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

 
Date: August 11th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 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


229/22:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 212 8

233/21:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 212 9

237/07:37:09 920 1 3 4 6 4 6
N/A 4 4 -0 5 219 7
000/00:14:15 840 0 4 -0 0 215 9

Coasting Arc #1 (Orbit 1342)
---------------------------------------

Vector Time (GMT): 2016/223/11:03:48
188
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5397424
35                 A    =         6779874
79  meter
 Y    =        -247303
20  meter          E    =           
0012371
 Z    =        4087361
11                 I    =           51
83946
 XDOT =       3202
101831                 Wp   =          104
16335
 YDOT =      -5804
255788  meter/sec      RA   =          146
14976  deg
 ZDOT =       3864
514481                 TA   =          305
94765
                                          MA   =          306
06235
                                          Ha   =            220
360  n
mi
                                          Hp   =            212
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17708085
13                 X    =        -5414112
27
 Y    =        -811362
22  feet           Y    =         -307754
07  meter
 Z    =       13409977
41                 Z    =         4061101
46
 XDOT =      10505
583434                 XDOT =        3247
996505
 YDOT =     -19042
833951  feet/sec       YDOT =       -5768
191085  meter/sec
 ZDOT =      12678
853284                 ZDOT =        3880
180907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9399662
90                 X    =         2865017
25
 Y    =       15130855
38  feet           Y    =         4611884
72  meter
 Z    =       13295323
79                 Z    =         4052414
69
 XDOT =     -20494
938882                 XDOT =       -6246
857371
 YDOT =       1493
229204  feet/sec       YDOT =         455
136261  meter/sec
 ZDOT =      12748
218143                 ZDOT =        3885
656890


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16223
51637333  
00016717  00000-0  10270-3 0  9002
2 25544  51
6414 146
9466 0001697 113
5366 246
5966 15
54981114 13435


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
51637333   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:       146
9466  deg
Eccentricity:     
0001697     
Arg of perigee:   113
5366  deg
Mean anomaly:     246
5966  deg
Mean motion:   15
54981114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1343
Checksum:              311


Coasting Arc #2 (Orbit 1357)
---------------------------------------

Vector Time (GMT): 2016/224/11:03:48
188
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4146650
72                 A    =         6776086
18  meter
 Y    =        1773928
75  meter          E    =           
0014472
 Z    =       -5070053
49                 I    =           51
85294
 XDOT =      -4741
052056                 Wp   =           80
01023
 YDOT =       5713
293870  meter/sec      RA   =          141
16320  deg
 ZDOT =      -1880
699086                 TA   =          171
80670
                                          MA   =          171
78304
                                          Ha   =            220
279  n
mi
                                          Hp   =            212
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13604497
12                 X    =         4151133
96
 Y    =        5819976
21  feet           Y    =         1820324
43  meter
 Z    =      -16634033
75                 Z    =        -5049899
37
 XDOT =     -15554
632729                 XDOT =       -4795
451635
 YDOT =      18744
402461  feet/sec       YDOT =        5659
972087  meter/sec
 ZDOT =      -6170
272593                 ZDOT =       -1903
861887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3210804
20                 X    =         -978653
12
 Y    =      -14544987
58  feet           Y    =        -4433312
21  meter
 Z    =      -16546287
09                 Z    =        -5043308
30
 XDOT =      23206
500928                 XDOT =        7073
341483
 YDOT =       2004
647041  feet/sec       YDOT =         611
016418  meter/sec
 ZDOT =      -6272
382392                 ZDOT =       -1911
822153


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16224
48038414  
00016717  00000-0  10270-3 0  9015
2 25544  51
6412 142
1347 0001757 109
8357 250
2986 15
54980674 13584


Satellite: ISS
Catalog Number: 25544
Epoch time:      16224
48038414   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       142
1347  deg
Eccentricity:     
0001757     
Arg of perigee:   109
8357  deg
Mean anomaly:     250
2986  deg
Mean motion:   15
54980674  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1358
Checksum:              313


