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

 
Date: June 7th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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


157/20:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 213 6

160/13:46:59 311 -0 2 1 5 1 5
N/A 1 5 -0 1 220 1
000/00:03:58 622 0 1 -0 0 214 5

161/01:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 4

166/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 214 5

170/05:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 214 4

Coasting Arc #1 (Orbit 284)
---------------------------------------

Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1769974
72                 A    =         6777168
47  meter
 Y    =        4255656
55  meter          E    =           
0013486
 Z    =       -4981010
88                 I    =           51
92179
 XDOT =      -5517
466542                 Wp   =          109
03947
 YDOT =       4844
310688  meter/sec      RA   =          125
27304  deg
 ZDOT =       2178
789014                 TA   =          182
14379
                                          MA   =          182
14958
                                          Ha   =            220
376  n
mi
                                          Hp   =            213
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5807003
68                 X    =         1746451
35
 Y    =       13962127
79  feet           Y    =         4275318
58  meter
 Z    =      -16341899
21                 Z    =        -4972469
34
 XDOT =     -18101
924350                 XDOT =       -5581
810555
 YDOT =      15893
407768  feet/sec       YDOT =        4782
250710  meter/sec
 ZDOT =       7148
257921                 ZDOT =        2151
830320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15114663
41                 X    =         4606949
41
 Y    =       -1182812
86  feet           Y    =         -360521
36  meter
 Z    =      -16305455
46                 Z    =        -4969902
82
 XDOT =       9236
854352                 XDOT =        2815
393206
 YDOT =      21147
243331  feet/sec       YDOT =        6445
679767  meter/sec
 ZDOT =       7029
976856                 ZDOT =        2142
736946


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   16155
51235522  
00016717  00000-0  10270-3 0  9000
2 25544  51
6386 126
2512 0001207 141
7461 218
3778 15
54715795  2854


Satellite: ISS
Catalog Number: 25544
Epoch time:      16155
51235522   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:       126
2512  deg
Eccentricity:     
0001207     
Arg of perigee:   141
7461  deg
Mean anomaly:     218
3778  deg
Mean motion:   15
54715795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             285
Checksum:              298


Coasting Arc #2 (Orbit 300)
---------------------------------------

Vector Time (GMT): 2016/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -390479
17                 A    =         6780863
00  meter
 Y    =       -5481182
35  meter          E    =           
0011510
 Z    =        3963892
65                 I    =           51
95226
 XDOT =       5608
539006                 Wp   =           84
72572
 YDOT =      -3330
012427  meter/sec      RA   =          120
29631  deg
 ZDOT =      -4041
090339                 TA   =           47
29570
                                          MA   =           47
19884
                                          Ha   =            220
315  n
mi
                                          Hp   =            213
455

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1281099
63                 X    =         -348413
33
 Y    =      -17982881
73  feet           Y    =        -5485314
24  meter
 Z    =       13004897
15                 Z    =         3962097
27
 XDOT =      18400
718524                 XDOT =        5664
989339
 YDOT =     -10925
237622  feet/sec       YDOT =       -3266
977876  meter/sec
 ZDOT =     -13258
170402                 ZDOT =       -4013
708388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17560411
87                 X    =        -5352413
54
 Y    =       -4103024
09  feet           Y    =        -1250601
74  meter
 Z    =       12998066
39                 Z    =         3961810
64
 XDOT =      -5164
114884                 XDOT =       -1574
022217
 YDOT =     -19634
639744  feet/sec       YDOT =       -5984
638194  meter/sec
 ZDOT =     -13138
294516                 ZDOT =       -4004
552168


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   16156
54078338  
00016717  00000-0  10270-3 0  9015
2 25544  51
6386 121
1198 0001090 143
8529 216
2698 15
54747371  3018


Satellite: ISS
Catalog Number: 25544
Epoch time:      16156
54078338   =   yrday
fracday
Element set:     901
Inclination:       51
6386  deg
RA of node:       121
1198  deg
Eccentricity:     
0001090     
Arg of perigee:   143
8529  deg
Mean anomaly:     216
2698  deg
Mean motion:   15
54747371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             301
Checksum:              307


