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

 
Date: November 24th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17545 17 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


329/19:38:37 914 5 2 5 8 5 8
N/A -2 1 -0 4 221 6
000/00:15:15 829 -1 6 0 3 215 1

Coasting Arc #1 (Orbit 1281)
---------------------------------------

Vector Time (GMT): 2015/327/10:18:02
162
Vector Time (MET): N/A
Weight (LBS)     : 906699
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6726414
29                 A    =         6785753
98  meter
 Y    =        -701556
89  meter          E    =           
0017663
 Z    =         417970
73                 I    =           51
72418
 XDOT =        117
410396                 Wp   =          141
54317
 YDOT =      -4777
235278  meter/sec      RA   =            8
74961  deg
 ZDOT =      -6006
458519                 TA   =           33
95007
                                          MA   =           33
83715
                                          Ha   =            220
322  n
mi
                                          Hp   =            212
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22068288
35                 X    =        -6720099
77
 Y    =       -2301695
84  feet           Y    =         -776740
79  meter
 Z    =        1371295
06                 Z    =          385309
72
 XDOT =        385
204710                 XDOT =         199
999667
 YDOT =     -15673
344088  feet/sec       YDOT =       -4775
460528  meter/sec
 ZDOT =     -19706
228738                 ZDOT =       -6005
687548

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19263719
98                 X    =         5871581
85
 Y    =      -11026469
82  feet           Y    =        -3360868
00  meter
 Z    =        1230308
98                 Z    =          374998
18
 XDOT =       7936
611334                 XDOT =        2419
079135
 YDOT =      11617
301856  feet/sec       YDOT =        3540
953606  meter/sec
 ZDOT =     -19701
897891                 ZDOT =       -6005
138477


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   15327
46208239  
00016717  00000-0  10270-3 0  9009
2 25544  51
6441   9
1474 0005687 167
8044 192
3248 15
55340621 12828


Satellite: ISS
Catalog Number: 25544
Epoch time:      15327
46208239   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:         9
1474  deg
Eccentricity:     
0005687     
Arg of perigee:   167
8044  deg
Mean anomaly:     192
3248  deg
Mean motion:   15
55340621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1282
Checksum:              301


Coasting Arc #2 (Orbit 1297)
---------------------------------------

Vector Time (GMT): 2015/328/10:18:02
162
Vector Time (MET): N/A
Weight (LBS)     : 906699
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6339057
78                 A    =         6784517
42  meter
 Y    =        1738514
32  meter          E    =           
0013510
 Z    =        1667040
57                 I    =           51
68847
 XDOT =      -2703
863052                 Wp   =           87
32719
 YDOT =       4344
155789  meter/sec      RA   =            3
77761  deg
 ZDOT =       5711
906010                 TA   =          290
93104
                                          MA   =          291
07558
                                          Ha   =            220
191  n
mi
                                          Hp   =            212
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20797433
67                 X    =         6311048
10
 Y    =        5703787
13  feet           Y    =         1809245
19  meter
 Z    =        5469293
21                 Z    =         1697767
22
 XDOT =      -8870
941773                 XDOT =       -2779
986462
 YDOT =      14252
479623  feet/sec       YDOT =        4313
493648  meter/sec
 ZDOT =      18739
849113                 ZDOT =        5698
586053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20052227
54                 X    =        -6111918
95
 Y    =        7842753
46  feet           Y    =         2390471
25  meter
 Z    =        5601695
45                 Z    =         1707396
77
 XDOT =       -745
362495                 XDOT =        -227
186488
 YDOT =     -15338
945527  feet/sec       YDOT =       -4675
310597  meter/sec
 ZDOT =      18681
380852                 ZDOT =        5694
084884


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   15328
49010004  
00016717  00000-0  10270-3 0  9015
2 25544  51
6439   4
0130 0005577 170
8184 189
3072 15
55359725 12988