Coasting Arc #3 (Orbit 1373)
---------------------------------------

Vector Time (GMT): 2016/225/11:03:48
188
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2601433
51                 A    =         6774798
74  meter
 Y    =       -3288417
98  meter          E    =           
0003823
 Z    =        5318052
16                 I    =           51
87378
 XDOT =       5720
016819                 Wp   =           91
45736
 YDOT =      -5102
431012  meter/sec      RA   =          136
17180  deg
 ZDOT =       -356
899950                 TA   =            1
93302
                                          MA   =            1
93154
                                          Ha   =            220
216  n
mi
                                          Hp   =            212
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8534886
83                 X    =        -2590300
82
 Y    =      -10788772
90  feet           Y    =        -3317446
75  meter
 Z    =       17447677
68                 Z    =         5305442
17
 XDOT =      18766
459379                 XDOT =        5778
382021
 YDOT =     -16740
259226  feet/sec       YDOT =       -5038
139618  meter/sec
 ZDOT =      -1170
931593                 ZDOT =        -328
972073

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3544527
54                 X    =        -1080371
99
 Y    =       13363334
93  feet           Y    =         4073144
49  meter
 Z    =       17393130
09                 Z    =         5301426
05
 XDOT =     -23642
858311                 XDOT =       -7206
343213
 YDOT =      -4906
413277  feet/sec       YDOT =       -1495
474767  meter/sec
 ZDOT =      -1048
086655                 ZDOT =        -319
456812


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   16225
50865310  
00016717  00000-0  10270-3 0  9023
2 25544  51
6414 137
0037 0001530 118
0297 242
1011 15
55014515 13749


Satellite: ISS
Catalog Number: 25544
Epoch time:      16225
50865310   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:       137
0037  deg
Eccentricity:     
0001530     
Arg of perigee:   118
0297  deg
Mean anomaly:     242
1011  deg
Mean motion:   15
55014515  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1374
Checksum:              256


Coasting Arc #4 (Orbit 1388)
---------------------------------------

Vector Time (GMT): 2016/226/11:03:48
188
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         965847
56                 A    =         6776899
33  meter
 Y    =        4657877
87  meter          E    =           
0013203
 Z    =       -4839264
35                 I    =           51
90433
 XDOT =      -6074
190757                 Wp   =          109
55426
 YDOT =       3907
181374  meter/sec      RA   =          131
18130  deg
 ZDOT =       2549
762239                 TA   =          185
46340
                                          MA   =          185
47782
                                          Ha   =            220
161  n
mi
                                          Hp   =            212
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3168791
20                 X    =          937197
01
 Y    =       15281751
55  feet           Y    =         4668518
51  meter
 Z    =      -15876851
53                 Z    =        -4834642
06
 XDOT =     -19928
447367                 XDOT =       -6129
815913
 YDOT =      12818
836528  feet/sec       YDOT =        3838
944649  meter/sec
 ZDOT =       8365
361675                 ZDOT =        2520
120627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10149222
85                 X    =         3093483
13
 Y    =      -11882038
13  feet           Y    =        -3621645
22  meter
 Z    =      -15857428
16                 Z    =        -4833344
10
 XDOT =      21456
125116                 XDOT =        6539
826935
 YDOT =       7342
529312  feet/sec       YDOT =        2238
002934  meter/sec
 ZDOT =       8235
206851                 ZDOT =        2510
091048


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   16226
47264915  
00016717  00000-0  10270-3 0  9035
2 25544  51
6424 132
1914 0001621 118
9928 241
1388 15
55002164 13890


Satellite: ISS
Catalog Number: 25544
Epoch time:      16226
47264915   =   yrday
fracday
Element set:     903
Inclination:       51
6424  deg
RA of node:       132
1914  deg
Eccentricity:     
0001621     
Arg of perigee:   118
9928  deg
Mean anomaly:     241
1388  deg
Mean motion:   15
55002164  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1389
Checksum:              299


