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

 
Date: January 1st 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


011/02:13:29 648 -0 2 4 9 4 9
N/A 4 4 -0 6 221 9
000/00:16:59 296 -2 2 -0 4 214 0

Coasting Arc #1 (Orbit 1890)
---------------------------------------

Vector Time (GMT): 2016/001/13:32:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3831218
94                 A    =         6778927
15  meter
 Y    =       -3769807
71  meter          E    =           
0013488
 Z    =        4131046
64                 I    =           51
67403
 XDOT =       6287
659929                 Wp   =           38
31673
 YDOT =       2227
041971  meter/sec      RA   =          172
87570  deg
 ZDOT =      -3782
037544                 TA   =           90
71589
                                          MA   =           90
56134
                                          Ha   =            220
633  n
mi
                                          Hp   =            212
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12569615
94                 X    =         3853022
27
 Y    =      -12368135
54  feet           Y    =        -3726842
69  meter
 Z    =       13553302
61                 Z    =         4149710
59
 XDOT =      20628
805540                 XDOT =        6280
660791
 YDOT =       7306
568146  feet/sec       YDOT =        2297
315710  meter/sec
 ZDOT =     -12408
259658                 ZDOT =       -3751
510610

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17164733
12                 X    =         5231810
66
 Y    =        3758094
45  feet           Y    =         1145467
19  meter
 Z    =       13634760
58                 Z    =         4155875
03
 XDOT =       5394
624264                 XDOT =        1644
281476
 YDOT =      20101
698067  feet/sec       YDOT =        6126
997571  meter/sec
 ZDOT =     -12276
469761                 ZDOT =       -3741
867983


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   16001
60556047  
00016717  00000-0  10270-3 0  9008
2 25544  51
6392 173
8287 0008272 347
9072  12
1881 15
55186618 18911


Satellite: ISS
Catalog Number: 25544
Epoch time:      16001
60556047   =   yrday
fracday
Element set:     900
Inclination:       51
6392  deg
RA of node:       173
8287  deg
Eccentricity:     
0008272     
Arg of perigee:   347
9072  deg
Mean anomaly:      12
1881  deg
Mean motion:   15
55186618  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1891
Checksum:              313


Coasting Arc #2 (Orbit 1905)
---------------------------------------

Vector Time (GMT): 2016/002/13:32:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5387989
24                 A    =         6783304
87  meter
 Y    =        3219700
70  meter          E    =           
0011722
 Z    =       -2556855
61                 I    =           51
72199
 XDOT =      -4474
531890                 Wp   =           14
35830
 YDOT =      -3304
600667  meter/sec      RA   =          167
88981  deg
 ZDOT =       5284
029752                 TA   =          316
91885
                                          MA   =          317
01054
                                          Ha   =            220
704  n
mi
                                          Hp   =            212
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17677130
05                 X    =        -5411172
15
 Y    =       10563322
50  feet           Y    =         3159319
09  meter
 Z    =       -8388633
89                 Z    =        -2583085
38
 XDOT =     -14680
222737                 XDOT =       -4462
914066
 YDOT =     -10841
865706  feet/sec       YDOT =       -3354
573042  meter/sec
 ZDOT =      17336
055617                 ZDOT =        5262
321671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18596558
72                 X    =        -5668231
10
 Y    =       -8735263
00  feet           Y    =        -2662508
16  meter
 Z    =       -8502768
46                 Z    =        -2591643
83
 XDOT =        110
077164                 XDOT =          33
551519
 YDOT =     -16966
788635  feet/sec       YDOT =       -5171
477176  meter/sec
 ZDOT =      17242
624733                 ZDOT =        5255
552019


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   16002
56941713  
00016717  00000-0  10270-3 0  9013
2 25544  51
6406 169
0160 0008342 351
6259   8
4754 15
55218639 19064


