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

 
Date: December 23rd 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19116 7 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 1718)
---------------------------------------

Vector Time (GMT): 2015/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         996990
92                 A    =         6776944
44  meter
 Y    =       -4664601
14  meter          E    =           
0001416
 Z    =        4813764
34                 I    =           51
35198
 XDOT =       6129
677115                 Wp   =          344
96073
 YDOT =       3878
711230  meter/sec      RA   =          228
26010  deg
 ZDOT =       2490
497664                 TA   =           80
47817
                                          MA   =           80
46217
                                          Ha   =            219
286  n
mi
                                          Hp   =            215
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3270967
58                 X    =         1025693
97
 Y    =      -15303809
50  feet           Y    =        -4653291
93  meter
 Z    =       15793190
11                 Z    =         4818676
99
 XDOT =      20110
489221                 XDOT =        6073
750884
 YDOT =      12725
430545  feet/sec       YDOT =        3946
944475  meter/sec
 ZDOT =       8170
924094                 ZDOT =        2520
138977

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15238420
33                 X    =         4644670
52
 Y    =        3463873
77  feet           Y    =         1055788
72  meter
 Z    =       15815270
86                 Z    =         4820494
56
 XDOT =     -12857
588474                 XDOT =       -3918
992967
 YDOT =      18697
698638  feet/sec       YDOT =        5699
058545  meter/sec
 ZDOT =       8298
373255                 ZDOT =        2529
344168


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
55265189  
00016717  00000-0  10270-3 0  9007
2 25544  51
6429 229
0137 0008292 306
7246  53
3144 15
54993861 17191


Satellite: ISS
Catalog Number: 25544
Epoch time:      15355
55265189   =   yrday
fracday
Element set:     900
Inclination:       51
6429  deg
RA of node:       229
0137  deg
Eccentricity:     
0008292     
Arg of perigee:   306
7246  deg
Mean anomaly:      53
3144  deg
Mean motion:   15
54993861  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1719
Checksum:              322


Coasting Arc #2 (Orbit 1733)
---------------------------------------

Vector Time (GMT): 2015/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2651528
18                 A    =         6774689
16  meter
 Y    =        3310523
83  meter          E    =           
0010314
 Z    =       -5290146
75                 I    =           51
36624
 XDOT =      -5737
495517                 Wp   =           54
16602
 YDOT =      -5072
508111  meter/sec      RA   =          223
23249  deg
 ZDOT =       -293
057137                 TA   =          212
99592
                                          MA   =          213
06033
                                          Ha   =            219
396  n
mi
                                          Hp   =            215
053

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8699239
43                 X    =        -2662652
56
 Y    =       10861298
67  feet           Y    =         3280810
92  meter
 Z    =      -17356124
52                 Z    =        -5303054
17
 XDOT =     -18823
804189                 XDOT =       -5678
923495
 YDOT =     -16642
086979  feet/sec       YDOT =       -5136
341057  meter/sec
 ZDOT =       -961
473545                 ZDOT =        -320
787016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10841934
43                 X    =        -3304621
62
 Y    =       -8610221
89  feet           Y    =        -2624395
63  meter
 Z    =      -17412529
13                 Z    =        -5307338
88
 XDOT =      16053
040621                 XDOT =        4892
966781
 YDOT =     -17992
338349  feet/sec       YDOT =       -5484
064729  meter/sec
 ZDOT =      -1080
460240                 ZDOT =        -329
324281


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
51662887  
00016717  00000-0  10270-3 0  9011
2 25544  51
6421 224
2012 0008456 309
9338  50
1071 15
55056155 17349


Satellite: ISS
Catalog Number: 25544
Epoch time:      15356
51662887   =   yrday
fracday
Element set:     901
Inclination:       51
6421  deg
RA of node:       224
2012  deg
Eccentricity:     
0008456     
Arg of perigee:   309
9338  deg
Mean anomaly:      50
1071  deg
Mean motion:   15
55056155  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1734
Checksum:              294


