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

 
Date: December 6th 2014

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 3791)
---------------------------------------

Vector Time (GMT): 2014/339/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1391439
61                 A    =         6787726
77  meter
 Y    =        4933367
10  meter          E    =           
0016087
 Z    =        4437125
53                 I    =           51
45488
 XDOT =      -6859
551861                 Wp   =           81
62173
 YDOT =       1026
557427  meter/sec      RA   =          329
35524  deg
 ZDOT =      -3279
956046                 TA   =           41
57312
                                          MA   =           41
45090
                                          Ha   =            227
321  n
mi
                                          Hp   =            215
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4565090
57                 X    =        -1468056
70
 Y    =       16185587
61  feet           Y    =         4917378
40  meter
 Z    =       14557498
46                 Z    =         4430180
29
 XDOT =     -22505
091407                 XDOT =       -6854
588036
 YDOT =       3367
970561  feet/sec       YDOT =         949
877474  meter/sec
 ZDOT =     -10761
010650                 ZDOT =       -3313
267147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16071611
36                 X    =        -4898627
14
 Y    =       -5040502
31  feet           Y    =        -1536345
10  meter
 Z    =       14526895
89                 Z    =         4427797
87
 XDOT =      -3200
087224                 XDOT =        -975
386586
 YDOT =     -21338
440182  feet/sec       YDOT =       -6503
956568  meter/sec
 ZDOT =     -10903
227304                 ZDOT =       -3323
303682


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   14339
58461381  
00016717  00000-0  10270-3 0  9003
2 25544  51
6433 329
7510 0007310  97
8404 262
3577 15
51823685 37921


Satellite: ISS
Catalog Number: 25544
Epoch time:      14339
58461381   =   yrday
fracday
Element set:     900
Inclination:       51
6433  deg
RA of node:       329
7510  deg
Eccentricity:     
0007310     
Arg of perigee:    97
8404  deg
Mean anomaly:     262
3577  deg
Mean motion:   15
51823685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3792
Checksum:              318


Coasting Arc #2 (Orbit 3806)
---------------------------------------

Vector Time (GMT): 2014/340/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1995720
18                 A    =         6789746
15  meter
 Y    =       -5222721
43  meter          E    =           
0013640
 Z    =       -3866360
11                 I    =           51
43547
 XDOT =       6430
380856                 Wp   =          102
31902
 YDOT =       -577
824080  meter/sec      RA   =          324
37192  deg
 ZDOT =       4109
202253                 TA   =          211
01024
                                          MA   =          211
09083
                                          Ha   =            227
309  n
mi
                                          Hp   =            215
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6547638
39                 X    =         2072755
29
 Y    =      -17134912
83  feet           Y    =        -5199972
92  meter
 Z    =      -12684908
49                 Z    =        -3856478
42
 XDOT =      21097
050051                 XDOT =        6416
402882
 YDOT =      -1895
748294  feet/sec       YDOT =        -505
993912  meter/sec
 ZDOT =      13481
634689                 ZDOT =        4140
406500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17092108
46                 X    =         5209674
66
 Y    =        6740192
04  feet           Y    =         2054410
53  meter
 Z    =      -12641730
48                 Z    =        -3853199
45
 XDOT =       2247
753618                 XDOT =         685
115303
 YDOT =      19777
115815  feet/sec       YDOT =        6028
064901  meter/sec
 ZDOT =      13614
779499                 ZDOT =        4149
784791


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   14340
55056934  
00016717  00000-0  10270-3 0  9017
2 25544  51
6436 324
9522 0007401 101
0620 259
1364 15
51832581 38073


Satellite: ISS
Catalog Number: 25544
Epoch time:      14340
55056934   =   yrday
fracday
Element set:     901
Inclination:       51
6436  deg
RA of node:       324
9522  deg
Eccentricity:     
0007401     
Arg of perigee:   101
0620  deg
Mean anomaly:     259
1364  deg
Mean motion:   15
51832581  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3807
Checksum:              284


