[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: January 10th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


011/02:13:29 747 -0 2 4 9 4 9
N/A 4 4 -0 6 221 8
000/00:16:59 494 -2 2 -0 4 213 9

Coasting Arc #1 (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    =       -1119331
31                 A    =         6775035
57  meter
 Y    =       -4340601
01  meter          E    =           
0013325
 Z    =        5077429
12                 I    =           51
86462
 XDOT =       6413
789923                 Wp   =           30
34673
 YDOT =      -3797
627772  meter/sec      RA   =          138
32252  deg
 ZDOT =      -1819
287755                 TA   =           77
27311
                                          MA   =           77
12420
                                          Ha   =            221
493  n
mi
                                          Hp   =            211
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3672346
82                 X    =        -1095374
30
 Y    =      -14240816
97  feet           Y    =        -4352984
61  meter
 Z    =       16658232
01                 Z    =         5072049
51
 XDOT =      21042
617857                 XDOT =        6464
616521
 YDOT =     -12459
408702  feet/sec       YDOT =       -3725
620185  meter/sec
 ZDOT =      -5968
791847                 ZDOT =       -1788
008188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12561121
63                 X    =         3828629
87
 Y    =       -7697767
09  feet           Y    =        -2346279
41  meter
 Z    =       16635693
49                 Z    =         5070559
38
 XDOT =      17412
636207                 XDOT =        5307
371516
 YDOT =      15714
507250  feet/sec       YDOT =        4789
781810  meter/sec
 ZDOT =      -5832
565735                 ZDOT =       -1777
766036


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
54515867  
00016717  00000-0  10270-3 0  9003
2 25544  51
6413 139
1769 0008776  14
9781 345
1631 15
55285411 19994


Satellite: ISS
Catalog Number: 25544
Epoch time:      16008
54515867   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:       139
1769  deg
Eccentricity:     
0008776     
Arg of perigee:    14
9781  deg
Mean anomaly:     345
1631  deg
Mean motion:   15
55285411  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1999
Checksum:              331


Coasting Arc #2 (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    =        -678790
10                 A    =         6778796
64  meter
 Y    =        5376479
22  meter          E    =           
0011328
 Z    =       -4076305
76                 I    =           51
90175
 XDOT =      -6237
804223                 Wp   =           57
84630
 YDOT =       2157
518537  meter/sec      RA   =          133
33597  deg
 ZDOT =       3898
173309                 TA   =          252
34763
                                          MA   =          252
47137
                                          Ha   =            221
501  n
mi
                                          Hp   =            211
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2227001
65                 X    =         -719060
00
 Y    =       17639367
51  feet           Y    =         5368663
71  meter
 Z    =      -13373706
57                 Z    =        -4079700
49
 XDOT =     -20465
236952                 XDOT =       -6280
402003
 YDOT =       7078
472890  feet/sec       YDOT =        2087
524786  meter/sec
 ZDOT =      12789
282511                 ZDOT =        3867
768589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17458581
26                 X    =        -5321375
57
 Y    =        3299273
92  feet           Y    =         1005618
69  meter
 Z    =      -13389383
19                 Z    =        -4081084
00
 XDOT =     -12727
440284                 XDOT =       -3879
323799
 YDOT =     -16166
052791  feet/sec       YDOT =       -4927
412891  meter/sec
 ZDOT =      12657
119597                 ZDOT =        3857
890053


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
50894764  
00016717  00000-0  10270-3 0  9017
2 25544  51
6422 134
3644 0008831  17
2531 342
8921 15
55319402 20147


Satellite: ISS
Catalog Number: 25544
Epoch time:      16009
50894764   =   yrday
fracday
Element set:     901
Inclination:       51
6422  deg
RA of node:       134
3644  deg
Eccentricity:     
0008831     
Arg of perigee:    17
2531  deg
Mean anomaly:     342
8921  deg
Mean motion:   15
55319402  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2014
Checksum:              288


