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

 
Date: August 28th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 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


239/10:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 215 6

246/19:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 215 4

250/21:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 1

250/21:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 215 2

Coasting Arc #1 (Orbit 1561)
---------------------------------------

Vector Time (GMT): 2016/237/12:45:53
942
Vector Time (MET): N/A
Weight (LBS)     : 929160
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -769899
78                 A    =         6785368
39  meter
 Y    =        6117341
29  meter          E    =           
0010259
 Z    =        2823074
31                 I    =           52
00926
 XDOT =      -4857
194880                 Wp   =           84
90770
 YDOT =      -2985
452329  meter/sec      RA   =           76
21964  deg
 ZDOT =       5129
473259                 TA   =          306
97883
                                          MA   =          307
07270
                                          Ha   =            219
723  n
mi
                                          Hp   =            215
441

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2525917
90                 X    =         -851961
45
 Y    =       20070017
34  feet           Y    =         6108273
04  meter
 Z    =        9262054
82                 Z    =         2819134
75
 XDOT =     -15935
678740                 XDOT =       -4848
366483
 YDOT =      -9794
791105  feet/sec       YDOT =       -3039
719141  meter/sec
 ZDOT =      16828
980507                 ZDOT =        5105
899882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8066866
05                 X    =         2458780
77
 Y    =      -18559382
85  feet           Y    =        -5656899
89  meter
 Z    =        9243727
46                 Z    =         2817488
13
 XDOT =      11333
310884                 XDOT =        3454
393157
 YDOT =      13281
567314  feet/sec       YDOT =        4048
221717  meter/sec
 ZDOT =      16726
468990                 ZDOT =        5098
227748


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
59045550  
00016717  00000-0  10270-3 0  9009
2 25544  51
6394  76
6927 0003283 245
1282 114
9529 15
54333632 15627


Satellite: ISS
Catalog Number: 25544
Epoch time:      16237
59045550   =   yrday
fracday
Element set:     900
Inclination:       51
6394  deg
RA of node:        76
6927  deg
Eccentricity:     
0003283     
Arg of perigee:   245
1282  deg
Mean anomaly:     114
9529  deg
Mean motion:   15
54333632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1562
Checksum:              310


Coasting Arc #2 (Orbit 1576)
---------------------------------------

Vector Time (GMT): 2016/238/12:45:53
942
Vector Time (MET): N/A
Weight (LBS)     : 929160
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1717400
95                 A    =         6781441
82  meter
 Y    =       -5072165
81  meter          E    =           
0004626
 Z    =       -4165513
13                 I    =           51
98730
 XDOT =       4719
657512                 Wp   =           71
61083
 YDOT =       4704
308941  meter/sec      RA   =           71
25957  deg
 ZDOT =      -3784
379628                 TA   =          159
58515
                                          MA   =          159
56665
                                          Ha   =            219
741  n
mi
                                          Hp   =            215
450

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5634517
54                 X    =         1794225
71
 Y    =      -16640963
95  feet           Y    =        -5052531
26  meter
 Z    =      -13666381
66                 Z    =        -4156983
72
 XDOT =      15484
440656                 XDOT =        4685
084753
 YDOT =      15434
084452  feet/sec       YDOT =        4756
893888  meter/sec
 ZDOT =     -12415
943663                 ZDOT =       -3761
536948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9877222
49                 X    =        -3010577
42
 Y    =       14565472
54  feet           Y    =         4439556
03  meter
 Z    =      -13628167
24                 Z    =        -4153865
37
 XDOT =      -9922
805864                 XDOT =       -3024
471227
 YDOT =     -18247
043675  feet/sec       YDOT =       -5561
698912  meter/sec
 ZDOT =     -12316
945010                 ZDOT =       -3754
204839


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
55487386  
00016717  00000-0  10270-3 0  9014
2 25544  51
6392  71
8837 0003054 248
8520 111
2307 15
54326230 15779


Satellite: ISS
Catalog Number: 25544
Epoch time:      16238
55487386   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:        71
8837  deg
Eccentricity:     
0003054     
Arg of perigee:   248
8520  deg
Mean anomaly:     111
2307  deg
Mean motion:   15
54326230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1577
Checksum:              307


