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

 
Date: January 17th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


027/19:27:44 236 2 4 2 8 2 8
N/A 1 5 -0 2 222 4
000/00:09:28 472 -0 3 0 0 213 1

Coasting Arc #1 (Orbit 2107)
---------------------------------------

Vector Time (GMT): 2016/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4340506
17                 A    =         6777243
75  meter
 Y    =         952483
32  meter          E    =           
0006777
 Z    =        5110963
76                 I    =           51
98175
 XDOT =        405
653687                 Wp   =           67
02993
 YDOT =      -7464
220375  meter/sec      RA   =          103
57319  deg
 ZDOT =       1736
295079                 TA   =            6
28471
                                          MA   =            6
27621
                                          Ha   =            222
021  n
mi
                                          Hp   =            213
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14240505
82                 X    =        -4375661
12
 Y    =        3124945
27  feet           Y    =          903748
36  meter
 Z    =       16768253
80                 Z    =         5089793
47
 XDOT =       1330
884799                 XDOT =         480
656191
 YDOT =     -24488
911991  feet/sec       YDOT =       -7459
264715  meter/sec
 ZDOT =       5696
506165                 ZDOT =        1738
447828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8595979
95                 X    =        -2620054
69
 Y    =      -11905567
47  feet           Y    =        -3628816
96  meter
 Z    =       16676277
05                 Z    =         5082929
25
 XDOT =      22099
755929                 XDOT =        6736
005607
 YDOT =      -7965
631913  feet/sec       YDOT =       -2427
924607  meter/sec
 ZDOT =       5707
219262                 ZDOT =        1739
560431


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   16015
55124352  
00016717  00000-0  10270-3 0  9007
2 25544  51
6424 104
2216 0005982  18
8944 341
2430 15
54505728 21088


Satellite: ISS
Catalog Number: 25544
Epoch time:      16015
55124352   =   yrday
fracday
Element set:     900
Inclination:       51
6424  deg
RA of node:       104
2216  deg
Eccentricity:     
0005982     
Arg of perigee:    18
8944  deg
Mean anomaly:     341
2430  deg
Mean motion:   15
54505728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2108
Checksum:              279


Coasting Arc #2 (Orbit 2122)
---------------------------------------

Vector Time (GMT): 2016/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4073262
44                 A    =         6776335
07  meter
 Y    =         982899
21  meter          E    =           
0017847
 Z    =       -5340014
80                 I    =           51
98451
 XDOT =      -1394
708406                 Wp   =           73
56522
 YDOT =       7521
513746  meter/sec      RA   =           98
59366  deg
 ZDOT =        326
383807                 TA   =          199
50216
                                          MA   =          199
57052
                                          Ha   =            222
029  n
mi
                                          Hp   =            213
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13363721
92                 X    =         4087908
03
 Y    =        3224734
95  feet           Y    =         1028531
02  meter
 Z    =      -17519733
60                 Z    =        -5320192
46
 XDOT =      -4575
814981                 XDOT =       -1480
297590
 YDOT =      24676
882370  feet/sec       YDOT =        7505
438637  meter/sec
 ZDOT =       1070
813014                 ZDOT =         319
400816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2660729
00                 X    =          810990
20
 Y    =       13598039
72  feet           Y    =         4144682
51  meter
 Z    =      -17433957
71                 Z    =        -5313870
31
 XDOT =     -23361
517320                 XDOT =       -7120
590479
 YDOT =       5878
857117  feet/sec       YDOT =        1791
875649  meter/sec
 ZDOT =       1039
129447                 ZDOT =         316
726655


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   16016
51555041  
00016717  00000-0  10270-3 0  9018
2 25544  51
6418  99
4123 0006149  21
9837 338
1579 15
54491176 21232


Satellite: ISS
Catalog Number: 25544
Epoch time:      16016
51555041   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:        99
4123  deg
Eccentricity:     
0006149     
Arg of perigee:    21
9837  deg
Mean anomaly:     338
1579  deg
Mean motion:   15
54491176  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2123
Checksum:              304


