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

 
Date: August 17th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


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

237/07:37:09 920 1 3 4 6 4 6
N/A 4 4 -0 5 219 8
000/00:14:15 840 0 4 -0 0 215 9

239/10:11:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 216 0

Coasting Arc #1 (Orbit 1420)
---------------------------------------

Vector Time (GMT): 2016/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4401789
45                 A    =         6785802
07  meter
 Y    =       -4912441
54  meter          E    =           
0009694
 Z    =       -1577836
48                 I    =           51
97477
 XDOT =       2700
038624                 Wp   =          140
97675
 YDOT =       4264
975827  meter/sec      RA   =          121
08061  deg
 ZDOT =      -5772
661727                 TA   =           56
20078
                                          MA   =           56
10851
                                          Ha   =            220
141  n
mi
                                          Hp   =            212
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14441566
45                 X    =         4464058
79
 Y    =      -16116934
19  feet           Y    =        -4862869
60  meter
 Z    =       -5176628
87                 Z    =        -1556302
86
 XDOT =       8858
394436                 XDOT =        2680
186535
 YDOT =      13992
702846  feet/sec       YDOT =        4295
058526  meter/sec
 ZDOT =     -18939
178895                 ZDOT =       -5759
594013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21224717
23                 X    =        -6469293
81
 Y    =        4335850
62  feet           Y    =         1321567
27  meter
 Z    =       -5081699
88                 Z    =        -1548902
12
 XDOT =       1427
257441                 XDOT =         435
028068
 YDOT =     -15040
372457  feet/sec       YDOT =       -4584
305525  meter/sec
 ZDOT =     -18882
788675                 ZDOT =       -5755
473988


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16228
52915288  
00016717  00000-0  10270-3 0  9006
2 25544  51
6438 121
9286 0001575 132
5417 227
5869 15
54990865 14218


Satellite: ISS
Catalog Number: 25544
Epoch time:      16228
52915288   =   yrday
fracday
Element set:     900
Inclination:       51
6438  deg
RA of node:       121
9286  deg
Eccentricity:     
0001575     
Arg of perigee:   132
5417  deg
Mean anomaly:     227
5869  deg
Mean motion:   15
54990865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1421
Checksum:              328


Coasting Arc #2 (Orbit 1436)
---------------------------------------

Vector Time (GMT): 2016/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4672446
96                 A    =         6782089
06  meter
 Y    =        3595644
10  meter          E    =           
0013753
 Z    =        3340837
26                 I    =           51
97896
 XDOT =      -1189
764562                 Wp   =           92
36363
 YDOT =      -5938
550342  meter/sec      RA   =          116
12165  deg
 ZDOT =       4710
279221                 TA   =          306
37769
                                          MA   =          306
50450
                                          Ha   =            220
114  n
mi
                                          Hp   =            212
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15329550
39                 X    =        -4728535
12
 Y    =       11796732
63  feet           Y    =         3543080
09  meter
 Z    =       10960752
15                 Z    =         3318003
88
 XDOT =      -3903
427041                 XDOT =       -1146
149818
 YDOT =     -19483
432880  feet/sec       YDOT =       -5951
611194  meter/sec
 ZDOT =      15453
671986                 ZDOT =        4704
605723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19388903
58                 X    =         5909737
81
 Y    =        -647521
43  feet           Y    =         -197364
53  meter
 Z    =       10860351
63                 Z    =         3310235
18
 XDOT =      -8114
800386                 XDOT =       -2473
391158
 YDOT =      16765
517623  feet/sec       YDOT =        5110
129772  meter/sec
 ZDOT =      15429
879404                 ZDOT =        4703
027242


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16229
55739162  
00016717  00000-0  10270-3 0  9016
2 25544  51
6443 116
7960 0001436 128
6258 231
5024 15
55019547 14375


Satellite: ISS
Catalog Number: 25544
Epoch time:      16229
55739162   =   yrday
fracday
Element set:     901
Inclination:       51
6443  deg
RA of node:       116
7960  deg
Eccentricity:     
0001436     
Arg of perigee:   128
6258  deg
Mean anomaly:     231
5024  deg
Mean motion:   15
55019547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1437
Checksum:              305


