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

 
Date: December 5th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14800 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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


There are no maneuvers



Coasting Arc #1 (Orbit 1455)
---------------------------------------

Vector Time (GMT): 2015/338/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1699682
00                 A    =         6783857
87  meter
 Y    =        5683089
82  meter          E    =           
0007071
 Z    =        3281944
73                 I    =           51
38176
 XDOT =      -5988
009932                 Wp   =          127
73476
 YDOT =        926
898888  meter/sec      RA   =          312
88002  deg
 ZDOT =      -4703
457387                 TA   =           13
97714
                                          MA   =           13
95758
                                          Ha   =            219
758  n
mi
                                          Hp   =            216
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5576384
52                 X    =        -1779047
97
 Y    =       18645307
82  feet           Y    =         5663639
04  meter
 Z    =       10767535
19                 Z    =         3273495
26
 XDOT =     -19645
701877                 XDOT =       -5975
081877
 YDOT =       3041
006850  feet/sec       YDOT =         860
009372  meter/sec
 ZDOT =     -15431
290641                 ZDOT =       -4732
514800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19421801
34                 X    =        -5919765
05
 Y    =        1531982
51  feet           Y    =          466948
27  meter
 Z    =       10729866
93                 Z    =         3270463
44
 XDOT =      -9836
580259                 XDOT =       -2998
189663
 YDOT =     -15681
604742  feet/sec       YDOT =       -4779
753125  meter/sec
 ZDOT =     -15557
008574                 ZDOT =       -4741
776213


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   15338
64755711  
00016717  00000-0  10270-3 0  9003
2 25544  51
6425 313
3539 0008078 241
8879 118
1458 15
54448920 14560


Satellite: ISS
Catalog Number: 25544
Epoch time:      15338
64755711   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:       313
3539  deg
Eccentricity:     
0008078     
Arg of perigee:   241
8879  deg
Mean anomaly:     118
1458  deg
Mean motion:   15
54448920  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1456
Checksum:              327


Coasting Arc #2 (Orbit 1470)
---------------------------------------

Vector Time (GMT): 2015/339/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2891007
99                 A    =         6787191
90  meter
 Y    =       -5903449
26  meter          E    =           
0003821
 Z    =       -1680853
90                 I    =           51
37155
 XDOT =       5075
563955                 Wp   =          317
15680
 YDOT =        867
120083  meter/sec      RA   =          307
88238  deg
 ZDOT =       5679
437508                 TA   =           24
35439
                                          MA   =           24
33634
                                          Ha   =            219
554  n
mi
                                          Hp   =            216
936

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9484934
36                 X    =         2964971
99
 Y    =      -19368271
86  feet           Y    =        -5870706
51  meter
 Z    =       -5514612
53                 Z    =        -1666630
26
 XDOT =      16652
112713                 XDOT =        5037
901504
 YDOT =       2844
882161  feet/sec       YDOT =         923
667692  meter/sec
 ZDOT =      18633
325156                 ZDOT =        5704
002413

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21533625
51                 X    =         6563449
06
 Y    =        1443590
88  feet           Y    =          440006
50  meter
 Z    =       -5451963
31                 Z    =        -1661758
42
 XDOT =       3756
165006                 XDOT =        1144
879094
 YDOT =      14803
439403  feet/sec       YDOT =        4512
088330  meter/sec
 ZDOT =      18739
264813                 ZDOT =        5711
727915


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   15339
61188310  
00016717  00000-0  10270-3 0  9017
2 25544  51
6420 308
5438 0008088 245
6943 114
3365 15
54459887 14710


Satellite: ISS
Catalog Number: 25544
Epoch time:      15339
61188310   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:       308
5438  deg
Eccentricity:     
0008088     
Arg of perigee:   245
6943  deg
Mean anomaly:     114
3365  deg
Mean motion:   15
54459887  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1471
Checksum:              321


