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

 
Date: January 4th 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 1936)
---------------------------------------

Vector Time (GMT): 2016/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6472412
62                 A    =         6785108
17  meter
 Y    =        1286038
34  meter          E    =           
0019262
 Z    =        1525753
20                 I    =           51
78631
 XDOT =        366
016970                 Wp   =           39
17183
 YDOT =      -5043
082855  meter/sec      RA   =          158
27363  deg
 ZDOT =       5778
343526                 TA   =          337
48913
                                          MA   =          337
57352
                                          Ha   =            221
007  n
mi
                                          Hp   =            212
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21234949
54                 X    =        -6493723
86
 Y    =        4219285
89  feet           Y    =         1213540
31  meter
 Z    =        5005751
96                 Z    =         1494259
99
 XDOT =       1200
843077                 XDOT =         394
313934
 YDOT =     -16545
547426  feet/sec       YDOT =       -5038
831864  meter/sec
 ZDOT =      18957
819966                 ZDOT =        5780
190046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8790147
21                 X    =        -2679236
87
 Y    =      -19819382
59  feet           Y    =        -6040947
81  meter
 Z    =        4869126
59                 Z    =         1484109
79
 XDOT =      14931
255997                 XDOT =        4551
046828
 YDOT =      -1941
766549  feet/sec       YDOT =        -591
850444  meter/sec
 ZDOT =      18966
693481                 ZDOT =        5781
048173


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
56136692  
00016717  00000-0  10270-3 0  9006
2 25544  51
6392 159
0703 0008424 359
0998   1
0138 15
55262162 19372


Satellite: ISS
Catalog Number: 25544
Epoch time:      16004
56136692   =   yrday
fracday
Element set:     900
Inclination:       51
6392  deg
RA of node:       159
0703  deg
Eccentricity:     
0008424     
Arg of perigee:   359
0998  deg
Mean anomaly:       1
0138  deg
Mean motion:   15
55262162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1937
Checksum:              302


Coasting Arc #2 (Orbit 1951)
---------------------------------------

Vector Time (GMT): 2016/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5884547
19                 A    =         6781272
03  meter
 Y    =          20315
42  meter          E    =           
0009792
 Z    =       -3383303
49                 I    =           51
80311
 XDOT =      -2695
368399                 Wp   =           32
23401
 YDOT =       5454
015482  meter/sec      RA   =          153
30097  deg
 ZDOT =      -4653
409980                 TA   =          187
12880
                                          MA   =          187
14274
                                          Ha   =            221
118  n
mi
                                          Hp   =            212
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19306257
19                 X    =         5900317
36
 Y    =          66651
64  feet           Y    =           86208
70  meter
 Z    =      -11100077
05                 Z    =        -3354679
40
 XDOT =      -8843
072174                 XDOT =       -2733
551864
 YDOT =      17893
751582  feet/sec       YDOT =        5423
660877  meter/sec
 ZDOT =     -15267
093110                 ZDOT =       -4666
595871

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4519083
21                 X    =         1377416
56
 Y    =       18842798
58  feet           Y    =         5743285
01  meter
 Z    =      -10976089
83                 Z    =        -3345512
18
 XDOT =     -18078
919080                 XDOT =       -5510
454536
 YDOT =      -4594
768659  feet/sec       YDOT =       -1400
485487  meter/sec
 ZDOT =     -15325
163576                 ZDOT =       -4671
109858


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
52519987  
00016717  00000-0  10270-3 0  9016
2 25544  51
6394 154
2570 0008592   2
9628 357
1575 15
55269058 19521


Satellite: ISS
Catalog Number: 25544
Epoch time:      16005
52519987   =   yrday
fracday
Element set:     901
Inclination:       51
6394  deg
RA of node:       154
2570  deg
Eccentricity:     
0008592     
Arg of perigee:     2
9628  deg
Mean anomaly:     357
1575  deg
Mean motion:   15
55269058  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1952
Checksum:              331