Coasting Arc #3 (Orbit 1451)
---------------------------------------

Vector Time (GMT): 2016/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4597035
79                 A    =         6777550
09  meter
 Y    =       -1780016
81  meter          E    =           
0011028
 Z    =       -4661710
79                 I    =           51
97732
 XDOT =       -256
567055                 Wp   =           76
45119
 YDOT =       7063
831666  meter/sec      RA   =          111
15045  deg
 ZDOT =      -2953
582863                 TA   =          164
26365
                                          MA   =          164
22935
                                          Ha   =            219
942  n
mi
                                          Hp   =            212
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15082138
43                 X    =         4639242
84
 Y    =       -5839950
15  feet           Y    =        -1728373
81  meter
 Z    =      -15294326
73                 Z    =        -4639277
45
 XDOT =       -841
755430                 XDOT =        -321
190610
 YDOT =      23175
300741  feet/sec       YDOT =        7060
601153  meter/sec
 ZDOT =      -9690
232489                 ZDOT =       -2954
986317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15815625
85                 X    =        -4820602
76
 Y    =       -3800099
46  feet           Y    =        -1158270
32  meter
 Z    =      -15195972
19                 Z    =        -4631732
32
 XDOT =      13509
543550                 XDOT =        4117
708874
 YDOT =     -17490
450164  feet/sec       YDOT =       -5331
089210  meter/sec
 ZDOT =      -9697
566101                 ZDOT =       -2955
818148


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16230
52135726  
00016717  00000-0  10270-3 0  9022
2 25544  51
6441 111
9847 0001324 132
9302 227
1963 15
55054331 14528


Satellite: ISS
Catalog Number: 25544
Epoch time:      16230
52135726   =   yrday
fracday
Element set:     902
Inclination:       51
6441  deg
RA of node:       111
9847  deg
Eccentricity:     
0001324     
Arg of perigee:   132
9302  deg
Mean anomaly:     227
1963  deg
Mean motion:   15
55054331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1452
Checksum:              274


Coasting Arc #4 (Orbit 1467)
---------------------------------------

Vector Time (GMT): 2016/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4219149
74                 A    =         6774864
79  meter
 Y    =        -299465
55  meter          E    =           
0004609
 Z    =        5289294
92                 I    =           51
97835
 XDOT =       1524
984448                 Wp   =          124
86450
 YDOT =      -7478
344116  meter/sec      RA   =          106
16784  deg
 ZDOT =        789
990099                 TA   =          317
60808
                                          MA   =          317
64367
                                          Ha   =            220
085  n
mi
                                          Hp   =            212
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13842354
79                 X    =        -4241180
05
 Y    =        -982498
54  feet           Y    =         -346769
84  meter
 Z    =       17353329
79                 Z    =         5268746
28
 XDOT =       5003
229817                 XDOT =        1604
658494
 YDOT =     -24535
249724  feet/sec       YDOT =       -7460
845199  meter/sec
 ZDOT =       2591
831034                 ZDOT =         797
591799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11084266
74                 X    =         3378484
50
 Y    =        8533618
11  feet           Y    =         2601046
80  meter
 Z    =       17263560
96                 Z    =         5261933
38
 XDOT =     -17099
506146                 XDOT =       -5211
929473
 YDOT =      16876
998669  feet/sec       YDOT =        5144
109194  meter/sec
 ZDOT =       2626
334705                 ZDOT =         800
506818


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16231
54958346  
00016717  00000-0  10270-3 0  9037
2 25544  51
6434 106
8523 0001432 137
7581 222
3683 15
55053460 14681


Satellite: ISS
Catalog Number: 25544
Epoch time:      16231
54958346   =   yrday
fracday
Element set:     903
Inclination:       51
6434  deg
RA of node:       106
8523  deg
Eccentricity:     
0001432     
Arg of perigee:   137
7581  deg
Mean anomaly:     222
3683  deg
Mean motion:   15
55053460  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1468
Checksum:              302


Coasting Arc #5 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2016/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3644777
80                 A    =         6775329
73  meter
 Y    =        2436053
15  meter          E    =           
0014697
 Z    =       -5178934
29                 I    =           51
98792
 XDOT =      -2586
435510                 Wp   =          104
66077
 YDOT =       7051
860973  meter/sec      RA   =          101
18149  deg
 ZDOT =       1496
702912                 TA   =          179
70082
                                          MA   =          179
69993
                                          Ha   =            219
815  n
mi
                                          Hp   =            213
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11957932
40                 X    =         3642422
91
 Y    =        7992300
36  feet           Y    =         2476798
00  meter
 Z    =      -16991254
22                 Z    =        -5161235
07
 XDOT =      -8485
680806                 XDOT =       -2672
369181
 YDOT =      23136
026813  feet/sec       YDOT =        7022
457332  meter/sec
 ZDOT =       4910
442625                 ZDOT =        1483
929721