Coasting Arc #3 (Orbit 1590)
---------------------------------------

Vector Time (GMT): 2016/239/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2378347
01                 A    =         6788779
15  meter
 Y    =       -6339796
24  meter          E    =           
0010157
 Z    =        -396250
67                 I    =           52
00553
 XDOT =       4550
371934                 Wp   =          154
11653
 YDOT =      -1334
499105  meter/sec      RA   =           66
81665  deg
 ZDOT =      -6027
530892                 TA   =           30
13472
                                          MA   =           30
07632
                                          Ha   =            219
639  n
mi
                                          Hp   =            215
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7802975
75                 X    =        -2305352
24
 Y    =      -20799856
43  feet           Y    =        -6365984
38  meter
 Z    =       -1300035
02                 Z    =         -407626
55
 XDOT =      14929
041779                 XDOT =        4594
235362
 YDOT =      -4378
277902  feet/sec       YDOT =       -1283
368686  meter/sec
 ZDOT =     -19775
363820                 ZDOT =       -6005
319934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12006208
66                 X    =        -3659492
40
 Y    =       18688038
66  feet           Y    =         5696114
18  meter
 Z    =       -1348596
93                 Z    =         -411052
34
 XDOT =     -11153
627385                 XDOT =       -3399
625627
 YDOT =      -8570
467428  feet/sec       YDOT =       -2612
278472  meter/sec
 ZDOT =     -19678
018449                 ZDOT =       -5997
860023


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
45499254  
00016717  00000-0  10270-3 0  9022
2 25544  51
6432  67
3988 0003247 255
4663 104
6130 15
54293111 15914


Satellite: ISS
Catalog Number: 25544
Epoch time:      16239
45499254   =   yrday
fracday
Element set:     902
Inclination:       51
6432  deg
RA of node:        67
3988  deg
Eccentricity:     
0003247     
Arg of perigee:   255
4663  deg
Mean anomaly:     104
6130  deg
Mean motion:   15
54293111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1591
Checksum:              310


Coasting Arc #4 (Orbit 1606)
---------------------------------------

Vector Time (GMT): 2016/240/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1474212
07                 A    =         6786762
03  meter
 Y    =        6270803
78  meter          E    =           
0010744
 Z    =        2119372
96                 I    =           51
98449
 XDOT =      -5259
543331                 Wp   =           66
61523
 YDOT =       -643
695781  meter/sec      RA   =           61
86706  deg
 ZDOT =       5544
997959                 TA   =          316
75582
                                          MA   =          316
84012
                                          Ha   =            219
497  n
mi
                                          Hp   =            215
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4836653
78                 X    =         1393685
91
 Y    =       20573503
23  feet           Y    =         6286839
21  meter
 Z    =        6953323
36                 Z    =         2126338
49
 XDOT =     -17255
719589                 XDOT =       -5278
889356
 YDOT =      -2111
862800  feet/sec       YDOT =        -702
619547  meter/sec
 ZDOT =      18192
250522                 ZDOT =        5519
401744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13341643
04                 X    =         4066532
80
 Y    =      -16378482
90  feet           Y    =        -4992161
59  meter
 Z    =        6982608
37                 Z    =         2128299
03
 XDOT =       7766
396090                 XDOT =        2367
197528
 YDOT =      14059
732023  feet/sec       YDOT =        4285
406321  meter/sec
 ZDOT =      18080
469732                 ZDOT =        5510
927174


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
48369323  
00016717  00000-0  10270-3 0  9031
2 25544  51
6419  62
2683 0003240 261
0262  99
0524 15
54351666 16078


Satellite: ISS
Catalog Number: 25544
Epoch time:      16240
48369323   =   yrday
fracday
Element set:     903
Inclination:       51
6419  deg
RA of node:        62
2683  deg
Eccentricity:     
0003240     
Arg of perigee:   261
0262  deg
Mean anomaly:      99
0524  deg
Mean motion:   15
54351666  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1607
Checksum:              293


