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

 
Date: January 5th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 24322 131 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


006/12:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 6
000/00:00:00 000 0 0 0 0 212 6

008/21:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 212 4

015/23:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 8
000/00:00:00 000 0 0 0 0 212 0

Coasting Arc #1 (Orbit 3628)
---------------------------------------

Vector Time (GMT): 2017/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2894867
64                 A    =         6777739
50  meter
 Y    =        3036750
58  meter          E    =           
0020605
 Z    =       -5340405
81                 I    =           51
88795
 XDOT =      -5357
678880                 Wp   =           78
50193
 YDOT =       5461
488677  meter/sec      RA   =          133
23976  deg
 ZDOT =        206
039485                 TA   =          193
43140
                                          MA   =          193
48633
                                          Ha   =            223
518  n
mi
                                          Hp   =            212
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9497597
23                 X    =         2886635
75
 Y    =        9963092
44  feet           Y    =         3069077
05  meter
 Z    =      -17521016
42                 Z    =        -5326363
39
 XDOT =     -17577
686615                 XDOT =       -5419
353296
 YDOT =      17918
269939  feet/sec       YDOT =        5401
230659  meter/sec
 ZDOT =        675
982562                 ZDOT =         179
863970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7457001
57                 X    =        -2272894
08
 Y    =       11661911
43  feet           Y    =         3554550
61  meter
 Z    =      -17459854
80                 Z    =        -5321763
74
 XDOT =     -20661
199881                 XDOT =       -6297
533724
 YDOT =     -12395
846261  feet/sec       YDOT =       -3778
253940  meter/sec
 ZDOT =        560
121968                 ZDOT =         170
725176


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   17004
51581192  
00016717  00000-0  10270-3 0  9001
2 25544  51
6407 134
2254 0007004  49
3951 310
7810 15
54001916 36290


Satellite: ISS
Catalog Number: 25544
Epoch time:      17004
51581192   =   yrday
fracday
Element set:     900
Inclination:       51
6407  deg
RA of node:       134
2254  deg
Eccentricity:     
0007004     
Arg of perigee:    49
3951  deg
Mean anomaly:     310
7810  deg
Mean motion:   15
54001916  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3629
Checksum:              275


Coasting Arc #2 (Orbit 3644)
---------------------------------------

Vector Time (GMT): 2017/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1635431
37                 A    =         6779166
59  meter
 Y    =       -4261242
81  meter          E    =           
0013024
 Z    =        5005585
50                 I    =           51
91457
 XDOT =       5739
174824                 Wp   =           54
94194
 YDOT =      -4652
362676  meter/sec      RA   =          128
25943  deg
 ZDOT =      -2074
335917                 TA   =           55
20583
                                          MA   =           55
08334
                                          Ha   =            223
657  n
mi
                                          Hp   =            212
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5365588
50                 X    =        -1611974
19
 Y    =      -13980455
42  feet           Y    =        -4279400
27  meter
 Z    =       16422524
59                 Z    =         4997697
95
 XDOT =      18829
313728                 XDOT =        5800
848302
 YDOT =     -15263
657073  feet/sec       YDOT =       -4587
838473  meter/sec
 ZDOT =      -6805
564032                 ZDOT =       -2046
307102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12176655
92                 X    =         3711444
72
 Y    =       -8779798
94  feet           Y    =        -2676082
72  meter
 Z    =       16388598
74                 Z    =         4995244
90
 XDOT =      18841
746998                 XDOT =        5742
964485
 YDOT =      13591
205910  feet/sec       YDOT =        4142
599561  meter/sec
 ZDOT =      -6681
683483                 ZDOT =       -2036
577126


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   17005
54473716  
00016717  00000-0  10270-3 0  9018
2 25544  51
6412 129
0965 0007032  53
1625 307
0172 15
53976617 36455


Satellite: ISS
Catalog Number: 25544
Epoch time:      17005
54473716   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       129
0965  deg
Eccentricity:     
0007032     
Arg of perigee:    53
1625  deg
Mean anomaly:     307
0172  deg
Mean motion:   15
53976617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3645
Checksum:              297