Satellite: ISS
Catalog Number: 25544
Epoch time:      15328
49010004   =   yrday
fracday
Element set:     901
Inclination:       51
6439  deg
RA of node:         4
0130  deg
Eccentricity:     
0005577     
Arg of perigee:   170
8184  deg
Mean anomaly:     189
3072  deg
Mean motion:   15
55359725  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1298
Checksum:              297


Coasting Arc #3 (Orbit 1312)
---------------------------------------

Vector Time (GMT): 2015/329/10:18:02
162
Vector Time (MET): N/A
Weight (LBS)     : 906699
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5126037
28                 A    =         6780234
58  meter
 Y    =       -2687706
00  meter          E    =           
0007666
 Z    =       -3531792
96                 I    =           51
64221
 XDOT =       5012
607044                 Wp   =          129
95417
 YDOT =      -3665
387032  meter/sec      RA   =          358
79364  deg
 ZDOT =      -4497
195672                 TA   =           91
67180
                                          MA   =           91
58399
                                          Ha   =            220
003  n
mi
                                          Hp   =            212
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16817707
61                 X    =        -5078445
20
 Y    =       -8817933
07  feet           Y    =        -2744762
47  meter
 Z    =      -11587247
25                 Z    =        -3556579
34
 XDOT =      16445
561169                 XDOT =        5075
067929
 YDOT =     -12025
548004  feet/sec       YDOT =       -3608
983308  meter/sec
 ZDOT =     -14754
578978                 ZDOT =       -4472
693303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18640163
45                 X    =         5681521
82
 Y    =       -3264266
29  feet           Y    =         -994948
37  meter
 Z    =      -11693776
28                 Z    =        -3564263
01
 XDOT =      -5966
461950                 XDOT =       -1818
577602
 YDOT =      18272
116026  feet/sec       YDOT =        5569
340965  meter/sec
 ZDOT =     -14647
934710                 ZDOT =       -4464
690500


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   15329
45384535  
00016717  00000-0  10270-3 0  9026
2 25544  51
6434 359
1991 0005588 173
8334 186
2889 15
55401185 13132


Satellite: ISS
Catalog Number: 25544
Epoch time:      15329
45384535   =   yrday
fracday
Element set:     902
Inclination:       51
6434  deg
RA of node:       359
1991  deg
Eccentricity:     
0005588     
Arg of perigee:   173
8334  deg
Mean anomaly:     186
2889  deg
Mean motion:   15
55401185  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1313
Checksum:              332


Coasting Arc #4 (Orbit 1318)
---------------------------------------

Vector Time (GMT): 2015/329/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          74105
60                 A    =         6776997
74  meter
 Y    =       -4219941
73  meter          E    =           
0013575
 Z    =       -5312176
88                 I    =           51
60787
 XDOT =       7652
692942                 Wp   =          125
33358
 YDOT =       -214
450587  meter/sec      RA   =          356
79392  deg
 ZDOT =        269
927129                 TA   =          147
28522
                                          MA   =          147
20108
                                          Ha   =            221
581  n
mi
                                          Hp   =            215
134

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         243128
60                 X    =          147093
63
 Y    =      -13844953
17  feet           Y    =        -4218704
64  meter
 Z    =      -17428401
85                 Z    =        -5311639
83
 XDOT =      25107
260309                 XDOT =        7653
210978
 YDOT =       -703
578042  feet/sec       YDOT =        -128
870243  meter/sec
 ZDOT =        885
587693                 ZDOT =         307
104470

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         317032
36                 X    =           96631
46
 Y    =      -13847502
68  feet           Y    =        -4220718
82  meter
 Z    =      -17425188
40                 Z    =        -5311197
43
 XDOT =      24089
302310                 XDOT =        7342
419344
 YDOT =       -794
745396  feet/sec       YDOT =        -242
238397  meter/sec
 ZDOT =       1046
267448                 ZDOT =         318
902318


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   15329
83934464  
00016717  00000-0  10270-3 0  9031
2 25544  51
6438 357
2731 0008227 207
5877 152
4840 15
54262749 13195


