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

 
Date: November 16th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14531 28 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


329/19:52:48 707 4 7 5 2 5 2
N/A 0 7 -0 6 220 0
000/00:13:37 414 2 1 -0 1 215 5

Coasting Arc #1 (Orbit 1173)
---------------------------------------

Vector Time (GMT): 2015/320/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4188723
60                 A    =         6775454
51  meter
 Y    =        1538153
30  meter          E    =           
0007992
 Z    =        5091390
61                 I    =           51
88329
 XDOT =      -4378
382256                 Wp   =          103
46474
 YDOT =      -6050
428818  meter/sec      RA   =           43
36988  deg
 ZDOT =      -1773
725126                 TA   =            3
61761
                                          MA   =            3
61184
                                          Ha   =            221
275  n
mi
                                          Hp   =            211
648

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13742531
51                 X    =        -4230344
73
 Y    =        5046434
70  feet           Y    =         1491079
35  meter
 Z    =       16704037
44                 Z    =         5070941
25
 XDOT =     -14364
771182                 XDOT =       -4301
783249
 YDOT =     -19850
488248  feet/sec       YDOT =       -6098
962433  meter/sec
 ZDOT =      -5819
308156                 ZDOT =       -1794
808905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5938377
72                 X    =         1810017
53
 Y    =      -13491289
53  feet           Y    =        -4112145
05  meter
 Z    =       16615333
86                 Z    =         5064353
76
 XDOT =      23261
345570                 XDOT =        7090
058130
 YDOT =       2959
167365  feet/sec       YDOT =         901
954213  meter/sec
 ZDOT =      -5909
209345                 ZDOT =       -1801
127008


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   15320
52244061  
00016717  00000-0  10270-3 0  9002
2 25544  51
6446  43
7957 0005986 146
5526 213
6006 15
55145108 11746


Satellite: ISS
Catalog Number: 25544
Epoch time:      15320
52244061   =   yrday
fracday
Element set:     900
Inclination:       51
6446  deg
RA of node:        43
7957  deg
Eccentricity:     
0005986     
Arg of perigee:   146
5526  deg
Mean anomaly:     213
6006  deg
Mean motion:   15
55145108  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1174
Checksum:              292


Coasting Arc #2 (Orbit 1188)
---------------------------------------

Vector Time (GMT): 2015/321/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5380762
99                 A    =         6779187
32  meter
 Y    =         120935
05  meter          E    =           
0012601
 Z    =       -4135932
05                 I    =           51
87173
 XDOT =       2792
787737                 Wp   =          126
73427
 YDOT =       6027
587375  meter/sec      RA   =           38
38410  deg
 ZDOT =       3810
297786                 TA   =          182
49677
                                          MA   =          182
50307
                                          Ha   =            221
062  n
mi
                                          Hp   =            211
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17653421
89                 X    =         5399101
81
 Y    =         396768
54  feet           Y    =          181208
92  meter
 Z    =      -13569330
87                 Z    =        -4109748
48
 XDOT =       9162
689427                 XDOT =        2706
668993
 YDOT =      19775
549132  feet/sec       YDOT =        6058
336568  meter/sec
 ZDOT =      12500
976989                 ZDOT =        3823
655728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12343057
77                 X    =        -3762164
01
 Y    =       12747847
35  feet           Y    =         3885543
87  meter
 Z    =      -13456180
10                 Z    =        -4101443
70
 XDOT =     -19752
414372                 XDOT =       -6020
535901
 YDOT =      -5872
380243  feet/sec       YDOT =       -1789
901498  meter/sec
 ZDOT =      12557
482016                 ZDOT =        3827
520519


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   15321
48634777  
00016717  00000-0  10270-3 0  9016
2 25544  51
6442  38
9839 0006027 149
6967 210
4535 15
55167294 11895


Satellite: ISS
Catalog Number: 25544
Epoch time:      15321
48634777   =   yrday
fracday
Element set:     901
Inclination:       51
6442  deg
RA of node:        38
9839  deg
Eccentricity:     
0006027     
Arg of perigee:   149
6967  deg
Mean anomaly:     210
4535  deg
Mean motion:   15
55167294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1189
Checksum:              335