Coasting Arc #3 (Orbit 1749)
---------------------------------------

Vector Time (GMT): 2015/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4223661
31                 A    =         6775800
56  meter
 Y    =       -1758254
68  meter          E    =           
0009173
 Z    =        5002021
80                 I    =           51
39425
 XDOT =       4718
548453                 Wp   =          351
19578
 YDOT =       5713
151503  meter/sec      RA   =          218
20510  deg
 ZDOT =      -1967
659239                 TA   =          118
02413
                                          MA   =          117
93131
                                          Ha   =            219
481  n
mi
                                          Hp   =            214
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13857156
54                 X    =         4218710
68
 Y    =       -5768552
10  feet           Y    =        -1711051
07  meter
 Z    =       16410832
67                 Z    =         5022527
35
 XDOT =      15480
802011                 XDOT =        4663
870054
 YDOT =      18743
935378  feet/sec       YDOT =        5765
611892  meter/sec
 ZDOT =      -6455
574930                 ZDOT =       -1944
869690

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5974550
87                 X    =         1821043
10
 Y    =       13662834
08  feet           Y    =         4164431
83  meter
 Z    =       16499821
72                 Z    =         5029145
66
 XDOT =     -17509
837876                 XDOT =       -5336
998585
 YDOT =      15368
205719  feet/sec       YDOT =        4684
229103  meter/sec
 ZDOT =      -6358
048009                 ZDOT =       -1937
933033


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
54485277  
00016717  00000-0  10270-3 0  9022
2 25544  51
6420 219
0682 0008542 313
2482  46
7957 15
55090938 17506


Satellite: ISS
Catalog Number: 25544
Epoch time:      15357
54485277   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:       219
0682  deg
Eccentricity:     
0008542     
Arg of perigee:   313
2482  deg
Mean anomaly:      46
7957  deg
Mean motion:   15
55090938  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1750
Checksum:              322


Coasting Arc #4 (Orbit 1764)
---------------------------------------

Vector Time (GMT): 2015/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5471878
10                 A    =         6779615
12  meter
 Y    =         226599
27  meter          E    =           
0004127
 Z    =       -3994011
69                 I    =           51
43137
 XDOT =      -3114
532654                 Wp   =           12
34847
 YDOT =      -5793
969347  meter/sec      RA   =          213
18701  deg
 ZDOT =       3942
962770                 TA   =          298
74537
                                          MA   =          298
78683
                                          Ha   =            219
579  n
mi
                                          Hp   =            214
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17952355
97                 X    =        -5454603
97
 Y    =         743435
91  feet           Y    =          165506
12  meter
 Z    =      -13103712
89                 Z    =        -4020550
94
 XDOT =     -10218
282987                 XDOT =       -3068
664953
 YDOT =     -19009
085784  feet/sec       YDOT =       -5828
542066  meter/sec
 ZDOT =      12936
229560                 ZDOT =        3927
943819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1319626
88                 X    =         -402222
27
 Y    =      -17834684
15  feet           Y    =        -5436011
73  meter
 Z    =      -13218536
20                 Z    =        -4029009
83
 XDOT =      17364
266202                 XDOT =        5292
628338
 YDOT =     -10814
039564  feet/sec       YDOT =       -3296
119259  meter/sec
 ZDOT =      12872
306476                 ZDOT =        3923
479014


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
50879672  
00016717  00000-0  10270-3 0  9036
2 25544  51
6405 214
2549 0008570 316
6942  43
3547 15
55098124 17656


Satellite: ISS
Catalog Number: 25544
Epoch time:      15358
50879672   =   yrday
fracday
Element set:     903
Inclination:       51
6405  deg
RA of node:       214
2549  deg
Eccentricity:     
0008570     
Arg of perigee:   316
6942  deg
Mean anomaly:      43
3547  deg
Mean motion:   15
55098124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1765
Checksum:              326