Satellite: ISS
Catalog Number: 25544
Epoch time:      15329
83934464   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:       357
2731  deg
Eccentricity:     
0008227     
Arg of perigee:   207
5877  deg
Mean anomaly:     152
4840  deg
Mean motion:   15
54262749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1319
Checksum:              330


Coasting Arc #5 (Orbit 1334)
---------------------------------------

Vector Time (GMT): 2015/330/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1908504
82                 A    =         6778505
48  meter
 Y    =        4231695
95  meter          E    =           
0003702
 Z    =        4937193
23                 I    =           51
58110
 XDOT =      -7308
998493                 Wp   =          159
92012
 YDOT =       -718
474008  meter/sec      RA   =          351
79078  deg
 ZDOT =      -2212
444434                 TA   =          311
66593
                                          MA   =          311
69761
                                          Ha   =            221
343  n
mi
                                          Hp   =            215
325

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6261498
74                 X    =        -1979666
28
 Y    =       13883516
89  feet           Y    =         4209955
55  meter
 Z    =       16198140
51                 Z    =         4927749
37
 XDOT =     -23979
653847                 XDOT =       -7289
673703
 YDOT =      -2357
198188  feet/sec       YDOT =        -800
099844  meter/sec
 ZDOT =      -7258
675965                 ZDOT =       -2247
903864

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6087215
16                 X    =        -1855383
18
 Y    =       14009049
49  feet           Y    =         4269958
29  meter
 Z    =       16156438
58                 Z    =         4924482
48
 XDOT =     -22953
376871                 XDOT =       -6996
189270
 YDOT =      -1436
900563  feet/sec       YDOT =        -437
967292  meter/sec
 ZDOT =      -7411
733313                 ZDOT =       -2259
096314


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   15330
86808059  
00016717  00000-0  10270-3 0  9047
2 25544  51
6434 352
1437 0008176 211
9559 148
1099 15
54308825 13359


Satellite: ISS
Catalog Number: 25544
Epoch time:      15330
86808059   =   yrday
fracday
Element set:     904
Inclination:       51
6434  deg
RA of node:       352
1437  deg
Eccentricity:     
0008176     
Arg of perigee:   211
9559  deg
Mean anomaly:     148
1099  deg
Mean motion:   15
54308825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1335
Checksum:              320


Coasting Arc #6 (Orbit 1349)
---------------------------------------

Vector Time (GMT): 2015/331/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3596390
19                 A    =         6781995
00  meter
 Y    =       -4120332
03  meter          E    =           
0008934
 Z    =       -4018758
77                 I    =           51
56213
 XDOT =       6352
680017                 Wp   =          167
31520
 YDOT =       1709
300892  meter/sec      RA   =          346
79132  deg
 ZDOT =       3925
647050                 TA   =          143
57469
                                          MA   =          143
51387
                                          Ha   =            221
160  n
mi
                                          Hp   =            215
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11799180
43                 X    =         3661719
33
 Y    =      -13518149
69  feet           Y    =        -4079749
23  meter
 Z    =      -13184904
11                 Z    =        -4001129
62
 XDOT =      20842
126040                 XDOT =        6314
024485
 YDOT =       5607
942560  feet/sec       YDOT =        1780
124310  meter/sec
 ZDOT =      12879
419456                 ZDOT =        3956
413774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11373403
66                 X    =         3466613
44
 Y    =      -13951072
80  feet           Y    =        -4252286
99  meter
 Z    =      -13107859
59                 Z    =        -3995275
60
 XDOT =      19935
820388                 XDOT =        6076
438054
 YDOT =       4005
549190  feet/sec       YDOT =        1220
891393  meter/sec
 ZDOT =      13011
989866                 ZDOT =        3966
054511


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   15331
83250143  
00016717  00000-0  10270-3 0  9051
2 25544  51
6441 347
3337 0008144 215
1818 144
8798 15
54326632 13503


Satellite: ISS
Catalog Number: 25544
Epoch time:      15331
83250143   =   yrday
fracday
Element set:     905
Inclination:       51
6441  deg
RA of node:       347
3337  deg
Eccentricity:     
0008144     
Arg of perigee:   215
1818  deg
Mean anomaly:     144
8798  deg
Mean motion:   15
54326632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1350
Checksum:              298


