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

 
Date: September 20th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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


265/22:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 215 0

278/01:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 213 3

Coasting Arc #1 (Orbit 1964)
---------------------------------------

Vector Time (GMT): 2016/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2775657
22                 A    =         6788889
09  meter
 Y    =       -5953296
88  meter          E    =           
0012363
 Z    =       -1686511
49                 I    =           51
36392
 XDOT =       5095
868529                 Wp   =           11
43321
 YDOT =        771
859414  meter/sec      RA   =          306
83970  deg
 ZDOT =       5681
192030                 TA   =          330
00233
                                          MA   =          330
07310
                                          Ha   =            221
938  n
mi
                                          Hp   =            215
535

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9106486
96                 X    =         2850214
64
 Y    =      -19531813
92  feet           Y    =        -5921840
96  meter
 Z    =       -5533174
17                 Z    =        -1672846
07
 XDOT =      16718
728771                 XDOT =        5059
261608
 YDOT =       2532
347158  feet/sec       YDOT =         828
640862  meter/sec
 ZDOT =      18639
081462                 ZDOT =        5705
857709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9828735
81                 X    =        -2995798
67
 Y    =       19195949
50  feet           Y    =         5850925
41  meter
 Z    =       -5472417
34                 Z    =        -1667992
80
 XDOT =     -15097
732247                 XDOT =       -4601
788789
 YDOT =      -2404
043908  feet/sec       YDOT =        -732
752583  meter/sec
 ZDOT =      18746
641898                 ZDOT =        5713
976450


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   16263
50326586  
00016717  00000-0  10270-3 0  9000
2 25544  51
6420 307
5138 0006396 339
2539  20
8353 15
53873653 19653


Satellite: ISS
Catalog Number: 25544
Epoch time:      16263
50326586   =   yrday
fracday
Element set:     900
Inclination:       51
6420  deg
RA of node:       307
5138  deg
Eccentricity:     
0006396     
Arg of perigee:   339
2539  deg
Mean anomaly:      20
8353  deg
Mean motion:   15
53873653  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1965
Checksum:              317


Coasting Arc #2 (Orbit 1980)
---------------------------------------

Vector Time (GMT): 2016/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3539287
10                 A    =         6789975
37  meter
 Y    =        5792324
50  meter          E    =           
0007330
 Z    =          62831
97                 I    =           51
34949
 XDOT =      -4116
218017                 Wp   =          108
49505
 YDOT =      -2443
999406  meter/sec      RA   =          301
85034  deg
 ZDOT =      -5984
666249                 TA   =           70
82588
                                          MA   =           70
74655
                                          Ha   =            222
025  n
mi
                                          Hp   =            215
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11611834
31                 X    =        -3604100
51
 Y    =       19003689
32  feet           Y    =         5752383
44  meter
 Z    =         206141
64                 Z    =           45480
77
 XDOT =     -13504
652286                 XDOT =       -4059
511417
 YDOT =      -8018
370755  feet/sec       YDOT =       -2489
713286  meter/sec
 ZDOT =     -19634
731787                 ZDOT =       -6004
524026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11957853
88                 X    =         3644753
86
 Y    =      -18788571
07  feet           Y    =        -5726756
46  meter
 Z    =         129327
96                 Z    =           39419
16
 XDOT =      11858
626786                 XDOT =        3614
509444
 YDOT =       7390
962718  feet/sec       YDOT =        2252
765437  meter/sec
 ZDOT =     -19720
993123                 ZDOT =       -6010
958704


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   16264
53226248  
00016717  00000-0  10270-3 0  9019
2 25544  51
6421 302
3860 0006380 343
6254  16
4692 15
53904398 19811


Satellite: ISS
Catalog Number: 25544
Epoch time:      16264
53226248   =   yrday
fracday
Element set:     901
Inclination:       51
6421  deg
RA of node:       302
3860  deg
Eccentricity:     
0006380     
Arg of perigee:   343
6254  deg
Mean anomaly:      16
4692  deg
Mean motion:   15
53904398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1981
Checksum:              304