Coasting Arc #5 (Orbit 1780)
---------------------------------------

Vector Time (GMT): 2015/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6238852
96                 A    =         6783872
78  meter
 Y    =        1192993
68  meter          E    =           
0008344
 Z    =        2380428
89                 I    =           51
47320
 XDOT =       1021
079431                 Wp   =           69
25587
 YDOT =       5386
928907  meter/sec      RA   =          208
18594  deg
 ZDOT =      -5357
766390                 TA   =           84
09201
                                          MA   =           83
99691
                                          Ha   =            219
833  n
mi
                                          Hp   =            214
286

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20468677
69                 X    =         6213485
79
 Y    =        3914021
26  feet           Y    =         1262618
56  meter
 Z    =        7809806
05                 Z    =         2410674
29
 XDOT =       3349
998134                 XDOT =         986
791382
 YDOT =      17673
651269  feet/sec       YDOT =        5398
156163  meter/sec
 ZDOT =     -17577
973721                 ZDOT =       -5352
888917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2898724
88                 X    =         -883531
34
 Y    =       20587044
96  feet           Y    =         6274931
30  meter
 Z    =        7940426
53                 Z    =         2420242
01
 XDOT =     -15977
570179                 XDOT =       -4869
963390
 YDOT =       4544
926596  feet/sec       YDOT =        1385
293626  meter/sec
 ZDOT =     -17557
832013                 ZDOT =       -5351
627198


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
53698355  
00016717  00000-0  10270-3 0  9048
2 25544  51
6404 209
1215 0008697 321
1915  38
8613 15
55151321 17819


Satellite: ISS
Catalog Number: 25544
Epoch time:      15359
53698355   =   yrday
fracday
Element set:     904
Inclination:       51
6404  deg
RA of node:       209
1215  deg
Eccentricity:     
0008697     
Arg of perigee:   321
1915  deg
Mean anomaly:      38
8613  deg
Mean motion:   15
55151321  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1781
Checksum:              311


Coasting Arc #6 (Orbit 1795)
---------------------------------------

Vector Time (GMT): 2015/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6340691
42                 A    =         6786319
02  meter
 Y    =       -2352248
43  meter          E    =           
0015512
 Z    =        -421818
30                 I    =           51
50816
 XDOT =       1317
253300                 Wp   =            9
08498
 YDOT =      -4616
624089  meter/sec      RA   =          203
19662  deg
 ZDOT =       5988
731281                 TA   =          346
35324
                                          MA   =          346
39514
                                          Ha   =            219
944  n
mi
                                          Hp   =            214
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20802793
39                 X    =        -6311867
74
 Y    =       -7717350
50  feet           Y    =        -2422993
02  meter
 Z    =       -1383918
31                 Z    =         -452550
00
 XDOT =       4321
697180                 XDOT =        1339
688985
 YDOT =     -15146
404493  feet/sec       YDOT =       -4601
768871  meter/sec
 ZDOT =      19648
068508                 ZDOT =        5995
184174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6313388
82                 X    =         1924320
91
 Y    =      -21261947
54  feet           Y    =        -6480641
61  meter
 Z    =       -1516459
63                 Z    =         -462216
90
 XDOT =      13840
211504                 XDOT =        4218
496466
 YDOT =       2715
844583  feet/sec       YDOT =         827
789429  meter/sec
 ZDOT =      19676
801128                 ZDOT =        5997
488984


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
50089263  
00016717  00000-0  10270-3 0  9050
2 25544  51
6388 204
3074 0008677 324
1834  35
8737 15
55134711 17965


Satellite: ISS
Catalog Number: 25544
Epoch time:      15360
50089263   =   yrday
fracday
Element set:     905
Inclination:       51
6388  deg
RA of node:       204
3074  deg
Eccentricity:     
0008677     
Arg of perigee:   324
1834  deg
Mean anomaly:      35
8737  deg
Mean motion:   15
55134711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1796
Checksum:              319