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5864490
25                 X    =        -1787496
63
 Y    =      -13231998
81  feet           Y    =        -4033113
24  meter
 Z    =      -16914304
41                 Z    =        -5155479
98
 XDOT =      18671
948333                 XDOT =        5691
209852
 YDOT =     -14479
868559  feet/sec       YDOT =       -4413
463937  meter/sec
 ZDOT =       4853
397665                 ZDOT =        1479
315608


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16232
51353996  
00016717  00000-0  10270-3 0  9046
2 25544  51
6431 102
0403 0001257 143
8972 216
2266 15
55074087 14834


Satellite: ISS
Catalog Number: 25544
Epoch time:      16232
51353996   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       102
0403  deg
Eccentricity:     
0001257     
Arg of perigee:   143
8972  deg
Mean anomaly:     216
2266  deg
Mean motion:   15
55074087  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1483
Checksum:              294


Coasting Arc #6 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2016/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2905585
62                 A    =         6778670
84  meter
 Y    =       -4353700
74  meter          E    =           
0010210
 Z    =        4300018
31                 I    =           52
00501
 XDOT =       3448
220831                 Wp   =           78
56433
 YDOT =      -5846
096288  meter/sec      RA   =           96
20214  deg
 ZDOT =      -3579
933462                 TA   =           47
77768
                                          MA   =           47
69109
                                          Ha   =            219
774  n
mi
                                          Hp   =            212
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9532761
23                 X    =        -2877572
82
 Y    =      -14283795
08  feet           Y    =        -4386035
99  meter
 Z    =       14107671
62                 Z    =         4285972
28
 XDOT =      11313
060469                 XDOT =        3530
726601
 YDOT =     -19180
105931  feet/sec       YDOT =       -5807
074928  meter/sec
 ZDOT =     -11745
188523                 ZDOT =       -3562
982282

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         713033
34                 X    =          217332
56
 Y    =       17207540
16  feet           Y    =         5244858
24  meter
 Z    =       14047023
96                 Z    =         4281532
90
 XDOT =     -18495
943834                 XDOT =       -5637
563680
 YDOT =      10317
618484  feet/sec       YDOT =        3144
810114  meter/sec
 ZDOT =     -11670
078624                 ZDOT =       -3557
039964


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16233
54175252  
00016717  00000-0  10270-3 0  9058
2 25544  51
6433  96
9071 0001044 146
8412 213
2807 15
55114694 14998


Satellite: ISS
Catalog Number: 25544
Epoch time:      16233
54175252   =   yrday
fracday
Element set:     905
Inclination:       51
6433  deg
RA of node:        96
9071  deg
Eccentricity:     
0001044     
Arg of perigee:   146
8412  deg
Mean anomaly:     213
2807  deg
Mean motion:   15
55114694  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1499
Checksum:              300


Coasting Arc #7 (Orbit 1504)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3859047
22                 A    =         6775390
91  meter
 Y    =       -2154039
07  meter          E    =           
0004948
 Z    =        5131848
68                 I    =           51
99535
 XDOT =       1846
031361                 Wp   =           72
50437
 YDOT =      -7261
274503  meter/sec      RA   =           94
31289  deg
 ZDOT =      -1656
905923                 TA   =           33
41598
                                          MA   =           33
38476
                                          Ha   =            219
883  n
mi
                                          Hp   =            212
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12660916
09                 X    =        -3859601
39
 Y    =       -7067057
33  feet           Y    =        -2197196
22  meter
 Z    =       16836773
88                 Z    =         5113101
46
 XDOT =       6056
533335                 XDOT =        1935
140001
 YDOT =     -23823
079079  feet/sec       YDOT =       -7240
132838  meter/sec
 ZDOT =      -5436
043055                 ZDOT =       -1647
721485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3203390
57                 X    =          976393
45
 Y    =      -14238003
11  feet           Y    =        -4339743
35  meter
 Z    =       16755196
41                 Z    =         5106983
87
 XDOT =      23537
766833                 XDOT =        7174
311331
 YDOT =      -1063
343979  feet/sec       YDOT =        -324
107245  meter/sec
 ZDOT =      -5394
635515                 ZDOT =       -1644
284905