Coasting Arc #3 (Orbit 1996)
---------------------------------------

Vector Time (GMT): 2016/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4030396
66                 A    =         6789060
04  meter
 Y    =       -5227645
80  meter          E    =           
0016926
 Z    =        1541527
57                 I    =           51
32963
 XDOT =       3079
318926                 Wp   =           40
76890
 YDOT =       4070
753429  meter/sec      RA   =          296
85972  deg
 ZDOT =       5730
715059                 TA   =          336
16531
                                          MA   =          336
24359
                                          Ha   =            222
218  n
mi
                                          Hp   =            215
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13223086
16                 X    =         4081065
83
 Y    =      -17151068
89  feet           Y    =        -5182291
76  meter
 Z    =        5057505
15                 Z    =         1561229
95
 XDOT =      10102
752382                 XDOT =        3005
732241
 YDOT =      13355
490252  feet/sec       YDOT =        4104
777497  meter/sec
 ZDOT =      18801
558592                 ZDOT =        5745
494671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13208106
60                 X    =        -4025830
89
 Y    =       17136738
72  feet           Y    =         5223277
96  meter
 Z    =        5144476
27                 Z    =         1568036
37
 XDOT =      -8717
205907                 XDOT =       -2657
004361
 YDOT =     -12404
492424  feet/sec       YDOT =       -3780
889291  meter/sec
 ZDOT =      18865
355167                 ZDOT =        5750
160255


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   16265
56125491  
00016717  00000-0  10270-3 0  9022
2 25544  51
6418 297
2582 0006511 349
1450  10
9561 15
53864632 19972


Satellite: ISS
Catalog Number: 25544
Epoch time:      16265
56125491   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:       297
2582  deg
Eccentricity:     
0006511     
Arg of perigee:   349
1450  deg
Mean anomaly:      10
9561  deg
Mean motion:   15
53864632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1997
Checksum:              318


Coasting Arc #4 (Orbit 2002)
---------------------------------------

Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2893390
44                 A    =         6778953
36  meter
 Y    =       -3449341
07  meter          E    =           
0012043
 Z    =       -5077050
16                 I    =           51
29166
 XDOT =       4303
413024                 Wp   =           72
61564
 YDOT =      -6104
638662  meter/sec      RA   =          294
66020  deg
 ZDOT =       1701
867475                 TA   =          213
88681
                                          MA   =          213
96381
                                          Ha   =            222
155  n
mi
                                          Hp   =            214
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9492750
79                 X    =        -2829941
64
 Y    =      -11316735
80  feet           Y    =        -3481342
56  meter
 Z    =      -16656988
72                 Z    =        -5090951
26
 XDOT =      14118
809135                 XDOT =        4363
089793
 YDOT =     -20028
342066  feet/sec       YDOT =       -6056
181199  meter/sec
 ZDOT =       5583
554708                 ZDOT =        1722
918016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4122234
17                 X    =        -1256456
97
 Y    =      -14113222
94  feet           Y    =        -4301710
35  meter
 Z    =      -16717063
85                 Z    =        -5095361
06
 XDOT =      19845
116847                 XDOT =        6048
791615
 YDOT =     -12493
650610  feet/sec       YDOT =       -3808
064706  meter/sec
 ZDOT =       5676
567799                 ZDOT =        1730
217865


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   16265
94712279  
00016717  00000-0  10270-3 0  9031
2 25544  51
6434 295
3371 0006719 347
3179  12
7804 15
53917397 20039


Satellite: ISS
Catalog Number: 25544
Epoch time:      16265
94712279   =   yrday
fracday
Element set:     903
Inclination:       51
6434  deg
RA of node:       295
3371  deg
Eccentricity:     
0006719     
Arg of perigee:   347
3179  deg
Mean anomaly:      12
7804  deg
Mean motion:   15
53917397  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2003
Checksum:              324


