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

 
Date: December 3rd 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 1422)
---------------------------------------

Vector Time (GMT): 2015/336/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3448552
49                 A    =         6776968
53  meter
 Y    =        2626225
41  meter          E    =           
0007782
 Z    =        5213360
13                 I    =           51
40780
 XDOT =      -5562
131643                 Wp   =          205
08488
 YDOT =       5165
243308  meter/sec      RA   =          323
58397  deg
 ZDOT =       1070
947536                 TA   =          234
58231
                                          MA   =          234
65500
                                          Ha   =            220
276  n
mi
                                          Hp   =            216
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11314148
58                 X    =         3393604
44
 Y    =        8616225
10  feet           Y    =         2664482
04  meter
 Z    =       17104199
91                 Z    =         5229979
20
 XDOT =     -18248
463397                 XDOT =       -5624
679549
 YDOT =      16946
336311  feet/sec       YDOT =        5102
694126  meter/sec
 ZDOT =       3513
607403                 ZDOT =        1043
775886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12919178
46                 X    =        -3937765
59
 Y    =        5735989
19  feet           Y    =         1748329
50  meter
 Z    =       17175453
52                 Z    =         5235078
23
 XDOT =      -5759
407517                 XDOT =       -1755
467411
 YDOT =     -23199
985888  feet/sec       YDOT =       -7071
355699  meter/sec
 ZDOT =       3395
142966                 ZDOT =        1034
839576


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   15336
52599216  
00016717  00000-0  10270-3 0  9004
2 25544  51
6406 323
9335 0008187 232
2016 127
8396 15
54382723 14238


Satellite: ISS
Catalog Number: 25544
Epoch time:      15336
52599216   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:       323
9335  deg
Eccentricity:     
0008187     
Arg of perigee:   232
2016  deg
Mean anomaly:     127
8396  deg
Mean motion:   15
54382723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1423
Checksum:              306


Coasting Arc #2 (Orbit 1437)
---------------------------------------

Vector Time (GMT): 2015/337/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1934189
75                 A    =         6776905
88  meter
 Y    =       -3863460
70  meter          E    =           
0009889
 Z    =       -5228423
90                 I    =           51
38238
 XDOT =       6183
062095                 Wp   =          130
98093
 YDOT =      -4420
387966  meter/sec      RA   =          318
56382  deg
 ZDOT =        973
875437                 TA   =          148
41013
                                          MA   =          148
35073
                                          Ha   =            220
113  n
mi
                                          Hp   =            216
422

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6345766
88                 X    =        -1865445
96
 Y    =      -12675395
99  feet           Y    =        -3884705
62  meter
 Z    =      -17153621
71                 Z    =        -5237652
97
 XDOT =      20285
636794                 XDOT =        6227
301667
 YDOT =     -14502
585191  feet/sec       YDOT =       -4350
997543  meter/sec
 ZDOT =       3195
129388                 ZDOT =        1004
019093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14123994
61                 X    =         4304993
56
 Y    =         324336
38  feet           Y    =           98857
73  meter
 Z    =      -17192694
40                 Z    =        -5240333
25
 XDOT =       3526
593969                 XDOT =        1074
905842
 YDOT =      23642
034348  feet/sec       YDOT =        7206
092069  meter/sec
 ZDOT =       3326
268562                 ZDOT =        1013
846658


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   15337
49034855  
00016717  00000-0  10270-3 0  9015
2 25544  51
6405 319
1241 0008187 236
0206 124
0169 15
54399752 14386


Satellite: ISS
Catalog Number: 25544
Epoch time:      15337
49034855   =   yrday
fracday
Element set:     901
Inclination:       51
6405  deg
RA of node:       319
1241  deg
Eccentricity:     
0008187     
Arg of perigee:   236
0206  deg
Mean anomaly:     124
0169  deg
Mean motion:   15
54399752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1438
Checksum:              305