Satellite: ISS
Catalog Number: 25544
Epoch time:      16002
56941713   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:       169
0160  deg
Eccentricity:     
0008342     
Arg of perigee:   351
6259  deg
Mean anomaly:       8
4754  deg
Mean motion:   15
55218639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1906
Checksum:              301


Coasting Arc #3 (Orbit 1921)
---------------------------------------

Vector Time (GMT): 2016/003/13:32:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6322252
31                 A    =         6785939
56  meter
 Y    =       -2400444
06  meter          E    =           
0009498
 Z    =         555126
36                 I    =           51
76129
 XDOT =       2155
846920                 Wp   =           89
08606
 YDOT =       4273
013140  meter/sec      RA   =          162
91799  deg
 ZDOT =      -5986
888692                 TA   =           84
93510
                                          MA   =           84
82669
                                          Ha   =            220
876  n
mi
                                          Hp   =            212
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20742297
61                 X    =         6345928
21
 Y    =       -7875472
62  feet           Y    =        -2329612
09  meter
 Z    =        1821280
71                 Z    =          585895
81
 XDOT =       7072
988584                 XDOT =        2136
986640
 YDOT =      14019
071983  feet/sec       YDOT =        4297
016013  meter/sec
 ZDOT =     -19642
023268                 ZDOT =       -5976
461741

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18317059
61                 X    =         5583039
77
 Y    =       12499861
88  feet           Y    =         3809957
90  meter
 Z    =        1954948
32                 Z    =          595868
25
 XDOT =      -6468
870937                 XDOT =       -1971
711862
 YDOT =      12586
745499  feet/sec       YDOT =        3836
440028  meter/sec
 ZDOT =     -19597
606159                 ZDOT =       -5973
350357


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   16003
59752299  
00016717  00000-0  10270-3 0  9027
2 25544  51
6399 163
8816 0008433 355
1019   5
0050 15
55241835 19223


Satellite: ISS
Catalog Number: 25544
Epoch time:      16003
59752299   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       163
8816  deg
Eccentricity:     
0008433     
Arg of perigee:   355
1019  deg
Mean anomaly:       5
0050  deg
Mean motion:   15
55241835  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1922
Checksum:              304


Coasting Arc #4 (Orbit 1937)
---------------------------------------

Vector Time (GMT): 2016/004/13:36:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6155948
46                 A    =         6782713
97  meter
 Y    =          97899
34  meter          E    =           
0016905
 Z    =        2820077
69                 I    =           51
78241
 XDOT =       2263
538145                 Wp   =           50
88658
 YDOT =      -5261
401809  meter/sec      RA   =          157
94716  deg
 ZDOT =       5113
659674                 TA   =          341
12205
                                          MA   =          341
18465
                                          Ha   =            221
012  n
mi
                                          Hp   =            212
216

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20196681
28                 X    =        -6170284
45
 Y    =         321192
06  feet           Y    =           28979
16  meter
 Z    =        9252223
40                 Z    =         2790138
69
 XDOT =       7426
306250                 XDOT =        2297
364139
 YDOT =     -17261
816958  feet/sec       YDOT =       -5235
900540  meter/sec
 ZDOT =      16777
098668                 ZDOT =        5124
737333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12412855
17                 X    =        -3783438
26
 Y    =      -16009782
06  feet           Y    =        -4879781
57  meter
 Z    =        9122534
84                 Z    =         2780548
62
 XDOT =      17031
367665                 XDOT =        5191
160864
 YDOT =      -3598
210416  feet/sec       YDOT =       -1096
734535  meter/sec
 ZDOT =      16825
992356                 ZDOT =        5128
562470


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   16004
62561991  
00016717  00000-0  10270-3 0  9030
2 25544  51
6413 158
7477 0008354 358
9775   1
1359 15
55275045 19384


Satellite: ISS
Catalog Number: 25544
Epoch time:      16004
62561991   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       158
7477  deg
Eccentricity:     
0008354     
Arg of perigee:   358
9775  deg
Mean anomaly:       1
1359  deg
Mean motion:   15
55275045  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1938
Checksum:              328