Coasting Arc #3 (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    =        2299047
84                 A    =         6783355
09  meter
 Y    =       -5915828
72  meter          E    =           
0017068
 Z    =        2387137
38                 I    =           51
93897
 XDOT =       5447
959036                 Wp   =           75
41296
 YDOT =        -74
858557  meter/sec      RA   =          128
36485  deg
 ZDOT =      -5396
078585                 TA   =           78
02841
                                          MA   =           77
83714
                                          Ha   =            221
550  n
mi
                                          Hp   =            210
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7542807
87                 X    =         2353433
68
 Y    =      -19408886
88  feet           Y    =        -5889815
33  meter
 Z    =        7831815
54                 Z    =         2398437
12
 XDOT =      17873
881352                 XDOT =        5474
602722
 YDOT =       -245
598940  feet/sec       YDOT =         -13
786526  meter/sec
 ZDOT =     -17703
669899                 ZDOT =       -5369
549378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20784340
33                 X    =         6335066
93
 Y    =         907548
22  feet           Y    =          276620
70  meter
 Z    =        7881860
71                 Z    =         2402391
14
 XDOT =       6040
219411                 XDOT =        1841
058877
 YDOT =      15452
166076  feet/sec       YDOT =        4709
820220  meter/sec
 ZDOT =     -17588
661989                 ZDOT =       -5361
024174


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
53697731  
00016717  00000-0  10270-3 0  9028
2 25544  51
6427 129
2297 0008818  21
7491 338
4046 15
55342913 20309


Satellite: ISS
Catalog Number: 25544
Epoch time:      16010
53697731   =   yrday
fracday
Element set:     902
Inclination:       51
6427  deg
RA of node:       129
2297  deg
Eccentricity:     
0008818     
Arg of perigee:    21
7491  deg
Mean anomaly:     338
4046  deg
Mean motion:   15
55342913  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2030
Checksum:              301


Coasting Arc #4 (Orbit 2038)
---------------------------------------

Vector Time (GMT): 2016/011/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3602692
29                 A    =         6776732
34  meter
 Y    =        2148261
51  meter          E    =           
0016639
 Z    =       -5335948
36                 I    =           51
91924
 XDOT =      -4243
208366                 Wp   =           66
05988
 YDOT =       6367
461274  meter/sec      RA   =          125
41316  deg
 ZDOT =       -295
510315                 TA   =          201
09560
                                          MA   =          201
16430
                                          Ha   =            221
839  n
mi
                                          Hp   =            213
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11819856
60                 X    =         3604321
52
 Y    =        7048102
07  feet           Y    =         2188558
63  meter
 Z    =      -17506392
27                 Z    =        -5318443
54
 XDOT =     -13921
287289                 XDOT =       -4312
660080
 YDOT =      20890
620979  feet/sec       YDOT =        6319
622603  meter/sec
 ZDOT =       -969
522030                 ZDOT =        -316
290777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5665441
12                 X    =        -1726826
45
 Y    =      -12646150
01  feet           Y    =        -3854546
52  meter
 Z    =      -17430897
57                 Z    =        -5312937
58
 XDOT =      22506
500055                 XDOT =        6859
981217
 YDOT =      -8594
221787  feet/sec       YDOT =       -2619
518801  meter/sec
 ZDOT =      -1060
752914                 ZDOT =        -323
317488


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
11524544  
00016717  00000-0  10270-3 0  9035
2 25544  51
6431 126
3448 0006181   3
4484 356
6710 15
54355401 20394


Satellite: ISS
Catalog Number: 25544
Epoch time:      16011
11524544   =   yrday
fracday
Element set:     903
Inclination:       51
6431  deg
RA of node:       126
3448  deg
Eccentricity:     
0006181     
Arg of perigee:     3
4484  deg
Mean anomaly:     356
6710  deg
Mean motion:   15
54355401  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2039
Checksum:              273