Coasting Arc #3 (Orbit 1453)
---------------------------------------

Vector Time (GMT): 2015/338/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         416030
18                 A    =         6779278
64  meter
 Y    =        4933760
77  meter          E    =           
0000679
 Z    =        4630103
52                 I    =           51
36687
 XDOT =      -6303
227349                 Wp   =          143
36077
 YDOT =       3259
284429  meter/sec      RA   =          313
54517  deg
 ZDOT =      -2906
986898                 TA   =          335
66895
                                          MA   =          335
67215
                                          Ha   =            219
809  n
mi
                                          Hp   =            216
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1364928
41                 X    =          338337
25
 Y    =       16186879
18  feet           Y    =         4937978
61  meter
 Z    =       15190628
33                 Z    =         4631935
90
 XDOT =     -20679
879754                 XDOT =       -6325
083829
 YDOT =      10693
190385  feet/sec       YDOT =        3188
675421  meter/sec
 ZDOT =      -9537
358589                 ZDOT =       -2937
660028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15050711
28                 X    =        -4587456
80
 Y    =       -6094622
80  feet           Y    =        -1857641
03  meter
 Z    =       15197530
69                 Z    =         4632207
35
 XDOT =       -804
300788                 XDOT =        -245
150880
 YDOT =     -22125
623552  feet/sec       YDOT =       -6743
890059  meter/sec
 ZDOT =      -9670
536362                 ZDOT =       -2947
579483


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15338
51897641  
00016717  00000-0  10270-3 0  9020
2 25544  51
6399 313
9933 0008197 240
4420 119
5917 15
54453017 14549


Satellite: ISS
Catalog Number: 25544
Epoch time:      15338
51897641   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       313
9933  deg
Eccentricity:     
0008197     
Arg of perigee:   240
4420  deg
Mean anomaly:     119
5917  deg
Mean motion:   15
54453017  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1454
Checksum:              323


Coasting Arc #4 (Orbit 1468)
---------------------------------------

Vector Time (GMT): 2015/339/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1006397
80                 A    =         6783242
87  meter
 Y    =       -5733932
92  meter          E    =           
0004404
 Z    =       -3483467
13                 I    =           51
35867
 XDOT =       5960
648295                 Wp   =          210
19094
 YDOT =      -1697
227026  meter/sec      RA   =          308
53462  deg
 ZDOT =       4509
552570                 TA   =          108
70795
                                          MA   =          108
66015
                                          Ha   =            219
643  n
mi
                                          Hp   =            216
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3301830
06                 X    =         1087362
80
 Y    =      -18812115
87  feet           Y    =        -5722225
94  meter
 Z    =      -11428697
94                 Z    =        -3478381
65
 XDOT =      19555
932727                 XDOT =        5957
278150
 YDOT =      -5568
330138  feet/sec       YDOT =       -1630
590053  meter/sec
 ZDOT =      14795
119979                 ZDOT =        4538
500323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15520387
25                 X    =         4730614
04
 Y    =       11155435
88  feet           Y    =         3400176
86  meter
 Z    =      -11405557
93                 Z    =        -3476414
06
 XDOT =      -2552
867226                 XDOT =        -778
113931
 YDOT =      18827
753037  feet/sec       YDOT =        5738
699126  meter/sec
 ZDOT =      14920
517155                 ZDOT =        4547
773629


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15339
48329760  
00016717  00000-0  10270-3 0  9030
2 25544  51
6397 309
1832 0008066 243
9128 116
1195 15
54459741 14697


Satellite: ISS
Catalog Number: 25544
Epoch time:      15339
48329760   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       309
1832  deg
Eccentricity:     
0008066     
Arg of perigee:   243
9128  deg
Mean anomaly:     116
1195  deg
Mean motion:   15
54459741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1469
Checksum:              331