Coasting Arc #3 (Orbit 3822)
---------------------------------------

Vector Time (GMT): 2014/341/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2551644
88                 A    =         6791773
83  meter
 Y    =        5458797
20  meter          E    =           
0020244
 Z    =        3112614
18                 I    =           51
41819
 XDOT =      -5944
382387                 Wp   =           98
31723
 YDOT =           
467262  meter/sec      RA   =          319
38942  deg
 ZDOT =      -4849
680522                 TA   =           45
73180
                                          MA   =           45
56585
                                          Ha   =            227
184  n
mi
                                          Hp   =            215
565

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8371538
33                 X    =        -2627616
98
 Y    =       17909439
64  feet           Y    =         5429837
97  meter
 Z    =       10211988
79                 Z    =         3100034
54
 XDOT =     -19502
566888                 XDOT =       -5920
387441
 YDOT =          1
533012  feet/sec       YDOT =         -65
872050  meter/sec
 ZDOT =     -15911
025335                 ZDOT =       -4878
499438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17998987
30                 X    =        -5486091
33
 Y    =       -8245109
63  feet           Y    =        -2513109
42  meter
 Z    =       10157264
43                 Z    =         3095934
20
 XDOT =       -807
431112                 XDOT =        -246
105003
 YDOT =     -18088
081131  feet/sec       YDOT =       -5513
247129  meter/sec
 ZDOT =     -16033
886493                 ZDOT =       -4887
128603


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   14341
58089718  
00016717  00000-0  10270-3 0  9028
2 25544  51
6439 319
8327 0007322 104
6830 255
5133 15
51895553 38236


Satellite: ISS
Catalog Number: 25544
Epoch time:      14341
58089718   =   yrday
fracday
Element set:     902
Inclination:       51
6439  deg
RA of node:       319
8327  deg
Eccentricity:     
0007322     
Arg of perigee:   104
6830  deg
Mean anomaly:     255
5133  deg
Mean motion:   15
51895553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              318


Coasting Arc #4 (Orbit 3837)
---------------------------------------

Vector Time (GMT): 2014/342/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2977633
00                 A    =         6793554
51  meter
 Y    =       -5660113
27  meter          E    =           
0011299
 Z    =       -2297149
46                 I    =           51
40151
 XDOT =       5391
008691                 Wp   =           79
83027
 YDOT =        655
017631  meter/sec      RA   =          314
40893  deg
 ZDOT =       5398
716727                 TA   =          254
54174
                                          MA   =          254
66656
                                          Ha   =            227
138  n
mi
                                          Hp   =            215
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9769137
14                 X    =         3051863
26
 Y    =      -18569925
44  feet           Y    =        -5626400
19  meter
 Z    =       -7536579
59                 Z    =        -2282504
71
 XDOT =      17687
036387                 XDOT =        5357
058127
 YDOT =       2149
007977  feet/sec       YDOT =         715
113048  meter/sec
 ZDOT =      17712
325220                 ZDOT =        5424
823191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18836549
52                 X    =         5741380
29
 Y    =        9296055
15  feet           Y    =         2833437
61  meter
 Z    =       -7473015
71                 Z    =        -2277775
19
 XDOT =       -982
950070                 XDOT =        -299
603181
 YDOT =      16254
255231  feet/sec       YDOT =        4954
296995  meter/sec
 ZDOT =      17823
493661                 ZDOT =        5432
600868


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   14342
54680658  
00016717  00000-0  10270-3 0  9036
2 25544  51
6442 315
0340 0007387 108
3116 251
8839 15
51920781 38382


Satellite: ISS
Catalog Number: 25544
Epoch time:      14342
54680658   =   yrday
fracday
Element set:     903
Inclination:       51
6442  deg
RA of node:       315
0340  deg
Eccentricity:     
0007387     
Arg of perigee:   108
3116  deg
Mean anomaly:     251
8839  deg
Mean motion:   15
51920781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3838
Checksum:              312