Coasting Arc #5 (Orbit 2018)
---------------------------------------

Vector Time (GMT): 2016/266/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1998841
33                 A    =         6781729
87  meter
 Y    =        4794033
85  meter          E    =           
0012656
 Z    =        4359532
79                 I    =           51
28841
 XDOT =      -4680
079253                 Wp   =           38
49330
 YDOT =       5042
692249  meter/sec      RA   =          289
64326  deg
 ZDOT =      -3384
414413                 TA   =           86
02959
                                          MA   =           85
88493
                                          Ha   =            222
280  n
mi
                                          Hp   =            214
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6557878
39                 X    =         1923907
81
 Y    =       15728457
50  feet           Y    =         4815967
58  meter
 Z    =       14302929
11                 Z    =         4369060
36
 XDOT =     -15354
590726                 XDOT =       -4719
679961
 YDOT =      16544
265910  feet/sec       YDOT =        4990
134793  meter/sec
 ZDOT =     -11103
721829                 ZDOT =       -3407
245761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -15831
52                 X    =           -4825
45
 Y    =       17006548
96  feet           Y    =         5183596
12  meter
 Z    =       14343673
42                 Z    =         4371951
66
 XDOT =     -19192
789526                 XDOT =       -5849
962248
 YDOT =       9473
624738  feet/sec       YDOT =        2887
560820  meter/sec
 ZDOT =     -11204
313640                 ZDOT =       -3415
074798


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   16266
97610371  
00016717  00000-0  10270-3 0  9046
2 25544  51
6431 290
2093 0006870 351
0088   9
0940 15
53955767 20190


Satellite: ISS
Catalog Number: 25544
Epoch time:      16266
97610371   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       290
2093  deg
Eccentricity:     
0006870     
Arg of perigee:   351
0088  deg
Mean anomaly:       9
0940  deg
Mean motion:   15
53955767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2019
Checksum:              310


Coasting Arc #6 (Orbit 2033)
---------------------------------------

Vector Time (GMT): 2016/267/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1167058
53                 A    =         6785446
91  meter
 Y    =       -5838613
27  meter          E    =           
0008304
 Z    =       -3249546
54                 I    =           51
28949
 XDOT =       4852
322962                 Wp   =           27
99587
 YDOT =      -3593
070615  meter/sec      RA   =          284
63475  deg
 ZDOT =       4725
275670                 TA   =          294
12963
                                          MA   =          294
21645
                                          Ha   =            222
391  n
mi
                                          Hp   =            214
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3828932
17                 X    =        -1085897
99
 Y    =      -19155555
36  feet           Y    =        -5851210
55  meter
 Z    =      -10661241
92                 Z    =        -3255018
26
 XDOT =      15919
694757                 XDOT =        4869
187545
 YDOT =     -11788
289418  feet/sec       YDOT =       -3538
714034  meter/sec
 ZDOT =      15502
872932                 ZDOT =        4748
888329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3492886
28                 X    =         1064631
74
 Y    =      -19206973
41  feet           Y    =        -5854285
50  meter
 Z    =      -10684101
25                 Z    =        -3256514
06
 XDOT =      17629
599660                 XDOT =        5373
501976
 YDOT =      -5453
247140  feet/sec       YDOT =       -1662
149728  meter/sec
 ZDOT =      15606
613537                 ZDOT =        4756
895806


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   16267
94077115  
00016717  00000-0  10270-3 0  9058
2 25544  51
6421 285
4023 0006762 354
3482   5
7593 15
53915749 20342


Satellite: ISS
Catalog Number: 25544
Epoch time:      16267
94077115   =   yrday
fracday
Element set:     905
Inclination:       51
6421  deg
RA of node:       285
4023  deg
Eccentricity:     
0006762     
Arg of perigee:   354
3482  deg
Mean anomaly:       5
7593  deg
Mean motion:   15
53915749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2034
Checksum:              314


Coasting Arc #7 (Orbit 2049)
---------------------------------------

Vector Time (GMT): 2016/268/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         346670
04                 A    =         6788509
18  meter
 Y    =        6536345
01  meter          E    =           
0012537
 Z    =        1791710
00                 I    =           51
29342
 XDOT =      -4880
550179                 Wp   =           85
02435
 YDOT =       1810
768079  meter/sec      RA   =          279
63494  deg
 ZDOT =      -5626
375635                 TA   =           75
20057
                                          MA   =           75
06171
                                          Ha   =            222
534  n
mi
                                          Hp   =            214
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1137368
90                 X    =          264849
85
 Y    =       21444701
47  feet           Y    =         6539764
37  meter
 Z    =        5878313
63                 Z    =         1793194
75
 XDOT =     -16012
303737                 XDOT =       -4873
105418
 YDOT =       5940
840154  feet/sec       YDOT =        1756
231646  meter/sec
 ZDOT =     -18459
237647                 ZDOT =       -5650
066182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6454003
99                 X    =        -1967180
42
 Y    =       20480523
53  feet           Y    =         6242463
57  meter
 Z    =        5883654
36                 Z    =         1793337
85
 XDOT =     -15472
546023                 XDOT =       -4716
032028
 YDOT =        490
069253  feet/sec       YDOT =         149
373108  meter/sec
 ZDOT =     -18563
002320                 ZDOT =       -5658
003107


