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

 
Date: December 16th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16059 75 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


There are no maneuvers



Coasting Arc #1 (Orbit 1640)
---------------------------------------

Vector Time (GMT): 2015/350/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3153804
25                 A    =         6786076
88  meter
 Y    =        5758869
79  meter          E    =           
0006044
 Z    =        1700985
31                 I    =           51
30559
 XDOT =      -3636
909098                 Wp   =          127
76929
 YDOT =       3668
516377  meter/sec      RA   =          253
26932  deg
 ZDOT =      -5666
758270                 TA   =           33
48816
                                          MA   =           33
44996
                                          Ha   =            218
603  n
mi
                                          Hp   =            216
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10347126
81                 X    =         3080910
06
 Y    =       18893929
75  feet           Y    =         5793730
04  meter
 Z    =        5580660
46                 Z    =         1716129
06
 XDOT =     -11932
116464                 XDOT =       -3650
134232
 YDOT =      12035
814884  feet/sec       YDOT =        3627
772433  meter/sec
 ZDOT =     -18591
726608                 ZDOT =       -5684
457472

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19653018
46                 X    =        -5990240
03
 Y    =        8779517
72  feet           Y    =         2675997
00  meter
 Z    =        5645026
11                 Z    =         1720603
96
 XDOT =     -10418
629487                 XDOT =       -3175
598268
 YDOT =     -11297
253887  feet/sec       YDOT =       -3443
402985  meter/sec
 ZDOT =     -18668
907746                 ZDOT =       -5690
283081


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
53961724  
00016717  00000-0  10270-3 0  9008
2 25544  51
6429 254
0325 0008142 286
4882  73
5376 15
54815274 16418


Satellite: ISS
Catalog Number: 25544
Epoch time:      15350
53961724   =   yrday
fracday
Element set:     900
Inclination:       51
6429  deg
RA of node:       254
0325  deg
Eccentricity:     
0008142     
Arg of perigee:   286
4882  deg
Mean anomaly:      73
5376  deg
Mean motion:   15
54815274  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1641
Checksum:              310


Coasting Arc #2 (Orbit 1656)
---------------------------------------

Vector Time (GMT): 2015/351/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2341303
64                 A    =         6787215
77  meter
 Y    =       -6358402
71  meter          E    =           
0011487
 Z    =         223553
35                 I    =           51
31994
 XDOT =       4570
498112                 Wp   =            7
62294
 YDOT =      -1471
720005  meter/sec      RA   =          248
27162  deg
 ZDOT =       5983
916483                 TA   =          354
79800
                                          MA   =          354
80992
                                          Ha   =            218
764  n
mi
                                          Hp   =            216
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7681442
38                 X    =        -2271114
34
 Y    =      -20860901
27  feet           Y    =        -6384192
27  meter
 Z    =         733442
75                 Z    =          212350
03
 XDOT =      14995
072547                 XDOT =        4557
548082
 YDOT =      -4828
477708  feet/sec       YDOT =       -1420
682333  meter/sec
 ZDOT =      19632
271926                 ZDOT =        6006
087448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21298411
76                 X    =         6491755
90
 Y    =       -6373890
45  feet           Y    =        -1942761
81  meter
 Z    =         686202
61                 Z    =          209154
56
 XDOT =       3427
857939                 XDOT =        1044
811100
 YDOT =      13587
279296  feet/sec       YDOT =        4141
402729  meter/sec
 ZDOT =      19728
369210                 ZDOT =        6013
206935


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
56797504  
00016717  00000-0  10270-3 0  9016
2 25544  51
6431 248
8996 0008264 291
1098  68
9171 15
54850788 16570


Satellite: ISS
Catalog Number: 25544
Epoch time:      15351
56797504   =   yrday
fracday
Element set:     901
Inclination:       51
6431  deg
RA of node:       248
8996  deg
Eccentricity:     
0008264     
Arg of perigee:   291
1098  deg
Mean anomaly:      68
9171  deg
Mean motion:   15
54850788  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1657
Checksum:              350