Coasting Arc #3 (Orbit 1967)
---------------------------------------

Vector Time (GMT): 2016/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4642751
06                 A    =         6776636
86  meter
 Y    =       -1478497
73  meter          E    =           
0009475
 Z    =        4700515
16                 I    =           51
81651
 XDOT =       4601
089419                 Wp   =           59
11795
 YDOT =      -5454
940052  meter/sec      RA   =          148
31460  deg
 ZDOT =       2829
286755                 TA   =            2
92316
                                          MA   =            2
91763
                                          Ha   =            221
255  n
mi
                                          Hp   =            211
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15232122
91                 X    =        -4648706
21
 Y    =       -4850714
34  feet           Y    =        -1530449
69  meter
 Z    =       15421637
65                 Z    =         4677947
20
 XDOT =      15095
437726                 XDOT =        4648
002449
 YDOT =     -17896
784949  feet/sec       YDOT =       -5403
225535  meter/sec
 ZDOT =       9282
436861                 ZDOT =        2851
751288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         809731
03                 X    =          246806
02
 Y    =      -16058933
91  feet           Y    =        -4894763
05  meter
 Z    =       15324127
49                 Z    =         4670794
06
 XDOT =      19948
587819                 XDOT =        6080
329567
 YDOT =       9955
662047  feet/sec       YDOT =        3034
485792  meter/sec
 ZDOT =       9380
719048                 ZDOT =        2859
243166


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
55327889  
00016717  00000-0  10270-3 0  9029
2 25544  51
6398 149
1221 0008518   5
9507 354
1746 15
55299685 19681


Satellite: ISS
Catalog Number: 25544
Epoch time:      16006
55327889   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       149
1221  deg
Eccentricity:     
0008518     
Arg of perigee:     5
9507  deg
Mean anomaly:     354
1746  deg
Mean motion:   15
55299685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1968
Checksum:              344


Coasting Arc #4 (Orbit 1982)
---------------------------------------

Vector Time (GMT): 2016/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3002555
96                 A    =         6774066
54  meter
 Y    =        2968959
96  meter          E    =           
0018901
 Z    =       -5311779
76                 I    =           51
83553
 XDOT =      -5852
886781                 Wp   =           59
48015
 YDOT =       4906
467912  meter/sec      RA   =          143
31950  deg
 ZDOT =       -558
135593                 TA   =          205
15474
                                          MA   =          205
24693
                                          Ha   =            221
319  n
mi
                                          Hp   =            211
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9850905
38                 X    =         2994935
48
 Y    =        9740682
29  feet           Y    =         3002494
37  meter
 Z    =      -17427098
94                 Z    =        -5297212
35
 XDOT =     -19202
384453                 XDOT =       -5904
605933
 YDOT =      16097
335668  feet/sec       YDOT =        4840
727932  meter/sec
 ZDOT =      -1831
153520                 ZDOT =        -586
692638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6690133
14                 X    =        -2039152
58
 Y    =       12220517
21  feet           Y    =         3724813
64  meter
 Z    =      -17364506
43                 Z    =        -5292701
56
 XDOT =     -19786
464677                 XDOT =       -6030
914434
 YDOT =     -13647
947351  feet/sec       YDOT =       -4159
894353  meter/sec
 ZDOT =      -1955
756495                 ZDOT =        -596
114580


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
51709693  
00016717  00000-0  10270-3 0  9034
2 25544  51
6406 144
3101 0008659  10
5043 349
6290 15
55301383 19837


Satellite: ISS
Catalog Number: 25544
Epoch time:      16007
51709693   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:       144
3101  deg
Eccentricity:     
0008659     
Arg of perigee:    10
5043  deg
Mean anomaly:     349
6290  deg
Mean motion:   15
55301383  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1983
Checksum:              295


Coasting Arc #5 (Orbit 1998)
---------------------------------------

Vector Time (GMT): 2016/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1121003
28                 A    =         6775074
48  meter
 Y    =       -4339735
36  meter          E    =           
0013236
 Z    =        5077895
60                 I    =           51
86443
 XDOT =       6413
284791                 Wp   =           30
20623
 YDOT =      -3799
076767  meter/sec      RA   =          138
32052  deg
 ZDOT =      -1817
793897                 TA   =           77
39846
                                          MA   =           77
25048
                                          Ha   =            221
481  n
mi
                                          Hp   =            211
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3677832
27                 X    =        -1097058
09
 Y    =      -14237976
89  feet           Y    =        -4352137
72  meter
 Z    =       16659762
46                 Z    =         5072507
85
 XDOT =      21040
960601                 XDOT =        6464
120373
 YDOT =     -12464
162621  feet/sec       YDOT =       -3727
074778  meter/sec
 ZDOT =      -5963
890738                 ZDOT =       -1786
516762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12556826
97                 X    =         3827320
86
 Y    =       -7702218
99  feet           Y    =        -2347636
35  meter
 Z    =       16637188
48                 Z    =         5071015
05
 XDOT =      17416
382542                 XDOT =        5308
513399
 YDOT =      15711
841487  feet/sec       YDOT =        4788
969285  meter/sec
 ZDOT =      -5827
674902                 ZDOT =       -1776
275310