Coasting Arc #5 (Orbit 1621)
---------------------------------------

Vector Time (GMT): 2016/241/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -342515
97                 A    =         6783159
71  meter
 Y    =       -5723620
72  meter          E    =           
0002225
 Z    =       -3626460
91                 I    =           51
95493
 XDOT =       5746
215178                 Wp   =           76
03653
 YDOT =       2463
797424  meter/sec      RA   =           56
90978  deg
 ZDOT =      -4433
072406                 TA   =          146
70895
                                          MA   =          146
69495
                                          Ha   =            219
506  n
mi
                                          Hp   =            215
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1123740
06                 X    =         -260872
02
 Y    =      -18778283
21  feet           Y    =        -5726994
59  meter
 Z    =      -11897837
63                 Z    =        -3627926
24
 XDOT =      18852
412002                 XDOT =        5739
770933
 YDOT =       8083
324881  feet/sec       YDOT =        2528
019261  meter/sec
 ZDOT =     -14544
200808                 ZDOT =       -4405
174892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13999345
76                 X    =        -4267000
59
 Y    =       12560973
67  feet           Y    =         3828584
78  meter
 Z    =      -11903172
32                 Z    =        -3628086
92
 XDOT =      -4625
859498                 XDOT =       -1409
961975
 YDOT =     -18817
531640  feet/sec       YDOT =       -5735
583644  meter/sec
 ZDOT =     -14422
699566                 ZDOT =       -4396
038828


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
44809921  
00016717  00000-0  10270-3 0  9042
2 25544  51
6405  57
4598 0003236 265
0647  95
0137 15
54331070 16220


Satellite: ISS
Catalog Number: 25544
Epoch time:      16241
44809921   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:        57
4598  deg
Eccentricity:     
0003236     
Arg of perigee:   265
0647  deg
Mean anomaly:      95
0137  deg
Mean motion:   15
54331070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1622
Checksum:              296


Coasting Arc #6 (Orbit 1637)
---------------------------------------

Vector Time (GMT): 2016/242/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -941113
27                 A    =         6779418
24  meter
 Y    =        4782978
09  meter          E    =           
0005253
 Z    =        4709746
07                 I    =           51
92416
 XDOT =      -5922
996006                 Wp   =          132
35157
 YDOT =      -3962
160959  meter/sec      RA   =           51
93882  deg
 ZDOT =       2834
760433                 TA   =          289
61481
                                          MA   =          289
67150
                                          Ha   =            219
583  n
mi
                                          Hp   =            215
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3087641
96                 X    =        -1017405
32
 Y    =       15692185
33  feet           Y    =         4772027
59  meter
 Z    =       15451922
82                 Z    =         4704988
92
 XDOT =     -19432
401593                 XDOT =       -5892
019719
 YDOT =     -12999
215746  feet/sec       YDOT =       -4028
222524  meter/sec
 ZDOT =       9300
395120                 ZDOT =        2806
063932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14111311
53                 X    =         4301127
75
 Y    =       -7570940
49  feet           Y    =        -2307622
66  meter
 Z    =       15430226
15                 Z    =         4703132
93
 XDOT =       1896
041717                 XDOT =         577
913515
 YDOT =      22271
387804  feet/sec       YDOT =        6788
319003  meter/sec
 ZDOT =       9175
685326                 ZDOT =        2796
748887


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
47679482  
00016717  00000-0  10270-3 0  9054
2 25544  51
6409  52
3292 0003209 270
3205  89
7580 15
54308455 16388


Satellite: ISS
Catalog Number: 25544
Epoch time:      16242
47679482   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:        52
3292  deg
Eccentricity:     
0003209     
Arg of perigee:   270
3205  deg
Mean anomaly:      89
7580  deg
Mean motion:   15
54308455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1638
Checksum:              316


Coasting Arc #7 (Orbit 1652)
---------------------------------------

Vector Time (GMT): 2016/243/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2327530
99                 A    =         6776956
30  meter
 Y    =       -3572062
75  meter          E    =           
0011421
 Z    =       -5277789
27                 I    =           51
89434
 XDOT =       5689
342799                 Wp   =           80
41923
 YDOT =       5048
768390  meter/sec      RA   =           46
95703  deg
 ZDOT =       -907
850618                 TA   =          180
91745
                                          MA   =          180
91954
                                          Ha   =            219
507  n
mi
                                          Hp   =            215
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7636256
54                 X    =         2392938
50
 Y    =      -11719365
98  feet           Y    =        -3545669
39  meter
 Z    =      -17315581
61                 Z    =        -5266323
80
 XDOT =      18665
822832                 XDOT =        5636
873219
 YDOT =      16564
200754  feet/sec       YDOT =        5112
096993  meter/sec
 ZDOT =      -2978
512525                 ZDOT =        -880
341489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13939124
08                 X    =        -4248645
02
 Y    =        1764472
28  feet           Y    =          537811
15  meter
 Z    =      -17264784
29                 Z    =        -5262306
25
 XDOT =        510
378394                 XDOT =         155
563334
 YDOT =     -23950
250361  feet/sec       YDOT =       -7300
036310  meter/sec
 ZDOT =      -2859
203869                 ZDOT =        -871
485339


