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

 
Date: December 21st 2013

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 36963 27 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 2361)
---------------------------------------

Vector Time (GMT): 2013/354/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1682067
68                 A    =         6800924
73  meter
 Y    =       -6469326
44  meter          E    =           
0009278
 Z    =       -1220568
33                 I    =           51
31306
 XDOT =       4445
151949                 Wp   =            5
41759
 YDOT =      -2251
617578  meter/sec      RA   =          263
83342  deg
 ZDOT =       5820
971688                 TA   =          341
27802
                                          MA   =          341
31212
                                          Ha   =            226
265  n
mi
                                          Hp   =            223
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5518594
77                 X    =        -1603672
08
 Y    =      -21224824
28  feet           Y    =        -6487697
96  meter
 Z    =       -4004489
27                 Z    =        -1228549
72
 XDOT =      14583
831854                 XDOT =        4441
723187
 YDOT =      -7387
196779  feet/sec       YDOT =       -2201
928712  meter/sec
 ZDOT =      19097
676141                 ZDOT =        5842
557149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13937640
50                 X    =         4248192
82
 Y    =      -16924201
96  feet           Y    =        -5158496
76  meter
 Z    =       -4037022
86                 Z    =        -1230484
57
 XDOT =      13245
060540                 XDOT =        4037
094453
 YDOT =       6340
378615  feet/sec       YDOT =        1932
547402  meter/sec
 ZDOT =      19188
840468                 ZDOT =        5848
758575


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   13354
60656022  
00016717  00000-0  10270-3 0  9000
2 25544  51
6510 264
6792 0005152 293
8748  66
1863 15
49928756 23629


Satellite: ISS
Catalog Number: 25544
Epoch time:      13354
60656022   =   yrday
fracday
Element set:     900
Inclination:       51
6510  deg
RA of node:       264
6792  deg
Eccentricity:     
0005152     
Arg of perigee:   293
8748  deg
Mean anomaly:      66
1863  deg
Mean motion:   15
49928756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2362
Checksum:              323


Coasting Arc #2 (Orbit 2377)
---------------------------------------

Vector Time (GMT): 2013/355/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1996759
21                 A    =         6801215
95  meter
 Y    =        6435052
45  meter          E    =           
0008477
 Z    =         893965
47                 I    =           51
31777
 XDOT =      -4379
844743                 Wp   =          130
68015
 YDOT =       2182
208064  meter/sec      RA   =          258
85921  deg
 ZDOT =      -5893
964084                 TA   =           39
61978
                                          MA   =           39
55786
                                          Ha   =            226
407  n
mi
                                          Hp   =            222
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6551047
27                 X    =         1920310
02
 Y    =       21112376
81  feet           Y    =         6456953
97  meter
 Z    =        2932957
57                 Z    =          903480
21
 XDOT =     -14369
569367                 XDOT =       -4375
290130
 YDOT =       7159
475277  feet/sec       YDOT =        2133
255720  meter/sec
 ZDOT =     -19337
152506                 ZDOT =       -5915
229577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12929202
51                 X    =        -3940820
93
 Y    =       17923562
11  feet           Y    =         5463101
73  meter
 Z    =        2971962
05                 Z    =          905854
03
 XDOT =     -12984
861240                 XDOT =       -3957
785706
 YDOT =      -6128
522061  feet/sec       YDOT =       -1867
973524  meter/sec
 ZDOT =     -19426
961039                 ZDOT =       -5921
337725


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   13355
63817798  
00016717  00000-0  10270-3 0  9014
2 25544  51
6505 259
5698 0005042 296
2689  63
7943 15
49929478 23781


Satellite: ISS
Catalog Number: 25544
Epoch time:      13355
63817798   =   yrday
fracday
Element set:     901
Inclination:       51
6505  deg
RA of node:       259
5698  deg
Eccentricity:     
0005042     
Arg of perigee:   296
2689  deg
Mean anomaly:      63
7943  deg
Mean motion:   15
49929478  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2378
Checksum:              369