Coasting Arc #3 (Orbit 1486)
---------------------------------------

Vector Time (GMT): 2015/340/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3768630
64                 A    =         6788287
26  meter
 Y    =        5635288
23  meter          E    =           
0011419
 Z    =        -130569
54                 I    =           51
35756
 XDOT =      -3919
187604                 Wp   =          176
21366
 YDOT =      -2758
815572  meter/sec      RA   =          302
89055  deg
 ZDOT =      -5990
115835                 TA   =            5
19907
                                          MA   =            5
18722
                                          Ha   =            219
317  n
mi
                                          Hp   =            217
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12364273
77                 X    =        -3830731
46
 Y    =       18488478
43  feet           Y    =         5592797
69  meter
 Z    =        -428377
75                 Z    =         -149027
73
 XDOT =     -12858
227047                 XDOT =       -3858
948460
 YDOT =      -9051
232192  feet/sec       YDOT =       -2802
305531  meter/sec
 ZDOT =     -19652
611006                 ZDOT =       -6009
008491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21871847
25                 X    =        -6666539
04
 Y    =       -4030578
48  feet           Y    =        -1228520
32  meter
 Z    =        -509257
17                 Z    =         -155221
59
 XDOT =       2978
025996                 XDOT =         907
702324
 YDOT =     -13681
234693  feet/sec       YDOT =       -4170
040334  meter/sec
 ZDOT =     -19733
662135                 ZDOT =       -6014
820219


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   15340
64047981  
00016717  00000-0  10270-3 0  9021
2 25544  51
6430 303
4130 0008078 248
7936 111
2354 15
54484332 14873


Satellite: ISS
Catalog Number: 25544
Epoch time:      15340
64047981   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:       303
4130  deg
Eccentricity:     
0008078     
Arg of perigee:   248
7936  deg
Mean anomaly:     111
2354  deg
Mean motion:   15
54484332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1487
Checksum:              298


Coasting Arc #4 (Orbit 1502)
---------------------------------------

Vector Time (GMT): 2015/341/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4320275
02                 A    =         6786568
14  meter
 Y    =       -4860664
05  meter          E    =           
0005984
 Z    =        1929740
18                 I    =           51
33535
 XDOT =       2633
783301                 Wp   =           60
46571
 YDOT =       4558
141322  meter/sec      RA   =          297
89638  deg
 ZDOT =       5574
484746                 TA   =          320
90100
                                          MA   =          320
94423
                                          Ha   =            219
081  n
mi
                                          Hp   =            217
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14174130
64                 X    =         4364932
97
 Y    =      -15947060
53  feet           Y    =        -4812102
26  meter
 Z    =        6331168
58                 Z    =         1950835
81
 XDOT =       8641
021329                 XDOT =        2555
538158
 YDOT =      14954
531896  feet/sec       YDOT =        4587
156305  meter/sec
 ZDOT =      18288
991949                 ZDOT =        5587
089468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20350891
39                 X    =         6202951
69
 Y    =        6315151
09  feet           Y    =         1924858
05  meter
 Z    =        6423278
05                 Z    =         1957815
15
 XDOT =      -9660
425164                 XDOT =       -2944
497590
 YDOT =      12441
189878  feet/sec       YDOT =        3792
074675  meter/sec
 ZDOT =      18342
519094                 ZDOT =        5590
799820


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   15341
66905736  
00016717  00000-0  10270-3 0  9036
2 25544  51
6427 298
2819 0008044 253
1740 106
8531 15
54519348 15032


Satellite: ISS
Catalog Number: 25544
Epoch time:      15341
66905736   =   yrday
fracday
Element set:     903
Inclination:       51
6427  deg
RA of node:       298
2819  deg
Eccentricity:     
0008044     
Arg of perigee:   253
1740  deg
Mean anomaly:     106
8531  deg
Mean motion:   15
54519348  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1503
Checksum:              312