Coasting Arc #3 (Orbit 1204)
---------------------------------------

Vector Time (GMT): 2015/322/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6069465
16                 A    =         6783650
14  meter
 Y    =       -1623013
82  meter          E    =           
0018293
 Z    =        2530796
03                 I    =           51
86078
 XDOT =       -754
148968                 Wp   =          118
14716
 YDOT =      -5492
677680  meter/sec      RA   =           33
41002  deg
 ZDOT =      -5310
410113                 TA   =           33
48936
                                          MA   =           33
37383
                                          Ha   =            221
069  n
mi
                                          Hp   =            211
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19912943
45                 X    =        -6063158
92
 Y    =       -5324848
50  feet           Y    =        -1690851
35  meter
 Z    =        8303136
59                 Z    =         2501326
74
 XDOT =      -2474
242020                 XDOT =        -666
876199
 YDOT =     -18020
596064  feet/sec       YDOT =       -5500
623052  meter/sec
 ZDOT =     -17422
605358                 ZDOT =       -5313
861733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17279282
91                 X    =         5266725
43
 Y    =      -11331339
91  feet           Y    =        -3453792
40  meter
 Z    =        8176094
65                 Z    =         2492073
65
 XDOT =      14181
379568                 XDOT =        4322
484492
 YDOT =       8994
375832  feet/sec       YDOT =        2741
485754  meter/sec
 ZDOT =     -17436
396312                 ZDOT =       -5314
613596


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   15322
51449534  
00016717  00000-0  10270-3 0  9027
2 25544  51
6439  33
8504 0005957 152
0220 208
1255 15
55176251 12050


Satellite: ISS
Catalog Number: 25544
Epoch time:      15322
51449534   =   yrday
fracday
Element set:     902
Inclination:       51
6439  deg
RA of node:        33
8504  deg
Eccentricity:     
0005957     
Arg of perigee:   152
0220  deg
Mean anomaly:     208
1255  deg
Mean motion:   15
55176251  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1205
Checksum:              281


Coasting Arc #4 (Orbit 1219)
---------------------------------------

Vector Time (GMT): 2015/323/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6145980
12                 A    =         6786164
90  meter
 Y    =        2815949
55  meter          E    =           
0010106
 Z    =        -574687
24                 I    =           51
84231
 XDOT =      -1523
600975                 Wp   =           72
01425
 YDOT =       4530
182378  meter/sec      RA   =           28
44601  deg
 ZDOT =       5993
140657                 TA   =          281
80178
                                          MA   =          281
91511
                                          Ha   =            220
864  n
mi
                                          Hp   =            211
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20163976
76                 X    =         6116826
34
 Y    =        9238679
62  feet           Y    =         2884514
94  meter
 Z    =       -1885456
84                 Z    =         -544901
77
 XDOT =      -4998
690862                 XDOT =       -1603
258093
 YDOT =      14862
803078  feet/sec       YDOT =        4512
699109  meter/sec
 ZDOT =      19662
534964                 ZDOT =        5985
545713

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20181077
57                 X    =        -6151192
44
 Y    =        9226598
19  feet           Y    =         2812267
13  meter
 Z    =       -1757299
52                 Z    =         -535624
89
 XDOT =      -7224
799000                 XDOT =       -2202
118735
 YDOT =     -12124
106934  feet/sec       YDOT =       -3695
427793  meter/sec
 ZDOT =      19628
775324                 ZDOT =        5982
850719


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   15323
47836403  
00016717  00000-0  10270-3 0  9039
2 25544  51
6441  29
0376 0005712 155
0895 205
0535 15
55173447 12205


Satellite: ISS
Catalog Number: 25544
Epoch time:      15323
47836403   =   yrday
fracday
Element set:     903
Inclination:       51
6441  deg
RA of node:        29
0376  deg
Eccentricity:     
0005712     
Arg of perigee:   155
0895  deg
Mean anomaly:     205
0535  deg
Mean motion:   15
55173447  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1220
Checksum:              288