Coasting Arc #3 (Orbit 2138)
---------------------------------------

Vector Time (GMT): 2016/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3658948
37                 A    =         6777936
61  meter
 Y    =       -2903792
80  meter          E    =           
0012471
 Z    =        4907313
78                 I    =           51
99496
 XDOT =       2295
766434                 Wp   =           42
90405
 YDOT =      -6924
903480  meter/sec      RA   =           93
61395  deg
 ZDOT =      -2373
477408                 TA   =           70
28119
                                          MA   =           70
14670
                                          Ha   =            222
080  n
mi
                                          Hp   =            212
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12004423
77                 X    =        -3650043
02
 Y    =       -9526879
25  feet           Y    =        -2944659
85  meter
 Z    =       16100110
83                 Z    =         4889561
19
 XDOT =       7532
042106                 XDOT =        2384
561068
 YDOT =     -22719
499606  feet/sec       YDOT =       -6898
734191  meter/sec
 ZDOT =      -7786
999370                 ZDOT =       -2362
109609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3382996
61                 X    =         1031137
37
 Y    =      -15029254
13  feet           Y    =        -4580916
66  meter
 Z    =       16023671
29                 Z    =         4884015
01
 XDOT =      22674
648198                 XDOT =        6911
232771
 YDOT =      -3188
033403  feet/sec       YDOT =        -971
712581  meter/sec
 ZDOT =      -7736
396276                 ZDOT =       -2358
053585


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   16017
54412672  
00016717  00000-0  10270-3 0  9025
2 25544  51
6423  94
2808 0006223  25
3863 334
7595 15
54561508 21395


Satellite: ISS
Catalog Number: 25544
Epoch time:      16017
54412672   =   yrday
fracday
Element set:     902
Inclination:       51
6423  deg
RA of node:        94
2808  deg
Eccentricity:     
0006223     
Arg of perigee:    25
3863  deg
Mean anomaly:     334
7595  deg
Mean motion:   15
54561508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2139
Checksum:              304


Coasting Arc #4 (Orbit 2153)
---------------------------------------

Vector Time (GMT): 2016/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3165152
05                 A    =         6781608
89  meter
 Y    =        4549469
62  meter          E    =           
0010132
 Z    =       -3913403
96                 I    =           52
00775
 XDOT =      -3083
973413                 Wp   =           68
67272
 YDOT =       5678
521138  meter/sec      RA   =           88
64436  deg
 ZDOT =       4119
302054                 TA   =          244
28113
                                          MA   =          244
38576
                                          Ha   =            222
146  n
mi
                                          Hp   =            212
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10384357
11                 X    =         3133053
07
 Y    =       14926081
44  feet           Y    =         4584685
08  meter
 Z    =      -12839251
83                 Z    =        -3898106
34
 XDOT =     -10118
023007                 XDOT =       -3167
252539
 YDOT =      18630
318694  feet/sec       YDOT =        5643
568349  meter/sec
 ZDOT =      13514
770517                 ZDOT =        4104
118831

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8688468
83                 X    =        -2648245
30
 Y    =       16025302
90  feet           Y    =         4884512
32  meter
 Z    =      -12773775
62                 Z    =        -3893446
81
 XDOT =     -20058
594368                 XDOT =       -6113
859563
 YDOT =       -187
816899  feet/sec       YDOT =         -57
246591  meter/sec
 ZDOT =      13447
840823                 ZDOT =        4098
901883


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   16018
50840464  
00016717  00000-0  10270-3 0  9037
2 25544  51
6415  89
4714 0006316  30
7379 329
4142 15
54572629 21545


Satellite: ISS
Catalog Number: 25544
Epoch time:      16018
50840464   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:        89
4714  deg
Eccentricity:     
0006316     
Arg of perigee:    30
7379  deg
Mean anomaly:     329
4142  deg
Mean motion:   15
54572629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2154
Checksum:              306