Coasting Arc #3 (Orbit 315)
---------------------------------------

Vector Time (GMT): 2016/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -841694
41                 A    =         6784994
41  meter
 Y    =        6267905
04  meter          E    =           
0005335
 Z    =       -2457432
54                 I    =           51
98166
 XDOT =      -5296
539897                 Wp   =           60
21961
 YDOT =       1387
347568  meter/sec      RA   =          115
33372  deg
 ZDOT =       5363
951900                 TA   =          272
40964
                                          MA   =          272
47071
                                          Ha   =            220
286  n
mi
                                          Hp   =            213
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2761464
60                 X    =         -899783
88
 Y    =       20563992
92  feet           Y    =         6258168
20  meter
 Z    =       -8062442
73                 Z    =        -2461661
54
 XDOT =     -17377
099399                 XDOT =       -5337
715914
 YDOT =       4551
665248  feet/sec       YDOT =        1327
887159  meter/sec
 ZDOT =      17598
267390                 ZDOT =        5338
122578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18945968
80                 X    =         5774731
29
 Y    =        8440250
31  feet           Y    =         2572588
29  meter
 Z    =       -8082011
84                 Z    =        -2463397
21
 XDOT =         11
806688                 XDOT =           3
598678
 YDOT =      16681
480924  feet/sec       YDOT =        5084
515386  meter/sec
 ZDOT =      17485
489064                 ZDOT =        5329
577067


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   16157
50493169  
00016717  00000-0  10270-3 0  9026
2 25544  51
6389 116
3095 0001099 148
1720 211
9500 15
54732850  3169


Satellite: ISS
Catalog Number: 25544
Epoch time:      16157
50493169   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:       116
3095  deg
Eccentricity:     
0001099     
Arg of perigee:   148
1720  deg
Mean anomaly:     211
9500  deg
Mean motion:   15
54732850  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             316
Checksum:              299


Coasting Arc #4 (Orbit 321)
---------------------------------------

Vector Time (GMT): 2016/157/20:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4288842
69                 A    =         6776128
38  meter
 Y    =        -405406
38  meter          E    =           
0005000
 Z    =        5227776
05                 I    =           51
95699
 XDOT =       2157
140767                 Wp   =          131
33112
 YDOT =      -7263
651713  meter/sec      RA   =          113
67353  deg
 ZDOT =       1202
463027                 TA   =          307
16671
                                          MA   =          307
21236
                                          Ha   =            220
405  n
mi
                                          Hp   =            213
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14071006
19                 X    =        -4309385
04
 Y    =       -1330073
41  feet           Y    =         -453482
67  meter
 Z    =       17151496
23                 Z    =         5206891
82
 XDOT =       7077
233486                 XDOT =        2232
363327
 YDOT =     -23830
878323  feet/sec       YDOT =       -7239
108706  meter/sec
 ZDOT =       3945
088670                 ZDOT =        1213
123632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13982718
38                 X    =         4261932
56
 Y    =       -2712221
46  feet           Y    =         -826685
10  meter
 Z    =       17060585
42                 Z    =         5200066
44
 XDOT =       -264
984315                 XDOT =         -80
767219
 YDOT =      23832
209620  feet/sec       YDOT =        7264
057492  meter/sec
 ZDOT =       3992
865694                 ZDOT =        1217
025464


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   16157
89058954  
00016717  00000-0  10270-3 0  9038
2 25544  51
6394 114
3842 0001081 158
3655 201
7544 15
54715755  3221


Satellite: ISS
Catalog Number: 25544
Epoch time:      16157
89058954   =   yrday
fracday
Element set:     903
Inclination:       51
6394  deg
RA of node:       114
3842  deg
Eccentricity:     
0001081     
Arg of perigee:   158
3655  deg
Mean anomaly:     201
7544  deg
Mean motion:   15
54715755  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             322
Checksum:              313


Coasting Arc #5 (Orbit 336)
---------------------------------------

Vector Time (GMT): 2016/158/20:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3555515
91                 A    =         6775811
17  meter
 Y    =        2363977
17  meter          E    =           
0014981
 Z    =       -5274381
99                 I    =           51
96823
 XDOT =      -3145
755263                 Wp   =          101
46719
 YDOT =       6913
729637  meter/sec      RA   =          108
68792  deg
 ZDOT =        977
594711                 TA   =          177
86252
                                          MA   =          177
85611
                                          Ha   =            220
184  n
mi
                                          Hp   =            213
625