Coasting Arc #5 (Orbit 1952)
---------------------------------------

Vector Time (GMT): 2016/005/13:36:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5055077
65                 A    =         6778186
27  meter
 Y    =        1263460
43  meter          E    =           
0014156
 Z    =       -4349401
19                 I    =           51
79629
 XDOT =      -4319
206593                 Wp   =           36
41727
 YDOT =       5279
751488  meter/sec      RA   =          152
96518  deg
 ZDOT =      -3480
969611                 TA   =          198
21718
                                          MA   =          198
26794
                                          Ha   =            221
103  n
mi
                                          Hp   =            212
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16584900
44                 X    =         5061701
23
 Y    =        4145211
37  feet           Y    =         1320026
95  meter
 Z    =      -14269688
95                 Z    =        -4324828
62
 XDOT =     -14170
625305                 XDOT =       -4361
015942
 YDOT =      17322
019316  feet/sec       YDOT =        5231
217709  meter/sec
 ZDOT =     -11420
503972                 ZDOT =       -3502
052545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6963614
93                 X    =         2122509
83
 Y    =       15708913
41  feet           Y    =         4788076
81  meter
 Z    =      -14163468
12                 Z    =        -4317025
08
 XDOT =     -21181
486126                 XDOT =       -6456
116971
 YDOT =      -1006
354322  feet/sec       YDOT =        -306
736797  meter/sec
 ZDOT =     -11512
752772                 ZDOT =       -3509
087045


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   16005
58945503  
00016717  00000-0  10270-3 0  9042
2 25544  51
6412 153
9349 0008485   2
2954 357
8236 15
55248497 19534


Satellite: ISS
Catalog Number: 25544
Epoch time:      16005
58945503   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:       153
9349  deg
Eccentricity:     
0008485     
Arg of perigee:     2
2954  deg
Mean anomaly:     357
8236  deg
Mean motion:   15
55248497  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1953
Checksum:              330


Coasting Arc #6 (Orbit 1968)
---------------------------------------

Vector Time (GMT): 2016/006/13:36:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3420032
74                 A    =         6774523
95  meter
 Y    =       -2678644
28  meter          E    =           
0007482
 Z    =        5193291
10                 I    =           51
81350
 XDOT =       5798
025601                 Wp   =           36
77047
 YDOT =      -4852
269864  meter/sec      RA   =          147
96998  deg
 ZDOT =       1320
401463                 TA   =           40
61417
                                          MA   =           40
55838
                                          Ha   =            221
226  n
mi
                                          Hp   =            211
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11220579
86                 X    =        -3415052
12
 Y    =       -8788203
03  feet           Y    =        -2716861
90  meter
 Z    =       17038356
62                 Z    =         5176689
29
 XDOT =      19022
393703                 XDOT =        5845
439998
 YDOT =     -15919
520550  feet/sec       YDOT =       -4787
167500  meter/sec
 ZDOT =       4332
025796                 ZDOT =        1348
681681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -263391
25                 X    =          -80281
65
 Y    =      -14335072
73  feet           Y    =        -4369330
17  meter
 Z    =       16966904
14                 Z    =         5171512
38
 XDOT =      23266
903744                 XDOT =        7091
752261
 YDOT =       4826
883770  feet/sec       YDOT =        1471
234173  meter/sec
 ZDOT =       4455
398549                 ZDOT =        1358
005478


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   16006
61753504  
00016717  00000-0  10270-3 0  9056
2 25544  51
6419 148
8003 0008567   5
9234 354
2019 15
55305502 19691


Satellite: ISS
Catalog Number: 25544
Epoch time:      16006
61753504   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:       148
8003  deg
Eccentricity:     
0008567     
Arg of perigee:     5
9234  deg
Mean anomaly:     354
2019  deg
Mean motion:   15
55305502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1969
Checksum:              301