Coasting Arc #5 (Orbit 1517)
---------------------------------------

Vector Time (GMT): 2015/342/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4563099
42                 A    =         6782754
77  meter
 Y    =        3585882
11  meter          E    =           
0002983
 Z    =       -3507098
38                 I    =           51
30994
 XDOT =      -1330
065888                 Wp   =          242
65894
 YDOT =      -6077
837606  meter/sec      RA   =          292
89313  deg
 ZDOT =      -4482
220666                 TA   =          338
84148
                                          MA   =          338
85382
                                          Ha   =            218
618  n
mi
                                          Hp   =            217
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14970798
63                 X    =        -4585822
08
 Y    =       11764705
09  feet           Y    =         3534727
67  meter
 Z    =      -11506228
29                 Z    =        -3529320
34
 XDOT =      -4363
733229                 XDOT =       -1240
229903
 YDOT =     -19940
412093  feet/sec       YDOT =       -6092
208722  meter/sec
 ZDOT =     -14705
448378                 ZDOT =       -4488
464102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17001008
19                 X    =        -5181907
30
 Y    =       -8441790
80  feet           Y    =        -2573057
84  meter
 Z    =      -11602942
54                 Z    =        -3536576
88
 XDOT =      15589
643318                 XDOT =        4751
723283
 YDOT =     -11141
497510  feet/sec       YDOT =       -3395
928441  meter/sec
 ZDOT =     -14731
195288                 ZDOT =       -4490
068324


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   15342
63333139  
00016717  00000-0  10270-3 0  9047
2 25544  51
6436 293
4718 0008024 256
8364 103
1894 15
54564311 15185


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
63333139   =   yrday
fracday
Element set:     904
Inclination:       51
6436  deg
RA of node:       293
4718  deg
Eccentricity:     
0008024     
Arg of perigee:   256
8364  deg
Mean anomaly:     103
1894  deg
Mean motion:   15
54564311  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1518
Checksum:              306


Coasting Arc #6 (Orbit 1533)
---------------------------------------

Vector Time (GMT): 2015/343/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4540547
29                 A    =         6778696
84  meter
 Y    =       -1917647
56  meter          E    =           
0005003
 Z    =        4656613
36                 I    =           51
28480
 XDOT =         92
972141                 Wp   =          188
03464
 YDOT =       7120
952138  meter/sec      RA   =          287
87647  deg
 ZDOT =       2837
337952                 TA   =          233
62501
                                          MA   =          233
67118
                                          Ha   =            218
564  n
mi
                                          Hp   =            217
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14896808
71                 X    =         4539033
05
 Y    =       -6291494
61  feet           Y    =        -1866880
97  meter
 Z    =       15277602
89                 Z    =         4678666
94
 XDOT =        305
026709                 XDOT =           -
445909
 YDOT =      23362
703865  feet/sec       YDOT =        7121
469271  meter/sec
 ZDOT =       9308
851548                 ZDOT =        2837
563224

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12192503
29                 X    =         3716275
00
 Y    =       10483743
64  feet           Y    =         3195445
06  meter
 Z    =       15373254
28                 Z    =         4685767
90
 XDOT =     -20075
243980                 XDOT =       -6118
934365
 YDOT =       9676
088617  feet/sec       YDOT =        2949
271810  meter/sec
 ZDOT =       9308
398839                 ZDOT =        2837
199966


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   15343
66187294  
00016717  00000-0  10270-3 0  9051
2 25544  51
6435 288
3405 0008032 260
1934  99
8312 15
54583124 15347


Satellite: ISS
Catalog Number: 25544
Epoch time:      15343
66187294   =   yrday
fracday
Element set:     905
Inclination:       51
6435  deg
RA of node:       288
3405  deg
Eccentricity:     
0008032     
Arg of perigee:   260
1934  deg
Mean anomaly:      99
8312  deg
Mean motion:   15
54583124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1534
Checksum:              312


Coasting Arc #7 (Orbit 1548)
---------------------------------------

Vector Time (GMT): 2015/344/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4305915
12                 A    =         6776121
68  meter
 Y    =         -13083
00  meter          E    =           
0006516
 Z    =       -5237804
96                 I    =           51
26849
 XDOT =       1036
317477                 Wp   =           82
86321
 YDOT =      -7548
480052  meter/sec      RA   =          282
84883  deg
 ZDOT =       -833
183856                 TA   =          179
12720
                                          MA   =          179
12607
                                          Ha   =            217
870  n
mi
                                          Hp   =            217
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14127018
11                 X    =        -4280005
22
 Y    =         -42923
22  feet           Y    =          -61089
24  meter
 Z    =      -17184399
47                 Z    =        -5258659
56
 XDOT =       3399
991723                 XDOT =        1124
696748
 YDOT =     -24765
354500  feet/sec       YDOT =       -7536
397033  meter/sec
 ZDOT =      -2733
542834                 ZDOT =        -827
935579

