                          MA   =          188
84312
                                          Ha   =            220
042  n
mi
                                          Hp   =            217
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3820511
10                 X    =        -1092962
92
 Y    =      -13428583
23  feet           Y    =        -4105654
71  meter
 Z    =      -17339738
20                 Z    =        -5290635
00
 XDOT =      24679
552539                 XDOT =        7539
402466
 YDOT =      -4240
292604  feet/sec       YDOT =       -1208
226052  meter/sec
 ZDOT =      -2148
824753                 ZDOT =        -618
378652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3759936
34                 X    =        -1146028
60
 Y    =      -13415751
56  feet           Y    =        -4089121
08  meter
 Z    =      -17362896
13                 Z    =        -5292210
74
 XDOT =      23698
137282                 XDOT =        7223
192244
 YDOT =      -4061
318352  feet/sec       YDOT =       -1237
889834  meter/sec
 ZDOT =      -1988
753809                 ZDOT =        -606
172161


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   16254
04930123  
00016717  00000-0  10270-3 0  9164
2 25544  51
6438 354
6233 0004992 285
9051  74
1551 15
53741229 18189


Satellite: ISS
Catalog Number: 25544
Epoch time:      16254
04930123   =   yrday
fracday
Element set:     916
Inclination:       51
6438  deg
RA of node:       354
6233  deg
Eccentricity:     
0004992     
Arg of perigee:   285
9051  deg
Mean anomaly:      74
1551  deg
Mean motion:   15
53741229  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1818
Checksum:              307


Coasting Arc #18 (Orbit 1833)
---------------------------------------

Vector Time (GMT): 2016/255/00:46:20
071
Vector Time (MET): N/A
Weight (LBS)     : 893926
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -481594
80                 A    =         6778854
34  meter
 Y    =        4306795
45  meter          E    =           
0004246
 Z    =        5214815
28                 I    =           51
55953
 XDOT =      -7563
205747                 Wp   =          336
84392
 YDOT =        532
281257  meter/sec      RA   =          349
15282  deg
 ZDOT =      -1134
563242                 TA   =          124
06753
                                          MA   =          124
02721
                                          Ha   =            220
095  n
mi
                                          Hp   =            217
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1580035
44                 X    =         -555049
95
 Y    =       14129906
32  feet           Y    =         4300999
55  meter
 Z    =       17108974
00                 Z    =         5212297
13
 XDOT =     -24813
667150                 XDOT =       -7563
084534
 YDOT =       1746
329583  feet/sec       YDOT =         447
705029  meter/sec
 ZDOT =      -3722
320347                 ZDOT =       -1171
303038

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1392837
86                 X    =         -424536
98
 Y    =       14163883
62  feet           Y    =         4317151
73  meter
 Z    =       17097138
93                 Z    =         5211207
95
 XDOT =     -23713
974644                 XDOT =       -7228
019471
 YDOT =       2368
982060  feet/sec       YDOT =         722
065732  meter/sec
 ZDOT =      -3882
921187                 ZDOT =       -1183
514378


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   16255
07839798  
00016717  00000-0  10270-3 0  9175
2 25544  51
6437 349
4972 0005232 288
9871  71
0714 15
53771208 18346


Satellite: ISS
Catalog Number: 25544
Epoch time:      16255
07839798   =   yrday
fracday
Element set:     917
Inclination:       51
6437  deg
RA of node:       349
4972  deg
Eccentricity:     
0005232     
Arg of perigee:   288
9871  deg
Mean anomaly:      71
0714  deg
Mean motion:   15
53771208  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1834
Checksum:              345


Coasting Arc #19 (Orbit 1848)
---------------------------------------

Vector Time (GMT): 2016/256/00:46:20
071
Vector Time (MET): N/A
Weight (LBS)     : 893926
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2050090
27                 A    =         6781177
26  meter
 Y    =       -4454249
93  meter          E    =           
0005440
 Z    =       -4689345
36                 I    =           51
53667
 XDOT =       7118
208954                 Wp   =          105
26651
 YDOT =        308
441974  meter/sec      RA   =          344
15355  deg
 ZDOT =       2820
296747                 TA   =          192
76411
                                          MA   =          192
77788
                                          Ha   =            220
293  n
mi
                                          Hp   =            217
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6726017
95                 X    =         2122525
16
 Y    =      -14613680
88  feet           Y    =        -4430919
77  meter
 Z    =      -15384991
34                 Z    =        -4679210
34
 XDOT =      23353
703917                 XDOT =        7100
531124
 YDOT =       1011
948732  feet/sec       YDOT =         387
943909  meter/sec
 ZDOT =       9252
942082                 ZDOT =        2854
832076

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6261468
21                 X    =         1908495
51
 Y    =      -14865385
91  feet           Y    =        -4530969
63  meter
 Z    =      -15339858
62                 Z    =        -4675588
91
 XDOT =      22231
045051                 XDOT =        6776
022531
 YDOT =       -335
398173  feet/sec       YDOT =        -102
229363  meter/sec
 ZDOT =       9403
743974                 ZDOT =        2866
261163


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   16256
04317173  
00016717  00000-0  10270-3 0  9182
2 25544  51
6448 344
6906 0005204 293
5171  66
5434 15
53747795 18494


Satellite: ISS
Catalog Number: 25544
Epoch time:      16256
04317173   =   yrday
fracday
Element set:     918
Inclination:       51
6448  deg
RA of node:       344
6906  deg
Eccentricity:     
0005204     
Arg of perigee:   293
5171  deg
Mean anomaly:      66
5434  deg
Mean motion:   15
53747795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1849
Checksum:              330


Coasting Arc #20 (Orbit 1864)
---------------------------------------

Vector Time (GMT): 2016/257/00:46:20
071
Vector Time (MET): N/A
Weight (LBS)     : 893926
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3453912
04                 A    =         6784590
73  meter
 Y    =        4489045
53  meter          E    =           
0008009
 Z    =        3731845
59                 I    =           51
51688
 XDOT =      -6246
402864                 Wp   =           63
44786
 YDOT =      -1250
878228  meter/sec      RA   =          339
16060  deg
 ZDOT =      -4265
905243                 TA   =           71
89608
                                          MA   =           71
80887
                                          Ha   =            220
496  n
mi
                                          Hp   =            216
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11331732
41                 X    =        -3521980
55
 Y    =       14727839
67  feet           Y    =         4450041
29  meter
 Z    =       12243587
91                 Z    =         3714901
78
 XDOT =     -20493
447718                 XDOT =       -6211
229206
 YDOT =      -4103
931194  feet/sec       YDOT =       -1320
533381  meter/sec
 ZDOT =     -13995
752110                 ZDOT =       -4296
162936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10576774
59                 X    =        -3223800
90
 Y    =       15338745
45  feet           Y    =         4675249
61  meter
 Z    =       12168713
69                 Z    =         3709023
93
 XDOT =     -19480
128027                 XDOT =       -5937
543023
 YDOT =      -2196
737923  feet/sec       YDOT =        -669
565719  meter/sec
 ZDOT =     -14127
681859                 ZDOT =       -4306
117431


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   16257
07225758  
00016717  00000-0  10270-3 0  9194
2 25544  51
6443 339
5645 0005090 298
5232  61
5407 15
53753386 18654


Satellite: ISS
Catalog Number: 25544
Epoch time:      16257
07225758   =   yrday
fracday
Element set:     919
Inclination:       51
6443  deg
RA of node:       339
5645  deg
Eccentricity:     
0005090     
Arg of perigee:   298
5232  deg
Mean anomaly:      61
5407  deg
Mean motion:   15
53753386  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1865
Checksum:              332
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