Coasting Arc #7 (Orbit 1365)
---------------------------------------

Vector Time (GMT): 2015/332/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4932542
28                 A    =         6785857
86  meter
 Y    =        3826948
29  meter          E    =           
0012562
 Z    =        2638013
93                 I    =           51
54411
 XDOT =      -4918
071121                 Wp   =          138
53868
 YDOT =      -2741
640664  meter/sec      RA   =          341
80164  deg
 ZDOT =      -5213
502639                 TA   =           11
65654
                                          MA   =           11
62748
                                          Ha   =            221
075  n
mi
                                          Hp   =            215
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16182881
48                 X    =        -4987784
14
 Y    =       12555604
61  feet           Y    =         3771480
27  meter
 Z    =        8654901
34                 Z    =         2613918
50
 XDOT =     -16135
403939                 XDOT =       -4861
722448
 YDOT =      -8994
884068  feet/sec       YDOT =       -2796
322324  meter/sec
 ZDOT =     -17104
667450                 ZDOT =       -5237
257216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15532234
14                 X    =        -4734224
97
 Y    =       13419526
13  feet           Y    =         4090271
56  meter
 Z    =        8549982
36                 Z    =         2606034
62
 XDOT =     -15511
875782                 XDOT =       -4728
019738
 YDOT =      -6980
500232  feet/sec       YDOT =       -2127
656471  meter/sec
 ZDOT =     -17206
721916                 ZDOT =       -5244
608840


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   15332
86119652  
00016717  00000-0  10270-3 0  9065
2 25544  51
6440 342
2039 0008136 218
1852 141
8725 15
54331386 13663


Satellite: ISS
Catalog Number: 25544
Epoch time:      15332
86119652   =   yrday
fracday
Element set:     906
Inclination:       51
6440  deg
RA of node:       342
2039  deg
Eccentricity:     
0008136     
Arg of perigee:   218
1852  deg
Mean anomaly:     141
8725  deg
Mean motion:   15
54331386  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1366
Checksum:              302


Coasting Arc #8 (Orbit 1380)
---------------------------------------

Vector Time (GMT): 2015/333/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5837558
42                 A    =         6788176
04  meter
 Y    =       -3327331
51  meter          E    =           
0001920
 Z    =        -957201
90                 I    =           51
52331
 XDOT =       3114
962214                 Wp   =           22
39398
 YDOT =       3768
748032  meter/sec      RA   =          336
81844  deg
 ZDOT =       5901
894055                 TA   =          327
22749
                                          MA   =          327
23939
                                          Ha   =            220
715  n
mi
                                          Hp   =            215
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19152094
54                 X    =         5878981
34
 Y    =      -10916441
95  feet           Y    =        -3261820
40  meter
 Z    =       -3140426
19                 Z    =         -928743
63
 XDOT =      10219
692303                 XDOT =        3043
918305
 YDOT =      12364
658899  feet/sec       YDOT =        3803
183988  meter/sec
 ZDOT =      19363
169472                 ZDOT =        5916
853697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18342643
08                 X    =         5590837
61
 Y    =      -12258885
38  feet           Y    =        -3736508
26  meter
 Z    =       -3016766
62                 Z    =         -919510
46
 XDOT =      10059
566634                 XDOT =        3066
155910
 YDOT =      10275
849542  feet/sec       YDOT =        3132
078940  meter/sec
 ZDOT =      19427
008611                 ZDOT =        5921
352225


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   15333
82557634  
00016717  00000-0  10270-3 0  9079
2 25544  51
6447 337
3938 0008139 222
7716 137
2804 15
54399864 13815


Satellite: ISS
Catalog Number: 25544
Epoch time:      15333
82557634   =   yrday
fracday
Element set:     907
Inclination:       51
6447  deg
RA of node:       337
3938  deg
Eccentricity:     
0008139     
Arg of perigee:   222
7716  deg
Mean anomaly:     137
2804  deg
Mean motion:   15
54399864  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1381
Checksum:              338