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16233
92733159  
00016717  00000-0  10270-3 0  9067
2 25544  51
6434  94
9792 0001525 157
2132 202
9089 15
55107408 15056


Satellite: ISS
Catalog Number: 25544
Epoch time:      16233
92733159   =   yrday
fracday
Element set:     906
Inclination:       51
6434  deg
RA of node:        94
9792  deg
Eccentricity:     
0001525     
Arg of perigee:   157
2132  deg
Mean anomaly:     202
9089  deg
Mean motion:   15
55107408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1505
Checksum:              307


Coasting Arc #8 (Orbit 1519)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3348053
57                 A    =         6779010
39  meter
 Y    =        4120324
08  meter          E    =           
0009134
 Z    =       -4225055
60                 I    =           52
00762
 XDOT =      -2820
809379                 Wp   =          117
55630
 YDOT =       6085
668660  meter/sec      RA   =           89
33588  deg
 ZDOT =       3701
527462                 TA   =          190
24601
                                          MA   =          190
26464
                                          Ha   =            219
778  n
mi
                                          Hp   =            212
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10984427
72                 X    =         3322253
55
 Y    =       13518123
62  feet           Y    =         4157619
67  meter
 Z    =      -13861730
97                 Z    =        -4208854
73
 XDOT =      -9254
623948                 XDOT =       -2906
631489
 YDOT =      19966
104528  feet/sec       YDOT =        6053
644914  meter/sec
 ZDOT =      12144
118969                 ZDOT =        3687
615868

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9621934
46                 X    =        -2932765
62
 Y    =       14586095
04  feet           Y    =         4445841
77  meter
 Z    =      -13791631
98                 Z    =        -4203689
43
 XDOT =     -20773
672776                 XDOT =       -6331
815462
 YDOT =      -2285
745039  feet/sec       YDOT =        -696
695088  meter/sec
 ZDOT =      12082
240324                 ZDOT =        3682
666851


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16234
89127691  
00016717  00000-0  10270-3 0  9073
2 25544  51
6421  90
1682 0001660 157
5347 202
5879 15
55102379 15201


Satellite: ISS
Catalog Number: 25544
Epoch time:      16234
89127691   =   yrday
fracday
Element set:     907
Inclination:       51
6421  deg
RA of node:        90
1682  deg
Eccentricity:     
0001660     
Arg of perigee:   157
5347  deg
Mean anomaly:     202
5879  deg
Mean motion:   15
55102379  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1520
Checksum:              308


Coasting Arc #9 (Orbit 1535)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2655949
18                 A    =         6783502
44  meter
 Y    =       -5629393
09  meter          E    =           
0014384
 Z    =        2678505
92                 I    =           52
02182
 XDOT =       3685
409919                 Wp   =          107
24077
 YDOT =      -4236
372889  meter/sec      RA   =           84
37161  deg
 ZDOT =      -5230
271968                 TA   =           42
66251
                                          MA   =           42
55090
                                          Ha   =            219
764  n
mi
                                          Hp   =            212
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8713744
04                 X    =        -2605813
45
 Y    =      -18469137
43  feet           Y    =        -5658813
18  meter
 Z    =        8787749
09                 Z    =         2665726
23
 XDOT =      12091
239893                 XDOT =        3757
914482
 YDOT =     -13898
861183  feet/sec       YDOT =       -4194
755141  meter/sec
 ZDOT =     -17159
684935                 ZDOT =       -5212
192863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14793344
85                 X    =         4509011
51
 Y    =      -14112287
20  feet           Y    =        -4301425
14  meter
 Z    =        8732880
67                 Z    =         2661782
03
 XDOT =      15993
038506                 XDOT =        4874
678137
 YDOT =       6156
959048  feet/sec       YDOT =        1876
641118  meter/sec
 ZDOT =     -17079
903283                 ZDOT =       -5205
954521


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16235
91947879  
00016717  00000-0  10270-3 0  9086
2 25544  51
6427  85
0353 0001486 161
4326 198
6882 15
55099194 15368


Satellite: ISS
Catalog Number: 25544
Epoch time:      16235
91947879   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:        85
0353  deg
Eccentricity:     
0001486     
Arg of perigee:   161
4326  deg
Mean anomaly:     198
6882  deg
Mean motion:   15
55099194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1536
Checksum:              348