Coasting Arc #5 (Orbit 1235)
---------------------------------------

Vector Time (GMT): 2015/324/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5483263
89                 A    =         6785099
76  meter
 Y    =       -3685006
84  meter          E    =           
0013820
 Z    =       -1518889
07                 I    =           51
81028
 XDOT =       3811
180037                 Wp   =          148
49783
 YDOT =      -3302
575224  meter/sec      RA   =           23
48342  deg
 ZDOT =      -5781
272285                 TA   =           48
06580
                                          MA   =           47
94807
                                          Ha   =            220
698  n
mi
                                          Hp   =            211
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17989710
93                 X    =        -5434271
42
 Y    =      -12089917
45  feet           Y    =        -3746050
41  meter
 Z    =       -4983231
86                 Z    =        -1545406
99
 XDOT =      12503
871511                 XDOT =        3875
910604
 YDOT =     -10835
220550  feet/sec       YDOT =       -3259
594260  meter/sec
 ZDOT =     -18967
428758                 ZDOT =       -5762
600790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20787998
60                 X    =         6336181
97
 Y    =       -6042127
12  feet           Y    =        -1841640
35  meter
 Z    =       -5097079
29                 Z    =        -1553589
77
 XDOT =       -208
179763                 XDOT =         -63
453192
 YDOT =      15120
679586  feet/sec       YDOT =        4608
783138  meter/sec
 ZDOT =     -18886
049555                 ZDOT =       -5756
467904


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   15324
50647249  
00016717  00000-0  10270-3 0  9043
2 25544  51
6435  23
9038 0005825 158
2610 201
8792 15
55230911 12367


Satellite: ISS
Catalog Number: 25544
Epoch time:      15324
50647249   =   yrday
fracday
Element set:     904
Inclination:       51
6435  deg
RA of node:        23
9038  deg
Eccentricity:     
0005825     
Arg of perigee:   158
2610  deg
Mean anomaly:     201
8792  deg
Mean motion:   15
55230911  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1236
Checksum:              294


Coasting Arc #6 (Orbit 1251)
---------------------------------------

Vector Time (GMT): 2015/325/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4165497
26                 A    =         6781176
56  meter
 Y    =        4172323
64  meter          E    =           
0015266
 Z    =        3343481
64                 I    =           51
76847
 XDOT =      -5747
511850                 Wp   =          109
92614
 YDOT =       1966
905298  meter/sec      RA   =           18
51022  deg
 ZDOT =       4683
639366                 TA   =          288
97610
                                          MA   =          289
14146
                                          Ha   =            220
536  n
mi
                                          Hp   =            211
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13666329
60                 X    =         4102290
08
 Y    =       13688725
85  feet           Y    =         4218551
64  meter
 Z    =       10969427
97                 Z    =         3363563
54
 XDOT =     -18856
666176                 XDOT =       -5791
830833
 YDOT =       6453
101370  feet/sec       YDOT =        1902
385120  meter/sec
 ZDOT =      15366
270887                 ZDOT =        4655
610926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19190141
67                 X    =        -5849155
18
 Y    =        1998954
68  feet           Y    =          609281
39  meter
 Z    =       11055350
41                 Z    =         3369670
81
 XDOT =       7010
933537                 XDOT =        2136
932542
 YDOT =     -17410
370460  feet/sec       YDOT =       -5306
680916  meter/sec
 ZDOT =      15244
733563                 ZDOT =        4646
594790


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   15325
53455950  
00016717  00000-0  10270-3 0  9054
2 25544  51
6439  18
7700 0005753 161
9587 198
1772 15
55276400 12520


Satellite: ISS
Catalog Number: 25544
Epoch time:      15325
53455950   =   yrday
fracday
Element set:     905
Inclination:       51
6439  deg
RA of node:        18
7700  deg
Eccentricity:     
0005753     
Arg of perigee:   161
9587  deg
Mean anomaly:     198
1772  deg
Mean motion:   15
55276400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1252
Checksum:              318