Coasting Arc #7 (Orbit 1811)
---------------------------------------

Vector Time (GMT): 2015/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5733778
71                 A    =         6785240
19  meter
 Y    =        3245459
01  meter          E    =           
0001011
 Z    =       -1624674
33                 I    =           51
53403
 XDOT =      -3644
678175                 Wp   =           16
81508
 YDOT =       3579
057308  meter/sec      RA   =          198
21318  deg
 ZDOT =      -5713
147151                 TA   =          180
98996
                                          MA   =          180
99016
                                          Ha   =            220
082  n
mi
                                          Hp   =            214
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18811609
93                 X    =         5704952
97
 Y    =       10647831
39  feet           Y    =         3309416
88  meter
 Z    =       -5330296
36                 Z    =        -1596890
91
 XDOT =     -11957
605561                 XDOT =       -3656
677311
 YDOT =      11742
314001  feet/sec       YDOT =        3538
233533  meter/sec
 ZDOT =     -18743
921099                 ZDOT =       -5730
880830

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9029598
37                 X    =        -2752221
58
 Y    =       19671821
46  feet           Y    =         5995971
18  meter
 Z    =       -5210646
28                 Z    =        -1588204
99
 XDOT =     -11257
270044                 XDOT =       -3431
215909
 YDOT =     -10152
626288  feet/sec       YDOT =       -3094
520493  meter/sec
 ZDOT =     -18821
282737                 ZDOT =       -5736
726978


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
52904378  
00016717  00000-0  10270-3 0  9067
2 25544  51
6383 199
1736 0008650 327
8275  32
2349 15
55165912 18122


Satellite: ISS
Catalog Number: 25544
Epoch time:      15361
52904378   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:       199
1736  deg
Eccentricity:     
0008650     
Arg of perigee:   327
8275  deg
Mean anomaly:      32
2349  deg
Mean motion:   15
55165912  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1812
Checksum:              323


Coasting Arc #8 (Orbit 1827)
---------------------------------------

Vector Time (GMT): 2015/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4414495
54                 A    =         6781268
52  meter
 Y    =       -3830052
45  meter          E    =           
0011195
 Z    =        3424394
11                 I    =           51
55139
 XDOT =       5657
545935                 Wp   =           47
58953
 YDOT =      -2414
695041  meter/sec      RA   =          193
22137  deg
 ZDOT =       4590
397082                 TA   =          352
61421
                                          MA   =          352
63069
                                          Ha   =            220
198  n
mi
                                          Hp   =            213
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14483253
09                 X    =        -4387972
99
 Y    =      -12565788
89  feet           Y    =        -3879270
21  meter
 Z    =       11234888
82                 Z    =         3403013
87
 XDOT =      18561
502411                 XDOT =        5661
829134
 YDOT =      -7922
227824  feet/sec       YDOT =       -2351
405001  meter/sec
 ZDOT =      15060
357879                 ZDOT =        4617
890091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11030727
12                 X    =         3362165
62
 Y    =      -15749359
55  feet           Y    =        -4800404
79  meter
 Z    =       11143030
59                 Z    =         3396395
72
 XDOT =       8596
414354                 XDOT =        2620
187095
 YDOT =      16765
993370  feet/sec       YDOT =        5110
274779  meter/sec
 ZDOT =      15179
758070                 ZDOT =        4626
790260


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
55717506  
00016717  00000-0  10270-3 0  9077
2 25544  51
6379 194
0379 0008682 330
9696  29
0973 15
55214875 18288


Satellite: ISS
Catalog Number: 25544
Epoch time:      15362
55717506   =   yrday
fracday
Element set:     907
Inclination:       51
6379  deg
RA of node:       194
0379  deg
Eccentricity:     
0008682     
Arg of perigee:   330
9696  deg
Mean anomaly:      29
0973  deg
Mean motion:   15
55214875  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              349