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   16268
96974250  
00016717  00000-0  10270-3 0  9068
2 25544  51
6427 280
2746 0006849 358
3943   1
7186 15
53942057 20509


Satellite: ISS
Catalog Number: 25544
Epoch time:      16268
96974250   =   yrday
fracday
Element set:     906
Inclination:       51
6427  deg
RA of node:       280
2746  deg
Eccentricity:     
0006849     
Arg of perigee:   358
3943  deg
Mean anomaly:       1
7186  deg
Mean motion:   15
53942057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2050
Checksum:              331


Coasting Arc #8 (Orbit 2064)
---------------------------------------

Vector Time (GMT): 2016/269/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         393398
23                 A    =         6789897
16  meter
 Y    =       -6765526
94  meter          E    =           
0017425
 Z    =        -193580
78                 I    =           51
29195
 XDOT =       4801
971213                 Wp   =           28
60934
 YDOT =        114
833177  meter/sec      RA   =          274
63954  deg
 ZDOT =       5984
071199                 TA   =          329
29373
                                          MA   =          329
39558
                                          Ha   =            222
610  n
mi
                                          Hp   =            214
435

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1290676
62                 X    =          469963
17
 Y    =      -22196610
70  feet           Y    =        -6760699
62  meter
 Z    =        -635107
56                 Z    =         -191483
13
 XDOT =      15754
498731                 XDOT =        4771
262248
 YDOT =        376
749267  feet/sec       YDOT =         168
360923  meter/sec
 ZDOT =      19632
779523                 ZDOT =        6007
323319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8608430
54                 X    =         2623849
63
 Y    =      -20500324
57  feet           Y    =        -6248498
93  meter
 Z    =        -624780
65                 Z    =         -190433
14
 XDOT =      13115
337785                 XDOT =        3997
554957
 YDOT =       4930
184785  feet/sec       YDOT =        1502
720322  meter/sec
 ZDOT =      19734
296303                 ZDOT =        6015
013513


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   16269
93439694  
00016717  00000-0  10270-3 0  9075
2 25544  51
6412 275
4665 0006849   1
8494 358
2683 15
53929160 20658


Satellite: ISS
Catalog Number: 25544
Epoch time:      16269
93439694   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       275
4665  deg
Eccentricity:     
0006849     
Arg of perigee:     1
8494  deg
Mean anomaly:     358
2683  deg
Mean motion:   15
53929160  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2065
Checksum:              347


Coasting Arc #9 (Orbit 2080)
---------------------------------------

Vector Time (GMT): 2016/270/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1131297
07                 A    =         6788978
21  meter
 Y    =        6533692
11  meter          E    =           
0005736
 Z    =       -1461670
76                 I    =           51
28611
 XDOT =      -4619
244087                 Wp   =           89
25420
 YDOT =      -2081
064361  meter/sec      RA   =          269
64637  deg
 ZDOT =      -5746
762161                 TA   =          106
76039
                                          MA   =          106
69744
                                          Ha   =            222
703  n
mi
                                          Hp   =            214
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3711604
54                 X    =        -1197174
24
 Y    =       21435997
74  feet           Y    =         6520672
68  meter
 Z    =       -4795507
76                 Z    =        -1467327
06
 XDOT =     -15155
000285                 XDOT =       -4567
714546
 YDOT =      -6827
638979  feet/sec       YDOT =       -2132
432383  meter/sec
 ZDOT =     -18854
206566                 ZDOT =       -5769
075845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10276646
40                 X    =        -3132321
82
 Y    =       19168211
25  feet           Y    =         5842470
79  meter
 Z    =       -4821319
15                 Z    =        -1469538
08
 XDOT =     -10700
033791                 XDOT =       -3261
370300
 YDOT =     -10487
316135  feet/sec       YDOT =       -3196
533958  meter/sec
 ZDOT =     -18951
293728                 ZDOT =       -5776
354328