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
44118971  
00016717  00000-0  10270-3 0  9064
2 25544  51
6396  47
5191 0003115 272
6745  87
4051 15
54351949 16538


Satellite: ISS
Catalog Number: 25544
Epoch time:      16243
44118971   =   yrday
fracday
Element set:     906
Inclination:       51
6396  deg
RA of node:        47
5191  deg
Eccentricity:     
0003115     
Arg of perigee:   272
6745  deg
Mean anomaly:      87
4051  deg
Mean motion:   15
54351949  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1653
Checksum:              316


Coasting Arc #8 (Orbit 1668)
---------------------------------------

Vector Time (GMT): 2016/244/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3685666
84                 A    =         6777212
28  meter
 Y    =        2215112
72  meter          E    =           
0002465
 Z    =        5238614
59                 I    =           51
87208
 XDOT =      -5015
238442                 Wp   =            2
20731
 YDOT =      -5692
605768  meter/sec      RA   =           41
97175  deg
 ZDOT =      -1119
009738                 TA   =           98
49668
                                          MA   =           98
46874
                                          Ha   =            219
664  n
mi
                                          Hp   =            215
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12092082
81                 X    =        -3735609
39
 Y    =        7267430
17  feet           Y    =         2173618
33  meter
 Z    =       17187055
73                 Z    =         5220589
34
 XDOT =     -16454
194362                 XDOT =       -4945
773960
 YDOT =     -18676
528110  feet/sec       YDOT =       -5748
301221  meter/sec
 ZDOT =      -3671
291790                 ZDOT =       -1143
202892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13542586
38                 X    =         4127780
33
 Y    =        4283582
72  feet           Y    =         1305636
01  meter
 Z    =       17107839
31                 Z    =         5214469
42
 XDOT =      -2717
076504                 XDOT =        -828
164918
 YDOT =      23702
458992  feet/sec       YDOT =        7224
509501  meter/sec
 ZDOT =      -3775
975379                 ZDOT =       -1150
917296


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   16244
46987552  
00016717  00000-0  10270-3 0  9077
2 25544  51
6395  42
3895 0003168 275
3568  84
7224 15
54326081 16690


Satellite: ISS
Catalog Number: 25544
Epoch time:      16244
46987552   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:        42
3895  deg
Eccentricity:     
0003168     
Arg of perigee:   275
3568  deg
Mean anomaly:      84
7224  deg
Mean motion:   15
54326081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1669
Checksum:              341


Coasting Arc #9 (Orbit 1683)
---------------------------------------

Vector Time (GMT): 2016/245/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4894913
27                 A    =         6779727
40  meter
 Y    =        -854801
14  meter          E    =           
0007085
 Z    =       -4619389
26                 I    =           51
85621
 XDOT =       3873
258753                 Wp   =          115
14609
 YDOT =       5882
999631  meter/sec      RA   =           36
98753  deg
 ZDOT =       3016
331722                 TA   =          184
88660
                                          MA   =          184
89352
                                          Ha   =            219
529  n
mi
                                          Hp   =            215
553

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16059426
75                 X    =         4926546
77
 Y    =       -2804465
68  feet           Y    =         -799886
55  meter
 Z    =      -15155476
58                 Z    =        -4595534
41
 XDOT =      12707
541842                 XDOT =        3792
533856
 YDOT =      19301
179891  feet/sec       YDOT =        5925
861957  meter/sec
 ZDOT =       9896
101450                 ZDOT =        3034
950099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13010811
94                 X    =        -3965695
48
 Y    =       -9982168
33  feet           Y    =        -3042564
91  meter
 Z    =      -15051038
95                 Z    =        -4587556
67
 XDOT =       4901
961787                 XDOT =        1494
117953
 YDOT =     -21428
156288  feet/sec       YDOT =       -6531
302037  meter/sec
 ZDOT =       9976
371315                 ZDOT =        3040
797977


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   16245
43426353  
00016717  00000-0  10270-3 0  9083
2 25544  51
6395  37
5792 0003109 277
6832  82
3967 15
54364460 16844