Coasting Arc #3 (Orbit 1671)
---------------------------------------

Vector Time (GMT): 2015/352/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1271081
24                 A    =         6785297
65  meter
 Y    =        6313949
61  meter          E    =           
0003720
 Z    =       -2129251
15                 I    =           51
32667
 XDOT =      -5304
399380                 Wp   =          246
96899
 YDOT =       -782
201811  meter/sec      RA   =          243
27422  deg
 ZDOT =      -5479
790569                 TA   =          316
73738
                                          MA   =          316
76659
                                          Ha   =            218
936  n
mi
                                          Hp   =            216
385

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4170214
03                 X    =         1210725
71
 Y    =       20715057
78  feet           Y    =         6327826
28  meter
 Z    =       -6985732
12                 Z    =        -2123222
89
 XDOT =     -17402
885105                 XDOT =       -5268
639669
 YDOT =      -2566
278908  feet/sec       YDOT =        -841
318987  meter/sec
 ZDOT =     -17978
315515                 ZDOT =       -5505
471419

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20883108
10                 X    =        -6365171
35
 Y    =        3278307
33  feet           Y    =          999228
07  meter
 Z    =       -6960837
17                 Z    =        -2121663
17
 XDOT =       3582
500029                 XDOT =        1091
946009
 YDOT =     -15631
458015  feet/sec       YDOT =       -4764
468403  meter/sec
 ZDOT =     -18089
172371                 ZDOT =       -5513
579739


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
53204495  
00016717  00000-0  10270-3 0  9027
2 25544  51
6435 244
0883 0008323 293
4763  66
5514 15
54858197 16721


Satellite: ISS
Catalog Number: 25544
Epoch time:      15352
53204495   =   yrday
fracday
Element set:     902
Inclination:       51
6435  deg
RA of node:       244
0883  deg
Eccentricity:     
0008323     
Arg of perigee:   293
4763  deg
Mean anomaly:      66
5514  deg
Mean motion:   15
54858197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1672
Checksum:              322


Coasting Arc #4 (Orbit 1687)
---------------------------------------

Vector Time (GMT): 2015/353/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          35549
79                 A    =         6781132
63  meter
 Y    =       -5646678
04  meter          E    =           
0005057
 Z    =        3748623
54                 I    =           51
32832
 XDOT =       5735
276042                 Wp   =           57
87473
 YDOT =       2842
941937  meter/sec      RA   =          238
26698  deg
 ZDOT =       4226
479846                 TA   =          347
23005
                                          MA   =          347
24285
                                          Ha   =            219
084  n
mi
                                          Hp   =            216
053

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         116633
17                 X    =           80480
26
 Y    =      -18525846
59  feet           Y    =        -5646029
40  meter
 Z    =       12298633
65                 Z    =         3748905
17
 XDOT =      18816
522446                 XDOT =        5682
528637
 YDOT =       9327
237327  feet/sec       YDOT =        2906
782515  meter/sec
 ZDOT =      13866
403694                 ZDOT =        4254
212703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18516461
81                 X    =         5643817
56
 Y    =         553131
54  feet           Y    =          168594
49  meter
 Z    =       12300880
96                 Z    =         3749308
52
 XDOT =      -9805
544781                 XDOT =       -2988
730049
 YDOT =      17110
340719  feet/sec       YDOT =        5215
231851  meter/sec
 ZDOT =      13985
763199                 ZDOT =        4262
860623


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   15353
56037045  
00016717  00000-0  10270-3 0  9037
2 25544  51
6436 238
9552 0008287 298
8227  61
2093 15
54894772 16880


Satellite: ISS
Catalog Number: 25544
Epoch time:      15353
56037045   =   yrday
fracday
Element set:     903
Inclination:       51
6436  deg
RA of node:       238
9552  deg
Eccentricity:     
0008287     
Arg of perigee:   298
8227  deg
Mean anomaly:      61
2093  deg
Mean motion:   15
54894772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1688
Checksum:              341