Coasting Arc #5 (Orbit 2169)
---------------------------------------

Vector Time (GMT): 2016/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2527692
86                 A    =         6785554
09  meter
 Y    =       -5817700
63  meter          E    =           
0016859
 Z    =        2398408
58                 I    =           52
02010
 XDOT =       3809
124667                 Wp   =           84
60232
 YDOT =      -3894
429776  meter/sec      RA   =           83
68545  deg
 ZDOT =      -5398
025559                 TA   =           68
73755
                                          MA   =           68
55760
                                          Ha   =            222
181  n
mi
                                          Hp   =            212
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8292955
57                 X    =        -2474100
39
 Y    =      -19086944
32  feet           Y    =        -5845667
41  meter
 Z    =        7868794
56                 Z    =         2386259
68
 XDOT =      12497
128174                 XDOT =        3878
611157
 YDOT =     -12777
000578  feet/sec       YDOT =       -3851
444873  meter/sec
 ZDOT =     -17710
057607                 ZDOT =       -5379
353291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13083085
68                 X    =         3987724
52
 Y    =      -16208835
29  feet           Y    =        -4940452
99  meter
 Z    =        7817225
29                 Z    =         2382690
27
 XDOT =      15973
786732                 XDOT =        4868
810196
 YDOT =       4337
318096  feet/sec       YDOT =        1322
014556  meter/sec
 ZDOT =     -17628
324068                 ZDOT =       -5373
113176


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   16019
53695065  
00016717  00000-0  10270-3 0  9047
2 25544  51
6421  84
3400 0006509  33
2010 326
9550 15
54600150 21706


Satellite: ISS
Catalog Number: 25544
Epoch time:      16019
53695065   =   yrday
fracday
Element set:     904
Inclination:       51
6421  deg
RA of node:        84
3400  deg
Eccentricity:     
0006509     
Arg of perigee:    33
2010  deg
Mean anomaly:     326
9550  deg
Mean motion:   15
54600150  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2170
Checksum:              267


Coasting Arc #6 (Orbit 2184)
---------------------------------------

Vector Time (GMT): 2016/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1798506
69                 A    =         6787938
89  meter
 Y    =        6506199
30  meter          E    =           
0017406
 Z    =        -631579
87                 I    =           52
02279
 XDOT =      -4423
199909                 Wp   =           38
97998
 YDOT =       1795
795032  meter/sec      RA   =           78
73628  deg
 ZDOT =       6006
269571                 TA   =          314
23282
                                          MA   =          314
37560
                                          Ha   =            222
378  n
mi
                                          Hp   =            212
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5900612
51                 X    =         1728687
01
 Y    =       21345798
22  feet           Y    =         6525921
04  meter
 Z    =       -2072112
42                 Z    =         -623012
51
 XDOT =     -14511
810725                 XDOT =       -4472
127772
 YDOT =       5891
715984  feet/sec       YDOT =        1746
058007  meter/sec
 ZDOT =      19705
608828                 ZDOT =        5984
664235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15946529
25                 X    =        -4860502
12
 Y    =       15372572
75  feet           Y    =         4685560
18  meter
 Z    =       -2036219
85                 Z    =         -620639
81
 XDOT =     -11036
806392                 XDOT =       -3364
018588
 YDOT =      -8896
543098  feet/sec       YDOT =       -2711
666336  meter/sec
 ZDOT =      19611
550286                 ZDOT =        5977
600527


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   16020
50119910  
00016717  00000-0  10270-3 0  9057
2 25544  51
6417  79
5299 0006673  36
4206 323
7399 15
54550859 21859


Satellite: ISS
Catalog Number: 25544
Epoch time:      16020
50119910   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:        79
5299  deg
Eccentricity:     
0006673     
Arg of perigee:    36
4206  deg
Mean anomaly:     323
7399  deg
Mean motion:   15
54550859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2185
Checksum:              320