Coasting Arc #5 (Orbit 1484)
---------------------------------------

Vector Time (GMT): 2015/340/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2216098
60                 A    =         6786662
92  meter
 Y    =        6114986
66  meter          E    =           
0009956
 Z    =        1914337
40                 I    =           51
35156
 XDOT =      -5256
021853                 Wp   =          147
67790
 YDOT =       -154
585596  meter/sec      RA   =          303
53383  deg
 ZDOT =      -5585
529988                 TA   =           11
12815
                                          MA   =           11
10615
                                          Ha   =            219
311  n
mi
                                          Hp   =            217
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7270664
71                 X    =        -2293612
42
 Y    =       20062292
18  feet           Y    =         6089771
32  meter
 Z    =        6280634
51                 Z    =         1903383
78
 XDOT =     -17244
166186                 XDOT =       -5226
769848
 YDOT =       -507
170589  feet/sec       YDOT =        -213
198195  meter/sec
 ZDOT =     -18325
229620                 ZDOT =       -5610
991995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15211328
41                 X    =        -4636412
90
 Y    =      -14986034
71  feet           Y    =        -4567743
38  meter
 Z    =        6232074
62                 Z    =         1899536
34
 XDOT =       6486
295573                 XDOT =        1977
022891
 YDOT =     -14257
414945  feet/sec       YDOT =       -4345
660075  meter/sec
 ZDOT =     -18435
187939                 ZDOT =       -5619
045284


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15340
51188727  
00016717  00000-0  10270-3 0  9043
2 25544  51
6397 304
0519 0008118 248
6417 111
3870 15
54519533 14855


Satellite: ISS
Catalog Number: 25544
Epoch time:      15340
51188727   =   yrday
fracday
Element set:     904
Inclination:       51
6397  deg
RA of node:       304
0519  deg
Eccentricity:     
0008118     
Arg of perigee:   248
6417  deg
Mean anomaly:     111
3870  deg
Mean motion:   15
54519533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1485
Checksum:              312


Coasting Arc #6 (Orbit 1499)
---------------------------------------

Vector Time (GMT): 2015/341/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3164137
57                 A    =         6788067
11  meter
 Y    =       -6000094
34  meter          E    =           
0005831
 Z    =        -108792
78                 I    =           51
33966
 XDOT =       4281
813534                 Wp   =            7
41333
 YDOT =       2150
224682  meter/sec      RA   =          298
54001  deg
 ZDOT =       5985
912448                 TA   =          351
40992
                                          MA   =          351
41990
                                          Ha   =            219
149  n
mi
                                          Hp   =            217
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10381028
77                 X    =         3231525
41
 Y    =      -19685348
87  feet           Y    =        -5964334
07  meter
 Z    =        -356931
68                 Z    =          -93258
35
 XDOT =      14047
944665                 XDOT =        4228
373233
 YDOT =       7054
542921  feet/sec       YDOT =        2197
807715  meter/sec
 ZDOT =      19638
820367                 ZDOT =        6006
583239

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13892498
49                 X    =         4234433
54
 Y    =       17387389
30  feet           Y    =         5299676
26  meter
 Z    =        -288613
82                 Z    =          -87969
49
 XDOT =     -10766
002843                 XDOT =       -3281
477667
 YDOT =       8926
677710  feet/sec       YDOT =        2720
851366  meter/sec
 ZDOT =      19727
677099                 ZDOT =        6012
995980


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15341
47617262  
00016717  00000-0  10270-3 0  9051
2 25544  51
6395 299
2417 0008095 250
5583 109
4695 15
54560512 15009


Satellite: ISS
Catalog Number: 25544
Epoch time:      15341
47617262   =   yrday
fracday
Element set:     905
Inclination:       51
6395  deg
RA of node:       299
2417  deg
Eccentricity:     
0008095     
Arg of perigee:   250
5583  deg
Mean anomaly:     109
4695  deg
Mean motion:   15
54560512  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1500
Checksum:              314


Coasting Arc #7 (Orbit 1515)
---------------------------------------

Vector Time (GMT): 2015/342/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3825158
15                 A    =         6786754
77  meter
 Y    =        5327763
90  meter          E    =           
0008505
 Z    =       -1721898
38                 I    =           51
32195
 XDOT =      -3158
574708                 Wp   =          202
00016
 YDOT =      -4098
171284  meter/sec      RA   =          293
54505  deg
 ZDOT =      -5662
189064                 TA   =          356
98191
                                          MA   =          356
98703
                                          Ha   =            218
753  n
mi
                                          Hp   =            217
276