Coasting Arc #3 (Orbit 3659)
---------------------------------------

Vector Time (GMT): 2017/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         462677
50                 A    =         6782179
42  meter
 Y    =        5303615
07  meter          E    =           
0013333
 Z    =       -4212486
79                 I    =           51
94508
 XDOT =      -5742
558618                 Wp   =           84
87503
 YDOT =       3444
390990  meter/sec      RA   =          123
28832  deg
 ZDOT =       3717
092716                 TA   =          223
12353
                                          MA   =          223
22804
                                          Ha   =            223
588  n
mi
                                          Hp   =            212
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1517970
79                 X    =          423798
97
 Y    =       17400311
91  feet           Y    =         5308571
79  meter
 Z    =      -13820494
70                 Z    =        -4210333
50
 XDOT =     -18840
415413                 XDOT =       -5798
703748
 YDOT =      11300
495374  feet/sec       YDOT =        3379
859792  meter/sec
 ZDOT =      12195
186076                 ZDOT =        3689
060811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16347365
05                 X    =        -4982676
87
 Y    =        6170513
84  feet           Y    =         1880772
62  meter
 Z    =      -13811936
08                 Z    =        -4209878
12
 XDOT =     -15470
061019                 XDOT =       -4715
274599
 YDOT =     -14046
609108  feet/sec       YDOT =       -4281
406456  meter/sec
 ZDOT =      12071
479236                 ZDOT =        3679
386871


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   17006
50934658  
00016717  00000-0  10270-3 0  9023
2 25544  51
6420 124
2897 0007016  55
7324 304
4492 15
54007151 36603


Satellite: ISS
Catalog Number: 25544
Epoch time:      17006
50934658   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:       124
2897  deg
Eccentricity:     
0007016     
Arg of perigee:    55
7324  deg
Mean anomaly:     304
4492  deg
Mean motion:   15
54007151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3660
Checksum:              290


Coasting Arc #4 (Orbit 3659)
---------------------------------------

Vector Time (GMT): 2017/006/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2827284
11                 A    =         6789069
04  meter
 Y    =        6044893
25  meter          E    =           
0016003
 Z    =       -1216988
88                 I    =           51
96834
 XDOT =      -4800
319298                 Wp   =           45
83130
 YDOT =      -1072
470378  meter/sec      RA   =          123
26686  deg
 ZDOT =       5883
532460                 TA   =          301
00306
                                          MA   =          301
16014
                                          Ha   =            223
623  n
mi
                                          Hp   =            212
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9275866
50                 X    =        -2888757
98
 Y    =       19832326
95  feet           Y    =         6012932
98  meter
 Z    =       -3992745
68                 Z    =        -1230872
11
 XDOT =     -15749
079061                 XDOT =       -4816
549279
 YDOT =      -3518
603604  feet/sec       YDOT =       -1126
241712  meter/sec
 ZDOT =      19302
928019                 ZDOT =        5860
174480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21715279
26                 X    =        -6618817
12
 Y    =       -2703805
95  feet           Y    =         -824120
05  meter
 Z    =       -4054749
03                 Z    =        -1235887
51
 XDOT =      -1731
600006                 XDOT =        -527
791682
 YDOT =     -14602
997168  feet/sec       YDOT =       -4450
993537  meter/sec
 ZDOT =      19200
515819                 ZDOT =        5852
317222


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   17006
50934649  
00016717  00000-0  10270-3 0  9034
2 25544  51
6423 124
2894 0007113  55
3979 304
7844 15
53994018 36603


Satellite: ISS
Catalog Number: 25544
Epoch time:      17006
50934649   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:       124
2894  deg
Eccentricity:     
0007113     
Arg of perigee:    55
3979  deg
Mean anomaly:     304
7844  deg
Mean motion:   15
53994018  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3660
Checksum:              321


Coasting Arc #5 (Orbit 3675)
---------------------------------------

Vector Time (GMT): 2017/007/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3544796
00                 A    =         6789562
14  meter
 Y    =       -5766964
56  meter          E    =           
0014309
 Z    =        -492082
17                 I    =           51
98631
 XDOT =       3808
679206                 Wp   =          109
48729
 YDOT =       2841
740867  meter/sec      RA   =          118
32049  deg
 ZDOT =      -6013
967424                 TA   =           75
79273
                                          MA   =           75
63382
                                          Ha   =            223
642  n
mi
                                          Hp   =            212
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11629908
13                 X    =         3611410
53
 Y    =      -18920487
40  feet           Y    =        -5726951
78  meter
 Z    =       -1614442
80                 Z    =         -474701
05
 XDOT =      12495
666686                 XDOT =        3805
832077
 YDOT =       9323
296808  feet/sec       YDOT =        2884
316440  meter/sec
 ZDOT =     -19730
864251                 ZDOT =       -5995
472750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21670358
82                 X    =         6605125
37
 Y    =        4886602
95  feet           Y    =         1489436
58  meter
 Z    =       -1537105
19                 Z    =         -468509
66
 XDOT =      -4375
481284                 XDOT =       -1333
646695
 YDOT =      13381
575909  feet/sec       YDOT =        4078
704337  meter/sec
 ZDOT =     -19650
111706                 ZDOT =       -5989
354048