Coasting Arc #7 (Orbit 2200)
---------------------------------------

Vector Time (GMT): 2016/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -886949
44                 A    =         6787169
54  meter
 Y    =       -6607963
34  meter          E    =           
0010140
 Z    =       -1271723
06                 I    =           52
01439
 XDOT =       4906
603927                 Wp   =          101
56666
 YDOT =        462
782656  meter/sec      RA   =           73
78928  deg
 ZDOT =      -5868
151429                 TA   =           92
18549
                                          MA   =           92
06938
                                          Ha   =            222
312  n
mi
                                          Hp   =            212
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2909939
10                 X    =         -806814
25
 Y    =      -21679669
75  feet           Y    =        -6617433
67  meter
 Z    =       -4172319
75                 Z    =        -1275837
29
 XDOT =      16097
781914                 XDOT =        4929
568860
 YDOT =       1518
315800  feet/sec       YDOT =         517
780258  meter/sec
 ZDOT =     -19252
465319                 ZDOT =       -5844
260907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17461069
61                 X    =         5322134
02
 Y    =      -13169985
25  feet           Y    =        -4014211
51  meter
 Z    =       -4188867
98                 Z    =        -1276766
96
 XDOT =       5694
429875                 XDOT =        1735
662226
 YDOT =      13597
273091  feet/sec       YDOT =        4144
448838  meter/sec
 ZDOT =     -19148
930269                 ZDOT =       -5836
593946


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   16021
52971515  
00016717  00000-0  10270-3 0  9068
2 25544  51
6422  74
3984 0006707  41
5801 318
5861 15
54631308 22019


Satellite: ISS
Catalog Number: 25544
Epoch time:      16021
52971515   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:        74
3984  deg
Eccentricity:     
0006707     
Arg of perigee:    41
5801  deg
Mean anomaly:     318
5861  deg
Mean motion:   15
54631308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2201
Checksum:              291


Coasting Arc #8 (Orbit 2216)
---------------------------------------

Vector Time (GMT): 2016/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -137190
99                 A    =         6784127
88  meter
 Y    =        6084049
08  meter          E    =           
0019099
 Z    =        2974559
92                 I    =           51
99355
 XDOT =      -5204
731151                 Wp   =           70
05197
 YDOT =      -2580
682381  meter/sec      RA   =           68
83594  deg
 ZDOT =       5018
696802                 TA   =          323
81875
                                          MA   =          323
94780
                                          Ha   =            222
457  n
mi
                                          Hp   =            211
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -450101
66                 X    =         -219662
99
 Y    =       19960790
94  feet           Y    =         6082053
65  meter
 Z    =        9759054
87                 Z    =         2973693
47
 XDOT =     -17075
889602                 XDOT =       -5199
864726
 YDOT =      -8466
805713  feet/sec       YDOT =       -2638
858153  meter/sec
 ZDOT =      16465
540688                 ZDOT =        4993
425675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17470623
01                 X    =        -5325045
89
 Y    =        9670051
80  feet           Y    =         2947431
79  meter
 Z    =        9754093
93                 Z    =         2973047
83
 XDOT =       -699
692711                 XDOT =        -213
266338
 YDOT =     -17827
864728  feet/sec       YDOT =       -5433
933169  meter/sec
 ZDOT =      16356
431595                 ZDOT =        4985
440350


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   16022
55821568  
00016717  00000-0  10270-3 0  9075
2 25544  51
6414  69
2671 0006849  45
8582 314
3133 15
54627419 22177


Satellite: ISS
Catalog Number: 25544
Epoch time:      16022
55821568   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:        69
2671  deg
Eccentricity:     
0006849     
Arg of perigee:    45
8582  deg
Mean anomaly:     314
3133  deg
Mean motion:   15
54627419  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2217
Checksum:              316