Coasting Arc #5 (Orbit 1404)
---------------------------------------

Vector Time (GMT): 2016/227/11:03:48
188
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         613620
65                 A    =         6781117
35  meter
 Y    =       -5675312
00  meter          E    =           
0013236
 Z    =        3648904
05                 I    =           51
93910
 XDOT =       5885
819763                 Wp   =           90
02714
 YDOT =      -2203
536237  meter/sec      RA   =          126
20445  deg
 ZDOT =      -4403
319193                 TA   =           46
81238
                                          MA   =           46
70187
                                          Ha   =            220
169  n
mi
                                          Hp   =            212
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2013191
09                 X    =          659313
26
 Y    =      -18619790
01  feet           Y    =        -5668194
67  meter
 Z    =       11971469
97                 Z    =         3651995
69
 XDOT =      19310
432292                 XDOT =        5931
411947
 YDOT =      -7229
449598  feet/sec       YDOT =       -2137
462063  meter/sec
 ZDOT =     -14446
585280                 ZDOT =       -4374
617057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15793955
76                 X    =        -4813997
72
 Y    =       10047593
54  feet           Y    =         3062506
51  meter
 Z    =       11985926
64                 Z    =         3653310
44
 XDOT =     -16986
177504                 XDOT =       -5177
386903
 YDOT =      -9563
614082  feet/sec       YDOT =       -2914
989572  meter/sec
 ZDOT =     -14320
800740                 ZDOT =       -4364
980065


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   16227
50090222  
00016717  00000-0  10270-3 0  9049
2 25544  51
6425 127
0598 0001652 121
5158 238
6157 15
55003241 14052


Satellite: ISS
Catalog Number: 25544
Epoch time:      16227
50090222   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:       127
0598  deg
Eccentricity:     
0001652     
Arg of perigee:   121
5158  deg
Mean anomaly:     238
6157  deg
Mean motion:   15
55003241  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1405
Checksum:              275


Coasting Arc #6 (Orbit 1419)
---------------------------------------

Vector Time (GMT): 2016/228/11:03:48
188
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1955670
52                 A    =         6785048
00  meter
 Y    =        6190648
17  meter          E    =           
0007057
 Z    =       -1967446
86                 I    =           51
97116
 XDOT =      -5216
656117                 Wp   =           53
03109
 YDOT =        131
089697  meter/sec      RA   =          121
24197  deg
 ZDOT =       5615
893304                 TA   =          285
36497
                                          MA   =          285
44294
                                          Ha   =            220
065  n
mi
                                          Hp   =            212
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6416241
87                 X    =        -2015193
72
 Y    =       20310525
50  feet           Y    =         6168445
76  meter
 Z    =       -6454878
14                 Z    =        -1977091
36
 XDOT =     -17115
013507                 XDOT =       -5245
013408
 YDOT =        430
084308  feet/sec       YDOT =          72
594944  meter/sec
 ZDOT =      18424
846798                 ZDOT =        5590
483653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19742346
35                 X    =         6017467
17
 Y    =       -7960274
24  feet           Y    =        -2426291
59  meter
 Z    =       -6498065
26                 Z    =        -1980610
29
 XDOT =      10688
404192                 XDOT =        3257
825598
 YDOT =      11606
491579  feet/sec       YDOT =        3537
658633  meter/sec
 ZDOT =      18313
783103                 ZDOT =        5582
041090


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   16228
46488223  
00016717  00000-0  10270-3 0  9058
2 25544  51
6429 122
2484 0001576 127
1610 232
9687 15
55027198 14206


Satellite: ISS
Catalog Number: 25544
Epoch time:      16228
46488223   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:       122
2484  deg
Eccentricity:     
0001576     
Arg of perigee:   127
1610  deg
Mean anomaly:     232
9687  deg
Mean motion:   15
55027198  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1420
Checksum:              308


Coasting Arc #7 (Orbit 1435)
---------------------------------------

Vector Time (GMT): 2016/229/11:03:48
188
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3028091
98                 A    =         6786761
94  meter
 Y    =       -6066402
05  meter          E    =           
0013667
 Z    =         -35681
99                 I    =           51
99341
 XDOT =       4215
398597                 Wp   =          134
88097
 YDOT =       2131
350567  meter/sec      RA   =          116
29080  deg
 ZDOT =      -6044
218748                 TA   =           45
50171
                                          MA   =           45
39008
                                          Ha   =            220
075  n
mi
                                          Hp   =            212
862