Coasting Arc #10 (Orbit 1550)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1823417
28                 A    =         6786403
84  meter
 Y    =        6487240
82  meter          E    =           
0009791
 Z    =        -770300
37                 I    =           52
02702
 XDOT =      -4388
385003                 Wp   =           45
93714
 YDOT =       1937
483265  meter/sec      RA   =           79
41942  deg
 ZDOT =       5982
538845                 TA   =          305
77936
                                          MA   =          305
87034
                                          Ha   =            219
749  n
mi
                                          Hp   =            213
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5982340
15                 X    =         1754481
56
 Y    =       21283598
49  feet           Y    =         6507246
01  meter
 Z    =       -2527232
19                 Z    =         -761610
50
 XDOT =     -14397
588593                 XDOT =       -4438
784773
 YDOT =       6356
572392  feet/sec       YDOT =        1888
127939  meter/sec
 ZDOT =      19627
752115                 ZDOT =        5961
098724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18119392
72                 X    =        -5522790
90
 Y    =       12674870
30  feet           Y    =         3863300
47  meter
 Z    =       -2490407
88                 Z    =         -759076
32
 XDOT =      -9863
696265                 XDOT =       -3006
454622
 YDOT =     -10297
681728  feet/sec       YDOT =       -3138
733391  meter/sec
 ZDOT =      19533
680050                 ZDOT =        5953
865679


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16236
88341282  
00016717  00000-0  10270-3 0  9090
2 25544  51
6427  80
2233 0001243 161
9967 198
1231 15
55049848 15510


Satellite: ISS
Catalog Number: 25544
Epoch time:      16236
88341282   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:        80
2233  deg
Eccentricity:     
0001243     
Arg of perigee:   161
9967  deg
Mean anomaly:     198
1231  deg
Mean motion:   15
55049848  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1551
Checksum:              314


Coasting Arc #11 (Orbit 1557)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4286860
41                 A    =         6780107
81  meter
 Y    =        2441113
07  meter          E    =           
0007812
 Z    =       -4658887
11                 I    =           51
99549
 XDOT =       -779
689125                 Wp   =          124
38664
 YDOT =       7022
796200  meter/sec      RA   =           77
21734  deg
 ZDOT =       2961
538963                 TA   =          174
99520
                                          MA   =          174
98738
                                          Ha   =            219
773  n
mi
                                          Hp   =            215
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14064502
66                 X    =         4281875
45
 Y    =        8008901
15  feet           Y    =         2489023
52  meter
 Z    =      -15285062
70                 Z    =        -4638074
91
 XDOT =      -2558
035187                 XDOT =        -872
547695
 YDOT =      23040
669949  feet/sec       YDOT =        7013
558134  meter/sec
 ZDOT =       9716
335179                 ZDOT =        2957
525562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8438277
88                 X    =         2571987
10
 Y    =      -13910708
98  feet           Y    =        -4239984
10  meter
 Z    =      -15194522
59                 Z    =        -4631290
49
 XDOT =      21935
905334                 XDOT =        6686
063946
 YDOT =       2711
137535  feet/sec       YDOT =         826
354721  meter/sec
 ZDOT =       9697
524593                 ZDOT =        2955
805496


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16237
33325012  
00016717  00000-0  10270-3 0  9106
2 25544  51
6434  77
9781 0003419 254
5833 105
4942 15
54176195 15589


Satellite: ISS
Catalog Number: 25544
Epoch time:      16237
33325012   =   yrday
fracday
Element set:     910
Inclination:       51
6434  deg
RA of node:        77
9781  deg
Eccentricity:     
0003419     
Arg of perigee:   254
5833  deg
Mean anomaly:     105
4942  deg
Mean motion:   15
54176195  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1558
Checksum:              309


Coasting Arc #12 (Orbit 1573)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4191897
43                 A    =         6783907
49  meter
 Y    =       -3960285
65  meter          E    =           
0008778
 Z    =        3565088
81                 I    =           51
99967
 XDOT =       1786
642658                 Wp   =           91
67716
 YDOT =      -5949
434882  meter/sec      RA   =           72
25443  deg
 ZDOT =      -4498
896777                 TA   =           46
46358
                                          MA   =           46
39069
                                          Ha   =            219
850  n
mi
                                          Hp   =            215
859