Coasting Arc #5 (Orbit 2054)
---------------------------------------

Vector Time (GMT): 2016/012/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2466846
06                 A    =         6777514
79  meter
 Y    =       -3701945
26  meter          E    =           
0010400
 Z    =        5111358
50                 I    =           51
94013
 XDOT =       4888
020680                 Wp   =           28
06752
 YDOT =      -5653
898927  meter/sec      RA   =          120
43069  deg
 ZDOT =      -1725
461686                 TA   =           78
59135
                                          MA   =           78
47455
                                          Ha   =            221
888  n
mi
                                          Hp   =            213
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8093326
98                 X    =        -2450095
05
 Y    =      -12145489
70  feet           Y    =        -3729437
72  meter
 Z    =       16769548
90                 Z    =         5099415
90
 XDOT =      16036
813256                 XDOT =        4959
262102
 YDOT =     -18549
537163  feet/sec       YDOT =       -5598
839441  meter/sec
 ZDOT =      -5660
963537                 ZDOT =       -1701
544476

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -73389
80                 X    =          -22369
21
 Y    =       14653357
78  feet           Y    =         4466343
45  meter
 Z    =       16718443
45                 Z    =         5095781
57
 XDOT =     -22664
559719                 XDOT =       -6908
157802
 YDOT =       6264
688796  feet/sec       YDOT =        1909
477145  meter/sec
 ZDOT =      -5556
249290                 ZDOT =       -1693
544784


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
14393245  
00016717  00000-0  10270-3 0  9042
2 25544  51
6431 121
2148 0006271   5
8278 354
2947 15
54399136 20559


Satellite: ISS
Catalog Number: 25544
Epoch time:      16012
14393245   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       121
2148  deg
Eccentricity:     
0006271     
Arg of perigee:     5
8278  deg
Mean anomaly:     354
2947  deg
Mean motion:   15
54399136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2055
Checksum:              295


Coasting Arc #6 (Orbit 2069)
---------------------------------------

Vector Time (GMT): 2016/013/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1351714
07                 A    =         6780671
78  meter
 Y    =        5043661
03  meter          E    =           
0009641
 Z    =       -4331544
38                 I    =           51
96614
 XDOT =      -5167
429996                 Wp   =           70
53778
 YDOT =       4415
578977  meter/sec      RA   =          115
45540  deg
 ZDOT =       3538
467903                 TA   =          235
30873
                                          MA   =          235
39961
                                          Ha   =            222
000  n
mi
                                          Hp   =            213
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4434757
44                 X    =         1316254
60
 Y    =       16547444
32  feet           Y    =         5058578
62  meter
 Z    =      -14211103
62                 Z    =        -4325064
21
 XDOT =     -16953
510485                 XDOT =       -5233
610121
 YDOT =      14486
807666  feet/sec       YDOT =        4357
423241  meter/sec
 ZDOT =      11609
146663                 ZDOT =        3513
205567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5310670
18                 X    =         1618692
27
 Y    =      -16311147
39  feet           Y    =        -4971637
72  meter
 Z    =      -14183924
22                 Z    =        -4323260
10
 XDOT =      20998
113247                 XDOT =        6400
224918
 YDOT =      -3135
302643  feet/sec       YDOT =        -955
640245  meter/sec
 ZDOT =      11498
812634                 ZDOT =        3504
838091


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
10831624  
00016717  00000-0  10270-3 0  9058
2 25544  51
6432 116
4054 0006325   9
5400 350
5871 15
54381137 20704


Satellite: ISS
Catalog Number: 25544
Epoch time:      16013
10831624   =   yrday
fracday
Element set:     905
Inclination:       51
6432  deg
RA of node:       116
4054  deg
Eccentricity:     
0006325     
Arg of perigee:     9
5400  deg
Mean anomaly:     350
5871  deg
Mean motion:   15
54381137  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2070
Checksum:              266