Coasting Arc #5 (Orbit 3853)
---------------------------------------

Vector Time (GMT): 2014/343/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3347856
51                 A    =         6794916
37  meter
 Y    =        5749190
45  meter          E    =           
0021053
 Z    =        1334081
76                 I    =           51
38601
 XDOT =      -4809
882865                 Wp   =          117
25229
 YDOT =      -1441
339796  meter/sec      RA   =          309
42907  deg
 ZDOT =      -5797
792772                 TA   =           48
17401
                                          MA   =           47
99443
                                          Ha   =            227
013  n
mi
                                          Hp   =            215
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10983781
22                 X    =        -3418377
03
 Y    =       18862173
39  feet           Y    =         5711358
13  meter
 Z    =        4376908
67                 Z    =         1317647
54
 XDOT =     -15780
455595                 XDOT =       -4765
244152
 YDOT =      -4728
805105  feet/sec       YDOT =       -1494
876939  meter/sec
 ZDOT =     -19021
629829                 ZDOT =       -5821
050225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19339103
96                 X    =        -5894558
89
 Y    =      -10150976
78  feet           Y    =        -3094017
72  meter
 Z    =        4305704
67                 Z    =         1312378
78
 XDOT =       3280
633969                 XDOT =         999
937234
 YDOT =     -14446
820131  feet/sec       YDOT =       -4403
390776  meter/sec
 ZDOT =     -19120
498780                 ZDOT =       -5827
928028


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   14343
57708567  
00016717  00000-0  10270-3 0  9041
2 25544  51
6451 309
9145 0007331 112
1534 248
0396 15
51960543 38547


Satellite: ISS
Catalog Number: 25544
Epoch time:      14343
57708567   =   yrday
fracday
Element set:     904
Inclination:       51
6451  deg
RA of node:       309
9145  deg
Eccentricity:     
0007331     
Arg of perigee:   112
1534  deg
Mean anomaly:     248
0396  deg
Mean motion:   15
51960543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3854
Checksum:              312


Coasting Arc #6 (Orbit 3868)
---------------------------------------

Vector Time (GMT): 2014/344/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3587085
97                 A    =         6795445
44  meter
 Y    =       -5756107
53  meter          E    =           
0015188
 Z    =        -373076
32                 I    =           51
36891
 XDOT =       4233
584247                 Wp   =           69
93432
 YDOT =       2264
455407  meter/sec      RA   =          304
44986  deg
 ZDOT =       5971
224379                 TA   =          286
03394
                                          MA   =          286
20116
                                          Ha   =            226
922  n
mi
                                          Hp   =            215
496

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11768654
77                 X    =         3652997
79
 Y    =      -18884867
23  feet           Y    =        -5715625
85  meter
 Z    =       -1224003
69                 Z    =         -355491
11
 XDOT =      13889
712095                 XDOT =        4178
941676
 YDOT =       7429
315640  feet/sec       YDOT =        2311
492136  meter/sec
 ZDOT =      19590
631165                 ZDOT =        5991
657953

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19580785
54                 X    =         5968223
43
 Y    =       10578884
38  feet           Y    =         3224443
96  meter
 Z    =       -1147899
53                 Z    =         -349879
78
 XDOT =      -5789
214600                 XDOT =       -1764
552610
 YDOT =      12773
324046  feet/sec       YDOT =        3893
309169  meter/sec
 ZDOT =      19677
302566                 ZDOT =        5997
641822


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   14344
54294860  
00016717  00000-0  10270-3 0  9056
2 25544  51
6450 305
1158 0007323 115
9975 244
1932 15
52007210 38692


Satellite: ISS
Catalog Number: 25544
Epoch time:      14344
54294860   =   yrday
fracday
Element set:     905
Inclination:       51
6450  deg
RA of node:       305
1158  deg
Eccentricity:     
0007323     
Arg of perigee:   115
9975  deg
Mean anomaly:     244
1932  deg
Mean motion:   15
52007210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3869
Checksum:              302


Coasting Arc #7 (Orbit 3884)
---------------------------------------

Vector Time (GMT): 2014/345/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3783138
60                 A    =         6795212
62  meter
 Y    =        5595977
45  meter          E    =           
0017546
 Z    =        -676133
92                 I    =           51
35237
 XDOT =      -3659
637900                 Wp   =          131
28157
 YDOT =      -3178
228121  meter/sec      RA   =          299
46948  deg
 ZDOT =      -5939
721496                 TA   =           56
04518
                                          MA   =           55
87852
                                          Ha   =            226
789  n
mi
                                          Hp   =            215
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12411872
06                 X    =        -3842148
52
 Y    =       18359506
07  feet           Y    =         5553342
04  meter
 Z    =       -2218287
14                 Z    =         -694654
85
 XDOT =     -12006
686024                 XDOT =       -3594
973016
 YDOT =     -10427
257615  feet/sec       YDOT =       -3218
790659  meter/sec
 ZDOT =     -19487
275250                 ZDOT =       -5957
342588