Satellite: ISS
Catalog Number: 25544
Epoch time:      16245
43426353   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:        37
5792  deg
Eccentricity:     
0003109     
Arg of perigee:   277
6832  deg
Mean anomaly:      82
3967  deg
Mean motion:   15
54364460  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1684
Checksum:              331


Coasting Arc #10 (Orbit 1699)
---------------------------------------

Vector Time (GMT): 2016/246/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5814947
32                 A    =         6783649
22  meter
 Y    =        -429463
61  meter          E    =           
0009243
 Z    =        3459853
97                 I    =           51
84371
 XDOT =      -2314
349246                 Wp   =           84
88525
 YDOT =      -5695
626852  meter/sec      RA   =           32
01242  deg
 ZDOT =      -4585
367521                 TA   =           54
65094
                                          MA   =           54
56459
                                          Ha   =            219
569  n
mi
                                          Hp   =            215
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19077911
15                 X    =        -5826519
07
 Y    =       -1409001
33  feet           Y    =         -494554
54  meter
 Z    =       11351226
93                 Z    =         3431578
66
 XDOT =      -7593
009337                 XDOT =       -2228
213793
 YDOT =     -18686
439803  feet/sec       YDOT =       -5721
026371  meter/sec
 ZDOT =     -15043
856695                 ZDOT =       -4596
400061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12197017
81                 X    =         3717651
03
 Y    =       14831500
86  feet           Y    =         4520641
46  meter
 Z    =       11227718
83                 Z    =         3422208
70
 XDOT =      -7270
457882                 XDOT =       -2216
035562
 YDOT =      17431
621501  feet/sec       YDOT =        5313
158234  meter/sec
 ZDOT =     -15090
996021                 ZDOT =       -4599
735587


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   16246
46293813  
00016717  00000-0  10270-3 0  9091
2 25544  51
6402  32
4493 0003263 282
7938  77
2850 15
54373554 17007


Satellite: ISS
Catalog Number: 25544
Epoch time:      16246
46293813   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:        32
4493  deg
Eccentricity:     
0003263     
Arg of perigee:   282
7938  deg
Mean anomaly:      77
2850  deg
Mean motion:   15
54373554  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1700
Checksum:              312


Coasting Arc #11 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2016/246/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         425244
16                 A    =         6777498
81  meter
 Y    =       -4416962
88  meter          E    =           
0011001
 Z    =       -5132734
19                 I    =           51
81595
 XDOT =       7026
364300                 Wp   =           70
16741
 YDOT =       2577
053386  meter/sec      RA   =           30
03341  deg
 ZDOT =      -1634
754630                 TA   =          184
07507
                                          MA   =          184
08403
                                          Ha   =            219
605  n
mi
                                          Hp   =            215
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1395158
01                 X    =          499536
54
 Y    =      -14491348
04  feet           Y    =        -4411792
73  meter
 Z    =      -16839679
12                 Z    =        -5130487
52
 XDOT =      23052
376312                 XDOT =        7004
965682
 YDOT =       8454
899559  feet/sec       YDOT =        2655
507058  meter/sec
 ZDOT =      -5363
368210                 ZDOT =       -1600
674914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14528443
18                 X    =         4428269
48
 Y    =       -1108562
33  feet           Y    =         -337889
80  meter
 Z    =      -16829018
24                 Z    =        -5129484
76
 XDOT =      -4276
067876                 XDOT =       -1303
345489
 YDOT =      23165
926343  feet/sec       YDOT =        7060
974349  meter/sec
 ZDOT =      -5214
902977                 ZDOT =       -1589
502428


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   16246
84869088  
00016717  00000-0  10270-3 0  9108
2 25544  51
6440  30
5288 0003011 286
0928  73
9893 15
54366304 17068


Satellite: ISS
Catalog Number: 25544
Epoch time:      16246
84869088   =   yrday
fracday
Element set:     910
Inclination:       51
6440  deg
RA of node:        30
5288  deg
Eccentricity:     
0003011     
Arg of perigee:   286
0928  deg
Mean anomaly:      73
9893  deg
Mean motion:   15
54366304  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1706
Checksum:              320