Coasting Arc #7 (Orbit 1983)
---------------------------------------

Vector Time (GMT): 2016/007/13:36:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1555044
30                 A    =         6774257
33  meter
 Y    =        3999183
17  meter          E    =           
0017128
 Z    =       -5254696
52                 I    =           51
83959
 XDOT =      -6515
691882                 Wp   =           67
60857
 YDOT =       3889
956855  meter/sec      RA   =          142
97168  deg
 ZDOT =       1041
369918                 TA   =          212
29588
                                          MA   =          212
40086
                                          Ha   =            221
317  n
mi
                                          Hp   =            211
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5101851
37                 X    =         1535733
90
 Y    =       13120679
69  feet           Y    =         4016465
18  meter
 Z    =      -17239817
97                 Z    =        -5247189
07
 XDOT =     -21376
941869                 XDOT =       -6563
764598
 YDOT =      12762
325640  feet/sec       YDOT =        3816
825202  meter/sec
 ZDOT =       3416
567974                 ZDOT =        1009
601912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6735485
53                 X    =        -2052975
99
 Y    =       12406066
82  feet           Y    =         3781369
17  meter
 Z    =      -17207997
77                 Z    =        -5244997
72
 XDOT =     -22602
805563                 XDOT =       -6889
335136
 YDOT =      -7765
691233  feet/sec       YDOT =       -2366
982688  meter/sec
 ZDOT =       3278
230819                 ZDOT =         999
204754


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   16007
58135457  
00016717  00000-0  10270-3 0  9065
2 25544  51
6422 143
9882 0008686  10
3147 349
8183 15
55305587 19843


Satellite: ISS
Catalog Number: 25544
Epoch time:      16007
58135457   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       143
9882  deg
Eccentricity:     
0008686     
Arg of perigee:    10
3147  deg
Mean anomaly:     349
8183  deg
Mean motion:   15
55305587  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1984
Checksum:              332


Coasting Arc #8 (Orbit 1999)
---------------------------------------

Vector Time (GMT): 2016/008/13:36:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         384435
54                 A    =         6777451
33  meter
 Y    =       -5073408
22  meter          E    =           
0015850
 Z    =        4474660
59                 I    =           51
87566
 XDOT =       6507
276564                 Wp   =           42
31192
 YDOT =      -2408
014567  meter/sec      RA   =          137
97842  deg
 ZDOT =      -3271
134149                 TA   =           80
60228
                                          MA   =           80
42313
                                          Ha   =            221
444  n
mi
                                          Hp   =            211
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1261271
47                 X    =          419403
20
 Y    =      -16645040
10  feet           Y    =        -5068914
09  meter
 Z    =       14680644
98                 Z    =         4476612
56
 XDOT =      21349
332559                 XDOT =        6549
609626
 YDOT =      -7900
310258  feet/sec       YDOT =       -2335
008912  meter/sec
 ZDOT =     -10732
067419                 ZDOT =       -3239
420965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13358457
78                 X    =         4071657
93
 Y    =       -9996236
98  feet           Y    =        -3046853
03  meter
 Z    =       14690008
67                 Z    =         4477514
64
 XDOT =      19250
757278                 XDOT =        5867
630818
 YDOT =      10069
469210  feet/sec       YDOT =        3069
174215  meter/sec
 ZDOT =     -10594
208478                 ZDOT =       -3229
114744


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   16008
60942018  
00016717  00000-0  10270-3 0  9079
2 25544  51
6427 138
8536 0008749  14
5886 345
5518 15
55285960 20000


Satellite: ISS
Catalog Number: 25544
Epoch time:      16008
60942018   =   yrday
fracday
Element set:     907
Inclination:       51
6427  deg
RA of node:       138
8536  deg
Eccentricity:     
0008749     
Arg of perigee:    14
5886  deg
Mean anomaly:     345
5518  deg
Mean motion:   15
55285960  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2000
Checksum:              323