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
54516147  
00016717  00000-0  10270-3 0  9049
2 25544  51
6412 139
1747 0008701  14
6352 345
5052 15
55271433 19998


Satellite: ISS
Catalog Number: 25544
Epoch time:      16008
54516147   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:       139
1747  deg
Eccentricity:     
0008701     
Arg of perigee:    14
6352  deg
Mean anomaly:     345
5052  deg
Mean motion:   15
55271433  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1999
Checksum:              301


Coasting Arc #6 (Orbit 2013)
---------------------------------------

Vector Time (GMT): 2016/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -671036
59                 A    =         6778845
36  meter
 Y    =        5373933
07  meter          E    =           
0011238
 Z    =       -4081050
88                 I    =           51
90150
 XDOT =      -6238
772374                 Wp   =           58
03484
 YDOT =       2166
099186  meter/sec      RA   =          133
33409  deg
 ZDOT =       3891
771774                 TA   =          252
08050
                                          MA   =          252
20307
                                          Ha   =            221
499  n
mi
                                          Hp   =            211
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2201563
63                 X    =         -711255
55
 Y    =       17631014
02  feet           Y    =         5366204
56  meter
 Z    =      -13389274
53                 Z    =        -4084407
82
 XDOT =     -20468
413299                 XDOT =       -6281
434937
 YDOT =       7106
624625  feet/sec       YDOT =        2096
094247  meter/sec
 ZDOT =      12768
280097                 ZDOT =        3861
362194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17442886
91                 X    =        -5316591
93
 Y    =        3321083
27  feet           Y    =         1012266
18  meter
 Z    =      -13404786
92                 Z    =        -4085779
05
 XDOT =     -12753
599427                 XDOT =       -3887
297105
 YDOT =     -16161
573688  feet/sec       YDOT =       -4926
047660  meter/sec
 ZDOT =      12636
094580                 ZDOT =        3851
481628


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
50896185  
00016717  00000-0  10270-3 0  9050
2 25544  51
6420 134
3623 0008746  16
9069 343
2374 15
55297103 20149


Satellite: ISS
Catalog Number: 25544
Epoch time:      16009
50896185   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       134
3623  deg
Eccentricity:     
0008746     
Arg of perigee:    16
9069  deg
Mean anomaly:     343
2374  deg
Mean motion:   15
55297103  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2014
Checksum:              303


Coasting Arc #7 (Orbit 2029)
---------------------------------------

Vector Time (GMT): 2016/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2284030
68                 A    =         6783414
55  meter
 Y    =       -5915739
73  meter          E    =           
0016988
 Z    =        2401835
56                 I    =           51
93867
 XDOT =       5455
900783                 Wp   =           75
40502
 YDOT =        -95
554199  meter/sec      RA   =          128
36305  deg
 ZDOT =      -5387
708496                 TA   =           77
85992
                                          MA   =           77
66966
                                          Ha   =            221
558  n
mi
                                          Hp   =            211
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7493538
97                 X    =         2338345
24
 Y    =      -19408594
92  feet           Y    =        -5889894
67  meter
 Z    =        7880037
93                 Z    =         2413062
18
 XDOT =      17899
936952                 XDOT =        5482
734645
 YDOT =       -313
498028  feet/sec       YDOT =         -34
392295  meter/sec
 ZDOT =     -17676
208975                 ZDOT =       -5361
140250

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20768239
18                 X    =         6330159
30
 Y    =         860657
59  feet           Y    =          262328
43  meter
 Z    =        7929766
13                 Z    =         2416992
72
 XDOT =       6109
404994                 XDOT =        1862
146642
 YDOT =      15456
200301  feet/sec       YDOT =        4711
049852  meter/sec
 ZDOT =     -17561
028118                 ZDOT =       -5352
601370


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
53700898  
00016717  00000-0  10270-3 0  9061
2 25544  51
6425 129
2277 0008723  21
4184 338
7333 15
55312169 20308