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   17007
53825815  
00016717  00000-0  10270-3 0  9043
2 25544  51
6415 119
1613 0007073  59
8494 300
3359 15
54014772 36763


Satellite: ISS
Catalog Number: 25544
Epoch time:      17007
53825815   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:       119
1613  deg
Eccentricity:     
0007073     
Arg of perigee:    59
8494  deg
Mean anomaly:     300
3359  deg
Mean motion:   15
54014772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3676
Checksum:              310


Coasting Arc #6 (Orbit 3691)
---------------------------------------

Vector Time (GMT): 2017/008/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3976500
19                 A    =         6787812
82  meter
 Y    =        5072437
66  meter          E    =           
0021031
 Z    =        2096018
44                 I    =           51
99603
 XDOT =      -2788
017239                 Wp   =           67
34933
 YDOT =      -4497
610977  meter/sec      RA   =          113
37354  deg
 ZDOT =       5558
679311                 TA   =          315
75928
                                          MA   =          315
92723
                                          Ha   =            223
707  n
mi
                                          Hp   =            212
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13046260
45                 X    =        -4043107
41
 Y    =       16641855
84  feet           Y    =         5027597
20  meter
 Z    =        6876700
91                 Z    =         2076540
32
 XDOT =      -9147
038185                 XDOT =       -2764
518006
 YDOT =     -14755
941524  feet/sec       YDOT =       -4528
657428  meter/sec
 ZDOT =      18237
136847                 ZDOT =        5545
192728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20102010
69                 X    =        -6127092
86
 Y    =       -6651836
79  feet           Y    =        -2027479
85  meter
 Z    =        6790252
30                 Z    =         2069668
90
 XDOT =      10239
659128                 XDOT =        3121
048102
 YDOT =     -12264
236469  feet/sec       YDOT =       -3738
139276  meter/sec
 ZDOT =      18178
671263                 ZDOT =        5540
859001


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   17008
56716407  
00016717  00000-0  10270-3 0  9054
2 25544  51
6425 114
0337 0007132  63
2536 296
9346 15
54027557 36922


Satellite: ISS
Catalog Number: 25544
Epoch time:      17008
56716407   =   yrday
fracday
Element set:     905
Inclination:       51
6425  deg
RA of node:       114
0337  deg
Eccentricity:     
0007132     
Arg of perigee:    63
2536  deg
Mean anomaly:     296
9346  deg
Mean motion:   15
54027557  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3692
Checksum:              310


Coasting Arc #7 (Orbit 3697)
---------------------------------------

Vector Time (GMT): 2017/008/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3467428
55                 A    =         6777915
31  meter
 Y    =       -2457386
02  meter          E    =           
0010773
 Z    =        5272608
69                 I    =           51
96592
 XDOT =       3428
387005                 Wp   =           60
63318
 YDOT =      -6806
236473  meter/sec      RA   =          111
36946  deg
 ZDOT =       -911
003374                 TA   =           38
07209
                                          MA   =           37
99601
                                          Ha   =            223
863  n
mi
                                          Hp   =            212
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11376077
93                 X    =        -3465303
53
 Y    =       -8062290
09  feet           Y    =        -2496149
63  meter
 Z    =       17298584
95                 Z    =         5255769
94
 XDOT =      11247
988861                 XDOT =        3508
666507
 YDOT =     -22330
172156  feet/sec       YDOT =       -6767
449008  meter/sec
 ZDOT =      -2988
856213                 ZDOT =        -894
154794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10911663
18                 X    =        -3325874
94
 Y    =        8825552
32  feet           Y    =         2690028
35  meter
 Z    =       17225038
31                 Z    =         5250191
68
 XDOT =     -17722
668230                 XDOT =       -5401
869276
 YDOT =     -16183
091772  feet/sec       YDOT =       -4932
606372  meter/sec
 ZDOT =      -2913
649166                 ZDOT =        -888
080266