Coasting Arc #9 (Orbit 2014)
---------------------------------------

Vector Time (GMT): 2016/009/13:36:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2068151
04                 A    =         6782023
55  meter
 Y    =        5700329
39  meter          E    =           
0012006
 Z    =       -3030848
70                 I    =           51
91476
 XDOT =      -5816
065460                 Wp   =           34
88349
 YDOT =        523
283278  meter/sec      RA   =          133
00167  deg
 ZDOT =       4972
149930                 TA   =          290
50442
                                          MA   =          290
63324
                                          Ha   =            221
525  n
mi
                                          Hp   =            211
255

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6785272
44                 X    =        -2117017
39
 Y    =       18701868
08  feet           Y    =         5676928
98  meter
 Z    =       -9943729
34                 Z    =        -3041013
40
 XDOT =     -19081
579593                 XDOT =       -5845
637028
 YDOT =       1716
808655  feet/sec       YDOT =         458
078437  meter/sec
 ZDOT =      16312
827853                 ZDOT =        4943
825404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18420497
07                 X    =        -5614567
51
 Y    =        7455641
02  feet           Y    =         2272479
38  meter
 Z    =       -9988806
22                 Z    =        -3044588
14
 XDOT =     -13526
325677                 XDOT =       -4122
824066
 YDOT =     -11812
833436  feet/sec       YDOT =       -3600
551631  meter/sec
 ZDOT =      16189
972380                 ZDOT =        4934
703581


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   16009
57322239  
00016717  00000-0  10270-3 0  9084
2 25544  51
6433 134
0409 0008845  16
5548 343
5893 15
55286054 20153


Satellite: ISS
Catalog Number: 25544
Epoch time:      16009
57322239   =   yrday
fracday
Element set:     908
Inclination:       51
6433  deg
RA of node:       134
0409  deg
Eccentricity:     
0008845     
Arg of perigee:    16
5548  deg
Mean anomaly:     343
5893  deg
Mean motion:   15
55286054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2015
Checksum:              311


Coasting Arc #10 (Orbit 2030)
---------------------------------------

Vector Time (GMT): 2016/010/13:36:27
741
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3441182
89                 A    =         6785390
69  meter
 Y    =       -5748751
29  meter          E    =           
0014654
 Z    =        1063288
71                 I    =           51
94706
 XDOT =       4593
049340                 Wp   =           87
41716
 YDOT =       1642
407962  meter/sec      RA   =          128
04067  deg
 ZDOT =      -5914
154656                 TA   =           81
10156
                                          MA   =           80
93569
                                          Ha   =            221
601  n
mi
                                          Hp   =            211
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11289970
10                 X    =         3500046
15
 Y    =      -18860732
58  feet           Y    =        -5709940
66  meter
 Z    =        3488480
01                 Z    =         1080147
48
 XDOT =      15069
059513                 XDOT =        4603
070220
 YDOT =       5388
477565  feet/sec       YDOT =        1693
826914  meter/sec
 ZDOT =     -19403
394540                 ZDOT =       -5891
818596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21494723
99                 X    =         6551591
87
 Y    =       -4543668
98  feet           Y    =        -1384910
31  meter
 Z    =        3562592
31                 Z    =         1085878
14
 XDOT =       6036
676085                 XDOT =        1839
978871
 YDOT =      13241
266930  feet/sec       YDOT =        4035
938160  meter/sec
 ZDOT =     -19306
870782                 ZDOT =       -5884
734214


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   16010
60127123  
00016717  00000-0  10270-3 0  9096
2 25544  51
6431 128
9071 0008811  21
5723 338
5800 15
55311493 20318


Satellite: ISS
Catalog Number: 25544
Epoch time:      16010
60127123   =   yrday
fracday
Element set:     909
Inclination:       51
6431  deg
RA of node:       128
9071  deg
Eccentricity:     
0008811     
Arg of perigee:    21
5723  deg
Mean anomaly:     338
5800  deg
Mean motion:   15
55311493  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2031
Checksum:              268