Coasting Arc #7 (Orbit 1266)
---------------------------------------

Vector Time (GMT): 2015/326/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2244089
07                 A    =         6776588
24  meter
 Y    =       -4350462
71  meter          E    =           
0011910
 Z    =       -4695440
49                 I    =           51
72219
 XDOT =       7090
799515                 Wp   =           98
75723
 YDOT =       -600
446939  meter/sec      RA   =           13
51976  deg
 ZDOT =      -2840
492141                 TA   =          143
10383
                                          MA   =          143
02183
                                          Ha   =            220
479  n
mi
                                          Hp   =            211
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7362496
94                 X    =        -2172465
20
 Y    =      -14273171
61  feet           Y    =        -4375157
19  meter
 Z    =      -15404988
50                 Z    =        -4706168
03
 XDOT =      23263
777935                 XDOT =        7110
785173
 YDOT =      -1969
970271  feet/sec       YDOT =        -521
041231  meter/sec
 ZDOT =      -9319
199937                 ZDOT =       -2805
997175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15727478
16                 X    =         4793735
34
 Y    =        3028823
54  feet           Y    =          923185
42  meter
 Z    =      -15450440
72                 Z    =        -4709294
33
 XDOT =     -12540
795724                 XDOT =       -3822
434537
 YDOT =      18474
107147  feet/sec       YDOT =        5630
907858  meter/sec
 ZDOT =      -9170
008833                 ZDOT =       -2795
018692


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   15326
49837522  
00016717  00000-0  10270-3 0  9060
2 25544  51
6435  13
9567 0005687 164
5803 195
5524 15
55277468 12677


Satellite: ISS
Catalog Number: 25544
Epoch time:      15326
49837522   =   yrday
fracday
Element set:     906
Inclination:       51
6435  deg
RA of node:        13
9567  deg
Eccentricity:     
0005687     
Arg of perigee:   164
5803  deg
Mean anomaly:     195
5524  deg
Mean motion:   15
55277468  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1267
Checksum:              341


Coasting Arc #8 (Orbit 1282)
---------------------------------------

Vector Time (GMT): 2015/327/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          21592
58                 A    =         6773918
32  meter
 Y    =        4229180
28  meter          E    =           
0007527
 Z    =        5288688
81                 I    =           51
68259
 XDOT =      -7621
416147                 Wp   =          149
44059
 YDOT =       -684
311737  meter/sec      RA   =            8
51511  deg
 ZDOT =        571
640774                 TA   =          295
07193
                                          MA   =          295
15003
                                          Ha   =            220
295  n
mi
                                          Hp   =            212
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          70841
81                 X    =          -51391
80
 Y    =       13875263
37  feet           Y    =         4229013
65  meter
 Z    =       17351341
23                 Z    =         5288616
43
 XDOT =     -25004
646151                 XDOT =       -7615
974440
 YDOT =      -2245
117246  feet/sec       YDOT =        -769
509017  meter/sec
 ZDOT =       1875
461858                 ZDOT =         534
629790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11075231
00                 X    =        -3375730
41
 Y    =       -8361146
31  feet           Y    =        -2548477
40  meter
 Z    =       17350143
67                 Z    =         5288323
79
 XDOT =      16200
809820                 XDOT =        4938
006833
 YDOT =     -17853
927572  feet/sec       YDOT =       -5441
877124  meter/sec
 ZDOT =       1715
675799                 ZDOT =         522
937983


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
52642434  
00016717  00000-0  10270-3 0  9072
2 25544  51
6437   8
8231 0005593 167
8889 192
2400 15
55337268 12836


Satellite: ISS
Catalog Number: 25544
Epoch time:      15327
52642434   =   yrday
fracday
Element set:     907
Inclination:       51
6437  deg
RA of node:         8
8231  deg
Eccentricity:     
0005593     
Arg of perigee:   167
8889  deg
Mean anomaly:     192
2400  deg
Mean motion:   15
55337268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1283
Checksum:              322