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   17008
95300325  
00016717  00000-0  10270-3 0  9066
2 25544  51
6403 112
1133 0007382  61
1068 299
0829 15
54021704 36989


Satellite: ISS
Catalog Number: 25544
Epoch time:      17008
95300325   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       112
1133  deg
Eccentricity:     
0007382     
Arg of perigee:    61
1068  deg
Mean anomaly:     299
0829  deg
Mean motion:   15
54021704  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3698
Checksum:              289


Coasting Arc #8 (Orbit 3712)
---------------------------------------

Vector Time (GMT): 2017/009/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2721474
92                 A    =         6780052
81  meter
 Y    =        3983936
12  meter          E    =           
0017165
 Z    =       -4778435
93                 I    =           51
98467
 XDOT =      -3966
498757                 Wp   =           91
23330
 YDOT =       5957
926678  meter/sec      RA   =          106
39631  deg
 ZDOT =       2716
314477                 TA   =          205
49103
                                          MA   =          205
57578
                                          Ha   =            223
778  n
mi
                                          Hp   =            212
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8928723
48                 X    =         2699934
52
 Y    =       13070656
55  feet           Y    =         4014249
45  meter
 Z    =      -15677283
24                 Z    =        -4765267
84
 XDOT =     -13013
447365                 XDOT =       -4046
021534
 YDOT =      19547
003538  feet/sec       YDOT =        5913
125748  meter/sec
 ZDOT =       8911
792903                 ZDOT =        2696
853847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14960437
97                 X    =         4559941
49
 Y    =       -5342112
43  feet           Y    =        -1628275
87  meter
 Z    =      -15620131
44                 Z    =        -4761016
06
 XDOT =      15111
463514                 XDOT =        4605
974079
 YDOT =      16592
078877  feet/sec       YDOT =        5057
265642  meter/sec
 ZDOT =       8825
237291                 ZDOT =        2689
932326


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   17009
91759383  
00016717  00000-0  10270-3 0  9076
2 25544  51
6410 107
3056 0007386  63
9056 296
2856 15
54023484 37132


Satellite: ISS
Catalog Number: 25544
Epoch time:      17009
91759383   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       107
3056  deg
Eccentricity:     
0007386     
Arg of perigee:    63
9056  deg
Mean anomaly:     296
2856  deg
Mean motion:   15
54023484  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3713
Checksum:              322


Coasting Arc #9 (Orbit 3728)
---------------------------------------

Vector Time (GMT): 2017/010/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1927649
44                 A    =         6783580
09  meter
 Y    =       -5296316
74  meter          E    =           
0018894
 Z    =        3762664
54                 I    =           52
00518
 XDOT =       4353
620021                 Wp   =           77
27582
 YDOT =      -4644
061363  meter/sec      RA   =          101
43207  deg
 ZDOT =      -4284
462792                 TA   =           57
93113
                                          MA   =           57
74780
                                          Ha   =            223
820  n
mi
                                          Hp   =            212
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6324309
18                 X    =        -1886558
45
 Y    =      -17376367
24  feet           Y    =        -5317643
60  meter
 Z    =       12344699
92                 Z    =         3753399
99
 XDOT =      14283
530251                 XDOT =        4426
039222
 YDOT =     -15236
421793  feet/sec       YDOT =       -4594
970937  meter/sec
 ZDOT =     -14056
636457                 ZDOT =       -4263
138929

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18408722
53                 X    =        -5610978
63
 Y    =        2008511
32  feet           Y    =          612194
25  meter
 Z    =       12304936
35                 Z    =         3750544
60
 XDOT =     -11158
979989                 XDOT =       -3401
257101
 YDOT =     -16292
900769  feet/sec       YDOT =       -4966
076154  meter/sec
 ZDOT =     -13962
108043                 ZDOT =       -4255
650531


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   17010
94648529  
00016717  00000-0  10270-3 0  9081
2 25544  51
6412 102
1778 0007484  67
1012 293
0930 15
54053057 37299


Satellite: ISS
Catalog Number: 25544
Epoch time:      17010
94648529   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       102
1778  deg
Eccentricity:     
0007484     
Arg of perigee:    67
1012  deg
Mean anomaly:     293
0930  deg
Mean motion:   15
54053057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3729
Checksum:              304