Coasting Arc #11 (Orbit 2038)
---------------------------------------

Vector Time (GMT): 2016/011/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3623793
21                 A    =         6776852
69  meter
 Y    =        2116566
24  meter          E    =           
0016588
 Z    =       -5334465
68                 I    =           51
91917
 XDOT =      -4220
069087                 Wp   =           66
05031
 YDOT =       6381
105822  meter/sec      RA   =          125
41027  deg
 ZDOT =       -329
177013                 TA   =          200
78526
                                          MA   =          200
85279
                                          Ha   =            221
867  n
mi
                                          Hp   =            214
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11889085
33                 X    =         3625768
09
 Y    =        6944114
97  feet           Y    =         2157101
26  meter
 Z    =      -17501527
82                 Z    =        -5316857
52
 XDOT =     -13845
371021                 XDOT =       -4289
511562
 YDOT =      20935
386554  feet/sec       YDOT =        6333
525962  meter/sec
 ZDOT =      -1079
977077                 ZDOT =        -349
845049

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5781824
90                 X    =        -1762300
23
 Y    =      -12601358
69  feet           Y    =        -3840894
13  meter
 Z    =      -17425579
44                 Z    =        -5311316
61
 XDOT =      22473
229577                 XDOT =        6849
840375
 YDOT =      -8666
203058  feet/sec       YDOT =       -2641
458692  meter/sec
 ZDOT =      -1170
723069                 ZDOT =        -356
836391


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   16011
11530088  
00016717  00000-0  10270-3 0  9103
2 25544  51
6431 126
3411 0006095   3
1882 356
9309 15
54316681 20391


Satellite: ISS
Catalog Number: 25544
Epoch time:      16011
11530088   =   yrday
fracday
Element set:     910
Inclination:       51
6431  deg
RA of node:       126
3411  deg
Eccentricity:     
0006095     
Arg of perigee:     3
1882  deg
Mean anomaly:     356
9309  deg
Mean motion:   15
54316681  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2039
Checksum:              278


Coasting Arc #12 (Orbit 2054)
---------------------------------------

Vector Time (GMT): 2016/012/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2502982
66                 A    =         6777597
28  meter
 Y    =       -3660174
21  meter          E    =           
0010199
 Z    =        5123976
20                 I    =           51
93986
 XDOT =       4864
318774                 Wp   =           27
75969
 YDOT =      -5688
662269  meter/sec      RA   =          120
42819  deg
 ZDOT =      -1677
265726                 TA   =           78
42167
                                          MA   =           78
30719
                                          Ha   =            221
926  n
mi
                                          Hp   =            213
764

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8211885
36                 X    =        -2486757
34
 Y    =      -12008445
57  feet           Y    =        -3688073
71  meter
 Z    =       16810945
53                 Z    =         5111856
78
 XDOT =      15959
051095                 XDOT =        4935
716577
 YDOT =     -18663
590122  feet/sec       YDOT =       -5633
866961  meter/sec
 ZDOT =      -5502
840307                 ZDOT =       -1653
463273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         101802
01                 X    =           31029
25
 Y    =       14607157
84  feet           Y    =         4452261
71  meter
 Z    =       16759065
97                 Z    =         5108163
31
 XDOT =     -22667
252093                 XDOT =       -6908
978438
 YDOT =       6390
169474  feet/sec       YDOT =        1947
723656  meter/sec
 ZDOT =      -5398
617278                 ZDOT =       -1645
498546


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   16012
14401635  
00016717  00000-0  10270-3 0  9113
2 25544  51
6431 121
2113 0006174   5
5118 354
6101 15
54352418 20551


Satellite: ISS
Catalog Number: 25544
Epoch time:      16012
14401635   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:       121
2113  deg
Eccentricity:     
0006174     
Arg of perigee:     5
5118  deg
Mean anomaly:     354
6101  deg
Mean motion:   15
54352418  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2055
Checksum:              248