Coasting Arc #9 (Orbit 2231)
---------------------------------------

Vector Time (GMT): 2016/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1317266
38                 A    =         6779795
80  meter
 Y    =       -5043209
68  meter          E    =           
0015229
 Z    =       -4351530
53                 I    =           51
96786
 XDOT =       5205
679041                 Wp   =           60
44005
 YDOT =       4383
859111  meter/sec      RA   =           63
86991  deg
 ZDOT =      -3506
749171                 TA   =          174
01197
                                          MA   =          173
99375
                                          Ha   =            222
399  n
mi
                                          Hp   =            211
831

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4321740
09                 X    =         1394700
30
 Y    =      -16545963
52  feet           Y    =        -5028046
03  meter
 Z    =      -14276674
98                 Z    =        -4344943
82
 XDOT =      17078
999478                 XDOT =        5173
304669
 YDOT =      14382
739864  feet/sec       YDOT =        4441
891563  meter/sec
 ZDOT =     -11505
082581                 ZDOT =       -3481
540301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16421479
08                 X    =         5005266
82
 Y    =       -4860548
85  feet           Y    =        -1481495
29  meter
 Z    =      -14247100
92                 Z    =        -4342516
36
 XDOT =      -3684
979746                 XDOT =       -1123
181826
 YDOT =      20937
280577  feet/sec       YDOT =        6381
683120  meter/sec
 ZDOT =     -11396
601030                 ZDOT =       -3473
683994


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   16023
52241963  
00016717  00000-0  10270-3 0  9089
2 25544  51
6422  64
4561 0006808  49
4080 310
7665 15
54664434 22324


Satellite: ISS
Catalog Number: 25544
Epoch time:      16023
52241963   =   yrday
fracday
Element set:     908
Inclination:       51
6422  deg
RA of node:        64
4561  deg
Eccentricity:     
0006808     
Arg of perigee:    49
4080  deg
Mean anomaly:     310
7665  deg
Mean motion:   15
54664434  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2232
Checksum:              297


Coasting Arc #10 (Orbit 2247)
---------------------------------------

Vector Time (GMT): 2016/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2541435
26                 A    =         6776468
77  meter
 Y    =        3588740
92  meter          E    =           
0009551
 Z    =        5147370
58                 I    =           51
94090
 XDOT =      -4882
844441                 Wp   =           81
23489
 YDOT =      -5711
813321  meter/sec      RA   =           58
89112  deg
 ZDOT =       1570
383081                 TA   =          353
70073
                                          MA   =          353
71273
                                          Ha   =            222
547  n
mi
                                          Hp   =            211
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8338042
19                 X    =        -2606379
70
 Y    =       11774084
37  feet           Y    =         3559957
69  meter
 Z    =       16887698
76                 Z    =         5134867
53
 XDOT =     -16019
830842                 XDOT =       -4826
238705
 YDOT =     -18739
545017  feet/sec       YDOT =       -5766
100044  meter/sec
 ZDOT =       5152
175463                 ZDOT =        1546
801382

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14468340
13                 X    =        -4409950
07
 Y    =        -819864
00  feet           Y    =         -249894
55  meter
 Z    =       16832745
96                 Z    =         5130620
97
 XDOT =       7157
776510                 XDOT =        2181
690280
 YDOT =     -22540
384668  feet/sec       YDOT =       -6870
309247  meter/sec
 ZDOT =       5051
019251                 ZDOT =        1539
550668


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   16024
55088821  
00016717  00000-0  10270-3 0  9096
2 25544  51
6410  59
3243 0006930  53
1512 307
0276 15
54697263 22489


Satellite: ISS
Catalog Number: 25544
Epoch time:      16024
55088821   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:        59
3243  deg
Eccentricity:     
0006930     
Arg of perigee:    53
1512  deg
Mean anomaly:     307
0276  deg
Mean motion:   15
54697263  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2248
Checksum:              299