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6382088
09                 X    =        -1945260
45
 Y    =      -12479545
95  feet           Y    =        -3803765
60  meter
 Z    =      -17274488
50                 Z    =        -5265264
09
 XDOT =      22669
237190                 XDOT =        6909
583495
 YDOT =      -7843
209206  feet/sec       YDOT =       -2390
610166  meter/sec
 ZDOT =      -2709
367359                 ZDOT =        -825
815171


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   15344
62611358  
00016717  00000-0  10270-3 0  9062
2 25544  51
6443 283
5302 0008017 264
2186  95
8053 15
54627917 15499


Satellite: ISS
Catalog Number: 25544
Epoch time:      15344
62611358   =   yrday
fracday
Element set:     906
Inclination:       51
6443  deg
RA of node:       283
5302  deg
Eccentricity:     
0008017     
Arg of perigee:   264
2186  deg
Mean anomaly:      95
8053  deg
Mean motion:   15
54627917  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1549
Checksum:              315


Coasting Arc #8 (Orbit 1564)
---------------------------------------

Vector Time (GMT): 2015/345/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3907512
65                 A    =         6776321
66  meter
 Y    =        2003634
36  meter          E    =           
0005153
 Z    =        5165427
39                 I    =           51
26329
 XDOT =      -2036
780456                 Wp   =          294
30665
 YDOT =       7278
253698  meter/sec      RA   =          277
81735  deg
 ZDOT =      -1281
341533                 TA   =          168
07330
                                          MA   =          168
06109
                                          Ha   =            217
450  n
mi
                                          Hp   =            217
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12819923
39                 X    =         3859725
20
 Y    =        6573603
53  feet           Y    =         2047063
04  meter
 Z    =       16946940
27                 Z    =         5184293
61
 XDOT =      -6682
350577                 XDOT =       -2111
791968
 YDOT =      23878
785100  feet/sec       YDOT =        7255
057787  meter/sec
 ZDOT =      -4203
876420                 ZDOT =       -1291
417375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         225173
57                 X    =           68632
90
 Y    =       14309307
57  feet           Y    =         4361476
95  meter
 Z    =       17028050
32                 Z    =         5190149
74
 XDOT =     -23140
577584                 XDOT =       -7053
248048
 YDOT =       5424
427963  feet/sec       YDOT =        1653
365643  meter/sec
 ZDOT =      -4248
845831                 ZDOT =       -1295
048209


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   15345
65461825  
00016717  00000-0  10270-3 0  9079
2 25544  51
6442 278
3992 0008185 268
2081  91
8134 15
54672719 15653


Satellite: ISS
Catalog Number: 25544
Epoch time:      15345
65461825   =   yrday
fracday
Element set:     907
Inclination:       51
6442  deg
RA of node:       278
3992  deg
Eccentricity:     
0008185     
Arg of perigee:   268
2081  deg
Mean anomaly:      91
8134  deg
Mean motion:   15
54672719  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1565
Checksum:              336


Coasting Arc #9 (Orbit 1579)
---------------------------------------

Vector Time (GMT): 2015/346/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3379606
92                 A    =         6779313
40  meter
 Y    =       -3849753
98  meter          E    =           
0003091
 Z    =       -4442601
45                 I    =           51
27013
 XDOT =       2913
005476                 Wp   =          168
21822
 YDOT =      -6305
115895  meter/sec      RA   =          272
79014  deg
 ZDOT =       3245
148214                 TA   =          134
65691
                                          MA   =          134
63172
                                          Ha   =            217
222  n
mi
                                          Hp   =            216
761

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11087949
23                 X    =        -3314726
28
 Y    =      -12630426
45  feet           Y    =        -3887183
76  meter
 Z    =      -14575464
07                 Z    =        -4458861
78
 XDOT =       9557
104579                 XDOT =        2967
530552
 YDOT =     -20686
075770  feet/sec       YDOT =       -6272
236202  meter/sec
 ZDOT =      10646
811725                 ZDOT =        3259
430889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5652210
07                 X    =         1722793
63
 Y    =      -15763630
78  feet           Y    =        -4804754
66  meter
 Z    =      -14644961
90                 Z    =        -4463784
39
 XDOT =      21534
883197                 XDOT =        6563
832398
 YDOT =      -2235
991821  feet/sec       YDOT =        -681
530307  meter/sec
 ZDOT =      10709
757238                 ZDOT =        3264
334006