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11665078
45                 X    =         3554437
81
 Y    =        7755830
62  feet           Y    =         2403732
04  meter
 Z    =      -17304402
84                 Z    =        -5257112
41
 XDOT =     -10320
719367                 XDOT =       -3227
581266
 YDOT =      22682
840017  feet/sec       YDOT =        6878
094052  meter/sec
 ZDOT =       3207
331729                 ZDOT =         962
115624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13550510
55                 X    =        -4130195
61
 Y    =       -3897954
04  feet           Y    =        -1188096
39  meter
 Z    =      -17229594
88                 Z    =        -5251580
52
 XDOT =       2837
393921                 XDOT =         864
837667
 YDOT =     -23744
854880  feet/sec       YDOT =       -7237
431767  meter/sec
 ZDOT =       3138
606183                 ZDOT =         956
647165


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   16158
85473038  
00016717  00000-0  10270-3 0  9040
2 25544  51
6392 109
5722 0001163 159
6494 200
4705 15
54764190  3376


Satellite: ISS
Catalog Number: 25544
Epoch time:      16158
85473038   =   yrday
fracday
Element set:     904
Inclination:       51
6392  deg
RA of node:       109
5722  deg
Eccentricity:     
0001163     
Arg of perigee:   159
6494  deg
Mean anomaly:     200
4705  deg
Mean motion:   15
54764190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             337
Checksum:              310


Coasting Arc #6 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2016/159/20:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2695348
91                 A    =         6778541
56  meter
 Y    =       -4165565
55  meter          E    =           
0008307
 Z    =        4612945
48                 I    =           51
98670
 XDOT =       3879
040616                 Wp   =           73
65295
 YDOT =      -5881
703771  meter/sec      RA   =          103
70881  deg
 ZDOT =      -3037
955941                 TA   =           46
55041
                                          MA   =           46
48133
                                          Ha   =            220
245  n
mi
                                          Hp   =            213
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8843008
24                 X    =        -2670975
86
 Y    =      -13666553
63  feet           Y    =        -4195571
07  meter
 Z    =       15134335
57                 Z    =         4599910
81
 XDOT =      12726
511207                 XDOT =        3959
280060
 YDOT =     -19296
928383  feet/sec       YDOT =       -5837
876704  meter/sec
 ZDOT =      -9967
047052                 ZDOT =       -3018
918457

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12779008
50                 X    =         3895041
79
 Y    =       10166758
50  feet           Y    =         3098827
99  meter
 Z    =       15078314
21                 Z    =         4595870
17
 XDOT =      -5342
764716                 XDOT =       -1628
474685
 YDOT =      21406
164442  feet/sec       YDOT =        6524
598922  meter/sec
 ZDOT =      -9882
990765                 ZDOT =       -3012
335585


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   16159
88314345  
00016717  00000-0  10270-3 0  9050
2 25544  51
6392 104
4411 0001153 168
0197 192
0983 15
54751536  3530


Satellite: ISS
Catalog Number: 25544
Epoch time:      16159
88314345   =   yrday
fracday
Element set:     905
Inclination:       51
6392  deg
RA of node:       104
4411  deg
Eccentricity:     
0001153     
Arg of perigee:   168
0197  deg
Mean anomaly:     192
0983  deg
Mean motion:   15
54751536  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              304


Coasting Arc #7 (Orbit 363)
---------------------------------------

Vector Time (GMT): 2016/160/13:48:58
622
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3878145
21                 A    =         6776556
25  meter
 Y    =        1767787
28  meter          E    =           
0013755
 Z    =       -5280429
48                 I    =           51
98607
 XDOT =      -2049
916910                 Wp   =          101
39536
 YDOT =       7318
850999  meter/sec      RA   =          100
07483  deg
 ZDOT =        944
110784                 TA   =          177
60946
                                          MA   =          177
60288
                                          Ha   =            220
138  n
mi
                                          Hp   =            214
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12723573
53                 X    =         3883739
10
 Y    =        5799827
03  feet           Y    =         1811187
21  meter
 Z    =      -17324243
71                 Z    =        -5261576
68
 XDOT =      -6725
449179                 XDOT =       -2136
191849
 YDOT =      24011
978342  feet/sec       YDOT =        7295
444955  meter/sec
 ZDOT =       3097
476324                 ZDOT =         933
944182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2576673
44                 X    =          785370
07
 Y    =      -13846173
05  feet           Y    =        -4220313
54  meter
 Z    =      -17242418
13                 Z    =        -5255489
05
 XDOT =      23917
985698                 XDOT =        7290
202041
 YDOT =        648
290401  feet/sec       YDOT =         197
598914  meter/sec
 ZDOT =       3051
796908                 ZDOT =         930
187697