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   16270
96335663  
00016717  00000-0  10270-3 0  9082
2 25544  51
6400 270
3392 0006740   5
3968 354
7256 15
53932215 20811


Satellite: ISS
Catalog Number: 25544
Epoch time:      16270
96335663   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       270
3392  deg
Eccentricity:     
0006740     
Arg of perigee:     5
3968  deg
Mean anomaly:     354
7256  deg
Mean motion:   15
53932215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2081
Checksum:              307


Coasting Arc #10 (Orbit 2096)
---------------------------------------

Vector Time (GMT): 2016/271/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1825299
52                 A    =         6786069
93  meter
 Y    =       -5823628
72  meter          E    =           
0016286
 Z    =        2944306
02                 I    =           51
27764
 XDOT =       4367
762082                 Wp   =           59
24740
 YDOT =       3888
559800  meter/sec      RA   =          264
64613  deg
 ZDOT =       4971
213029                 TA   =          334
59681
                                          MA   =          334
67678
                                          Ha   =            222
602  n
mi
                                          Hp   =            214
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5988515
47                 X    =         1875982
99
 Y    =      -19106393
42  feet           Y    =        -5802933
22  meter
 Z    =        9659796
64                 Z    =         2953296
71
 XDOT =      14329
928089                 XDOT =        4299
806594
 YDOT =      12757
742125  feet/sec       YDOT =        3937
023725  meter/sec
 ZDOT =      16309
754032                 ZDOT =        4992
264951

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11387788
62                 X    =         3470997
97
 Y    =      -16445541
94  feet           Y    =        -5012601
18  meter
 Z    =        9700034
99                 Z    =         2956570
66
 XDOT =       8538
707181                 XDOT =        2602
597949
 YDOT =      15610
196650  feet/sec       YDOT =        4757
987939  meter/sec
 ZDOT =      16401
035098                 ZDOT =        4999
035498


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   16271
99230909  
00016717  00000-0  10270-3 0  9094
2 25544  51
6397 265
2102 0006655   8
0322 352
0936 15
53974140 20973


Satellite: ISS
Catalog Number: 25544
Epoch time:      16271
99230909   =   yrday
fracday
Element set:     909
Inclination:       51
6397  deg
RA of node:       265
2102  deg
Eccentricity:     
0006655     
Arg of perigee:     8
0322  deg
Mean anomaly:     352
0936  deg
Mean motion:   15
53974140  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2097
Checksum:              311


Coasting Arc #11 (Orbit 2111)
---------------------------------------

Vector Time (GMT): 2016/272/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2535935
38                 A    =         6782385
99  meter
 Y    =        4722646
76  meter          E    =           
0012865
 Z    =       -4169383
55                 I    =           51
26827
 XDOT =      -3990
492086                 Wp   =           44
18210
 YDOT =      -5396
882365  meter/sec      RA   =          259
63698  deg
 ZDOT =      -3683
741977                 TA   =          187
72728
                                          MA   =          187
74712
                                          Ha   =            222
864  n
mi
                                          Hp   =            213
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8319997
96                 X    =        -2568303
62
 Y    =       15494247
91  feet           Y    =         4694106
66  meter
 Z    =      -13679079
88                 Z    =        -4181781
80
 XDOT =     -13092
165638                 XDOT =       -3911
952118
 YDOT =     -17706
306972  feet/sec       YDOT =       -5441
068100  meter/sec
 ZDOT =     -12085
767640                 ZDOT =       -3702
935304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12288905
18                 X    =        -3745658
30
 Y    =       12520832
15  feet           Y    =         3816349
64  meter
 Z    =      -13734004
61                 Z    =        -4186124
61
 XDOT =      -6541
637972                 XDOT =       -1993
891254
 YDOT =     -19775
953467  feet/sec       YDOT =       -6027
710617  meter/sec
 ZDOT =     -12168
693146                 ZDOT =       -3709
017671