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   15346
61882671  
00016717  00000-0  10270-3 0  9083
2 25544  51
6445 273
5886 0008158 271
8621  88
1597 15
54666297 15808


Satellite: ISS
Catalog Number: 25544
Epoch time:      15346
61882671   =   yrday
fracday
Element set:     908
Inclination:       51
6445  deg
RA of node:       273
5886  deg
Eccentricity:     
0008158     
Arg of perigee:   271
8621  deg
Mean anomaly:      88
1597  deg
Mean motion:   15
54666297  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1580
Checksum:              355


Coasting Arc #10 (Orbit 1595)
---------------------------------------

Vector Time (GMT): 2015/347/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2733962
77                 A    =         6783450
84  meter
 Y    =        5347653
98  meter          E    =           
0004830
 Z    =        3148901
98                 I    =           51
28322
 XDOT =      -3672
991649                 Wp   =           91
95996
 YDOT =       4711
819088  meter/sec      RA   =          267
77475  deg
 ZDOT =      -4806
660548                 TA   =           51
51863
                                          MA   =           51
47532
                                          Ha   =            218
053  n
mi
                                          Hp   =            217
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8969694
11                 X    =         2658664
61
 Y    =       17544796
52  feet           Y    =         5377805
64  meter
 Z    =       10331043
23                 Z    =         3162000
66
 XDOT =     -12050
497536                 XDOT =       -3702
058429
 YDOT =      15458
724043  feet/sec       YDOT =        4670
583209  meter/sec
 ZDOT =     -15769
883688                 ZDOT =       -4824
573377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10678785
24                 X    =        -3254893
74
 Y    =       16525368
61  feet           Y    =         5036932
35  meter
 Z    =       10386601
46                 Z    =         3165836
13
 XDOT =     -18166
037073                 XDOT =       -5537
008100
 YDOT =      -1765
210476  feet/sec       YDOT =        -538
036153  meter/sec
 ZDOT =     -15848
197736                 ZDOT =       -4830
530670


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   15347
64729788  
00016717  00000-0  10270-3 0  9097
2 25544  51
6442 268
4578 0008062 275
6871  84
3363 15
54688163 15961


Satellite: ISS
Catalog Number: 25544
Epoch time:      15347
64729788   =   yrday
fracday
Element set:     909
Inclination:       51
6442  deg
RA of node:       268
4578  deg
Eccentricity:     
0008062     
Arg of perigee:   275
6871  deg
Mean anomaly:      84
3363  deg
Mean motion:   15
54688163  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1596
Checksum:              362


Coasting Arc #11 (Orbit 1610)
---------------------------------------

Vector Time (GMT): 2015/348/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1970558
18                 A    =         6786691
91  meter
 Y    =       -6325012
49  meter          E    =           
0008538
 Z    =       -1446351
33                 I    =           51
29648
 XDOT =       4312
847870                 Wp   =          339
65059
 YDOT =      -2660
856390  meter/sec      RA   =          262
77019  deg
 ZDOT =       5757
771844                 TA   =            4
48744
                                          MA   =            4
47979
                                          Ha   =            218
274  n
mi
                                          Hp   =            217
272

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6465085
89                 X    =        -1892658
08
 Y    =      -20751353
31  feet           Y    =        -6346612
88  meter
 Z    =       -4745247
13                 Z    =        -1455735
21
 XDOT =      14149
763354                 XDOT =        4314
312682
 YDOT =      -8729
843800  feet/sec       YDOT =       -2612
619582  meter/sec
 ZDOT =      18890
327572                 ZDOT =        5778
726078

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14414243
07                 X    =         4393461
29
 Y    =      -16256406
51  feet           Y    =        -4954952
70  meter
 Z    =       -4784580
90                 Z    =        -1458340
26
 XDOT =      13548
662041                 XDOT =        4129
632190
 YDOT =       6424
443595  feet/sec       YDOT =        1958
170408  meter/sec
 ZDOT =      18981
385883                 ZDOT =        5785
526417