Coasting Arc #9 (Orbit 1297)
---------------------------------------

Vector Time (GMT): 2015/328/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2287303
31                 A    =         6774992
70  meter
 Y    =       -3881378
24  meter          E    =           
0016090
 Z    =       -5074159
70                 I    =           51
65423
 XDOT =       7201
820342                 Wp   =          121
53289
 YDOT =       1874
381293  meter/sec      RA   =            3
50392  deg
 ZDOT =       1808
639580                 TA   =          166
01448
                                          MA   =          165
96987
                                          Ha   =            220
225  n
mi
                                          Hp   =            212
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7504275
97                 X    =         2355184
79
 Y    =      -12734180
59  feet           Y    =        -3855420
44  meter
 Z    =      -16647505
59                 Z    =        -5062883
37
 XDOT =      23628
019494                 XDOT =        7171
539390
 YDOT =       6149
544925  feet/sec       YDOT =        1954
747448  meter/sec
 ZDOT =       5933
856890                 ZDOT =        1843
551949

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5853999
23                 X    =         1784298
97
 Y    =       13632725
51  feet           Y    =         4155254
73  meter
 Z    =      -16597965
04                 Z    =        -5059059
75
 XDOT =     -17819
802319                 XDOT =       -5431
475747
 YDOT =      15075
652057  feet/sec       YDOT =        4595
058747  meter/sec
 ZDOT =       6084
316335                 ZDOT =        1854
499619


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
49020463  
00016717  00000-0  10270-3 0  9082
2 25544  51
6436   4
0093 0005466 170
1945 189
9316 15
55333931 12986


Satellite: ISS
Catalog Number: 25544
Epoch time:      15328
49020463   =   yrday
fracday
Element set:     908
Inclination:       51
6436  deg
RA of node:         4
0093  deg
Eccentricity:     
0005466     
Arg of perigee:   170
1945  deg
Mean anomaly:     189
9316  deg
Mean motion:   15
55333931  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1298
Checksum:              312


Coasting Arc #10 (Orbit 1313)
---------------------------------------

Vector Time (GMT): 2015/329/11:27:21
181
Vector Time (MET): N/A
Weight (LBS)     : 907028
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4320598
62                 A    =         6778795
16  meter
 Y    =        3305959
94  meter          E    =           
0011743
 Z    =        4032044
16                 I    =           51
63512
 XDOT =      -5911
092989                 Wp   =          105
53429
 YDOT =      -2944
289613  meter/sec      RA   =          358
50013  deg
 ZDOT =      -3913
631617                 TA   =           25
05323
                                          MA   =           24
99629
                                          Ha   =            220
112  n
mi
                                          Hp   =            212
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14175192
33                 X    =        -4376832
15
 Y    =       10846325
28  feet           Y    =         3257329
55  meter
 Z    =       13228491
32                 Z    =         4010918
62
 XDOT =     -19393
349703                 XDOT =       -5858
718513
 YDOT =      -9659
742825  feet/sec       YDOT =       -3010
098330  meter/sec
 ZDOT =     -12839
998742                 ZDOT =       -3942
220125

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -733856
29                 X    =         -223679
40
 Y    =      -17901544
51  feet           Y    =        -5456390
77  meter
 Z    =       13136513
68                 Z    =         4004009
37
 XDOT =      17669
102196                 XDOT =        5385
542349
 YDOT =     -10252
291412  feet/sec       YDOT =       -3124
898422  meter/sec
 ZDOT =     -12962
901426                 ZDOT =       -3951
092355


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
51821646  
00016717  00000-0  10270-3 0  9099
2 25544  51
6430 358
8750 0005405 173
2983 186
8243 15
55406244 13141


Satellite: ISS
Catalog Number: 25544
Epoch time:      15329
51821646   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:       358
8750  deg
Eccentricity:     
0005405     
Arg of perigee:   173
2983  deg
Mean anomaly:     186
8243  deg
Mean motion:   15
55406244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1314
Checksum:              314