Coasting Arc #10 (Orbit 3743)
---------------------------------------

Vector Time (GMT): 2017/011/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1192530
72                 A    =         6787115
26  meter
 Y    =        6228218
05  meter          E    =           
0012686
 Z    =       -2418047
71                 I    =           52
02244
 XDOT =      -4572
467148                 Wp   =           60
67542
 YDOT =       2958
395247  meter/sec      RA   =           96
47863  deg
 ZDOT =       5392
219285                 TA   =          272
45248
                                          MA   =          272
59771
                                          Ha   =            223
810  n
mi
                                          Hp   =            212
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3912502
37                 X    =         1134542
10
 Y    =       20433786
27  feet           Y    =         6241229
71  meter
 Z    =       -7933227
40                 Z    =        -2412395
13
 XDOT =     -15001
532637                 XDOT =       -4631
401291
 YDOT =       9706
021152  feet/sec       YDOT =        2906
932846  meter/sec
 ZDOT =      17691
008153                 ZDOT =        5369
865044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20800789
55                 X    =         6340080
65
 Y    =         741767
71  feet           Y    =          226090
80  meter
 Z    =       -7909508
69                 Z    =        -2410818
25
 XDOT =       6106
244539                 XDOT =        1861
183336
 YDOT =      15397
944125  feet/sec       YDOT =        4693
293369  meter/sec
 ZDOT =      17592
238856                 ZDOT =        5362
114403


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   17011
91106662  
00016717  00000-0  10270-3 0  9097
2 25544  51
6412  97
3710 0007409  70
8034 289
3920 15
54040343 37440


Satellite: ISS
Catalog Number: 25544
Epoch time:      17011
91106662   =   yrday
fracday
Element set:     909
Inclination:       51
6412  deg
RA of node:        97
3710  deg
Eccentricity:     
0007409     
Arg of perigee:    70
8034  deg
Mean anomaly:     289
3920  deg
Mean motion:   15
54040343  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3744
Checksum:              291


Coasting Arc #11 (Orbit 3759)
---------------------------------------

Vector Time (GMT): 2017/012/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -418484
44                 A    =         6789293
52  meter
 Y    =       -6727076
66  meter          E    =           
0018782
 Z    =         766663
25                 I    =           52
03379
 XDOT =       4695
992462                 Wp   =          108
46560
 YDOT =       -986
837857  meter/sec      RA   =           91
53260  deg
 ZDOT =      -5981
932470                 TA   =           63
29231
                                          MA   =           63
10017
                                          Ha   =            223
808  n
mi
                                          Hp   =            212
139

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1372980
44                 X    =         -346953
44
 Y    =      -22070461
47  feet           Y    =        -6731356
53  meter
 Z    =        2515299
37                 Z    =          764803
65
 XDOT =      15406
799415                 XDOT =        4735
735338
 YDOT =      -3237
657010  feet/sec       YDOT =        -934
101453  meter/sec
 ZDOT =     -19625
762696                 ZDOT =       -5959
024711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21874782
70                 X    =        -6667433
77
 Y    =       -3243324
76  feet           Y    =         -988565
39  meter
 Z    =        2508346
46                 Z    =          764544
00
 XDOT =       -165
586344                 XDOT =         -50
470718
 YDOT =     -14272
929591  feet/sec       YDOT =       -4350
388939  meter/sec
 ZDOT =     -19524
906396                 ZDOT =       -5951
191470


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   17012
93994672  
00016717  00000-0  10270-3 0  9108
2 25544  51
6425  92
2424 0007444  74
3367 285
8606 15
54056264 37606


Satellite: ISS
Catalog Number: 25544
Epoch time:      17012
93994672   =   yrday
fracday
Element set:     910
Inclination:       51
6425  deg
RA of node:        92
2424  deg
Eccentricity:     
0007444     
Arg of perigee:    74
3367  deg
Mean anomaly:     285
8606  deg
Mean motion:   15
54056264  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3760
Checksum:              318