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13752944
33                 X    =        -4164618
55
 Y    =      -12993063
14  feet           Y    =        -4007009
61  meter
 Z    =       11696485
60                 Z    =         3544792
11
 XDOT =       5861
688511                 XDOT =        1874
891560
 YDOT =     -19519
143315  feet/sec       YDOT =       -5928
962166  meter/sec
 ZDOT =     -14760
160030                 ZDOT =       -4490
003217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13177263
68                 X    =        -4016429
97
 Y    =       13651881
37  feet           Y    =         4161093
44  meter
 Z    =       11608479
65                 Z    =         3538264
60
 XDOT =     -18442
872182                 XDOT =       -5621
387441
 YDOT =      -5258
726404  feet/sec       YDOT =       -1602
859808  meter/sec
 ZDOT =     -14720
195883                 ZDOT =       -4486
715705


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16238
36205377  
00016717  00000-0  10270-3 0  9112
2 25544  51
6431  72
8506 0003440 257
3332 102
7436 15
54166683 15741


Satellite: ISS
Catalog Number: 25544
Epoch time:      16238
36205377   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:        72
8506  deg
Eccentricity:     
0003440     
Arg of perigee:   257
3332  deg
Mean anomaly:     102
7436  deg
Mean motion:   15
54166683  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1574
Checksum:              297


Coasting Arc #13 (Orbit 1588)
---------------------------------------

Vector Time (GMT): 2016/239/07:44:17
840
Vector Time (MET): N/A
Weight (LBS)     : 929483
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3925561
31                 A    =         6787272
16  meter
 Y    =        5116414
65  meter          E    =           
0004487
 Z    =       -2108141
23                 I    =           52
00189
 XDOT =      -2835
775932                 Wp   =            8
72610
 YDOT =       4461
117031  meter/sec      RA   =           67
29930  deg
 ZDOT =       5552
405976                 TA   =          328
05159
                                          MA   =          328
07879
                                          Ha   =            219
614  n
mi
                                          Hp   =            215
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12879138
16                 X    =         3878296
87
 Y    =       16786137
30  feet           Y    =         5160048
58  meter
 Z    =       -6916473
87                 Z    =        -2089186
91
 XDOT =      -9303
726810                 XDOT =       -2912
421502
 YDOT =      14636
210733  feet/sec       YDOT =        4428
977068  meter/sec
 ZDOT =      18216
555041                 ZDOT =        5538
444327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16737325
84                 X    =         5101536
91
 Y    =      -12985953
84  feet           Y    =        -3958118
73  meter
 Z    =       -6834555
04                 Z    =        -2083172
38
 XDOT =      13725
841267                 XDOT =        4183
636418
 YDOT =       8146
299465  feet/sec       YDOT =        2482
992077  meter/sec
 ZDOT =      18154
697001                 ZDOT =        5533
551646


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   16239
32655051  
00016717  00000-0  10270-3 0  9128
2 25544  51
6444  68
0418 0003595 262
6540  97
4204 15
54202018 15897


Satellite: ISS
Catalog Number: 25544
Epoch time:      16239
32655051   =   yrday
fracday
Element set:     912
Inclination:       51
6444  deg
RA of node:        68
0418  deg
Eccentricity:     
0003595     
Arg of perigee:   262
6540  deg
Mean anomaly:      97
4204  deg
Mean motion:   15
54202018  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1589
Checksum:              299


Coasting Arc #14 (Orbit 1590)
---------------------------------------

Vector Time (GMT): 2016/239/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910045
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2163569
92                 A    =         6789036
10  meter
 Y    =       -6393663
10  meter          E    =           
0009086
 Z    =        -675846
01                 I    =           52
00520
 XDOT =       4685
355012                 Wp   =          159
76571
 YDOT =       -955
176589  meter/sec      RA   =           66
81863  deg
 ZDOT =      -5995
183692                 TA   =           27
49724
                                          MA   =           27
44920
                                          Ha   =            219
608  n
mi
                                          Hp   =            215
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7098326
51                 X    =        -2088630
62
 Y    =      -20976584
98  feet           Y    =        -6417438
59  meter
 Z    =       -2217342
56                 Z    =         -686173
84
 XDOT =      15371
899647                 XDOT =        4724
809600
 YDOT =      -3133
781459  feet/sec       YDOT =        -902
561350  meter/sec
 ZDOT =     -19669
237835                 ZDOT =       -5972
327742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12493078
87                 X    =        -3807890
44
 Y    =       18279207
02  feet           Y    =         5571502
30  meter
 Z    =       -2261312
81                 Z    =         -689248
15
 XDOT =     -10496
634781                 XDOT =       -3199
374281
 YDOT =      -9582
063963  feet/sec       YDOT =       -2920
613096  meter/sec
 ZDOT =     -19569
142755                 ZDOT =       -5964
674712