Coasting Arc #9 (Orbit 1396)
---------------------------------------

Vector Time (GMT): 2015/334/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6219222
49                 A    =         6788263
92  meter
 Y    =        2559714
59  meter          E    =           
0013531
 Z    =        -852908
31                 I    =           51
49468
 XDOT =      -1139
605556                 Wp   =          177
94198
 YDOT =      -4738
254031  meter/sec      RA   =          331
83811  deg
 ZDOT =      -5926
665817                 TA   =           11
30968
                                          MA   =           11
27930
                                          Ha   =            220
575  n
mi
                                          Hp   =            215
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20404273
26                 X    =        -6243240
49
 Y    =        8398013
75  feet           Y    =         2490032
89  meter
 Z    =       -2798255
59                 Z    =         -883178
40
 XDOT =      -3738
863373                 XDOT =       -1057
746924
 YDOT =     -15545
452857  feet/sec       YDOT =       -4750
539868  meter/sec
 ZDOT =     -19444
441657                 ZDOT =       -5932
003220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19561637
50                 X    =        -5962387
11
 Y    =       10171094
29  feet           Y    =         3100149
54  meter
 Z    =       -2929576
09                 Z    =         -892934
79
 XDOT =      -4236
076396                 XDOT =       -1291
156085
 YDOT =     -13739
408859  feet/sec       YDOT =       -4187
771820  meter/sec
 ZDOT =     -19466
506788                 ZDOT =       -5933
391269


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   15334
85422888  
00016717  00000-0  10270-3 0  9086
2 25544  51
6448 332
2639 0008262 226
1154 133
9317 15
54379719 13975


Satellite: ISS
Catalog Number: 25544
Epoch time:      15334
85422888   =   yrday
fracday
Element set:     908
Inclination:       51
6448  deg
RA of node:       332
2639  deg
Eccentricity:     
0008262     
Arg of perigee:   226
1154  deg
Mean anomaly:     133
9317  deg
Mean motion:   15
54379719  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1397
Checksum:              335


Coasting Arc #10 (Orbit 1412)
---------------------------------------

Vector Time (GMT): 2015/335/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6090656
90                 A    =         6785565
03  meter
 Y    =       -1542079
54  meter          E    =           
0007298
 Z    =        2560036
07                 I    =           51
45841
 XDOT =       -813
463022                 Wp   =          105
11352
 YDOT =       5526
347884  meter/sec      RA   =          326
85093  deg
 ZDOT =       5249
820049                 TA   =          283
73127
                                          MA   =          283
81250
                                          Ha   =            220
264  n
mi
                                          Hp   =            216
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19982470
15                 X    =         6095012
41
 Y    =       -5059316
07  feet           Y    =        -1473945
52  meter
 Z    =        8399068
49                 Z    =         2589633
93
 XDOT =      -2668
841935                 XDOT =        -900
701277
 YDOT =      18131
062610  feet/sec       YDOT =        5516
763251  meter/sec
 ZDOT =      17223
819060                 ZDOT =        5245
656681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19281766
80                 X    =         5877082
52
 Y    =       -7137181
33  feet           Y    =        -2175412
87  meter
 Z    =        8527265
44                 Z    =         2599110
51
 XDOT =      -1366
727922                 XDOT =        -416
578671
 YDOT =      16918
824518  feet/sec       YDOT =        5156
857713  meter/sec
 ZDOT =      17204
677611                 ZDOT =        5243
985736


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   15335
88285853  
00016717  00000-0  10270-3 0  9090
2 25544  51
6446 327
1330 0008025 231
1638 128
8799 15
54438688 14131


Satellite: ISS
Catalog Number: 25544
Epoch time:      15335
88285853   =   yrday
fracday
Element set:     909
Inclination:       51
6446  deg
RA of node:       327
1330  deg
Eccentricity:     
0008025     
Arg of perigee:   231
1638  deg
Mean anomaly:     128
8799  deg
Mean motion:   15
54438688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1413
Checksum:              335