Coasting Arc #5 (Orbit 1702)
---------------------------------------

Vector Time (GMT): 2015/354/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1496139
68                 A    =         6776905
03  meter
 Y    =        4491098
27  meter          E    =           
0009023
 Z    =       -4856166
93                 I    =           51
33234
 XDOT =      -5734
006035                 Wp   =           27
40936
 YDOT =      -4492
464904  meter/sec      RA   =          233
24782  deg
 ZDOT =      -2382
049421                 TA   =          219
09977
                                          MA   =          219
16501
                                          Ha   =            219
229  n
mi
                                          Hp   =            215
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4908594
75                 X    =        -1522659
53
 Y    =       14734574
37  feet           Y    =         4474219
38  meter
 Z    =      -15932306
19                 Z    =        -4863499
12
 XDOT =     -18812
355759                 XDOT =       -5671
772883
 YDOT =     -14739
058083  feet/sec       YDOT =       -4556
238277  meter/sec
 ZDOT =      -7815
122771                 ZDOT =       -2409
753243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14681198
54                 X    =        -4474829
31
 Y    =       -4962599
79  feet           Y    =        -1512600
42  meter
 Z    =      -15964816
86                 Z    =        -4866076
18
 XDOT =      14576
309263                 XDOT =        4442
859063
 YDOT =     -17533
778633  feet/sec       YDOT =       -5344
295727  meter/sec
 ZDOT =      -7934
070110                 ZDOT =       -2418
304570


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   15354
52440913  
00016717  00000-0  10270-3 0  9047
2 25544  51
6436 234
1436 0008471 302
0945  57
9385 15
54949516 17030


Satellite: ISS
Catalog Number: 25544
Epoch time:      15354
52440913   =   yrday
fracday
Element set:     904
Inclination:       51
6436  deg
RA of node:       234
1436  deg
Eccentricity:     
0008471     
Arg of perigee:   302
0945  deg
Mean anomaly:      57
9385  deg
Mean motion:   15
54949516  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1703
Checksum:              311


Coasting Arc #6 (Orbit 1718)
---------------------------------------

Vector Time (GMT): 2015/355/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3010180
96                 A    =         6774930
92  meter
 Y    =       -2981703
38  meter          E    =           
0006265
 Z    =        5290276
94                 I    =           51
34597
 XDOT =       5222
144685                 Wp   =          315
33211
 YDOT =       5610
319163  meter/sec      RA   =          228
21940  deg
 ZDOT =        195
187483                 TA   =          132
82610
                                          MA   =          132
77343
                                          Ha   =            219
290  n
mi
                                          Hp   =            215
546

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9875921
79                 X    =         3017601
08
 Y    =       -9782491
39  feet           Y    =        -2948000
38  meter
 Z    =       17356551
66                 Z    =         5304917
73
 XDOT =      17133
020620                 XDOT =        5158
072445
 YDOT =      18406
558935  feet/sec       YDOT =        5668
358374  meter/sec
 ZDOT =        640
378881                 ZDOT =         220
400480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9844918
54                 X    =         3000731
17
 Y    =        9699925
85  feet           Y    =         2956537
40  meter
 Z    =       17420386
68                 Z    =         5309733
86
 XDOT =     -17586
123528                 XDOT =       -5360
250451
 YDOT =      16531
485619  feet/sec       YDOT =        5038
796817  meter/sec
 ZDOT =        748
370606                 ZDOT =         228
103361


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   15355
55270271  
00016717  00000-0  10270-3 0  9050
2 25544  51
6437 229
0109 0008429 305
6259  54
4109 15
54965156 17192


Satellite: ISS
Catalog Number: 25544
Epoch time:      15355
55270271   =   yrday
fracday
Element set:     905
Inclination:       51
6437  deg
RA of node:       229
0109  deg
Eccentricity:     
0008429     
Arg of perigee:   305
6259  deg
Mean anomaly:      54
4109  deg
Mean motion:   15
54965156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1719
Checksum:              316


Coasting Arc #7 (Orbit 1733)
---------------------------------------

Vector Time (GMT): 2015/356/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4391622
25                 A    =         6776139
10  meter
 Y    =        1343174
79  meter          E    =           
0006144
 Z    =       -4986889
07                 I    =           51
37152
 XDOT =      -4158
082228                 Wp   =           70
06688
 YDOT =      -6115
901082  meter/sec      RA   =          223
19089  deg
 ZDOT =       2018
567003                 TA   =          219
60831
                                          MA   =          219
65322
                                          Ha   =            219
423  n
mi
                                          Hp   =            215
190