Coasting Arc #7 (Orbit 2085)
---------------------------------------

Vector Time (GMT): 2016/014/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -252892
62                 A    =         6784672
74  meter
 Y    =       -6066549
31  meter          E    =           
0015337
 Z    =        3020591
03                 I    =           51
99235
 XDOT =       5165
615391                 Wp   =           72
30921
 YDOT =      -2707
026541  meter/sec      RA   =          110
49146  deg
 ZDOT =      -4979
030697                 TA   =           73
26858
                                          MA   =           73
10032
                                          Ha   =            222
074  n
mi
                                          Hp   =            213
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -829700
19                 X    =         -199708
71
 Y    =      -19903376
99  feet           Y    =        -6069079
97  meter
 Z    =        9910075
55                 Z    =         3019491
69
 XDOT =      16947
557057                 XDOT =        5219
687770
 YDOT =      -8881
320674  feet/sec       YDOT =       -2648
958843  meter/sec
 ZDOT =     -16335
402550                 ZDOT =       -4953
806453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9893974
75                 X    =        -3015683
50
 Y    =       17292037
79  feet           Y    =         5270613
12  meter
 Z    =        9906417
52                 Z    =         3019476
06
 XDOT =     -17897
689486                 XDOT =       -5455
215755
 YDOT =       -897
555130  feet/sec       YDOT =        -273
574804  meter/sec
 ZDOT =     -16225
534766                 ZDOT =       -4945
542997


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
13697858  
00016717  00000-0  10270-3 0  9062
2 25544  51
6430 111
2751 0006409  14
2836 345
8497 15
54401521 20866


Satellite: ISS
Catalog Number: 25544
Epoch time:      16014
13697858   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:       111
2751  deg
Eccentricity:     
0006409     
Arg of perigee:    14
2836  deg
Mean anomaly:     345
8497  deg
Mean motion:   15
54401521  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2086
Checksum:              302


Coasting Arc #8 (Orbit 2100)
---------------------------------------

Vector Time (GMT): 2016/015/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -702221
97                 A    =         6787636
34  meter
 Y    =        6597686
73  meter          E    =           
0014786
 Z    =       -1396812
68                 I    =           52
01265
 XDOT =      -4927
251746                 Wp   =           28
67420
 YDOT =        703
397617  meter/sec      RA   =          105
53800  deg
 ZDOT =       5837
591731                 TA   =          316
17369
                                          MA   =          316
29092
                                          Ha   =            222
113  n
mi
                                          Hp   =            213
195

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2303877
84                 X    =         -769161
69
 Y    =       21645953
84  feet           Y    =         6589459
73  meter
 Z    =       -4582718
75                 Z    =        -1400386
47
 XDOT =     -16165
524101                 XDOT =       -4963
107320
 YDOT =       2307
734964  feet/sec       YDOT =         648
097365  meter/sec
 ZDOT =      19152
203843                 ZDOT =        5813
569534

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13207110
70                 X    =         4025527
34
 Y    =      -17299536
27  feet           Y    =        -5272898
66  meter
 Z    =       -4599429
69                 Z    =        -1401906
17
 XDOT =      13848
871168                 XDOT =        4221
135932
 YDOT =       5541
576622  feet/sec       YDOT =        1689
072554  meter/sec
 ZDOT =      19047
908379                 ZDOT =        5805
802474


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
10133612  
00016717  00000-0  10270-3 0  9074
2 25544  51
6429 106
4648 0006454  16
4264 343
7097 15
54423465 21016


Satellite: ISS
Catalog Number: 25544
Epoch time:      16015
10133612   =   yrday
fracday
Element set:     907
Inclination:       51
6429  deg
RA of node:       106
4648  deg
Eccentricity:     
0006454     
Arg of perigee:    16
4264  deg
Mean anomaly:     343
7097  deg
Mean motion:   15
54423465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2101
Checksum:              284