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   16160
59017690  
00016717  00000-0  10270-3 0  9064
2 25544  51
6425 100
9165 0001221 222
8987 137
2070 15
54501777  3646


Satellite: ISS
Catalog Number: 25544
Epoch time:      16160
59017690   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:       100
9165  deg
Eccentricity:     
0001221     
Arg of perigee:   222
8987  deg
Mean anomaly:     137
2070  deg
Mean motion:   15
54501777  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             364
Checksum:              294


Coasting Arc #8 (Orbit 371)
---------------------------------------

Vector Time (GMT): 2016/161/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3735299
99                 A    =         6777049
47  meter
 Y    =       -2354893
04  meter          E    =           
0003433
 Z    =        5138791
30                 I    =           51
99143
 XDOT =       2252
484507                 Wp   =           63
17216
 YDOT =      -7148
124526  meter/sec      RA   =           97
66750  deg
 ZDOT =      -1636
046330                 TA   =           42
54585
                                          MA   =           42
51926
                                          Ha   =            220
206  n
mi
                                          Hp   =            214
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12254921
24                 X    =        -3733651
30
 Y    =       -7726027
05  feet           Y    =        -2396655
02  meter
 Z    =       16859551
52                 Z    =         5120649
96
 XDOT =       7390
041033                 XDOT =        2340
196392
 YDOT =     -23451
852119  feet/sec       YDOT =       -7122
445131  meter/sec
 ZDOT =      -5367
606071                 ZDOT =       -1624
892145

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5870119
20                 X    =         1789212
33
 Y    =      -13343948
90  feet           Y    =        -4067235
62  meter
 Z    =       16780935
45                 Z    =         5114829
12
 XDOT =      23302
058669                 XDOT =        7102
467482
 YDOT =       3553
738232  feet/sec       YDOT =        1083
179413  meter/sec
 ZDOT =      -5317
648646                 ZDOT =       -1620
819307


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   16161
10446878  
00016717  00000-0  10270-3 0  9077
2 25544  51
6432  98
3481 0001659 217
9223 142
1813 15
54529050  3721


Satellite: ISS
Catalog Number: 25544
Epoch time:      16161
10446878   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:        98
3481  deg
Eccentricity:     
0001659     
Arg of perigee:   217
9223  deg
Mean anomaly:     142
1813  deg
Mean motion:   15
54529050  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             372
Checksum:              302


Coasting Arc #9 (Orbit 386)
---------------------------------------

Vector Time (GMT): 2016/162/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3208222
25                 A    =         6780211
03  meter
 Y    =        4103042
52  meter          E    =           
0008195
 Z    =       -4349571
81                 I    =           52
00538
 XDOT =      -3033
802771                 Wp   =          121
22338
 YDOT =       6095
090855  meter/sec      RA   =           92
69506  deg
 ZDOT =       3512
653360                 TA   =          184
35077
                                          MA   =          184
35790
                                          Ha   =            220
042  n
mi
                                          Hp   =            214
491

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10525663
54                 X    =         3183230
81
 Y    =       13461425
58  feet           Y    =         4138779
68  meter
 Z    =      -14270248
70                 Z    =        -4334047
44
 XDOT =      -9953
421165                 XDOT =       -3118
797006
 YDOT =      19997
017241  feet/sec       YDOT =        6060
689283  meter/sec
 ZDOT =      11524
453281                 ZDOT =        3497
710117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11581236
93                 X    =        -3529961
02
 Y    =       12640365
48  feet           Y    =         3852783
40  meter
 Z    =      -14203368
67                 Z    =        -4329186
77
 XDOT =     -20426
636495                 XDOT =       -6226
038804
 YDOT =      -5842
863080  feet/sec       YDOT =       -1780
904667  meter/sec
 ZDOT =      11458
169775                 ZDOT =        3492
450147


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   16162
06876522  
00016717  00000-0  10270-3 0  9087
2 25544  51
6432  93
5396 0001625 220
2247 139
8786 15
54534330  3874


Satellite: ISS
Catalog Number: 25544
Epoch time:      16162
06876522   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:        93
5396  deg
Eccentricity:     
0001625     
Arg of perigee:   220
2247  deg
Mean anomaly:     139
8786  deg
Mean motion:   15
54534330  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             387
Checksum:              315