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12549731
48                 X    =        -3876085
76
 Y    =       17479540
34  feet           Y    =         5284703
79  meter
 Z    =       -5649272
92                 Z    =        -1740603
94
 XDOT =     -10362
777914                 XDOT =       -3085
008009
 YDOT =     -13445
443846  feet/sec       YDOT =       -4133
080906  meter/sec
 ZDOT =     -18576
735774                 ZDOT =       -5677
354566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11334338
61                 X    =        -3454706
41
 Y    =      -18265570
97  feet           Y    =        -5567346
03  meter
 Z    =       -5731148
28                 Z    =        -1746854
00
 XDOT =      15017
744324                 XDOT =        4577
408470
 YDOT =      -3468
514749  feet/sec       YDOT =       -1057
203295  meter/sec
 ZDOT =     -18641
421239                 ZDOT =       -5681
905194


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15342
50472432  
00016717  00000-0  10270-3 0  9065
2 25544  51
6405 294
1101 0008111 256
0807 103
9444 15
54568863 15169


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
50472432   =   yrday
fracday
Element set:     906
Inclination:       51
6405  deg
RA of node:       294
1101  deg
Eccentricity:     
0008111     
Arg of perigee:   256
0807  deg
Mean anomaly:     103
9444  deg
Mean motion:   15
54568863  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1516
Checksum:              288


Coasting Arc #8 (Orbit 1531)
---------------------------------------

Vector Time (GMT): 2015/343/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4212031
65                 A    =         6783068
36  meter
 Y    =       -4131243
52  meter          E    =           
0004673
 Z    =        3344568
79                 I    =           51
29868
 XDOT =       1979
788578                 Wp   =          108
09732
 YDOT =       5777
015339  meter/sec      RA   =          288
54225  deg
 ZDOT =       4635
772156                 TA   =          291
09447
                                          MA   =          291
14442
                                          Ha   =            218
650  n
mi
                                          Hp   =            217
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13819001
47                 X    =         4241668
29
 Y    =      -13553948
54  feet           Y    =        -4083976
33  meter
 Z    =       10972994
71                 Z    =         3365101
99
 XDOT =       6495
369349                 XDOT =        1892
522284
 YDOT =      18953
462397  feet/sec       YDOT =        5798
666371  meter/sec
 ZDOT =      15209
226232                 ZDOT =        4645
178171

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7541738
47                 X    =         2298721
88
 Y    =       17771430
11  feet           Y    =         5416731
90  meter
 Z    =       11062521
78                 Z    =         3371856
64
 XDOT =     -18683
226336                 XDOT =       -5694
647387
 YDOT =      -1577
197448  feet/sec       YDOT =        -480
729782  meter/sec
 ZDOT =      15248
700772                 ZDOT =        4647
803995


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15343
53325524  
00016717  00000-0  10270-3 0  9079
2 25544  51
6409 288
9793 0008225 258
9066 101
1162 15
54623793 15324


Satellite: ISS
Catalog Number: 25544
Epoch time:      15343
53325524   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       288
9793  deg
Eccentricity:     
0008225     
Arg of perigee:   258
9066  deg
Mean anomaly:     101
1162  deg
Mean motion:   15
54623793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1532
Checksum:              317


Coasting Arc #9 (Orbit 1546)
---------------------------------------

Vector Time (GMT): 2015/344/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4359281
07                 A    =         6778935
10  meter
 Y    =        2483224
61  meter          E    =           
0002932
 Z    =       -4561519
37                 I    =           51
27605
 XDOT =       -814
542545                 Wp   =           29
13204
 YDOT =      -6995
507423  meter/sec      RA   =          283
52568  deg
 ZDOT =      -3028
129677                 TA   =          210
44180
                                          MA   =          210
45883
                                          Ha   =            217
947  n
mi
                                          Hp   =            217
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14302103
25                 X    =        -4364566
70
 Y    =        8147062
37  feet           Y    =         2434447
10  meter
 Z    =      -14965614
74                 Z    =        -4582708
78
 XDOT =      -2672
383677                 XDOT =        -721
546841
 YDOT =     -22951
139839  feet/sec       YDOT =       -7004
095939  meter/sec
 ZDOT =      -9934
808651                 ZDOT =       -3031
861347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2624041
58                 X    =         -799807
87
 Y    =      -16164036
63  feet           Y    =        -4926798
36  meter
 Z    =      -15057646
98                 Z    =        -4589570
80
 XDOT =      21222
805474                 XDOT =        6468
711109
 YDOT =       5828
383701  feet/sec       YDOT =        1776
491352  meter/sec
 ZDOT =      -9949
535293                 ZDOT =       -3032
618357