Coasting Arc #13 (Orbit 2069)
---------------------------------------

Vector Time (GMT): 2016/013/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1404319
26                 A    =         6780700
96  meter
 Y    =        4998619
31  meter          E    =           
0009700
 Z    =       -4367232
52                 I    =           51
96560
 XDOT =      -5149
308787                 Wp   =           71
77636
 YDOT =       4480
734181  meter/sec      RA   =          115
45311  deg
 ZDOT =       3482
004863                 TA   =          233
41362
                                          MA   =          233
50291
                                          Ha   =            222
045  n
mi
                                          Hp   =            213
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4607346
66                 X    =         1369532
90
 Y    =       16399669
64  feet           Y    =         5014128
93  meter
 Z    =      -14328190
68                 Z    =        -4360495
17
 XDOT =     -16894
057699                 XDOT =       -5215
944572
 YDOT =      14700
571459  feet/sec       YDOT =        4422
778542  meter/sec
 ZDOT =      11423
900469                 ZDOT =        3456
829449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5084875
66                 X    =         1549870
10
 Y    =      -16282846
70  feet           Y    =        -4963011
68  meter
 Z    =      -14299888
06                 Z    =        -4358605
88
 XDOT =      21067
007589                 XDOT =        6421
223913
 YDOT =      -3330
421965  feet/sec       YDOT =       -1015
112615  meter/sec
 ZDOT =      11313
931461                 ZDOT =        3448
486309


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   16013
10843175  
00016717  00000-0  10270-3 0  9120
2 25544  51
6433 116
4021 0006218   9
2034 350
9232 15
54326706 20706


Satellite: ISS
Catalog Number: 25544
Epoch time:      16013
10843175   =   yrday
fracday
Element set:     912
Inclination:       51
6433  deg
RA of node:       116
4021  deg
Eccentricity:     
0006218     
Arg of perigee:     9
2034  deg
Mean anomaly:     350
9232  deg
Mean motion:   15
54326706  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2070
Checksum:              260


Coasting Arc #14 (Orbit 2085)
---------------------------------------

Vector Time (GMT): 2016/014/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -322575
50                 A    =         6784677
97  meter
 Y    =       -6029600
09  meter          E    =           
0015250
 Z    =        3087201
49                 I    =           51
99168
 XDOT =       5160
502837                 Wp   =           71
56793
 YDOT =      -2811
030458  meter/sec      RA   =          110
48913  deg
 ZDOT =      -4926
427242                 TA   =           73
13907
                                          MA   =           72
97188
                                          Ha   =            222
126  n
mi
                                          Hp   =            213
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1058318
57                 X    =         -270123
15
 Y    =      -19782152
53  feet           Y    =        -6032914
08  meter
 Z    =       10128613
80                 Z    =         3085761
88
 XDOT =      16930
783585                 XDOT =        5215
483071
 YDOT =      -9222
540873  feet/sec       YDOT =       -2753
014856  meter/sec
 ZDOT =     -16162
819036                 ZDOT =       -4901
225629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9635030
77                 X    =        -2936757
38
 Y    =       17312535
32  feet           Y    =         5276860
76  meter
 Z    =       10123473
59                 Z    =         3085634
75
 XDOT =     -18063
628065                 XDOT =       -5505
793834
 YDOT =       -618
891891  feet/sec       YDOT =        -188
638248  meter/sec
 ZDOT =     -16053
030370                 ZDOT =       -4892
963657


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   16014
13713294  
00016717  00000-0  10270-3 0  9133
2 25544  51
6430 111
2720 0006300  13
8867 346
2458 15
54340826 20863


Satellite: ISS
Catalog Number: 25544
Epoch time:      16014
13713294   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:       111
2720  deg
Eccentricity:     
0006300     
Arg of perigee:    13
8867  deg
Mean anomaly:     346
2458  deg
Mean motion:   15
54340826  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2086
Checksum:              280