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19285151
97                 X    =        -5878114
32
 Y    =      -10901714
35  feet           Y    =        -3322842
53  meter
 Z    =       -2298340
00                 Z    =         -700534
03
 XDOT =       8658
263594                 XDOT =        2639
038744
 YDOT =     -11267
110973  feet/sec       YDOT =       -3434
215425  meter/sec
 ZDOT =     -19561
782498                 ZDOT =       -5962
431305


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   14345
57317828  
00016717  00000-0  10270-3 0  9061
2 25544  51
6459 299
9961 0007283 119
6848 240
5029 15
52035276 38856


Satellite: ISS
Catalog Number: 25544
Epoch time:      14345
57317828   =   yrday
fracday
Element set:     906
Inclination:       51
6459  deg
RA of node:       299
9961  deg
Eccentricity:     
0007283     
Arg of perigee:   119
6848  deg
Mean anomaly:     240
5029  deg
Mean motion:   15
52035276  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3885
Checksum:              351


Coasting Arc #8 (Orbit 3900)
---------------------------------------

Vector Time (GMT): 2014/346/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3875042
52                 A    =         6794118
26  meter
 Y    =       -5324675
96  meter          E    =           
0018705
 Z    =        1648999
20                 I    =           51
33409
 XDOT =       3146
385360                 Wp   =           83
30805
 YDOT =       4066
998161  meter/sec      RA   =          294
48707  deg
 ZDOT =       5685
138713                 TA   =          294
81699
                                          MA   =          295
01142
                                          Ha   =            226
702  n
mi
                                          Hp   =            215
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12713394
10                 X    =         3926285
99
 Y    =      -17469409
31  feet           Y    =        -5281056
27  meter
 Z    =        5410102
37                 Z    =         1667947
81
 XDOT =      10322
786615                 XDOT =        3073
056852
 YDOT =      13343
169818  feet/sec       YDOT =        4101
772818  meter/sec
 ZDOT =      18652
029899                 ZDOT =        5700
245468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18610733
58                 X    =         5672551
60
 Y    =       10934317
83  feet           Y    =         3332780
07  meter
 Z    =        5491916
61                 Z    =         1673936
18
 XDOT =     -11500
676248                 XDOT =       -3505
406121
 YDOT =      10087
595266  feet/sec       YDOT =        3074
699037  meter/sec
 ZDOT =      18715
651907                 ZDOT =        5704
530701


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   14346
60338225  
00016717  00000-0  10270-3 0  9071
2 25544  51
6455 294
8770 0007264 123
5111 236
6736 15
52077214 39018


Satellite: ISS
Catalog Number: 25544
Epoch time:      14346
60338225   =   yrday
fracday
Element set:     907
Inclination:       51
6455  deg
RA of node:       294
8770  deg
Eccentricity:     
0007264     
Arg of perigee:   123
5111  deg
Mean anomaly:     236
6736  deg
Mean motion:   15
52077214  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3901
Checksum:              303


Coasting Arc #9 (Orbit 3915)
---------------------------------------

Vector Time (GMT): 2014/347/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3953763
52                 A    =         6792182
80  meter
 Y    =        4854699
60  meter          E    =           
0012231
 Z    =       -2630735
03                 I    =           51
31656
 XDOT =      -2655
197132                 Wp   =          126
10614
 YDOT =      -4965
120690  meter/sec      RA   =          289
50079  deg
 ZDOT =      -5196
034489                 TA   =           83
64546
                                          MA   =           83
50618
                                          Ha   =            226
560  n
mi
                                          Hp   =            215
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12971665
08                 X    =        -3994976
78
 Y    =       15927492
12  feet           Y    =         4810255
71  meter
 Z    =       -8631020
44                 Z    =        -2650041
78
 XDOT =      -8711
276681                 XDOT =       -2574
237986
 YDOT =     -16289
766042  feet/sec       YDOT =       -4994
359965  meter/sec
 ZDOT =     -17047
357246                 ZDOT =       -5208
736605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17290859
93                 X    =        -5270254
11
 Y    =      -11024128
26  feet           Y    =        -3360154
29  meter
 Z    =       -8714262
64                 Z    =        -2656107
25
 XDOT =      14404
719256                 XDOT =        4390
558429
 YDOT =      -9137
404614  feet/sec       YDOT =       -2785
080926  meter/sec
 ZDOT =     -17100
562716                 ZDOT =       -5212
251516