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   16272
95694749  
00016717  00000-0  10270-3 0  9109
2 25544  51
6387 260
4018 0006796  13
6360 346
4975 15
53968615 21123


Satellite: ISS
Catalog Number: 25544
Epoch time:      16272
95694749   =   yrday
fracday
Element set:     910
Inclination:       51
6387  deg
RA of node:       260
4018  deg
Eccentricity:     
0006796     
Arg of perigee:    13
6360  deg
Mean anomaly:     346
4975  deg
Mean motion:   15
53968615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2112
Checksum:              336


Coasting Arc #12 (Orbit 2127)
---------------------------------------

Vector Time (GMT): 2016/273/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3224000
98                 A    =         6779330
65  meter
 Y    =       -3293982
27  meter          E    =           
0007778
 Z    =        4964222
28                 I    =           51
26406
 XDOT =       3498
592205                 Wp   =           66
23423
 YDOT =       6514
639017  meter/sec      RA   =          254
61911  deg
 ZDOT =       2051
130731                 TA   =            3
72958
                                          MA   =            3
72379
                                          Ha   =            222
879  n
mi
                                          Hp   =            213
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10577431
03                 X    =         3236481
32
 Y    =      -10807028
45  feet           Y    =        -3257858
81  meter
 Z    =       16286818
50                 Z    =         4979914
55
 XDOT =      11478
320884                 XDOT =        3415
520262
 YDOT =      21373
487588  feet/sec       YDOT =        6553
298441  meter/sec
 ZDOT =       6729
431533                 ZDOT =        2067
923378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12978285
78                 X    =         3955781
51
 Y    =       -7614685
55  feet           Y    =        -2320956
16  meter
 Z    =       16355886
71                 Z    =         4985274
27
 XDOT =       4752
421021                 XDOT =        1448
537927
 YDOT =      22705
845272  feet/sec       YDOT =        6920
741639  meter/sec
 ZDOT =       6801
702949                 ZDOT =        2073
159059


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   16273
98588931  
00016717  00000-0  10270-3 0  9119
2 25544  51
6383 255
2731 0006794  17
5899 342
5488 15
53933786 21285


Satellite: ISS
Catalog Number: 25544
Epoch time:      16273
98588931   =   yrday
fracday
Element set:     911
Inclination:       51
6383  deg
RA of node:       255
2731  deg
Eccentricity:     
0006794     
Arg of perigee:    17
5899  deg
Mean anomaly:     342
5488  deg
Mean motion:   15
53933786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2128
Checksum:              358


Coasting Arc #13 (Orbit 2142)
---------------------------------------

Vector Time (GMT): 2016/274/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3894023
76                 A    =         6777803
82  meter
 Y    =        1708540
09  meter          E    =           
0018544
 Z    =       -5293163
28                 I    =           51
26874
 XDOT =      -2825
783048                 Wp   =           69
23271
 YDOT =      -7111
542774  meter/sec      RA   =          249
59542  deg
 ZDOT =       -210
784299                 TA   =          198
71039
                                          MA   =          198
77864
                                          Ha   =            222
955  n
mi
                                          Hp   =            213
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12775668
49                 X    =        -3887127
52
 Y    =        5605446
49  feet           Y    =         1665032
28  meter
 Z    =      -17366021
25                 Z    =        -5312063
15
 XDOT =      -9270
941759                 XDOT =       -2745
026037
 YDOT =     -23331
833249  feet/sec       YDOT =       -7142
691068  meter/sec
 ZDOT =       -691
549539                 ZDOT =        -224
314172

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13663234
41                 X    =        -4164553
85
 Y    =        2252005
43  feet           Y    =          686411
26  meter
 Z    =      -17448837
41                 Z    =        -5318405
64
 XDOT =      -2959
869077                 XDOT =        -902
168095
 YDOT =     -23913
125007  feet/sec       YDOT =       -7288
720502  meter/sec
 ZDOT =       -749
488453                 ZDOT =        -228
444081


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   16274
95051441  
00016717  00000-0  10270-3 0  9129
2 25544  51
6381 250
4651 0006640  22
0292 338
1144 15
53982473 21433