Coasting Arc #11 (Orbit 1318)
---------------------------------------

Vector Time (GMT): 2015/329/19:59:37
414
Vector Time (MET): N/A
Weight (LBS)     : 906444
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5323639
29                 A    =         6784544
78  meter
 Y    =       -2797621
24  meter          E    =           
0002359
 Z    =       -3143838
33                 I    =           51
63432
 XDOT =       4740
027544                 Wp   =          152
10030
 YDOT =       3572
067478  meter/sec      RA   =          356
72280  deg
 ZDOT =       4847
300703                 TA   =          171
68152
                                          MA   =          171
67761
                                          Ha   =            220
049  n
mi
                                          Hp   =            215
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17466008
16                 X    =         5369799
22
 Y    =       -9178547
36  feet           Y    =        -2737830
52  meter
 Z    =      -10314430
22                 Z    =        -3117864
60
 XDOT =      15551
271471                 XDOT =        4676
184648
 YDOT =      11719
381490  feet/sec       YDOT =        3624
716366  meter/sec
 ZDOT =      15903
217531                 ZDOT =        4870
172452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16937716
20                 X    =         5162615
90
 Y    =      -10234037
64  feet           Y    =        -3119334
67  meter
 Z    =      -10201611
97                 Z    =        -3109451
33
 XDOT =      15390
527628                 XDOT =        4691
032821
 YDOT =       9519
447221  feet/sec       YDOT =        2901
527513  meter/sec
 ZDOT =      16001
284851                 ZDOT =        4877
191623


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
83946755  
00016717  00000-0  10270-3 0  9105
2 25544  51
6445 357
2693 0004624 225
1516 134
9261 15
54364073 13198


Satellite: ISS
Catalog Number: 25544
Epoch time:      15329
83946755   =   yrday
fracday
Element set:     910
Inclination:       51
6445  deg
RA of node:       357
2693  deg
Eccentricity:     
0004624     
Arg of perigee:   225
1516  deg
Mean anomaly:     134
9261  deg
Mean motion:   15
54364073  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1319
Checksum:              317


Coasting Arc #12 (Orbit 1334)
---------------------------------------

Vector Time (GMT): 2015/330/19:59:37
414
Vector Time (MET): N/A
Weight (LBS)     : 906444
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6252274
16                 A    =         6787721
38  meter
 Y    =        2130488
15  meter          E    =           
0013052
 Z    =        1528126
11                 I    =           51
61308
 XDOT =      -2842
555792                 Wp   =          137
30500
 YDOT =      -4197
482856  meter/sec      RA   =          351
74404  deg
 ZDOT =      -5758
714366                 TA   =           25
98339
                                          MA   =           25
91792
                                          Ha   =            219
991  n
mi
                                          Hp   =            215
556

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20512710
49                 X    =        -6283056
30
 Y    =        6989790
51  feet           Y    =         2060398
87  meter
 Z    =        5013537
10                 Z    =         1497678
63
 XDOT =      -9325
970445                 XDOT =       -2767
433084
 YDOT =     -13771
269212  feet/sec       YDOT =       -4228
849749  meter/sec
 ZDOT =     -18893
419837                 ZDOT =       -5772
341019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19934047
74                 X    =        -6075897
75
 Y    =        8577203
41  feet           Y    =         2614331
60  meter
 Z    =        4881530
45                 Z    =         1487890
48
 XDOT =      -9629
467723                 XDOT =       -2935
061762
 YDOT =     -11556
519759  feet/sec       YDOT =       -3522
427222  meter/sec
 ZDOT =     -18951
405943                 ZDOT =       -5776
388532


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
86814306  
00016717  00000-0  10270-3 0  9117
2 25544  51
6444 352
1392 0004615 228
3767 131
6991 15
54359664 13352


Satellite: ISS
Catalog Number: 25544
Epoch time:      15330
86814306   =   yrday
fracday
Element set:     911
Inclination:       51
6444  deg
RA of node:       352
1392  deg
Eccentricity:     
0004615     
Arg of perigee:   228
3767  deg
Mean anomaly:     131
6991  deg
Mean motion:   15
54359664  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1335
Checksum:              313