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   14347
56917533  
00016717  00000-0  10270-3 0  9083
2 25544  51
6461 290
0770 0007259 126
7994 233
3825 15
52120825 39167


Satellite: ISS
Catalog Number: 25544
Epoch time:      14347
56917533   =   yrday
fracday
Element set:     908
Inclination:       51
6461  deg
RA of node:       290
0770  deg
Eccentricity:     
0007259     
Arg of perigee:   126
7994  deg
Mean anomaly:     233
3825  deg
Mean motion:   15
52120825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3916
Checksum:              324


Coasting Arc #10 (Orbit 3931)
---------------------------------------

Vector Time (GMT): 2014/348/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3971855
12                 A    =         6789947
20  meter
 Y    =       -4273562
14  meter          E    =           
0018468
 Z    =        3462911
30                 I    =           51
29930
 XDOT =       2247
144426                 Wp   =          105
67200
 YDOT =       5771
770439  meter/sec      RA   =          284
51053  deg
 ZDOT =       4520
416653                 TA   =          295
17298
                                          MA   =          295
36440
                                          Ha   =            226
477  n
mi
                                          Hp   =            215
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13031020
73                 X    =         4002526
15
 Y    =      -14020873
15  feet           Y    =        -4228974
89  meter
 Z    =       11361257
55                 Z    =         3482280
42
 XDOT =       7372
521083                 XDOT =        2160
477350
 YDOT =      18936
254721  feet/sec       YDOT =        5796
414738  meter/sec
 ZDOT =      14830
763297                 ZDOT =        4531
122664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15592912
13                 X    =         4752719
62
 Y    =       11015974
14  feet           Y    =         3357668
92  meter
 Z    =       11444647
80                 Z    =         3488328
65
 XDOT =     -17020
891962                 XDOT =       -5187
967870
 YDOT =       8553
698005  feet/sec       YDOT =        2607
167152  meter/sec
 ZDOT =      14875
313851                 ZDOT =        4533
995662


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   14348
59933055  
00016717  00000-0  10270-3 0  9095
2 25544  51
6457 284
9574 0007283 130
8128 229
3656 15
52147931 39320


Satellite: ISS
Catalog Number: 25544
Epoch time:      14348
59933055   =   yrday
fracday
Element set:     909
Inclination:       51
6457  deg
RA of node:       284
9574  deg
Eccentricity:     
0007283     
Arg of perigee:   130
8128  deg
Mean anomaly:     229
3656  deg
Mean motion:   15
52147931  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3932
Checksum:              339


Coasting Arc #11 (Orbit 3946)
---------------------------------------

Vector Time (GMT): 2014/349/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4013843
81                 A    =         6787333
08  meter
 Y    =        3501426
67  meter          E    =           
0013030
 Z    =       -4216447
75                 I    =           51
28482
 XDOT =      -1859
653440                 Wp   =           99
92899
 YDOT =      -6482
695783  meter/sec      RA   =          279
51460  deg
 ZDOT =      -3624
880524                 TA   =          132
77035
                                          MA   =          132
66067
                                          Ha   =            226
347  n
mi
                                          Hp   =            215
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13168778
91                 X    =        -4032217
02
 Y    =       11487620
29  feet           Y    =         3456438
66  meter
 Z    =      -13833489
98                 Z    =        -4235991
04
 XDOT =      -6101
225198                 XDOT =       -1769
415624
 YDOT =     -21268
686952  feet/sec       YDOT =       -6502
986973  meter/sec
 ZDOT =     -11892
652637                 ZDOT =       -3633
695518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13292440
06                 X    =        -4051535
73
 Y    =      -11241112
68  feet           Y    =        -3426291
14  meter
 Z    =      -13917471
97                 Z    =        -4242045
46
 XDOT =      19326
752511                 XDOT =        5890
794165
 YDOT =      -8132
106876  feet/sec       YDOT =       -2478
666176  meter/sec
 ZDOT =     -11929
016062                 ZDOT =       -3635
964096