Coasting Arc #11 (Orbit 2262)
---------------------------------------

Vector Time (GMT): 2016/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3750260
63                 A    =         6775832
81  meter
 Y    =       -1931092
43  meter          E    =           
0020513
 Z    =       -5319949
18                 I    =           51
92238
 XDOT =       4122
259245                 Wp   =           82
25707
 YDOT =       6423
732679  meter/sec      RA   =           53
90471  deg
 ZDOT =        578
796537                 TA   =          193
22820
                                          MA   =          193
28207
                                          Ha   =            222
459  n
mi
                                          Hp   =            211
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12304004
70                 X    =         3797417
28
 Y    =       -6335605
07  feet           Y    =        -1888890
89  meter
 Z    =      -17453901
50                 Z    =        -5301617
23
 XDOT =      13524
472587                 XDOT =        4047
309631
 YDOT =      21075
238447  feet/sec       YDOT =        6469
411446  meter/sec
 ZDOT =       1898
938769                 ZDOT =         598
638903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12124391
28                 X    =         3695514
46
 Y    =        6878269
70  feet           Y    =         2096496
60  meter
 Z    =      -17373993
29                 Z    =        -5295593
16
 XDOT =      -9657
968339                 XDOT =       -2943
748750
 YDOT =      21996
687942  feet/sec       YDOT =        6704
590485  meter/sec
 ZDOT =       1983
727508                 ZDOT =         604
640144


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   16025
51506375  
00016717  00000-0  10270-3 0  9104
2 25544  51
6421  54
5132 0006883  55
8990 304
2815 15
54694595 22631


Satellite: ISS
Catalog Number: 25544
Epoch time:      16025
51506375   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        54
5132  deg
Eccentricity:     
0006883     
Arg of perigee:    55
8990  deg
Mean anomaly:     304
2815  deg
Mean motion:   15
54694595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2263
Checksum:              309


Coasting Arc #12 (Orbit 2278)
---------------------------------------

Vector Time (GMT): 2016/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4797752
98                 A    =         6777925
02  meter
 Y    =         193349
35  meter          E    =           
0014682
 Z    =        4775808
32                 I    =           51
90900
 XDOT =      -2940
960964                 Wp   =           60
65132
 YDOT =      -6564
955636  meter/sec      RA   =           48
91879  deg
 ZDOT =      -2675
500496                 TA   =           55
70890
                                          MA   =           55
56999
                                          Ha   =            222
577  n
mi
                                          Hp   =            211
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15740659
37                 X    =        -4822756
79
 Y    =         634348
27  feet           Y    =          139558
02  meter
 Z    =       15668662
48                 Z    =         4752441
82
 XDOT =      -9648
822059                 XDOT =       -2854
335292
 YDOT =     -21538
568359  feet/sec       YDOT =       -6597
359123  meter/sec
 ZDOT =      -8777
888768                 ZDOT =       -2689
576071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9469396
68                 X    =        -2886272
11
 Y    =      -12714894
00  feet           Y    =        -3875499
69  meter
 Z    =       15567264
89                 Z    =         4744902
34
 XDOT =      11433
487952                 XDOT =        3484
927128
 YDOT =     -19388
602303  feet/sec       YDOT =       -5909
645982  meter/sec
 ZDOT =      -8837
628182                 ZDOT =       -2693
709070


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   16026
54350111  
00016717  00000-0  10270-3 0  9114
2 25544  51
6407  49
3807 0007026  59
7946 300
3902 15
54757932 22796


Satellite: ISS
Catalog Number: 25544
Epoch time:      16026
54350111   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:        49
3807  deg
Eccentricity:     
0007026     
Arg of perigee:    59
7946  deg
Mean anomaly:     300
3902  deg
Mean motion:   15
54757932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2279
Checksum:              304