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15344
49748736  
00016717  00000-0  10270-3 0  9080
2 25544  51
6413 284
1684 0008123 263
6167  96
4061 15
54630390 15479


Satellite: ISS
Catalog Number: 25544
Epoch time:      15344
49748736   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       284
1684  deg
Eccentricity:     
0008123     
Arg of perigee:   263
6167  deg
Mean anomaly:      96
4061  deg
Mean motion:   15
54630390  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1547
Checksum:              323


Coasting Arc #10 (Orbit 1562)
---------------------------------------

Vector Time (GMT): 2015/345/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4306214
68                 A    =         6776105
20  meter
 Y    =        -544847
68  meter          E    =           
0005692
 Z    =        5208238
45                 I    =           51
26102
 XDOT =       -294
041161                 Wp   =          244
97418
 YDOT =       7589
524730  meter/sec      RA   =          278
49877  deg
 ZDOT =       1035
601072                 TA   =          195
04326
                                          MA   =          195
06020
                                          Ha   =            218
003  n
mi
                                          Hp   =            217
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14128000
91                 X    =         4286687
37
 Y    =       -1787557
99  feet           Y    =         -496802
43  meter
 Z    =       17087396
47                 Z    =         5229109
89
 XDOT =       -964
701972                 XDOT =        -383
917835
 YDOT =      24900
015520  feet/sec       YDOT =        7585
733937  meter/sec
 ZDOT =       3397
641312                 ZDOT =        1033
955103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3025615
77                 X    =         -922207
69
 Y    =       13803915
79  feet           Y    =         4207433
53  meter
 Z    =       17177673
00                 Z    =         5235754
73
 XDOT =     -22116
284601                 XDOT =       -6741
043546
 YDOT =      -9070
881179  feet/sec       YDOT =       -2764
804583  meter/sec
 ZDOT =       3389
027876                 ZDOT =        1032
975697


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15345
52598079  
00016717  00000-0  10270-3 0  9099
2 25544  51
6419 279
0378 0008272 267
2765  92
7441 15
54678136 15636


Satellite: ISS
Catalog Number: 25544
Epoch time:      15345
52598079   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       279
0378  deg
Eccentricity:     
0008272     
Arg of perigee:   267
2765  deg
Mean anomaly:      92
7441  deg
Mean motion:   15
54678136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1563
Checksum:              349


Coasting Arc #11 (Orbit 1577)
---------------------------------------

Vector Time (GMT): 2015/346/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4088104
53                 A    =         6776159
48  meter
 Y    =       -1495715
88  meter          E    =           
0006206
 Z    =       -5198372
46                 I    =           51
25733
 XDOT =       1334
864489                 Wp   =          108
24514
 YDOT =      -7467
538418  meter/sec      RA   =          273
46551  deg
 ZDOT =       1098
026318                 TA   =          172
34295
                                          MA   =          172
33346
                                          Ha   =            217
163  n
mi
                                          Hp   =            216
679

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13412416
43                 X    =        -4045823
38
 Y    =       -4907204
32  feet           Y    =        -1541194
83  meter
 Z    =      -17055027
75                 Z    =        -5218129
22
 XDOT =       4379
476670                 XDOT =        1412
935300
 YDOT =     -24499
797959  feet/sec       YDOT =       -7452
174673  meter/sec
 ZDOT =       3602
448549                 ZDOT =        1104
699737

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8902781
80                 X    =         2713567
89
 Y    =      -11036541
15  feet           Y    =        -3363937
74  meter
 Z    =      -17140092
65                 Z    =        -5224300
24
 XDOT =      21017
675105                 XDOT =        6406
187372
 YDOT =      11308
239877  feet/sec       YDOT =        3446
751515  meter/sec
 ZDOT =       3632
747636                 ZDOT =        1107
261480


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15346
49017752  
00016717  00000-0  10270-3 0  9102
2 25544  51
6418 274
2266 0008199 271
1607  88
8607 15
54677162 15789