Coasting Arc #12 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2016/247/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2168082
10                 A    =         6776666
07  meter
 Y    =        3604793
06  meter          E    =           
0001948
 Z    =        5313259
16                 I    =           51
78317
 XDOT =      -6804
224267                 Wp   =          355
23449
 YDOT =      -3516
775532  meter/sec      RA   =           25
04260  deg
 ZDOT =       -388
623310                 TA   =           98
47450
                                          MA   =           98
45242
                                          Ha   =            219
769  n
mi
                                          Hp   =            215
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7113130
24                 X    =        -2234040
05
 Y    =       11826748
89  feet           Y    =         3580179
96  meter
 Z    =       17431952
64                 Z    =         5302566
59
 XDOT =     -22323
570429                 XDOT =       -6762
505332
 YDOT =     -11537
977466  feet/sec       YDOT =       -3592
631708  meter/sec
 ZDOT =      -1275
010861                 ZDOT =        -421
574581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13012671
42                 X    =        -3966262
25
 Y    =       -4773887
41  feet           Y    =        -1455080
88  meter
 Z    =       17384532
36                 Z    =         5298805
46
 XDOT =       6604
818890                 XDOT =        2013
148798
 YDOT =     -23191
054021  feet/sec       YDOT =       -7068
633266  meter/sec
 ZDOT =      -1418
351067                 ZDOT =        -432
313405


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   16247
87735989  
00016717  00000-0  10270-3 0  9115
2 25544  51
6423  25
3995 0002884 292
1040  67
9806 15
54383644 17227


Satellite: ISS
Catalog Number: 25544
Epoch time:      16247
87735989   =   yrday
fracday
Element set:     911
Inclination:       51
6423  deg
RA of node:        25
3995  deg
Eccentricity:     
0002884     
Arg of perigee:   292
1040  deg
Mean anomaly:      67
9806  deg
Mean motion:   15
54383644  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1722
Checksum:              336


Coasting Arc #13 (Orbit 1736)
---------------------------------------

Vector Time (GMT): 2016/248/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3828568
42                 A    =         6778563
71  meter
 Y    =       -2713097
62  meter          E    =           
0008784
 Z    =       -4899979
17                 I    =           51
76081
 XDOT =       5978
561512                 Wp   =          103
87740
 YDOT =       4166
696535  meter/sec      RA   =           20
05171  deg
 ZDOT =       2365
731286                 TA   =          189
26367
                                          MA   =          189
27988
                                          Ha   =            219
715  n
mi
                                          Hp   =            215
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12560920
00                 X    =         3882424
35
 Y    =       -8901238
91  feet           Y    =        -2669983
45  meter
 Z    =      -16076047
16                 Z    =        -4881249
87
 XDOT =      19614
703125                 XDOT =        5920
032439
 YDOT =      13670
264222  feet/sec       YDOT =        4233
225837  meter/sec
 ZDOT =       7761
585583                 ZDOT =        2394
630917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11388839
59                 X    =         3471318
31
 Y    =       10485450
13  feet           Y    =         3195965
20  meter
 Z    =      -15993677
69                 Z    =        -4874872
96
 XDOT =      -8440
374891                 XDOT =       -2572
626267
 YDOT =      21190
346085  feet/sec       YDOT =        6458
817487  meter/sec
 ZDOT =       7887
080797                 ZDOT =        2403
982227


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   16248
84173150  
00016717  00000-0  10270-3 0  9120
2 25544  51
6434  20
5912 0003140 295
7000  64
3829 15
54369249 17373


Satellite: ISS
Catalog Number: 25544
Epoch time:      16248
84173150   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:        20
5912  deg
Eccentricity:     
0003140     
Arg of perigee:   295
7000  deg
Mean anomaly:      64
3829  deg
Mean motion:   15
54369249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1737
Checksum:              297


Coasting Arc #14 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2016/249/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5246245
96                 A    =         6782096
17  meter
 Y    =        1779206
45  meter          E    =           
0009163
 Z    =        3907978
21                 I    =           51
74166
 XDOT =      -4603
335575                 Wp   =           67
90584
 YDOT =      -4575
585529  meter/sec      RA   =           15
06611  deg
 ZDOT =      -4085
541950                 TA   =           64
86191
                                          MA   =           64
76689
                                          Ha   =            219
819  n
mi
                                          Hp   =            215
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17212093
04                 X    =        -5284734
86
 Y    =        5837291
50  feet           Y    =         1720324
64  meter
 Z    =       12821450
82                 Z    =         3882399
58
 XDOT =     -15102
807005                 XDOT =       -4531
982281
 YDOT =     -15011
763545  feet/sec       YDOT =       -4626
664599  meter/sec
 ZDOT =     -13404
009023                 ZDOT =       -4107
729990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9645609
72                 X    =        -2939981
84
 Y    =      -15496926
22  feet           Y    =        -4723463
11  meter
 Z    =       12709335
57                 Z    =         3873805
48
 XDOT =      10043
173361                 XDOT =        3061
159240
 YDOT =     -17352
710304  feet/sec       YDOT =       -5289
106101  meter/sec
 ZDOT =     -13500
084457                 ZDOT =       -4114
825743