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14408209
49                 X    =        -4382091
04
 Y    =        4406741
44  feet           Y    =         1294118
46  meter
 Z    =      -16361184
63                 Z    =        -5008199
54
 XDOT =     -13642
002061                 XDOT =       -4099
189159
 YDOT =     -20065
292263  feet/sec       YDOT =       -6162
070374  meter/sec
 ZDOT =       6622
595155                 ZDOT =        1998
510332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4744119
05                 X    =        -1446007
49
 Y    =      -14194282
05  feet           Y    =        -4326417
17  meter
 Z    =      -16453568
75                 Z    =        -5015047
76
 XDOT =      18698
465598                 XDOT =        5699
292314
 YDOT =     -13811
551439  feet/sec       YDOT =       -4209
760879  meter/sec
 ZDOT =       6536
973510                 ZDOT =        1992
469526


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   15356
51671307  
00016717  00000-0  10270-3 0  9063
2 25544  51
6429 224
1985 0008559 309
1462  50
8930 15
54994496 17348


Satellite: ISS
Catalog Number: 25544
Epoch time:      15356
51671307   =   yrday
fracday
Element set:     906
Inclination:       51
6429  deg
RA of node:       224
1985  deg
Eccentricity:     
0008559     
Arg of perigee:   309
1462  deg
Mean anomaly:      50
8930  deg
Mean motion:   15
54994496  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1734
Checksum:              335


Coasting Arc #8 (Orbit 1749)
---------------------------------------

Vector Time (GMT): 2015/357/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5491403
46                 A    =         6779864
54  meter
 Y    =         288890
41  meter          E    =           
0009138
 Z    =        3968188
30                 I    =           51
40837
 XDOT =       2558
228035                 Wp   =           28
45670
 YDOT =       6039
547302  meter/sec      RA   =          218
17337  deg
 ZDOT =      -3968
245143                 TA   =          103
06793
                                          MA   =          102
96590
                                          Ha   =            219
628  n
mi
                                          Hp   =            214
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18016415
56                 X    =         5468488
90
 Y    =         947803
18  feet           Y    =          350170
41  meter
 Z    =       13018990
50                 Z    =         3994808
87
 XDOT =       8393
136599                 XDOT =        2509
778461
 YDOT =      19814
787737  feet/sec       YDOT =        6067
884581  meter/sec
 ZDOT =     -13019
176979                 ZDOT =       -3955
934859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -213428
48                 X    =          -65053
00
 Y    =       17956466
39  feet           Y    =         5473130
96  meter
 Z    =       13134056
39                 Z    =         4003260
39
 XDOT =     -18140
168171                 XDOT =       -5529
123258
 YDOT =       9296
718950  feet/sec       YDOT =        2833
639936  meter/sec
 ZDOT =     -12967
024849                 ZDOT =       -3952
349174


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   15357
54497454  
00016717  00000-0  10270-3 0  9077
2 25544  51
6428 219
0659 0008716 313
2321  46
8104 15
55046889 17504


Satellite: ISS
Catalog Number: 25544
Epoch time:      15357
54497454   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       219
0659  deg
Eccentricity:     
0008716     
Arg of perigee:   313
2321  deg
Mean anomaly:      46
8104  deg
Mean motion:   15
55046889  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1750
Checksum:              325


Coasting Arc #9 (Orbit 1764)
---------------------------------------

Vector Time (GMT): 2015/358/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6105707
71                 A    =         6784238
59  meter
 Y    =       -1714693
97  meter          E    =           
0010219
 Z    =       -2390747
34                 I    =           51
44684
 XDOT =       -559
910705                 Wp   =          349
20224
 YDOT =      -5465
340458  meter/sec      RA   =          213
17011  deg
 ZDOT =       5355
933132                 TA   =          343
98594
                                          MA   =          344
01822
                                          Ha   =            219
742  n
mi
                                          Hp   =            214
825