Coasting Arc #9 (Orbit 2116)
---------------------------------------

Vector Time (GMT): 2016/016/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1580172
97                 A    =         6788453
44  meter
 Y    =       -6586233
78  meter          E    =           
0010001
 Z    =        -438915
22                 I    =           52
02254
 XDOT =       4506
254290                 Wp   =          104
03506
 YDOT =       1474
615615  meter/sec      RA   =          100
59171  deg
 ZDOT =      -6021
277534                 TA   =           80
67066
                                          MA   =           80
55758
                                          Ha   =            222
174  n
mi
                                          Hp   =            213
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5184294
54                 X    =         1655836
47
 Y    =      -21608378
53  feet           Y    =        -6568140
18  meter
 Z    =       -1440010
58                 Z    =         -431055
40
 XDOT =      14784
298852                 XDOT =        4518
678428
 YDOT =       4837
977741  feet/sec       YDOT =        1525
076982  meter/sec
 ZDOT =     -19754
847553                 ZDOT =       -5999
357261

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15407165
47                 X    =        -4696104
04
 Y    =       16016198
70  feet           Y    =         4881737
36  meter
 Z    =       -1404704
41                 Z    =         -428153
91
 XDOT =      -9250
544281                 XDOT =       -2819
565897
 YDOT =     -10588
576985  feet/sec       YDOT =       -3227
398265  meter/sec
 ZDOT =     -19660
065916                 ZDOT =       -5992
388091


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
12997281  
00016717  00000-0  10270-3 0  9088
2 25544  51
6426 101
3343 0006305  20
5581 339
5825 15
54401085 21175


Satellite: ISS
Catalog Number: 25544
Epoch time:      16016
12997281   =   yrday
fracday
Element set:     908
Inclination:       51
6426  deg
RA of node:       101
3343  deg
Eccentricity:     
0006305     
Arg of perigee:    20
5581  deg
Mean anomaly:     339
5825  deg
Mean motion:   15
54401085  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2117
Checksum:              287


Coasting Arc #10 (Orbit 2132)
---------------------------------------

Vector Time (GMT): 2016/017/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2306974
12                 A    =         6786353
58  meter
 Y    =        5983403
11  meter          E    =           
0018888
 Z    =        2187107
59                 I    =           52
02059
 XDOT =      -3976
951104                 Wp   =           55
92414
 YDOT =      -3558
813985  meter/sec      RA   =           95
64260  deg
 ZDOT =       5517
554927                 TA   =          328
25072
                                          MA   =          328
36448
                                          Ha   =            222
236  n
mi
                                          Hp   =            212
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7568812
72                 X    =        -2384334
52
 Y    =       19630587
62  feet           Y    =         5957172
43  meter
 Z    =        7175549
83                 Z    =         2175713
08
 XDOT =     -13047
739843                 XDOT =       -3963
661777
 YDOT =     -11675
898900  feet/sec       YDOT =       -3603
212615  meter/sec
 ZDOT =      18102
214329                 ZDOT =        5498
268237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16268696
21                 X    =         4958698
60
 Y    =      -13367838
57  feet           Y    =        -4074517
19  meter
 Z    =        7125014
22                 Z    =         2171704
33
 XDOT =       4765
543557                 XDOT =        1452
537676
 YDOT =      15445
433640  feet/sec       YDOT =        4707
768174  meter/sec
 ZDOT =      18019
243607                 ZDOT =        5492
265451


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
15859416  
00016717  00000-0  10270-3 0  9090
2 25544  51
6421  96
2028 0006508  23
0191 337
1252 15
54465526 21338


Satellite: ISS
Catalog Number: 25544
Epoch time:      16017
15859416   =   yrday
fracday
Element set:     909
Inclination:       51
6421  deg
RA of node:        96
2028  deg
Eccentricity:     
0006508     
Arg of perigee:    23
0191  deg
Mean anomaly:     337
1252  deg
Mean motion:   15
54465526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2133
Checksum:              292