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9934684
97                 X    =         3095876
29
 Y    =      -19902893
87  feet           Y    =        -6032160
90  meter
 Z    =        -117066
90                 Z    =          -20807
90
 XDOT =      13830
047892                 XDOT =        4220
611632
 YDOT =       6992
619970  feet/sec       YDOT =        2178
519092  meter/sec
 ZDOT =     -19830
114001                 ZDOT =       -6023
729149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21598828
13                 X    =        -6583322
81
 Y    =        5322111
72  feet           Y    =         1622179
65  meter
 Z    =         -51035
25                 Z    =          -15555
55
 XDOT =      -3326
622491                 XDOT =       -1013
954535
 YDOT =     -13587
348156  feet/sec       YDOT =       -4141
423718  meter/sec
 ZDOT =     -19740
924744                 ZDOT =       -6017
033862


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   16229
49312004  
00016717  00000-0  10270-3 0  9066
2 25544  51
6437 117
1164 0001580 135
4553 224
6727 15
55012447 14367


Satellite: ISS
Catalog Number: 25544
Epoch time:      16229
49312004   =   yrday
fracday
Element set:     906
Inclination:       51
6437  deg
RA of node:       117
1164  deg
Eccentricity:     
0001580     
Arg of perigee:   135
4553  deg
Mean anomaly:     224
6727  deg
Mean motion:   15
55012447  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1436
Checksum:              287


Coasting Arc #8 (Orbit 1442)
---------------------------------------

Vector Time (GMT): 2016/229/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1450640
32                 A    =         6778783
09  meter
 Y    =        5038129
96  meter          E    =           
0009970
 Z    =       -4307560
51                 I    =           51
97410
 XDOT =      -5057
241486                 Wp   =          116
35728
 YDOT =       4509
853940  meter/sec      RA   =          113
91658  deg
 ZDOT =       3573
705332                 TA   =          189
94661
                                          MA   =          189
96636
                                          Ha   =            219
973  n
mi
                                          Hp   =            212
847

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4759318
64                 X    =         1415118
71
 Y    =       16529297
75  feet           Y    =         5054153
31  meter
 Z    =      -14132416
37                 Z    =        -4300600
15
 XDOT =     -16591
999626                 XDOT =       -5124
655116
 YDOT =      14796
108728  feet/sec       YDOT =        4452
923602  meter/sec
 ZDOT =      11724
755027                 ZDOT =        3548
975226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11694490
21                 X    =        -3564480
62
 Y    =       12646839
90  feet           Y    =         3854756
80  meter
 Z    =      -14102848
29                 Z    =        -4298548
16
 XDOT =     -20332
350017                 XDOT =       -6197
300285
 YDOT =      -5855
658244  feet/sec       YDOT =       -1784
804633  meter/sec
 ZDOT =      11615
904726                 ZDOT =        3540
527761


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   16229
94296928  
00016717  00000-0  10270-3 0  9073
2 25544  51
6438 114
8683 0001793 144
6386 215
4887 15
55063554 14438


Satellite: ISS
Catalog Number: 25544
Epoch time:      16229
94296928   =   yrday
fracday
Element set:     907
Inclination:       51
6438  deg
RA of node:       114
8683  deg
Eccentricity:     
0001793     
Arg of perigee:   144
6386  deg
Mean anomaly:     215
4887  deg
Mean motion:   15
55063554  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1443
Checksum:              345


Coasting Arc #9 (Orbit 1458)
---------------------------------------

Vector Time (GMT): 2016/230/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -202453
40                 A    =         6783307
86  meter
 Y    =       -6163875
05  meter          E    =           
0014696
 Z    =        2807235
37                 I    =           52
00075
 XDOT =       5110
926868                 Wp   =          104
91076
 YDOT =      -2517
657429  meter/sec      RA   =          108
95037  deg
 ZDOT =      -5140
779835                 TA   =           43
37163
                                          MA   =           43
25607
                                          Ha   =            220
003  n
mi
                                          Hp   =            212
838

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -664217
18                 X    =         -147148
39
 Y    =      -20222687
16  feet           Y    =        -6165829
69  meter
 Z    =        9210089
79                 Z    =         2806386
46
 XDOT =      16768
132770                 XDOT =        5163
671264
 YDOT =      -8260
030936  feet/sec       YDOT =       -2460
208895  meter/sec
 ZDOT =     -16866
075574                 ZDOT =       -5115
824564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16791155
81                 X    =         5117944
29
 Y    =      -11291783
28  feet           Y    =        -3441735
55  meter
 Z    =        9207428
04                 Z    =         2806424
07
 XDOT =      15103
624959                 XDOT =        4603
584887
 YDOT =       8746
018884  feet/sec       YDOT =        2665
786556  meter/sec
 ZDOT =     -16756
568748                 ZDOT =       -5107
402154