Satellite: ISS
Catalog Number: 25544
Epoch time:      16274
95051441   =   yrday
fracday
Element set:     912
Inclination:       51
6381  deg
RA of node:       250
4651  deg
Eccentricity:     
0006640     
Arg of perigee:    22
0292  deg
Mean anomaly:     338
1144  deg
Mean motion:   15
53982473  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2143
Checksum:              286


Coasting Arc #14 (Orbit 2158)
---------------------------------------

Vector Time (GMT): 2016/275/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4487943
80                 A    =         6778741
98  meter
 Y    =         -37190
72  meter          E    =           
0011337
 Z    =        5076306
93                 I    =           51
28464
 XDOT =       1957
222612                 Wp   =           38
40890
 YDOT =       7227
968613  meter/sec      RA   =          244
57131  deg
 ZDOT =      -1666
673755                 TA   =           67
81824
                                          MA   =           67
69798
                                          Ha   =            222
946  n
mi
                                          Hp   =            213
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14724225
07                 X    =         4463367
29
 Y    =        -122016
79  feet           Y    =           12859
79  meter
 Z    =       16654550
29                 Z    =         5098048
82
 XDOT =       6421
334029                 XDOT =        1884
348249
 YDOT =      23713
807785  feet/sec       YDOT =        7249
447887  meter/sec
 ZDOT =      -5468
089747                 ZDOT =       -1657
343969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14238904
27                 X    =         4340018
02
 Y    =        3301396
18  feet           Y    =         1006265
56  meter
 Z    =       16749511
21                 Z    =         5105251
02
 XDOT =        971
881617                 XDOT =         296
229517
 YDOT =      23527
411568  feet/sec       YDOT =        7171
155046  meter/sec
 ZDOT =      -5428
500306                 ZDOT =       -1654
606893


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   16275
97944184  
00016717  00000-0  10270-3 0  9138
2 25544  51
6388 245
3362 0006645  25
6223 334
5258 15
53962693 21595


Satellite: ISS
Catalog Number: 25544
Epoch time:      16275
97944184   =   yrday
fracday
Element set:     913
Inclination:       51
6388  deg
RA of node:       245
3362  deg
Eccentricity:     
0006645     
Arg of perigee:    25
6223  deg
Mean anomaly:     334
5258  deg
Mean motion:   15
53962693  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2159
Checksum:              337


Coasting Arc #15 (Orbit 2173)
---------------------------------------

Vector Time (GMT): 2016/276/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4957565
55                 A    =         6781435
46  meter
 Y    =       -1504485
15  meter          E    =           
0012172
 Z    =       -4384619
20                 I    =           51
30917
 XDOT =       -890
904623                 Wp   =           78
29698
 YDOT =      -6826
122610  meter/sec      RA   =          239
55400  deg
 ZDOT =       3359
917491                 TA   =          225
84378
                                          MA   =          225
94391
                                          Ha   =            223
050  n
mi
                                          Hp   =            213
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16264978
85                 X    =        -4919074
63
 Y    =       -4935974
91  feet           Y    =        -1559709
34  meter
 Z    =      -14385233
61                 Z    =        -4408608
50
 XDOT =      -2922
915430                 XDOT =        -830
828257
 YDOT =     -22395
415387  feet/sec       YDOT =       -6835
748951  meter/sec
 ZDOT =      11023
351349                 ZDOT =        3355
736456

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14713669
78                 X    =        -4484726
55
 Y    =       -8330836
22  feet           Y    =        -2539238
88  meter
 Z    =      -14489769
51                 Z    =        -4416481
75
 XDOT =       1332
320935                 XDOT =         406
091421
 YDOT =     -21437
361538  feet/sec       YDOT =       -6534
107797  meter/sec
 ZDOT =      11006
174793                 ZDOT =        3354
682077


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   16276
94405382  
00016717  00000-0  10270-3 0  9149
2 25544  51
6392 240
5283 0006646  30
8782 329
2760 15
54002812 21743


Satellite: ISS
Catalog Number: 25544
Epoch time:      16276
94405382   =   yrday
fracday
Element set:     914
Inclination:       51
6392  deg
RA of node:       240
5283  deg
Eccentricity:     
0006646     
Arg of perigee:    30
8782  deg
Mean anomaly:     329
2760  deg
Mean motion:   15
54002812  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2174
Checksum:              306