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   16249
87038792  
00016717  00000-0  10270-3 0  9137
2 25544  51
6425  15
4614 0003119 302
9833  57
1020 15
54426654 17531


Satellite: ISS
Catalog Number: 25544
Epoch time:      16249
87038792   =   yrday
fracday
Element set:     913
Inclination:       51
6425  deg
RA of node:        15
4614  deg
Eccentricity:     
0003119     
Arg of perigee:   302
9833  deg
Mean anomaly:      57
1020  deg
Mean motion:   15
54426654  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1753
Checksum:              302


Coasting Arc #15 (Orbit 1767)
---------------------------------------

Vector Time (GMT): 2016/250/19:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6250178
28                 A    =         6785953
62  meter
 Y    =        -879206
96  meter          E    =           
0005707
 Z    =       -2484667
16                 I    =           51
72233
 XDOT =       2783
475662                 Wp   =           16
10781
 YDOT =       4763
163679  meter/sec      RA   =           10
09088  deg
 ZDOT =       5324
653610                 TA   =          316
07756
                                          MA   =          316
12291
                                          Ha   =            219
902  n
mi
                                          Hp   =            215
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20505834
25                 X    =         6271614
73
 Y    =       -2884537
28  feet           Y    =         -809193
67  meter
 Z    =       -8151795
15                 Z    =        -2454253
16
 XDOT =       9132
137999                 XDOT =        2704
140964
 YDOT =      15627
177423  feet/sec       YDOT =        4793
847313  meter/sec
 ZDOT =      17469
335992                 ZDOT =        5337
981888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7850450
73                 X    =         2392817
38
 Y    =       19218009
98  feet           Y    =         5857649
44  meter
 Z    =       -8018732
67                 Z    =        -2444109
72
 XDOT =     -11530
646351                 XDOT =       -3514
541008
 YDOT =      12011
691012  feet/sec       YDOT =        3661
163420  meter/sec
 ZDOT =      17526
652729                 ZDOT =        5342
123752


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   16250
83474979  
00016717  00000-0  10270-3 0  9147
2 25544  51
6417  10
6535 0003017 306
7399  53
3477 15
54416941 17685


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
83474979   =   yrday
fracday
Element set:     914
Inclination:       51
6417  deg
RA of node:        10
6535  deg
Eccentricity:     
0003017     
Arg of perigee:   306
7399  deg
Mean anomaly:      53
3477  deg
Mean motion:   15
54416941  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1768
Checksum:              326


Coasting Arc #16 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2016/250/21:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909722
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2231785
18                 A    =         6778724
97  meter
 Y    =       -4240792
71  meter          E    =           
0010053
 Z    =       -4803902
21                 I    =           51
69534
 XDOT =       7160
692118                 Wp   =           56
53101
 YDOT =       -830
233047  meter/sec      RA   =            9
88842  deg
 ZDOT =      -2592
283512                 TA   =          187
91585
                                          MA   =          187
93173
                                          Ha   =            219
855  n
mi
                                          Hp   =            215
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7322129
85                 X    =        -2160862
36
 Y    =      -13913361
91  feet           Y    =        -4265353
95  meter
 Z    =      -15760834
02                 Z    =        -4814571
00
 XDOT =      23493
084378                 XDOT =        7182
036016
 YDOT =      -2723
861703  feet/sec       YDOT =        -750
038307  meter/sec
 ZDOT =      -8504
867166                 ZDOT =       -2557
446684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8026446
24                 X    =         2446460
81
 Y    =      -13465722
80  feet           Y    =        -4104352
31  meter
 Z    =      -15806631
03                 Z    =        -4817861
14
 XDOT =      13735
294208                 XDOT =        4186
517675
 YDOT =      17997
389401  feet/sec       YDOT =        5485
604290  meter/sec
 ZDOT =      -8352
489231                 ZDOT =       -2545
838718