Coasting Arc #13 (Orbit 1350)
---------------------------------------

Vector Time (GMT): 2015/331/19:59:37
414
Vector Time (MET): N/A
Weight (LBS)     : 906444
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6642545
35                 A    =         6788496
33  meter
 Y    =       -1356974
80  meter          E    =           
0008125
 Z    =         251480
04                 I    =           51
58504
 XDOT =        732
036261                 Wp   =           44
72311
 YDOT =       4716
310065  meter/sec      RA   =          346
76856  deg
 ZDOT =       6000
715571                 TA   =          317
98846
                                          MA   =          318
05074
                                          Ha   =            219
716  n
mi
                                          Hp   =            215
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21793127
80                 X    =         6656004
07
 Y    =       -4452017
05  feet           Y    =        -1282618
24  meter
 Z    =         825065
74                 Z    =          283781
23
 XDOT =       2401
693771                 XDOT =         650
093326
 YDOT =      15473
458217  feet/sec       YDOT =        4724
037539  meter/sec
 ZDOT =      19687
387045                 ZDOT =        6004
073040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21263143
55                 X    =         6481006
15
 Y    =       -6510704
29  feet           Y    =        -1984462
67  meter
 Z    =         964917
00                 Z    =          294106
70
 XDOT =       3267
271891                 XDOT =         995
864472
 YDOT =      13637
002268  feet/sec       YDOT =        4156
558291  meter/sec
 ZDOT =      19700
892443                 ZDOT =        6004
832017


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
89679930  
00016717  00000-0  10270-3 0  9124
2 25544  51
6447 347
0084 0004547 234
1888 125
8843 15
54402347 13515


Satellite: ISS
Catalog Number: 25544
Epoch time:      15331
89679930   =   yrday
fracday
Element set:     912
Inclination:       51
6447  deg
RA of node:       347
0084  deg
Eccentricity:     
0004547     
Arg of perigee:   234
1888  deg
Mean anomaly:     125
8843  deg
Mean motion:   15
54402347  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1351
Checksum:              323


Coasting Arc #14 (Orbit 1365)
---------------------------------------

Vector Time (GMT): 2015/332/19:59:37
414
Vector Time (MET): N/A
Weight (LBS)     : 906444
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6457255
56                 A    =         6786702
35  meter
 Y    =         428036
89  meter          E    =           
0007498
 Z    =       -2029188
62                 I    =           51
54886
 XDOT =       1403
605335                 Wp   =          177
00711
 YDOT =      -5101
843936  meter/sec      RA   =          341
79028  deg
 ZDOT =      -5550
970305                 TA   =           25
45356
                                          MA   =           25
41665
                                          Ha   =            219
517  n
mi
                                          Hp   =            215
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21185221
67                 X    =        -6451704
94
 Y    =        1404320
50  feet           Y    =          355858
78  meter
 Z    =       -6657442
97                 Z    =        -2060543
46
 XDOT =       4605
004379                 XDOT =        1487
515839
 YDOT =     -16738
333124  feet/sec       YDOT =       -5085
678306  meter/sec
 ZDOT =     -18211
844833                 ZDOT =       -5543
948377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20849921
74                 X    =        -6355056
15
 Y    =        3774002
62  feet           Y    =         1150316
00  meter
 Z    =       -6793007
27                 Z    =        -2070508
62
 XDOT =       3082
819553                 XDOT =         939
643400
 YDOT =     -15644
640311  feet/sec       YDOT =       -4768
486367  meter/sec
 ZDOT =     -18180
424431                 ZDOT =       -5541
393366


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
86114838  
00016717  00000-0  10270-3 0  9134
2 25544  51
6452 342
1989 0004696 237
0830 122
9872 15
54406035 13669


Satellite: ISS
Catalog Number: 25544
Epoch time:      15332
86114838   =   yrday
fracday
Element set:     913
Inclination:       51
6452  deg
RA of node:       342
1989  deg
Eccentricity:     
0004696     
Arg of perigee:   237
0830  deg
Mean anomaly:     122
9872  deg
Mean motion:   15
54406035  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1366
Checksum:              317