Coasting Arc #9 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2015/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2550646
58                 A    =         6776743
74  meter
 Y    =        4152592
68  meter          E    =           
0013224
 Z    =       -4719914
34                 I    =           51
56722
 XDOT =      -7048
714617                 Wp   =           30
76599
 YDOT =       1190
235375  meter/sec      RA   =          188
21811  deg
 ZDOT =      -2754
262785                 TA   =          211
87323
                                          MA   =          211
95332
                                          Ha   =            220
295  n
mi
                                          Hp   =            213
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8368263
07                 X    =         2526948
87
 Y    =       13623991
72  feet           Y    =         4180983
43  meter
 Z    =      -15485283
25                 Z    =        -4707581
35
 XDOT =     -23125
704124                 XDOT =       -7048
121308
 YDOT =       3904
971704  feet/sec       YDOT =        1111
415450  meter/sec
 ZDOT =      -9036
295227                 ZDOT =       -2788
501967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12527407
11                 X    =        -3818353
69
 Y    =       10016645
39  feet           Y    =         3053073
51  meter
 Z    =      -15432623
27                 Z    =        -4703863
57
 XDOT =      -5870
143946                 XDOT =       -1789
219875
 YDOT =     -21531
430542  feet/sec       YDOT =       -6562
780029  meter/sec
 ZDOT =      -9184
695077                 ZDOT =       -2799
495060


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
52103261  
00016717  00000-0  10270-3 0  9083
2 25544  51
6373 189
2244 0008606 335
9203  24
1547 15
55234557 18433


Satellite: ISS
Catalog Number: 25544
Epoch time:      15363
52103261   =   yrday
fracday
Element set:     908
Inclination:       51
6373  deg
RA of node:       189
2244  deg
Eccentricity:     
0008606     
Arg of perigee:   335
9203  deg
Mean anomaly:      24
1547  deg
Mean motion:   15
55234557  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              300


Coasting Arc #10 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2015/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907469
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -309454
27                 A    =         6774288
92  meter
 Y    =       -4218828
56  meter          E    =           
0007034
 Z    =        5290979
38                 I    =           51
59094
 XDOT =       7655
302949                 Wp   =          357
34578
 YDOT =         41
311873  meter/sec      RA   =          183
20370  deg
 ZDOT =        487
580927                 TA   =           88
04177
                                          MA   =           87
96122
                                          Ha   =            220
446  n
mi
                                          Hp   =            213
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1015269
93                 X    =         -287956
47
 Y    =      -13841301
04  feet           Y    =        -4222169
07  meter
 Z    =       17358856
22                 Z    =         5289528
19
 XDOT =      25115
823323                 XDOT =        7651
903586
 YDOT =        135
537641  feet/sec       YDOT =         126
899506  meter/sec
 ZDOT =       1599
674956                 ZDOT =         524
760040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13560455
00                 X    =         4133226
68
 Y    =       -2986509
23  feet           Y    =         -910288
01  meter
 Z    =       17353302
27                 Z    =         5289286
53
 XDOT =       3040
537997                 XDOT =         926
755982
 YDOT =      23904
238293  feet/sec       YDOT =        7286
011832  meter/sec
 ZDOT =       1760
605511                 ZDOT =         536
632560


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
54912926  
00016717  00000-0  10270-3 0  9093
2 25544  51
6376 184
0891 0008616 339
9863  20
0951 15
55211699 18597


Satellite: ISS
Catalog Number: 25544
Epoch time:      15364
54912926   =   yrday
fracday
Element set:     909
Inclination:       51
6376  deg
RA of node:       184
0891  deg
Eccentricity:     
0008616     
Arg of perigee:   339
9863  deg
Mean anomaly:      20
0951  deg
Mean motion:   15
55211699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              344
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