Coasting Arc #10 (Orbit 402)
---------------------------------------

Vector Time (GMT): 2016/163/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2575762
13                 A    =         6784370
07  meter
 Y    =       -5495593
84  meter          E    =           
0012278
 Z    =        3018132
50                 I    =           52
01927
 XDOT =       3718
888732                 Wp   =          102
42824
 YDOT =      -4489
775634  meter/sec      RA   =           87
73329  deg
 ZDOT =      -4986
978516                 TA   =           43
17638
                                          MA   =           43
08017
                                          Ha   =            220
103  n
mi
                                          Hp   =            214
450

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8450663
15                 X    =        -2528778
32
 Y    =      -18030163
53  feet           Y    =        -5524135
28  meter
 Z    =        9902009
51                 Z    =         3005733
80
 XDOT =      12201
078518                 XDOT =        3793
042645
 YDOT =     -14730
235019  feet/sec       YDOT =       -4447
773514  meter/sec
 ZDOT =     -16361
478072                 ZDOT =       -4968
733403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16231956
76                 X    =         4947500
42
 Y    =      -11578887
67  feet           Y    =        -3529244
96  meter
 Z    =        9849022
14                 Z    =         3001981
95
 XDOT =      15837
612538                 XDOT =        4827
304302
 YDOT =       8312
776135  feet/sec       YDOT =        2533
734166  meter/sec
 ZDOT =     -16281
099619                 ZDOT =       -4962
479164


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   16163
09734261  
00016717  00000-0  10270-3 0  9095
2 25544  51
6428  88
4097 0001506 224
7475 135
3557 15
54519313  4030


Satellite: ISS
Catalog Number: 25544
Epoch time:      16163
09734261   =   yrday
fracday
Element set:     909
Inclination:       51
6428  deg
RA of node:        88
4097  deg
Eccentricity:     
0001506     
Arg of perigee:   224
7475  deg
Mean anomaly:     135
3557  deg
Mean motion:   15
54519313  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             403
Checksum:              309


Coasting Arc #11 (Orbit 417)
---------------------------------------

Vector Time (GMT): 2016/164/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1868073
41                 A    =         6787523
58  meter
 Y    =        6381297
85  meter          E    =           
0007350
 Z    =       -1347178
81                 I    =           52
02694
 XDOT =      -4287
631189                 Wp   =           33
87212
 YDOT =       2485
665391  meter/sec      RA   =           82
78217  deg
 ZDOT =       5849
827566                 TA   =          311
53770
                                          MA   =          311
60072
                                          Ha   =            220
013  n
mi
                                          Hp   =            214
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6128849
76                 X    =         1803121
30
 Y    =       20936016
57  feet           Y    =         6401824
82  meter
 Z    =       -4419878
00                 Z    =        -1338261
48
 XDOT =     -14067
031460                 XDOT =       -4343
523765
 YDOT =       8155
070182  feet/sec       YDOT =        2437
405295  meter/sec
 ZDOT =      19192
347657                 ZDOT =        5828
863777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19339482
70                 X    =        -5894674
33
 Y    =       10109167
61  feet           Y    =         3081274
29  meter
 Z    =       -4382242
56                 Z    =        -1335707
53
 XDOT =     -10022
408805                 XDOT =       -3054
830204
 YDOT =     -10924
050858  feet/sec       YDOT =       -3329
650702  meter/sec
 ZDOT =      19100
497671                 ZDOT =        5821
831690


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   16164
06162869  
00016717  00000-0  10270-3 0  9104
2 25544  51
6424  83
6003 0001526 236
0794 124
0214 15
54487975  4181


Satellite: ISS
Catalog Number: 25544
Epoch time:      16164
06162869   =   yrday
fracday
Element set:     910
Inclination:       51
6424  deg
RA of node:        83
6003  deg
Eccentricity:     
0001526     
Arg of perigee:   236
0794  deg
Mean anomaly:     124
0214  deg
Mean motion:   15
54487975  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             418
Checksum:              299