Coasting Arc #16 (Orbit 2189)
---------------------------------------

Vector Time (GMT): 2016/277/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5220530
29                 A    =         6785218
31  meter
 Y    =        2895883
11  meter          E    =           
0017023
 Z    =        3215927
45                 I    =           51
33816
 XDOT =       -389
409206                 Wp   =           73
81137
 YDOT =       6007
322036  meter/sec      RA   =          234
54745  deg
 ZDOT =      -4751
692660                 TA   =           68
78986
                                          MA   =           68
60809
                                          Ha   =            223
059  n
mi
                                          Hp   =            213
246

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17127724
05                 X    =         5172137
92
 Y    =        9500928
84  feet           Y    =         2953992
39  meter
 Z    =       10550943
08                 Z    =         3241170
03
 XDOT =      -1277
589258                 XDOT =        -433
473585
 YDOT =      19709
061799  feet/sec       YDOT =        6002
720453  meter/sec
 ZDOT =     -15589
542848                 ZDOT =       -4753
692094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14810009
16                 X    =         4514090
79
 Y    =       12726397
88  feet           Y    =         3879006
07  meter
 Z    =       10660741
32                 Z    =         3249393
95
 XDOT =      -4172
440419                 XDOT =       -1271
759840
 YDOT =      17992
600420  feet/sec       YDOT =        5484
144608  meter/sec
 ZDOT =     -15599
224084                 ZDOT =       -4754
643501


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   16277
97296669  
00016717  00000-0  10270-3 0  9150
2 25544  51
6384 235
4003 0006529  33
6641 326
4925 15
54003876 21903


Satellite: ISS
Catalog Number: 25544
Epoch time:      16277
97296669   =   yrday
fracday
Element set:     915
Inclination:       51
6384  deg
RA of node:       235
4003  deg
Eccentricity:     
0006529     
Arg of perigee:    33
6641  deg
Mean anomaly:     326
4925  deg
Mean motion:   15
54003876  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2190
Checksum:              327


Coasting Arc #17 (Orbit 2191)
---------------------------------------

Vector Time (GMT): 2016/278/01:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1211208
52                 A    =         6780271
62  meter
 Y    =        4737369
05  meter          E    =           
0016408
 Z    =       -4713047
00                 I    =           51
32851
 XDOT =      -5782
327959                 Wp   =           57
77124
 YDOT =      -4203
292656  meter/sec      RA   =          233
86082  deg
 ZDOT =      -2737
412963                 TA   =          184
96031
                                          MA   =          184
97659
                                          Ha   =            223
064  n
mi
                                          Hp   =            213
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3973781
24                 X    =        -1241198
61
 Y    =       15542549
37  feet           Y    =         4723656
26  meter
 Z    =      -15462752
62                 Z    =        -4719004
25
 XDOT =     -18970
892253                 XDOT =       -5721
598501
 YDOT =     -13790
330237  feet/sec       YDOT =       -4267
615291  meter/sec
 ZDOT =      -8981
013659                 ZDOT =       -2765
354558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7356861
93                 X    =         2242371
52
 Y    =       14227081
34  feet           Y    =         4336414
39  meter
 Z    =      -15489520
20                 Z    =        -4721205
76
 XDOT =     -22271
436993                 XDOT =       -6788
333995
 YDOT =       1600
934003  feet/sec       YDOT =         487
964684  meter/sec
 ZDOT =      -9102
396097                 ZDOT =       -2774
410330


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   16278
10158048  
00016717  00000-0  10270-3 0  9165
2 25544  51
6428 234
7603 0006347  34
3143 325
8419 15
54005015 21923


Satellite: ISS
Catalog Number: 25544
Epoch time:      16278
10158048   =   yrday
fracday
Element set:     916
Inclination:       51
6428  deg
RA of node:       234
7603  deg
Eccentricity:     
0006347     
Arg of perigee:    34
3143  deg
Mean anomaly:     325
8419  deg
Mean motion:   15
54005015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2192
Checksum:              292
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