Satellite: ISS
Catalog Number: 25544
Epoch time:      16010
53700898   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:       129
2277  deg
Eccentricity:     
0008723     
Arg of perigee:    21
4184  deg
Mean anomaly:     338
7333  deg
Mean motion:   15
55312169  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2030
Checksum:              293


Coasting Arc #8 (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    =        3619707
47                 A    =         6776841
94  meter
 Y    =        2122726
68  meter          E    =           
0016546
 Z    =       -5334738
03                 I    =           51
91906
 XDOT =      -4224
647598                 Wp   =           66
04122
 YDOT =       6378
455649  meter/sec      RA   =          125
41182  deg
 ZDOT =       -322
716477                 TA   =          200
85585
                                          MA   =          200
92343
                                          Ha   =            221
851  n
mi
                                          Hp   =            214
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11875680
69                 X    =         3621615
09
 Y    =        6964326
38  feet           Y    =         2163215
63  meter
 Z    =      -17502421
35                 Z    =        -5317149
88
 XDOT =     -13860
392382                 XDOT =       -4294
091480
 YDOT =      20926
691763  feet/sec       YDOT =        6330
824582  meter/sec
 ZDOT =      -1058
781093                 ZDOT =        -343
406757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5759209
85                 X    =        -1755407
16
 Y    =      -12610109
70  feet           Y    =        -3843561
44  meter
 Z    =      -17426560
82                 Z    =        -5311615
74
 XDOT =      22479
937234                 XDOT =        6851
884869
 YDOT =      -8651
998525  feet/sec       YDOT =       -2637
129150  meter/sec
 ZDOT =      -1149
623031                 ZDOT =        -350
405100


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
11528977  
00016717  00000-0  10270-3 0  9073
2 25544  51
6429 126
3428 0006090   2
7923 357
3262 15
54319857 20393


Satellite: ISS
Catalog Number: 25544
Epoch time:      16011
11528977   =   yrday
fracday
Element set:     907
Inclination:       51
6429  deg
RA of node:       126
3428  deg
Eccentricity:     
0006090     
Arg of perigee:     2
7923  deg
Mean anomaly:     357
3262  deg
Mean motion:   15
54319857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2039
Checksum:              310


Coasting Arc #9 (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    =       -2497413
90                 A    =         6777596
19  meter
 Y    =       -3666662
32  meter          E    =           
0010195
 Z    =        5122090
18                 I    =           51
93978
 XDOT =       4868
066276                 Wp   =           27
59830
 YDOT =      -5683
228225  meter/sec      RA   =          120
42970  deg
 ZDOT =      -1684
655396                 TA   =           78
65616
                                          MA   =           78
54163
                                          Ha   =            221
910  n
mi
                                          Hp   =            213
774

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8193615
15                 X    =        -2481107
28
 Y    =      -12029732
03  feet           Y    =        -3694499
09  meter
 Z    =       16804757
82                 Z    =         5109998
01
 XDOT =      15971
346050                 XDOT =        4939
438932
 YDOT =     -18645
761893  feet/sec       YDOT =       -5628
391150  meter/sec
 ZDOT =      -5527
084634                 ZDOT =       -1660
834801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          74678
37                 X    =           22761
97
 Y    =       14614416
28  feet           Y    =         4454474
08  meter
 Z    =       16752997
56                 Z    =         5106313
66
 XDOT =     -22666
955397                 XDOT =       -6908
888005
 YDOT =       6370
405289  feet/sec       YDOT =        1941
699532  meter/sec
 ZDOT =      -5422
783934                 ZDOT =       -1652
864543


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
14400312  
00016717  00000-0  10270-3 0  9080
2 25544  51
6429 121
2130 0006171   5
1211 355
0004 15
54355599 20554


Satellite: ISS
Catalog Number: 25544
Epoch time:      16012
14400312   =   yrday
fracday
Element set:     908
Inclination:       51
6429  deg
RA of node:       121
2130  deg
Eccentricity:     
0006171     
Arg of perigee:     5
1211  deg
Mean anomaly:     355
0004  deg
Mean motion:   15
54355599  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2055
Checksum:              248