Coasting Arc #12 (Orbit 3775)
---------------------------------------

Vector Time (GMT): 2017/013/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -304494
18                 A    =         6789185
97  meter
 Y    =        6713698
89  meter          E    =           
0020594
 Z    =         901231
36                 I    =           52
03260
 XDOT =      -4720
377270                 Wp   =           62
73308
 YDOT =      -1026
867024  meter/sec      RA   =           86
58997  deg
 ZDOT =       5959
918467                 TA   =          306
97279
                                          MA   =          307
16115
                                          Ha   =            223
844  n
mi
                                          Hp   =            212
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -998996
67                 X    =         -383923
52
 Y    =       22026571
17  feet           Y    =         6709849
67  meter
 Z    =        2956795
79                 Z    =          899559
67
 XDOT =     -15486
802067                 XDOT =       -4737
493570
 YDOT =      -3368
986298  feet/sec       YDOT =       -1079
749466  meter/sec
 ZDOT =      19553
538277                 ZDOT =        5936
947141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21423314
40                 X    =         6529826
23
 Y    =        5221115
48  feet           Y    =         1591396
00  meter
 Z    =        2948224
24                 Z    =          898618
75
 XDOT =      -5916
642288                 XDOT =       -1803
392569
 YDOT =      13116
516764  feet/sec       YDOT =        3997
914310  meter/sec
 ZDOT =      19452
762559                 ZDOT =        5929
202028


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   17013
96882057  
00016717  00000-0  10270-3 0  9116
2 25544  51
6417  87
1147 0007513  77
5306 282
6687 15
54062161 37761


Satellite: ISS
Catalog Number: 25544
Epoch time:      17013
96882057   =   yrday
fracday
Element set:     911
Inclination:       51
6417  deg
RA of node:        87
1147  deg
Eccentricity:     
0007513     
Arg of perigee:    77
5306  deg
Mean anomaly:     282
6687  deg
Mean motion:   15
54062161  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3776
Checksum:              321


Coasting Arc #13 (Orbit 3790)
---------------------------------------

Vector Time (GMT): 2017/014/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1096004
15                 A    =         6786739
81  meter
 Y    =       -6198699
00  meter          E    =           
0011603
 Z    =       -2543022
76                 I    =           52
02252
 XDOT =       4634
345700                 Wp   =          100
76676
 YDOT =       2991
269794  meter/sec      RA   =           81
64368  deg
 ZDOT =      -5316
610773                 TA   =          107
60528
                                          MA   =          107
47851
                                          Ha   =            223
801  n
mi
                                          Hp   =            212
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3595814
14                 X    =         1177590
67
 Y    =      -20336938
98  feet           Y    =        -6185986
50  meter
 Z    =       -8343250
53                 Z    =        -2537500
81
 XDOT =      15204
546261                 XDOT =        4626
377119
 YDOT =       9813
877278  feet/sec       YDOT =        3043
049751  meter/sec
 ZDOT =     -17442
948730                 ZDOT =       -5294
118258

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19386887
26                 X    =        -5909123
24
 Y    =       -7147928
19  feet           Y    =        -2178688
51  meter
 Z    =       -8317843
49                 Z    =        -2535278
70
 XDOT =      11816
900951                 XDOT =        3601
791410
 YDOT =     -11953
443959  feet/sec       YDOT =       -3643
409719  meter/sec
 ZDOT =     -17344
634801                 ZDOT =       -5286
644687


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   17014
93338465  
00016717  00000-0  10270-3 0  9124
2 25544  51
6424  82
3070 0007455  81
1284 279
0712 15
54080368 37917


Satellite: ISS
Catalog Number: 25544
Epoch time:      17014
93338465   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:        82
3070  deg
Eccentricity:     
0007455     
Arg of perigee:    81
1284  deg
Mean anomaly:     279
0712  deg
Mean motion:   15
54080368  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3791
Checksum:              305


Coasting Arc #14 (Orbit 3806)
---------------------------------------

Vector Time (GMT): 2017/015/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1867886
58                 A    =         6783137
37  meter
 Y    =        5236695
47  meter          E    =           
0018627
 Z    =        3870475
36                 I    =           52
00473
 XDOT =      -4445
405781                 Wp   =           92
82550
 YDOT =      -4673
901474  meter/sec      RA   =           76
68841  deg
 ZDOT =       4160
285467                 TA   =          313
64265
                                          MA   =          313
79697
                                          Ha   =            223
853  n
mi
                                          Hp   =            212
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6128236
81                 X    =        -1945106
38
 Y    =       17180759
40  feet           Y    =         5215375
72  meter
 Z    =       12698409
98                 Z    =         3861214
37
 XDOT =     -14584
664637                 XDOT =       -4413
018899
 YDOT =     -15334
322422  feet/sec       YDOT =       -4723
431927  meter/sec
 ZDOT =      13649
230534                 ZDOT =        4138
770076