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   16230
97119548  
00016717  00000-0  10270-3 0  9081
2 25544  51
6433 109
7363 0001744 144
7723 215
3546 15
55050441 14592


Satellite: ISS
Catalog Number: 25544
Epoch time:      16230
97119548   =   yrday
fracday
Element set:     908
Inclination:       51
6433  deg
RA of node:       109
7363  deg
Eccentricity:     
0001744     
Arg of perigee:   144
7723  deg
Mean anomaly:     215
3546  deg
Mean motion:   15
55050441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1459
Checksum:              307


Coasting Arc #10 (Orbit 1473)
---------------------------------------

Vector Time (GMT): 2016/231/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -909476
16                 A    =         6786358
15  meter
 Y    =        6656751
22  meter          E    =           
0009503
 Z    =        -931965
62                 I    =           52
01967
 XDOT =      -4830
946741                 Wp   =           47
82292
 YDOT =        167
020988  meter/sec      RA   =          103
99711  deg
 ZDOT =       5952
236948                 TA   =          302
13829
                                          MA   =          302
23047
                                          Ha   =            219
943  n
mi
                                          Hp   =            212
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2983845
68                 X    =         -979319
05
 Y    =       21839734
96  feet           Y    =         6646190
28  meter
 Z    =       -3057630
00                 Z    =         -936553
54
 XDOT =     -15849
562799                 XDOT =       -4861
368194
 YDOT =        547
969120  feet/sec       YDOT =         112
828337  meter/sec
 ZDOT =      19528
336445                 ZDOT =        5928
695992

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19954004
68                 X    =        -6081980
63
 Y    =        9358686
09  feet           Y    =         2852527
52  meter
 Z    =       -3078823
00                 Z    =         -938425
25
 XDOT =      -8446
521727                 XDOT =       -2574
499822
 YDOT =     -11666
683018  feet/sec       YDOT =       -3556
004984  meter/sec
 ZDOT =      19425
406163                 ZDOT =        5920
863799


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   16231
93515132  
00016717  00000-0  10270-3 0  9098
2 25544  51
6427 104
9248 0001546 148
8514 211
2731 15
55020905 14747


Satellite: ISS
Catalog Number: 25544
Epoch time:      16231
93515132   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:       104
9248  deg
Eccentricity:     
0001546     
Arg of perigee:   148
8514  deg
Mean anomaly:     211
2731  deg
Mean motion:   15
55020905  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1474
Checksum:              289


Coasting Arc #11 (Orbit 1489)
---------------------------------------

Vector Time (GMT): 2016/232/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1904909
62                 A    =         6786081
59  meter
 Y    =       -6411262
49  meter          E    =           
0011081
 Z    =       -1118192
72                 I    =           52
02558
 XDOT =       4306
837013                 Wp   =          143
51083
 YDOT =       2304
235042  meter/sec      RA   =           99
04917  deg
 ZDOT =      -5913
198622                 TA   =           48
56384
                                          MA   =           48
46869
                                          Ha   =            219
892  n
mi
                                          Hp   =            212
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6249703
47                 X    =         1981892
01
 Y    =      -21034325
77  feet           Y    =        -6389530
16  meter
 Z    =       -3668611
28                 Z    =        -1108751
88
 XDOT =      14130
042693                 XDOT =        4309
473666
 YDOT =       7559
826252  feet/sec       YDOT =        2352
411305  meter/sec
 ZDOT =     -19400
257945                 ZDOT =       -5892
271200

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20964550
01                 X    =         6389994
84
 Y    =       -6503721
62  feet           Y    =        -1982334
35  meter
 Z    =       -3626239
22                 Z    =        -1105277
71
 XDOT =       1186
846774                 XDOT =         361
750897
 YDOT =      14520
403073  feet/sec       YDOT =        4425
818857  meter/sec
 ZDOT =     -19309
174207                 ZDOT =       -5885
436298