Coasting Arc #10 (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    =        1397434
78                 A    =         6780708
42  meter
 Y    =        5004498
64  meter          E    =           
0009642
 Z    =       -4362640
22                 I    =           51
96556
 XDOT =      -5151
796202                 Wp   =           71
57740
 YDOT =       4472
272334  meter/sec      RA   =          115
45461  deg
 ZDOT =       3489
309703                 TA   =          233
69738
                                          MA   =          233
78646
                                          Ha   =            222
030  n
mi
                                          Hp   =            213
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4584759
77                 X    =         1362560
88
 Y    =       16418958
80  feet           Y    =         5019930
79  meter
 Z    =      -14313124
09                 Z    =        -4355936
53
 XDOT =     -16902
218509                 XDOT =       -5218
372663
 YDOT =      14672
809496  feet/sec       YDOT =        4414
289211  meter/sec
 ZDOT =      11447
866479                 ZDOT =        3464
122350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5114427
39                 X    =         1558877
47
 Y    =      -16286499
32  feet           Y    =        -4964124
99  meter
 Z    =      -14284968
45                 Z    =        -4354058
38
 XDOT =      21058
433683                 XDOT =        6418
610587
 YDOT =      -3304
815162  feet/sec       YDOT =       -1007
307661  meter/sec
 ZDOT =      11337
847247                 ZDOT =        3455
775841


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
10841653  
00016717  00000-0  10270-3 0  9095
2 25544  51
6431 116
4038 0006215   8
8147 351
3114 15
54329870 20708


Satellite: ISS
Catalog Number: 25544
Epoch time:      16013
10841653   =   yrday
fracday
Element set:     909
Inclination:       51
6431  deg
RA of node:       116
4038  deg
Eccentricity:     
0006215     
Arg of perigee:     8
8147  deg
Mean anomaly:     351
3114  deg
Mean motion:   15
54329870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2070
Checksum:              277


Coasting Arc #11 (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    =        -314786
09                 A    =         6784688
19  meter
 Y    =       -6033766
92  meter          E    =           
0015212
 Z    =        3079915
52                 I    =           51
99165
 XDOT =       5161
179938                 Wp   =           71
60953
 YDOT =      -2799
464155  meter/sec      RA   =          110
49065  deg
 ZDOT =      -4932
261909                 TA   =           73
19327
                                          MA   =           73
02646
                                          Ha   =            222
112  n
mi
                                          Hp   =            213
472

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1032762
76                 X    =         -262252
33
 Y    =      -19795823
23  feet           Y    =        -6036993
35  meter
 Z    =       10104709
72                 Z    =         3078513
95
 XDOT =      16933
005046                 XDOT =        5216
059127
 YDOT =      -9184
593685  feet/sec       YDOT =       -2741
441547  meter/sec
 ZDOT =     -16181
961644                 ZDOT =       -4907
057252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9664065
62                 X    =        -2945607
20
 Y    =       17310331
01  feet           Y    =         5276188
89  meter
 Z    =       10099735
19                 Z    =         3078399
29
 XDOT =     -18045
466447                 XDOT =       -5500
258173
 YDOT =       -650
085884  feet/sec       YDOT =        -198
146177  meter/sec
 ZDOT =     -16072
161897                 ZDOT =       -4898
794946


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
13711561  
00016717  00000-0  10270-3 0  9105
2 25544  51
6429 111
2737 0006296  13
5092 346
6228 15
54343821 20867


Satellite: ISS
Catalog Number: 25544
Epoch time:      16014
13711561   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:       111
2737  deg
Eccentricity:     
0006296     
Arg of perigee:    13
5092  deg
Mean anomaly:     346
6228  deg
Mean motion:   15
54343821  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2086
Checksum:              286


Coasting Arc #12 (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    =        -626022
84                 A    =         6787724
17  meter
 Y    =        6586074
55  meter          E    =           
0014380
 Z    =       -1486680
12                 I    =           52
01208
 XDOT =      -4940
282074                 Wp   =           28
25852
 YDOT =        833
719377  meter/sec      RA   =          105
53712  deg
 ZDOT =       5808
886800                 TA   =          315
58946
                                          MA   =          315
70469
                                          Ha   =            222
164  n
mi
                                          Hp   =            213
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2053880
71                 X    =         -692401
84
 Y    =       21607856
14  feet           Y    =         6578702
80  meter
 Z    =       -4877559
44                 Z    =        -1489882
39
 XDOT =     -16208
274520                 XDOT =       -4977
454535
 YDOT =       2735
299792  feet/sec       YDOT =         778
266048  meter/sec
 ZDOT =      19058
027560                 ZDOT =        5784
798107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12972436
22                 X    =         3953998
56
 Y    =      -17397880
97  feet           Y    =        -5302874
12  meter
 Z    =       -4892657
26                 Z    =        -1491281
93
 XDOT =      14100
111574                 XDOT =        4297
714008
 YDOT =       5215
752814  feet/sec       YDOT =        1589
761458  meter/sec
 ZDOT =      18953
419771                 ZDOT =        5777
002346