Coasting Arc #12 (Orbit 433)
---------------------------------------

Vector Time (GMT): 2016/165/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1027506
81                 A    =         6788032
42  meter
 Y    =       -6683997
03  meter          E    =           
0010917
 Z    =        -517374
94                 I    =           52
02411
 XDOT =       4747
239063                 Wp   =          146
48416
 YDOT =       -269
330842  meter/sec      RA   =           77
83672  deg
 ZDOT =      -6017
636808                 TA   =           39
06923
                                          MA   =           38
99043
                                          Ha   =            219
947  n
mi
                                          Hp   =            214
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3371085
32                 X    =         -950175
12
 Y    =      -21929124
12  feet           Y    =        -6695054
87  meter
 Z    =       -1697424
34                 Z    =         -522178
98
 XDOT =      15574
931308                 XDOT =        4779
129093
 YDOT =       -883
631371  feet/sec       YDOT =        -216
065304  meter/sec
 ZDOT =     -19742
902913                 ZDOT =       -5994
498434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20724806
91                 X    =         6316921
14
 Y    =       -7916187
67  feet           Y    =        -2412854
00  meter
 Z    =       -1717062
00                 Z    =         -523360
50
 XDOT =       3604
807996                 XDOT =        1098
745477
 YDOT =      13649
317611  feet/sec       YDOT =        4160
312008  meter/sec
 ZDOT =     -19642
001189                 ZDOT =       -5986
881962


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   16165
09019512  
00016717  00000-0  10270-3 0  9115
2 25544  51
6423  78
4701 0001516 235
0560 125
0450 15
54534598  4341


Satellite: ISS
Catalog Number: 25544
Epoch time:      16165
09019512   =   yrday
fracday
Element set:     911
Inclination:       51
6423  deg
RA of node:        78
4701  deg
Eccentricity:     
0001516     
Arg of perigee:   235
0560  deg
Mean anomaly:     125
0450  deg
Mean motion:   15
54534598  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             434
Checksum:              280


Coasting Arc #13 (Orbit 449)
---------------------------------------

Vector Time (GMT): 2016/166/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          90447
27                 A    =         6785899
17  meter
 Y    =        6380101
39  meter          E    =           
0012468
 Z    =        2292975
36                 I    =           52
00967
 XDOT =      -5044
465393                 Wp   =           73
45500
 YDOT =      -1897
625501  meter/sec      RA   =           72
88796  deg
 ZDOT =       5458
025636                 TA   =          311
95588
                                          MA   =          312
06206
                                          Ha   =            219
929  n
mi
                                          Hp   =            214
470

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         296743
00                 X    =            7958
32
 Y    =       20932091
17  feet           Y    =         6380651
43  meter
 Z    =        7522885
04                 Z    =         2293214
87
 XDOT =     -16550
083309                 XDOT =       -5049
383598
 YDOT =      -6225
805449  feet/sec       YDOT =       -1954
063997  meter/sec
 ZDOT =      17906
908255                 ZDOT =        5433
508688

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20324838
81                 X    =        -6195010
87
 Y    =        5014437
84  feet           Y    =         1528400
65  meter
 Z    =        7522674
88                 Z    =         2292911
30
 XDOT =       2626
139821                 XDOT =         800
447418
 YDOT =     -16163
240720  feet/sec       YDOT =       -4926
555772  meter/sec
 ZDOT =      17800
423419                 ZDOT =        5425
569058


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   16166
11875375  
00016717  00000-0  10270-3 0  9127
2 25544  51
6426  73
3395 0001402 241
7112 118
3899 15
54542370  4505


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
11875375   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:        73
3395  deg
Eccentricity:     
0001402     
Arg of perigee:   241
7112  deg
Mean anomaly:     118
3899  deg
Mean motion:   15
54542370  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             450
Checksum:              296


Coasting Arc #14 (Orbit 455)
---------------------------------------

Vector Time (GMT): 2016/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3706451
71                 A    =         6785931
37  meter
 Y    =        5209791
11  meter          E    =           
0004976
 Z    =       -2268726
13                 I    =           52
00613
 XDOT =      -2956
627873                 Wp   =           36
16916
 YDOT =       4481
855887  meter/sec      RA   =           70
66167  deg
 ZDOT =       5471
627677                 TA   =          298
72231
                                          MA   =          298
77231
                                          Ha   =            219
914  n
mi
                                          Hp   =            214
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12160274
63                 X    =         3658939
60
 Y    =       17092490
52  feet           Y    =         5250973
65  meter
 Z    =       -7443327
21                 Z    =        -2250836
00
 XDOT =      -9700
222682                 XDOT =       -3033
104313
 YDOT =      14704
251599  feet/sec       YDOT =        4448
364856  meter/sec
 ZDOT =      17951
534373                 ZDOT =        5457
079654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18562396
36                 X    =         5657818
41
 Y    =       -9828656
88  feet           Y    =        -2995774
62  meter
 Z    =       -7366381
49                 Z    =        -2245273
08
 XDOT =      12554
529001                 XDOT =        3826
620440
 YDOT =      10329
197126  feet/sec       YDOT =        3148
339284  meter/sec
 ZDOT =      17887
241428                 ZDOT =        5452
031187