Coasting Arc #11 (Orbit 1427)
---------------------------------------

Vector Time (GMT): 2015/336/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5478873
88                 A    =         6781472
10  meter
 Y    =         259982
75  meter          E    =           
0002551
 Z    =       -3985871
25                 I    =           51
41849
 XDOT =       2586
620753                 Wp   =          180
25320
 YDOT =      -6040
602043  meter/sec      RA   =          321
85256  deg
 ZDOT =      -3951
997591                 TA   =           48
51112
                                          MA   =           48
48923
                                          Ha   =            219
948  n
mi
                                          Hp   =            216
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17975308
01                 X    =        -5462011
92
 Y    =         852961
78  feet           Y    =          198808
73  meter
 Z    =      -13077005
42                 Z    =        -4012445
71
 XDOT =       8486
288561                 XDOT =        2673
173406
 YDOT =     -19818
248171  feet/sec       YDOT =       -6011
192708  meter/sec
 ZDOT =     -12965
871362                 ZDOT =       -3939
222142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17651179
19                 X    =        -5380079
42
 Y    =        3042663
18  feet           Y    =          927403
74  meter
 Z    =      -13191868
20                 Z    =        -4020881
43
 XDOT =       6291
886327                 XDOT =        1917
766953
 YDOT =     -19434
718315  feet/sec       YDOT =       -5923
702143  meter/sec
 ZDOT =     -12909
424465                 ZDOT =       -3934
792577


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   15336
84717825  
00016717  00000-0  10270-3 0  9108
2 25544  51
6442 322
3234 0008215 235
0416 124
9966 15
54470891 14286


Satellite: ISS
Catalog Number: 25544
Epoch time:      15336
84717825   =   yrday
fracday
Element set:     910
Inclination:       51
6442  deg
RA of node:       322
3234  deg
Eccentricity:     
0008215     
Arg of perigee:   235
0416  deg
Mean anomaly:     124
9966  deg
Mean motion:   15
54470891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1428
Checksum:              308


Coasting Arc #12 (Orbit 1443)
---------------------------------------

Vector Time (GMT): 2015/337/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4500461
71                 A    =         6777826
10  meter
 Y    =        1181022
90  meter          E    =           
0007787
 Z    =        4932331
23                 I    =           51
38192
 XDOT =      -4014
651942                 Wp   =          190
64277
 YDOT =       6154
706643  meter/sec      RA   =          316
84007  deg
 ZDOT =       2182
460422                 TA   =          237
94912
                                          MA   =          238
02478
                                          Ha   =            219
795  n
mi
                                          Hp   =            216
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14765294
33                 X    =         4462961
17
 Y    =        3874747
04  feet           Y    =         1231140
27  meter
 Z    =       16182189
06                 Z    =         4954102
67
 XDOT =     -13171
430255                 XDOT =       -4093
778641
 YDOT =      20192
607096  feet/sec       YDOT =        6109
369692  meter/sec
 ZDOT =       7160
303221                 ZDOT =        2162
765813

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15059470
90                 X    =         4590126
73
 Y    =        1787446
67  feet           Y    =          544813
75  meter
 Z    =       16276000
58                 Z    =         4960924
98
 XDOT =     -10132
239692                 XDOT =       -3088
306658
 YDOT =      20745
300881  feet/sec       YDOT =        6323
167709  meter/sec
 ZDOT =       7073
950980                 ZDOT =        2156
140259


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   15337
87576647  
00016717  00000-0  10270-3 0  9118
2 25544  51
6442 317
1926 0008007 238
1837 121
8537 15
54496031 14448


Satellite: ISS
Catalog Number: 25544
Epoch time:      15337
87576647   =   yrday
fracday
Element set:     911
Inclination:       51
6442  deg
RA of node:       317
1926  deg
Eccentricity:     
0008007     
Arg of perigee:   238
1837  deg
Mean anomaly:     121
8537  deg
Mean motion:   15
54496031  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1444
Checksum:              320