Coasting Arc #13 (Orbit 2293)
---------------------------------------

Vector Time (GMT): 2016/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5552684
15                 A    =         6781949
88  meter
 Y    =        1376789
52  meter          E    =           
0011925
 Z    =       -3650110
17                 I    =           51
90182
 XDOT =       1369
635650                 Wp   =           77
81654
 YDOT =       6117
047138  meter/sec      RA   =           43
94245  deg
 ZDOT =       4405
416518                 TA   =          239
06602
                                          MA   =          239
18328
                                          Ha   =            222
538  n
mi
                                          Hp   =            211
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18217467
69                 X    =         5554606
18
 Y    =        4517025
99  feet           Y    =         1438893
92  meter
 Z    =      -11975427
06                 Z    =        -3623132
54
 XDOT =       4493
555283                 XDOT =        1279
732336
 YDOT =      20069
052290  feet/sec       YDOT =        6131
860805  meter/sec
 ZDOT =      14453
466267                 ZDOT =        4411
851132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6905280
73                 X    =         2104729
57
 Y    =       17532232
59  feet           Y    =         5343824
49  meter
 Z    =      -11858685
61                 Z    =        -3614527
37
 XDOT =     -12541
765279                 XDOT =       -3822
730057
 YDOT =      14701
328128  feet/sec       YDOT =        4480
964813  meter/sec
 ZDOT =      14480
145743                 ZDOT =        4413
548422


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   16027
50764759  
00016717  00000-0  10270-3 0  9129
2 25544  51
6418  44
5699 0007089  63
1254 297
0623 15
54760799 22948


Satellite: ISS
Catalog Number: 25544
Epoch time:      16027
50764759   =   yrday
fracday
Element set:     912
Inclination:       51
6418  deg
RA of node:        44
5699  deg
Eccentricity:     
0007089     
Arg of perigee:    63
1254  deg
Mean anomaly:     297
0623  deg
Mean motion:   15
54760799  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2294
Checksum:              341


Coasting Arc #14 (Orbit 2298)
---------------------------------------

Vector Time (GMT): 2016/027/19:32:28
472
Vector Time (MET): N/A
Weight (LBS)     : 922190
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3404160
97                 A    =         6777201
50  meter
 Y    =       -2527459
23  meter          E    =           
0018545
 Z    =       -5302949
98                 I    =           51
87469
 XDOT =       5231
360020                 Wp   =           85
52776
 YDOT =       5542
152797  meter/sec      RA   =           42
39851  deg
 ZDOT =        720
312720                 TA   =          191
32111
                                          MA   =          191
36289
                                          Ha   =            222
440  n
mi
                                          Hp   =            213
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11168507
12                 X    =         3457929
60
 Y    =       -8292189
09  feet           Y    =        -2489091
24  meter
 Z    =      -17398129
87                 Z    =        -5286283
04
 XDOT =      17163
254660                 XDOT =        5165
498595
 YDOT =      18182
916000  feet/sec       YDOT =        5600
285108  meter/sec
 ZDOT =       2363
230708                 ZDOT =         745
564671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1249049
68                 X    =         -380710
34
 Y    =      -13945027
81  feet           Y    =        -4250444
48  meter
 Z    =      -17325326
79                 Z    =        -5280759
61
 XDOT =      23420
012985                 XDOT =        7138
419958
 YDOT =      -5153
864726  feet/sec       YDOT =       -1570
897969  meter/sec
 ZDOT =       2471
645596                 ZDOT =         753
357578


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   16027
82902877  
00016717  00000-0  10270-3 0  9130
2 25544  51
6427  42
9655 0004881  54
8507 305
3103 15
54246842 22996


Satellite: ISS
Catalog Number: 25544
Epoch time:      16027
82902877   =   yrday
fracday
Element set:     913
Inclination:       51
6427  deg
RA of node:        42
9655  deg
Eccentricity:     
0004881     
Arg of perigee:    54
8507  deg
Mean anomaly:     305
3103  deg
Mean motion:   15
54246842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2299
Checksum:              320