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   16166
50446308  
00016717  00000-0  10270-3 0  9131
2 25544  51
6430  71
4176 0001237 253
6191 106
4826 15
54560475  4561


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
50446308   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:        71
4176  deg
Eccentricity:     
0001237     
Arg of perigee:   253
6191  deg
Mean anomaly:     106
4826  deg
Mean motion:   15
54560475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             456
Checksum:              296


Coasting Arc #15 (Orbit 471)
---------------------------------------

Vector Time (GMT): 2016/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3103123
46                 A    =         6788071
18  meter
 Y    =       -6012909
97  meter          E    =           
0012191
 Z    =         454889
46                 I    =           52
00184
 XDOT =       4017
241631                 Wp   =          135
47274
 YDOT =      -2535
502826  meter/sec      RA   =           65
71337  deg
 ZDOT =      -6021
973678                 TA   =           39
64441
                                          MA   =           39
55534
                                          Ha   =            219
902  n
mi
                                          Hp   =            214
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10180851
23                 X    =        -3037864
63
 Y    =      -19727394
90  feet           Y    =        -6047246
32  meter
 Z    =        1492419
49                 Z    =          439973
11
 XDOT =      13179
926611                 XDOT =        4074
548045
 YDOT =      -8318
578825  feet/sec       YDOT =       -2490
258383  meter/sec
 ZDOT =     -19757
131489                 ZDOT =       -6002
319826

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20774642
48                 X    =        -6332111
03
 Y    =        7837121
31  feet           Y    =         2388754
57  meter
 Z    =        1428606
66                 Z    =          435439
31
 XDOT =      -6151
893164                 XDOT =       -1875
097036
 YDOT =     -12666
158626  feet/sec       YDOT =       -3860
645149  meter/sec
 ZDOT =     -19670
964019                 ZDOT =       -5995
709833


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   16167
53301433  
00016717  00000-0  10270-3 0  9145
2 25544  51
6434  66
2880 0001355 252
7568 107
3437 15
54534189  4727


Satellite: ISS
Catalog Number: 25544
Epoch time:      16167
53301433   =   yrday
fracday
Element set:     914
Inclination:       51
6434  deg
RA of node:        66
2880  deg
Eccentricity:     
0001355     
Arg of perigee:   252
7568  deg
Mean anomaly:     107
3437  deg
Mean motion:   15
54534189  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             472
Checksum:              306


Coasting Arc #16 (Orbit 487)
---------------------------------------

Vector Time (GMT): 2016/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2251033
23                 A    =         6787238
44  meter
 Y    =        6243879
20  meter          E    =           
0012661
 Z    =        1388294
03                 I    =           51
98625
 XDOT =      -4956
282700                 Wp   =           57
53616
 YDOT =        482
465246  meter/sec      RA   =           60
76473  deg
 ZDOT =       5834
408436                 TA   =          317
52575
                                          MA   =          317
62365
                                          Ha   =            219
828  n
mi
                                          Hp   =            214
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7385279
61                 X    =         2174301
51
 Y    =       20485167
97  feet           Y    =         6268622
57  meter
 Z    =        4554770
45                 Z    =         1399043
36
 XDOT =     -16260
770012                 XDOT =       -4989
650648
 YDOT =       1582
891227  feet/sec       YDOT =         426
853607  meter/sec
 ZDOT =      19141
759959                 ZDOT =        5810
250865

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21111617
17                 X    =         6434820
91
 Y    =       -5297800
46  feet           Y    =        -1614769
58  meter
 Z    =        4600361
57                 Z    =         1402190
21
 XDOT =       -426
548500                 XDOT =        -130
011983
 YDOT =      14920
774122  feet/sec       YDOT =        4547
851953  meter/sec
 ZDOT =      19036
372117                 ZDOT =        5802
286221