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
10151252  
00016717  00000-0  10270-3 0  9119
2 25544  51
6427 106
4637 0006332  15
6111 344
5236 15
54355393 21017


Satellite: ISS
Catalog Number: 25544
Epoch time:      16015
10151252   =   yrday
fracday
Element set:     911
Inclination:       51
6427  deg
RA of node:       106
4637  deg
Eccentricity:     
0006332     
Arg of perigee:    15
6111  deg
Mean anomaly:     344
5236  deg
Mean motion:   15
54355393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2101
Checksum:              260


Coasting Arc #13 (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    =        1492238
35                 A    =         6788708
34  meter
 Y    =       -6613446
68  meter          E    =           
0010223
 Z    =        -321891
83                 I    =           52
02247
 XDOT =       4544
332179                 Wp   =          104
71217
 YDOT =       1311
012269  meter/sec      RA   =          100
59099  deg
 ZDOT =      -6030
679997                 TA   =           78
73712
                                          MA   =           78
62225
                                          Ha   =            222
234  n
mi
                                          Hp   =            213
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4895795
11                 X    =         1567644
23
 Y    =      -21697659
70  feet           Y    =        -6596337
86  meter
 Z    =       -1056075
55                 Z    =         -314459
79
 XDOT =      14909
226310                 XDOT =        4558
628613
 YDOT =       4301
221356  feet/sec       YDOT =        1361
909917  meter/sec
 ZDOT =     -19785
695528                 ZDOT =       -6008
570204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15201511
33                 X    =        -4633420
65
 Y    =       16240099
89  feet           Y    =         4949982
45  meter
 Z    =       -1022619
39                 Z    =         -311694
39
 XDOT =      -9613
420699                 XDOT =       -2930
170629
 YDOT =     -10203
920816  feet/sec       YDOT =       -3110
155065  meter/sec
 ZDOT =     -19690
061684                 ZDOT =       -6001
530801


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
13019633  
00016717  00000-0  10270-3 0  9120
2 25544  51
6424 101
3335 0006174  19
8039 340
3353 15
54326077 21170


Satellite: ISS
Catalog Number: 25544
Epoch time:      16016
13019633   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:       101
3335  deg
Eccentricity:     
0006174     
Arg of perigee:    19
8039  deg
Mean anomaly:     340
3353  deg
Mean motion:   15
54326077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2117
Checksum:              274


Coasting Arc #14 (Orbit 2132)
---------------------------------------

Vector Time (GMT): 2016/017/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2211736
84                 A    =         6786822
17  meter
 Y    =        6066094
41  meter          E    =           
0018859
 Z    =        2055337
11                 I    =           52
02119
 XDOT =      -4045
727648                 Wp   =           54
66000
 YDOT =      -3375
042191  meter/sec      RA   =           95
64263  deg
 ZDOT =       5582
200324                 TA   =          327
97239
                                          MA   =          328
08686
                                          Ha   =            222
293  n
mi
                                          Hp   =            213
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7256354
47                 X    =        -2289388
92
 Y    =       19901884
54  feet           Y    =         6040927
11  meter
 Z    =        6743231
97                 Z    =         2044404
52
 XDOT =     -13273
384673                 XDOT =       -4034
802210
 YDOT =     -11072
973066  feet/sec       YDOT =       -3420
223143  meter/sec
 ZDOT =      18314
305524                 ZDOT =        5562
573795

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16127357
93                 X    =         4915618
70
 Y    =      -13758648
11  feet           Y    =        -4193635
94  meter
 Z    =        6694684
04                 Z    =         2040539
70
 XDOT =       5230
491803                 XDOT =        1594
253901
 YDOT =      15041
883305  feet/sec       YDOT =        4584
766031  meter/sec
 ZDOT =      18229
826592                 ZDOT =        5556
451145


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16017
15886987  
00016717  00000-0  10270-3 0  9138
2 25544  51
6419  96
2023 0006360  22
1595 337
9832 15
54385220 21338