Coasting Arc #15 (Orbit 2314)
---------------------------------------

Vector Time (GMT): 2016/028/19:32:28
472
Vector Time (MET): N/A
Weight (LBS)     : 922190
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4642428
20                 A    =         6779221
91  meter
 Y    =        1184220
05  meter          E    =           
0012446
 Z    =        4789554
02                 I    =           51
85758
 XDOT =      -4222
644752                 Wp   =           59
65478
 YDOT =      -5838
520166  meter/sec      RA   =           37
41466  deg
 ZDOT =      -2638
121987                 TA   =           56
32661
                                          MA   =           56
20798
                                          Ha   =            222
512  n
mi
                                          Hp   =            212
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15231063
65                 X    =        -4678590
62
 Y    =        3885236
38  feet           Y    =         1132103
37  meter
 Z    =       15713759
90                 Z    =         4766914
74
 XDOT =     -13853
821364                 XDOT =       -4144
228491
 YDOT =     -19155
249890  feet/sec       YDOT =       -5885
302252  meter/sec
 ZDOT =      -8655
255864                 ZDOT =       -2658
443467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4358780
33                 X    =        -1328556
24
 Y    =       15204118
82  feet           Y    =         4634215
41  meter
 Z    =       15615326
35                 Z    =         4759551
47
 XDOT =     -22388
938485                 XDOT =       -6824
148450
 YDOT =       2598
193263  feet/sec       YDOT =         791
929306  meter/sec
 ZDOT =      -8742
215947                 ZDOT =       -2664
627421


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   16028
85778090  
00016717  00000-0  10270-3 0  9143
2 25544  51
6427  37
8357 0004873  57
3316 302
8306 15
54294052 23157


Satellite: ISS
Catalog Number: 25544
Epoch time:      16028
85778090   =   yrday
fracday
Element set:     914
Inclination:       51
6427  deg
RA of node:        37
8357  deg
Eccentricity:     
0004873     
Arg of perigee:    57
3316  deg
Mean anomaly:     302
8306  deg
Mean motion:   15
54294052  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2315
Checksum:              314


Coasting Arc #16 (Orbit 2329)
---------------------------------------

Vector Time (GMT): 2016/029/19:32:28
472
Vector Time (MET): N/A
Weight (LBS)     : 922190
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5634018
37                 A    =         6782916
68  meter
 Y    =          57935
22  meter          E    =           
0010039
 Z    =       -3784142
93                 I    =           51
84448
 XDOT =       2789
311783                 Wp   =           83
21022
 YDOT =       5730
395227  meter/sec      RA   =           32
43747  deg
 ZDOT =       4251
419370                 TA   =          231
63273
                                          MA   =          231
72297
                                          Ha   =            222
461  n
mi
                                          Hp   =            212
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18484312
22                 X    =         5651333
28
 Y    =         190076
20  feet           Y    =          121035
19  meter
 Z    =      -12415167
11                 Z    =        -3756732
60
 XDOT =       9151
285378                 XDOT =        2704
374497
 YDOT =      18800
509274  feet/sec       YDOT =        5761
112446  meter/sec
 ZDOT =      13948
226281                 ZDOT =        4264
762397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9231600
55                 X    =         2813791
85
 Y    =      -16106548
75  feet           Y    =        -4909276
06  meter
 Z    =      -12296297
82                 Z    =        -3747911
58
 XDOT =      19657
974416                 XDOT =        5991
750602
 YDOT =        602
646967  feet/sec       YDOT =         183
686796  meter/sec
 ZDOT =      14004
932370                 ZDOT =        4268
703386


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   16029
82222262  
00016717  00000-0  10270-3 0  9157
2 25544  51
6433  33
0265 0004859  61
0013 299
1627 15
54286470 23306


Satellite: ISS
Catalog Number: 25544
Epoch time:      16029
82222262   =   yrday
fracday
Element set:     915
Inclination:       51
6433  deg
RA of node:        33
0265  deg
Eccentricity:     
0004859     
Arg of perigee:    61
0013  deg
Mean anomaly:     299
1627  deg
Mean motion:   15
54286470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2330
Checksum:              287
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