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15986663
68                 X    =         4872735
09
 Y    =        8844034
26  feet           Y    =         2695661
64  meter
 Z    =       12656738
86                 Z    =         3857774
00
 XDOT =     -16811
389712                 XDOT =       -5124
111584
 YDOT =      10904
052717  feet/sec       YDOT =        3323
555268  meter/sec
 ZDOT =      13555
523199                 ZDOT =        4131
723471


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   17015
96224749  
00016717  00000-0  10270-3 0  9138
2 25544  51
6423  77
1787 0007454  84
8958 275
3046 15
54084378 38072


Satellite: ISS
Catalog Number: 25544
Epoch time:      17015
96224749   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:        77
1787  deg
Eccentricity:     
0007454     
Arg of perigee:    84
8958  deg
Mean anomaly:     275
3046  deg
Mean motion:   15
54084378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3807
Checksum:              344


Coasting Arc #15 (Orbit 3807)
---------------------------------------

Vector Time (GMT): 2017/015/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3702861
61                 A    =         6785228
97  meter
 Y    =       -4707353
38  meter          E    =           
0020279
 Z    =        3171121
64                 I    =           52
01235
 XDOT =       2600
688158                 Wp   =           90
73808
 YDOT =      -5338
214296  meter/sec      RA   =           76
23505  deg
 ZDOT =      -4861
032608                 TA   =           52
84098
                                          MA   =           52
65595
                                          Ha   =            223
836  n
mi
                                          Hp   =            212
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12148496
08                 X    =        -3665351
06
 Y    =      -15444072
77  feet           Y    =        -4748551
55  meter
 Z    =       10403942
39                 Z    =         3153225
68
 XDOT =       8532
441464                 XDOT =        2683
800271
 YDOT =     -17513
826431  feet/sec       YDOT =       -5308
666928  meter/sec
 ZDOT =     -15948
269712                 ZDOT =       -4848
197638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10223325
71                 X    =        -3116069
68
 Y    =       16828594
22  feet           Y    =         5129355
52  meter
 Z    =       10326150
59                 Z    =         3147410
70
 XDOT =     -18199
022943                 XDOT =       -5547
062193
 YDOT =      -1251
407087  feet/sec       YDOT =        -381
428880  meter/sec
 ZDOT =     -15890
870140                 ZDOT =       -4843
537219


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   17016
02655056  
00016717  00000-0  10270-3 0  9146
2 25544  51
6435  76
8592 0007440  84
6769 275
5233 15
54094059 38086


Satellite: ISS
Catalog Number: 25544
Epoch time:      17016
02655056   =   yrday
fracday
Element set:     914
Inclination:       51
6435  deg
RA of node:        76
8592  deg
Eccentricity:     
0007440     
Arg of perigee:    84
6769  deg
Mean anomaly:     275
5233  deg
Mean motion:   15
54094059  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3808
Checksum:              326


Coasting Arc #16 (Orbit 3822)
---------------------------------------

Vector Time (GMT): 2017/016/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3311780
75                 A    =         6788199
45  meter
 Y    =        5679638
69  meter          E    =           
0013747
 Z    =       -1682833
96                 I    =           52
01382
 XDOT =      -3472
315948                 Wp   =           61
95309
 YDOT =       3712
057067  meter/sec      RA   =           71
28340  deg
 ZDOT =       5736
788912                 TA   =          279
70957
                                          MA   =          279
86482
                                          Ha   =            223
745  n
mi
                                          Hp   =            212
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10865422
39                 X    =         3256197
69
 Y    =       18633985
20  feet           Y    =         5716362
45  meter
 Z    =       -5521108
78                 Z    =        -1666881
64
 XDOT =     -11392
112690                 XDOT =       -3541
433169
 YDOT =      12178
664918  feet/sec       YDOT =        3672
840889  meter/sec
 ZDOT =      18821
485932                 ZDOT =        5719
753810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13382434
77                 X    =         4078966
12
 Y    =      -16939630
41  feet           Y    =        -5163199
35  meter
 Z    =       -5452046
54                 Z    =        -1661783
79
 XDOT =      14302
480373                 XDOT =        4359
396018
 YDOT =       5310
440822  feet/sec       YDOT =        1618
622362  meter/sec
 ZDOT =      18745
920612                 ZDOT =        5713
756603


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   17016
99110211  
00016717  00000-0  10270-3 0  9152
2 25544  51
6434  72
0507 0007362  87
7607 272
4389 15
54111979 38233