Satellite: ISS
Catalog Number: 25544
Epoch time:      16017
15886987   =   yrday
fracday
Element set:     913
Inclination:       51
6419  deg
RA of node:        96
2023  deg
Eccentricity:     
0006360     
Arg of perigee:    22
1595  deg
Mean anomaly:     337
9832  deg
Mean motion:   15
54385220  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2133
Checksum:              310


Coasting Arc #15 (Orbit 2147)
---------------------------------------

Vector Time (GMT): 2016/018/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2868155
49                 A    =         6783197
29  meter
 Y    =       -4995044
22  meter          E    =           
0010176
 Z    =       -3595474
86                 I    =           52
01060
 XDOT =       3429
747047                 Wp   =           51
49581
 YDOT =       5185
841052  meter/sec      RA   =           90
68741  deg
 ZDOT =      -4470
898115                 TA   =          170
71643
                                          MA   =          170
69761
                                          Ha   =            222
320  n
mi
                                          Hp   =            213
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9409958
94                 X    =         2941263
33
 Y    =      -16387940
36  feet           Y    =        -4962561
76  meter
 Z    =      -11796177
37                 Z    =        -3581364
67
 XDOT =      11252
450941                 XDOT =        3393
220403
 YDOT =      17013
914214  feet/sec       YDOT =        5223
990619  meter/sec
 ZDOT =     -14668
300901                 ZDOT =       -4454
325930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16139739
92                 X    =        -4919392
73
 Y    =        9903680
36  feet           Y    =         3018641
77  meter
 Z    =      -11734037
16                 Z    =        -3576534
53
 XDOT =      -1165
214473                 XDOT =        -355
157371
 YDOT =     -19184
878118  feet/sec       YDOT =       -5847
550850  meter/sec
 ZDOT =     -14597
415103                 ZDOT =       -4449
292123


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16018
12324597  
00016717  00000-0  10270-3 0  9141
2 25544  51
6413  91
3925 0006340  25
5052 334
6413 15
54375008 21480


Satellite: ISS
Catalog Number: 25544
Epoch time:      16018
12324597   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:        91
3925  deg
Eccentricity:     
0006340     
Arg of perigee:    25
5052  deg
Mean anomaly:     334
6413  deg
Mean motion:   15
54375008  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2148
Checksum:              285


Coasting Arc #16 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2016/019/02:21:59
296
Vector Time (MET): N/A
Weight (LBS)     : 922092
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3418777
06                 A    =         6779355
25  meter
 Y    =        3482423
71  meter          E    =           
0010674
 Z    =        4695798
76                 I    =           51
99727
 XDOT =      -2741
850201                 Wp   =           78
57444
 YDOT =      -6568
932996  meter/sec      RA   =           85
72032  deg
 ZDOT =       2871
903754                 TA   =          343
05966
                                          MA   =          343
09527
                                          Ha   =            222
607  n
mi
                                          Hp   =            212
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11216460
17                 X    =        -3480274
34
 Y    =       11425274
64  feet           Y    =         3443848
66  meter
 Z    =       15406163
92                 Z    =         4679042
04
 XDOT =      -8995
571526                 XDOT =       -2682
141394
 YDOT =     -21551
617442  feet/sec       YDOT =       -6599
260435  meter/sec
 ZDOT =       9422
256410                 ZDOT =        2858
729379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15305925
66                 X    =         4665246
14
 Y    =       -4932440
35  feet           Y    =        -1503407
82  meter
 Z    =       15332822
24                 Z    =         4673444
22
 XDOT =      -2245
313346                 XDOT =        -684
371508
 YDOT =      22183
804467  feet/sec       YDOT =        6761
623602  meter/sec
 ZDOT =       9366
380005                 ZDOT =        2854
872626


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16019
15190724  
00016717  00000-0  10270-3 0  9159
2 25544  51
6414  86
2614 0006517  29
9008 330
2516 15
54363774 21645


Satellite: ISS
Catalog Number: 25544
Epoch time:      16019
15190724   =   yrday
fracday
Element set:     915
Inclination:       51
6414  deg
RA of node:        86
2614  deg
Eccentricity:     
0006517     
Arg of perigee:    29
9008  deg
Mean anomaly:     330
2516  deg
Mean motion:   15
54363774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2164
Checksum:              298
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