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   16239
45514915  
00016717  00000-0  10270-3 0  9136
2 25544  51
6434  67
4007 0003744 262
8739  97
1988 15
54159822 15914


Satellite: ISS
Catalog Number: 25544
Epoch time:      16239
45514915   =   yrday
fracday
Element set:     913
Inclination:       51
6434  deg
RA of node:        67
4007  deg
Eccentricity:     
0003744     
Arg of perigee:   262
8739  deg
Mean anomaly:      97
1988  deg
Mean motion:   15
54159822  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1591
Checksum:              334


Coasting Arc #15 (Orbit 1606)
---------------------------------------

Vector Time (GMT): 2016/240/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910045
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1266364
48                 A    =         6786755
52  meter
 Y    =        6239755
36  meter          E    =           
0010246
 Z    =        2334767
99                 I    =           51
98329
 XDOT =      -5328
043239                 Wp   =           67
43665
 YDOT =       -957
243320  meter/sec      RA   =           61
86888  deg
 ZDOT =       5433
047814                 TA   =          318
47600
                                          MA   =          318
55379
                                          Ha   =            219
501  n
mi
                                          Hp   =            215
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4154739
11                 X    =         1185154
67
 Y    =       20471638
31  feet           Y    =         6253462
68  meter
 Z    =        7659999
95                 Z    =         2340722
19
 XDOT =     -17480
456821                 XDOT =       -5343
334206
 YDOT =      -3140
562074  feet/sec       YDOT =       -1016
910427  meter/sec
 ZDOT =      17824
960019                 ZDOT =        5407
128704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13612002
77                 X    =         4148938
44
 Y    =      -15832927
48  feet           Y    =        -4825876
30  meter
 Z    =        7684869
50                 Z    =         2342348
22
 XDOT =       7197
754275                 XDOT =        2193
875503
 YDOT =      14808
942802  feet/sec       YDOT =        4513
765766  meter/sec
 ZDOT =      17711
825940                 ZDOT =        5398
564546


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   16240
48393935  
00016717  00000-0  10270-3 0  9149
2 25544  51
6421  62
2707 0003738 268
2921  91
7803 15
54214268 16076


Satellite: ISS
Catalog Number: 25544
Epoch time:      16240
48393935   =   yrday
fracday
Element set:     914
Inclination:       51
6421  deg
RA of node:        62
2707  deg
Eccentricity:     
0003738     
Arg of perigee:   268
2921  deg
Mean anomaly:      91
7803  deg
Mean motion:   15
54214268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1607
Checksum:              309


Coasting Arc #16 (Orbit 1621)
---------------------------------------

Vector Time (GMT): 2016/241/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910045
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -160764
08                 A    =         6783120
61  meter
 Y    =       -5642567
80  meter          E    =           
0002501
 Z    =       -3764168
32                 I    =           51
95361
 XDOT =       5756
081526                 Wp   =           54
93762
 YDOT =       2693
176695  meter/sec      RA   =           56
91120  deg
 ZDOT =      -4283
574421                 TA   =          169
85081
                                          MA   =          169
84576
                                          Ha   =            219
524  n
mi
                                          Hp   =            215
936

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -527441
22                 X    =          -79371
08
 Y    =      -18512361
54  feet           Y    =        -5643910
60  meter
 Z    =      -12349633
59                 Z    =        -3764751
37
 XDOT =      18884
781908                 XDOT =        5746
345384
 YDOT =       8835
881546  feet/sec       YDOT =        2757
490464  meter/sec
 ZDOT =     -14053
721855                 ZDOT =       -4255
636983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14114282
73                 X    =        -4302033
37
 Y    =       11988989
79  feet           Y    =         3654244
09  meter
 Z    =      -12351126
30                 Z    =        -3764623
30
 XDOT =      -4187
465675                 XDOT =       -1276
339538
 YDOT =     -19280
639999  feet/sec       YDOT =       -5876
739072  meter/sec
 ZDOT =     -13932
089008                 ZDOT =       -4246
500730


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   16241
44842827  
00016717  00000-0  10270-3 0  9156
2 25544  51
6407  57
4628 0003731 272
0202  88
0523 15
54197950 16229