Coasting Arc #11 (Orbit 2147)
---------------------------------------

Vector Time (GMT): 2016/018/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2964633
95                 A    =         6782549
11  meter
 Y    =       -4844097
96  meter          E    =           
0010906
 Z    =       -3721332
52                 I    =           52
00948
 XDOT =       3323
644758                 Wp   =           50
87333
 YDOT =       5364
825731  meter/sec      RA   =           90
68591  deg
 ZDOT =      -4337
447656                 TA   =          173
18737
                                          MA   =          173
17254
                                          Ha   =            222
244  n
mi
                                          Hp   =            212
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9726489
35                 X    =         3036658
07
 Y    =      -15892709
83  feet           Y    =        -4810542
66  meter
 Z    =      -12209096
18                 Z    =        -3706756
29
 XDOT =      10904
346319                 XDOT =        3284
476307
 YDOT =      17601
134288  feet/sec       YDOT =        5401
774017  meter/sec
 ZDOT =     -14230
471313                 ZDOT =       -4321
397301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16184788
33                 X    =        -4933123
48
 Y    =        9316508
92  feet           Y    =         2839671
92  meter
 Z    =      -12144963
51                 Z    =        -3701784
88
 XDOT =       -620
310642                 XDOT =        -189
070684
 YDOT =     -19531
206703  feet/sec       YDOT =       -5953
111803  meter/sec
 ZDOT =     -14161
882527                 ZDOT =       -4316
541794


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
12291635  
00016717  00000-0  10270-3 0  9103
2 25544  51
6414  91
3926 0006487  26
4070 333
7412 15
54465510 21481


Satellite: ISS
Catalog Number: 25544
Epoch time:      16018
12291635   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:        91
3926  deg
Eccentricity:     
0006487     
Arg of perigee:    26
4070  deg
Mean anomaly:     333
7412  deg
Mean motion:   15
54465510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2148
Checksum:              288


Coasting Arc #12 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2016/019/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3508702
25                 A    =         6778697
10  meter
 Y    =        3257666
79  meter          E    =           
0010261
 Z    =        4789144
69                 I    =           51
99622
 XDOT =      -2591
990030                 Wp   =           77
87705
 YDOT =      -6715
119800  meter/sec      RA   =           85
71695  deg
 ZDOT =       2666
064653                 TA   =          345
95434
                                          MA   =          345
98286
                                          Ha   =            222
526  n
mi
                                          Hp   =            212
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11511490
33                 X    =        -3568132
99
 Y    =       10687883
18  feet           Y    =         3218097
69  meter
 Z    =       15712416
97                 Z    =         4771956
15
 XDOT =      -8503
904297                 XDOT =       -2529
657791
 YDOT =     -22031
232938  feet/sec       YDOT =       -6743
756726  meter/sec
 ZDOT =       8746
931276                 ZDOT =        2653
624625

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15229934
67                 X    =         4642084
09
 Y    =       -4141369
67  feet           Y    =        -1262289
48  meter
 Z    =       15637245
62                 Z    =         4766232
47
 XDOT =      -2848
450084                 XDOT =        -868
207586
 YDOT =      22386
770506  feet/sec       YDOT =        6823
487650  meter/sec
 ZDOT =       8694
267772                 ZDOT =        2650
012817


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
15151523  
00016717  00000-0  10270-3 0  9119
2 25544  51
6416  86
2612 0006665  30
9105 329
2439 15
54461324 21641


Satellite: ISS
Catalog Number: 25544
Epoch time:      16019
15151523   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:        86
2612  deg
Eccentricity:     
0006665     
Arg of perigee:    30
9105  deg
Mean anomaly:     329
2439  deg
Mean motion:   15
54461324  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2164
Checksum:              284