Coasting Arc #3 (Orbit 2392)
---------------------------------------

Vector Time (GMT): 2013/356/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2312156
58                 A    =         6801200
86  meter
 Y    =       -6363195
57  meter          E    =           
0011137
 Z    =        -568356
54                 I    =           51
32450
 XDOT =       4347
367173                 Wp   =           13
52618
 YDOT =      -2107
948531  meter/sec      RA   =          253
88368  deg
 ZDOT =       5948
731714                 TA   =          340
32255
                                          MA   =          340
36549
                                          Ha   =            226
400  n
mi
                                          Hp   =            222
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7585815
55                 X    =        -2238069
17
 Y    =      -20876625
88  feet           Y    =        -6388637
30  meter
 Z    =       -1864686
81                 Z    =         -579409
09
 XDOT =      14263
015658                 XDOT =        4341
718532
 YDOT =      -6915
841638  feet/sec       YDOT =       -2059
365408  meter/sec
 ZDOT =      19516
836331                 ZDOT =        5969
836820

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11792126
18                 X    =         3594240
06
 Y    =      -18818929
51  feet           Y    =        -5736009
72  meter
 Z    =       -1910187
06                 Z    =         -582225
02
 XDOT =      12780
789160                 XDOT =        3895
584536
 YDOT =       6029
651300  feet/sec       YDOT =        1837
837716  meter/sec
 ZDOT =      19605
959583                 ZDOT =        5975
896481


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   13356
60529269  
00016717  00000-0  10270-3 0  9026
2 25544  51
6496 254
7782 0005250 300
7150  59
3484 15
50004423 23930


Satellite: ISS
Catalog Number: 25544
Epoch time:      13356
60529269   =   yrday
fracday
Element set:     902
Inclination:       51
6496  deg
RA of node:       254
7782  deg
Eccentricity:     
0005250     
Arg of perigee:   300
7150  deg
Mean anomaly:      59
3484  deg
Mean motion:   15
50004423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2393
Checksum:              300


Coasting Arc #4 (Orbit 2408)
---------------------------------------

Vector Time (GMT): 2013/357/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2600596
15                 A    =         6801295
63  meter
 Y    =        6276713
21  meter          E    =           
0007425
 Z    =         209742
06                 I    =           51
33394
 XDOT =      -4351
415556                 Wp   =          138
75487
 YDOT =       2006
466450  meter/sec      RA   =          248
91006  deg
 ZDOT =      -5976
082818                 TA   =           38
98027
                                          MA   =           38
92678
                                          Ha   =            226
535  n
mi
                                          Hp   =            222
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8532139
59                 X    =         2529196
40
 Y    =       20592891
11  feet           Y    =         6305395
51  meter
 Z    =         688130
11                 Z    =          222202
27
 XDOT =     -14276
297755                 XDOT =       -4344
498914
 YDOT =       6582
895176  feet/sec       YDOT =        1957
845078  meter/sec
 ZDOT =     -19606
570925                 ZDOT =       -5997
204569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10646207
58                 X    =        -3244964
07
 Y    =       19581863
51  feet           Y    =         5968552
00  meter
 Z    =         739580
37                 Z    =          225424
10
 XDOT =     -12590
719472                 XDOT =       -3837
651295
 YDOT =      -6088
042463  feet/sec       YDOT =       -1855
635343  meter/sec
 ZDOT =     -19695
749784                 ZDOT =       -6003
264534


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   13357
63685810  
00016717  00000-0  10270-3 0  9036
2 25544  51
6492 249
6682 0005170 303
3446  56
7209 15
50012870 24095


Satellite: ISS
Catalog Number: 25544
Epoch time:      13357
63685810   =   yrday
fracday
Element set:     903
Inclination:       51
6492  deg
RA of node:       249
6682  deg
Eccentricity:     
0005170     
Arg of perigee:   303
3446  deg
Mean anomaly:      56
7209  deg
Mean motion:   15
50012870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2409
Checksum:              305


Coasting Arc #5 (Orbit 2424)
---------------------------------------

Vector Time (GMT): 2013/358/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2879926
68                 A    =         6801122
74  meter
 Y    =       -6150750
04  meter          E    =           
0012576
 Z    =         144441
76                 I    =           51
34496
 XDOT =       4392
184385                 Wp   =           22
37367
 YDOT =      -1912
240472  meter/sec      RA   =          243
93517  deg
 ZDOT =       5983
150827                 TA   =          339
18657
                                          MA   =          339
23774
                                          Ha   =            226
541  n
mi
                                          Hp   =            222
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9448578
34                 X    =        -2811635
24
 Y    =      -20179626
11  feet           Y    =        -6182573
38  meter
 Z    =         473890
29                 Z    =          130617
06
 XDOT =      14410
053758                 XDOT =        4384
176657
 YDOT =      -6273
754830  feet/sec       YDOT =       -1863
169255  meter/sec
 ZDOT =      19629
759932                 ZDOT =        6004
468044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9397740
65                 X    =         2864431
35
 Y    =      -20204612
69  feet           Y    =        -6158365
95  meter
 Z    =         416666
63                 Z    =          126999
99
 XDOT =      12510
157859                 XDOT =        3813
096115
 YDOT =       6237
878681  feet/sec       YDOT =        1901
305422  meter/sec
 ZDOT =      19719
748714                 ZDOT =        6010
579408