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   16250
89904110  
00016717  00000-0  10270-3 0  9159
2 25544  51
6404  10
3319 0003150 307
2860  52
8005 15
54395823 17692


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
89904110   =   yrday
fracday
Element set:     915
Inclination:       51
6404  deg
RA of node:        10
3319  deg
Eccentricity:     
0003150     
Arg of perigee:   307
2860  deg
Mean anomaly:      52
8005  deg
Mean motion:   15
54395823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1769
Checksum:              285


Coasting Arc #17 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2016/250/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894613
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1935081
29                 A    =         6778228
10  meter
 Y    =        4260384
02  meter          E    =           
0003311
 Z    =        4901980
93                 I    =           51
69314
 XDOT =      -7280
706669                 Wp   =          117
22075
 YDOT =        621
012227  meter/sec      RA   =            9
72466  deg
 ZDOT =       2331
674344                 TA   =          309
97189
                                          MA   =          310
00096
                                          Ha   =            219
733  n
mi
                                          Hp   =            215
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6348691
91                 X    =         1863485
02
 Y    =       13977637
85  feet           Y    =         4281623
56  meter
 Z    =       16082614
59                 Z    =         4911206
76
 XDOT =     -23886
832904                 XDOT =       -7298
436158
 YDOT =       2037
441688  feet/sec       YDOT =         539
495586  meter/sec
 ZDOT =       7649
850210                 ZDOT =        2296
263313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5826588
80                 X    =        -1775944
27
 Y    =       14158368
80  feet           Y    =         4315470
81  meter
 Z    =       16122102
75                 Z    =         4914016
92
 XDOT =     -16939
192794                 XDOT =       -5163
065964
 YDOT =     -15515
549031  feet/sec       YDOT =       -4729
139345  meter/sec
 ZDOT =       7495
004100                 ZDOT =        2284
477250


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   16250
96333132  
00016717  00000-0  10270-3 0  9168
2 25544  51
6407  10
0117 0003319 305
9294  54
1551 15
54419779 17701


Satellite: ISS
Catalog Number: 25544
Epoch time:      16250
96333132   =   yrday
fracday
Element set:     916
Inclination:       51
6407  deg
RA of node:        10
0117  deg
Eccentricity:     
0003319     
Arg of perigee:   305
9294  deg
Mean anomaly:      54
1551  deg
Mean motion:   15
54419779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1770
Checksum:              293


Coasting Arc #18 (Orbit 1784)
---------------------------------------

Vector Time (GMT): 2016/251/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 894613
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -34050
97                 A    =         6776568
60  meter
 Y    =       -4219808
70  meter          E    =           
0012632
 Z    =       -5313039
15                 I    =           51
65570
 XDOT =       7643
807501                 Wp   =           77
14331
 YDOT =        364
716405  meter/sec      RA   =            4
72557  deg
 ZDOT =       -336
589501                 TA   =          189
63278
                                          MA   =          189
65702
                                          Ha   =            219
887  n
mi
                                          Hp   =            215
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -111715
78                 X    =           38947
05
 Y    =      -13844516
73  feet           Y    =        -4219781
79  meter
 Z    =      -17431230
79                 Z    =        -5313026
88
 XDOT =      25078
108599                 XDOT =        7640
796055
 YDOT =       1196
576132  feet/sec       YDOT =         450
177713  meter/sec
 ZDOT =      -1104
296264                 ZDOT =        -299
465065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9868579
03                 X    =         3007942
89
 Y    =       -9712088
01  feet           Y    =        -2960244
43  meter
 Z    =      -17430359
30                 Z    =        -5312773
51
 XDOT =      16035
662457                 XDOT =        4887
669917
 YDOT =      17997
145993  feet/sec       YDOT =        5485
530099  meter/sec
 ZDOT =       -942
164619                 ZDOT =        -287
171776


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   16251
92768699  
00016717  00000-0  10270-3 0  9176
2 25544  51
6410   5
2022 0003275 310
6319  49
4548 15
54408271 17852


Satellite: ISS
Catalog Number: 25544
Epoch time:      16251
92768699   =   yrday
fracday
Element set:     917
Inclination:       51
6410  deg
RA of node:         5
2022  deg
Eccentricity:     
0003275     
Arg of perigee:   310
6319  deg
Mean anomaly:      49
4548  deg
Mean motion:   15
54408271  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1785
Checksum:              312
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