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   16232
96336466  
00016717  00000-0  10270-3 0  9105
2 25544  51
6423  99
7921 0001654 153
0025 207
1214 15
55067147 14904


Satellite: ISS
Catalog Number: 25544
Epoch time:      16232
96336466   =   yrday
fracday
Element set:     910
Inclination:       51
6423  deg
RA of node:        99
7921  deg
Eccentricity:     
0001654     
Arg of perigee:   153
0025  deg
Mean anomaly:     207
1214  deg
Mean motion:   15
55067147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1490
Checksum:              293


Coasting Arc #12 (Orbit 1504)
---------------------------------------

Vector Time (GMT): 2016/233/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3855079
65                 A    =         6775381
20  meter
 Y    =       -2169589
38  meter          E    =           
0004957
 Z    =        5128258
95                 I    =           51
99533
 XDOT =       1856
609048                 Wp   =           72
66377
 YDOT =      -7255
346321  meter/sec      RA   =           94
31243  deg
 ZDOT =      -1671
049405                 TA   =           33
39599
                                          MA   =           33
36473
                                          Ha   =            219
866  n
mi
                                          Hp   =            212
890

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12647899
11                 X    =        -3855442
78
 Y    =       -7118075
41  feet           Y    =        -2212701
09  meter
 Z    =       16824996
54                 Z    =         5109531
47
 XDOT =       6091
237034                 XDOT =        1945
719314
 YDOT =     -23803
629661  feet/sec       YDOT =       -7234
086361  meter/sec
 ZDOT =      -5482
445553                 ZDOT =       -1661
813580

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3256034
43                 X    =          992439
30
 Y    =      -14239734
41  feet           Y    =        -4340271
05  meter
 Z    =       16743508
05                 Z    =         5103421
25
 XDOT =      23528
785144                 XDOT =        7171
573712
 YDOT =      -1028
132744  feet/sec       YDOT =        -313
374860  meter/sec
 ZDOT =      -5440
814410                 ZDOT =       -1658
360232


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   16233
92730642  
00016717  00000-0  10270-3 0  9117
2 25544  51
6433  94
9789 0001545 158
1861 201
9358 15
55116044 15056


Satellite: ISS
Catalog Number: 25544
Epoch time:      16233
92730642   =   yrday
fracday
Element set:     911
Inclination:       51
6433  deg
RA of node:        94
9789  deg
Eccentricity:     
0001545     
Arg of perigee:   158
1861  deg
Mean anomaly:     201
9358  deg
Mean motion:   15
55116044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1505
Checksum:              307


Coasting Arc #13 (Orbit 1519)
---------------------------------------

Vector Time (GMT): 2016/234/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3340513
86                 A    =         6779017
30  meter
 Y    =        4136531
26  meter          E    =           
0009076
 Z    =       -4215125
45                 I    =           52
00766
 XDOT =      -2832
163241                 Wp   =          117
75496
 YDOT =       6071
654617  meter/sec      RA   =           89
33541  deg
 ZDOT =       3715
924369                 TA   =          190
22031
                                          MA   =          190
23878
                                          Ha   =            219
758  n
mi
                                          Hp   =            212
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10959691
15                 X    =         3314484
93
 Y    =       13571296
77  feet           Y    =         4173741
25  meter
 Z    =      -13829151
73                 Z    =        -4198961
76
 XDOT =      -9291
874149                 XDOT =       -2917
897731
 YDOT =      19920
126696  feet/sec       YDOT =        6039
504395  meter/sec
 ZDOT =      12191
352917                 ZDOT =        3701
957836

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9680118
10                 X    =        -2950500
00
 Y    =       14578051
79  feet           Y    =         4443390
18  meter
 Z    =      -13759218
12                 Z    =        -4193809
68
 XDOT =     -20741
500710                 XDOT =       -6322
009416
 YDOT =      -2331
007906  feet/sec       YDOT =        -710
491210  meter/sec
 ZDOT =      12129
236561                 ZDOT =        3696
991304


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   16234
89124596  
00016717  00000-0  10270-3 0  9120
2 25544  51
6421  90
1678 0001678 158
5610 201
5614 15
55112046 15207