Satellite: ISS
Catalog Number: 25544
Epoch time:      15346
49017752   =   yrday
fracday
Element set:     910
Inclination:       51
6418  deg
RA of node:       274
2266  deg
Eccentricity:     
0008199     
Arg of perigee:   271
1607  deg
Mean anomaly:      88
8607  deg
Mean motion:   15
54677162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1578
Checksum:              335


Coasting Arc #12 (Orbit 1593)
---------------------------------------

Vector Time (GMT): 2015/347/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3720933
83                 A    =         6778898
66  meter
 Y    =        3418986
65  meter          E    =           
0004068
 Z    =        4520918
08                 I    =           51
26595
 XDOT =      -2308
708230                 Wp   =          358
81580
 YDOT =       6619
759657  meter/sec      RA   =          268
43795  deg
 ZDOT =      -3102
129274                 TA   =          122
45069
                                          MA   =          122
41135
                                          Ha   =            218
039  n
mi
                                          Hp   =            217
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12207788
16                 X    =         3660464
40
 Y    =       11217147
82  feet           Y    =         3460258
05  meter
 Z    =       14832408
39                 Z    =         4538847
12
 XDOT =      -7574
502068                 XDOT =       -2367
491431
 YDOT =      21718
371577  feet/sec       YDOT =        6593
613781  meter/sec
 ZDOT =     -10177
589480                 ZDOT =       -3113
486674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14363299
63                 X    =        -4377933
73
 Y    =        8140386
24  feet           Y    =         2481189
73  meter
 Z    =       14909210
95                 Z    =         4544327
50
 XDOT =     -17824
202864                 XDOT =       -5432
817033
 YDOT =     -12693
696207  feet/sec       YDOT =       -3869
038604  meter/sec
 ZDOT =     -10227
950557                 ZDOT =       -3117
479330


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15347
51863501  
00016717  00000-0  10270-3 0  9118
2 25544  51
6420 269
0960 0008164 274
7476  85
2744 15
54703392 15946


Satellite: ISS
Catalog Number: 25544
Epoch time:      15347
51863501   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:       269
0960  deg
Eccentricity:     
0008164     
Arg of perigee:   274
7476  deg
Mean anomaly:      85
2744  deg
Mean motion:   15
54703392  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1594
Checksum:              318


Coasting Arc #13 (Orbit 1608)
---------------------------------------

Vector Time (GMT): 2015/348/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3205945
61                 A    =         6783012
32  meter
 Y    =       -5009257
67  meter          E    =           
0003920
 Z    =       -3256689
29                 I    =           51
28146
 XDOT =       3213
648135                 Wp   =          296
22965
 YDOT =      -5123
614552  meter/sec      RA   =          263
42017  deg
 ZDOT =       4714
561895                 TA   =           25
77617
                                          MA   =           25
75664
                                          Ha   =            218
134  n
mi
                                          Hp   =            217
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10518194
25                 X    =        -3133872
86
 Y    =      -16434572
40  feet           Y    =        -5044705
40  meter
 Z    =      -10684676
16                 Z    =        -3272088
49
 XDOT =      10543
465010                 XDOT =        3247
801303
 YDOT =     -16809
759030  feet/sec       YDOT =       -5087
486868  meter/sec
 ZDOT =      15467
722752                 ZDOT =        4730
255632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18742067
27                 X    =         5712582
10
 Y    =       -5296870
78  feet           Y    =        -1614486
21  meter
 Z    =      -10750253
92                 Z    =        -3276677
39
 XDOT =      12720
546995                 XDOT =        3877
222724
 YDOT =      13459
341467  feet/sec       YDOT =        4102
407279  meter/sec
 ZDOT =      15536
523688                 ZDOT =        4735
532420


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15348
48279613  
00016717  00000-0  10270-3 0  9121
2 25544  51
6417 264
2847 0008226 278
5309  81
4912 15
54733812 16091


Satellite: ISS
Catalog Number: 25544
Epoch time:      15348
48279613   =   yrday
fracday
Element set:     912
Inclination:       51
6417  deg
RA of node:       264
2847  deg
Eccentricity:     
0008226     
Arg of perigee:   278
5309  deg
Mean anomaly:      81
4912  deg
Mean motion:   15
54733812  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1609
Checksum:              326