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20031849
45                 X    =        -6074466
48
 Y    =       -5625636
40  feet           Y    =        -1782797
10  meter
 Z    =       -7843659
25                 Z    =        -2420331
88
 XDOT =      -1836
977379                 XDOT =        -524
771332
 YDOT =     -17930
907014  feet/sec       YDOT =       -5471
405843  meter/sec
 ZDOT =      17571
959093                 ZDOT =        5353
297972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4454808
28                 X    =         1357825
56
 Y    =      -20274582
97  feet           Y    =        -6179692
89  meter
 Z    =       -7971307
06                 Z    =        -2429654
39
 XDOT =      16307
060224                 XDOT =        4970
391956
 YDOT =      -3313
801258  feet/sec       YDOT =       -1010
046624  meter/sec
 ZDOT =      17561
537465                 ZDOT =        5352
756619


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   15358
50895710  
00016717  00000-0  10270-3 0  9082
2 25544  51
6412 214
2529 0008730 316
3188  43
7273 15
55017024 17659


Satellite: ISS
Catalog Number: 25544
Epoch time:      15358
50895710   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       214
2529  deg
Eccentricity:     
0008730     
Arg of perigee:   316
3188  deg
Mean anomaly:      43
7273  deg
Mean motion:   15
55017024  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1765
Checksum:              305


Coasting Arc #10 (Orbit 1780)
---------------------------------------

Vector Time (GMT): 2015/359/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6128004
98                 A    =         6786571
50  meter
 Y    =        2878419
71  meter          E    =           
0004723
 Z    =         448288
56                 I    =           51
48162
 XDOT =      -1672
897101                 Wp   =          110
80526
 YDOT =       4499
880567  meter/sec      RA   =          208
18125  deg
 ZDOT =      -5975
805942                 TA   =           64
35076
                                          MA   =           64
30198
                                          Ha   =            219
960  n
mi
                                          Hp   =            214
554

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20105003
20                 X    =         6093184
73
 Y    =        9443634
21  feet           Y    =         2946752
37  meter
 Z    =        1470762
99                 Z    =          477972
71
 XDOT =      -5488
507550                 XDOT =       -1694
063558
 YDOT =      14763
387686  feet/sec       YDOT =        4481
055433  meter/sec
 ZDOT =     -19605
662539                 ZDOT =       -5983
983402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7903360
49                 X    =        -2408944
28
 Y    =       20749402
77  feet           Y    =         6324417
96  meter
 Z    =        1598656
38                 Z    =          487270
46
 XDOT =     -13610
444495                 XDOT =       -4148
463482
 YDOT =      -3659
354302  feet/sec       YDOT =       -1115
371191  meter/sec
 ZDOT =     -19641
834911                 ZDOT =       -5986
831281


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   15359
53718948  
00016717  00000-0  10270-3 0  9094
2 25544  51
6408 209
1201 0008629 320
3253  39
7268 15
55041489 17818


Satellite: ISS
Catalog Number: 25544
Epoch time:      15359
53718948   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       209
1201  deg
Eccentricity:     
0008629     
Arg of perigee:   320
3253  deg
Mean anomaly:      39
7268  deg
Mean motion:   15
55041489  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1781
Checksum:              326


Coasting Arc #11 (Orbit 1796)
---------------------------------------

Vector Time (GMT): 2015/360/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5467361
65                 A    =         6785562
68  meter
 Y    =       -3687580
60  meter          E    =           
0015215
 Z    =        1554403
85                 I    =           51
50594
 XDOT =       3868
961912                 Wp   =           28
14016
 YDOT =      -3311
243280  meter/sec      RA   =          203
19467  deg
 ZDOT =       5743
251910                 TA   =          348
90473
                                          MA   =          348
93825
                                          Ha   =            220
046  n
mi
                                          Hp   =            214
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17937538
22                 X    =        -5433270
49
 Y    =      -12098361
55  feet           Y    =        -3748529
80  meter
 Z    =        5099750
17                 Z    =         1527927
23
 XDOT =      12693
444593                 XDOT =        3877
803292
 YDOT =     -10863
659056  feet/sec       YDOT =       -3267
929155  meter/sec
 ZDOT =      18842
689993                 ZDOT =        5762
067468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10384517
06                 X    =         3165200
80
 Y    =      -19011474
20  feet           Y    =        -5794697
34  meter
 Z    =        4985853
54                 Z    =         1519688
16
 XDOT =      10591
471247                 XDOT =        3228
280436
 YDOT =      10757
011459  feet/sec       YDOT =        3278
737093  meter/sec
 ZDOT =      18924
677614                 ZDOT =        5768
241737