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   13358
66839535  
00016717  00000-0  10270-3 0  9046
2 25544  51
6482 244
5563 0005308 307
4672  52
5996 15
50079074 24259


Satellite: ISS
Catalog Number: 25544
Epoch time:      13358
66839535   =   yrday
fracday
Element set:     904
Inclination:       51
6482  deg
RA of node:       244
5563  deg
Eccentricity:     
0005308     
Arg of perigee:   307
4672  deg
Mean anomaly:      52
5996  deg
Mean motion:   15
50079074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2425
Checksum:              329


Coasting Arc #6 (Orbit 2439)
---------------------------------------

Vector Time (GMT): 2013/359/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3125266
05                 A    =         6800947
77  meter
 Y    =        6013707
92  meter          E    =           
0005794
 Z    =        -528860
75                 I    =           51
35874
 XDOT =      -4469
596873                 Wp   =          145
99264
 YDOT =       1802
508745  meter/sec      RA   =          238
96277  deg
 ZDOT =      -5952
773560                 TA   =           39
72371
                                          MA   =           39
68129
                                          Ha   =            226
670  n
mi
                                          Hp   =            222
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10253497
52                 X    =         3060356
21
 Y    =       19730012
87  feet           Y    =         6048293
73  meter
 Z    =       -1735107
45                 Z    =         -513835
97
 XDOT =     -14664
031736                 XDOT =       -4460
503833
 YDOT =       5913
742602  feet/sec       YDOT =        1752
577911  meter/sec
 ZDOT =     -19530
096981                 ZDOT =       -5974
464266

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8176482
20                 X    =        -2492191
77
 Y    =       20682482
69  feet           Y    =         6304020
73  meter
 Z    =       -1672801
74                 Z    =         -509869
97
 XDOT =     -12487
243180                 XDOT =       -3806
111721
 YDOT =      -6513
600030  feet/sec       YDOT =       -1985
345289  meter/sec
 ZDOT =     -19621
643661                 ZDOT =       -5980
676988


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   13359
63543946  
00016717  00000-0  10270-3 0  9053
2 25544  51
6480 239
7653 0005286 310
5903  49
4787 15
50101325 24405


Satellite: ISS
Catalog Number: 25544
Epoch time:      13359
63543946   =   yrday
fracday
Element set:     905
Inclination:       51
6480  deg
RA of node:       239
7653  deg
Eccentricity:     
0005286     
Arg of perigee:   310
5903  deg
Mean anomaly:      49
4787  deg
Mean motion:   15
50101325  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2440
Checksum:              312


Coasting Arc #7 (Orbit 2455)
---------------------------------------

Vector Time (GMT): 2013/360/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3350391
17                 A    =         6800589
52  meter
 Y    =       -5838651
02  meter          E    =           
0013459
 Z    =         904335
69                 I    =           51
37380
 XDOT =       4584
039033                 Wp   =           31
99201
 YDOT =      -1712
035845  meter/sec      RA   =          233
98930  deg
 ZDOT =       5900
380294                 TA   =          337
82074
                                          MA   =          337
87891
                                          Ha   =            226
682  n
mi
                                          Hp   =            222
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10992097
00                 X    =        -3289246
08
 Y    =      -19155679
19  feet           Y    =        -5875775
38  meter
 Z    =        2966980
59                 Z    =          888208
06
 XDOT =      15039
498139                 XDOT =        4574
180240
 YDOT =      -5616
915501  feet/sec       YDOT =       -1660
829559  meter/sec
 ZDOT =      19358
203064                 ZDOT =        5922
625137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6893474
83                 X    =         2101131
13
 Y    =      -20991408
64  feet           Y    =        -6398181
35  meter
 Z    =        2899997
18                 Z    =          883919
14
 XDOT =      12615
730215                 XDOT =        3845
274570
 YDOT =       6843
826206  feet/sec       YDOT =        2085
998227  meter/sec
 ZDOT =      19452
072547                 ZDOT =        5928
991712