Coasting Arc #14 (Orbit 1624)
---------------------------------------

Vector Time (GMT): 2015/349/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2524216
30                 A    =         6786449
80  meter
 Y    =        6099614
08  meter          E    =           
0006396
 Z    =        1557556
24                 I    =           51
29801
 XDOT =      -4035
190040                 Wp   =          136
91318
 YDOT =       3132
628158  meter/sec      RA   =          258
41560  deg
 ZDOT =      -5718
938711                 TA   =           25
97374
                                          MA   =           25
94166
                                          Ha   =            218
463  n
mi
                                          Hp   =            217
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8281549
56                 X    =         2448255
34
 Y    =       20011857
23  feet           Y    =         6127416
70  meter
 Z    =        5110092
64                 Z    =         1569634
27
 XDOT =     -13238
812467                 XDOT =       -4042
139648
 YDOT =      10277
651438  feet/sec       YDOT =        3087
465562  meter/sec
 ZDOT =     -18762
922280                 ZDOT =       -5738
557422

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21496962
11                 X    =        -6552274
05
 Y    =        2532770
81  feet           Y    =          771988
54  meter
 Z    =        5161126
96                 Z    =         1573111
50
 XDOT =      -6163
125961                 XDOT =       -1878
520793
 YDOT =     -13839
893151  feet/sec       YDOT =       -4218
399432  meter/sec
 ZDOT =     -18848
299622                 ZDOT =       -5744
961725


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15349
51121721  
00016717  00000-0  10270-3 0  9133
2 25544  51
6420 259
1531 0008170 282
2466  77
7772 15
54757890 16254


Satellite: ISS
Catalog Number: 25544
Epoch time:      15349
51121721   =   yrday
fracday
Element set:     913
Inclination:       51
6420  deg
RA of node:       259
1531  deg
Eccentricity:     
0008170     
Arg of perigee:   282
2466  deg
Mean anomaly:      77
7772  deg
Mean motion:   15
54757890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1625
Checksum:              311


Coasting Arc #15 (Orbit 1640)
---------------------------------------

Vector Time (GMT): 2015/350/11:25:26
438
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1660332
03                 A    =         6787393
47  meter
 Y    =       -6564196
07  meter          E    =           
0010829
 Z    =         352165
68                 I    =           51
30820
 XDOT =       4732
000839                 Wp   =            8
99622
 YDOT =       -875
596962  meter/sec      RA   =          253
41800  deg
 ZDOT =       5974
522824                 TA   =          354
81947
                                          MA   =          354
83066
                                          Ha   =            218
634  n
mi
                                          Hp   =            216
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5447283
55                 X    =        -1588516
85
 Y    =      -21536076
36  feet           Y    =        -6582361
48  meter
 Z    =        1155399
21                 Z    =          344274
21
 XDOT =      15524
937137                 XDOT =        4712
418479
 YDOT =      -2872
693444  feet/sec       YDOT =        -822
790437  meter/sec
 ZDOT =      19601
452836                 ZDOT =        5997
462208

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22215206
17                 X    =         6771194
84
 Y    =         187018
69  feet           Y    =           57003
30  meter
 Z    =        1122528
05                 Z    =          342146
55
 XDOT =      -1115
825059                 XDOT =        -340
103478
 YDOT =      14003
662344  feet/sec       YDOT =        4268
316282  meter/sec
 ZDOT =      19700
755887                 ZDOT =        6004
790394


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   15350
53961997  
00016717  00000-0  10270-3 0  9145
2 25544  51
6415 254
0207 0008231 286
6033  73
4216 15
54778714 16410


Satellite: ISS
Catalog Number: 25544
Epoch time:      15350
53961997   =   yrday
fracday
Element set:     914
Inclination:       51
6415  deg
RA of node:       254
0207  deg
Eccentricity:     
0008231     
Arg of perigee:   286
6033  deg
Mean anomaly:      73
4216  deg
Mean motion:   15
54778714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1641
Checksum:              309
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