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   15360
56540446  
00016717  00000-0  10270-3 0  9107
2 25544  51
6396 203
9852 0008685 323
4290  36
6269 15
55089208 17970


Satellite: ISS
Catalog Number: 25544
Epoch time:      15360
56540446   =   yrday
fracday
Element set:     910
Inclination:       51
6396  deg
RA of node:       203
9852  deg
Eccentricity:     
0008685     
Arg of perigee:   323
4290  deg
Mean anomaly:      36
6269  deg
Mean motion:   15
55089208  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1797
Checksum:              331


Coasting Arc #12 (Orbit 1811)
---------------------------------------

Vector Time (GMT): 2015/361/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4173158
95                 A    =         6781838
92  meter
 Y    =        4173595
87  meter          E    =           
0007029
 Z    =       -3348087
25                 I    =           51
52232
 XDOT =      -5746
005269                 Wp   =             
44682
 YDOT =       2005
406820  meter/sec      RA   =          198
20343  deg
 ZDOT =      -4655
318524                 TA   =          218
62381
                                          MA   =          218
67411
                                          Ha   =            220
215  n
mi
                                          Hp   =            214
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13691466
37                 X    =         4142442
11
 Y    =       13692899
85  feet           Y    =         4220091
45  meter
 Z    =      -10984538
23                 Z    =        -3327889
41
 XDOT =     -18851
723322                 XDOT =       -5745
389736
 YDOT =       6579
418702  feet/sec       YDOT =        1941
155055  meter/sec
 ZDOT =     -15273
354739                 ZDOT =       -4683
229383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12101465
14                 X    =        -3688526
58
 Y    =       15179022
54  feet           Y    =         4626566
07  meter
 Z    =      -10897873
82                 Z    =        -3321671
94
 XDOT =      -7486
417033                 XDOT =       -2281
859912
 YDOT =     -17037
286184  feet/sec       YDOT =       -5192
964829  meter/sec
 ZDOT =     -15394
477269                 ZDOT =       -4692
236672


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   15361
52934383  
00016717  00000-0  10270-3 0  9112
2 25544  51
6386 199
1725 0008741 327
6540  32
4077 15
55096643 18121


Satellite: ISS
Catalog Number: 25544
Epoch time:      15361
52934383   =   yrday
fracday
Element set:     911
Inclination:       51
6386  deg
RA of node:       199
1725  deg
Eccentricity:     
0008741     
Arg of perigee:   327
6540  deg
Mean anomaly:      32
4077  deg
Mean motion:   15
55096643  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1812
Checksum:              317


Coasting Arc #13 (Orbit 1827)
---------------------------------------

Vector Time (GMT): 2015/362/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2328252
05                 A    =         6777396
95  meter
 Y    =       -4340450
17  meter          E    =           
0005323
 Z    =        4650569
70                 I    =           51
53809
 XDOT =       7072
978470                 Wp   =           38
38635
 YDOT =       -699
529652  meter/sec      RA   =          193
19871  deg
 ZDOT =       2890
430454                 TA   =           22
86802
                                          MA   =           22
84433
                                          Ha   =            220
418  n
mi
                                          Hp   =            213
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7638622
21                 X    =        -2302133
36
 Y    =      -14240322
09  feet           Y    =        -4366340
52  meter
 Z    =       15257774
61                 Z    =         4639322
83
 XDOT =      23205
309940                 XDOT =        7066
234725
 YDOT =      -2295
044791  feet/sec       YDOT =        -620
472845  meter/sec
 ZDOT =       9483
039547                 ZDOT =        2924
772578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13144342
91                 X    =         4006395
72
 Y    =       -9477418
19  feet           Y    =        -2888717
07  meter
 Z    =       15209858
72                 Z    =         4635964
94
 XDOT =       4515
938860                 XDOT =        1376
458165
 YDOT =      21708
593786  feet/sec       YDOT =        6616
779386  meter/sec
 ZDOT =       9631
781366                 ZDOT =        2935
766960


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   15362
55753098  
00016717  00000-0  10270-3 0  9129
2 25544  51
6386 194
0374 0008795 331
6260  28
4413 15
55089766 18282