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   16168
56155696  
00016717  00000-0  10270-3 0  9158
2 25544  51
6443  61
1571 0001352 268
3966  91
7032 15
54562117  4886


Satellite: ISS
Catalog Number: 25544
Epoch time:      16168
56155696   =   yrday
fracday
Element set:     915
Inclination:       51
6443  deg
RA of node:        61
1571  deg
Eccentricity:     
0001352     
Arg of perigee:   268
3966  deg
Mean anomaly:      91
7032  deg
Mean motion:   15
54562117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             488
Checksum:              318


Coasting Arc #17 (Orbit 502)
---------------------------------------

Vector Time (GMT): 2016/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1107859
56                 A    =         6783995
64  meter
 Y    =       -5936334
82  meter          E    =           
0003148
 Z    =       -3092136
64                 I    =           51
95886
 XDOT =       5678
408591                 Wp   =          113
11696
 YDOT =       1502
448228  meter/sec      RA   =           55
81042  deg
 ZDOT =      -4924
075596                 TA   =          102
24242
                                          MA   =          102
20716
                                          Ha   =            219
779  n
mi
                                          Hp   =            214
522

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3634709
86                 X    =        -1026375
26
 Y    =      -19476164
12  feet           Y    =        -5948267
67  meter
 Z    =      -10144805
25                 Z    =        -3097321
18
 XDOT =      18629
949447                 XDOT =        5685
105023
 YDOT =       4929
292085  feet/sec       YDOT =        1565
986009  meter/sec
 ZDOT =     -16155
103661                 ZDOT =       -4896
474648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19703366
74                 X    =        -6005586
18
 Y    =        1968512
47  feet           Y    =          600002
60  meter
 Z    =      -10166191
81                 Z    =        -3098655
26
 XDOT =       6583
076323                 XDOT =        2006
521663
 YDOT =     -16832
525179  feet/sec       YDOT =       -5130
553675  meter/sec
 ZDOT =     -16035
111654                 ZDOT =       -4887
502032


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   16169
52580945  
00016717  00000-0  10270-3 0  9165
2 25544  51
6442  56
3483 0001462 268
4434  91
6551 15
54561981  5037


Satellite: ISS
Catalog Number: 25544
Epoch time:      16169
52580945   =   yrday
fracday
Element set:     916
Inclination:       51
6442  deg
RA of node:        56
3483  deg
Eccentricity:     
0001462     
Arg of perigee:   268
4434  deg
Mean anomaly:      91
6551  deg
Mean motion:   15
54561981  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             503
Checksum:              316


Coasting Arc #18 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2016/170/05:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 893042
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         447406
56                 A    =         6781498
84  meter
 Y    =        5534074
00  meter          E    =           
0009862
 Z    =        3887001
61                 I    =           51
93338
 XDOT =      -5988
818157                 Wp   =          100
41650
 YDOT =      -2426
952355  meter/sec      RA   =           52
12857  deg
 ZDOT =       4134
058351                 TA   =          306
34099
                                          MA   =          306
43199
                                          Ha   =            219
737  n
mi
                                          Hp   =            214
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1467869
31                 X    =          366608
41
 Y    =       18156410
77  feet           Y    =         5538624
92  meter
 Z    =       12752629
96                 Z    =         3888979
49
 XDOT =     -19648
353533                 XDOT =       -5981
315868
 YDOT =      -7962
442108  feet/sec       YDOT =       -2493
881902  meter/sec
 ZDOT =      13563
183565                 ZDOT =        4104
983877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -860865
34                 X    =         -262391
75
 Y    =       18190048
40  feet           Y    =         5544326
75  meter
 Z    =       12760114
15                 Z    =         3889282
79
 XDOT =     -17278
422074                 XDOT =       -5266
463048
 YDOT =     -10268
025231  feet/sec       YDOT =       -3129
694090  meter/sec
 ZDOT =      13436
961118                 ZDOT =        4095
585749


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   16170
29720716  
00016717  00000-0  10270-3 0  9174
2 25544  51
6403  52
4997 0001393 266
6121  93
4873 15
54613387  5155


Satellite: ISS
Catalog Number: 25544
Epoch time:      16170
29720716   =   yrday
fracday
Element set:     917
Inclination:       51
6403  deg
RA of node:        52
4997  deg
Eccentricity:     
0001393     
Arg of perigee:   266
6121  deg
Mean anomaly:      93
4873  deg
Mean motion:   15
54613387  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              313
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