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   13360
66692738  
00016717  00000-0  10270-3 0  9063
2 25544  51
6471 234
6529 0005311 313
9875  46
0837 15
50151403 24563


Satellite: ISS
Catalog Number: 25544
Epoch time:      13360
66692738   =   yrday
fracday
Element set:     906
Inclination:       51
6471  deg
RA of node:       234
6529  deg
Eccentricity:     
0005311     
Arg of perigee:   313
9875  deg
Mean anomaly:      46
0837  deg
Mean motion:   15
50151403  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2456
Checksum:              310


Coasting Arc #8 (Orbit 2470)
---------------------------------------

Vector Time (GMT): 2013/361/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3534612
62                 A    =         6800097
48  meter
 Y    =        5658598
86  meter          E    =           
0003608
 Z    =       -1305670
66                 I    =           51
39126
 XDOT =      -4730
185135                 Wp   =          148
56289
 YDOT =       1618
516978  meter/sec      RA   =          229
01860  deg
 ZDOT =      -5801
054017                 TA   =           45
66484
                                          MA   =           45
63528
                                          Ha   =            226
804  n
mi
                                          Hp   =            222
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11596498
08                 X    =         3477416
81
 Y    =       18564956
89  feet           Y    =         5697805
42  meter
 Z    =       -4283696
40                 Z    =        -1288638
42
 XDOT =     -15518
980103                 XDOT =       -4719
752187
 YDOT =       5310
095072  feet/sec       YDOT =        1565
679678  meter/sec
 ZDOT =     -19032
329452                 ZDOT =       -5824
007449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5681541
39                 X    =        -1731733
82
 Y    =       21153209
39  feet           Y    =         6447498
22  meter
 Z    =       -4212869
17                 Z    =        -1284082
52
 XDOT =     -12831
388369                 XDOT =       -3911
007175
 YDOT =      -7249
310622  feet/sec       YDOT =       -2209
589877  meter/sec
 ZDOT =     -19129
173590                 ZDOT =       -5830
572110


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   13361
63392475  
00016717  00000-0  10270-3 0  9077
2 25544  51
6468 229
8617 0005344 318
1472  41
9269 15
50191688 24718


Satellite: ISS
Catalog Number: 25544
Epoch time:      13361
63392475   =   yrday
fracday
Element set:     907
Inclination:       51
6468  deg
RA of node:       229
8617  deg
Eccentricity:     
0005344     
Arg of perigee:   318
1472  deg
Mean anomaly:      41
9269  deg
Mean motion:   15
50191688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2471
Checksum:              329


Coasting Arc #9 (Orbit 2486)
---------------------------------------

Vector Time (GMT): 2013/362/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3687380
01                 A    =         6799530
59  meter
 Y    =       -5445786
62  meter          E    =           
0013686
 Z    =        1692461
48                 I    =           51
40972
 XDOT =       4910
148648                 Wp   =           42
29836
 YDOT =      -1554
745927  meter/sec      RA   =          224
04716  deg
 ZDOT =       5678
215595                 TA   =          336
29498
                                          MA   =          336
35797
                                          Ha   =            226
825  n
mi
                                          Hp   =            221
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12097703
45                 X    =        -3634431
50
 Y    =      -17866754
02  feet           Y    =        -5486725
33  meter
 Z    =        5552695
15                 Z    =         1674676
69
 XDOT =      16109
411575                 XDOT =        4899
585936
 YDOT =      -5100
872463  feet/sec       YDOT =       -1499
896992  meter/sec
 ZDOT =      18629
316256                 ZDOT =        5702
042937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4460653
96                 X    =         1359607
33
 Y    =      -21130419
23  feet           Y    =        -6440551
78  meter
 Z    =        5478658
68                 Z    =         1669895
16
 XDOT =      13223
164534                 XDOT =        4030
420550
 YDOT =       7662
237378  feet/sec       YDOT =        2335
449953  meter/sec
 ZDOT =      18729
838145                 ZDOT =        5708
854667


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   13362
66536415  
00016717  00000-0  10270-3 0  9086
2 25544  51
6460 224
7491 0005261 320
8897  39
1873 15
50223820 24874