Satellite: ISS
Catalog Number: 25544
Epoch time:      15362
55753098   =   yrday
fracday
Element set:     912
Inclination:       51
6386  deg
RA of node:       194
0374  deg
Eccentricity:     
0008795     
Arg of perigee:   331
6260  deg
Mean anomaly:      28
4413  deg
Mean motion:   15
55089766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              335


Coasting Arc #14 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2015/363/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         184936
41                 A    =         6774594
56  meter
 Y    =        4257825
23  meter          E    =           
0014342
 Z    =       -5276534
29                 I    =           51
56000
 XDOT =      -7610
904855                 Wp   =           49
95610
 YDOT =       -538
515795  meter/sec      RA   =          188
18452  deg
 ZDOT =       -693
524450                 TA   =          213
36210
                                          MA   =          213
45256
                                          Ha   =            220
423  n
mi
                                          Hp   =            213
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         606746
74                 X    =          162941
59
 Y    =       13969242
88  feet           Y    =         4259770
60  meter
 Z    =      -17311464
21                 Z    =        -5275689
12
 XDOT =     -24970
160287                 XDOT =       -7600
948560
 YDOT =      -1766
784104  feet/sec       YDOT =        -623
570258  meter/sec
 ZDOT =      -2275
342685                 ZDOT =        -730
471943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13719498
71                 X    =        -4181703
21
 Y    =        2717415
09  feet           Y    =          828268
12  meter
 Z    =      -17308543
90                 Z    =        -5275644
18
 XDOT =      -1639
271531                 XDOT =        -499
649963
 YDOT =     -23949
537151  feet/sec       YDOT =       -7299
818924  meter/sec
 ZDOT =      -2435
165209                 ZDOT =        -742
238356


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   15363
52144060  
00016717  00000-0  10270-3 0  9131
2 25544  51
6380 189
2240 0008642 335
3330  24
7409 15
55141193 18438


Satellite: ISS
Catalog Number: 25544
Epoch time:      15363
52144060   =   yrday
fracday
Element set:     913
Inclination:       51
6380  deg
RA of node:       189
2240  deg
Eccentricity:     
0008642     
Arg of perigee:   335
3330  deg
Mean anomaly:      24
7409  deg
Mean motion:   15
55141193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              283


Coasting Arc #15 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2015/364/12:05:54
436
Vector Time (MET): N/A
Weight (LBS)     : 920943
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2064938
61                 A    =         6775251
03  meter
 Y    =       -3942860
05  meter          E    =           
0010918
 Z    =        5110037
73                 I    =           51
59442
 XDOT =       7298
893223                 Wp   =            5
04795
 YDOT =       1697
348407  meter/sec      RA   =          183
16879  deg
 ZDOT =      -1628
873468                 TA   =          100
74053
                                          MA   =          100
61759
                                          Ha   =            220
497  n
mi
                                          Hp   =            213
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6774732
98                 X    =         2084052
93
 Y    =      -12935892
56  feet           Y    =        -3919661
86  meter
 Z    =       16765215
66                 Z    =         5120114
92
 XDOT =      23946
500074                 XDOT =        7287
282915
 YDOT =       5568
728368  feet/sec       YDOT =        1778
904598  meter/sec
 ZDOT =      -5344
073059                 ZDOT =       -1593
445578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13837625
99                 X    =         4217708
40
 Y    =        4501890
77  feet           Y    =         1372176
31  meter
 Z    =       16809517
12                 Z    =         5123540
82
 XDOT =      -1313
858689                 XDOT =        -400
464128
 YDOT =      23554
362674  feet/sec       YDOT =        7179
369743  meter/sec
 ZDOT =      -5191
008614                 ZDOT =       -1582
219426


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   15364
54959678  
00016717  00000-0  10270-3 0  9144
2 25544  51
6383 184
0897 0008654 338
8695  21
2100 15
55137323 18594


Satellite: ISS
Catalog Number: 25544
Epoch time:      15364
54959678   =   yrday
fracday
Element set:     914
Inclination:       51
6383  deg
RA of node:       184
0897  deg
Eccentricity:     
0008654     
Arg of perigee:   338
8695  deg
Mean anomaly:      21
2100  deg
Mean motion:   15
55137323  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              342
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