Coasting Arc #13 (Orbit 1458)
---------------------------------------

Vector Time (GMT): 2015/338/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3254218
05                 A    =         6776081
84  meter
 Y    =       -2712770
28  meter          E    =           
0008508
 Z    =       -5294953
24                 I    =           51
35282
 XDOT =       5029
444739                 Wp   =          114
64106
 YDOT =      -5781
152838  meter/sec      RA   =          311
81656  deg
 ZDOT =       -132
823308                 TA   =          154
10870
                                          MA   =          154
06610
                                          Ha   =            219
502  n
mi
                                          Hp   =            216
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10676568
41                 X    =        -3197920
20
 Y    =       -8900164
96  feet           Y    =        -2748846
22  meter
 Z    =      -17371893
83                 Z    =        -5310625
04
 XDOT =      16500
802948                 XDOT =        5094
362416
 YDOT =     -18967
036869  feet/sec       YDOT =       -5724
547287  meter/sec
 ZDOT =       -435
772007                 ZDOT =        -108
233448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11830877
22                 X    =        -3606051
38
 Y    =       -7134073
24  feet           Y    =        -2174465
52  meter
 Z    =      -17439039
19                 Z    =        -5315419
14
 XDOT =      12803
043897                 XDOT =        3902
367780
 YDOT =     -20458
572698  feet/sec       YDOT =       -6235
772958  meter/sec
 ZDOT =       -328
359540                 ZDOT =        -100
083988


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   15338
84004561  
00016717  00000-0  10270-3 0  9128
2 25544  51
6430 312
3815 0008105 242
1854 117
8478 15
54565527 14594


Satellite: ISS
Catalog Number: 25544
Epoch time:      15338
84004561   =   yrday
fracday
Element set:     912
Inclination:       51
6430  deg
RA of node:       312
3815  deg
Eccentricity:     
0008105     
Arg of perigee:   242
1854  deg
Mean anomaly:     117
8478  deg
Mean motion:   15
54565527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1459
Checksum:              306


Coasting Arc #14 (Orbit 1474)
---------------------------------------

Vector Time (GMT): 2015/339/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1897459
99                 A    =         6777278
17  meter
 Y    =        4154724
47  meter          E    =           
0002625
 Z    =        5009172
67                 I    =           51
33672
 XDOT =      -5585
438264                 Wp   =          267
12322
 YDOT =       4882
943073  meter/sec      RA   =          306
79222  deg
 ZDOT =      -1935
287672                 TA   =          201
73145
                                          MA   =          201
74259
                                          Ha   =            219
295  n
mi
                                          Hp   =            216
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6225262
42                 X    =         1826526
86
 Y    =       13630985
81  feet           Y    =         4175546
41  meter
 Z    =       16434293
53                 Z    =         5018218
06
 XDOT =     -18324
928687                 XDOT =       -5630
224398
 YDOT =      16020
154439  feet/sec       YDOT =        4820
232642  meter/sec
 ZDOT =      -6349
369001                 ZDOT =       -1962
529626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8396749
32                 X    =         2559329
19
 Y    =       12361000
25  feet           Y    =         3767632
88  meter
 Z    =       16472520
87                 Z    =         5020824
36
 XDOT =     -14319
129815                 XDOT =       -4364
470768
 YDOT =      18341
943431  feet/sec       YDOT =        5590
624358  meter/sec
 ZDOT =      -6468
045220                 ZDOT =       -1971
460183


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   15339
86858953  
00016717  00000-0  10270-3 0  9134
2 25544  51
6432 307
2508 0008189 245
8776 114
1521 15
54594262 14758


Satellite: ISS
Catalog Number: 25544
Epoch time:      15339
86858953   =   yrday
fracday
Element set:     913
Inclination:       51
6432  deg
RA of node:       307
2508  deg
Eccentricity:     
0008189     
Arg of perigee:   245
8776  deg
Mean anomaly:     114
1521  deg
Mean motion:   15
54594262  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1475
Checksum:              336