Coasting Arc #13 (Orbit 2178)
---------------------------------------

Vector Time (GMT): 2016/020/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3981409
93                 A    =         6776370
34  meter
 Y    =       -1406511
97  meter          E    =           
0019500
 Z    =       -5316316
84                 I    =           51
98452
 XDOT =       1734
665433                 Wp   =           69
71302
 YDOT =       7426
563905  meter/sec      RA   =           80
73836  deg
 ZDOT =       -661
102544                 TA   =          193
96670
                                          MA   =          194
02071
                                          Ha   =            222
342  n
mi
                                          Hp   =            212
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13062368
54                 X    =         4022666
15
 Y    =       -4614540
57  feet           Y    =        -1361758
27  meter
 Z    =      -17441984
38                 Z    =        -5296876
17
 XDOT =       5691
159558                 XDOT =        1654
702168
 YDOT =      24365
367141  feet/sec       YDOT =        7445
515012  meter/sec
 ZDOT =      -2168
971601                 ZDOT =        -652
869904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13851620
19                 X    =        -4221973
83
 Y    =       -1730833
98  feet           Y    =         -527558
20  meter
 Z    =      -17357393
46                 Z    =        -5290533
53
 XDOT =       5611
416053                 XDOT =        1710
359613
 YDOT =     -23347
417235  feet/sec       YDOT =       -7116
292773  meter/sec
 ZDOT =      -2134
705195                 ZDOT =        -650
658143


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16020
11581248  
00016717  00000-0  10270-3 0  9129
2 25544  51
6405  81
4503 0006585  34
2475 325
9102 15
54517482 21796


Satellite: ISS
Catalog Number: 25544
Epoch time:      16020
11581248   =   yrday
fracday
Element set:     912
Inclination:       51
6405  deg
RA of node:        81
4503  deg
Eccentricity:     
0006585     
Arg of perigee:    34
2475  deg
Mean anomaly:     325
9102  deg
Mean motion:   15
54517482  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2179
Checksum:              289


Coasting Arc #14 (Orbit 2194)
---------------------------------------

Vector Time (GMT): 2016/021/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4324026
21                 A    =         6776885
99  meter
 Y    =        -567064
34  meter          E    =           
0010985
 Z    =        5182226
27                 I    =           51
98072
 XDOT =       -746
870959                 Wp   =           44
72482
 YDOT =      -7501
231320  meter/sec      RA   =           75
75754  deg
 ZDOT =      -1434
562894                 TA   =           59
05651
                                          MA   =           58
94859
                                          Ha   =            222
508  n
mi
                                          Hp   =            212
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14186437
70                 X    =        -4342536
50
 Y    =       -1860447
31  feet           Y    =         -615522
23  meter
 Z    =       17002054
70                 Z    =         5161176
51
 XDOT =      -2450
364040                 XDOT =        -655
966432
 YDOT =     -24610
338975  feet/sec       YDOT =       -7509
074972  meter/sec
 ZDOT =      -4706
571173                 ZDOT =       -1437
970561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12109591
68                 X    =         3691003
54
 Y    =        7820909
39  feet           Y    =         2383813
18  meter
 Z    =       16910863
63                 Z    =         5154431
23
 XDOT =      -7819
172684                 XDOT =       -2383
283834
 YDOT =      22379
890045  feet/sec       YDOT =        6821
390486  meter/sec
 ZDOT =      -4719
883640                 ZDOT =       -1438
620533


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16021
14438546  
00016717  00000-0  10270-3 0  9136
2 25544  51
6410  76
3196 0006541  37
9543 322
2070 15
54522901 21955


Satellite: ISS
Catalog Number: 25544
Epoch time:      16021
14438546   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:        76
3196  deg
Eccentricity:     
0006541     
Arg of perigee:    37
9543  deg
Mean anomaly:     322
2070  deg
Mean motion:   15
54522901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2195
Checksum:              285