Satellite: ISS
Catalog Number: 25544
Epoch time:      13362
66536415   =   yrday
fracday
Element set:     908
Inclination:       51
6460  deg
RA of node:       224
7491  deg
Eccentricity:     
0005261     
Arg of perigee:   320
8897  deg
Mean anomaly:      39
1873  deg
Mean motion:   15
50223820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2487
Checksum:              314


Coasting Arc #10 (Orbit 2501)
---------------------------------------

Vector Time (GMT): 2013/363/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3793642
61                 A    =         6798726
70  meter
 Y    =        5236892
66  meter          E    =           
0001377
 Z    =       -2099104
21                 I    =           51
43021
 XDOT =      -5111
406242                 Wp   =          111
79913
 YDOT =       1499
411220  meter/sec      RA   =          219
07828  deg
 ZDOT =      -5500
327469                 TA   =           91
46031
                                          MA   =           91
44453
                                          Ha   =            226
932  n
mi
                                          Hp   =            221
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12446334
02                 X    =         3744997
44
 Y    =       17181406
37  feet           Y    =         5279043
80  meter
 Z    =       -6886824
83                 Z    =        -2080792
69
 XDOT =     -16769
705520                 XDOT =       -5101
073994
 YDOT =       4919
328151  feet/sec       YDOT =        1442
310512  meter/sec
 ZDOT =     -18045
693795                 ZDOT =       -5525
132989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3358972
72                 X    =        -1023814
88
 Y    =       20973180
82  feet           Y    =         6392625
51  meter
 Z    =       -6810528
63                 Z    =        -2075849
13
 XDOT =     -13709
780669                 XDOT =       -4178
741148
 YDOT =      -8085
898704  feet/sec       YDOT =       -2464
581925  meter/sec
 ZDOT =     -18150
336753                 ZDOT =       -5532
222642


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   13363
63231557  
00016717  00000-0  10270-3 0  9094
2 25544  51
6458 219
9575 0005326 325
9842  34
0967 15
50277152 25021


Satellite: ISS
Catalog Number: 25544
Epoch time:      13363
63231557   =   yrday
fracday
Element set:     909
Inclination:       51
6458  deg
RA of node:       219
9575  deg
Eccentricity:     
0005326     
Arg of perigee:   325
9842  deg
Mean anomaly:      34
0967  deg
Mean motion:   15
50277152  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2502
Checksum:              319


Coasting Arc #11 (Orbit 2517)
---------------------------------------

Vector Time (GMT): 2013/364/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901192
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3858345
77                 A    =         6797929
38  meter
 Y    =       -5004197
29  meter          E    =           
0013186
 Z    =        2484493
77                 I    =           51
45135
 XDOT =       5340
165857                 Wp   =           53
01109
 YDOT =      -1481
444754  meter/sec      RA   =          214
10893  deg
 ZDOT =       5297
524485                 TA   =          334
88533
                                          MA   =          334
94940
                                          Ha   =            226
963  n
mi
                                          Hp   =            221
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12658614
72                 X    =        -3814169
91
 Y    =      -16417970
11  feet           Y    =        -5047097
05  meter
 Z    =        8151226
29                 Z    =         2465857
09
 XDOT =      17520
229191                 XDOT =        5330
600974
 YDOT =      -4860
383052  feet/sec       YDOT =       -1421
781691  meter/sec
 ZDOT =      17380
329675                 ZDOT =        5323
443030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2308053
41                 X    =          703494
68
 Y    =      -20633081
12  feet           Y    =        -6288963
12  meter
 Z    =        8073513
00                 Z    =         2460806
76
 XDOT =      14376
306985                 XDOT =        4381
898369
 YDOT =       8466
867838  feet/sec       YDOT =        2580
701317  meter/sec
 ZDOT =      17489
670141                 ZDOT =        5330
851459


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   13364
66370634  
00016717  00000-0  10270-3 0  9100
2 25544  51
6448 214
8448 0005183 328
3070  31
7768 15
50299201 25183


Satellite: ISS
Catalog Number: 25544
Epoch time:      13364
66370634   =   yrday
fracday
Element set:     910
Inclination:       51
6448  deg
RA of node:       214
8448  deg
Eccentricity:     
0005183     
Arg of perigee:   328
3070  deg
Mean anomaly:      31
7768  deg
Mean motion:   15
50299201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2518
Checksum:              307
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