Coasting Arc #15 (Orbit 1489)
---------------------------------------

Vector Time (GMT): 2015/340/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -534749
54                 A    =         6780750
57  meter
 Y    =       -5374021
41  meter          E    =           
0005382
 Z    =       -4103608
23                 I    =           51
32877
 XDOT =       5700
711952                 Wp   =          186
00196
 YDOT =      -3458
328257  meter/sec      RA   =          301
77162  deg
 ZDOT =       3780
394480                 TA   =          123
20114
                                          MA   =          123
14953
                                          Ha   =            219
153  n
mi
                                          Hp   =            216
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1754427
61                 X    =         -454682
12
 Y    =      -17631303
85  feet           Y    =        -5379553
53  meter
 Z    =      -13463281
59                 Z    =        -4106011
66
 XDOT =      18703
123202                 XDOT =        5720
596153
 YDOT =     -11346
221316  feet/sec       YDOT =       -3394
468067  meter/sec
 ZDOT =      12402
869028                 ZDOT =        3808
135988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5001212
74                 X    =        -1524369
64
 Y    =      -16990540
89  feet           Y    =        -5178716
86  meter
 Z    =      -13472573
41                 Z    =        -4106440
38
 XDOT =      14878
171931                 XDOT =        4534
866805
 YDOT =     -14324
646970  feet/sec       YDOT =       -4366
152397  meter/sec
 ZDOT =      12523
406655                 ZDOT =        3817
134348


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   15340
83282993  
00016717  00000-0  10270-3 0  9149
2 25544  51
6418 302
4388 0008171 249
0176 111
0103 15
54620242 14903


Satellite: ISS
Catalog Number: 25544
Epoch time:      15340
83282993   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:       302
4388  deg
Eccentricity:     
0008171     
Arg of perigee:   249
0176  deg
Mean anomaly:     111
0103  deg
Mean motion:   15
54620242  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1490
Checksum:              286


Coasting Arc #16 (Orbit 1505)
---------------------------------------

Vector Time (GMT): 2015/341/19:46:15
829
Vector Time (MET): N/A
Weight (LBS)     : 906045
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -718366
51                 A    =         6784669
49  meter
 Y    =        6186432
25  meter          E    =           
0007399
 Z    =        2679247
36                 I    =           51
32701
 XDOT =      -5439
294259                 Wp   =          133
33578
 YDOT =       1606
571715  meter/sec      RA   =          296
76363  deg
 ZDOT =      -5163
983964                 TA   =           16
25531
                                          MA   =           16
23158
                                          Ha   =            218
770  n
mi
                                          Hp   =            217
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2356845
50                 X    =         -800506
28
 Y    =       20296693
73  feet           Y    =         6177939
61  meter
 Z    =        8790181
61                 Z    =         2675558
38
 XDOT =     -17845
453605                 XDOT =       -5431
770017
 YDOT =       5270
904578  feet/sec       YDOT =        1545
788233  meter/sec
 ZDOT =     -16942
204606                 ZDOT =       -5190
389033

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1853684
11                 X    =          565002
92
 Y    =       20356231
67  feet           Y    =         6204579
41  meter
 Z    =        8772997
04                 Z    =         2674009
50
 XDOT =     -14771
735883                 XDOT =       -4502
425097
 YDOT =       8701
778137  feet/sec       YDOT =        2652
301976  meter/sec
 ZDOT =     -17056
590978                 ZDOT =       -5198
848930


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   15341
86132993  
00016717  00000-0  10270-3 0  9158
2 25544  51
6423 297
3078 0008209 254
0474 105
9775 15
54687696 15067


Satellite: ISS
Catalog Number: 25544
Epoch time:      15341
86132993   =   yrday
fracday
Element set:     915
Inclination:       51
6423  deg
RA of node:       297
3078  deg
Eccentricity:     
0008209     
Arg of perigee:   254
0474  deg
Mean anomaly:     105
9775  deg
Mean motion:   15
54687696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1506
Checksum:              339
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