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   14349
56507769  
00016717  00000-0  10270-3 0  9104
2 25544  51
6464 280
1569 0007259 134
0706 226
1044 15
52202241 39479


Satellite: ISS
Catalog Number: 25544
Epoch time:      14349
56507769   =   yrday
fracday
Element set:     910
Inclination:       51
6464  deg
RA of node:       280
1569  deg
Eccentricity:     
0007259     
Arg of perigee:   134
0706  deg
Mean anomaly:     226
1044  deg
Mean motion:   15
52202241  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3947
Checksum:              307


Coasting Arc #12 (Orbit 3962)
---------------------------------------

Vector Time (GMT): 2014/350/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4037897
29                 A    =         6785139
57  meter
 Y    =       -2649924
65  meter          E    =           
0014506
 Z    =        4759549
92                 I    =           51
27318
 XDOT =       1538
511567                 Wp   =          128
40905
 YDOT =       7047
730321  meter/sec      RA   =          274
51474  deg
 ZDOT =       2604
379910                 TA   =          295
71296
                                          MA   =          295
86265
                                          Ha   =            226
187  n
mi
                                          Hp   =            215
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13247694
52                 X    =         4044108
74
 Y    =       -8693978
52  feet           Y    =        -2604735
71  meter
 Z    =       15615321
27                 Z    =         4779180
58
 XDOT =       5047
610129                 XDOT =        1446
936529
 YDOT =      23122
474808  feet/sec       YDOT =        7064
422836  meter/sec
 ZDOT =       8544
553509                 ZDOT =        2611
631658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10739319
21                 X    =         3273344
50
 Y    =       11537643
91  feet           Y    =         3516673
86  meter
 Z    =       15699513
59                 Z    =         4785211
74
 XDOT =     -21143
797697                 XDOT =       -6444
629538
 YDOT =       7950
389978  feet/sec       YDOT =        2423
278865  meter/sec
 ZDOT =       8574
155467                 ZDOT =        2613
402586


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   14350
59518398  
00016717  00000-0  10270-3 0  9110
2 25544  51
6461 275
0367 0007275 138
7210 221
4493 15
52234022 39630


Satellite: ISS
Catalog Number: 25544
Epoch time:      14350
59518398   =   yrday
fracday
Element set:     911
Inclination:       51
6461  deg
RA of node:       275
0367  deg
Eccentricity:     
0007275     
Arg of perigee:   138
7210  deg
Mean anomaly:     221
4493  deg
Mean motion:   15
52234022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3963
Checksum:              304


Coasting Arc #13 (Orbit 3977)
---------------------------------------

Vector Time (GMT): 2014/351/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4114031
81                 A    =         6783434
25  meter
 Y    =        1660225
06  meter          E    =           
0018276
 Z    =       -5146627
61                 I    =           51
26714
 XDOT =      -1211
973225                 Wp   =           99
59526
 YDOT =      -7419
235495  meter/sec      RA   =          269
51017  deg
 ZDOT =      -1431
880818                 TA   =          156
56823
                                          MA   =          156
48484
                                          Ha   =            226
120  n
mi
                                          Hp   =            215
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13497479
69                 X    =        -4107290
20
 Y    =        5446932
62  feet           Y    =         1614257
24  meter
 Z    =      -16885261
18                 Z    =        -5166596
71
 XDOT =      -3976
290108                 XDOT =       -1121
963849
 YDOT =     -24341
323803  feet/sec       YDOT =       -7432
285224  meter/sec
 ZDOT =      -4697
771711                 ZDOT =       -1437
550197

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7786949
95                 X    =        -2373462
35
 Y    =      -12178727
81  feet           Y    =        -3712076
24  meter
 Z    =      -16970712
34                 Z    =        -5172673
12
 XDOT =      22331
964580                 XDOT =        6806
782804
 YDOT =      -7734
301713  feet/sec       YDOT =       -2357
415162  meter/sec
 ZDOT =      -4720
566828                 ZDOT =       -1438
828769


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   14351
56088663  
00016717  00000-0  10270-3 0  9126
2 25544  51
6469 270
2359 0007220 141
7381 218
4285 15
52277138 39785