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   15348
61147197  
00016717  00000-0  10270-3 0  9105
2 25544  51
6441 263
6465 0008217 279
3720  80
6503 15
54725204 16119


Satellite: ISS
Catalog Number: 25544
Epoch time:      15348
61147197   =   yrday
fracday
Element set:     910
Inclination:       51
6441  deg
RA of node:       263
6465  deg
Eccentricity:     
0008217     
Arg of perigee:   279
3720  deg
Mean anomaly:      80
6503  deg
Mean motion:   15
54725204  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1611
Checksum:              298


Coasting Arc #12 (Orbit 1626)
---------------------------------------

Vector Time (GMT): 2015/349/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1075675
88                 A    =         6787574
97  meter
 Y    =        6681802
49  meter          E    =           
0006667
 Z    =        -454097
99                 I    =           51
30361
 XDOT =      -4807
489668                 Wp   =          185
30019
 YDOT =        368
666264  meter/sec      RA   =          257
77366  deg
 ZDOT =      -5962
845149                 TA   =          359
62049
                                          MA   =          359
62099
                                          Ha   =            218
538  n
mi
                                          Hp   =            217
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3529120
33                 X    =         1003084
20
 Y    =       21921924
19  feet           Y    =         6693425
56  meter
 Z    =       -1489822
79                 Z    =         -449048
43
 XDOT =     -15772
603898                 XDOT =       -4782
289784
 YDOT =       1209
534988  feet/sec       YDOT =         315
047068  meter/sec
 ZDOT =     -19563
140252                 ZDOT =       -5986
137633

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16665561
01                 X    =        -5079663
00
 Y    =       14674649
69  feet           Y    =         4472833
23  meter
 Z    =       -1469270
30                 Z    =         -447833
59
 XDOT =      -8288
771018                 XDOT =       -2526
417406
 YDOT =     -11382
283840  feet/sec       YDOT =       -3469
320114  meter/sec
 ZDOT =     -19663
868667                 ZDOT =       -5993
547170


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   15349
63990902  
00016717  00000-0  10270-3 0  9119
2 25544  51
6436 258
5153 0008225 281
8067  78
2163 15
54702468 16270


Satellite: ISS
Catalog Number: 25544
Epoch time:      15349
63990902   =   yrday
fracday
Element set:     911
Inclination:       51
6436  deg
RA of node:       258
5153  deg
Eccentricity:     
0008225     
Arg of perigee:   281
8067  deg
Mean anomaly:      78
2163  deg
Mean motion:   15
54702468  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1627
Checksum:              323


Coasting Arc #13 (Orbit 1642)
---------------------------------------

Vector Time (GMT): 2015/350/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -47016
91                 A    =         6785223
34  meter
 Y    =       -6376896
04  meter          E    =           
0008409
 Z    =        2301459
35                 I    =           51
30325
 XDOT =       5112
776677                 Wp   =           38
42648
 YDOT =       1909
225471  meter/sec      RA   =          252
77356  deg
 ZDOT =       5390
385878                 TA   =          347
35579
                                          MA   =          347
37687
                                          Ha   =            218
710  n
mi
                                          Hp   =            216
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -154254
94                 X    =           13115
05
 Y    =      -20921574
93  feet           Y    =        -6377085
72  meter
 Z    =        7550719
65                 Z    =         2301376
65
 XDOT =      16774
201697                 XDOT =        5064
862948
 YDOT =       6263
863093  feet/sec       YDOT =        1966
131718  meter/sec
 ZDOT =      17684
993039                 ZDOT =        5415
106329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17398696
49                 X    =         5303122
69
 Y    =      -11619327
68  feet           Y    =        -3541571
08  meter
 Z    =        7551559
05                 Z    =         2301715
20
 XDOT =       3026
947304                 XDOT =         922
613538
 YDOT =      16104
309157  feet/sec       YDOT =        4908
593431  meter/sec
 ZDOT =      17791
471483                 ZDOT =        5422
840508


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   15350
66832680  
00016717  00000-0  10270-3 0  9123
2 25544  51
6428 253
3824 0008349 287
2020  72
8219 15
54768079 16435