Satellite: ISS
Catalog Number: 25544
Epoch time:      17016
99110211   =   yrday
fracday
Element set:     915
Inclination:       51
6434  deg
RA of node:        72
0507  deg
Eccentricity:     
0007362     
Arg of perigee:    87
7607  deg
Mean anomaly:     272
4389  deg
Mean motion:   15
54111979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              309


Coasting Arc #17 (Orbit 3838)
---------------------------------------

Vector Time (GMT): 2017/017/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2692170
82                 A    =         6789507
78  meter
 Y    =       -6226378
26  meter          E    =           
0018164
 Z    =         -42270
16                 I    =           52
00576
 XDOT =       4343
244983                 Wp   =          118
93408
 YDOT =      -1850
238762  meter/sec      RA   =           66
33835  deg
 ZDOT =      -6043
447700                 TA   =           61
51896
                                          MA   =           61
33612
                                          Ha   =            223
801  n
mi
                                          Hp   =            212
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8832581
42                 X    =        -2622140
44
 Y    =      -20427750
20  feet           Y    =        -6256092
37  meter
 Z    =        -138681
64                 Z    =          -55177
58
 XDOT =      14249
491415                 XDOT =        4392
967805
 YDOT =      -6070
337145  feet/sec       YDOT =       -1801
391729  meter/sec
 ZDOT =     -19827
584316                 ZDOT =       -6022
229011

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15535503
18                 X    =        -4735221
37
 Y    =       15935404
41  feet           Y    =         4857111
26  meter
 Z    =        -194249
14                 Z    =          -59207
14
 XDOT =      -9921
000155                 XDOT =       -3023
920847
 YDOT =      -9856
529118  feet/sec       YDOT =       -3004
270075  meter/sec
 ZDOT =     -19733
974822                 ZDOT =       -6014
915526


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   17018
01995414  
00016717  00000-0  10270-3 0  9164
2 25544  51
6427  66
9223 0007387  92
9504 267
2494 15
54066614 38394


Satellite: ISS
Catalog Number: 25544
Epoch time:      17018
01995414   =   yrday
fracday
Element set:     916
Inclination:       51
6427  deg
RA of node:        66
9223  deg
Eccentricity:     
0007387     
Arg of perigee:    92
9504  deg
Mean anomaly:     267
2494  deg
Mean motion:   15
54066614  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3839
Checksum:              332


Coasting Arc #18 (Orbit 3854)
---------------------------------------

Vector Time (GMT): 2017/018/23:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1911009
07                 A    =         6788087
10  meter
 Y    =        6279296
94  meter          E    =           
0020481
 Z    =        1700283
20                 I    =           51
98793
 XDOT =      -5104
804321                 Wp   =           74
59929
 YDOT =        -11
167893  meter/sec      RA   =           61
39136  deg
 ZDOT =       5726
806733                 TA   =          303
95975
                                          MA   =          304
15425
                                          Ha   =            223
634  n
mi
                                          Hp   =            212
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6269714
78                 X    =         1832391
25
 Y    =       20601367
92  feet           Y    =         6300227
57  meter
 Z    =        5578356
97                 Z    =         1709375
21
 XDOT =     -16748
045671                 XDOT =       -5132
117812
 YDOT =        -36
640068  feet/sec       YDOT =         -68
405927  meter/sec
 ZDOT =      18788
736002                 ZDOT =        5701
943057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16448055
21                 X    =         5013367
23
 Y    =      -13883552
78  feet           Y    =        -4231706
89  meter
 Z    =        5617133
79                 Z    =         1712102
38
 XDOT =       5637
344592                 XDOT =        1718
262632
 YDOT =      14304
579734  feet/sec       YDOT =        4360
035903  meter/sec
 ZDOT =      18679
456075                 ZDOT =        5693
498212


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   17019
04879769  
00016717  00000-0  10270-3 0  9173
2 25544  51
6428  61
7935 0007206  95
3275 264
8700 15
54130433 38552


Satellite: ISS
Catalog Number: 25544
Epoch time:      17019
04879769   =   yrday
fracday
Element set:     917
Inclination:       51
6428  deg
RA of node:        61
7935  deg
Eccentricity:     
0007206     
Arg of perigee:    95
3275  deg
Mean anomaly:     264
8700  deg
Mean motion:   15
54130433  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3855
Checksum:              329
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