Coasting Arc #15 (Orbit 1381)
---------------------------------------

Vector Time (GMT): 2015/333/19:59:37
414
Vector Time (MET): N/A
Weight (LBS)     : 906444
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5740095
94                 A    =         6782927
36  meter
 Y    =         616870
96  meter          E    =           
0008541
 Z    =        3556343
08                 I    =           51
50672
 XDOT =      -3332
724391                 Wp   =          108
64983
 YDOT =       5280
084735  meter/sec      RA   =          336
80103  deg
 ZDOT =       4451
845693                 TA   =          293
42611
                                          MA   =          293
51589
                                          Ha   =            219
344  n
mi
                                          Hp   =            215
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18832335
76                 X    =         5715495
85
 Y    =        2023854
86  feet           Y    =          680922
73  meter
 Z    =       11667792
25                 Z    =         3584167
78
 XDOT =     -10934
135142                 XDOT =       -3413
145402
 YDOT =      17323
112648  feet/sec       YDOT =        5242
366067  meter/sec
 ZDOT =      14605
792955                 ZDOT =        4435
460882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18861519
86                 X    =         5748991
25
 Y    =        -423256
21  feet           Y    =         -129008
49  meter
 Z    =       11787881
80                 Z    =         3592946
37
 XDOT =      -8719
794054                 XDOT =       -2657
793228
 YDOT =      17232
212757  feet/sec       YDOT =        5252
378448  meter/sec
 ZDOT =      14533
885897                 ZDOT =        4429
928421


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
88977014  
00016717  00000-0  10270-3 0  9141
2 25544  51
6453 337
0681 0004452 242
0020 118
0683 15
54447612 13829


Satellite: ISS
Catalog Number: 25544
Epoch time:      15333
88977014   =   yrday
fracday
Element set:     914
Inclination:       51
6453  deg
RA of node:       337
0681  deg
Eccentricity:     
0004452     
Arg of perigee:   242
0020  deg
Mean anomaly:     118
0683  deg
Mean motion:   15
54447612  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1382
Checksum:              294


Coasting Arc #16 (Orbit 1396)
---------------------------------------

Vector Time (GMT): 2015/334/19:59:37
414
Vector Time (MET): N/A
Weight (LBS)     : 906444
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4568734
28                 A    =         6778832
20  meter
 Y    =       -1784340
94  meter          E    =           
0006303
 Z    =       -4685316
23                 I    =           51
46460
 XDOT =       4904
411238                 Wp   =           73
28075
 YDOT =      -5172
778355  meter/sec      RA   =          331
79832  deg
 ZDOT =      -2813
760498                 TA   =          168
73165
                                          MA   =          168
71753
                                          Ha   =            219
104  n
mi
                                          Hp   =            215
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14989285
70                 X    =        -4525682
20
 Y    =       -5854136
95  feet           Y    =        -1835190
60  meter
 Z    =      -15371772
41                 Z    =        -4707405
85
 XDOT =      16090
588050                 XDOT =        4975
558243
 YDOT =     -16971
057596  feet/sec       YDOT =       -5117
536050  meter/sec
 ZDOT =      -9231
497698                 ZDOT =       -2789
763178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15588323
91                 X    =        -4751321
13
 Y    =       -3608617
12  feet           Y    =        -1099906
50  meter
 Z    =      -15466836
53                 Z    =        -4714291
77
 XDOT =      13222
709458                 XDOT =        4030
281843
 YDOT =     -18019
975053  feet/sec       YDOT =       -5492
488396  meter/sec
 ZDOT =      -9126
730140                 ZDOT =       -2781
827347


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
85408505  
00016717  00000-0  10270-3 0  9154
2 25544  51
6453 332
2583 0004586 246
9317 113
1352 15
54499228 13972


Satellite: ISS
Catalog Number: 25544
Epoch time:      15334
85408505   =   yrday
fracday
Element set:     915
Inclination:       51
6453  deg
RA of node:       332
2583  deg
Eccentricity:     
0004586     
Arg of perigee:   246
9317  deg
Mean anomaly:     113
1352  deg
Mean motion:   15
54499228  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1397
Checksum:              320
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