Satellite: ISS
Catalog Number: 25544
Epoch time:      14351
56088663   =   yrday
fracday
Element set:     912
Inclination:       51
6469  deg
RA of node:       270
2359  deg
Eccentricity:     
0007220     
Arg of perigee:   141
7381  deg
Mean anomaly:     218
4285  deg
Mean motion:   15
52277138  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3978
Checksum:              325


Coasting Arc #14 (Orbit 3993)
---------------------------------------

Vector Time (GMT): 2014/352/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4195737
16                 A    =         6782604
09  meter
 Y    =        -648620
69  meter          E    =           
0009043
 Z    =        5284162
73                 I    =           51
26595
 XDOT =        902
854945                 Wp   =          135
25943
 YDOT =       7614
490041  meter/sec      RA   =          264
50418  deg
 ZDOT =        211
240548                 TA   =          312
67937
                                          MA   =          312
75551
                                          Ha   =            225
832  n
mi
                                          Hp   =            215
755

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13765541
87                 X    =         4177009
37
 Y    =       -2128020
63  feet           Y    =         -601806
30  meter
 Z    =       17336491
88                 Z    =         5304499
67
 XDOT =       2962
122523                 XDOT =         816
614689
 YDOT =      24981
922706  feet/sec       YDOT =        7624
104139  meter/sec
 ZDOT =        693
046417                 ZDOT =         215
417571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4795037
64                 X    =         1461527
47
 Y    =       12961784
25  feet           Y    =         3950751
84  meter
 Z    =       17423327
14                 Z    =         5310630
11
 XDOT =     -22952
413506                 XDOT =       -6995
895637
 YDOT =       7508
600701  feet/sec       YDOT =        2288
621494  meter/sec
 ZDOT =        709
450759                 ZDOT =         216
240591


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   14352
59094469  
00016717  00000-0  10270-3 0  9132
2 25544  51
6467 265
1155 0007157 146
8411 213
3190 15
52328042 39947


Satellite: ISS
Catalog Number: 25544
Epoch time:      14352
59094469   =   yrday
fracday
Element set:     913
Inclination:       51
6467  deg
RA of node:       265
1155  deg
Eccentricity:     
0007157     
Arg of perigee:   146
8411  deg
Mean anomaly:     213
3190  deg
Mean motion:   15
52328042  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3994
Checksum:              313


Coasting Arc #15 (Orbit 4008)
---------------------------------------

Vector Time (GMT): 2014/353/13:00:52
258
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4333111
39                 A    =         6782930
19  meter
 Y    =        -412657
17  meter          E    =           
0019512
 Z    =       -5218796
91                 I    =           51
27163
 XDOT =       -547
324600                 Wp   =          114
79092
 YDOT =      -7559
598709  meter/sec      RA   =          259
49700  deg
 ZDOT =       1047
256618                 TA   =          165
34221
                                          MA   =          165
28555
                                          Ha   =            225
863  n
mi
                                          Hp   =            215
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14216244
71                 X    =        -4302823
48
 Y    =       -1353862
10  feet           Y    =         -460943
02  meter
 Z    =      -17122037
11                 Z    =        -5239773
19
 XDOT =      -1795
684383                 XDOT =        -467
837997
 YDOT =     -24801
833034  feet/sec       YDOT =       -7565
274904  meter/sec
 ZDOT =       3435
881294                 ZDOT =        1044
790177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1714464
95                 X    =         -522568
92
 Y    =      -14068643
31  feet           Y    =        -4288122
48  meter
 Z    =      -17211408
90                 Z    =        -5246037
43
 XDOT =      22802
324072                 XDOT =        6950
148377
 YDOT =      -6990
715954  feet/sec       YDOT =       -2130
770223  meter/sec
 ZDOT =       3426
752625                 ZDOT =        1044
474200


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   14353
55660408  
00016717  00000-0  10270-3 0  9142
2 25544  51
6473 260
3147 0007118 149
9152 210
2410 15
52341903 40095


Satellite: ISS
Catalog Number: 25544
Epoch time:      14353
55660408   =   yrday
fracday
Element set:     914
Inclination:       51
6473  deg
RA of node:       260
3147  deg
Eccentricity:     
0007118     
Arg of perigee:   149
9152  deg
Mean anomaly:     210
2410  deg
Mean motion:   15
52341903  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4009
Checksum:              281
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