Coasting Arc #15 (Orbit 2100)
---------------------------------------

Vector Time (GMT): 2016/015/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -617606
44                 A    =         6787721
45  meter
 Y    =        6584710
35  meter          E    =           
0014363
 Z    =       -1496374
75                 I    =           52
01214
 XDOT =      -4941
561474                 Wp   =           28
40351
 YDOT =        847
886682  meter/sec      RA   =          105
53558  deg
 ZDOT =       5805
691637                 TA   =          315
33634
                                          MA   =          315
45195
                                          Ha   =            222
178  n
mi
                                          Hp   =            213
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2026267
86                 X    =         -683923
73
 Y    =       21603380
41  feet           Y    =         6577433
06  meter
 Z    =       -4909365
97                 Z    =        -1499535
99
 XDOT =     -16212
472027                 XDOT =       -4978
876741
 YDOT =       2781
780453  feet/sec       YDOT =         792
418248  meter/sec
 ZDOT =      19047
544742                 ZDOT =        5781
596382

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12946353
07                 X    =         3946048
42
 Y    =      -17408533
38  feet           Y    =        -5306120
97  meter
 Z    =       -4924285
61                 Z    =        -1500922
25
 XDOT =      14127
051486                 XDOT =        4305
925293
 YDOT =       5180
115470  feet/sec       YDOT =        1578
899195  meter/sec
 ZDOT =      18942
905891                 ZDOT =        5773
797716


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16015
10153184  
00016717  00000-0  10270-3 0  9148
2 25544  51
6429 106
4621 0006335  15
9894 344
1458 15
54352100 21011


Satellite: ISS
Catalog Number: 25544
Epoch time:      16015
10153184   =   yrday
fracday
Element set:     914
Inclination:       51
6429  deg
RA of node:       106
4621  deg
Eccentricity:     
0006335     
Arg of perigee:    15
9894  deg
Mean anomaly:     344
1458  deg
Mean motion:   15
54352100  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2101
Checksum:              273


Coasting Arc #16 (Orbit 2116)
---------------------------------------

Vector Time (GMT): 2016/016/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1483731
17                 A    =         6788720
54  meter
 Y    =       -6615877
56  meter          E    =           
0010296
 Z    =        -310840
65                 I    =           52
02258
 XDOT =       4547
845745                 Wp   =          104
70683
 YDOT =       1295
383842  meter/sec      RA   =          100
58946  deg
 ZDOT =      -6031
433214                 TA   =           78
62390
                                          MA   =           78
50826
                                          Ha   =            222
248  n
mi
                                          Hp   =            213
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4867884
41                 X    =         1559111
19
 Y    =      -21705635
04  feet           Y    =        -6598864
02  meter
 Z    =       -1019818
39                 Z    =         -303449
99
 XDOT =      14920
753756                 XDOT =        4562
320337
 YDOT =       4249
946987  feet/sec       YDOT =        1346
321776  meter/sec
 ZDOT =     -19788
166711                 ZDOT =       -6009
305920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15181263
22                 X    =        -4627249
03
 Y    =       16261208
58  feet           Y    =         4956416
37  meter
 Z    =        -986541
26                 Z    =         -300697
78
 XDOT =      -9647
768235                 XDOT =       -2940
639758
 YDOT =     -10166
998591  feet/sec       YDOT =       -3098
901171  meter/sec
 ZDOT =     -19692
454075                 ZDOT =       -6002
260002


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16016
13021777  
00016717  00000-0  10270-3 0  9155
2 25544  51
6426 101
3319 0006177  20
2018 339
9378 15
54322873 21171


Satellite: ISS
Catalog Number: 25544
Epoch time:      16016
13021777   =   yrday
fracday
Element set:     915
Inclination:       51
6426  deg
RA of node:       101
3319  deg
Eccentricity:     
0006177     
Arg of perigee:    20
2018  deg
Mean anomaly:     339
9378  deg
Mean motion:   15
54322873  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2117
Checksum:              290
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