Satellite: ISS
Catalog Number: 25544
Epoch time:      16234
89124596   =   yrday
fracday
Element set:     912
Inclination:       51
6421  deg
RA of node:        90
1678  deg
Eccentricity:     
0001678     
Arg of perigee:   158
5610  deg
Mean anomaly:     201
5614  deg
Mean motion:   15
55112046  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1520
Checksum:              291


Coasting Arc #14 (Orbit 1535)
---------------------------------------

Vector Time (GMT): 2016/235/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2644046
65                 A    =         6783509
49  meter
 Y    =       -5642993
46  meter          E    =           
0014392
 Z    =        2661573
67                 I    =           52
02187
 XDOT =       3696
384823                 Wp   =          107
60002
 YDOT =      -4213
056124  meter/sec      RA   =           84
37118  deg
 ZDOT =      -5241
378996                 TA   =           42
51293
                                          MA   =           42
40157
                                          Ha   =            219
741  n
mi
                                          Hp   =            212
961

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8674693
73                 X    =        -2593677
47
 Y    =      -18513758
06  feet           Y    =        -5672279
14  meter
 Z    =        8732197
07                 Z    =         2648852
36
 XDOT =      12127
246794                 XDOT =        3768
681788
 YDOT =     -13822
362611  feet/sec       YDOT =       -4171
316809  meter/sec
 ZDOT =     -17196
125316                 ZDOT =       -5223
247084

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14848066
22                 X    =         4525690
58
 Y    =      -14088833
89  feet           Y    =        -4294276
57  meter
 Z    =        8677586
29                 Z    =         2644928
30
 XDOT =      15933
448618                 XDOT =        4856
515139
 YDOT =       6211
340735  feet/sec       YDOT =        1893
216656  meter/sec
 ZDOT =     -17116
116951                 ZDOT =       -5216
992447


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   16235
91944103  
00016717  00000-0  10270-3 0  9139
2 25544  51
6426  85
0348 0001504 162
5616 197
5589 15
55109845 15363


Satellite: ISS
Catalog Number: 25544
Epoch time:      16235
91944103   =   yrday
fracday
Element set:     913
Inclination:       51
6426  deg
RA of node:        85
0348  deg
Eccentricity:     
0001504     
Arg of perigee:   162
5616  deg
Mean anomaly:     197
5589  deg
Mean motion:   15
55109845  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1536
Checksum:              316


Coasting Arc #15 (Orbit 1550)
---------------------------------------

Vector Time (GMT): 2016/236/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1806465
19                 A    =         6786384
55  meter
 Y    =        6494640
59  meter          E    =           
0009820
 Z    =        -747149
83                 I    =           52
02700
 XDOT =      -4397
356877                 Wp   =           46
04303
 YDOT =       1905
417319  meter/sec      RA   =           79
41903  deg
 ZDOT =       5986
298810                 TA   =          305
92403
                                          MA   =          306
01511
                                          Ha   =            219
723  n
mi
                                          Hp   =            213
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5926723
06                 X    =         1737335
53
 Y    =       21307875
96  feet           Y    =         6514455
13  meter
 Z    =       -2451278
97                 Z    =         -738542
77
 XDOT =     -14427
023876                 XDOT =       -4447
415675
 YDOT =       6251
369156  feet/sec       YDOT =        1855
963570  meter/sec
 ZDOT =      19640
087960                 ZDOT =        5964
815936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18160804
19                 X    =        -5535413
12
 Y    =       12629894
60  feet           Y    =         3849591
88  meter
 Z    =       -2414818
03                 Z    =         -736036
53
 XDOT =      -9777
368333                 XDOT =       -2980
141868
 YDOT =     -10357
184503  feet/sec       YDOT =       -3156
869837  meter/sec
 ZDOT =      19545
834751                 ZDOT =        5957
570432


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   16236
88336805  
00016717  00000-0  10270-3 0  9141
2 25544  51
6427  80
2227 0001258 163
3508 196
7687 15
55061536 15513


Satellite: ISS
Catalog Number: 25544
Epoch time:      16236
88336805   =   yrday
fracday
Element set:     914
Inclination:       51
6427  deg
RA of node:        80
2227  deg
Eccentricity:     
0001258     
Arg of perigee:   163
3508  deg
Mean anomaly:     196
7687  deg
Mean motion:   15
55061536  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1551
Checksum:              318