Coasting Arc #15 (Orbit 2209)
---------------------------------------

Vector Time (GMT): 2016/022/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4523925
53                 A    =         6779805
73  meter
 Y    =        2398658
23  meter          E    =           
0013087
 Z    =       -4453885
87                 I    =           51
98081
 XDOT =       -368
209847                 Wp   =           82
59839
 YDOT =       6882
433047  meter/sec      RA   =           70
78032  deg
 ZDOT =       3342
590972                 TA   =          220
98752
                                          MA   =          221
08596
                                          Ha   =            222
449  n
mi
                                          Hp   =            212
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14842275
37                 X    =         4518401
62
 Y    =        7869613
62  feet           Y    =         2449217
10  meter
 Z    =      -14612486
45                 Z    =        -4431923
43
 XDOT =      -1208
037556                 XDOT =        -461
380141
 YDOT =      22580
160916  feet/sec       YDOT =        6877
794369  meter/sec
 ZDOT =      10966
505813                 ZDOT =        3340
576376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10336934
50                 X    =        -3150697
64
 Y    =      -13346649
81  feet           Y    =        -4068058
86  meter
 Z    =      -14517694
06                 Z    =        -4424993
15
 XDOT =       9540
917910                 XDOT =        2908
071779
 YDOT =     -19271
117225  feet/sec       YDOT =       -5873
836530  meter/sec
 ZDOT =      10956
410200                 ZDOT =        3339
513829


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16022
10866104  
00016717  00000-0  10270-3 0  9149
2 25544  51
6398  71
5082 0006578  42
3957 317
7703 15
54551516 22104


Satellite: ISS
Catalog Number: 25544
Epoch time:      16022
10866104   =   yrday
fracday
Element set:     914
Inclination:       51
6398  deg
RA of node:        71
5082  deg
Eccentricity:     
0006578     
Arg of perigee:    42
3957  deg
Mean anomaly:     317
7703  deg
Mean motion:   15
54551516  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2210
Checksum:              297


Coasting Arc #16 (Orbit 2225)
---------------------------------------

Vector Time (GMT): 2016/023/02:21:59
494
Vector Time (MET): N/A
Weight (LBS)     : 922092
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4486382
27                 A    =         6783865
66  meter
 Y    =       -3994175
67  meter          E    =           
0017852
 Z    =        3141920
77                 I    =           51
98362
 XDOT =       1627
869421                 Wp   =           78
36496
 YDOT =      -5689
299896  meter/sec      RA   =           65
81431  deg
 ZDOT =      -4881
199415                 TA   =           65
59804
                                          MA   =           65
41185
                                          Ha   =            222
409  n
mi
                                          Hp   =            212
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14719101
95                 X    =        -4456646
77
 Y    =      -13104250
90  feet           Y    =        -4044179
23  meter
 Z    =       10308139
03                 Z    =         3120199
55
 XDOT =       5340
778941                 XDOT =        1715
077876
 YDOT =     -18665
682074  feet/sec       YDOT =       -5670
608177  meter/sec
 ZDOT =     -16014
433777                 ZDOT =       -4873
080204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8341213
92                 X    =         2542402
00
 Y    =       17908516
52  feet           Y    =         5458515
83  meter
 Z    =       10214708
54                 Z    =         3113443
16
 XDOT =     -11123
331831                 XDOT =       -3390
391542
 YDOT =      14345
291144  feet/sec       YDOT =        4372
444741  meter/sec
 ZDOT =     -15978
085997                 ZDOT =       -4870
120612


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16023
13720784  
00016717  00000-0  10270-3 0  9157
2 25544  51
6401  66
3769 0006550  44
4522 315
7156 15
54594365 22260


Satellite: ISS
Catalog Number: 25544
Epoch time:      16023
13720784   =   yrday
fracday
Element set:     915
Inclination:       51
6401  deg
RA of node:        66
3769  deg
Eccentricity:     
0006550     
Arg of perigee:    44
4522  deg
Mean anomaly:     315
7156  deg
Mean motion:   15
54594365  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2226
Checksum:              301
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