Satellite: ISS
Catalog Number: 25544
Epoch time:      15350
66832680   =   yrday
fracday
Element set:     912
Inclination:       51
6428  deg
RA of node:       253
3824  deg
Eccentricity:     
0008349     
Arg of perigee:   287
2020  deg
Mean anomaly:      72
8219  deg
Mean motion:   15
54768079  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1643
Checksum:              322


Coasting Arc #14 (Orbit 1657)
---------------------------------------

Vector Time (GMT): 2015/351/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1097748
35                 A    =         6781117
06  meter
 Y    =        5472556
15  meter          E    =           
0004874
 Z    =       -3853059
98                 I    =           51
29906
 XDOT =      -5152
803644                 Wp   =          338
26326
 YDOT =      -3924
399606  meter/sec      RA   =          247
76478  deg
 ZDOT =      -4099
714214                 TA   =          248
45110
                                          MA   =          248
50305
                                          Ha   =            218
904  n
mi
                                          Hp   =            216
665

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3601536
58                 X    =        -1140145
60
 Y    =       17954580
53  feet           Y    =         5460043
50  meter
 Z    =      -12641272
91                 Z    =        -3858495
36
 XDOT =     -16905
523766                 XDOT =       -5088
622300
 YDOT =     -12875
326792  feet/sec       YDOT =       -3981
662636  meter/sec
 ZDOT =     -13450
505950                 ZDOT =       -4124
589681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16831859
64                 X    =        -5130350
82
 Y    =        7169819
64  feet           Y    =         2185361
03  meter
 Z    =      -12665780
51                 Z    =        -3860529
90
 XDOT =       1731
375081                 XDOT =         527
723125
 YDOT =     -19920
323671  feet/sec       YDOT =       -6071
714655  meter/sec
 ZDOT =     -13557
291391                 ZDOT =       -4132
262416


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   15351
63245390  
00016717  00000-0  10270-3 0  9138
2 25544  51
6419 248
5713 0008428 290
0898  69
9348 15
54779526 16586


Satellite: ISS
Catalog Number: 25544
Epoch time:      15351
63245390   =   yrday
fracday
Element set:     913
Inclination:       51
6419  deg
RA of node:       248
5713  deg
Eccentricity:     
0008428     
Arg of perigee:   290
0898  deg
Mean anomaly:      69
9348  deg
Mean motion:   15
54779526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1658
Checksum:              348


Coasting Arc #15 (Orbit 1673)
---------------------------------------

Vector Time (GMT): 2015/352/14:36:25
397
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2316272
52                 A    =         6777174
68  meter
 Y    =       -4072872
27  meter          E    =           
0001905
 Z    =        4898261
62                 I    =           51
29891
 XDOT =       4861
371498                 Wp   =          269
34762
 YDOT =       5482
050395  meter/sec      RA   =          242
74257  deg
 ZDOT =       2260
202786                 TA   =          158
46483
                                          MA   =          158
45681
                                          Ha   =            219
023  n
mi
                                          Hp   =            216
450

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7599319
31                 X    =         2337850
36
 Y    =      -13362441
83  feet           Y    =        -4046849
69  meter
 Z    =       16070412
12                 Z    =         4909565
87
 XDOT =      15949
381555                 XDOT =        4788
729363
 YDOT =      17985
729643  feet/sec       YDOT =        5536
007224  meter/sec
 ZDOT =       7415
363470                 ZDOT =        2283
642072

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15240177
36                 X    =         4645206
06
 Y    =       -1563508
18  feet           Y    =         -476557
29  meter
 Z    =       16120021
33                 Z    =         4913382
50
 XDOT =      -5664
760619                 XDOT =       -1726
619037
 YDOT =      22245
911198  feet/sec       YDOT =        6780
553733  meter/sec
 ZDOT =       7515
669014                 ZDOT =        2290
775915


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   15352
66084143  
00016717  00000-0  10270-3 0  9140
2 25544  51
6420 243
4382 0008298 294
7871  65
2418 15
54784848 16749


Satellite: ISS
Catalog Number: 25544
Epoch time:      15352
66084143   =   yrday
fracday
Element set:     914
Inclination:       51
6420  deg
RA of node:       243
4382  deg
Eccentricity:     
0008298     
Arg of perigee:   294
7871  deg
Mean anomaly:      65
2418  deg
Mean motion:   15
54784848  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1674
Checksum:              333
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