Coasting Arc #16 (Orbit 1557)
---------------------------------------

Vector Time (GMT): 2016/237/07:44:17
840
Vector Time (MET): N/A
Weight (LBS)     : 929483
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4283560
29                 A    =         6780120
16  meter
 Y    =        2470266
12  meter          E    =           
0007725
 Z    =       -4646470
87                 I    =           51
99558
 XDOT =       -802
350404                 Wp   =          124
76693
 YDOT =       7009
823520  meter/sec      RA   =           77
21656  deg
 ZDOT =       2986
272828                 TA   =          174
88439
                                          MA   =          174
87649
                                          Ha   =            219
746  n
mi
                                          Hp   =            215
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14053675
50                 X    =         4278189
26
 Y    =        8104547
63  feet           Y    =         2518137
50  meter
 Z    =      -15244327
02                 Z    =        -4625675
65
 XDOT =      -2632
383214                 XDOT =        -895
182372
 YDOT =      22998
108663  feet/sec       YDOT =        7000
332191  meter/sec
 ZDOT =       9797
483033                 ZDOT =        2982
149410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8533542
74                 X    =         2601023
83
 Y    =      -13896689
41  feet           Y    =        -4235710
93  meter
 Z    =      -15153866
35                 Z    =        -4618898
46
 XDOT =      21892
096660                 XDOT =        6672
711062
 YDOT =       2777
721113  feet/sec       YDOT =         846
649395  meter/sec
 ZDOT =       9778
193845                 ZDOT =        2980
393484


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   16237
33320185  
00016717  00000-0  10270-3 0  9157
2 25544  51
6434  77
9776 0003445 254
6141 105
4632 15
54188549 15587


Satellite: ISS
Catalog Number: 25544
Epoch time:      16237
33320185   =   yrday
fracday
Element set:     915
Inclination:       51
6434  deg
RA of node:        77
9776  deg
Eccentricity:     
0003445     
Arg of perigee:   254
6141  deg
Mean anomaly:     105
4632  deg
Mean motion:   15
54188549  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1558
Checksum:              318


Coasting Arc #17 (Orbit 1573)
---------------------------------------

Vector Time (GMT): 2016/238/07:44:17
840
Vector Time (MET): N/A
Weight (LBS)     : 929483
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4183168
28                 A    =         6783935
49  meter
 Y    =       -3989098
34  meter          E    =           
0008807
 Z    =        3543144
70                 I    =           51
99982
 XDOT =       1812
638160                 Wp   =           92
23274
 YDOT =      -5924
744677  meter/sec      RA   =           72
25371  deg
 ZDOT =      -4521
060368                 TA   =           46
22329
                                          MA   =           46
15045
                                          Ha   =            219
820  n
mi
                                          Hp   =            215
849

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13724305
37                 X    =        -4155461
26
 Y    =      -13087592
99  feet           Y    =        -4035722
29  meter
 Z    =       11624490
49                 Z    =         3522891
44
 XDOT =       5946
975589                 XDOT =        1900
716698
 YDOT =     -19438
138705  feet/sec       YDOT =       -5903
982215  meter/sec
 ZDOT =     -14832
875224                 ZDOT =       -4512
040944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13271399
03                 X    =        -4045122
42
 Y    =       13621505
66  feet           Y    =         4151834
92  meter
 Z    =       11536679
71                 Z    =         3516379
98
 XDOT =     -18362
940348                 XDOT =       -5597
024218
 YDOT =      -5336
517671  feet/sec       YDOT =       -1626
570586  meter/sec
 ZDOT =     -14792
365355                 ZDOT =       -4508
712960


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   16238
36199708  
00016717  00000-0  10270-3 0  9167
2 25544  51
6430  72
8500 0003468 257
3657 102
7108 15
54179570 15749


Satellite: ISS
Catalog Number: 25544
Epoch time:      16238
36199708   =   yrday
fracday
Element set:     916
Inclination:       51
6430  deg
RA of node:        72
8500  deg
Eccentricity:     
0003468     
Arg of perigee:   257
3657  deg
Mean anomaly:     102
7108  deg
Mean motion:   15
54179570  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1574
Checksum:              320
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