Satellite: ISS
Catalog Number: 25544
Epoch time:      16241
44842827   =   yrday
fracday
Element set:     915
Inclination:       51
6407  deg
RA of node:        57
4628  deg
Eccentricity:     
0003731     
Arg of perigee:   272
0202  deg
Mean anomaly:      88
0523  deg
Mean motion:   15
54197950  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1622
Checksum:              299


Coasting Arc #17 (Orbit 1637)
---------------------------------------

Vector Time (GMT): 2016/242/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910045
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1085565
86                 A    =         6779539
19  meter
 Y    =        4684848
37  meter          E    =           
0004309
 Z    =        4777468
26                 I    =           51
92342
 XDOT =      -5890
927749                 Wp   =          136
40588
 YDOT =      -4109
486657  meter/sec      RA   =           51
94040  deg
 ZDOT =       2686
763615                 TA   =          287
14278
                                          MA   =          287
18996
                                          Ha   =            219
644  n
mi
                                          Hp   =            215
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3561567
78                 X    =        -1161078
83
 Y    =       15370237
44  feet           Y    =         4672286
87  meter
 Z    =       15674108
46                 Z    =         4772011
30
 XDOT =     -19327
190777                 XDOT =       -5857
587520
 YDOT =     -13482
567773  feet/sec       YDOT =       -4175
176402  meter/sec
 ZDOT =       8814
841258                 ZDOT =        2658
228641

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14136453
79                 X    =         4308791
11
 Y    =       -7061480
44  feet           Y    =        -2152339
24  meter
 Z    =       15649370
87                 Z    =         4769928
24
 XDOT =       1594
952068                 XDOT =         486
141390
 YDOT =      22485
926586  feet/sec       YDOT =        6853
710423  meter/sec
 ZDOT =       8690
865315                 ZDOT =        2648
975748


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16242
47721184  
00016717  00000-0  10270-3 0  9163
2 25544  51
6412  52
3329 0003709 277
0559  83
0172 15
54175057 16388


Satellite: ISS
Catalog Number: 25544
Epoch time:      16242
47721184   =   yrday
fracday
Element set:     916
Inclination:       51
6412  deg
RA of node:        52
3329  deg
Eccentricity:     
0003709     
Arg of perigee:   277
0559  deg
Mean anomaly:      83
0172  deg
Mean motion:   15
54175057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1638
Checksum:              305


Coasting Arc #18 (Orbit 1652)
---------------------------------------

Vector Time (GMT): 2016/243/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910045
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2423335
03                 A    =         6777274
25  meter
 Y    =       -3486150
91  meter          E    =           
0011142
 Z    =       -5292244
46                 I    =           51
89432
 XDOT =       5637
897889                 Wp   =           78
80180
 YDOT =       5125
194949  meter/sec      RA   =           46
95947  deg
 ZDOT =       -793
806883                 TA   =          183
62692
                                          MA   =          183
63501
                                          Ha   =            219
573  n
mi
                                          Hp   =            215
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7950574
23                 X    =         2487844
94
 Y    =      -11437502
98  feet           Y    =        -3458691
22  meter
 Z    =      -17363006
75                 Z    =        -5280315
79
 XDOT =      18497
040318                 XDOT =        5584
023545
 YDOT =      16814
944058  feet/sec       YDOT =        5187
940414  meter/sec
 ZDOT =      -2604
353290                 ZDOT =        -766
551074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13924453
34                 X    =        -4244173
38
 Y    =        1403089
22  feet           Y    =          427661
59  meter
 Z    =      -17310200
69                 Z    =        -5276149
17
 XDOT =        676
408566                 XDOT =         206
169331
 YDOT =     -23987
710496  feet/sec       YDOT =       -7311
454159  meter/sec
 ZDOT =      -2486
166472                 ZDOT =        -757
783541


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16243
44168848  
00016717  00000-0  10270-3 0  9174
2 25544  51
6399  47
5233 0003614 279
8517  80
2227 15
54221616 16531


Satellite: ISS
Catalog Number: 25544
Epoch time:      16243
44168848   =   yrday
fracday
Element set:     917
Inclination:       51
6399  deg
RA of node:        47
5233  deg
Eccentricity:     
0003614     
Arg of perigee:   279
8517  deg
Mean anomaly:      80
2227  deg
Mean motion:   15
54221616  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1653
Checksum:              319
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